20081201 NM 2008 12 1 USAA920082024 120081024A53136545800 STRINGER BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT Q3 MAJOR REPAIR NR 03C20553006/006 LEVEL 2 EXFOLIATION CORROSION AT STRINGER 18R BETWEEN BS294 TO BS325. REPAIRED STRINGER 18R BETWEEN BS294 TO BS325 IAW B737 SRM 53-00-03. 2L72 4F RTA16WE 20081201 NM 2008 12 1 ASAA0893789 120081115A5230 SKIN BOEING737 737990 NM CARGO DOOR DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02320AS 33680 FWD CARGO DOOR OUTER SKIN YELLOW DOT APPLIED AT DENT NOT ON SAD RUN 28 INCHES FROM AFT EDGE 22 INCHES FROM TOP. 2L74 4F RTA16WE 20081201 NM 2008 12 1 SWAA086608 120081125A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 8R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086565 120081123A3350411A2212 LENS BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29920WN 32460 FOUND R2 DOOR EGRESS LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 DL757081635 120081118A5340146N85154 ATTACH ANGLE BOEING757 757232 1384965NM BS 1461 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 CORROSION ON ATTACH ANGLE BS 1461 RBL 22 WL 145, AFT CARGO COMPARTMENT OUT OF LIMITS. REMOVED AND REPLACED PART. 2L72 4F RTA2NM 20081201 NM 2008 12 1 AALA200820026 120081023A5320 TEE FITTING BOEING757 757223 1384957NM BS 1720 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21663AM53392 25279 TEE FITTING CORRODED AFT RT CORNER OF DECK PLATE. REPLACED TEE FITTING IAW SRM 53-60-51. 2L72 4F RTA2NM 20081201 NM 2008 12 1 AALA200820027 120081027A5340415N400110 FITTING BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21604AA43723 27055 AFT OUTBOARD RIGHT SIDE GALLEY FITTING CORRODED. REPLACED FITTING IAW SRM 53-00-51. 2L72 4F RTA2NM 20081201 NM 2008 12 1 DLM88081598 120081120A750013277503 DUCT DOUG MD88 MD88 3023688NM PWA JT8 JT8D219 52053NE NR 2 ENGINE DAMAGED A DALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27980DL 53267 725545 RT ENGINE FIRE LIGHT CAME ON DURING FLIGHT. FOUND BLOWN DUCT AT AFT SIDE OF COWL ANTI-ICE VALVE. REPLACED DUCT FROM 13TH STAGE SADDLE DUCT TO COWL ANTI-ICE VALVE. 2L72 4F4 FRTA6WE E9NE 20081201 NM 2008 12 1 DL757081611 120081115A5320143N51974 ANGLE BOEING757 757232 1384965NM PWA 4060 PW4060 52119NE BS 660 WL 208 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 724164 WL 208, BS 660 RBL 48, WEB UPPER ANGLE CRACKED. REMOVED AND REPLACED ANGLE. 2L72 4F4 FRTA2NM E24NE 20081201 EA 2008 12 1 SWIA200820480 120081119A5241 HANDLE CNDAIRCL600 CL6002B19 1900309EA GALLEY DOOR NICKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07408SW 7055 FLT 4852 - GALLEY SERVICE DOOR HARD TO OPEN FROM OUTSIDE. REMOVED BURR FROM OUTER HANDLE DOOR ALIGNMENT PIN. 2L72 4F RTA21EA 20081201 NM 2008 12 1 AALA200820031 120081024A5315146N509131 FLOORBEAM BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21697AN45632 26977 FLOORBEAM CORRODED. REPAIRED IAW EA B757-53-004789. 2L72 4F RTA2NM 20081201 WP 2008 12 1 AALA200810196 120081112A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT WEAK A AALAK NONE O OTHER ININSP/MAINT 1 SW21584AA 53247 MID CABIN EMERGENCY LIGHT BATTERY PACK WEAK AT STATION 500R. INSTALLED NEW BATTERY PACK. 2L72 4F A6WE 20081201 NM 2008 12 1 AALA200820036 120081028A5320146N8769U48 CHANNEL BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21663AM53392 25297 HAT CHANNEL CORRODED. REPLACED HAT CHANNEL IAW SRM 51-21-03-7. 