20030409000632003040900063SO 2003 4 9 2003FA0000324 220011116G8520SA639193 BUSHING CONT A50 A502 17002SO CRANK C/WEIGHT MISMANUFACTURED B JZYRO OTHER W INADEQUATE Q C NRNOT REPORTED 1 NM09 WHILE CHECKING THE SIZE OF THE NEW MFG SA639193 BUSHINGS PRIOR TO INSTALLATION IN THE COUNTERWEIGHTS I FOUND TWO NEW STANDARD SIZE BUSHINGS THAT WERE APPROXIMATELY .002 SMALL IN THE OUTER DIAMETER. 3 O E190 20030507001582003050700158CE 2003 5 7 2003FA0000400 120010816G323012416308 BUMPER BLOCK CESSNA210 P210N 2073454CE CONT O520 TSIO520* 17040SO MLG DEBONDED B SMTRO OTHER O OTHER NRNOT REPORTED 1 EA175555S136 P21000417 LT AND RT MAIN LANDING GEAR SHELL BUMPER DEBONDS. THE BUMPER EDGES CURL OVER PREVENTING MAIN GEAR STRUT FROM MAKING FULL DOWN TRAVEL. THIS CONDITION PREVENTS MAIN GEAR STRUT FROM CONTACTING DOWNLOCKS AND PROPER DOWNLOCK SWITCH ACTUATION, THEREFORE, AN UNSAFE CONDITION IT APPEARS THAT MFG MAY HAVE CHANGED THE COMPOSITION OF THE SHELL BUMPER MATERIAL WHICH DOES NOT HAVE GOOD BONDING QUALITIES. (PHOTO) 1H71 3O3 O 3A21 E8CE 20010326003272001032600327CE 2001 3 26 20010222CW001 120010125G7602S12345 LEVER CESSNA177 177B 2073708CE LYC O360 O360* 41514EA PANEL BROKEN D K NONE O OTHER ININSP/MAINT 1 SW01160213292 17702479 MIXTURE CONTROL BROKE ON GROUND RUN UP. BREAK APPEARS TO BE DEFECT IN MATERIAL. 1H71 3O3 O A13CE E286 20010326003282001032600328EA 2001 3 26 20010215CW003 220010116G8530AEL6510212 CYLINDER PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA HEAD UNSERVICEABLE B MW2RK NONE O OTHER ININSP/MAINT 1 GL174350G1081 288490058 L2749236A A CRACK RUNS FROM TOP SPARKPLUG HOLE AROUND OUTSIDE EXHAUST SEAT TO TOP SPARKPLUG AND CYLINDER WILL SPLIT IN TWO PIECES. 1L71 3O3 O 2A13 E286 20010326003292001032600329EU 2001 3 26 20010222CW003 120010118G79203033356 FUEL FILTER PILATSPC12 PC1245 EU PWA PT6 PT6A66 52043NE DISCHG FUEL FLTRUNBONDED G K NONE O OTHER ININSP/MAINT 1 CE05302PB 302 UPON 100 HOUR INSPECTION, REPLACEMENT OF ENGINE DISCHARGE FUEL FILTER. NEW FILTER FROM 100 HR KIT WAS NOT GLUED TOGETHER. THE TOP AND BOTTOM OF FILTER WERE LOOSE AND COULD BE PULLED OFF. 1L71 3T4 TRTA78EU E26NE 20010326004302001032600430SW 2001 3 26 E27R730 120010122G53003107041 CHANNEL GULSTM690TP 690A 0141722SW GARRTTTPE331TPE331* 01514WP LT & RT FAILED B E27RK NONE O OTHER ININSP/MAINT 1 WP07921ST10545 11200 DURING PRESSURIZATION LEAK CHECKS, THE CABIN WAS FOUND TO HAVE TWO LARGE LEAKS IN THE LEFT AND RIGHT WING ROOT AREA. ON EXAMINATION OF THE SUSPECT AREAS IT WAS FOUND THAT THE LEFT AND RIGHT SUPPORT CHANNELS PN 3107041 & 3107042 HAD FAILED FROM FS 144 WL TO FS 175 WL 14, THE FAILURE ALLOWED THE AIRCRAFT SKIN TO PULL AWAY FROM ITS SUPPORTING STRUCTURE ABOVE THE PICTURE WINDOWS IN EXCESS OF .25. 1H72 3T3 T 2A4 E2WE 20010326004312001032600431WP 2001 3 26 E27R7302 220010122G72103103435 GEAR GULSTM690TP 690A 0141722SW GARRTTTPE331TPE33110 01514WP BULL GEAR FAILED B E27RO OTHER O OTHER CRCRUISE 1 WP0748AZ 6991 1612 11307 P79291C BULL GEAR FOUND TO HAVE SHED APPROX 6 IN OF TEETH IN 2 SEGMENTS CAUSING EXTENSIVE DAMAGE TO GEAR BOX COMPONENTS AND CASE. WHICH RESULTED IN AN IN FLIGHT SHUTDOWN. 1H72 3T4 T 2A4 E4WE 20010326004952001032600495NM 2001 3 26 AU010148 120010217G2910DSC252A40230 PIPE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC, MAIN LEAKING W K NONE OK OTHER FLUID LOSS ININSP/MAINT 1 AUS (AUS) HYDRAULIC LINE LOCATED IN RH WHEEL BAY CONTAINED A PINHOLE LEAK. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010327002052001032700205SO 2001 3 27 CA010213006 220010126G8530 CYLINDER HEAD CONT 642344 CESSNA421 421B 2076014CE CONT O520 GTSIO520H 17032SO MCAULY3AF34C3AF34C92 GL SP PLUG-INJECTR CRACKED W O OTHER O OTHER ININSP/MAINT 1 CA 100 (CAN) AT 100 HOUR INSPECTION IN NOVEMBER 2000, FOUND FOUR CYLINDERS WITH SIMILAR CRACKS. AT NEXT 100 HOUR INSPECTION IN JANUARY 2001 FOUND SIX MORE CYLINDERS WITH CRACKS IN SAME LOCATION (BETWEEN SPARK PLUG HOLE AND INJECTOR HOLE). CYLINDERS REPLACED AFTER DETECTING CRACKS. PAST EXPERIENCE SHOWS THAT CRACKS ARE VERY COMMON IN THIS AREA.2001-02-15 TC: PART #S, TSN, ADDITIONAL CONTRIBUTING FACTORS WERE NOT GIVEN. 1L72 3O3 O A7CE E7CE 5 CP22EA 20010327002062001032700206SO 2001 3 27 CA010213008 120010122G52804752932 HINGE PIPER PA31 PIPER PA31 PA31 7103102SO LYC O540 TIO540A2C 41532EA IN RADIUS CRACKED W O OTHER O OTHER ININSP/MAINT 1 CA 317712043 (CAN) DURING INSPECTION AS PER AIRWORTHINESS DIRECTIVE 200-25-01,(2)TWO GEAR DOOR HINGES FOUND CRACKED. HINGES REPLACED. 1L72 3O3 O A20SO E14EA 20010327002072001032700207EA 2001 3 27 CA010213009 120010124G2701C2CF834A CONTROL COLUMN DHAV DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE AT WELD CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 15576 497 (CAN) COMPLETED INSPECTION AS PER SB 2/28 AND AD CF-84-01R1, FOUND CRACK IN WELD. 128 HOURS SINCE LAST INSPECTION.SUBMITTER FEELS LACK OF MAINTENANCE MAY BE RESPONSIBLE FOR THIS CRACK BEING NOTED EARLY. 1H71 3R3 R A806 5E1 20010327002092001032700209EA 2001 3 27 CA010213018 120010125G2760 ACTUATOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE ACTUATOR LUG BROKEN W O OTHER F FLT CONT AFFECTED APAPPROACH 1 CA (CAN) ON APPROACH, AT LAST FLP SELECTION, A/C ROLLED TO THE RIGHT FOLLOWED BY FLT SPLR DEPLOY CAUTION MESSAGE.CREW DECLARED EMERGENCY AND LANDED WITHOUT ANY FURTHER EVENT. MAINTENANCE FOUND FLIGHT SPOILER PANEL ACTUATOR LUG BROKEN. PANEL REPLACED. AIRCRAFT RETURNED TO SERVICE. AD IN PROGRESS 2L72 4F4 FRTA21EA E15NE 20010327002102001032700210EA 2001 3 27 CA010213019 120010124G2611 SMOKE DETECTOR CNDAIRCL600 CL6002B19 EA GE CF34 CF341A NE LAV SMOKE DETCTRFAULTY W O OTHER N FALSE WARNING APAPPROACH 1 CA (CAN) ON SHORT FINAL, SMOKE TOILET CAUTION MESSAGE CAME ON. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT ANY FURTHER EVENT.LAV SMOKE DETECTOR FOUND FAULTY & REPLACED. 2L72 4F4 FRTA21EA E15NE 20010327002112001032700211EA 2001 3 27 CA010213021 120010124G2740 STABILIZER CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE HORIZ STAB FAILED W O OTHER F FLT CONT AFFECTED CLCLIMB 1 CA (CAN) ON CLIMBOUT, STAB AND MACH TRIM DISENGAGED AT 8.2 UNITS AT NOSE UP TRIM. WOULD NOT RE-ENGAGE. AIRCRAFT PERFORMED A FLAP 20 DEGREES PER QRH WITHOUT ANY FURTHER EVENT. MAINTENANCE REPLACED THE HORIZONTAL STAB TRIM PANEL AND RETURNED AIRCRAFT TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010327002122001032700212EA 2001 3 27 CA010213023 120010125G5610 WINDSHIELD CNDAIR CL6002B19 CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE F/O WINDSHIELD CRACKED W A UNSCHED LANDING D INFLIGHT SEPARATION CRCRUISE 1 CA 7037 (CAN) IN CRUISE FLIGHT, F/O WINDSHIELD SHATTERED. NO INFO ON ALTITUDE OR IF EMERGENCY WAS DECLARED. AIRCRAFT RETURNED INTO SERVICE AFTER WINDSHIELD REPLACEMENT. 2L72 4F4 FRTA21EA E15NE 20010327002132001032700213EA 2001 3 27 CA010213024 120010117G5610NP1393219 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE L/H WINDSHIELD CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA 00201H3495 (CAN) DURING TAXI, CAPTAIN WINDSHIELD CRACKED.AIRCRAFT RETURNED INTO SERVICE AFTER WINDSHIELD REPLACEMENT. 2L72 4F4 FRTA21EA E15NE 20010327002142001032700214EA 2001 3 27 CA010213025 120010113G5610NP1393216 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE R/H WINDSHIELD CRACKED W O OTHER O OTHER CLCLIMB 1 CA 99298H2154 (CAN) CREW RPORTED THAT PASSING FLT 160 AT A DIFFERENTIAL CABIN PRESSURE 6,4, R/H WINDSHIELD CRACKED. NO INFO IF EMERGENCY WAS DECLARED.AIRCRAFT RETURNED INTO SERVICE AFTER WINDSHIELD REPLACEMENT. 2L72 4F4 FRTA21EA E15NE 20010327002152001032700215EA 2001 3 27 CA010213028 120010130G7800NAS6303U4 BOLT GE CF343B1 CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE DELTA BRCKET POSSHEARED W O OTHER O OTHER ININSP/MAINT 1 CA 3100 (CAN) MAINTENANCE FOUND THE L/H EXHAUST NOZZLE CRACKED DURING A CHECK INSPECTION. DURING REPLACEMENT OF THE EXHAUST NOZZLE, MAINTENANCE FOUND TWO (OUT OF THREE) DELTA BRACKETS ATTACH BOLTS SHEARED, AT 2 AND 10 OCLOCK POSITION.FAULTY PARTS REPLACED PER AMM. 2L72 4F4 FRTA21EA E15NE 20010327002162001032700216EA 2001 3 27 CA010213032 120010129G5610 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE L/H WINDSHIELD CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) DURING CUSTOMER ACCEPTANCE FLIGHT, IN CRUISE, L/H WINDSHIELD CRACKED. L/H WINDSHIELD REMOVED AND REPLACED. 2L72 4F4 FRTA21EA E15NE 20010327002312001032700231SO 2001 3 27 20010301CW009 120010301G7920CH48110 OIL FILTER PIPER PA38 PA38112 7103812SO LYC O320 O320* 41508EA OIL SUMP FLAKING G K NONE O OTHER ININSP/MAINT 1 EA232602B 3879A0146 FOUND SEALANT MATERIAL IN OIL SUMP DURING NORMAL 50 HR OIL CHANGE. FOUND ON SUCTION SCREEN. SEALANT CAME FROM THE OIL FILTER. AREA THAT SEALS THE INLET TO THE OUTLET AREA OF THE FILTER IS FLAKING OFF AND GETTING STUCK IN THE FILTER AND ON THE OIL SUCTION SCREEN. 1L71 3O3 O A18SO E274 20010327002322001032700232SO 2001 3 27 20010301CW010 120010301G7920CH48110 OIL FILTER PIPER PA38 PA38112 7103812SO LYC O235 O235* 41505EA OIL SUMP DEFECTIVE G K NONE O OTHER ININSP/MAINT 1 EA232596E 3878A0483 SEALANT USED IN MANUFACTURE OF FILTER TO SEAL THE INLET AND OUTLET TO THE FILTER APPEARS TO BE FLAKING OFF. PIECES ARE BEING FOUND INSIDE THE FILTER ON THE PLEATS AND ON THE OIL SUMP SUCTION SCREEN. THESE PIECES COULD GET INTO THE PRESSURE SYSTEM AND STARVE A BEARING FOR OIL. 1L71 3O3 O A18SO E223 20010327004172001032700417NM 2001 3 27 AU010151 120010109G528028489 DOOR BOEING 737400 BOEING757 757* NM CFMINTCFM56 CFM563C 13802EU LANDING GEAR DOOCRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 10341 28489 (AUS) RT MAIN LANDING GEAR STRUT DOOR CRACKED THROUGH LOWER ATTACHMENT BOLT HOLDER. 2L72 4F4 FRTA2NM E21EU 20010327004182001032700418SO 2001 3 27 AU010152 120010213G3242RFS1015 DISK BFGOODRICH 214791 EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE BRAKE BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS 0671 (AUS) BRAKE ROTATING DISC (CARRIER AND LINING ASSEMBLY) BROKEN. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010327004192001032700419SO 2001 3 27 AU010153 120010213G5330120056 SKIN EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) SKIN SURROUNDING THE COPILOTS WINDOW FRAME CRACKED. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010327004202001032700420NM 2001 3 27 AU010154 120010202G57536546435274SP SKIN BOEING737 7374Q8 NM CFMINTCFM56 CFM563C 13802EU TE FLAPS DELAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT AFT OUTER FLAP TRAILING EDGE DELAMINATING AT INBOARD AFT CORNER. 2L72 4F4 FRTA16WE E21EU 20010327004212001032700421CE 2001 3 27 AU010157 120010202G2410646655 GEAR CESSNA ALTERNATOR CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL DC GENERATOR-ALTDAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 185 EO030305377 (AUS) LH ENGINE ALTERNATOR DRIVE GEAR DAMAGED AND OUTER SHELL DISTORTED. EVIDENCE OF VICE MARKS ON OUTSIDE OF SHELL. FURTHERDAMAGE FOUND:-1. OIL SEAL INSTALLED BACKWARDS.2. SUPPRESSOR CAPACITOR LOOSE INSIDE OF ALTERNATOR AND SCREW LOOSE. 3. PITTING IN CASE HARDENING ON THE SLIP RING END OF THE ROTOR SHAFT. 4. STATOR CORE LAMINATIONS BADLY DISTORTED RENDERING CORE UNSERVICEABLE. THE ROTOR IN ALTERNATOR AT TIME OF STRIP DOWN INSPECTION SHOWED NO SIGNS OF CONTACT WITH STATOR POLES.PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010327004222001032700422CE 2001 3 27 AU010158 120010222G528008411066 BRACKET CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL LANDING GEAR DR BROKEN W K NONE OD OTHER INFLIGHT SEPARATION LDLANDING 1 AUS 5203 (AUS) LH MAIN LANDING GEAR DOOR BRACKET FAILED. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010330000662001033000066NM 2001 3 30 CA010129018 120010104G275065162266 SWITCH BOEING727 72722 1384002NM PWA JT8 JT8D7B 52053NE KRUGER FLAP FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) AFTER DEPARTER&UPON FLAP RETRACTION, NR 5 LEADING EDGE FLAP IN TRANSIT LIGHT ILLUMINATED. FUEL DUMPED & A/C RETURNED TO AIRPORT OF DEPTR: MAINT CHANGED OUT FLAP SWITCH, P/N 40174 & SYS TESTED & FUNCTIONED NORMALLY. A/C DEPARTED & SAME FAULT RECURRED. MAINT REPL NR 5 LEADING EDGE FLAP ACTUATOR, P/N 65-17818-20 & LEADING EDGE POS CNTL MODEL, P/N 65-60212-11, AS PRECAUTIONARY MEASURE: SYS AGAIN TESTED AS PER THE MM& OPALLY CHECKED SEVERAL TIMES W/O FAULT. A/C RT-SRV. DISCREPANCY RETURNED ON NEXT DEPTR: A/C RETURNED AGAIN FOR MAINT TROUBLESHOOTING. FINAL RPT: L/E FLAP POS SWITCHES SWAPP ED BETWEEN 5 & 3 FLAP. WIRING FROM COCKPIT T 2L73 4F4 F A3WE E2EA 20010330000692001033000069EA 2001 3 30 CA010130011 220010105G7200 ENGINE DHAV DHC6 DHC6 2802606EA PWA PT6 PT6A27 52043EA RIGHT FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) RT ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE. AFTER REACHING CRUISING ALTERNATE RT ENGINE LOW OIL PRESSURE CAPTION APPEARED. LOW OIL PRESSURE GAUGE INDICATION OBSERVED. PRECAUTIONARY ENGINE SHUT DOWN. DIVERTED BACK TO AIRFIELD. 1H72 3T4 TRTA9EA E4EA 20010330000702001033000070NM 2001 3 30 CA010130012 120010101G304007802 WINDSHIELD DHAV DHC8 DHC8102 2809003NM PWA 120 PW120 NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA 10554 (CAN) LEFT WINDSHIELD SHATTERED INFLIGHT. AIRCRAFT LANDED. WINDSHIELD REPLACED IN ACCORDANCE WITH DHC8 MM 56-10-11. RAN AIRCRAFT OPERATIONS CHECKED, OK. AIRCRAFT RETURNED TO SERVICE. NOTE PCA A0101001 2H72 4T4 TRTA13NM E20NE 20010330000712001033000071GL 2001 3 30 CA010131009 120010101G7160653885 FLANGE DIAMONDA20 DA20C1 2990001GL CONT O240 IO240B 17063SO SNSNCHW69EK W69EK63 EA INTAKE PIPE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 569 (CAN) FLANGE CRACKED. 1L71 3O3 ONTTA4CH E7SO 5 NTA4CH 20010330000722001033000072EA 2001 3 30 CA010131015 120010105G5753F35 SEALANT DHAV DHAV DHC7 DHC7103 2802710EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL UNDER NR 4 FLAP PEELING W K NONE O OTHER ININSP/MAINT 1 CA 10482 (CAN) THE SEALANT USED UNDER THE NR 4 FLAP TRACK AS PER AD CF-87-04, SB 7-57-30 WAS FOUND PEELING OFF. 10481.68 HOURS HAVE ACCUMULATED ON THIS AIRCRAFT AFTER INITIAL APPLICATION BACK IN OCTOBER OF 1987. THIS AIRCRAFT HAS BEEN OPERATING IN ASIA. 2H74 4T4 T A20EA E4EA 6 CP1NE 20010330000732001033000073SO 2001 3 30 CA010131016 120010105G812046C1983985 TURBOCHARGER PIPER PA46 PA46350P SO LYC O540 TIO540AE2A 41532EA ENGINE FAILED W O OTHER O OTHER CRCRUISE 1 CA 159 (CAN) PILOT REPORTED LOSS IN MANIFOLD PRESSURE FOUND TURBOCHARGER TURBINE MISSING A BLADE AND TURBO SEIZED. 1L71 3O3 ORTA25SO E14EA 20010330000752001033000075CE 2001 3 30 CA010131018 120010110G551112326194 RIB CESSNA 183260029 CESSNA210 T210M 2073451CE CONT O520 TSIO520R 17040SO MCAULYD3A34 D3A34C402 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A 50 HOUR INSPECTION OF THE HORIZONTAL STAB, THE 4 RIBS WERE FOUND TO BE LOOSE & CRACKED. THIS IS DONE BY SQUEEZING THE NOSE RIBS (WITH A MODERATE AMOUNT OF PRESSURE) AND LISTEN FOR CLICKING SOUNDS & FEELING OF LOOSE RIVETS. THEREFORE, THE LOWER SKIN WAS PEELED BACK THE 4 RIBS WERE REMOVED AND REPLACED WITH NEW RIBS. THE SKIN WAS RIVETED BACK ON. STAB WAS INSTALLED AND AIRCRAFT WAS RETUNED TO SERVICE. 7 B&C S.D. FOUND DUING 50 HOUR INSPECTION. NO ACTION REQUIED BY FLIGHT CREW. 1H71 3O3 O 3A21 E8CE 5 CP47GL 20010330000852001033000085EA 2001 3 30 CA010202005 120010107G3244256K433 TIRE 60085123 CNDAIRCL601 CL6012A12 1900303EA GE CF34 CF341A NE MLG FAILED W O OTHER O OTHER TOTAKEOFF 1 CA 249 (CAN) ON TAKEOFF CREW HEARD MUFFLED BANG. NO AIRCRAFT CONTROL PROBLEMS NOTED. CONTINUED TO DESTINATION LANDED WITHOUT INCIDENT. DURIG POST FLIGHT FOUND THE NR 3 TIRE HAD LOST ALL TREAD. THE TIRE WAS STILL INFLATED. DAMAGE TO RIGHT INBOARD FLAPS LOWER SURFACE AND THE RIGHT MAIN LANDING GEAR INBOARD WEIGHT ON WHEEL ANTI-SKID HARNESS. 2L72 4F4 FRTA21AE E15NE 20010330000872001033000087EA 2001 3 30 CA010202008 120010103G5610 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) THE CREW REPORTED THAT THE CAPTS FRONT WINDSHIELD SHATTERED IN CRUISE. THE LANDING WAS UNEVENTFUL.THE MAINTENANCE REPLACED THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010330000882001033000088EA 2001 3 30 CA010202011 120010103G2752 ACTUATOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE RT FLAP FAILED W O OTHER J WARNING INDICATION APAPPROACH 1 CA (CAN) THE CREW REPORTED THE FLAP FAIL CAUTION MESSAGE WHICH APPEARED ON APPROACH (SELECTIION OF 45 DEGREES, STOPPED AT 37). THE MAINTENANCE REPLACED THE RT OUTBOARD FLAP INBOARD ACTUATOR 2L72 4F4 FRTA21EA E15NE 20010330000892001033000089EA 2001 3 30 CA010202013 120010106G261247259701 FIRE DETECTOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NR 1 ENGINE FAILED W O OTHER N FALSE WARNING DEDESCENT 1 CA (CAN) DURING DESCENT INTO MEMPHIS, THE CREW ON AIRCRAFT 7416 SHUT DOWN ENGINE NR 1 PER THE EMERGENCY PROCEDURES DUE TO THE POSTING OF AN INTERMITTENT LT ENGINE FIRE MESSAGE ON THE EICAS. DURING TROUBLESHOOTING THE MECHANICS FOUND THE FIRE DETECTION UNIT UNDER THE LT CONSOLE SHORTED AND CONTAMINATED (COFFEE) WITH LIQUID. A NEW CONTROLLER AND BOTTLE WAS INSTALLED AND THE SYSTEM SUCCESSFULLY TESTED PER THE AMM. 2L72 4F4 FRTA21EA E15NE 20010330000902001033000090NE 2001 3 30 CA010202022 220010107G7210 GEARBOX CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 ENGINE FAILED W EA ENGINE SHUTDOWN UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION NRNOT REPORTED 1 CA (CAN) NR 2 ENGINE VIBRATION FLUCTUATION INDICATED .4 TO .7 MILS APPROXIMITELY 3 TO 5 MIN. LATER, NR 2 ENGINE SHUT DOWN UNCOMMANDED. PERFORMED QRH PROCEDURE & DIVERTED INTO NEXT AIRPORT (ISO), THE FLIGHT CREW DECLARED EMERGENCY (UNEVENTFUL).FOUND METAL IN CHIP DETECTOR (SUSPECT GEARBOX - INTERNAL) NOT CONFIRMED. REPLACEMENT OF ENGINE S/N 807528 IN PROGRESS. 2L72 4F4 FRTA21EA E15NE 20010330000912001033000091EA 2001 3 30 CA010205006 120010111G3040NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA 1566 (CAN) THE CREW REPORTED THAT THE LT WINDSHIELD CORE PLY CRACKED DURING FLIGHT.THE MAINTENANCE REPLACED THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010330000922001033000092EA 2001 3 30 CA010205008 120010101G5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) THE CREW REPORTED THAT THE RT WINDSHIELD CARACKED IN FLIGHT. THE MAINTENANCE REPLACED THE RT WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010402000812001040200081NE 2001 4 2 AU010001 220010102G7310226311001 PIPE BAC 146 146100A 1500260EU LYC ALF502ALF502R5 41580NE ENGINE FUEL CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE FUEL PIPE FROM FLOW DIVIDED TO FUEL MANIFOLD CHAFED ON COMBUSTOR HOUSING. 2H74 4F4 FRTA49EU E6NE 20010402000822001040200082CE 2001 4 2 AU010002 120010103G32215842000211 TRUNNION CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO MCAULY3AF32C3AF32C87 GL NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR TRUNNION PINS CRACKED. FOUND DURING INSPECTION IAW CESSNA SB MEB88-5R2. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010402000832001040200083CE 2001 4 2 AU010003 120010102G323108411066 ARM CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL MLG DOOR CRACKED W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) RT MAIN LANDING GEAR INNER DOOR BELLCRANK IDLER ARM CRACKED. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010402000842001040200084 2001 4 2 AU010004 420010104G2211065006401 COMPUTER REIMS 406 F406 EU PWA PT6 PT6A112 52043NE MCAULY3G34C73GFR34C701 GL AUTOPILOT FAULTY W O OTHER BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 AUS 3823 (AUS) AUTOPILOT COMPUTER SUSPECT FAULTY. 1L72 3T3 TRTA54EU E4EA 5 CP60GL 20010402000852001040200085CE 2001 4 2 AU010006 120010103G554010164001419 FITTING BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCD4N3HCD4N3A GL RUDDER CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER CENTER HINGE ASSEMBLY ATTACHMENT FITTING CORRODED. 