2L72 4F RTA2NM 20081201 EA 2008 12 1 SWIA200820454 120080830A5210 ANGLE CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07961SW 7857 C-CHECK, PASSENGER DOOR ANGLE CRACKED. REPAIRED PER SRM. 2L72 4F RTA21EA 20081201 NM 2008 12 1 SWAA086591 120081125A335081000 TRIM PANEL BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29428WN 29844 DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRIM LOOSE AT ROW 1. REMOVED AND REPLACED TRIM PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 DL76G081622 120081122A284041817054 PRESSURE SWITCH BOEING767 767332 1382001NM NR 2 ENGINE FAILED A DALAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 SO271608 30573 2 RT ENG WOULD NOT START. RTB, RT ENG PRESS SWITCH POPPING C/B REPLACED FUEL PRESSURE SWITCH PER M/M. OP CKS GOOD RAN ENG AT IDLE, NO FAULTS NOTED. ETOPS CATEGORY 'D': INABILITY TO CTRL ENG OR GET DESIRED PWR. 2L72 4F RTA1NM 20081201 NM 2008 12 1 ASAA0893816 120081120A5320146A7502 SUPPORT ANGLE BOEING737 737990 NM BS 727-727I CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02320AS 33680 CORROSION ON THE LOWER BULKHEAD SUPPORT ANGLE. REMOVED AND REPLACED SECTION BS 727I-772. 2L74 4F RTA16WE 20081201 NE 2008 12 1 ASAA0853779 220081115A72003370051180 SPINNER BOEING737 737890 1384527NM CFMINTCFM56 CFM567B27 13046NE NR 1 ENGINE WORN A ASAAK NONE O OTHER ININSP/MAINT 1 NM02579AS 35187 894547 SPINNER FRONT CONE MISSING MORE THAN 20 PERCENT OF BLACK ANODIZED COATING. REMOVED AND REPLACED SPINNER CONE REF MM 72-21-01. 2L72 4F4 FRTA16WE E00055EN 20081201 NM 2008 12 1 ASAA0893844 120081122A5320146A7510 INTERCOSTAL BOEING737 737990 NM BS 500J-500K BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02320AS 33680 WHILE WORKING CARD (FUSE 5043 CUST CARD 5140481) FOUND BAFFLE INTERCOSTAL BENT FWD CARGO BAY STA 500S 500K. REMOVED FABRICATED NEW AND INSTALLED INTERCOSTAL. 2L74 4F RTA16WE 20081201 CE 2008 12 1 GUUA10100802 120081010A5220 LOCK BEECH 1900 1900D 1154162CE EMERGENCY EXIT LACK OF LUBE A GUUAK NONE O OTHER ININSP/MAINT 1 SO2969549 UE194 AT SCHEDULED ROUTINE MAINT DISCOVERED LT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN. APPLIED LUBRICANT TO LT AFT EMERGENCY EXIT LOCKING ASSY. OPS CHECK NORMAL. 2L72 4T RTA24CE 20081201 NM 2008 12 1 USAA2008112192102120081105A5320D53480043204 SILL AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19804AW 1043 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL OF L-2 DOOR BETWEEN FR67 +17 INCHES AND FR68, Y1732 IN PASSENGER CABIN. REPAIRED LOWER SILL OF L-2 DOOR BETWEEN FR67 +17 INCHES AND FR68, Y1732 IAW A319 SRM 53-41-14. 2L72 4F RTA28NM 20081202 EU 2008 12 2 USAA2008112492119120081121A2530 OVEN AIRBUS320 A320232 3930326EU GALLEY ODOR A USAAK NONE B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA19648AW 770 FLT 138 LAS-SNA - BURNING SMELL - NR 2 OVEN EMITS ACRID SMELL WHEN OPERATED. MAINTENANCE COULD NOT DETERMINE CAUSE FOR ODOR - PULLED CIRCUIT BREAKER. MAINTENANCE CLEANED NR 2 OVEN AND NO ODOR NOTED. NO SUBSEQUENT EVENTS. 