1L72 4T4 T A24CE E4EA 5 CSTC 20010402000862001040200086SO 2001 4 2 AU010007 120010106G3230 DOWNLOCK PIPER PA34 PA34200 7103405SO LYC O360 IO360C1E6 41514EA HARTZLHCC2Y HCC2YK2 GL MLG CONTAMINATED W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) LT MAIN LANDING GEAR DOWNLOCK ARM JAMMED BY A STONE PREVENTING LANDING GEAR FROM CORRECTLY LOCKING IN THE DOWN POSITION. 1L72 3O3 O A7SO 1E10 5 CP920 20010402000872001040200087SO 2001 4 2 AU010008 220010103G8530631996 RETAINER CESSNA172 R172K 2072431CE CONT O360 IO360HB 17025SO MCAULY2A34C 2A34C203 GL ENGINE CYLINDER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 3 CYLINDER ROCKER HAT REMOVED TO REPAIR OIL LEAK. THE ROCKER PIN RETAINER WAS FOUND TO CRACKED. ON FURTHER INSPECTION OTHER ROCKER PIN RETAINERS SHOWED SIGNS OF INCIPIENT FAILURE. 1H71 3O3 O 3A17 E1CE 5 CP3EA 20010402000882001040200088EU 2001 4 2 AU010009 220010104G73210164168190 FUEL CONTROL SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU NR 1 ENGINE MALFUNCTIONED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AUS (AUS) NR 1 ENGINE FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND THE PPNG OF THE FCU INTERNAL CIRCUIT TO BE OPEN CIRCUITED. 2G72 4U4 U H4EU E12NE 20010402000892001040200089WP 2001 4 2 AU010010 220010110G726131080801 PIPE SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL RT ENGINE OIL CHAFED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) RT ENGINE OIL PIPE LEAKING DUE TO CONTINUED CHAFING WITH ANOTHERPIPE. 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20010402000902001040200090 2001 4 2 AU010012 420010103G25657A146723 SLIDE BOEING747 747438 NM RROYCERB211 RB211524G19 NE PAX DOOR DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS 12456 (AUS) NR 4 LT MAIN DOOR ESCAPE SLIDE TORN. 2L74 4F4 FRTA20WE E30NE 20010402000912001040200091NM 2001 4 2 AU010013 120010109G2510 SEAT BACK BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU COCKPIT BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OBSERVERS SEAT BACK REST SEPARATED FROM SEAT BASE DUE TO A BROKEN BRACKET. 2L72 4F4 FRTA16WE E21EU 20010402000922001040200092NM 2001 4 2 AU010014 120010109G78301275084 ARM RROYCE RB211524G BOEING747 747438 NM RROYCERB211 RB211524G19 NE THRUST REVERSER DAMAGED W K NONE J WARNING INDICATION ININSP/MAINT 1 AUS 31016 (AUS) NR 2 ENGINE THRUST REVERSER COWL POSITION (TRCP) RESOLVER ARM DISCONNECTED AT ADJUSTMENT TURNBUCKLE AND ATTACHED BY ONLY ONE THREAD AT THE RESOLVER. SAFETY WASHER LOCKTABS PARTIALLY BENT AND RESOLVER APPEARS TO HAVE SUFFERED CONTACT DAMAGE. 2L74 4F4 FRTA20WE E30NE 20010402000932001040200093NM 2001 4 2 AU010015 120010109G2823737M28500011 VALVE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU FUEL SELECTOR FAILED W O OTHER O OTHER NRNOT REPORTED 1 AUS 3161 (AUS) NR 1 ENGINE FUEL SHUTOFF VALVE FAILED IN THE CLOSED POSITION. 2L72 4F4 FRTA16WE E21EU 20010402000942001040200094NM 2001 4 2 AU010016 120010110G3260841005 PSEU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG FAULTY W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) PROXIMITY SENSE ELECTRICAL UNIT (PSEU) FAULTY. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010402000952001040200095SO 2001 4 2 AU010017 120010109G79202W127984S190 HOSE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE OIL DETERIORATED W O OTHER KBJFLUID LOSS SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION LDLANDING 1 AUS (AUS) RT ENGINE TURBOCHARGER OIL RETURN HOSE DETERIORATED AND LEAKING.HOSE FAILED PRESSURE TESTING. THE HOSE HAD BEEN AFFECTED BY THE HEAT FROM THE TURBOCHARGER. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010402000972001040200097EU 2001 4 2 AU010018 120010111G2760 BUSHING FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU DRAG CONTROL CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) SPEED BRAKE CABLE INPUT QUADRANT CORRODED. THE FOLLOWING ITEMSWERE FOUND DETERIORATED: GROOVE OF PULLEY ASSEMBLY. WEB ADJACENT TO STOP PIN HOLE OF BRACKET. INTERNAL SPLINE OF LEVER. EXTERNAL SPLINE ON SHAFT AND BUSHING. BEARING AND FOUND CORRODED AND ROUGH TO ROTATE 2L72 4F4 FRTA20EU E2EU 20010402000982001040200098CE 2001 4 2 AU010019 120010104G323051420025 DRAG BRACE CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C87 GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR DRAG BRACE CRACKED IN AREA ADJACENT TO THE ACTUATOR ATTACHMENT LUG. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010402000992001040200099CE 2001 4 2 AU010020 120010112G32215842000211 PIN CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL NLG TRUNNION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR TRUNNION PIN CRACKED. FOUND DURING INSPECTION IAW CESSNA SB CQB00-3. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20010402001002001040200100CE 2001 4 2 AU010021 120010103G52101313232C12 PIN BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCB3T HCB3TN3 GL PAX DOOR SHEARED W O OTHER O OTHER CRCRUISE 1 AUS (AUS) DOOR HOOK CLEVIS PIN SHEARED. DOOR DIFFICULT TO OPEN. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010402001012001040200101EU 2001 4 2 AU010022 120010112G291024Q2395 HOSE BRAERO748 HS7482B 1500248EU RROYCEDART DART5322L 54509EU HYDRAULIC SYS CRACKED W O OTHER KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS (AUS) RT GEARBOX MOUNTED HYDRAULIC PUMP OUTLET HOSE END FITTING CRACKED ON FLARED OLIVE. 2L72 3T4 T A24EU E297 20010402001022001040200102SO 2001 4 2 AU010023 120010115G323040336000 DRAG BRACE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL NLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR DRAG BRACE ACTUATOR ATTACHMENT LUGS CRACKED. FOUND USING VISUAL AND CONFIRMED USING NDI. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010402001032001040200103EU 2001 4 2 AU010024 120010116G3213200877682 PIN BAC 146 146100A 1500260EU LYC ALF502ALF502R5 41580NE RT MLG FRACTURED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR WHEEL LEVER TO OLEO ATTACHMENT PIN FRACTURED AND MIGRATED. 2H74 4F4 FRTA49EU E6NE 20010402001042001040200104GL 2001 4 2 AU010025 220010112G72309380M28P05 TURBINE WHEEL GE GE CF6 CF680C2* GL ENGINE OUT OF TOLERANCEW K NONE O OTHER ININSP/MAINT 1 AUS 6513 (AUS) HIGH PRESSURE COMPRESSOR ROTOR SPOOL NR 3 STAGE TO NR 9 STAGE OUTSIDE OF LIMITS AS PER AD/CF6/41, AD/CF6-43, FAA AD FAD 99-24-15 AND FAA AD FAD 2000-16-12. 4 F E23EA 20010402001052001040200105NM 2001 4 2 AU010026 120010112G80119702038 CLAMP GE CF680C2 BOEING767 767338 1385151NM GE CF6 CF680C2* GL STARTER FAILED W O OTHER J WARNING INDICATION CLCLIMB 1 AUS 4159 9702038 (AUS) RT ENGINE STARTER CLAMP BROKEN AND STARTER LOOSE. SEAL CUT. 2L72 4F4 FRTA1NM E23EA 20010402001062001040200106NM 2001 4 2 AU010027 120010111G2910AV13J5147 VALVE BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU HYDRAULIC SYS SEIZED W K NONE O OTHER ININSP/MAINT 1 AUS 25973 (AUS) HYDRAULIC STANDBY MODULE SHUTOFF VALVE SEIZED. 2L72 4F4 FRTA16WE E21EU 20010402001072001040200107NE 2001 4 2 AU010028 220010103G8500 ENGINE DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE NACELLE SEIZED W A UNSCHED LANDING EY VIBRATION/BUFFET ENGINE STOPPAGE CLCLIMB 1 AUS (AUS) ENGINE RAN ROUGH AND THEN SEIZED. LIMITED INFORMATION PROVIDED. 1H71 3R3 R A806 5E1 20010402001082001040200108EA 2001 4 2 AU010029 220010116G731025765311 FLOW DIVIDER CESSNA182 182S 2072701CE LYC O540 IO540AB1A5 EA MCAULY3D36C B3D36C431 GL FUEL DIST CORRODED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AUS 92 (AUS) ENGINE FUEL FLOW DIVIDED CORRODED. PARTICLES OF CORROSION BLOCKING FUEL INJECTORS. AIRCRAFT HAD BEEN CONTAMINATED WITH EDAAND DECONTAMINATED IAW AD/GEN/80 AND MANUFACTURERS INSTRUCTIONS. 1H71 3O3 ONT3A13 1E4 5 C 20010402001092001040200109SO 2001 4 2 AU010030 120010113G2150MS21346221 SWITCH EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE AIR CONDITIONINGFAULTY W O OTHER J WARNING INDICATION CRCRUISE 1 AUS (AUS) AIR CONDITIONING SYSTEM CROSS BLEED VALVE SWITCH FAULTY. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010402001102001040200110NM 2001 4 2 AU010031 120010104G2530CA16371 CONNECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE GALLEY DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LIQUID HEATER CONNECTORS DAMAGED DUE TO OVERHEATING. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010402001112001040200111NM 2001 4 2 AU010032 120010104G2530CA16731 CONNECTOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE GALLEY DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LIQUID HEATER CONNECTORS DAMAGED DUE TO OVERHEATING. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010402001122001040200112NM 2001 4 2 AU010033 120010114G7830 DOOR RROYCE RB211524D4 BOEING747 747338 NM RROYCERB211 RB211524D41954555NE THRUST REVERSER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 ENGINE BLOCKER PARTIALLY MISSING. DAMAGE TO CORONA AND COLD STREAM DUCT AT 10 OCLOCK POSITION. 2L72 4F4 FRTA20WE E12EU 20010402001132001040200113 2001 4 2 AU010034 420010115G2330311038 CONTROL BOX BOEING767 767338 1385151NM GE CF6 CF680C2* GL ENTERTAIN SYS FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 311038 (AUS) SEAT 5A HARNESS PLUG TO SEAT ELECTRONICS BOX ARCING. ARCING CONTINUED WITH PLUG DISCONNECTED. NO CIRCUIT BREAKERS POPPED. 2L72 4F4 FRTA1NM E23EA 20010402001142001040200114NM 2001 4 2 AU010035 120010116G7830 DOOR RROYCE RB211524G BOEING747 747438 NM RROYCERB211 RB211524G19 NE THRUST REVERSER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 1 ENGINE THRUST REVERSER NR 9 BLOCKER DOOR PARTLY MISSING. DAMAGE TO CORONA WITH A 76.2MM BY 25.4MM (3IN BY 1IN) HOLE ADJACENT TO BLOCKER DOOR POSITION. DAMAGE ALSO TO LT COMBUSTION FAIRING AND INTEGRATED NOZZLE ASSEMBLY. 2L74 4F4 FRTA20WE E30NE 20010402001212001040200121EU 2001 4 2 AU010039 120010116G2770A78300401 LOCK FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU ELEVATOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR GUSTLOCK HOUSING MOUNTING LUGS CRACKED. FOUND DURING INSPECTION IAW AD/F28/72 AMDT1. SUSPECT CAUSED BY LOOSE MOUNT.BOLTS. 2L72 4F4 FRTA20EU E2EU 20010402001222001040200122CE 2001 4 2 AU010040 120010116G32215842000211 PIN CESSNA441 441 2076020CE GARRTTTPE331TPE3318 01514WP HARTZLHCB3T HCB3TN5 GL NLG TRUNNION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NOSE LANDING GEAR TRUNNION PIN CRACKED. 1L72 3T4 TRTA28CE E4WE 6 CP15EA 20010402001232001040200123NE 2001 4 2 AU010041 220010107G731021631001 PIPE BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE FUEL DIST WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 3 ENGINE LT PRIMARY FUEL PIPE CHAFING ON COMBUSTOR CASE IN AREA OF THE FORWARD FLANGE OF THE CUSTOMER BLEED FLANGE. 2H74 4F4 FRTA49EU E6NE 20010402001242001040200124EU 2001 4 2 AU010042 120010104G7603 CABLE LYC IO540K1B5 BNORM BN2 BN2A26 1520226EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL POWER LEVER LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE THROTTLE CABLE OUTER CONDUIT DISCONNECTED AT FIREWALL. THE NUT SECURING THE CONDUIT HAD NO LOCKWIRE. 1H72 3O3 O A17EU 1E4 5 CP920 20010402001252001040200125EU 2001 4 2 AU010043 120010105G7602 CABLE LYC IO540K1B5 BNORM BN2 BN2A26 1520226EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL MIXTURE CONTROL MISINSTALLED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE MIXTURE CONTROL INNER CABLE ONLY ENGAGED IN THE ENGINE CONTROL END BY APPROXIMATELY 1.5 TURNS. 1H72 3O3 O A17EU 1E4 5 CP920 20010402001262001040200126EU 2001 4 2 AU010044 120010110G6120 CONTROL CABLE HARTZL HCC2YK2 BNORM BN2 BN2A26 1520226EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL PROP CONTROL SEIZED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT PROPELLER CSU CONTROL CABLE OUTER CONDUIT WORN THROUGH WITHTHE INNER CABLE CATCHING ON THE WORN AREA. CONTROL SEIZED. 1H72 3O3 O A17EU 1E4 5 CP920 20010402001272001040200127NE 2001 4 2 AU010045 220010117G72603022375 SEAL PILATSPC12 PC12 7090550EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL ENGINE FAILED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) NR 4 ACCESSORY DRIVE SEAL MIGRATED OUT OF SEAL CARRIER PNO 3007737 ALLOWING APPROXIMATELY 3.5 LITRES OF OIL TO LEAK FROM THE ENGINE DRIVEN LOW PRESSURE FUEL PUMP DRIVE SPLINE DRAIN. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010402001282001040200128SW 2001 4 2 AU010046 120010122G3233MS28775116 SEAL EA1568 GULSTM500 500S 0141107SW LYC O540 IO540E1B5 41532EA HARTZLHCA3V HCA3VK2 GL MLG ACTUATOR WORN W O OTHER K FLUID LOSS DEDESCENT 1 AUS 2020 (AUS) MAIN LANDING GEAR RETRACTION ACTUATOR SEAL WORN. 1H72 3O3 O 6A1 1E4 5 CP6EA 20010402001292001040200129SO 2001 4 2 AU010047 220010111G7314 SEAL CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO FUEL PUMP FAILED W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT ENGINE DRIVEN FUEL PUMP SEAL FAILED. FUEL LEAKING FROM VENT. 1L72 3O3 O A7CE E8CE 20010402001302001040200130EU 2001 4 2 AU010048 120010108G5711 SPAR BAC 146 146300A 1500267EU LYC ALF502ALF502R5 41580NE LT & RT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING FORWARD AND AFT SPARS CONTAINED PITTING CORROSIONIN AREAS OUTBOARD OF RIB NR 13. HEAVY STAINING FOUND IN WING TANKS SUSPECTED FROM CLADOSPORIUM RESINAE. 2H74 4F4 FRTA49EU E6NE 20010402001312001040200131NM 2001 4 2 AU010049 120010122G324226056623 BRAKE BOEING747 747338 NM RROYCERB211 RB211524D41954555NE LT WING MLG FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 7020 (AUS) LT FORWARD WING LANDING GEAR NR 2 POSITION BRAKE FAILED. 2L72 4F4 FRTA20WE E12EU 20010402001322001040200132NM 2001 4 2 AU010050 120010119G2432401767 BATTERY BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU BATTERY BAY DISCHARGED W O OTHER HJ ELECT. POWER LOSS-50 PC WARNING INDICATION NRNOT REPORTED 1 AUS 4 (AUS) MAIN AIRCRAFT BATTERY DISCHARGED. 2L72 4F4 FRTA16WE E21EU 20010402001332001040200133EU 2001 4 2 AU010051 120010118G7722897476 COMPENSATOR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP ROTOL R333 R333482F12 GL EGT/TIT INDICATOOUT OF TOLERANCEW C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AUS (AUS) LT ENGINE EGT COMPENSATOR OUT OF TOLERANCE. 2L72 4T4 TRTA56EU E4WE 6 CP61GL 20010402001342001040200134NM 2001 4 2 AU010052 120010123G2400S010488308 RELAY DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE ELECTRICAL SEPARATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RELAY BASE SEPARATED AT PRODUCTION BREAK ALLOWING THE RELAY CONTACTS TO COME AWAY FROM THE RELAY. BASE MANUFACTURER CLOVER. THE RELAYS ARE USED IN NUMEROUS AREAS. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010402001352001040200135NE 2001 4 2 AU010053 220010118G73218063023 FUEL CONTROL STBROSSD3 SD360 8100606EU PWA PT6 PT6A67R 52043NE HARTZLHCA6A HCA6A3 NE RT ENGINE FAULTY W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) RT ENGINE FUEL CONTROL UNIT FAULTY. 2H72 4T4 T A41EU E26NE 6 CP14NE 20010402001362001040200136WP 2001 4 2 AU010054 120010121G3234630294W PISTON LKHEED1049 C121C 5262118WP WRIGHTR3350 R3350* 67040EA HAMSTD43E 43E60 NE MLG STRUT BROKEN W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LANDING GEAR SELECTOR VALVE PISTONS (2OFF4) BROKEN ACROSS SHANK IN AN O-RING SEAL GROOVE. BROKEN PISTON JAMMED IN PORT. 2L74 4R4 R 6A5 E272 6 CP871 20010402001372001040200137SO 2001 4 2 AU010055 220010125G8520632043 CONNECTING ROD CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3AF34C3AF34C74 GL ENGINE FAILED W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS 847 (AUS) LT ENGINE NR 5 CYLINDER CONNECTING ROD SEPARATED FROM CRANKSHAFT AND PENETRATED THE CRANKCASE. 1L72 3O3 O A25CE E7CE 5 CP22EA 20010402001382001040200138EU 2001 4 2 AU010056 120010128G57537257830022 FITTING 7257800504 SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R390 R3904123F27 NE TE FLAP CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 1114 (AUS) RT FLAP ASSEMBLY OUTBOARD FITTING AFT ATTACHMENT LUG CRACKED. CRACK APPEARS TO HAVE EMANATED FROM THE BOLT/BUSHING HOLE AND PROGRESSED THROUGH ONE SIDE OF THE LUG. FOUND DURING VISUAL INSPECTION IAW SB-340-57-037. 2L72 4T4 TRTA52EU E8NE 6 CP31NE 20010402001392001040200139EA 2001 4 2 AU010057 220010119G853017C21191 KEY ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA ENGINE BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 5 CYLINDER EXHAUST VALVE KEY BROKEN WITH DAMAGE TO TAPPET AND SOCKET. SUSPECT TAPPET DAMAGED AT MANUFACTURE CAUSING INCORRECT VALVE CLEARANCE. 1G71 3O3 O H11NM E295 20010402001402001040200140SW 2001 4 2 AU010058 120010127G2133A6009 ADAPTER SWRNGNSA227 SA227* SW GARRTTTPE331TPE33112UA 01514WP MCAULY4HFR344HFR34C652 NE PRESSURE REG FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AUS (AUS) CABIN PRESSURISATION SYSTEM OUTFLOW VALVE SUCTION FITTING FAILED. 2L72 4T4 TRTA5SW E4WE 6 C3PNE 20010402001412001040200141SO 2001 4 2 AU010036 120010116G27521202001 ACTUATOR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL TE FLAP WORN W O OTHER J WARNING INDICATION LDLANDING 1 AUS (AUS) FLAP MOTOR BRUSHES AND COMMUTATOR WORN. MOTOR INOPERATIVE. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010402002522001040200252SO 2001 4 2 CA010206004 220010104G8530628309 VALVE GUIDE CESSNA150 150M 2071830CE CONT O200 O200A 17020SO EXHAUST VALVE WORN W ED ENGINE SHUTDOWN RETURN TO BLOCK RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA 1439 (CAN) ENGINE RAN VERY ROUGH AT START UP.CYLINDER NR 3 REMOVED DUE TO LOW COMPRESSION. EXHAUST GUID WORN CAUSING CARBON TO JAM VALVE IN OPEN POSITION. CYLINDER RELACED DUE TO ABOVE PROBLEM. 1H71 3O3 O 3A19 E252 20010402002692001040200269EA 2001 4 2 AU010005 120010107G5230 HANDLE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE CARGO DOOR MALFUNCTIONED W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) CARGO DOOR MASTER CAUTION LIGHT ILLUMINATED. INVESTIGATION FOUNDTHE CARGO DOOR HANDLE PARTIALLY RELEASED. A FUNCTIONAL CHECK OF THE DOOR LATCHING SYSTEM COULD FIND NO FAULT. SUSPECT THAT THEHANDLE WAS INCORRECTLY STOWED. 2L72 4F4 FRTA21EA E15NE 20010402002702001040200270CE 2001 4 2 AU010011 120010110G28974410174 WIRE CESSNA C441 CESSNA441 441 2076020CE GARRTTTPE331TPE331* 01514WP HARTZLHCB3T HCB3TN5 GL BOOST PUMP CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS 4410174 (AUS) LT FUEL TANK BOOST PUMP WIRING CHAFED THROUGH TO BARE WIRE. 1L72 3T3 TRTA28CE E2WE 6 CP15EA 20010402002712001040200271SW 2001 4 2 AU010059 120010123G65102006505008 BOLT BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE TAIL ROTOR DRIVEWORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL ROTOR DRIVESHAFT TO TAIL ROTOR GEARBOX INPUT COUPLING BOLT SEPARATED. MARKS ON BOLT INDICATE THAT IT HAD BEEN LOOSE FOR SOME TIME. 1G72 4U4 U H4SW E22EA 20010402002722001040200272SW 2001 4 2 AU010060 120010113G733442D218 PRESSURE SWITCH BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FUEL PRESSURE LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NR 2 ENGINE FUEL PRESSURE SWITCH LEAKING FUEL FROM SOLDERED JOINT AT BASE OF CONNECTOR PLUG CONNECTOR. 1G72 4U4 U H4SW E22EA 20010402002732001040200273SW 2001 4 2 AU010061 120010113G733442D218 PRESSURE SWITCH BELL 412 412 1182202SW PWA PT6T PT6T3B 52045NE FUEL PRESSURE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) FUEL PRESSURE SWITCH LEAKING FROM SOLDERED JOINT AT BASE OF CONNECTOR PLUG FITTING. 1G72 4U4 U H4SW E22EA 20010402002742001040200274 2001 4 2 AU010063 420010101G2565B732560135 CABLE BOEING737 737377 NM GE CFM56 CFM563B1 13802NE ESCAPE SLIDE FRAYED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) L2 DOOR SLIDE ATTACHMENT CABLE FRAYED IN LOOP AREA. 2L72 4F4 FRTA16WE E2GL 20010402002752001040200275NM 2001 4 2 AU010064 120010109G28976130024 WIRE BOEING737 737377 NM GE CFM56 CFM563B1 13802NE FUEL SYSTEM DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) KAPTON WIRES LOCATED IN REFUEL PANEL HAVE DAMAGED INSULATION ALLOWING THE WIRES TO BE EXPOSED. 2L72 4F4 FRTA16WE E2GL 20010402002762001040200276EU 2001 4 2 AU010065 120010123G5343 FITTING AIRBUS320 A320211 3930320EU CFMINTCFM56 CFM565A1 NE MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT MAIN LANDING GEAR DOOR ACTUATOR FITTING AND CONNECTING STRIP CRACKED IN TWO PLACES. CRACK LENGTHS 20MM (0.78IN) IN FORWARD FLANGE AND 28MM (1.102IN) IN AFT FLANGE. CONNECTION STRAP CRACKED FROM FASTENER HOLE. CRACK LENGTH 5MM (0.196IN). FOUND DURING NDI INSPECTION IAW SB A320-53A1135 AND AN ENGINEERING RELEASE A32-53-40-9B. 2L72 4F4 FRTA28NM E29NE 20010402002772001040200277CE 2001 4 2 AU010066 120010120G551107326022 SPAR CESSNA185 A185F 2072821CE CONT O520 IO520D 17032SO MCAULYD3A34 D3A34C401 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER REAR SPAR CRACKED IN AREA BEHIND THERE INFORCED HINGE BRACKET CRACK LENGTH 50MM (1.96IN). CAUSED BY SEVERE CORROSION ON THE DOUBLER BRACKET SECURING THE ATTACHMENT HINGE PNO 0732101-11. 1H71 3O3 O 3A24 E5CE 5 CP47GL 20010402002802001040200280SO 2001 4 2 AU010069 120010128G3250 PIN EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE NLG STEERING LOOSE W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AUS (AUS) NOSE WHEEL STEERING RELAY BOX CONNECTOR PIN LOOSE. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010402002822001040200282EU 2001 4 2 AU010071 120010202G7931PDCR3301028 TRANSMITTER BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE OIL PRESSURE FAULTY W O OTHER J WARNING INDICATION CRCRUISE 1 AUS 3153 (AUS) NR 3 ENGINE OIL PRESSURE TRANSMITTER FAULTY. 2H74 4F4 FRTA49EU E6NE 20010402002832001040200283NE 2001 4 2 AU010072 220010203G73218061963 FMU BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE FUEL CONTROL FAULTY W O OTHER J WARNING INDICATION DEDESCENT 1 AUS (AUS) NR 2 ENGINE FUEL METERING UNIT (FMU) AND ELECTRONIC ENGINE CONTROLLER (EEC) FAULTY. 2L72 4F4 FTRA6WE E00061EN 20010402002842001040200284NE 2001 4 2 AU010073 220010203G7321114E6112G117 EEC BOEING717 717200 1383700NM RROYCEBR700 BR700715A130 NE FUEL CONTROL FAULTY W O OTHER J WARNING INDICATION DEDESCENT 1 AUS (AUS) NR 2 ENGINE ELECTRONIC ENGINE CONTROLLER (EEC) FAULTY. SEE ALSO MDR 01/0072. 2L72 4F4 FTRA6WE E00061EN 20010402002852001040200285NE 2001 4 2 AU010074 320010129G6111RFC11U1R6A BLADE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PROPELLER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT PROPELLER BLADE DAMAGED BY MISSING SPINNER ATTACHMENT SCREW. THREE SCREWS MISSING FROM SPINNER. ONE SCREW WAS FOUND EMBEDDED IN THE PROPELLER BLADE. MAINTENANCE HAD BEEN CARRIED OUT ON THE PROPELLER PRIOR TO THE FLIGHT. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010402002872001040200287EA 2001 4 2 AU010076 220010112G7414K3984 CAPACITOR SLICK 4381 CESSNA150 152 2071835CE LYC O235 O235L2C 41505EA MCAULY1A103 1A103TCM GL LT MAGNETO BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS 2068 97020839 (AUS) LT MAGNETO CAPACITOR CONNECTING WIRE BROKEN DUE TO LOOSE BEARING CAP. FURTHER INVESTIGATION FOUND THE BEARINGS TO BE DRY AND AN UNKNOWN SUBSTANCE UNDER THE BEARING CAP HOLD-DOWN PLATES WHICH PREVENTED THE CAP BEING PROPERLY SECURED. 1H71 3O3 ONT3A19 E223 5 NP50GL 20010402002882001040200288SO 2001 4 2 AU010077 220010206G8550 GEAR CONT O520 TSIO520K 17040SO SCAV PUMP FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OIL SCAVENGE PUMP GEAR FAULTY. ROCKWELL HARDNESS TEST GAVE A READING OF 34 WHICH IS BELOW SPECIFICATION. 3 O E8CE 20010402002902001040200290GL 2001 4 2 AU010079 320010128G6114737568 HUB LYC O360 O360A2A 41514EA MCAULY2D36C 2D36C14 GL PROPELLER DAMAGED W C ABORTED TAKEOFF D INFLIGHT SEPARATION TOTAKEOFF 1 AUS (AUS) PROPELLER HUB FAILED DUE TO CRACK ORIGINATING IN THE ROOT OF THEBLADE RETAINING THREAD. PROPELLER BLADE SEPARATED FROM HUB. 3 O E286 5 CP901 20010402002912001040200291NM 2001 4 2 AU010080 120010127G7110 PANEL RROYCE RB211524D4 BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE COWLING MISSING W K NONE O OTHER ININSP/MAINT 1 AUS 15288 (AUS) NR 1 ENGINE NR 1 AND NR 3 & 4 ACOUSTIC PANELS MISSING. 2L74 4F4 F A20WE E12EU 20010402002922001040200292NM 2001 4 2 AU010081 120010127G291013206001 SWITCH BOEING767 767238 NM PWA JT9 JT9D7R4E 52054NE HYDRAULIC SYS FAULTY W O OTHER J WARNING INDICATION CRCRUISE 1 AUS (AUS) LT HYDRAULIC TAIL SHUTOFF VALVE SWITCH MODULE FAULTY. 2L72 4F4 FRTA1NM E3NE 20010402002952001040200295NM 2001 4 2 AU010084 120010130G2741 WIRE BOEING747 747438 NM RROYCERB211 RB211524G19 NE STABILIZER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT STABILISER POSITION ROTARY VARIABLE DISPLACEMENT TRANSDUCER(RVDT) PLUG DM7884 HAD CHAFED WIRING ADJACENT TO PLUG. 2L74 4F4 FRTA20WE E30NE 20010402002962001040200296NM 2001 4 2 AU010085 120010131G2120 UNKNOWN BOEING767 767338 1385151NM RROYCERB211 RB211524* NE AIR CONDITIONINGODOR W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) FUMES IN CABIN. INVESTIGATION CONTINUING INTO CAUSE. 2L72 4F4 FRTA1NM E12EU 20010403000012001040300001EA 2001 4 3 AU010155 220010219G7310420218 SWITCH BELL 412 412 1182202SW PWA PT6T PT6T3 52045EA FUEL BYPASS LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) FUEL FILTER BYPASS SWITCH LEAKING FROM SWITCH BODY IN THE AREA WHERE THE ELECTRICAL CONNECTOR IS SOLDERED TO THE SWITCH. FUEL WAS SEEN RUNNING INTO THE ENGINE INTAKE PLENUM. A REPLACEMENT SWITCH HAD POOR SOLDERING OF THE CONNECTOR IN THE SAME AREA ASTHE FAILED ITEM. 1G72 4U4 U H4SW E22EA 20010403000022001040300002EU 2001 4 3 AU010156 120010211G77142454401 SENSOR AEROSPSA365 SA365C 8680667EU TMECA ARRIELARRIEL1A 60030NE ENGINE FAULTY W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE OVERSPEED SENSOR FAULTY. 1G72 3U3 U H10EU E19EU 20010403000032001040300003EU 2001 4 3 AU010159 120010212G772221186009 COMPUTER BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE ENGINE FAULTY W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) LT ENGINE SINGLE RED LINE COMPUTER FAULTY. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010403000042001040300004EU 2001 4 3 AU010160 120010223G7160TU195MM660MMCC HOSE BNORM BN2 BN2B20 1520302EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL ENG AIR INTAKE FAILED W C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 1 ENGINE INTAKE HOSE LOCATED BETWEEN THE AIR FILTER AND THE FCU COLLAPSED DUE TO LOOSE INNER SUPPORT WIRE. 1H72 3O3 O A17EU 1E4 5 CP920 20010403000782001040300078 2001 4 3 CA010212033 420010123G2562R889V BATTERY CESSNA150 150L 2071826CE CONT O200 O200A 17020SO ELT UNAPPOVED PART W K NONE O OTHER ININSP/MAINT 1 CA (CAN) ELT SENT IN FOR RECERTIFICATION. WAS EQUIPPED WITH A NON-APPROVED BATTERY PACK ARTEX . ONLY APPROVED BATTERY IS TECHNISONIC. BATTERY REPLACED AND ELT RECERTIFIED. 1H71 3O3 O 3A19 E252 20010403000802001040300080CE 2001 4 3 CA010213003 120010118G7160 HOSE CESSNA150 150 2071802CE CONT O200 O200* 17020SO CARB HEAT CONTAMINATED W C ABORTED TAKEOFF RE PARTIAL RPM/PWR LOSS VIBRATION/BUFFET TOTAKEOFF 1 CA (CAN) DURING THE WINTER MONTHS WE ARE RECEIVING COMPLAINTS OF A SERIOUS NATURE. UPON TAKEOFF, USUALLY THE FIRST ONE, THE AIRCRAFT RUNS VERY ROUGH. I HAVE EXPERIENCED THIS PERSONALLY. WE HAVE DETERMINED THAT SNOW COLLECTS IN THE SCAT HOSE THAT PROVIDES AIR FOR CARB HEAT. THIS SNOW MELTS AFTER THE ENGINE HAS WARMED UP AND UPON SELECTION OF CARB HEAT THE ENGINE WANTS TO QUIT. WE HAVE REMEDIED THIS ON SEVERAL AIRCRAFT BYMAKING A SMALL HOLE IN THE LOW SPOT OF THE SUBJECT SCAT HOSE, USING A SOLDERING IRON. 1H71 3O3 ONT3A19 E252 20010403000842001040300084EA 2001 4 3 CA010213020 120010124G2740 ACTUATOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE HORIZONTAL STAB FAILED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 CA (CAN) DURING TAKEOFF ROLL, CONFIG TRIM AND CONFIG STAB WARNINGS APPEARED. CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS.HSTA AND MCU REPLACED. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010403000852001040300085EA 2001 4 3 CA010213027 120010213G5730 PANEL CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE RT AND LT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE JACKING AIRCRAFT, MAINTENANCE FOUND TWO CRACKS ON AFT SECTION OF LOWER WING PLANK. ONE ON THE LT AND ONE ON THE RT SIDE, AT WS 148, NEAR THE WING JACKING POINTS. REPAIR ACTIVE, AIRCRAFT WILL RETURN INTO SERVICE SOON. 2L72 4F4 FRTA21EA E15NE 20010403000862001040300086EA 2001 4 3 CA010214004 120010201G5210601R31765303 STRUCTURE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE PAX DOOR LATCH CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING A ROUTINE E3 (1200 HOURS) INSPECTION WHEN REMOVING THE PASSENGER DOOR SIDE PANELS A CRACK WAS FOUND IN THE PASSENGER DOOR LATCH BOX ASSEMBLY 601R31765-3/03. THE AIRCRAFT REMAINED GROUNDED UNTIL A NEW LATCH BOX WAS INSTALLED. FOLLOWING THE REPLACEMENT OF THE FAULTY COMPONENT, THE AIRCRAFT WAS THEN RELEASED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010403000872001040300087EA 2001 4 3 CA010214008 220010112G8500 ENGINE PIPER PA28 PA28R200 7102811SO LYC O360 IO360C1C 41514EA ENGINE BAY FAILED W A UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 CA 687 (CAN) ENGINE HAD STOPPED / SEIZED AFTER THE ENGINE HEATER PLATE WHICH HAD BEEN INSTALLED THE DAY BEFORE THE FLIGHT WAS DISLODGED WHEN THE NOSE LANDING GEAR DRAG LINK CONTACTED WITH THE PLATE IN GEAR UP POSITION. THE PLANE LANDED THE PILOT DIDNT NOTICE ANYTHING. ON THE SECOND FLIGHT WHEN SELECTING GEAR UP THE PLATE WAS PUSHED ON THE QUICK DRAIN BY THE LANDING GEAR AND ALLOWED THE ENGINE OIL TO DRAIN COMPLETELY. ENGINE STOPPED THE PILOT HAD TO MAKE A FORCED LANDING IN A FIELD. ONLY MINOR DAMAGES WERE MADE TO THE PLANE. 1L71 3O3 O 2A13 1E10 20010403000892001040300089SW 2001 4 3 CA010214011 120010119G2510502565213 SHOULDER BELT HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA COCKPIT FAILED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) MAIN STRAP SHREADED.REPLACED SHOULDER STRAP. 1G71 3O3 OO 4H12 E286 20010403000912001040300091CE 2001 4 3 CA010214027 120010125G57530621229 HINGE CESSNA305 305A 2074002CE CONT O470 O47011 17026SO LT WING TE FLAPSCRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3667 (CAN) WING FLAP HINGE INBOARD FOUND CRACKED AT BOTH LOWER FLANGES THAT ATTACH TO THE SPAR. PART REPLACED WITH NEW. 1H71 3O3 O 5A5 E269 20010403001242001040300124EU 2001 4 3 CA010208013 120010123G2431RG390E BATTERY BRAERODH125 BAE125800A 1500285EU GARRTTTFE731TFE7315R 01518WP MAIN BATTERY OVERHEATED W O OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 CA 407 (CAN) ENGINE ROTATION TOO SLOW AT START ATTEMPTS FOR SUCCESSFUL ENGINE LIGHT OFF. BATTERY VENTED EXCESSIVE AMOUNTS OF SMOKE AND VAPOR (STEAM AND ACID GAS) DUE TO SEVERAL SUCCESSIVE FAILED ENGINE START ATTEMPTS WITHOUT ALLOWING SUFFICIENT RECHARGING BY AIRCRAFT ELECTRICAL SYSTEM. HOT BATTERIES REMOVED FROM AIRCRAFT. STRUCTURE NEUTRALIZED AND RINSED WITH FRESH WATER. - NEW BATTERIES FITTED. 2L72 4F4 FRTA3EU E6WE 20010403001252001040300125NE 2001 4 3 CA010208014 120010124G62207610308010103 HUB SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 3985 3985 (CAN) DURING THE POST FLIGHT INSPECTION BY AME A FINE LINE WAS NOTICED ON THE UPPER DAMPER ATTACH LUG. THE LUG WAS PAINT STRIPPED AND A DEFINITE CRACK CAN BE SEEN. STARTING NEAR THE BOLT HOLE PROGRESSING INBOARD FOR APPROXIMATELY 1 1/4 INCH. THE MAIN ROTOR HUB WAS REPLACED. 1G72 3U3 U H1NE E1GL 20010403001262001040300126SW 2001 4 3 CA010208016 120010122G6220471202527 GRIP BELL 47 47J2 1181104SW LYC O435 TVO435* 41516EA MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2261 31 (CAN) AIRCRAFT IS BEING IMPORTED INTO CANADA. CRACKS IN ROOT OF THREADS FOUND DURING EDDY CURRENT INSPECTION. 1G71 3O3 O 2H1 1E13 20010403001282001040300128SO 2001 4 3 CA010209003 120010209G6310 ENGINE PIPER PA31 PA31P 7103120SO LYC O541 TIGO541E1A 41539EA NACELLE FAILED W O OTHER J WARNING INDICATION DEDESCENT 1 CA 1231 (CAN) ENGINE LOSSED MANIFOLD PRESSURE FOLLOWED BY LOSS OF OIL PRESSURE. VISUAL INSPECTION REVEALS CRACKED CASE. 1L72 3O3 O A8EA E19EA 20010403001292001040300129WP 2001 4 3 CA010209004 120010112G2435230321183 BELL ASSY LUCAS 23032018 HUGHES369 369D 4470706WP ALLSN 250C 250C20B 03013GL STARTER GEN UNAPPOVED PART W K NONE O OTHER ININSP/MAINT 1 CA 1177 2514 (CAN) STARTER GEN RECEIVED FOR OVERHAUL. FOUND THE ADE (COMM END) END BELL ASSEMBLY TO BE 3, WHICH ACCORDING TO THE OEM IS AN OLD, OBSOLETED PART THAT WAS APPLICABLE ONLY TO THE 23032-005 STARTER-GENERATOR, WHICH IS ITSELF OBSOLETE, UNSUPPORTED AND NOT LISTED IN THE OVERHAUL MANUAL. THE ASSEMBLY IS ALSO CORRODED AND CRACKED AROUND THE MOUNTING HOLES. THE CORRECT ASSY IS P/N 23032-1423. A CORRECT ASSY WAS INSTALLED DURING OVERHAUL, ALONG WITH THE CORRECT BEARING RETAINER AND FAN COVER.THE OFFENDING PARTS ARE BEING TRANSMITTED TO THE AIRCRAFT OPERATOR FOR FOLLOW-UP. 1G71 3U3 U H3WE E4CE 20010403001302001040300130SW 2001 4 3 CA010209006 120010129G2435230791281 BRUSHES LUCAS 230790001 SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL STARTER GEN UNAPPOVED PART W K NONE O OTHER ININSP/MAINT 1 CA 499 10020 (CAN) DURING SCHEDULED MAINTENANCE, AT BRUSH INSPECTION IT WAS FOUND THAT THE BRUSHES INSTALLED IN THIS STARTER-GENERATOR WERE. THIS BRUSH IS ONLY APPROVED FOR THE STARTER GEN MODELS 23079-009 AND 23079-000-2.THE BRUSHES WERE REMOVED AND REPLACED WITH FAA-PMA LONG LIFE BRUSH PART NO.M23088-1320, WHICH IS APPROVED FOR THIS STARTER-GENERATOR MODEL 23079-000-1 WHEN USED ON THE FAIRCHILD SA227AC AIRCRAFT. THE STARTER GEN WAS RETURNED TO SERVICE. 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20010403001312001040300131EU 2001 4 3 CA010209007 120010131G32409595601511 BRAKE PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL LT MLG FROZEN W O OTHER O OTHER LDLANDING 1 CA (CAN) TAKEOFF IN FT ST. JOHN IN POWDER SNOW MAY HAVE CAUSED MOISTURE TO ENTER LT BRAKE ASSEMBLY. DURING FLIGHT TO FT NELSON, BRAKE FROZE. ON LANDING IN FT. NELSON LT TIRE WOULD NOT ROTATE AND TIRE FLAT SPOTTED AND BLEW. AIRCRAFT WAS STOPPED ON RUNWAY AND MAINTENANCE WAS CALLED. TIRE AND WHEEL ASSEMBLY WAS REPLACED AND GEAR ASSEMBLY INSPECTED FOR DAMAGE. THIS IS THE 3RD SUCH INCIDENT IN THE LAST 12 MONTHS. 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010403001322001040300132NE 2001 4 3 CA010209009 220010116G72304036T24P01 BLADE LEAR 25 25B 5170511CE GE CJ610 CJ6106 30006NE ENGINE SEPARATED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 2264 2264 (CAN) AIRCRAFT IN CLIMB FL110, LOUD BANG HEARD, RT FIRE WARNING ACTIVATED. POWER REDUCED, FUEL SHUT OFF, FIRE WARNING DE-ACTIVATED. AIRCRAFT RETURNED TO DEPARTURE AIRPORT AND SINGLE ENGINE LANDING CARRIED OUT WITHOUT FURTHER INCIDENT. GROUND INSPECTION REVEALED THAT FINAL STAGE TURBINE HAD LOST ONE BLADE (CONTAINMENT RING DAMAGED BUT NOT PENETRATED) RESULTANT IMBALANCE CAUSED SEVERE DAMAGE TO REMAINING BLADES AND SHROUD AND CAUSED EXHAUST TAIL PIPE TO SEPARATE AT MOUNTING FLANGE. HOT GASES RELASED INSIDE COWLING CAUSED FIRE WARNING TO ACTIVATE. ENGINE OVERHAUL AGENCY MAY HAVE MORE INFORMATION AFTER THEIR ANALYSIS. 2L72 4J4 J A10CE 1E16 20010403001332001040300133SW 2001 4 3 CA010209015 120010121G5610412669001100 WINDOW BELL 212 212 1181420SW PWA PT6T PT6T3 52045EA COCKPIT FAILED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) WHILE IN STRAIGHT AND LEVEL FLIGHT A LOUD BANG WAS HEARD. IT WAS DISCOVERED THAT THE RT REAR SLIDING DOOR WINDOW HAD SHATTERED. AN UNEVENTFUL LANDING WAS CARRIED OUT. ALLL PIECES WERE RECOVERED. 1G71 4U4 U H4SW E22EA 20010403001342001040300134EU 2001 4 3 CA010209017 120010131G3310MS24149A1 RELAY BRAERODH125 HS125700A 4230170EU GARRTTTFE731TFE7313R 01518WP LIGHTING FAILED W O OTHER J WARNING INDICATION TXTAXI/GRND HDL 1 CA (CAN) AFTER TAXI IN AT YVR THE NR 2 AC INVERTER FAIL LIGHT ILLUMINATED AS WELL AS XS2 BUSS FAIL LIGHT ILLUMINATED. RESET THE NR 2 INVERTER SWITCH FAILED TO RESET THE SYSTEM. MAINTENANCE TROUBLESHOOT THE PROBLEM BACK TO A FAULTY RELAY WITHIN THE CABIN LIGHTING SYSTEM. FURTHER INVESTIGATION FOUND THE LIGHTING RELAY CHATTERING, CAUSED A FLUCTUATING VOLTAGE ON THE XS2 BUSS RESULTING IN THE NR 2 INVERTER TRIPPING OFF LINE. AFTER TRACING THE HISTORY OF THIS PROBLEM IT WAS FOUND THAT IN MORE THAN ONE OCCASIION THE CABIN LIGHTING HAS CAUSED A TOTALFAILURE OF THE AIRCRAFTS RIGHT AC BUSS THUS LEAVING CONCERNS AS TO HOW A SECONDARY SYSTEM CAN FAIL A PRIMARY SYSTEM ON THE AIRCRAFT. 2L72 4F4 F A3EU E6WE 20010403001362001040300136CE 2001 4 3 CA010212005 120010123G531224120651 BULKHEAD CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 10545 (CAN) DURING INSPECTION OF AIRCRAFT FOLLOWING A GEAR UP LANDING, THE TWO BULKHEADS RUNNING VERTICALLY IN FRONT OF CABIN DOORS WERE FOUND CRACKED AT FLOOR LEVEL. THE CRACK IS LOCATED AT THE CUT OUT FOR THE HEAT DISCHARGE DUCT. THESE CRACKS WERE NOT CAUSED BY THE GEAR UP LANDING. 1H71 3O3 O 3A17 E286 5 CP7EA 20010403001372001040300137CE 2001 4 3 CA010212006 120010123G531205120122 BULKHEAD CESSNA172 172P 2072436CE LYC O320 O320D2J 41508EA FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 15904 (CAN) DURING ROUTINE CESSNA PROGRESSIVE CARE INSPECTION, THE BULKHEAD AT THE BACK END OF THE BAGGAGE COMPARTMENT STATION 108 WAS FOUND TO BE CRACKED AT BOTH LOWER CORNERS, AND THE UPPER RIGHT CORNER. THE CRACKS ARE APPROXIMATELY 2 INCHES LONG. THIS AIRCRAFT IS USED FOR FLIGHT TRAINING AND ON OCCASION BANNER TOWING. 1H71 3O3 ONT3A12 E274 20010403001382001040300138EA 2001 4 3 CA010212007 120010125G2701C3CF3913 CONTROL COLUMN DHAV DHC3 DHC3 2800202EA PWA PT6 PT6A34 52043EA COCKPIT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WHILE CARRYING OUT AIRWORTHINESS DIRECTIVE CF-82-34 WE FOUND A CRACK IN THE LOWER WELD ASSEMBLY OF THE AILERON CONTROL COLUMN LOCATED AT THE CUT HOLE FOR THE AILERON CHAIN. THE CRACK WAS APPROXIMATELY 1/4 INCH LONG. 1H71 3R4 T A815 E4EA 20010403001392001040300139NE 2001 4 3 CA010212011 220010118G7200 ENGINE BOEING727 727225 1384077NM PWA JT8 JT8D7B 52053NE NR 1 FAILED W A UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 CA (CAN) ENROUTE TO CPH FROM EMA NR 1 ENGINE OIL QUANTITY SLOWLY DECREASED TO 1 GALLON AT WHICH POINT THE INFLIGHT SHUT DOWN WAS PERFORMED. THE A/C LANDED WITHOUT INCIDENT AT CPH. THE ENGINE MAINTAINED POSITIVE OIL PRESSUE FOR THE 20-25 MINUTE PERIOD OF WINDMILL CONDITION. THE ENGINE WAS REMOVED AND IS ENROUTE FOR ASSESSMENT. 2L73 4F4 F A3WE E2EA 20010403001512001040300151NM 2001 4 3 AU010086 120010130G5730113T161331 PANEL BOEING767 767338 1385151NM GE CF6 CF680C2* GL LT WING FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PANEL 551VB LOCATED ON LT WING LOWER SURFACE AFT OF THE LT MAIN LANDING GEAR MISSING A CENTRE SECTION APPROXIMATELY 6 FEET LONG. 2L72 4F4 FRTA1NM E23EA 20010403001522001040300152NM 2001 4 3 AU010087 120010128G291065C268393152 PIPE BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU HYDRAULIC SYS CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HYDRAULIC SYSTEM A ENGINE DRIVEN PUMP HYDRAULIC LINE CHAFED BY LOWER AILERON PCU. 2L72 4F4 FRTA16WE E21EU 20010403001542001040300154SO 2001 4 3 AU010089 120010205G2910D100366 FITTING EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE HYDRAULIC SYS LEAKING W O OTHER K FLUID LOSS CRCRUISE 1 AUS (AUS) HYDRAULIC FITTING LOCATED IN LT OUTBOARD NACELLE LEAKING UNDERPRESSURE. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010403001552001040300155EU 2001 4 3 AU010090 120010119G3610 LOOP AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE PNEUMATIC DIST FAULTY W D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 AUS (AUS) WING LOOP A PNEUMATIC SYSTEM INOPERATIVE. 2L72 4F RTA35EU E24NE 20010403001562001040300156EU 2001 4 3 AU010091 120010202G3610 DUCT AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE PNEUMATIC DIST LEAKING W O OTHER J WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) NR 1 BLEED AIR SYSTEM LEAKING. 