2L72 4F RTA28NM 20081202 EA 2008 12 2 MALA080199 120081126A2120 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA CABIN ODOR A MALAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL158944B N8944B CAPTAIN CALLED-ADVISED THEY HAD AN AMBER CAUTION SMOKE IN THE LAVATORY. FLT ATTENDANT ADVISED SMOKE ALARM WAS GOING OFF AND THERE WAS A FIRE ODOR. FLIGHT RETURNED TO MSP BUT WHILE ON THE APPROACH CAUTION AND ALARM WENT OFF. FLIGHT DID NOT DECLARE AN EMERGENCY BUT DID LAND OVERWEIGHT. 2L72 4F RTA21EA 20081202 NM 2008 12 2 USAA2008112892141120081112A552265C25746132 REPAIR BOEING737 7373G7 138447JNM RT ELEVATOR DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19307AW 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED ON RIGHT ELEVATOR UPPER SURFACE AT ELEVATOR STA 108.5. REPAIRED RIGHT ELEVATOR UPPER SURFACE IAW B737 SRM 51-70-03-0G. 2L72 4F RTA16WE 20081202 NM 2008 12 2 USAABB08172 120081126A335020121 CHARGER BOEING767 767201 1385125NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19249AU 23901 BRU - DURING THE DAILY CHECK, THE EMERGENCY FLOOR PATH LIGHTING WAS FOUND INOPERABLE FROM ROW 1A/B TO ROW 8A/B. MAINTENANCE REPLACED THE BATTERY CHARGER ASSEMBLY. OPERATIONALLY CHECKS OK. 2L72 4F RTA1NM 20081202 NM 2008 12 2 USAA2008112892143120081127A575465C25602223 REPAIR BOEING737 7373G7 138447JNM LE SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19307AW 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED ON LEFT WING NR 2 SLAT UPPER SURFACE WS 251. REPAIRED NR 2 SLAT UPPER SURFACE IAW B737 SRM 51-70-10-2R. 2L72 4F RTA16WE 20081202 NM 2008 12 2 USAABB08173 120081125A3260835606 PSEU BOEING757 757225 1384959NM FAILED A USAAK NONE N FALSE WARNING TOTAKEOFF 1 EA19920UW 22199 FLIGHT 882, LAS-BOS - AFTER TAKEOFF IN LAS, THE CREW RECEIVED "GEAR DOORS AND GEAR DISAGREE" MESSAGE ON EICAS. THE DOOR AND GEAR AMBER LIGHT ON FORWARD PANEL ILLUMINATED. ALL INDICATIONS WERE NORMAL AFTER RECYCLING THE GEAR. MAINTENANCE REPLACED PSEU CARD. 2L72 4F RTA2NM 20081202 NM 2008 12 2 UALA2008111305435120080823A3350363674 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29654UA 25392 ROW 14 LT EEL STRIP INOP. REPLACED STRIP. 2L72 4F4 FRTA1NM E24NE 20081202 NE 2008 12 2 UALA2008111305610220080906A732153T424 THERMOCOUPLE BOEING777 777222 1385219NM PWA PW4090PW40903 51538NE RT ENGINE FAULTY A UALAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 WP29206UA 30212 RIGHT ENG 2.9 STAB BLEED VALVE TC PROBE CHANNEL B SIGNAL OUT OF RANGE. REPLACED NR 2 ENG EEC PER MM 73-21-04. NO HELP CORRECTING PROBLEM. EEC OP CHECKS NORMAL. INSTALLED NEW GOOD PROBE IN 'B' POSITION, CHECKS OK. 2L72 4F4 FRTT0001SE E46NE 20081202 2008 12 2 UALA2008111306226420081021A2565101655305 SLIDE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE OVERWING EXIT NO TEST A UALAK NONE WL INADEQUATE Q C NO TEST ININSP/MAINT 1 WP29642UA 25092 DURING LT OVERWING SLIDE DEPLOYMENT TEST, AFT HATCH STEP FAILED TO DROP DOWN, CABLE KINKED, STEP WILL NOT DROP FREELY. REPLACED AFT SUPPORT CABLE. OPS CHECKS GOOD. SLIDE FAULTY. AFTER CHECKING THE SLIDE SYS OUT, VERIFIED THE BOTTLE PRESSURE AND WHITE DISK WERE CORRECT, THEY WERE PULLED AND SET UP THE SLIDE SYS IAW ROUTINE JIC 6-1950-50-1 0. WITH HYD PWR ON AND SPOILERS UP, THE LT AFT OVERWING HATCH WAS REMOVED, THE SPOILER BLOW DOWN ACTUATOR FIRED, PUSHING 85625, THE INBD SPOILER TO THE DOWN POSITION. LT OVERWING SLIDE COMPARTMENT DOOR OPENED TO THE FULL OPEN POSITION. THIS PULLED THE CABLE THAT ACTUATES THE BOTTLE. AT THE INFLATION BOTTLE, THE BELL CRANK MOVED SLIGHTLY ENOUGH TO PULL THE CABLE FROM THE2L72 4F4 FRTA1NM E24NE 20081202 NM 2008 12 2 UALA2008111306339120081031A335078941 LIGHT BOEING777 777222 1385219NM PWA PW4077PW4077 NE CABIN LOOSE A UALAO OTHER W INADEQUATE Q C ININSP/MAINT 1 WP29778UA 26940 EEL STRIP AT SEAT 2E IS LOOSE WITH WIRES SHOWING. SECURED LIGHT, CHECKS GOOD. 2L72 4F4 FRTT0001SE E46NE 20081202 NM 2008 12 2 UALA2008111306369120081103A3350362624 LIGHT BOEING757 757222 1384956NM PWA 2037 PW2037 NE CABIN LOOSE A UALAO OTHER W INADEQUATE Q C ININSP/MAINT 1 WP29548UA 25396 EMERGENCY LIGHT STRIP IN FRONT OF FC CLOSET IS LOOSE. SECURED LIGHT STRIP. 2L72 4F4 FRTA2NM E17NE 20081202 NM 2008 12 2 UALA2008112406616120081119A2421S281T00137 GENERATOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE APU FAULTY A UALAO OTHER W INADEQUATE Q C ININSP/MAINT 1 WP29643UA 25093 APU GENERATOR INOPERATIVE. CHECKED FEEDER CONNECTOR PER TIP 24-21-01-200A & FOUND OK. TRIED NEW GCU, NO HELP. BPCU BITE SHOWS "REPLACE GEN-(DIODE)". NEEDS GENERATOR REPLACED. REPLACED APU GENERATOR. OPS NORMAL. 2L72 4F4 FRTA1NM E24NE 20081202 NM 2008 12 2 UALA2008112406621120081122A5330 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29552UA 26641 FUSELAGE SKIN DENT STA 760, AT STR 17L. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SKIN AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20081202 NM 2008 12 2 UALA2008112406623120081122A5220BACC2A4D00134JJ CABLE BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EMERGENCY EXIT KINKED A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 RT AFT EMERG EXIT HATCH STEP FWD CABLE IS KINKED. REPLACED CABLE. 2L72 4F4 FRTA1NM E24NE 20081203 NM 2008 12 3 AALA200820041 120081103A5330146N5318 PLATE BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21604AA43723 27055 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R. 2L72 4F RTA2NM 20081203 EA 2008 12 3 BSY2008F00010 220081031A74141068291018 MAGNETO PIPER PA31 PA31350 7103110SO LYC O540 TIO540J2BD 41532EA RT ENGINE INTERMITTENT D BSYAO OTHER R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 GL073587P 318052120 RT ENGINE LOST POWER ON TAKE OFF, ABORTED TAKEOFF. (K) 1L72 3O3 O A20SO E14EA 20081203 NM 2008 12 3 AALA200802733 120081013A3350 LAMP BOEING757 757223 1384957NM EMERGENCY LIGHT BURNED OUT A AALAK NONE L NO TEST ININSP/MAINT 1 SW217667A 25301 MIA - EMERGENCY LIGHT AT SEAT ROW 5 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 5. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20081203 NM 2008 12 3 AALA200802736 120081014A3350 LAMP BOEING757 757223 1384957NM EMERGENCY LIGHT BURNED OUT A AALAK NONE L NO TEST ININSP/MAINT 1 SW21617AM 24525 DFW - EMERGENCY LIGHT AT SEAT ROW 11DEF BULL NOSE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT ROW 11DEF BULL NOSE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA2NM 20081203 SO 2008 12 3 FDKA2008111600296120081116A3222 STRUT EMB 145 EMB145LR 3260212SO NLG LOW A FDKAK NONE O OTHER CRCRUISE 1 SW07848MJ 145530 FRL FLT 6250 CLT-CVG - LANDING GEAR AIR GOUND FAIL. MX SERVICED NOSE STRUT AND OPS CHECKED GOOD. 2L72 4T RTT00011AT 20081203 SO 2008 12 3 FDKA2008112800300120081128A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A FDKAK NONE O OTHER NRNOT REPORTED 1 SW07858MJ 145767 FRL FLT 6167 CVG-IND - AFT CEILING EXIT LOCATOR, FWD SIDE OUT. MX REMOVED AND REPLACED NR 3 AND NR 4 BATTERY PACKS. 