2L72 4F RTA35EU E24NE 20010403001572001040300157EU 2001 4 3 AU010092 120010202G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING CONTAMINATED W O OTHER N FALSE WARNING NRNOT REPORTED 1 AUS (AUS) FORWARD CARGO DOOR MICROSWITCH CONTAMINATED WITH DIRT AND PAINT. 2L72 4F4 FRTA20EU E2EU 20010403001582001040300158EU 2001 4 3 AU010094 120010131G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING OUT OF ADJ W O OTHER N FALSE WARNING CRCRUISE 1 AUS (AUS) SERVICE DOOR MICROSWITCH OUT OF ADJUSTMENT. 2L72 4F4 FRTA20EU E2EU 20010403001592001040300159EU 2001 4 3 AU010095 120010130G3610 DUCT FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU PNEUMATIC DIST LEAKING W O OTHER N FALSE WARNING NRNOT REPORTED 1 AUS (AUS) TAIL SECTION PNEUMATIC DUCT LEAK WARNING. INVESTIGATION COULD FIND NO LEAKS. 2L72 4F4 FRTA20EU E2EU 20010403001632001040300163EU 2001 4 3 AU010096 120010129G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) SERVICE DOOR WARNING LIGHT ILLUMINATED. SUSPECT MICROSWITCHES OUT OF ADJUSTMENT. 2L72 4F4 FRTA20EU E2EU 20010403001642001040300164EU 2001 4 3 AU010097 120010128G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING STUCK W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 AUS (AUS) CARGO DOOR MICROSWITCHES STICKING INTERMITTENTLY. 2L72 4F4 FRTA20EU E2EU 20010403001652001040300165EU 2001 4 3 AU010098 120010128G243223531 BATTERY FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU BATTERY BAY OVERHEATED W A UNSCHED LANDING MJ OVER TEMP WARNING INDICATION CRCRUISE 1 AUS (AUS) FORWARD BATTERY OVERTEMPERATURE. 2L72 4F4 FRTA20EU E2EU 20010403001662001040300166EU 2001 4 3 AU010099 120010126G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 AUS (AUS) FORWARD SERVICE DOOR MICROSWITCH OUT OF ADJUSTMENT. 2L72 4F4 FRTA20EU E2EU 20010403001672001040300167EU 2001 4 3 AU010100 120010125G5312 BULKHEAD FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU FUSELAGE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) REAR PRESSURE BULKHEAD CRACKED. 2L72 4F4 FRTA20EU E2EU 20010403001682001040300168EU 2001 4 3 AU010101 120010120G3230 UPLOCK FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU RT MLG LOOSE W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) RT MAIN LANDING GEAR DOOR UPLOCK HOOK LOOSE. 2L72 4F4 FRTA20EU E2EU 20010403001692001040300169EU 2001 4 3 AU010102 120010105G5270 SWITCH FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU DOOR WARNING STUCK W C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AUS (AUS) CARGO DOOR MICROSWITCHES STICKING INTERMITTENTLY. 2L72 4F4 FRTA20EU E2EU 20010403001702001040300170SO 2001 4 3 AU010103 120010202G273141734078 CONTROL CABLE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ELEVATOR TAB WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELEVATOR TRIM CABLE SEVERELY WORN IN THE AREA AROUND THE TRIM SERVO. ALL WIRE STRANDS BROKEN EXCEPT FOR TWO. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403001712001040300171EA 2001 4 3 AU010104 220010202G8550LW13383 BAFFLE PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA HARTZLHCE3Y HCE3YR2 GL ENGINE SUMP LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS 691 (AUS) ENGINE SUMP BAFFLE RIVET MISSING. THREE REMAINING RIVETS LOOSE. METAL IN OIL SYSTEM CAME FROM WORKING RIVETS. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403001722001040300172EU 2001 4 3 AU010105 220010205G72619584 ENGINE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU OIL PRESSURE LOW W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) NO2 ENGINE LOW OIL PRESSURE. ENGINE REMOVED AND AWAITING STRIPREPORT. 2L72 4F4 FRTA20EU E2EU 20010403001732001040300173NM 2001 4 3 AU010106 120010105G5310 STRUCTURE BOEING727 727277 138408SNM PWA JT8 JT8D15 52051NE FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) NUMEROUS AREAS OF CORROSION FOUND DURING CPCP INSPECTION IAWAD/B727/128. 2L73 4F4 FRTA3WE E2EA 20010403001742001040300174NM 2001 4 3 AU010107 120010130G252011 BOLT BOEING737 737377 NM GE CFM56 CFM563B1 13802NE SEAT BELT LOOSE W K NONE O OTHER ININSP/MAINT 1 AUS 4006 (AUS) SEAT BELT ATTACHMENT BOLT LOOSE AT SEAT 11E. FOUND DURING INSPECTION IAW ER B73-25-20-246. 2L72 4F4 FRTA16WE E2GL 20010403001752001040300175NE 2001 4 3 AU010108 220010207G72000292005250 ENGINE SKRSKYS76 S76C 8143008NE TMECA ARRIELARRIEL1S 60030NE NR 1 SEIZED W K NONE O OTHER ININSP/MAINT 1 AUS 1738 (AUS) NR 1 ENGINE INTERNAL FAILURE. INSPECTION FOUND COMPRESSOR SEIZED AND SEVERAL TURBINE BLADES MISSING/BROKEN. 1G72 3U3 UNCH1NE E19EU 20010403001762001040300176NM 2001 4 3 AU010109 120010123G3230113T1110 FITTING BOEING767 767277 NM GE CF6 CF680A 30025NE MLG CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT MAIN LANDING GEAR SIDE STRUT SWIVEL ASSEMBLY FITTINGS COORODED IN AREA BENEATH BUSHING FLANGE. 2L72 4F4 FRTA1NM E13NE 20010403001772001040300177CE 2001 4 3 AU010110 120010214G5330101120108604 SKIN BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE MCAULY4HFR344HFR34C754 NE FUSELAGE DEBONDED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TOP SKIN DISBONDED. 1L72 4T4 T A24CE E4EA 6 C3PNE 20010403001802001040300180SO 2001 4 3 AU010113 120010208G2823480700 PIN PIPER PA23 PA23250 7102308SO LYC O540 IO540C4B5 41532EA HARTZLHCE2Y HCE2YK2 GL FUEL SELECTOR BROKEN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT FUEL SELECTOR ROLL PINS (2OFF) BROKEN. 1L72 3O3 O 1A10 1E4 5 CP9EA 20010403001812001040300181CE 2001 4 3 AU010114 120010206G2731 BOLT CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO MCAULY3AF32C3AF32C93 GL FLIGHT CONTROL WORN W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) EXCESSIVE TRIM TAB FREE-PLAY DUE TO WORN AFT PUSHROD BOLT. 1L72 3O3 O A7CE E8CE 5 CP22EA 20010403001822001040300182EU 2001 4 3 AU010115 120010129G7933J03040C CONNECTOR FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE OIL TEMP CONTAMINATED W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION CLCLIMB 1 AUS (AUS) NR 1 ENGINE OIL TEMPERATURE PROBE CONNECTOR PLUG LOOSE AND CONTAMINATED. 2L72 4F4 FRT E25NE 20010403001832001040300183NM 2001 4 3 AU010116 120010122G291082910010113 PIPE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC SYS FRACTURED W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) HYDRAULIC PIPE FRACTURED ON RADIUS AT STA. 110.0. LOSS OF HYDRAULIC FLUID. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010403001842001040300184WP 2001 4 3 AU010117 120010130G5720157 FITTING DHAVXXDH82 DH82AROBRTSN2801002WP DHAVXXGIPSY GIPSYMAJOR1 20004WP LT WING FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 157 (AUS) LT WING FRONT LOWER INTERPLANE STRUT ATTACHMENT FITTING BROKEN AWAY DUE TO WOOD ROT. 1Q71 3I3 I A8EU A8EU 20010403001852001040300185NM 2001 4 3 AU010118 120010120G3260 UPLOCK SENSOR DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG OUT OF ADJ W C ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 AUS (AUS) RT MAIN LANDING GEAR UPLOCK SENSOR OUT OF ADJ. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010403001862001040300186CE 2001 4 3 AU010119 120010206G8011PM2407 STARTER CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL LT ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT ENGINE STARTER MOTOR FAULTY. ONE NEGATIVE BRUSH MISSING WITH THE OTHER NEGATIVE BRUSH LOOSE IN THE BRUSH HOLDER AND EVIDENCE OF SEVERE ARCING AROUND THE BRUSH/PIGTAIL SECURING SCREW. BOTHPOSITIVE BRUSHES WERE LOOSE AND THE BRUSH HOLDERS WITHSEVERE ARCING AROUND THE SECURING SCREW. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010403001872001040300187NE 2001 4 3 AU010120 220010216G7200 ENGINE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCB3T HCB3TN3 GL ENGINE BAY MAKING METAL W K NONE O OTHER ININSP/MAINT 1 AUS 4811 (AUS) ENGINE CHIP DETECTOR CONTAMINATED BY METAL CHIP. SUSPECT CHIP WAS A PART OF A TAB WASHER. 1L72 4T4 T A24CE E4EA 6 CP15EA 20010403001882001040300188CE 2001 4 3 AU010121 120010115G551104320016 RIB CESSNA150 150M 2071830CE CONT O200 O200A 17020SO MCAULY1A102 1A102OCM GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER FORWARD ATTACHMENT RIBS CRACKED. 1H71 3O3 O 3A19 E252 5 NP918 20010403001892001040300189CE 2001 4 3 AU010122 120010115G5511043200146 RIB CESSNA150 150M 2071830CE CONT O200 O200A 17020SO MCAULY1A102 1A102OCM GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) HORIZONTAL STABILISER FORWARD ATTACHMENT RIBS CRACKED. 1H71 3O3 O 3A19 E252 5 NP918 20010403001902001040300190EU 2001 4 3 AU010124 220010206G73210164168200 FUEL CONTROL SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU NR 2 ENGINE FAULTY W A UNSCHED LANDING EJ VIBRATION/BUFFET WARNING INDICATION CRCRUISE 1 AUS 258 (AUS) NR 2 ENGINE FUEL CONTROL UNIT FAULTY. 2G72 4U4 U H4EU E12NE 20010403001932001040300193SO 2001 4 3 AU010126 120010206G524312007993614 DOOR EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE HYDRAULIC BAY SEPARATED W O OTHER D INFLIGHT SEPARATION NRNOT REPORTED 1 AUS (AUS) RT HYDRAULIC BAY DOOR FAILED AND SEPARATED DURING FLIGHT. DOORHAD BEEN OPENED FOR MAINTENANCE BEFORE FLIGHT AND IT IS SUSPECTED THAT IT WAS NOT PROPERLY CLOSED AND LATCHED. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010403001942001040300194NM 2001 4 3 AU010127 120010204G7603 CABLE RROYCE RB211524D4 BOEING747 747SP38 NM RROYCERB211 RB211524D41954555NE POWER LEVER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE THRUST CONTROL SYSTEM CABLES, PULLEYS AND FITTINGS DAMAGED. FOUND DURING INSPECTION IAW AD/B747/229 AND FAAAD/2000-05-30 AMDT39-11640. 2L74 4F4 FRTA20WE E12EU 20010403001952001040300195CE 2001 4 3 AU010128 120010201G270105131679 WHEEL CESSNA182 182C 2072708CE CONT O470 O470L 17026SO HARTZLHCA2X BHCA2XF1 GL CONTROL COLUMN CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) BOTH CONTROL WHEELS CRACKED FROM BOTTOM RIVET HOLE. 1H71 3O3 ONT3A13 E273 5 CP908 20010403001962001040300196NM 2001 4 3 AU010129 120010202G261251291001 FIRE LOOP BOEING747 747338 NM RROYCERB211 RB211524D41954555NE APU BAY MALFUNCTIONED W FA ACTIVATE FIRE EXT. UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) APU LOWER DOOR FIRE DETECTOR LOOP HAD HIGH RESISTANCE. FALSE WARNING INDICATION RESULTED IN DISCHARGE OF FIRE BOTTLE. 2L72 4F4 FRTA20WE E12EU 20010403001972001040300197NM 2001 4 3 AU010130 120010202G2910 HOSE BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU HYDRAULIC SYS FAILED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) LT MAIN LANDING GEAR DOWNLOCK HYDRAULIC HOSE SPLIT. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA16WE E21EU 20010403001982001040300198NM 2001 4 3 AU010131 120010110G3260841005 PSEU DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE MLG FAULTY W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 AUS (AUS) LANDING GEAR PROXIMITY SWITCH ELECTRONIC UNIT (PSEU) FAULTY. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010403002002001040300200SO 2001 4 3 AU010132 220010202G8530 EXHAUST VALVE CESSNA206 U206F 2073333CE CONT O520 IO520F 17032SO MCAULY3A32C D3A32C90 GL ENGINE LEAKING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE EXHAUST VALVE LEAKING. 1H71 3O3 O A4CE E5CE 5 CP21EA 20010403002012001040300201SO 2001 4 3 AU010133 120010207G532012043522001LH BEAM EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE CABIN CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLIGHT ATTENDANT SEAT SUPPORT FRAMES CORRODED. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010403002022001040300202SO 2001 4 3 AU010134 120010207G532012025916001RH BEAM EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE CABIN CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FLIGHT ATTENDANTS SEAT SUPPORT FRAMES CORRODED. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010403002032001040300203EU 2001 4 3 AU010135 120010203G7712P66230C ENGINE BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP ROTOL R333 R333482F12 GL LEFT OUT OF ADJ W C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT ENGINE RPM ROLLBACK. SUSPECT CAUSED BY NR 1 TORQUE BRIDGE PIT OUT OF ADJUSTMENT. 2L72 4T4 TRTA56EU E4WE 6 CP61GL 20010403002042001040300204SO 2001 4 3 AU010136 120010206G21332091G010800 OUTFLOW VALVE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE CABIN PRESSURE FAULTY W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 AUS 4884 (AUS) PRESSURISATION SYSTEM OUTFLOW VALVE FAULTY. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010403002052001040300205SO 2001 4 3 AU010137 120010126G2751487927 SWITCH PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL LT WING TE FLAPSFAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LH WING FLAP UPLIMIT MICROSWITCH FAILED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403002062001040300206CE 2001 4 3 AU010138 120010220G35101013800491 HOSE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE MCAULY4HFR344HFR34C754 NE CREW OXYGEN SPLIT W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) COPILOTS OXYGEN HOSE FAILED. HOSE HAD BEEN INCORRECTLY FITTED WITH A TIGHT RADIUS. 1L72 4T4 T A24CE E4EA 6 C3PNE 20010403002072001040300207GL 2001 4 3 AU010139 220010123G72106877180 GEARBOX BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL ENGINE MAKING METAL W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 AUS (AUS) ENGINE GEARBOX OUT OF LIMITS. CHIP DETECTORS CONTAMINATED WITHMETAL PARTICLES. 1G71 3U3 U H2SW E4CE 20010403002082001040300208EU 2001 4 3 AU010140 120010119G5302332A2400200001 STRUCTURE SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU TAIL BOOM CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL BOOM CRACKED IN AREA OF PYLON DECK. 2G72 4U4 U H4EU E12NE 20010403002092001040300209SO 2001 4 3 AU010141 120010213G7112 BAFFLE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE AIR DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE BAFFLES DAMAGED. FOUND DURING INSPECTION IAW AD/PA31/96REQ1. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403002102001040300210EA 2001 4 3 AU010142 220010119G8530LW16740 EXHAUST VALVE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 AUS 1146 (AUS) LH ENGINE EXHAUST VALVES (2OFF) ERODED. RT ENGINE EXHAUST VALVES(4OFF) ERODED. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010403002112001040300211NE 2001 4 3 AU010143 220010215G7200RB211524G ENGINE BOEING747 747438 NM RROYCERB211 RB211524G19 NE NR 4 FIRE W FA ACTIVATE FIRE EXT. UNSCHED LANDING AJ FLAME/FIRE WARNING INDICATION CLCLIMB 1 AUS 16202 (AUS) NR 4 ENGINE FIRE. INVESTIGATION FOUND FIRE/HEAT DAMAGE TO WIRING AND CLAMPS IN AREA OF COMBUSTION CHAMBER COWLING. 2L74 4F4 FRTA20WE E30NE 20010403002122001040300212NM 2001 4 3 AU010144 120010216G2741 WIRE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HORIZONTAL STAB WORN W O OTHER J WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) HORIZONTAL STABILISER SURFACE POSITION INDICATOR WIRE CHAFED ANDSHORT CIRCUITING INSIDE CONDUIT LOCATED BETWEEN THE FORWARD SPAROF THE HORIZONTAL STABILISER AND THE RT ELEVATOR SYNCHRO. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010403002132001040300213NE 2001 4 3 AU010146 220010208G7321CPW3111697503B EEC DHAV DHC8 DHC8202 2809007NM PWA 120 PW123D 52152NE HAMSTD14SF 14SF23 NE LT ENGINE OUT OF ADJ W C ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT ENGINE ELECTRONIC UNIT AUTO-FEATHER OPERATION FUNCTION OUT OF ADJUSTMENT. UNIT HAD BEEN ADJUSTED ON THE PREVIOUS NIGHT WITHOUTCHECKING THE AUTO-FEATHER FUNCTION. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000012001040400001NE 2001 4 4 AU010038 320010111G61117922141 TAPE HAMSTD SFA13MIOA DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE PROPELLER BLADE LOOSE W O OTHER O OTHER CLCLIMB 1 AUS (AUS) LT PROPELLER BLADE LEADING EDGE TAPE LOOSE ON ONE BLADE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000142001040400014CE 2001 4 4 CA010219009 120010129G275005235372 ROD CESSNA172 172N 2072434CE LYC O320 O320D2J 41508EA TE FLAPS BENT W K NONE O OTHER ININSP/MAINT 1 CA 9627 (CAN) FLAP ROD BENT. 1H71 3O3 ONT3A12 E274 20010404000172001040400017EU 2001 4 4 CA010219018 120010201G261172111211000 SMOKE DETECTOR BAG JETSTMJETSTM3101 1500215EU GARRTTTPE331TPE33110UG 01514WP ROTOL R333 R333482F12 GL CARGO POD FAILED W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CA (CAN) JUST AFTER TAKEOFF OUT OF LA RONGE HEADING NORTH APPROXIMATELY 80 MILES, THE BAGGAGE POD SMOKE ALARM WENT OFF. THE AIRSCREW TURNED AROUND, & DECLARED AN EMERGENCY TO LANDED BACK IN YVC. MAINTENANCE FOUND NO SMOKE OR FIRE IN THE POD. THE SMOKE DETECTOR WAS REMOVED, THE LENSE WAS CLEANED, DETECTOR REINSTALLED AND TESTED S. THIS IS AN ONGOING PROBLEM WITH THIS UNIT IN THAT IF THE LENSE (SENSOR) GET A LITTLE DUSTY, IT WILL GIVE FALSE INDICATION. AIRCRAFT WAS REKEASED FOR SERVICES. 2L72 4T4 TRTA21EU E4WE 6 CP61GL 20010404000192001040400019EA 2001 4 4 CA010219021 220010205G8500 ENGINE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RIGHT FAILED W A UNSCHED LANDING RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 CA 821 (CAN) AFTER TAKEOFF OUT OF URANIUM CITY PILOT HAD TO RETURN TO AIRPORT AFTER EXPERIENCING LOSS OF POWER ON RT ENGINE. MAINTENANCE INVESTIGATED AND FOUND THAT THE ACCESSORY CASE COMPONENT DRIVE GEARS WOULD NOT TURN. ALSO FOUND OIL FILTER FULL OF METAL. MATINTENANCE SUSPECTS THAT ONE OF THE DRIVE GEARS IN THE ACCESSORY CASE HAS LET GO. ENGINE IS BEING SENT TO PRO AERO ENGINES FOR STRIP DOWN AND REPAIR. FURTHER REPORT TO FOLLOW. 1L72 3O3 O A20SO E14EA 20010404000232001040400023NM 2001 4 4 CA010222010 120010205G272082700544001 CONTROL CABLE DHAV DHC8 DHC8* NM PWA 120 PW120 NE RUDDER BROKEN W D RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA (CAN) AFTER ENGINE STARTING, BEFORE TAXIING OUT FOR TAKEOFF, CREW CHECKED CNTLS FOR FREEDOM OF MOVEMENT. AT THAT TIME, PILOT FOUND THAT RUDDER PEDALS WERE NOT HAVING ANY RESISTANCE WHEN MOVED&WITH BOTH ENGINES RUNNING HE COULD NO T SEE ANY RUDDER MOVEMENT ON AFCS IND. AT TIME HE CALLED OFF FLT, SHUTDOWN ENGINES&CALLED MAINT. MAINTENACE CREW ARRIVED ATTHE SCENE FOUND RUDDER CABLE ASSY BROKEN. DETAILED INSP IN THE AREA REVEALED RUDDER CABLE ASSY NEXT TO 1ST ONE - DAMAGED, CORRODED, WITH 30 PERCENT OF DIAMETER, WIRES BROKEN. LOOKING TO GET ACCESS TO ALL INVOLVED AREA, THOROUGH INSP REVEALED PORT SIDE ELEV CABLE ASSY 2H72 4T4 TRTA13NM E20NE 20010404000242001040400024NM 2001 4 4 CA010222011 120010206G49408Z7591125 BRACKET DHAV DHC8 DHC8* NM PWC 150 PW150A EA APU DAMAGED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING TROUBLESHOOTING FOR APU FAILED START, THE GROUND CABLE FROM APU SHUNT WAS FOUND SEPARATED FROM 4900-GS10 (STN X792) ON BRACKET. THE ATTACHMENT BRACKET WAS FOUND BURNT AS WELL AS THE CABLE CONNECTION. SYD WAS ISSUED AND THE CABLE WAS REPAIRED AND INSTALLED. BASED ON THE INFORMATION PROVIDED BY THE OPERATOR, IT IS BELIEVED THAT THE MOST PROBABLE CAUSE OF DAMAGE WAS IMPROPER INSTALLATION TORQUING OF THE GROUND STUD AND ATTACHING HARDWARE. 2H72 4T4 TRTA13NM E00062EN 20010404000252001040400025CE 2001 4 4 CA010222015 120010212G2752D14500462 TRANSMISSION CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL TE FLAPS FAILED W D RETURN TO BLOCK F FLT CONT AFFECTED TXTAXI/GRND HDL 1 CA (CAN) AFTER LANDING THE PILOTS SELECTED FLAPS TO THE UP POSITION AND THE FLAP CIRCUIT BREAKER POPPED. THE FLAP CIRCUIT BREAKER WAS RESET AND THE FLAPS WERE SELECTED UP NORMALLY. WHEN THE FLAPS WERE RESELECTED TO THE DOWN POSITION THE CIRCUIT BREAKER POPPED AGAIN. THE FLAP TRANSMISSION AND MOTOR ASSEMBLY WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010404000262001040400026CE 2001 4 4 CA010222016 120010212G7160NAS561C410 ROLL PIN CESSNA 26520251 CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE MCAULY3AF34C3GFR34C703 GL BELLCRANK BROKEN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING THE ROUTINE 100 HOUR INSPECTION THE AIRCRAFT ENGINEER FOUND THAT THE ROLL PINS, QUANTITY 4, SECURING THE BELL CRANK TO THE AIR BYPASS DUCT FOR THE ENGINE, WERE LOOSE. UPON RMEOVAL WE FOUND THAT ALL FOUR PINS WERE BROKEN. PIN REPLACED WITH NEW. 1H71 3T3 T A37CE E4EA 5 CP60GL 20010404000282001040400028CE 2001 4 4 CA010223002 120010206G6100 BLADE MCAULY 1C172MDM CESSNA172 172 2072402CE CONT O300 O300A 17022SO MCAULY1C172 1C172MDM GL PROPELLER CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 765 633 71581 (CAN) EXTRA WORK REQUIRED TO REMOVE CORROSION FROM BLADE FACE (CAMBER FACE) IN ACCORDANCE WITH MCCAULEY MANUAL 730720. 1H71 3O3 ONT3A12 E253 5 NP910 20010404000322001040400032NM 2001 4 4 CA010223007 120010131G243523088002B STARTER GEN DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 2 ENGINE DISINTEGRATED W D RETURN TO BLOCK E VIBRATION/BUFFET TXTAXI/GRND HDL 1 CA 15963773 611A (CAN) A VIBRATION WAS FELT DURING START-UP ON NR 2 ENGINE AND THEN DURING TAXI THE NR 2 D.C. GENERATOR LIGHT CAME ON. THE CREW WERE UNABLE TO SUCCESSFULLY RESET THE NR 2 GENERATOR AND RETURNED TO THE GATE. INVESTIGATION REVEALED THE NR 2 GENERATOR FAN END BEARING HAD FAILED. STARTER GENERATOR REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000332001040400033NM 2001 4 4 CA010223008 120010120G291082970010391 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC SYS LEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA 31326 (CAN) UPON ARRIVAL AT THE GATE HYDRAULIC FLUID WAS NOTICED TO BE LEAKING FROM THE LT WHEEL WELL AREA. INVESTIGATION REVEALED THAT THE AFT NR 1 DOOR CLOSE LINE WAS LEAKING.LINE REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000342001040400034NM 2001 4 4 CA010223010 120010120G291082950010277 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE O OTHER ININSP/MAINT 1 CA 25366 (CAN) A PUDDLE OF HYDRAULIC FLUID WAS NOTICED AROUND THE LT MAIN WHEEL AREA. INVESTIGATION REVEALED THAT THE LEAK WAS COMING FROM THE LT OUTBOARD ROLL SPOILER LIFT DUMP LINE.LINE REPLACED. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000382001040400038CE 2001 4 4 CA010226002 120010215G2431A876K TERMINAL CESSNA560 560XL CE PWA 545 PW545A NE BATTERY FAILED W K NONE O OTHER ININSP/MAINT 1 CA 474 (CAN) AIRCRAFT ARRIVED AT ST. HUBERT (YHU) PILOTS SHUT DOWN ENGINES AND APU, HAD NO POWER ON AIRCRAFT WITH BATTERY SWITCH ON BATTERY. PILOT TOOK SWITCH AND TOGGLED IT TO OFF AND THEN TO EMERGENCY POWER AND STILL NO POWER ON AIRCRAFT. UNABLE TO PUT BATTERY ON LINE. 2L72 4F4 FRTA22CE E00059EN 20010404000392001040400039EA 2001 4 4 CA010226005 120010203G4990 APU CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE APU BAY LEAKING W O OTHER KJ FLUID LOSS WARNING INDICATION APAPPROACH 1 CA (CAN) THE CREW REPORTED THE SMOKE TOILET CAUTION MESSAGE AT 9000 FEET. SMOKE WAS VISIBLE WHEN BLEED WAS TRANSFERRED IN CABIN AND COCKPIT WHEN BLEEDS WERE TRANSFERRED TO APU. AIRCRAFT DID AN EMERGENCY LANDING.THE MAINTENANCE FOUND OIL COMING FROM COMPRESSOR DRAIN OF THE APU. APU WAS DEFERRED TO BE REPLACED LATER. 2L72 4F4 FRTA21EA E15NE 20010404000402001040400040EA 2001 4 4 CA010226008 120010206G5610601R3303312 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CRCRUISE 1 CA (CAN) THE RT WINDSHIELD SHATTERED IN CRUISE DURING THE FLIGHT NR 5.THE MAINTENANCE REPLACED THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010404000412001040400041EA 2001 4 4 CA010226009 120010206G5610601R330339 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT FAILED W O OTHER O OTHER CLCLIMB 1 CA (CAN) THE LT WINDSHIELD SHATTERED IN CRUISE AT 35,000 DURING THE FLIGHT NR 5.THE MAINTENANCE REPLACED THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010404000422001040400042EA 2001 4 4 CA010226010 120010202G5610NP1393222 WINDOW CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE COCKPIT CRACKED W O OTHER O OTHER CRCRUISE 1 CA (CAN) THE RT WINDOW CRACKED IN CRUISE. THE MAINTENANCE REPLACED THE WINDOW. 2L72 4F4 FRTA21EA E15NE 20010404000432001040400043EA 2001 4 4 CA010226011 220010205G74144347 MAGNETO HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA ENGINE FAILED W O OTHER E VIBRATION/BUFFET TXTAXI/GRND HDL 1 CA 576 (CAN) AIRCRAFT HARD TO START. RETARD LOW INTENSITY SPARK. REPLACED MAGNETO. 1G71 3O3 OO 4H12 E286 20010404000442001040400044SW 2001 4 4 CA010226012 120010125G8011SAZ4401 RELAY HUGHES269 269C1 8059504SW LYC O360 HO360C1A 41514EA STARTER FAILED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA (CAN) ENGAGEMENT INTERMITTENT DUE TO VIBRATION. REPLACED STARTER RELAY. 1G71 3O3 OO 4H12 E286 20010404000462001040400046EA 2001 4 4 CA010226018 220010101G74144250R MAGNETO CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160DTM GL ENGINE FAILED W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION CRCRUISE 1 CA 525 (CAN) ENGINE STARTING RUNNING ROUGH IN CRUISE FLIGHT PILOT RETURNED TO STATION. GROUND RUN INDICATED EXCESSIVE RPM LOSS ON RT MAGNETO. MAGNETO REPLACED AND FOLLOW UP GROUND RUN CARRIED OUT RESULTING IN NORMAL RPM (STATIC) AND RT RPM DROP WITHIN LIMITS. NO APPARENT EXTERNAL PROBLEMS WITH MAGNETO COULD BE IDENTIFIED. AN SC REPORT MAY FOLLOW SHOULD WE CHOOSE TO HAVE THE MAGNETO OVERHAULED. 1H71 3O3 ONT3A12 E274 5 NP910 20010404000472001040400047WP 2001 4 4 CA010226020 220010201G7412103784005C EXCITER GULSTM690TP 690D 3970405SW GARRTTTPE331TPE331* 01514WP ROTOL R306 R306382F7 GL LT ENGINE SHORTED W O OTHER O OTHER TXTAXI/GRND HDL 1 CA 5 (CAN) LT ENGINE WOULD NOT START. NO IGNITION. IGNITION SYSTEM CHECKED AND THE EXCITER WAS FOUND TO BE AT FAULT. 1H72 3T3 T 2A4 E2WE 6 CP8EU 20010404000482001040400048NM 2001 4 4 CA010228008 120010206G6320A0061 GEARBOX ROBSINR22 R22BETA NM LYC O360 O360J2A 41514EA MAIN ROTOR FAILED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 1747 (CAN) MAIN ROTOR GEARBOX CHIP DETECTOR LIGHT ACTIVATED IN FLIGHT. PILOT LANDED ON GROUND LIGHT WENT OUT. CHIP DETECTOR REMOVED AT MAINTENANCE FACILITY. FUZZ PARTICULATE FOUND, DETECTOR CLEANED, INSPECTED, REINSTALLED. HELICOPTER GROUND RUN ON GROUND FOR 30 MINUTES WITH NO LIGHT INDICATION. GEARBOX OIL REPLACED AT CUSTOMER REQUEST. 1G71 3O3 O H10WE E286 20010404000502001040400050NE 2001 4 4 CA010301002 220010103G7310226311001 LINE HONEYWELL BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE ENGINE FUEL MISREPAIRED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) DURING RECEIPT OF A LOANER ENGINE, IT WAS NOTED THAT ONE OF THE INSTALLED LINES FROM THE FLOW DIVIDER TO THE FUEL MANIFOLD HAD AN UNAPPROVED WELD REPAIR ACCOMPLISHED ON IT. THE LINE WAS REPLACED. 2H74 4F4 FRTA49EU E6NE 20010404000512001040400051NM 2001 4 4 CA010301004 120010127G291082950010175 LINE DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYDRAULIC SYS LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 CA (CAN) DURING ROUTINE INSPECTION, HYDRAULIC FLUID WAS FOUND LEAKING FROM THE LT WING INBOARD FLAP CANOE. INVESTIGAITON RESULTED IN REPLACEMENT OF A LEAKING FLIGHT SPOILER UNLOAD LINE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404000522001040400052EA 2001 4 4 CA010301005 120010209G7112311269001 ADAPTER DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE HAMSTD14SF 14SF15 NE VENTURI CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING SCHEDULED INSPECTION OF THE R/H ENGINE, THE ENGINE BLEED AIR VENTURI ADAPTER WAS FOUND TO HAVE A V SHAPED CRACKED ON THE OUTSIDE OF THE 90 DEGREE BEND OF THE VENTURI. THE VEE HAD OPENED UP, ALLOWING BLEED AIR TO BE DUMPED INTO THE ENGINE COMPARTMENT. THE ADAPTER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (THIS AREA OF THE ADAPTER IS COVERED WITH A SHROUD, MAKING INSPECITON A DELIBERATE ACTION.) 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010404001962001040400196NE 2001 4 4 CA010301017 220010117G7200 ENGINE BOEING767 7673S1 1385211NM GE CF6 CF680C2B2 30025NE RIGHT FAILED W E ENGINE SHUTDOWN Y ENGINE STOPPAGE LDLANDING 1 CA 3233832338 720611 (CAN) ON FINAL INTO YYZ, RIGHT ENGINE SHUTDOWN, 4 MINUTES TO LANDING. ENGINE SHUTDOWN CHECKLIST COMPLETED. LANDED WITHOUT INCIDENT. ON INSPECTION OF RT ENGINE METAL FOUND IN TAILPIPE. RT ENGINE REPLACED. OFF PART NUMBER 6-7200-9-0002, SERIAL NUMBER 2611.2001-03-06 TC: EXPECT OPERATOR TO FOLLOW-UP WHEN TEAR DOWN AVAILABLE. 2L72 4F4 FRTA1NM E13NE 20010404001992001040400199NE 2001 4 4 CA010301029 120010216G6210S611520107 BLADE SKRSKYS61 S61N 8142104NE GE CT58 CT581401 30011NE MAIN ROTOR DEBONDED W K NONE O OTHER ININSP/MAINT 1 CA 8770 (CAN) AIRCRAFT LANDED TO REFUEL. IT WAS NOTED THAT DURING A WALKAROUND THAT, A ROTOR BLADE POCKET HAD BECOME DEBONDED. A TEMPORARY REPAIR WAS MADE AND THE AIRCRAFT WAS FLOWN BACK TO BASE. 2G72 4U4 U 1H15 1E3 20010404002002001040400200EA 2001 4 4 CA010301030 120010301G275072740196011 TUBE DHAV DHC7 DHC7103 2802710EA PWA PT6 PT6A50 52043EA HAMSTD24PF 24PF305 GL FLAP DRIVE WORN W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING INSPECTION, SEVERE WEARING WAS NOTED ON OUTBOARD FLAP DRIVE SECONDARY DRIVE TUBE P/N 72740196-011 BY THE STEADY BEARINGS. UNABLE TO DETECT WEAR PROPERLY UNLESS STEADY BEARING REMOVED. WEAR WAS FOUND ON BOTH SIDES OF FLAP DRIVE SYSTEM. MAXIMUM WEAR FOUND 0.0265 INCH. TUBE THICKNESS APPROXIMATELY 0.040. BOTH WORN TUBES REPLACED WITH SERVICEABLE UNITS. 2H74 4T4 T A20EA E4EA 6 CP1NE 20010404002012001040400201NE 2001 4 4 CA010301031 120010209G29103935 SHUTOFF VALVE SKRSKYS76 S76A 8143006NE ALLSN 250C 250C30S 03013GL ACTUATOR LEAKING W ED ENGINE SHUTDOWN RETURN TO BLOCK KJ FLUID LOSS WARNING INDICATION TXTAXI/GRND HDL 1 CA 162 (CAN) ON START UP THE NR 1 SERVO JAM WARNING LIGHT WOULD NOT EXTINGUISH WHEN NORMAL HYDRAULIC PRESSURE WAS REACHED. THE FLIGHT CREW SHUT DOWN AND UPON EXITING THE AIRCRAFT SAW HYDRAULIC FLUID UNDER THE AIRCRAFT. THE ENGINEER FOUND THE NR 1 HYDRAULIC SYSTEM FLUID LOW WHICH CAUSED THE NR 1 SERVO JAM LIGHT TO STAY ON. FURTHER INVESTIGATION FOUND THE TAIL SERVO SHUT OFF VALVE LEAKING FROM THE ELECTRICAL ACTUATOR BODY. THE VALVE WAS REPLACED, NR 1 HYDRAULIC SYSTEM REPLENISHED AND BLED. THE AIRCRAFT WAS TEST FLOWN AND THEN RETURNED TO SERVICE. 1G72 3U3 U H1NE E1GL 20010404002022001040400202EA 2001 4 4 CA010301032 120010213G3246901230602 FITTING DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE LT FLOAT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CORROSION AND STRESS CRACK DEVELOPED ON THE TAPER HOLE OF THE SPREADER BAR ATTACH FITTING LT FLOAT AFT SPREADER ATTACH P/N 901-23060-2 WAS REMOVED AND QUARANTINED. REPLACEMENT P/N S1901-23060-2 INSTALLED AS PER STC SF-92-7. 1H71 3R3 R A806 5E1 20010404002032001040400203EA 2001 4 4 CA010301033 120010213G3246901230602 FITTING DHAV DHC2 DHC2MK1 2800102EA PWA R985 R985AN14B 52008NE LT FLOAT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) CORROSION AND STRESS CRACK DEVELOPED ON THE TAPER HOLE OF THE SPREADER BAR ATTACH FITTING RT FLOAT FORWARD SPREADER ATTACH WAS REMOVED AND QUARANTINED. REPLACEMENT P/N S1901-23060-2 INSTALLED AS PER STC SF-92-7. 1H71 3R3 R A806 5E1 20010404002042001040400204EA 2001 4 4 CA010301035 220010216G8540LW10292 IDLER GEAR PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA ENGINE WORN W K NONE O OTHER ININSP/MAINT 1 CA 820 (CAN) THE IDLER GEAR BETWEEN THE CRANKSHAFT AND THE CAMSHAFT GEAR DISENGAGED DUE TO FRACTURING OF THE CRANKCASE AND ACCESSORY CASE. THESE FRACTURES ARE DIRECTLY OPPOSITE THE CRAN GEAR AND WOULD INDICATE THAT A SOLID OBJECT WENT IN BETWEEN THE CRANK GEAR AND IDLER GEAR. THE UPPER ROW OF TEETH ON THE IDLER, DRIVES THE MAGNETO AND THERE IS ONE TOOTH MISSING. THIS MISSING TOOTH IS PROBABLY WHAT WENT IN BETWEEN THE GEARS. 1L72 3O3 O A20SO E14EA 20010404002052001040400205EA 2001 4 4 CA010301036 220010212G72503027102 TURBINE BLADES PWA PT6T PT6T3 52045EA ENGINE WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 3000 (CAN) POWER TURBINE SECTION DISASSEMBLED FOR EVALUATION. POWER TURBINE BLADES SHOWED A DIFFERENT CONFIG THAN P/N 3027102 POWER TURBINE BLA DES NORMALLY FOUND ON THIS MODEL ENGINE. ALSO PART NO (P/N 3013102) STAMPED ON BLADES WAS CROSSED OUT & P/N 3027102 WAS ENGRAVED. P&W WAS NOTIFIED & RESPONDED THAT SUBJECT BLADES WERE APPLICABLE TO A PT6A ENGINE & NOT PT6T. THEY ALSO STATED THAT THERE IS NO APPRD MODS THAT WOULD ALLOW 3013102 BLADES TO BE REIDENTIFIED. P&WSTATES BLADES MUST BE REMVD FROM SERVICE. 2001-03-05 TC: FORWAEDED TO MAINT & MFG S.U.P. 4 U E22EA 20010404002072001040400207EU 2001 4 4 CA010302007 120010214G2912583400 FILTER 704A44633025SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE HYD SYSTEM CLOGGED W A UNSCHED LANDING F FLT CONT AFFECTED HOHOVERING 1 CA 257 (CAN) - UPON HOVERING IN AERIAL LONG LINE WORK. THE PILOT NOTICED SOME FEEDBACK IN CYCLIC CONTROLS WHEN INPUTING AGGRESSIVE MOVEMENTS (I.E. WINDY CONDITIONS). HE IMMEDIATELY ABORTED THE TASK AT HAND AND LANDED.- ON INSPECTION OF HYDRAULIC FILTER FOUND A BLACK DEPOSIT IN FILTER MEDIA.- THIS IS ABNORMAL CONSIDERING THE 500 HR FILTER LIFE, AND TAFT OF 257.2 HOURS. - POSSIBLE CAUSE: DEPOSITS INSIDE HYDRAULIC LINES AND COMPONENTS AT TIME OF MANUFACTURE AND HIGH DETERGENT ATTRIBUTES OF AEROSHELL FLUID 41). 1G71 3U3 U H9EU E19EU 20010404002102001040400210CE 2001 4 4 CA010302010 120010131G3230ALM50 CURRENT LIMITER BEECH 200 200BEECH 1152920CE PWA PT6 PT6A41 52043EA HARTZLHCD4N3HCD4N3A GL MLG FAILED W O OTHER J WARNING INDICATION APAPPROACH 1 CA (CAN) AIR NUNAVUT KING AIR WAS ON APPROACH TO IGALUIT AT NIGHT. FLIGHT CREW SELECTED GEAR, THEY RECEIVED AN UNSAFE GEAR INDICATION AND HAD TO USE GEAR EMERGENCY EXTENSION METHOD, AFTER WHICH GAVE 3 GREEN GEAR DOWN AND LOCKED INDICATION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. AN INSPECTION OF LANDING GEAR SYSTEM WAS ACCOMPLISHED. IT WAS DISCOVERED THAT R/H GENERATOR BUS POWER LIMITER HAD FAILED. MAINTENANCE WAS UNSUCCESSFUL AT FINDING A CAUSE FOR LIMITER FAILURE. NEW POWER LIMITER INSTALLED. GEAR SWINGS ACCOMPLISHED AS PER AVIA DESIGNS MAINTENANCE MANUAL. AIRCRAFT RETURNED TO SERVICE. 1L72 4T4 T A24CE E4EA 5 CSTC 20010404002112001040400211EU 2001 4 4 CA010302012 120010302G62401179405303 INDICATOR BOLKMS117 BK117A4 5626017EU LYC LTS101LTS101650B1 41560NE TRIPLE TACH FAULTY W A UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CA 12 468 (CAN) NR (ROTOR RPM) NEEDLE STARTED TO READ LOW. PILOTS RECOGNIZED THIS AS AN INDICATION PROBLEM. PILOTS LANDED AT BASE WITHOUT INCIDENT. PROBLEM WAS CORRECTED BY INSTALLING A SERVICEABLE TACHOMETER. 1G72 3U3 U H13EU E5NE 20010404002132001040400213CE 2001 4 4 CA010302014 120010209G304010138402522 WINDSHIELD BEECH B300 B300 1159232CE PWA PT6 PT6A60A 52043NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA 1205 98108H3288 (CAN) WHILE IN CRUISE FLIGHT AT FL310 AND OAT -46 DEGREES C, A LOUD BANG WAS HEARD AND THE RT WINDSHIELD CRACKED. (WINDSHIELD HEAT HAD BEEN ON FOR THE ENTIRE FLIGHT (1 HOUR PLUS)). FLIGHT CREW REFERENCED ABNORMAL OCCURRENCE IN POH AND MADE AN UNSCHEDULED, UNEVENTFUL LANDING IN YYC. AIRCRAFT GROUNDED FOR WINDSHIELD REPLACEMENT. NOTE: SIMILAR OCCURRENCE TO LT WINDSHIELD FAILURE IN OCTOBER 1999. 2L72 4T4 TRTA24CE E4EA 20010404002212001040400221NM 2001 4 4 CA010306015 120010128G2120 UNKNOWN DHAV DHC8 DHC8* NM PWC 150 PW150A EA CABIN ODOR W A UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 CA (CAN) DURING A TAKEOFF A SMELL WAS NOTED AND INCREASE DRAMATICALLY DURING THE CLIMB. CREW NOTED THAT THERE WAS NO VISIBLE SIGN OF SMOKE. CREW RETURNED TO BASE FOR INVESTIGATION. MAINTENANCE CARRIED OUT AN APU START, BLEED ON, SMELL PRESENT FOR 2 MIN. THEN DISAPPEARED. ENGINE RUN PERFORMED NO SMELL. DC CONTACTOR BOXES CHECKED, NO FAULT. AREA AROUND WATER BOILER INSPECTED, NO FAULT. EPCU CHECKED FOR FAULT CODES, NO FAULT. CDS CHECKED, NO FAULT. ENGINE RUN PERFORMED AGAIN, NO FAULT. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E00062EN 20010404002292001040400229CE 2001 4 4 CA010302006 120010214G531207126161 BULKHEAD CESSNA182 182H 2072718CE CONT O470 O470R 17026SO MCAULY2A34C 2A34C50 GL VERTICAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 4269 (CAN) CRACK ABOVE LT RUDDER STOP BOLT LOCATION ON (BULKHEAD) FLANGE BEND RADIUS DIRECTLY ABOVE BOLT. A/C HANGARED FOR LAST 15 YRS & NOT SUBJECTED TO WIND. REMOVAL & INSP SHOWS POOR STANDARD PRACTISE OF DRIVING 90 DEGS STIFFENER INTO BEND RADIUS OF FLANGE (ASSY IS SANDWICH OF STIFFENERS). THUS WHEN RUDDER STOP BOLT JAM NUT IS TIGHTENED, STIFFENER CUTS INTO BEND RADIUS. REPL PART WORSE&REJECTED (NEW). NEW BULKHEAD STIFFENER PLAC ED SO AS TO RIDE UP BEND RADIUS ENOUGH TO FIT 0.015 FEELER GAUGE. ASSY MANUFACTURED & RIVETED WITH GAP. FEW STROKES WITH FILE WOULD MATCH BEND RADIUS & NOT CAUSE PROBLEM DURING MANUFACTURE: SK210-161-1 WILL BE INST (SEB99-12R1). 1H71 3O3 ONT3A13 E273 5 CP3EA 20010405000662001040500066CE 2001 4 5 CA010307004 120010220G3246C1630030201 WHEEL MCAULY CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA NLG DAMAGED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA (CAN) REPORTED TO MAINTENANCE OF CLICKING NOISE FROM FRONT AREA DURING TAXI. INSPECTION REVEALED THREE (3) THRU BOLTS MISSING ON WHEEL RIM RESULTING IN DAMAGE TO NOSE FORK. TWO OF THREE REMAINING BOLTS FOUND LOOSE. SUSPECT INCORRECT TORQUE ON WHEEL BOLTS. 1H71 3O3 ONT3A12 E274 20010405000672001040500067SW 2001 4 5 CA010307007 120010214G6230206010332121 BEARING BELL 206040002007BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL MAST CORRODED W K NONE O OTHER ININSP/MAINT 1 CA 4456 1461 NOF4734 (CAN) SEVERE PITTING OF LOWER BEARING JOURNAL INNER RACE AT LOWER PORTION OF MAST ASSEMBLY. 1G71 3U3 U H2SW E4CE 20010405000722001040500072SW 2001 4 5 CA010307013 120010109G6510206040102103 COVER BELL 206 206L 1181522SW ALLSN 250C 250C20B 03013GL T/R COUPLING GROOVED W K NONE O OTHER ININSP/MAINT 1 CA 15 (CAN)WHEN REINSTALLING A MAIN DRIVESHAFT AFTER A INPUT TRANSMISSION SEAL REPLACEMENT, FOUND THAT THE TRANSMISSION END OF THE SHAFT COULD NOT MOVE. OPENED THE COUPLING END FOUND THAT SPRINGS WAS NOT INSTALLED PROPERLY. THE COVER WAS GROOVED. INSPECTED THE INNER AND OUTER COUPLING ON BOTH END OF DRIVESHAFT ASSEMBLY. NO MORE DAMAGE FOUND 15.0 HOUR SINCE LAST INSPECTION. COMPLETED THE SHAFT INSPECTION AFTER REPLACING THE COVER AND THE SPRING THAT WERE DAMAGED BY NEW PARTS. A/C WAS RETURNED TO SERVICE. 1G71 3U3 U H2SW E4CE 20010405000742001040500074WP 2001 4 5 CA010307015 120010225G6310 ENGINE LKHEED1011 1011385114 WP RROYCERB211 RB21122B02 54555NE ENGINE FAILED W A UNSCHED LANDING O OTHER CLCLIMB 1 CA 47592 (CAN) AFTER TAKEOFF ENGINE NR 3 VIBS INCREASED TO 2.5 UNITS, THROTTLE RETARDED TO KEEP BELOW LIMITS. AIRCRAFT RETURNED TO MAINTENANCE BASE YMX. TROUBLESHOOTING CARRIED OUT AS PER MM 79-00-00 PAGE 121, ENGINE RUNS CARRIED OUT AS PER TEST NR 21 VIBRATIONS WITHIN LIMITS, AIRCRAFT RETURNED TO SERVICE.SUSPECT OIL FINDING. 2L73 4F4 F A23WE E12EU 20010405000762001040500076NE 2001 4 5 CA010307017 220010218G7200 ENGINE LKHEED1011 1011385115 5265015WP RROYCERB211 RB21122B02 54555NE NR 2 VIBRATION W K NONE O OTHER ININSP/MAINT 1 CA 44530 (CAN) AFTER TAKEOFF (DURING FIRST STAGES OF CLIMB) THE NR 2 ENGINE VIBRATION INCREASED, FLIGHT CREW SHUTDOWN ENGINE IN ACCORDANCE WITH OPERATING PROCEDURE AND RTURNED TO BASE. MAINTENANCE PERFORMED TEST 21 IN ACCORDANCE WITH ROLLS ROYCE PROCEDURES, ENGINE VIBRATIONS RETURNED TO NORMAL, AIRCRAFT RETURNED TO SERVICE. NO FURTHER REPORTED INCIDENTS.MAINTENANCE SUSPECT OIL HIDING AS CAUSE OF ENGINE VIBRATION . 2L73 4F4 F A23WE E12EU 20010405000772001040500077EA 2001 4 5 CA010307018 120010220G3232 BRACE CNDAIRCL600 CL6002B16 1900305EA GE CF34 CF343B1 NE MLG DOOR SHEARED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) AIRCRAFT 604-54F05 WITH TSN OF 611.3 HOURS AND 304 CYCLES HAS BEEN FOUND TO HAVE A BROKEN TRUNNION PIN AT L/H MLG SIDE BRACE ACTUATOR INBOARD END.THIS WAS FOUND AS THE AIRCRAFT WAS ON JACKS AND A TECHNICIAN NOTICED THAT THE GEAR MOVED. THE FORWARD ATTACH NUT WAS SHEARED OFF AND LAYING ON TOP OF THE WING. THIS ALLOWED THE PIN TO MIGRATE APPROXIMATELY 0.3 INCHES AFT, ALLOWING THE GEAR TO MOVE. PART REPLACED. BROKEN PART RETURNED TO BOMBARDIER FOR ANALYSIS.UNDER INVESTIGATION 2L72 4F4 FRTA21EA E15NE 20010405000782001040500078EA 2001 4 5 CA010307021 120010219G5610NP1393215 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) DURING THE PRE-FLIGHT INSPECTION, IT WAS NOTICED THAT THE CAPTAINS WINDSHIELD WAS CRACKED. THE AIRCRAFT RETURNED TO SERVICE AFTER REPLACEMENT OF THE WINDSHIELD. 2L72 4F4 FRTA21EA E15NE 20010405000792001040500079NE 2001 4 5 CA010307024 220010219G7200 ENGINE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE NR 2 FAILED W O OTHER J WARNING INDICATION DEDESCENT 1 CA (CAN) PILOT REPORT IN DESCENT: AUDIT ENGINE OIL AND MASTER WARNING. ENGINE NR 2 OIL PRESSURE RAPIDLY DROPPED TO 0 PSI. CREW INITATED AN IN-FLIGHT SHUTDOWN PROCEDURE, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PARTICLE ON NR 2 CHIP DETECTOR. AT THE TIME OF WRITING THE CAUSE FOR THE LOSS OIL PRESSURE HAS NOT BEEN DETERMINDED. THE CUSTOMER AND THE MANUFACTURER WILL CONTINUE THE INVESTIGATION. 2L72 4F4 FRTA21EA E15NE 20010405000802001040500080EA 2001 4 5 CA010307026 120010219G5730601R10046 PANEL CNDAIRCL600 CL6002B19 EA GE CF34 CF34* NE LT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 18652 (CAN) DURING A SERVICE CHECK, THE MECHANIC FOUND A SUSPECTED CRACK N THE LT WING LOWER SKIN AT WING STATION WS 148.019. THE CRACK WAS CONFIRMED WITH LPI AND EDDY CURENT NDT. THE REPAIR WAS CARRIED OUT PER REPAIR ENGINEERING ORDER 601R-57-21-130. THE AIRCRAFT SUBSEQUENTLY RETURNED TO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405000812001040500081EA 2001 4 5 CA010307027 120010219G5730601R10046 PANEL CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE WING CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 13895 (CAN) DURING A C CHECK INSPECTION, A CRACK WAS FOUND IN THE LOWER WING PLANK AT WING STATION WS 148.019.AT THE TIME OF REPORT, THE AIRCRAFT WAS STILL IN C CHECK. REPAIR ENGINEERING ORDER (REO) 601R-57-21-130 WILL BE APPLIED PRIOR TO RETURNING THE AIRCRAFT INTO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405000822001040500082EA 2001 4 5 CA010307028 120010219G5600NP1393215 WINDOW CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 CA (CAN) WHILE MANOEUVRING ON THE GROUND, THE LT SIDE WINDOW WAS FOUND CRACKED. THE WINDOW WAS REPLACED AND THE AIRCRAFT RETURNED INTO SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405000832001040500083NE 2001 4 5 CA010307030 220010221G7200 ENGINE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE LEFT FAILED W A UNSCHED LANDING E VIBRATION/BUFFET CLCLIMB 1 CA (CAN) ENGINE VIBRATION DURING CLIMB OUT AND LEVEL FLIGHT (FL230). MAXIMUM VALUE WAS 3.3 MILS. LATER FLUCTUATION BETWEEN 2.3 AND 3.3 MILS. ENGINE SHUT DOWN IN FLIGHT. SINGLE ENGINE OPERATION AS PER QRH. CHANGE LEFT ENGINE. REASON: HIGH N1 VIBRATION. 2L72 4F4 FRTA21EA E15NE 20010405000842001040500084EA 2001 4 5 CA010307033 120010222G5270601R317001 SENSOR CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE PASSENGER DOOR OUT OF ADJ W A UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CA (CAN) DURING CLIMB CREW RECD PASSENGER ENTRANCE DOOR WARNING MESSAGE PAX DR LATCH (AMBER) & PASSENGER DOOR (WARNING) EICAS MESSAGES. A/C RETURNED TO DEPTR AIRPORT&LANDED W/O INCID.&LATER FERRIED TO MAINT BA SE. MAINT FINDINGS: 1. PSEU FAULT LOG 2 RECORDED S47 & S46;2. FLT CREW RPT EICAS MESSAGES EXTINGUISHED BELOW 7000 ASI; 3. GREEN ALIGNMENT MARKS ON CAM LATCHES NOT WITHIN RANGE WHEN INNER DOORHANDLE IS SLOWLY ENGAGED; 4. PROX SENSOR PSSMB GAP .068 INCH, .018 INCH BEYOND LIMITS;5. A/C RECORDS SHOWN HAVE BEEN NO ADJUSTMENT MADE TO PSSMB SENSOR OR DOOR MECHANISM WITHIN PAST 30 DAYS. RECTIFICATION 1. PROX SENSOR PSSMB GAP ADJUSTED WITHIN LIMITS;2. INNER DOOR HANDLE STOP ADJUSTED;3. DOOR MECHANISM LUBRICATED A 2L72 4F4 FRTA21EA E15NE 20010405000902001040500090EA 2001 4 5 CA010308007 120010202G492049100011 APU CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE APU BAY DAMAGED W K NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 CA (CAN) SMELL OF FUEL AND SMOKE IN AIRCRAFT AFTER APU STARTED ON DESCENT. EMERGENCY RESPONSE CALLED. FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. APU REPLACED OPERATION AND LEAK CHECK CARRIED OUT AND SYSTEM CHECKED SERVICEABLE. 2L72 4F4 FRTA21EA E15NE 20010405000922001040500092NM 2001 4 5 CA010308011 120010208G2497 WIRE BOEING737 7372Q9 138448MNM PWA JT8 JT8D9A 52048NE FIREWALL CHAFED W K NONE O OTHER ININSP/MAINT 1 CA (CAN) WIRE W200-453-06 CHAFED THROUGH INSULATION AND WIRE. LENGTH & WIDTH OF CHAFE IS 3/8 INCH, DEPTH 1/8 INCH. APPEARS TO HAVE RUBBED AGAINST COWLING AT SOME TIME. HOWEVER, AT TIME OF DISCOVERY, IT WAS NOT APPARENT WHAT THE WIRE HAD CHAFED. THERE HAD BEEN NO REPORTED ELECTRICAL POWER DEFECT. THE HARNESS HAS BEEN REPLACED WITH PARTICULAR EMPHASIS TO CORRECT ROUTING AND CLAMPING. 2L72 4F4 F A16WE E2EA 20010405000932001040500093NM 2001 4 5 CA010308012 120010219G2761654456113 ACTUATOR BOEING737 737201 1384454NM PWA JT8 JT8D9A 52048NE SPOILER LEAKING W O OTHER K FLUID LOSS DEDESCENT 1 CA (CAN) AT APPROXIMATELY 20 MINUTES OUT, THE A SYSTEM HYDRAULIC LIGHT ILLUMINATED. THE HYDRAULIC FLUID GAUGE WAS CHECKED AND FOUND TO BE EMPTY. THE USE OF ALTERNATE FLAP AND GEAR EXTENSION WAS REQUIRED. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE FIRE DEPARTMENT WAS ALERTED AND STANDING BY AS A PRECAUTION MEASURE. MAINTENANCE FOUND THE LEFT INBOARD FLIGHT SPOILER ACTUATOR LEAKING. 2L72 4F4 F A16WE E2EA 20010405000942001040500094CE 2001 4 5 CA010308013 120010212G551010138000110 BOOT BEECH B300 BEECH B300 B300 1159232CE PWA PT6 PT6A60A 52043NE HORIZ STAB DEICEDETACHED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA 3880 FL26 (CAN) AIRCRAFT WAS IN CLIMBOUT FROM ST.JOHNS AIRPORT, AT 22,000 FEET, AIRSPEED 140 KNOTS, RATE OF CLIMB 1,800 F.P.M., PILOT EXPERIENCED SEVERE BUFFETING TO THE POINT THAT A/C WAS ABOUT TO STALL. STALL WARNING DID NOT ACTIVATE, A/C WAS PLACED IN LEVEL FLIGHT AND BUFFETING STOPPED. A/C RETURNED TO ST. JOHNS FOR MAINTENANCE. UPON INSPECTION MAINTENANCE DISCOVERED THAT THE RIGHT DE-ICER BOOT HAD DETACHED FROM THE HORIZONTAL STABILIZER ON THE OUTBOARD END. NEW DE-ICER BOOTS WRE INSTALLED ON THE LEFT AND RIGHT SIDE, A/C WAS TEST FLOWN ALL FLIGHT CHARACTERISTICS NORMAL. 2L72 4T4 TRTA24CE E4EA 20010405000962001040500096SW 2001 4 5 CA010313014 120010228G6220471401241 TUBE BELL 47 47G2 1181008SW LYC O435 VO435A1F 41516EA MAIN ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 79 (CAN) DURING DAILY INSPECTION ON MAIN CONTROL STABILIZER BAR AS PER AD 74-08-02. PILOT FOUND STABILIZER BAR TUBE WAS CRACKED. 1G71 3O3 O H1 E279 20010405000972001040500097NM 2001 4 5 CA010313015 120010304G2913570347 PUMP DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE HYD SYSTEM FAILED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA 137703804 MX452601C (CAN) HYDRAULIC PUMP FAILED CAUSING FAILURE OF NR 1 HYDRAULIC SYSTEM. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010405000992001040500099CE 2001 4 5 CA010313017 120010215G7721RHM38E SPARK PLUG BEECH 76 76 1153005CE LYC O360 O360A1G6D EA ENGINE DAMAGED W A UNSCHED LANDING R PARTIAL RPM/PWR LOSS CRCRUISE 1 CA 300 (CAN) IN CRUISE PILOT REPORT RT ENGINE SURGING, THEN COMPLETELY ROUGH RUNNING. ENGINE SHUTDOWN, AIRCRAFT LANDED SAFELY. COMPRESSION TEST REVEALED ONE WEAK CYLINDER 50/80 PSI. BOTH SPARK PLUGS IN THAT CYLINDER SHORTED DUE TO BEING PEENED OVER BY FOREIGN OBJECT BOUNCING BACK AND FORTH IN CYLINDER. SUSPECT CERAMIC PIECE FROM A PLUG CAME OFF AND DID DAMAGE, HOWEVER PIECE NOT FOUND, NEW CYLINER ASSEMBLY INSTALLED, SPARK PLUGS ARE RECONDITIONED IN HOUSE USING CHAMPION PLUG CLEANER/TESTER. 1L72 3O3 O A29CE E286 20010405001002001040500100EU 2001 4 5 KBMA88643 120010215G7110350A58154322 HINGE PIN SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1 60030NE ENG COWLING BROKEN E KBMAK NONE O OTHER ININSP/MAINT 1 WP19115SH2169 3141 COWLING HINGE PIN BROKEN. 1G71 3U3 U H9EU E19EU 20010405001052001040500105 2001 4 5 KBMA88646 420010218G2312064105430 VHF COMM SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE E KBMAK NONE L NO TEST ININSP/MAINT 1 WP19350SH4474 2957 VHF INOPERATIVE, COMES ON ONLY WHEN VOLUME IS ALL THE WAY DOWN. 1G71 3U3 UNCH9EU E19EU 20010405001062001040500106 2001 4 5 KBMA88649 420010220G2312064010540030 VHF COMM SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT MALFUNCTIONED E KBMAK NONE L NO TEST ININSP/MAINT 1 WP191188P9792 2347 VHF HAS CONSTANT SQUELCH ON AFTER APPROX 30 MINUTES OF OPERATION. WILL NOT RESET. 1G71 3U3 UNCH9EU E19EU 20010405001072001040500107 2001 4 5 KBMA88819 420010208G3422200DCL GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT MALFUNCTIONED E KBMAK NONE O OTHER ININSP/MAINT 1 WP19270SH7475 1864 DIRECTIONAL GYRO MAKES EXCESSIVE NOISE. 1G71 3U3 UNCH9EU E19EU 20010405001082001040500108 2001 4 5 KBMA88818 420010208G34215040017901 GYRO SNIAS 350 AS350BA 8680817EU TMECA ARRIELARRIEL1 60030NE COCKPIT INOPERATIVE E KBMAK NONE O OTHER ININSP/MAINT 1 WP19270SH7475 1864 PRECESSING AND FLAG INDICATOR INOPERATIVE. 1G71 3U3 UNCH9EU E19EU 20010405001092001040500109GL 2001 4 5 KBMA88679 220010227G73107G547 PRESSURE SWITCH BELL 206 206B 1181511SW ALLSN 250C 250C20 03013GL FUEL SYSTEM MALFUNCTIONED E KBMAK NONE J WARNING INDICATION ININSP/MAINT 1 WP19667JM9830 3444 FUEL PRESSURE SWITCHES NOT OPERATING PROPERLY. CAUTION LITE REMAINS ON WITH CIRCUIT BREAKER IN. 1G71 3U3 U H2SW E4CE 20010405001112001040500111EU 2001 4 5 20010314CW001 120010218G2612B332M FIRE DETECTOR BOLKMS105 BO105CBS 5626008EU ALLSN 250C 250C20B 03013GL NR 1 ENGINE SHORTED E ALGAK NONE O OTHER ININSP/MAINT 1 SW035416F 794 836063 DURING PRESTART CHECK. AFT PROBE SHORTED TO ELBOW ON ENGINE AIR SYSTEM. 1G72 3U3 UNCH3EU E4CE 20010405001122001040500112SW 2001 4 5 20010314CW002 120010217G6510206061432121 HOUSING BELL 407 407 SW ALLSN 250C 250C47B GL BLOWER CRACKED E ALGAK NONE O OTHER ININSP/MAINT 1 SW03577AL 53247 CAE847167 FOUND DURING ROUTINE MAINTENANCE. BLOWER HOUSING HAD CRACKED. 1G71 3U3 UO H2SW E1GL 20010405001132001040500113SW 2001 4 5 20010314CW003 120010201G5320NAS6606D70 BOLT BELL 214 214ST 1182106SW GE CT7TS CT71 30030NE FUSELAGE BROKEN E ALGAK NONE O OTHER ININSP/MAINT 1 SO03392AL 28114 DURING DAILY INSPECTION, FOUND UPPER RETAINER BOLT, PN NAS6606D70, ON THE FWD NODAL BEAM ASSY HELPER SPRING BROKE, CRACKING THE HELPER SPRING SIDE PLATE AND CAUSING CONTACT DAMAGE TO THE RIGHT TORSION ARM ASSEMBLY. NEED SCHEDULED INSPECTION OR RETIREMENT OF BOTH UPPER AND LOWER BOLTS DUE TO THE HIGH STRESS LOAD ON THESE PARTS. 2G72 4U4 U H10SW E8NE 20010405001142001040500114EU 2001 4 5 20010314CW004 120010126G6520365A33619721 FLANGE AEROSPAS365 AS365N2 8680815EU TMECA ARRIELARRIEL1 60030NE TAIL ROTOR G/B WORN E EGRAK NONE O OTHER ININSP/MAINT 1 EA17272NE M538 6435 DURING T INSPECTION, FOUND BOLTS ATTACHING SLIDING FLANGE TO FLEXIBLE COUPLING HAVE LOW TORQUE. COTTER KEYS WERE INSTALLED. SLIDING FLANGE AND FLEXIBLE COUPLING HAVE GROOVES WORN ON ATTACHING SURFACE. REPLACED SLIDING FLANGE, FLEXIBLE COUPLING, AND ATTACH HARDWARE WITH NEW. 1G72 3U3 URTH10EU E19EU 20010405001372001040500137SW 2001 4 5 20010319CW006 120010216G631047620669S CLUTCH BELL BELL 47 47G3B1 1181028SW LYC O435 TVO435B1A 41516EA M/R TRANSMISSIONDAMAGED H ARUAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 WP1148020 369 B123119 2812 67452C AIRCRAFT IN CRUISE AT 300 FT AGL CLUTCH SLIPPED AUTOROTATION PERFORMED DISASSEMBLED FOUND PARTIAL CONTACT OF CLUTCH/DRUM FACE. DRUM AT MAX LIMITS. MORE CAUTIOUS MEASUREMENT DURING OVERHAUL AND REQUIRED INSPECTION. 1G71 3O3 O 2H3 1E13 20010405001492001040500149EA 2001 4 5 CA010313019 220010228G741410382681 CAPACITOR BENDIX D6LH3200 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA MAGNETO FAILED W K NONE R PARTIAL RPM/PWR LOSS TXTAXI/GRND HDL 1 CA 124 (CAN) AIRCRAFT HAD FLOWN 2-3 HOURS ENGINE SHUT DOWN TO UNLOAD PASSENGERS. PILOT STARTED 1 ENGINE BUT 2ND WOULD NOT START. PROBLEM WAS INVESTIGATED AND CAPACITOR FOUND U/S. CAPACITOR REPLACED AND ENGINE STARTED. WE HAVE HAD 3 SUCH CASES IN THE LAST MONTH. WE HAE TESTED THE U/S CAPACITORS AS PER MANUFACTURERS INSTRUCTIONS AND CAPACITORS CHECK OUT SERVICEABLE. WE HAVE ALSO NOTICED THAT POINTS ARE NOT LASTING AS LONG IN THE MAGS. ALL CAPACITORS WERE REPLACED AS PER TELEDYNE CSB 662A. 1L72 3O3 O A20SO E14EA 20010405001542001040500154CE 2001 4 5 CA010313024 120010309G2431 BATTERY CESSNA172 172L 2072432CE LYC O320 O320E2D 41508EA MCAULY1C160 1C160CTM GL MAIN BATTERY FAILED W A UNSCHED LANDING HGJELECT. POWER LOSS-50 PC MULTIPLE FAILURE WARNING INDICATION CRCRUISE 1 CA (CAN) PILOT ENCOUNTERED COMPLETE (GREATER THAN 50 PERCENT) ELECT. FAILURE IN FLT. AFTER ATTEMPTING TO GET A/C RADIOS TO TRANSMIT/RECEIVE, PILOT SQUAKED RADIO FAILURE CODE. FURTHER ATTEMTPS AT GETTING OTHER ELECT. SYSS TO FUNCTION, PILOT FOUND THAT ALL ELECT. SYS WAS UNSERVICEABLE. A/C RETURNED TO POINT OF DEPTR & THEN CONTACTED TOWER ON LAND LINE.AFTER BRIEF INSP , FOUND THAT A/C BATTERY COMPLETELY DISCHARGED. BATTERY (NEW & INST NOV.2000) ELECTROLYTE LEVEL INSP OK, BATTERY CHARGED OVERNIGHT. AFTER BATTERY CHARGED, GROUND RUN/FUNCTION CHECKED. NOTED WITH CHARGING SYS COMPLETELY LOADED UP, CHARGE IND. WEAK. SUSPECT BATTERY VOLTAGE INITY LOW & CHARGING SYS UNABLE TO KEEP UP WITH DE 1H71 3O3 ONT3A12 E274 5 NP910 20010405001552001040500155EU 2001 4 5 CA010313025 120010226G53023160S451010060 GUARD AEROSPSA316 SA315B 8680615EU TMECA ARTST3ARTOUSTE3B 60003EU TAIL ROTOR CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 2714 (CAN) WHILE CLEANING AIRCRAFT, AME FOUND CRACK COMING FROM UNDER BOTTOM CLAMP.NEW TAIL ROTOR GUARD WAS INSTALLED. 1G71 4U3 U H1IN E11N 20010405001592001040500159CE 2001 4 5 CA010314003 120010226G561010138402522 WINDSHIELD BEECH B300 B300 1159232CE PWA PT6 PT6A60A 52043NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA 5 (CAN) WHILE IN CRUISE FLIGHT AT FL310 AND OAT -50 DEGREES C, FLIGHT CREW OBSERVED RT WINDSHIELD OUTER PANE CRACK DEVELOP. CRACK WAS DIAGONAL IN LOWER INBOARD CORNER (APPROXIMATELY 6 INCHES). POH ABNORMAL CHECKLIST FOLLOWED AND FLIGHT RETURNED TO POINT OF DEPARTURE. 2L72 4T4 TRTA24CE E4EA 20010405001612001040500161WP 2001 4 5 CA010314007 220010312G723031037081 BEARING MTSBSIMU2 MU2B60 5780460CE GARRTTTPE331TPE33110 01514WP COMPRESSOR WRONG PART W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA (CAN) GARRETT SB 72-0634 DATED AUG 17 1989 (OPTIONAL COMPLIANCE) LISTED COMPRESSOR BEARING P/N 3103708-1 AS REPL FOR P/N 3101405-1. BULLETIN APPLICABLE TO ALL MODELS OF TPE 331 ENGINE WHICH PREV HAD P/N 3101405-1 BEARING. SUBSEQUENT REVISION NR 1 TO SB DATED APR 27, 1990 DELETED SOME ENGINE MODELS FROM EFFECTIVITY LIST. ENGINE MODEL DELETED FROM LIST, HOWEVER IT NOT RECOMMENDED TO REMOVE ANY P/N 3103708-1 BEARINGS INST IN COMPLIANCE WITH T HE 1ST ISSUE OF SB- IN NOV 1998 P/N 3103708-1 BEARING INST INTO ENGINE. SUBSEQUENET REVIEW OF LIFE LIMITED COMPONENTS IN ENGINE, AGAINST REQMTS OF SB 72-0180 TBO REQMTS, INDICATED PART NO LONGER LISTED ON APPLICABLE LIFE LIMIT TABLES. 1H72 3T4 TRTA10SW E4WE 20010405001622001040500162NE 2001 4 5 CA010314009 320010218G61147827015 HUB DHAV DHC8 DHC8101 2809002NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE LT PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 9085 (CAN) DURING ROUTINE MAINTENANCE CHECK, FOUND LEFT PROPELLER ASSEMBLY HAD EVIDENCE OF OIL LEAK. UPON FURTHER INVESTIGATION LEAK WAS FOUND TO BE COMING FROM NR 4 BLADE. AFTER REMOVING THE LEFT NR 4 BLADE THE OUTER BEARING RACE WITHIN THE PROPELLER HUB WAS FOUND TO BE CRACKED AND GALLED.LEFT PROPELLER HUB, PROPELLER ACTUATOR, AND 3 BLADES WERE REPLACED DUE TO OIL CONTAMINATION AND AN ADDITIONAL BEARING RACE FOUND GALLED. AIRCRAFT RETURNED TO SERVICE. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010405001672001040500167SO 2001 4 5 CA010314023 120010223G562045099013 WINDOW PIPER PA31T PA31T2 7103127SO PWA PT6 PT6A135 52043NE FUSELAGE BROKEN W A UNSCHED LANDING D INFLIGHT SEPARATION CLCLIMB 1 CA 12355 (CAN) - THE AIRCRAFT WAS CLIMBING THROUGH 16,000 FEET WHEN THE CABIN PRESSURIZATION WAS LOST. - THE PILOTS INITIATED EMERGENCY DESCENT TO 10,000 FEET AND DECLARED EMERGENCY. - THE CAUSE FOR DEPRESSURIZATION WAS FOUND TO BE A BROKEN WINDOW IN THE CABIN AREA (3RD WINDOW ON LT SIDE).- AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENTS. 1L72 3T4 TRTA8EA E4EA 20010405001692001040500169EU 2001 4 5 CA010314026 120010227G21339599091131 REGULATOR PILATSPC12 PC1245 EU PWA PT6 PT6A67B 52043NE HARTZLHCE4A HCE4A3D GL CABIN PRESSURE CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 CA 2649 (CAN) SAFETY VALVE FAILED TON OPEN WHEN CARRYING OUT 1500 HOUR PRESSURIZATION CHECK. FAILED SAFETY VALVE WAS REMOVED AND VALVE AND SENSE LINE WERE FOUND CONTAMINATED WITH JET FUEL. FUEL APPEARED TO HAVE COME FROM A PREVIOUSLY SEEPING FUEL FILTER BOWL SEAL AND HAD ENETRED THE OUTFLOW VALVE WHERE THE AMBIENT PRESSURE SENSE LINE PROTRUDES THROUGH THE PRESSURE BULKHEAD (APPROX 12 -14 INCHES AFT OF THE FUEL BOWL). 1L71 3T4 TRTA78EU E26NE 5 CP210NE 20010405001702001040500170SW 2001 4 5 CA010314027 120010223G3222 STRUT GULSTM112 112 0144701SW LYC O360 IO360C1D6 41514EA HARTZLHCE2Y HCE2YR1BF GL NLG CONTAMINATED W O OTHER J WARNING INDICATION LDLANDING 1 CA 1711 1711 (CAN) A/C HAD UNCOMMANDED NOSE GEAR RETRACTION UPON LDG. IT NOTICED DURING POWER PACK PRESSURE TEST THAT 700PSI ON UP SIDE WHEN GEAR EXTENDING & THAT PRESSURE WOULD NOT DECREASE BELOW 50-100 PSI WHEN GEAR WAS FULLY EXTENDED.RESIDUAL PRESSURE PREVENTING DETENT PINS FROM ENGAGING. HYDRAULIC POWER PACK REMOVED & DISASSEMBLED. FOUND ONE 8 OF INCH OF BLACK SLUDGE & 1 X 5 INCH PIECE OF PAPER IN RESERVOIR.VALVE BODY ALSO DISSASSEMBLED. FOUND GEAR UP CHECK VALVE O-RING HARD & BRITTLE & SEATS OF MOST OF VALVES COVERED WITH SLIMY GOO. NOSE GEAR ACTUATOR DISASSEMBLED. MAIN PRESSURE O-RING MS28775-117 NOTICED TO BE ROLLED. 1L71 3O3 O A12SO 1E10 5 CP9EA 20010405002212001040500221EA 2001 4 5 CA010320010 120010308G5610NP1393212 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W A UNSCHED LANDING O OTHER CRCRUISE 1 CA (CAN) RT WINDSHIELD INNER PLY FOUND CRACKED, UNIT REPLACED AND AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405002222001040500222EA 2001 4 5 CA010320013 120010308G3234 HANDLE CNDAIRCL600 CL6002B19 EA GE CF34 CF343A1 30015NE MLG SELECTOR FAILED W A UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CA (CAN) DURING CLIMBOUT LANDING GEAR WOULD NOT RETRACT, ANTI-SKID FAIL MESSAGE SHOW ON EICAS. MAINTENANCE REPLACED LANDING GEAR HANDLE AND AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405002232001040500223 2001 4 5 CA010320014 420010308G34178220371140 ADC CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE E/E BAY FAILED W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) DURING CRUISE STABILIZER TRIM CH2 AND MACH TRIM FAILED. MAINTENANCE REPLACED ADC AND AIRCRAFT BACK IN SERVICE. 2L72 4F4 FRTA21EA E15NE 20010405002242001040500224CE 2001 4 5 CA010320018 120010228G2820120010679 LINE CESSNA206 U206G 2073356CE CONT O550 IO550F 17042SO FUEL DISTRIBUT CHAFED W K NONE O OTHER ININSP/MAINT 1 CA 1970 (CAN) LINE ASSEMBLY - FUEL, STRAINER TO ELBOW FOUND CHAFING AGAINST RT NOSE GEAR STEERING BOOT.1.50 INCH X 0/032 INCH TUBING FOUND WORN BY 0/018 INCH ON ONE SIDE. PART HAS BEEN REPLACED WITH A NEW LINE ASSEMBLY - FUEL AND PROTECTED WITH NYLON SPIRAL WRAP. 1H71 3O3 O A4CE E3SO 20010405002272001040500227EU 2001 4 5 CA010320021 120010214G2910 LINE AIRBUS310 A310304 EU GE CF6 CF680C2A5 NE HYDRAULIC SYS LOOSE W A UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CA (CAN) PILOT OBSERVED GREEN SYSTEM HYDRAULICS WAS LOOSING FLUID. AIRCRAFT DIVERTED TO YYT. HYDRAULIC LINE IN NR 1 ENGINE PYLONFOUND LOOSE. LINE TIGHTENED AND LEAK CHECK CARRIED OUT SERVICEABLE. 2L72 4F4 FRTA35EU E13NE 20010405002332001040500233SO 2001 4 5 CA010322002 120010208G3242 LINER PIPER PA34 PA34200T 7103406SO CONT O360 TSIO360EB 17025SO BRAKES DESTROYED W K NONE W INADEQUATE Q C ININSP/MAINT 1 CA 43 (CAN) WHILE CONDUCTING A GENERAL WALK AROUND FOR A PRE-PURCHASE, THE INBOARD PRESSURE PLATE SIDE OF THE BRAKE CALIPERS, THE BRAKE LINERS WERE TOTALLY DESTROYED, RESULTING IN THE STEEL PRESSURE PLATE TO COME IN FULL CONTACT WITH THE BRAKE DISC WHICH CREATED DEEP GROOVES AND SIGNIFICANT AMOUNT OF HEAT TO DISCOLOR THE PRESSURE PLATES AND DISCS. 1L72 3O3 O A7SO E9CE 20010405002392001040500239NM 2001 4 5 CA010322012 120010317G4920 COMPRESSOR BOEING737 737281 138448PNM PWA JT8 JT8D17 52049NE APU MAKING METAL W K NONE O OTHER ININSP/MAINT 1 CA 41944881 (CAN) THE AIRCRAFT WAS CLIMBING OUT OF VANCOUVER WHEN THE APU DID AN AUTO SHUT DOWN AND THE APU FIRE HANDLE ILLUMINATED. THE FIRE HANDLE WAS PULLED BUT THE BOTTLE WAS NOT DISCHARGED DUE TO THE FIRE INDICATION GOING OUT. THE AIRCRAFT RETURNED TO VANCOUVER WHERE THE APU AREA WAS INSPECTED AND NO EVIDENCE OF A FIRE WAS DISCOVERED. THE APU WAS PLACED ON MEL AND THE AIRCRAFT WAS RELEASED TO SERVICE. FURTHER INVESTIGATION LATER IN THE DAY FOUND THAT THERE WAS METAL FRAGMENTS FOUND IN THE INTAKE OF THE APU AND THE APU WAS REMOVED FROMTHE AIRCRAFT. IT WILL BE RETURNED TO THE OVERHAUL FACILITY FOR DISASSEMBLY AND REPAIR. 2L72 4F4 F A16WE E2EA 20010405002402001040500240EU 2001 4 5 CA010323002 120010217G2701AS2219 CONTROL CABLE SIREN S1609 SNIAS 350 AS350B2 8680813EU TMECA ARRIELARRIEL1D NE CARGO HOOK BROKEN W O OTHER O OTHER CLCLIMB 1 CA 876 (CAN) MANUAL / EMERGENCY RELEASE CABLE SHEATH BROKEN AWAY FROM FERRULE / SLEEVE WHERE CABLE ASSEMBLY ATTACHES TO THE CARGO HOOK.THE CARGO SUSPENSION SYSTEM (SWING) ALLOWS FOR A LOT OF MOVEMENT OF THE CARGO HOOK. THERE APPEARS TO BE A LOT OF FLEXING OF THE CABLE ASSY WHERE IT ATTACHES TO THE CARGO HOOK LEADING TO FAILURE OF THE CABLE SHEATH.THIS FAILURE RESULTED IN AN UNCOMMANDED LOAD RELEASE. 1G71 3U3 U H9EU E19EU 20010405002412001040500241NE 2001 4 5 CA010323003 220010309G75302496722 WASHER BENDIX 153212A DHAV DHC8 DHC8* NM PWA 120 PW120 NE VALVE SEALS CRACKED W K NONE O OTHER ININSP/MAINT 1 CA RF4252 (CAN) COMPRESSION WASHER CRACKED AND JAMMED BETWEEN THE VALVE SEAL AND SEALING SURFACE PREVENTING THE A SIDE FROM COLOSING. 2H72 4T4 TRTA13NM E20NE 20010405002442001040500244SO 2001 4 5 CA010323006 120010307G7721LW16740 EXHAUST VALVE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA NR 5 CYLINDER BROKEN W K NONE O OTHER ININSP/MAINT 1 CA 1724 (CAN) PILOT REPORTED HIGH OIL TEMP VERNATHERN REPLACED AND ON GROUND RUN ENGINE RAN ROUGH. LARGE AMOUNT OF OIL NOTED COMING FROM SNIFFLE VALVE MIXED WITH FUEL. SPARK PLUGS REMOVED AND FOUND THOSE REMOVED FROM NR 5 CYLINDER WERE DAMAGED. REMOVED CYLINDER AND FOUND 1/3 OF VALVE FACE (EXHAUST) MISSING. REPLACED CYLINDER AND CHECKED ALL SCREENS AND FILTERS. 1L72 3O3 O A20SO E14EA 20010405002462001040500246CE 2001 4 5 CA010323008 120010302G5751991300003 SKIN BEECH 100 100BEECH 1152916CE PWA PT6 PT6A28 EA RT AILERON CRACKED W K NONE O OTHER ININSP/MAINT 1 CA 13438 (CAN) WHEN CHECKING SB 57-3148 IT WAS NOTICED THAT THIS AILERON WAS ALSO CRACKED AS PER SB 57-3148. KIT 109-4011-1 INSTALLED. 1L72 3T4 T A14CE E4EA 20010405002492001040500249CE 2001 4 5 CA010323011 120010313G561011450431S WINDSHIELD BEECH 1900 1900D 1154162CE PWA PT6 PT6A67D NE HARTZLHCE4A HCE4A3I NE COCKPIT CRACKED W O OTHER O OTHER DEDESCENT 1 CA 7057 (CAN) ON DESCENT IN YWG PILOT HEARD SNAPING AND CRACKING AS THE OUTER LAYER OF LT WINDSHIELD SHATTERED. THEY DESCENDED TO YWG ASKING FOR PRIORITY LANDING WITHOUT INCIDENT. 2L72 4T4 TRTA24CE E26NE 5 CP10NE 20010405002502001040500250CE 2001 4 5 CA010323013 120010315G7603S351 CLAMP CESSNA CESSNA172 172M 2072418CE LYC O320 O320E2D 41508EA THROTTLE CABLE LOOSE W K NONE O OTHER ININSP/MAINT 1 CA (CAN) THROTTLE SHEAF HAD VIBRATED LOOSE FROM CONNECTING CLAMP WHICH LEFT NO CONTROL FOR THROTTLE ADJUSTMENT. THROTTLE CABLE WAS RE-POSITIONED IN THE SHEAF AND NEW HARDWARE WAS INSTALLED.AIRCRAFT WAS GROUND UN AND ALL PARAMETERS NORMAL. 1H71 3O3 ONT3A12 E274 20010405002552001040500255NE 2001 4 5 AU010161 220010222G7530216035037 ACTUATOR LYC ALF502R5 BAG BAE146BAE146200A 1500266EU LYC ALF502ALF502R5 41580NE COMPRESSOR BLEEDFAULTY W O OTHER E VIBRATION/BUFFET APAPPROACH 1 AUS XRC8122 (AUS) NR 3 ENGINE BLEED BAND ACTUATOR FOLLOWUP ARM RETAINING CLIP AND PIN MISSING ALLOWING THE FOLLOWUP ARM AND THE OPERATING LEVER TO FOUL EACH OTHER WHICH RESULTED IN THE BLEED BAND REMAINING CLOSED. 2H74 4F4 FRTA49EU E6NE 20010405002562001040500256EU 2001 4 5 AU010162 120010221G2450A2043C POWER UNIT SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE AC POWER DIST FAULTY W O OTHER HBJELECT. POWER LOSS-50 PC SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) RT POWER DISTRIBUTION UNIT (PDU) FAULTY. STARTER-GENERATOR WOULDNOT DISENGAGE AND AN OVERTEMPERATURE WAS OBSERVED WITH SMOKE COMING FROM THE COWLS. THE FIRE BOTTLE WAS DISCHARGED AS APRECAUTION. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010405002572001040500257WP 2001 4 5 AU010163 220010228G7210851 GEARBOX BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE LEFT ENGINE MAKING METAL W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT ENGINE REMOVED DUE TO SUSPECT DISTRESS IN THE GEARBOX AND VIBRATION. OIL ANALYSIS FOUND METAL CONTAMINATION. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010405002582001040500258CE 2001 4 5 AU010164 120010222G271050452133 TUBE CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL AILERON CONTROL CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) OUTBOARD PUSH-PULL TUBE LOCATED IN RT WHEEL WELL CORRODED INTERNALLY. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010405002592001040500259SW 2001 4 5 AU010165 120010226G5712273102336 RIB SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL RT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RT WING RIB CRACKED IN BEND RADIUS. RIB FORMS THE INNER WALL OF THE BATTERY BOX. CRACK LENGTH 203.2MM (8IN). 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20010405002602001040500260SW 2001 4 5 AU010166 120010226G5712273102336 RIB SWRNGNSA227 SA227AC 8780603SW GARRTTTPE331TPE33111U 01514WP ROTOL R321 R321482F8 GL LT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING RIB CRACKED IN BEND RADIUS. RIB FORMS THE INNER WALL OF THE BATTERY BOX. CRACK LENGTH 76.2MM (3IN). 2L72 4T4 TRTA8SW E4WE 6 CP61GL 20010405002612001040500261EU 2001 4 5 AU010167 120010223G7714AG34 TACH GENERATOR BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE ENGINE FAULTY W O OTHER P NO WARNING INDICATION CLCLIMB 1 AUS (AUS) TACHO-GENERATOR ZERO OUTPUT. INVESTIGATION ALSO FOUND BROKENWIRE STRANDS AT THE ENGINE WIRING DISCONNECT SPLICE. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010405002622001040500262EU 2001 4 5 AU010168 220010219G7230 COMPRESSOR FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU NR 1 ENGINE DAMAGED W O OTHER E VIBRATION/BUFFET CLCLIMB 1 AUS (AUS) NO1 ENGINE VIBRATION. BORESCOPE INSPECTION FOUND DAMAGE TO THESEVENTH STAGE HPC. 2L72 4F4 FRTA20EU E2EU 20010405002632001040500263EU 2001 4 5 AU010169 120010218G2133566920 OUTFLOW VALVE FOKKERF28 F28MK0100 4990807EU RROYCETAY TAY62015 04564NE CABIN COOLING SYFAILED W O OTHER J WARNING INDICATION CRCRUISE 1 AUS 4585 (AUS) AVIONICS COOLING SYSTEM OUTFLOW VALVE FAILED. 2L72 4F4 FRT E25NE 20010405002642001040500264CE 2001 4 5 AU010170 120010201G3260JE1 SWITCH CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO MCAULY3AF32C3AF32C87 GL MLG WORN W O OTHER N FALSE WARNING LDLANDING 1 AUS (AUS) RT MAIN LANDING GEAR MICROSWITCH ARM WORN. ARM BROKE OFF DURING FLIGHT. 1L72 3O3 O 3A10 E5CE 5 CP22EA 20010405002652001040500265 2001 4 5 AU010172 420010305G3423 COMPASS CESSNA150 150B 2071806CE CONT O200 O200A 17020SO MCAULY1A100 1A100MCM GL COCKPIT OUT OF ADJ W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) COMPASS SWING OUT OF DATE. NO COMPASS CORRECTION CARD FITTED. 1H71 3O3 O 3A19 E252 5 NP918 20010405002662001040500266SO 2001 4 5 AU010173 120010228G551140122002 SPAR PIPER PA31350 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 311274 (AUS) HORIZONTAL STABILISER SPAR CRACKED. FOUND DURING INSPECTION IAW PIPER MSB 1007. WHEN INSPECTED IAW AD/PA31/97 AMDT2 NO CRACKS WERE FOUND DUE TO CRACKS BEING HIDDEN BY THE ELEVATOR OUTBOARD HINGE ATTACHMENT FITTING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010405002672001040500267SO 2001 4 5 AU010174 120010228G551140122003 SPAR PIPER PA31350 PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL HORIZONTAL STAB CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 311274 (AUS) HORIZONTAL STABILISER SPAR CRACKED. FOUND DURING INSPECTION IAW PIPER MSB 1007. WHEN INSPECTED IAW AD/PA31/97 AMDT2 NO CRACKS WERE FOUND DUE TO CRACKS BEING HIDDEN BY THE ELEVATOR OUTBOARD HINGE ATTACHMENT FITTING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010405002682001040500268CE 2001 4 5 AU010175 120010223G275208615582 GEAR CESSNA402 402C 207590RCE CONT O520 TSIO520VB 17040SO TE FLAP ACTUATORWORN W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) FLAP ACTUATOR TRANSFER GEAR STRIPPED. 1L72 3O3 O A7CE E8CE 20010405002692001040500269EA 2001 4 5 AU010176 220010225G74144370 SHAFT PIPER PA28 PA28161 7102803SO LYC O320 O320D3G 41508EA SNSNCH74D 74DM EA MAGNETO FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAGNETO SHAFT BROKEN IN AREA WHERE THE POINTS CAM ATTACHES. 1L71 3O3 O 2A13 E274 5 NP88614 20010405002702001040500270SO 2001 4 5 AU010177 220010308G8500IO470L ENGINE BEECH 95 95B55 1152729CE CONT O470 IO470L 17026SO MCAULY2AF34C2AF34C55 GL RIGHT FAILED W C ABORTED TAKEOFF EYJVIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION TOTAKEOFF 1 AUS 1450 20139971L (AUS) RT ENGINE CATASTROPHIC FAILURE. 1L72 3O3 ORT3A16 3E1 5 CP5EA 20010405002712001040500271WP 2001 4 5 AU010178 120010204G243615891A VOLT REGULATOR DOUG DC4 C54E 3021530WP PWA R2000 R2000* 52023NE HAMSTD23E 23E50 NE DC SYSTEM OVERHEATED W A UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CRCRUISE 1 AUS R704 (AUS) NR 2 GENERATOR VOLTAGE REGULATOR FAULTY. 2L74 4R4 R A762 5E5 6 CP603 20010405002722001040500272SO 2001 4 5 AU010179 220010219G8530649166 CYLINDER CESSNA210 210L 2073448CE CONT O520 IO520L 17032SO MCAULY3A32C D3A32C88 GL ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 397 270089R (AUS) NR 1 AND NR 3 CYLINDERS CRACKED FROM UPPER SPARK PLUG HOLE. CRACK LENGTHS APPROXIMATELY 25.4MM (1IN). BOTH CYLINDERS ARE P0.015IN. 1H71 3O3 O 3A21 E5CE 5 CP21EA 20010405002732001040500273SO 2001 4 5 AU010180 220010220G8520 CRANKCASE CESSNA172 172B 2072406CE CONT O300 O300C 17022SO MCAULY1C172 1C172EM GL ENGINE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE IN AN EXTREMELY POOR CONDITION. DEFECTS INCLUDE CRACKED CRANKCASE, WORN CRANKSHAFT, WORN GEARS, WORN CYLINDERS AND VALVES. 1H71 3O3 ONT3A12 E253 5 NP910 20010405002742001040500274NE 2001 4 5 AU010181 320010227G6111RFC11U16A BLADE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PROPELLER DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT PROPELLER NR 1 BLADE DAMAGED BY FOD. LEADING EDGE SHEATH HAD APIECE MISSING APPROXIMATELY 10MM (0.393IN) IN DIAMETER. THE LEFT FRONT PASSENGER WINDOW BEHIND THE GALLEY HAD A LARGE IMPACT MARK APPROXIMATELY 12MM (0.472IN) IN DIAMETER. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010405002752001040500275EA 2001 4 5 AU010182 220010307G852068606 CRANKSHAFT FUJI FA200 FA200160 3730101WP LYC O320 O320D2A 41508EA MCAULY1C172 1C172MGM GL ENGINE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS L639239A (AUS) CRANKSHAFT INTERNAL BORE CORRODED. FOUND DURING INSPECTION IAWAD/LYC/102 AMDT2 PART 1 AND PART 2. 1L71 3O3 O A4PC E274 5 NP910 20010405002762001040500276SW 2001 4 5 AU010183 120010307G6230206040002109 MAST BELL 206 206B 1181511SW ALLSN 250C 250C20B 03013GL MAIN ROTOR DAMAGED W O OTHER E VIBRATION/BUFFET NRNOT REPORTED 1 AUS (AUS) MAIN ROTOR MAST SUBJECTED TO TORSIONAL DAMAGE DURING N2 LOCKUP ON START. 1G71 3U3 U H2SW E4CE 20010405002772001040500277EA 2001 4 5 AU010184 220010307G8520L639239A PUSHROD FUJI FA200 FA200160 3730101WP LYC O320 O320D2A 41508EA MCAULY1C172 1C172MGM GL ENGINE MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS L639239A (AUS) ENGINE PUSHRODS AND TAPPETS INCORRECTLY FITTED DURING ASSEMBLY FOLLOWING A BULK STRIP FOLLOWING A PROPELLER STRIKE. METAL CONTAMINATION OF ENGINE. 1L71 3O3 O A4PC E274 5 NP910 20010405002782001040500278SO 2001 4 5 AU010185 120010308G81204091709001 TURBOCHARGER PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL RT ENGINE FAULTY W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION CRCRUISE 1 AUS 1 (AUS) RT ENGINE TURBOCHARGER FAULTY. LOSS OF ENGINE OIL (4LITRES). 1L72 3O3 O A20SO E14EA 5 CP33EA 20010405002792001040500279NE 2001 4 5 AU010186 320010305G6111RFC11MIRGADE BLADE EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14RF 14RF9 NE PROPELLER CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 4860 (AUS) PROPELLER BLADE NICKEL SHEATH CRACKED. CRACK LENGTH APPROXIMATELY 50.8MM (2IN) LOCATED ON THE FACE APPROXIMATELY 50.8MM (2IN) FROMTHE BLADE HEATER. 2L72 4T4 TRTA31SO E20NE 6 CP11NE 20010405002802001040500280EA 2001 4 5 AU010188 120010311G5610NP1393225 WINDSHIELD CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE COCKPIT CRACKED W D RETURN TO BLOCK O OTHER TXTAXI/GRND HDL 1 AUS 9910H4795 (AUS) CAPTAINS SIDE WINDOW OUTER PANE SHATTERED. 2L72 4F4 FRTA21EA E15NE 20010405002812001040500281CE 2001 4 5 AU010189 120010225G2750 WIRE CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL TE FLAPS BROKEN W O OTHER F FLT CONT AFFECTED LDLANDING 1 AUS (AUS) FLAP PRESELECT MICROSWITCH WIRE BROKEN. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010405002822001040500282SO 2001 4 5 AU010190 120010312G521041420002 HINGE PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA HARTZLHCE3Y HCE3YR2 GL PAX DOOR CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TOP CABIN DOOR FORWARD HINGE FAILED DUE TO CORROSION INDUCED CRACKING. 1L72 3O3 O A20SO E14EA 5 CP33EA 20010405002832001040500283EA 2001 4 5 AU010191 220010110G7250 ENGINE EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL TURBINE SECTION DAMAGED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE SKI JUMP SEVERELY CRACKED AND DISTORTED IN AREA AROUND NR 3 BEARING COVER. SOME PIECES OF THE EXHAUST CASING HAVE COMPLETELY BROKEN AWAY CAUSING DAMAGE TO THE POWER TURBINE DISC AND BLADES. POWER TURBINE STATOR CRACKED THROUGH THE INNER BAND. 1L72 4T4 T A21SO E4EA 6 CP15EA 20010405002842001040500284 2001 4 5 AU010192 420010312G3497 WIRE BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE NAVIGATION UNIT LOOSE W O OTHER J WARNING INDICATION CRCRUISE 1 AUS (AUS) NR 2 COMPASS SYSTEM FAULTY. INVESTIGATION FOUND A LOOSE WIRE TERMINAL AND NUT ON THE RT FLUX VALVE TERMINAL BLOCK LOCATED AT THE RH OUTER WING TRAILING EDGE. 2H74 4F4 FRTA49EU E6NE 20010405002852001040500285SO 2001 4 5 AU010193 220010306G7314 PUMP BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF34C3AF34C502 GL ENGINE CONTAMINATED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS (AUS) RT ENGINE DRIVEN FUEL PUMP ADJUSTABLE ORIFICE CONTAMINATED WITH A SMALL PARTICLE. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20010405002862001040500286NE 2001 4 5 AU010194 220010310G7323430121204 DRIVE SHAFT BOLKMS117 BK117B1 5626012EU LYC LTS101LTS101750B1 41560NE GOVERNOR SHEARED W O OTHER E VIBRATION/BUFFET CRCRUISE 1 AUS 2238 (AUS) NR 1 ENGINE POWER TURBINE GOVERNOR DRIVE COUPLING SHEARED. 1G72 3U3 U H13EU E5NE10 20010405002872001040500287CE 2001 4 5 AU010195 120010314G28205892000017 LINE BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF34C3AF34C502 GL FUEL DIST LOOSE W O OTHER EYJVIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION LDLANDING 1 AUS 7522 (AUS) RT ENGINE MAIN FUEL LINE FLARE NUT DISCONNECTED ON AFT SIDE OFFIREWALL. PERSONNEL/MAINTENANCE ERROR. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20010405002882001040500288NE 2001 4 5 AU010196 220010312G73238210161E GOVERNOR PWA PW120A DHAV DHC8 DHC8102 2809003NM PWA 120 PW120A NE HAMSTD14SF 14SF7 NE NR 1 ENGINE FAULTY W C ABORTED TAKEOFF ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS 2248689 (AUS) NR 1 ENGINE OVERSPEED GOVERNOR FAULTY. THE GOVERNOR WAS A NEWLY FITTED ITEM WITH NO HOURS SINCE OVERHAUL. 2H72 4T4 TRTA13NM E20NE 6 CP7NE 20010405002892001040500289NM 2001 4 5 AU010197 120010226G4900211734219 GCU BOEING767 767338 1385151NM GE CF6 CF680C2* GL APU FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 18690 (AUS) APU GENERATOR CONTROL UNIT (GCU) FAULTY. INVESTIGATION FOUND THETOP COVER COOLING HOLES BLOCKED WITH DUST. 2L72 4F4 FRTA1NM E23EA 20010405002902001040500290NM 2001 4 5 AU010198 120010222G2840BACJ40A204 JUMPER BOEING747 747438 NM RROYCERB211 RB211524G19 NE FUEL WIRING MISSING W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) FUEL CROSSFEED MANIFOLDS IN CENTER WING TANK HAD MISSING BONDINGJUMPERS. 2L74 4F4 FRTA20WE E30NE 20010405002912001040500291NM 2001 4 5 AU010199 120010227G291065C268393061 LINE BOEING737 737376 NM CFMINTCFM56 CFM563C 13802EU HYDRAULIC SYSTEMLEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) HYDRAULIC B SYSTEM RESERVOIR TO STANDBY SYSTEM SUPPLY LINE LEAKING. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA16WE E21EU 20010405002922001040500292NM 2001 4 5 AU010200 120010223G27821267625 ACTUATOR BOEING747 747438 NM RROYCERB211 RB211524G19 NE SLATS JAMMED W A UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 AUS 41940 (AUS) RH OUTBOARD LEADING EDGE FLAP DRIVE ACTUATOR JAMMED. 2L74 4F4 FRTA20WE E30NE 20010405002932001040500293NM 2001 4 5 AU010201 120010224G2530GENM2585013 OVEN BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU GALLEY BURNED W D RETURN TO BLOCK B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 AUS 221 (AUS) REAR GALLEY OVEN FAN MOTOR BURNT. 2L72 4F4 FRTA16WE E21EU 20010405002942001040500294NM 2001 4 5 AU010202 120010223G3250 NUT BOEING747 747238B 1384828NM RROYCERB211 RB211524D41954555NE NLG STEERING UNLOCKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT NOSE GEAR STEERING CABLES DID NOT HAVE SPLIT PINS FITTED THROUGH CASTELLATED NUTS. BOTH NUTS WERE ONLY FINGER TIGHT AND THE LT NUT WAS HELD BY ONLY TWO THREADS.PERSONNEL/MAINTENANCE ERROR. 2L74 4F4 F A20WE E12EU 20010405002952001040500295NM 2001 4 5 AU010203 120010220G3320 LIGHT BOEING747 747438 NM RROYCERB211 RB211524G19 NE CABIN CONTAMINATED W O OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 AUS (AUS) CROSSOVER CEILING LIGHT LOCATED AT DOOR NR 5 RT HAD SEVERAL PIECES OF TISSUE STUFFED INTO THE LIGHT. THE TISSUE HAD BEGUN TO SMOULDER. THE CROSSOVER LIGHT LENS AND ASSOCIATED METAL GRILL ASSEMBLY WAS MISSING. 2L74 4F4 FRTA20WE E30NE 20010405002962001040500296 2001 4 5 AU010204 420010220G25657A146913 RESERVOIR BOEING747 747438 NM RROYCERB211 RB211524G19 NE ESCAPE SLIDE DISCHARGED W K NONE O OTHER ININSP/MAINT 1 AUS 5336 GJ1033 (AUS) NO5 LH MAIN ENTRY DOOR EMERGENCY ESCAPE SLIDE INFLATION RESERVOIR PRESSURE BELOW LIMITS. 2L74 4F4 FRTA20WE E30NE 20010405002972001040500297NM 2001 4 5 AU010205 120010217G3320 SOCKET BOEING747 747338 NM RROYCERB211 RB211524D41954555NE LIGHT BURNED W O OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 AUS (AUS) SIDEWALL WASH LIGHT SOCKET LOCATED AT SEAT 25 HJK BURNED OUT AND ARCING DUE TO WATER CONTAMINATION. AREA AROUND SEATS FOUND TO BE SOAKING WET DUE TO BLOCKAGE OF RT SIDE UPPER DECK DOOR DRAINBLOCKAGE ALLOWING WATER LEAKAGE. AIRCRAFT HAD BEEN ON THE GROUNDDURING A SEVERE RAIN STORM. 2L72 4F4 FRTA20WE E12EU 20010405002982001040500298NM 2001 4 5 AU010206 120010219G2823737M28500011 SHUTOFF VALVE 737M2850001XBOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU FUEL SELECTOR FAILED W O OTHER RJ PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) NR 2 ENGINE FUEL SHUTOFF VALVE FAILED. 2L72 4F4 FRTA16WE E21EU 20010405003002001040500300NM 2001 4 5 AU010208 120010309G2910AS11506K0264 HOSE BOEING767 767338 1385151NM GE CF6 CF680C2* GL HYDRAULIC SYSTEMFAILED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) NR 4 BRAKE HYDRAULIC HOSE FAILED. 2L72 4F4 FRTA1NM E23EA 20010405003022001040500302 2001 4 5 AU010210 420010306G2565D31591475 SLIDE BOEING737 737476 NM CFMINTCFM56 CFM563C 13802EU PAX DOOR FAILED W K NONE L NO TEST ININSP/MAINT 1 AUS 5661 (AUS) NR 1 RT MAIN ENTRY DOOR ESCAPE SLIDE FAILED TO FULLY DEPLOY. INVESTIGATION FOUND THAT THE SLIDE EXHAUST VALVE WAS STUCK OPEN AND THE VALVE ELEMENT HAD BROKEN AWAY FROM THE VALVE BODY. 2L72 4F4 FRTA16WE E21EU 20010405003032001040500303NM 2001 4 5 AU010211 120010304G2610 WARNING HORN BOEING767 767338 1385151NM GE CF6 CF680C2* GL DETECTION SYSTEMINOPERATIVE W K NONE L NO TEST ININSP/MAINT 1 AUS (AUS) FIRE TEST WARNING BELL INOPERATIVE. 2L72 4F4 FRTA1NM E23EA 20010405003042001040500304EU 2001 4 5 AU010213 120010320G7712SELOC29EC INDICATOR FOKKERF27 F27MK50 EU PWA PWA120PW125B NE ENGINE TORQUE MALFUNCTIONED W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AUS 3921 (AUS) LT ENGINE TORQUE INDICATOR SUSPECT FAULTY. 2H72 4T4 TRTA817 E20NE 20010405003052001040500305 2001 4 5 AU010214 420010223G6113C19042 SPINNER GROB G115 G115 EU LYC O360 O360A1F6 41514EA HARTZLHCF2Y HCF2YR1 GL PROPELLER DEBONDED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) PROPELLER SPINNERS (7OFF) FOUND TO HAVE DISBONDED OR POOR BONDING BETWEEN THE INTERNAL FORWARD SUPPORT BULKHEAD AND THE SPINNER WALL. THE SPINNERS WERE NEW ASSEMBLIES BEING INSPECTED ON RECEIPT FROM THE MANUFACTURER. 1L71 3O3 ONTA57EU E286 5 CP27EA 20010405003062001040500306NE 2001 4 5 AU010215 220010316G8530114650 CYLINDER DOUG DC3 DC3CS1C3G 3021458WP PWA R1830 R183092 52020NE HAMSTD23E 23E50 NE ENGINE SEPARATED W O OTHER EYJVIBRATION/BUFFET ENGINE STOPPAGE WARNING INDICATION CRCRUISE 1 AUS 381 (AUS) RT ENGINE NNR 1 CYLINDER UPPER BARREL AND HEAD SEPARATED. DAMAGE TO PISTON, RINGS, BARREL, INDUCTION TUBE AND PUSHROD TUBE. OIL FILTER METAL CONTAMINATION. 2L72 4R4 R A669 5E4 6 CP603 20010405003072001040500307EU 2001 4 5 AU010216 120010312G7921 PLUG GARRTT 7997 BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP ROTOL R333 R333482F12 GL DOOR ACTUATOR CONTAMINATED W C ABORTED TAKEOFF EN VIBRATION/BUFFET FALSE WARNING TOTAKEOFF 1 AUS 7921 (AUS) LT ENGINE OIL COOLER DOOR ACTUATOR PLUG CONTAMINATED. 2L72 4T4 TRTA56EU E4WE 6 CP61GL 20010405003082001040500308CE 2001 4 5 AU010217 120010313G323312810013 ACTUATOR CESSNA172 172RG 2072438CE LYC O360 O360F1A6 41514EA MCAULY2D34C B2D34C220 GL MLG CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 6006 (AUS) RT MAIN LANDING GEAR ACTUATOR BODY CRACKED. FOUND FOLLOWING INSPECTION IAW SEB01-2. 1H71 3O3 O 3A17 E286 5 CP7EA 20010405003092001040500309NE 2001 4 5 AU010218 220010307G7321 CONNECTOR PWA 7397 EMB 120 EMB120 3260201SO PWA 118 PW118A NE HAMSTD14SF 14SF9 NE EEC CONTAMINATED W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 AUS (AUS) LT ENGINE TORQUE SIGNAL CONDITIONER AND ENGINE ELECTRONIC CONTROL (EEC) ELECTRICAL CONNECTORS CONTAMINATED WITH OIL. 2L72 4T4 TRTA31SO E20NE 6 NP11NE 20010405003102001040500310GL 2001 4 5 AU010219 320010306G6111A22173QTY2 BLOCK HARTZL HCM2YR1BF BEECH 23 C24R 1151254CE LYC O360 IO360A1B6 41514EA HARTZLHCM2Y HCM2YR GL PROPELLER BLADE CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS 1240 EN273 (AUS) PROPELLER PITCH CHANGE BLOCKS CRACKED. PITCH CONTROL FORK WORNEXCESSIVELY. HUB PRELOAD PLATE DAMAGED DUE TO PREVIOUS FOREIGN OBJECT STRIKE. 1L71 3O3 O A1CE 1E10 5 CP43GL 20010405003112001040500311SO 2001 4 5 AU010220 220010223G8520629680 COLLAR CESSNA310 310R 2074245CE CONT O520 IO520M 17032SO ENGINE MISMANUFACTURED W O OTHER KJ FLUID LOSS WARNING INDICATION LDLANDING 1 AUS (AUS) LT ENGINE CRANKSHAFT OIL TRANSFER COLLAR HAD INCORRECT CLEARANCE. THE MEASURED CLEARANCE WAS 0.0254MM (0.001IN) WITH THE CORRECTMANUFACTURERS LIMITS BEING 0.127MM TO 0.4572MM (0.005IN TO0.0018IN). 1L72 3O3 O 3A10 E5CE 20010405003122001040500312CE 2001 4 5 AU010221 120010225G3260ICH16 DOWNLOCK SWITCH CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL MLG FAULTY W O OTHER P NO WARNING INDICATION DEDESCENT 1 AUS (AUS) LT MAIN LANDING GEAR DOWNLOCK MICROSWITCH WIRE BROKEN. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010405003132001040500313EU 2001 4 5 AU010222 120010112G533011207 PLATE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU FUSELAGE CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LOWER LT FUSELAGE PANEL 95B REBATE PLATE CONTAINED SEVERE EXFOLIATION CORROSION (LEVEL2). 2L72 4F4 FRTA20EU E2EU 20010405003142001040500314 2001 4 5 AU010223 420010304G6122PCE21275 GOVERNOR PWA PT6A20 PILATSPC6 PC6 7090102EU PWA PT6 PT6A20 52043EA HARTZLHCB3T HCB3TN3 GL PROPELLER FAILED W D RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 AUS PCE21275 (AUS) PROPELLER REVERSE GOVERNOR IDLER GEAR BEARING COLLAPSED. METALCONTAMINATION OF ENGINE. 1H71 3O3 T 7A15 E4EA 6 CP15EA 20010405003152001040500315EA 2001 4 5 AU010224 220010202G7261 RELIEF VALVE EMB 110 EMB110P1 3260122SO PWA PT6 PT6A34 52043EA HARTZLHCB3T HCB3TN3 GL ENGINE CONTAMINATED W C ABORTED TAKEOFF ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) RT ENGINE OIL PRESSURE RELIEF VALVE CONTAMINATED BY A PIECE OF O-RING SEAL. 1L72 4T4 T A21SO E4EA 6 CP15EA 20010405003162001040500316EU 2001 4 5 AU010226 220010113G72502425 STATOR SNIAS AS332 AS332L 8680809EU TMECA MAKILAMAKILA1A 60040EU TURBINE SECTION CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE FIRST STAGE TURBINE NOZZLE GUIDE VANE INNER RING CRACKED.CRACK RAN FOR APPROXIMATELY 270 DEGREES OF CIRCUMFERENCE. 2G72 4U4 U H4EU E12NE 20010405003172001040500317CE 2001 4 5 AU010227 120010312G5321 SCREW BEECH 58 58 1152740CE CONT O520 IO520C 17032SO MCAULY3AF32C3AF32C512 GL FLOOR PANEL UNAPPROVED PART W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) INCORRECT LENGTH SCREW FITTED TO PILOTS FLOOR PANEL. LONG SCREW CUT A GROOVE IN PIPE. 1L72 3O3 O 3A16 E5CE 5 CP22EA 20010405003182001040500318EA 2001 4 5 AU010228 220010313G7314AN9296J CAP LYC O360A1F6 GROB G115 G115 EU LYC O360 O360A1F6 41514EA ENGINE FUEL PUMPCONTAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ELECTRIC FUEL PUMP OUTLET T FITTING BLANKING CAP CONTAMINATED WITH SWARF. THE BLANKING CAPS ARE FITTED DURING MODIFICATION IAW EO E121-01 REV1. 1L71 3O3 ONTA57EU E286 20010405003202001040500320WP 2001 4 5 AU010230 120010315G6420C1281 HUB ROBSINR44 R44 7640120WP LYC O540 O540F1B5 41532EA TAIL ROTOR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) TAIL ROTOR HUB CONTAINED STRESS CORROSION AND CRACKING FROM THE TEETER BEARING RACES. 1G71 3O3 O H11NM E295 20010405003222001040500322CE 2001 4 5 AU010233 120010319G7810 EXHAUST PIPE BEECH 200 200BEECH 1152920CE PWA PT6 PT6A42 52043NE HARTZLHCD4N3HCD4N3A GL ENGINE FAILED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) ENGINE EXHAUST DUCT FAILED IN AREA AROUND NR 3 BEARING COVER SUPPORT. 1L72 4T4 T A24CE E4EA 5 CSTC 20010405003252001040500325EU 2001 4 5 AU010237 120010303G2432 BATTERY FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU E/E BAY OVERHEATED W O OTHER MJ OVER TEMP WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) AFT BATTERY OVERHEATED. 2L72 4F4 FRTA20EU E2EU 20010405003262001040500326EU 2001 4 5 AU010238 120010223G2910 PIPE FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU HYDRAULIC SYSTEMCHAFED W O OTHER N FALSE WARNING CLCLIMB 1 AUS (AUS) HYDRAULIC PIPES LOCATED IN LT WHEEL WELL RUBBING ON LANDING GEARDOOR PREVENTING REAR UPLOCK SWITCH FROM ACTIVATING. 2L72 4F4 FRTA20EU E2EU 20010405003272001040500327EU 2001 4 5 AU010239 120010222G2910 HYDRAULIC SYSTEM FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU NR 2 LOW W K NONE KJ FLUID LOSS WARNING INDICATION ININSP/MAINT 1 AUS (AUS) NR 2 HYDRAULIC SYSTEM LOW QUANTITY. INVESTIGATION COULD FIND NOEVIDENCE OF LEAKS. SUSPECT SYSTEM NOT REPLENISHED. 2L72 4F4 FRTA20EU E2EU 20010405003282001040500328EU 2001 4 5 AU010240 120010119G2612 FIRE LOOP AIRBUS310 A310324 3930206EU PWA 4152 PW4152 NE LT ENGINE FAULTY W D RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 AUS (AUS) LT ENGINE FIRE LOOP A FAULTY. 2L72 4F RTA35EU E24NE 20010405003292001040500329EU 2001 4 5 AU010241 120010206G2131 CONTROLLER FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU CABIN PRESSURE FAULTY W O OTHER J WARNING INDICATION CLCLIMB 1 AUS (AUS) CABIN PRESSURISATION SYSTEM FAULTY. 2L72 4F4 FRTA20EU E2EU 20010405003302001040500330EU 2001 4 5 AU010242 120010306G2913 PUMP FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU HYDRAULIC SYS LEAKING W C ABORTED TAKEOFF KJ FLUID LOSS WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 2 HYDRAULIC SYSTEM ENGINE DRIVEN PUMP SILENCER LEAKING INTERNALLY. 2L72 4F4 FRTA20EU E2EU 20010405003312001040500331EU 2001 4 5 AU010243 120010226G5610 WINDOW FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU COCKPIT STUCK W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CAPTAINS SLIDING WINDOW STUCK OPEN. INVESTIGATION FOUND WORN TRACK AND UPPER ROLLER. 2L72 4F4 FRTA20EU E2EU 20010405003322001040500332CE 2001 4 5 AU010251 120010322G270105600144 CONTROL COLUMN CESSNA172 172N 2072434CE LYC O320 O320H2AD 41508EA MCAULY1C160 1C160DTM GL COCKPIT CONTAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) CONTROL YOKE CONTAMINATED INTERNALLY WITH WATER. FOUND DURING INSPECTION IAW CESSNA SEB 01-3 1H71 3O3 ONT3A12 E274 5 NP910 20010405003332001040500333EA 2001 4 5 AU010252 220010312G7414 PIN BNORM BN2 BN2A21 1520221EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YR2 GL IMPULSE COUPLINGFAILED W O OTHER EKJVIBRATION/BUFFET FLUID LOSS WARNING INDICATION LDLANDING 1 AUS (AUS) RT ENGINE MAGNETO IMPULSE COUPLING PIN MIGRATED OUT, ALLOWING THE FLANGE SECURING PIN AND FLANGE TO FAIL. LOSS OF ENGINE OIL. 1H72 3O3 O A17EU 1E4 5 CP920 20010405003342001040500334 2001 4 5 AU010253 420010319G341628702501 ALTIMETER BEECH 1900 1900C 1154161CE PWA PT6 PT6A65B 52043EA COCKPIT FAILED W O OTHER O OTHER CLCLIMB 1 AUS (AUS) ALTIMETER INTERNAL FAILURE. 2L72 4T4 TRTA24CE E4EA 20010405003352001040500335NE 2001 4 5 AU010254 220010326G73216068T72P09 HMU SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE FUEL CONTROL FAULTY W O OTHER ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION CLCLIMB 1 AUS (AUS) RT ENGINE HYDROMECHANICAL UNIT (HMU) FAULTY. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010405003362001040500336EA 2001 4 5 AU010255 220010313G74144370 MAGNETO PIPER PA28 PA28181 7102807SO LYC O360 O360A4M 41514EA RIGHT FAILED W O OTHER ERJVIBRATION/BUFFET PARTIAL RPM/PWR LOSS WARNING INDICATION NRNOT REPORTED 1 AUS (AUS) RT MAGNETO FAILED. 1L71 3O3 O 2A13 E286 20010405003372001040500337CE 2001 4 5 AU010256 120010313G5512 SKIN CESSNA210 210N 2073453CE CONT O520 IO520L 17032SO MCAULYD3A34 D3A34C404 GL HORIZONTAL STAB CHAFED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT HORIZONTAL STABILIZER LOWER SKINS CHAFED BY THE GAP SEAL STRIP / ANGLE AT THE FUSELAGE TO STABILISER JUNCTION.REDUCTION IN SKIN THICKNESS FROM 0.635MM (0.025IN) TO 0.33MM(0.013IN). 1H71 3O3 O 3A21 E5CE 5 CP47GL 20010405003382001040500338EU 2001 4 5 AU010257 120010213G5711 SPAR BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE LT & RT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING FORWARD AND AFT SPAR LOWER FLANGES CORRODED. 2H74 4F4 FRTA49EU E6NE 20010405003392001040500339EU 2001 4 5 AU010258 120010212G5711 SPAR BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R3A 41580NE LT & RT WING CRACKED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT AND RT WING FORWARD AND AFT LOWER SPAR CAPS CRACKED IN AREABETWEEN RIBS NR 13 AND NR 18. CORROSION ALSO FOUND ON LOWER SKINS AT RIB BAYS NR 13 TO NR 18. 2H74 4F4 FRTA49EU E6NE 20010405003402001040500340EU 2001 4 5 AU010259 120010212G5730 SKIN BAG BAE146BAE146100A 1500260EU LYC ALF502ALF502R5 41580NE LT WING CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) LT WING LOWER SKIN CORRODED AT RIB BAYS NR 14 TO NR 16. RT WING LOWER SKIN CORRODED AT RIB BAYS NR 14 AND NR 15. 2H74 4F4 FRTA49EU E6NE 20010405003412001040500341NM 2001 4 5 AU010260 120010318G2897W60000818R WIRE BOEING747 747438 NM RROYCERB211 RB211524G19 NE FUEL SYSTEM SHORTED W O OTHER N FALSE WARNING CLCLIMB 1 AUS (AUS) FUEL SYSTEM CONTROL VALVE WIRE PNO W6400-008-18R LOCATED IN NR 4 STRUT KNEE CAP DISCONNECT PLUG D14300P CHAFED AND SHORT CIRCUITING TO GROUND. 2L74 4F4 FRTA20WE E30NE 20010405003422001040500342NM 2001 4 5 AU010261 120010309G324226088127 BRAKE BOEING767 767338 1385151NM GE CF6 CF680C2* GL RT MLG DELAMINATED W K NONE O OTHER ININSP/MAINT 1 AUS 15104 (AUS) RT MAIN LANDING GEAR NR 7 BRAKE STATORS DELAMINATED. 2L72 4F4 FRTA1NM E23EA 20010405003432001040500343NM 2001 4 5 AU010262 120010318G324226088127 BRAKE BOEING767 767338 1385151NM GE CF6 CF680C2* GL LT MLG FAILED W K NONE O OTHER ININSP/MAINT 1 AUS 13318 (AUS) LT NR 4 MAIN WHEEL BRAKE ASSEMBLY ROTORS DISINTEGRATED. 2L72 4F4 FRTA1NM E23EA 20010405003442001040500344EU 2001 4 5 AU010263 120010325G21607828602 CONTROL VALVE SAAB SF340 340B 7860101EU GE CT7TP CT79B 30030NE ROTOL R375 R3754123F21 NE CABIN TEMP SEIZED W C ABORTED TAKEOFF BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TOTAKEOFF 1 AUS 16660 (AUS) DUAL TEMPERATURE CONTROL VALVE SEIZED IN OPEN POSITION. 2L72 4T4 TRTA52EU E8NE 6 CP17NE 20010405003452001040500345NE 2001 4 5 AU010264 220010323G73216078T55P18 FUEL CONTROL GE CNDAIRCL600 CL6002B19 EA GE CF34 CF343B1 NE RT ENGINE LEAKING W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) RT ENGINE FUEL CONTROL UNIT LEAKING FROM THE AREA OF THE THROTTLE CONTROL INPUT ARM. 2L72 4F4 FRTA21EA E15NE 20010405003462001040500346GL 2001 4 5 AU010265 320010325G6111660715698 EROSION SHIELD ROTOL 6607152727 FOKKERF27 F27MK50 EU PWA PWA120PW125B NE ROTOL R352 R3526123F1 GL PROPELLER BLADE SEPARATED W O OTHER D INFLIGHT SEPARATION CLCLIMB 1 AUS 1779 F50470 (AUS) PROPELLER BLADE EROSION SHIELD SEPARATED. 2H72 4T4 TRTA817 E20NE 6 CP16NG 20010405003472001040500347EU 2001 4 5 AU010266 220010324G7321B12597 AMPLIFIER FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU FUEL CONTROL FAULTY W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 AUS 7419 (AUS) NR 1 ENGINE POWER FLUCTUATIONS. ENGINE CONTROL AMPLIFIER AND TEMPERATURE CONTROL ACTUATOR CHANGED. 2L72 4F4 FRTA20EU E2EU 20010405003482001040500348EU 2001 4 5 AU010267 120010324G2913 COUPLING FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU HYDRAULIC PUMP CRACKED W K NONE K FLUID LOSS ININSP/MAINT 1 AUS (AUS) NR 1 HYDRAULIC SYSTEM HYDRAULIC PUMP PRESSURE LINE ELBOW COUPLING THREADED SECTION CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. 2L72 4F4 FRTA20EU E2EU 20010405003492001040500349SW 2001 4 5 AU010268 120010320G6210206015001117AS BLADE BELL 206 206L 1181522SW ALLSN 250C 250C30 03013GL MAIN ROTOR CORRODED W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) MAIN ROTOR BLADE CORRODED IN AREA BETWEEN PAINT AND LEADING EDGESTRIP ON UNDERSIDE OF BLADE. CORROSION DEPTH APPROXIMATELY 1.52MM (0.060IN). FOUND BEFORE FITMENT. 1G71 3U3 U H2SW E1GL 20010405003502001040500350EU 2001 4 5 AU010269 120010309G5270 WARNING SYSTEM FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU PAX DOOR INTERMITTENT W O OTHER N FALSE WARNING NRNOT REPORTED 1 AUS (AUS) PASSENGER DOOR WARNING LIGHT INTERMITTENT IN OPERATION. INVESTIGATION COULD FIND NO FAULT. 2L72 4F4 FRTA20EU E2EU 20010405003512001040500351 2001 4 5 AU010270 420010310G344220412170413 RADAR FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU WEATHER FAULTY W C ABORTED TAKEOFF F FLT CONT AFFECTED TOTAKEOFF 1 AUS 780 2673 (AUS) RADAR RECEIVE/TRANSMIT UNIT FAULTY. 2L72 4F4 FRTA20EU E2EU 20010405003522001040500352 2001 4 5 AU010271 420010312G2212637SUE1 WARNING SYSTEM FOKKERF28 F28MK1000 4990808EU RROYCESPEY SPEY55515 54521EU ALTITUDE CONTROLFAILED W A UNSCHED LANDING P NO WARNING INDICATION CRCRUISE 1 AUS (AUS) ALTITUDE ALERT SYSTEM FAILED. ALTITUDE PRESELECT COUPLER CHANGED. 2L72 4F4 FRTA20EU E2EU 20010405003532001040500353EU 2001 4 5 AU010272 220010314G7200RB18355515H ENGINE FOKKERF28 F28MK4000 4990810EU RROYCESPEY SPEY55515 54521EU NR 1 VIBRATES W C ABORTED TAKEOFF EJ VIBRATION/BUFFET WARNING INDICATION TOTAKEOFF 1 AUS (AUS) NR 1 ENGINE VIBRATION AND NOISE. 2L72 4F4 FRTA20EU E2EU 20010405003542001040500354CE 2001 4 5 AU010273 120010316G3260 FASTENER CESSNA404 404CESSNA 2075901CE CONT O520 GTSIO520M 17032SO MCAULY3FF32 3FF32C501 GL MLG UPLOCK FAILED W O OTHER N FALSE WARNING CRCRUISE 1 AUS (AUS) LANDING GEAR UPLOCK ASSEMBLY HI-LOK FASTENERS FAILED. BRACKETS TORN AWAY FROM SPAR BOX. 1L72 3O3 O A25CE E7CE 5 CP45GL 20010405003552001040500355EU 2001 4 5 AU010274 120010321G2720NB45961 LEVER BNORM BN2 BN2B20 1520302EU LYC O540 IO540K1B5 41532EA HARTZLHCC2Y HCC2YK2 GL RUDDER CONTROL SLOOSE W K NONE O OTHER ININSP/MAINT 1 AUS (AUS) RUDDER CONTROL RT IDLER LEVER LOOSE AND CATCHING ON FUSELAGE FRAME OPENING. 1H72 3O3 O A17EU 1E4 5 CP920 20010405003562001040500356 2001 4 5 AU010276 420010317G61221680640 PICKUP WOODWARD 89741016 BAG JETSTMJETSTM3201 1500217EU GARRTTTPE331TPE33112UHR WP MCAULY4HFR344HFR34C653 NE PROP GOVERNOR FAULTY W C ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 AUS 2330240 (AUS) LT ENGINE GOVERNOR MAGNETIC PICKUP (MONOPOLE) OUTPUT VOLTAGEUNSTABLE. 2L72 4T4 TRTA56EU E4WE 6 C3PNE 20010405003572001040500357GL 2001 4 5 AU010277 320010320G6110991996 SPACER MCAULY B3DF36C527 PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA MCAULY3DF36CB3DF36C526 GL PROPELLER ASSY MISINSTALLED W K NONE W INADEQUATE Q C ININSP/MAINT 1 AUS 597 991996 (AUS) RT PROPELLER SPACER INCORRECTLY FITTED. 1L72 3O3 O A20SO E14EA 5 C 20010409000062001040900006EU 2001 4 9 R7MR32651 120010128G2460SP461310 SWITCH BOLKMSBK117 BK117C1 5626025EU TMECA ARRIELARRIEL1 60030NE DC SYSTEM WORN B R7MRK NONE O OTHER ININSP/MAINT 1 NM07117SU1080 7527 TOGGLE SWITCH WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 UNCH13EU E19EU 20010409000072001040900007EU 2001 4 9 R7MR32656 120010226G6320ZARISEC135 TRANSMISSION UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR COLLAPSED B R7MAK NONE L NO TEST NRNOT REPORTED 1 NM07135SJ594 EC1350054 MAIN ROTOR TRANSMISSION COLLAPSED. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. 1G72 3U3 UO H88EU E42NE 20010409000092001040900009EU 2001 4 9 R7MR32657 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ946 EC1350054 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409000102001040900010EU 2001 4 9 R7MR32658 120010228G6220L621M1003101 DAMPER UROCOPEC135 EC135P1 8680990EU PWA PW206 PW206A NE MAIN ROTOR WORN B R7MAK NONE O OTHER ININSP/MAINT 1 NM07135SJ946 EC1350054 ELASTOMERICS WORN BEYOND SERVICEABLE LIMITS. SPLITLINE CRACK LONGER THAN 40MM. REPLACED WITH NEW UNIT, CORRECTED PROBLEM NOTE: THE REPLACEMENT DAMPER HAS LESS THAN 1 YEAR TO SERVICE LIFE. 1G72 3U3 UO H88EU E42NE 20010409000192001040900019SO 2001 4 9 20010305CW013 120010123G7714640925 ADAPTER PIPER PA34 PA34200T 7103406SO TMECA ARRIELARRIEL1 60030NE TACH GENERATOR FAILED B K NONE O OTHER ININSP/MAINT 1 NE012240D274 347970032 807536R 90 DEGREE TACH ADAPTER PUT ON AIRCRAFT. WHEN ADAPTER FAI