2L72 4T RTT00011AT 20081203 NM 2008 12 3 AALA200802728 120081012A3350 LAMP BOEING777 777223 1385213NM EMERGENCY LIGHT BURNED OUT A AALAK NONE L NO TEST ININSP/MAINT 1 SW21771AN 29579 DFW - EMERGENCY PROXIMITY LIGHT AT SEAT 22C INOPERATIVE. REPLACED LAMP FOR EMERGENCY PROXIMITY LIGHT AT SEAT 22C. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTT00001SE 20081203 NM 2008 12 3 AALA200802729 120081029A29306937317300 CONTROL MODULE BOEING737 737823 13844BZNM HYD SYSTEM FAULTED A AALAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW21905AN 29507 PIT INFLIGHT LAX TO IAD - DURING CRUISE, CREW REPORTED ENGINE NR 1 HYDRAULIC LOW PRESSURE INDICATION ILLUMINATED FOLLOWED BY ENGINE NUMBER TWO HYDRAULIC LOW PRESSURE INDICATION. CREW TURNED OFF BOTH PUMPS AND LANDED PIT WITHOUT INCIDENT. EICAS SHOWED NORMAL HYDRAULIC PRESSURES AND QUANTITIES. FOUND HYDRAULIC PRESSURE INDICATING SYSTEM FAULTED. REPLACED HYDRAULIC RESERVOIR PRESSURE MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA16WE 20081203 WP 2008 12 3 AALA200810199 120081110A5313 STRINGER DOUG DC9 DC982 3022082WP ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 LONGERON 30 CORRODED FROM STATION 465-494. INSTALLED LONGERON REPAIR AT STATION 465-494 PER ESO 80559 DATED 11/04/2008. 2L72 4F A6WE 20081203 CE 2008 12 3 BSY2008F00018 120081023A3700442CW12 PUMP BEECH 58 58 1152740CE VACUUM SYSTEM FAILED E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL079044V TH216 RT ENGINE DRIVEN VAC PUMP FAILED. THE SCREW FOR CHECKING WEAR ON VANES WAS MISSING, CAUSING PREMATURE FAILURE. (K) 1L72 3O 3A16 20081203 EA 2008 12 3 HNAA2008112000323120081116A325189923 LINK DHAV DHC8 DHC8311 1386006EA NLG STEERING BROKEN A HNAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA07326EN9769 5343 SAM0190106 234 IN PREPARATION FOR LANDING AT PHL THE FLIGHT CREW SELECTED THE GEAR DOWN AND THE NOSE GEAR INDICATOR WAS RED. THE MAIN GEAR INDICTED NORMAL. THE FLIGHT CREW DID THE ALTERNATE EXTENSION AND THE NOSE GEAR DID NOT COME DOWN. THE AIRCRAFT LANDED WITH THE NOSE STILL RETRACTED, , THERE WERE NO INJURES REPORTED. UPON INSPECTION, LINK ON THE STEERING ACTUATOR FOUND BROKEN. STEERING ACTUATOR AND LINKS REPLACED. ACFT FERRIED TO SBY. DURING INSPECTION AFTER A NOSE GEAR UP LANDING, THE FRAME MEMBER AT X167.5 WAS BUCKLED BETWEEN STRINGERS 32S AND 32P.FRAME MEMBER WAS REPLACED IAW DEHAVILLAND STRUCTURAL REPAIR MANUAL PROCEDURES. AIRCRAFT HAS NOT BEEN RELEASED YET DUE TO OTHER ONGOING WORK. 2H72 4T RTA13NM 20081203 NM 2008 12 3 HNAA2008120200326120081124A3350 LIGHT DHAV DHC8 DHC8102 2809003NM CABIN MALFUNCTIONED A HNAAK NONE O OTHER UKUNKNOWN 1 EA07938HA 152 EMERGENCY EXIT SIGN AT SEAT 4A REMAINS ILLUMINATED CONSTANTLY. INSPECTED AND FOUND LIGHT NOT TO BE ILLUMINATED. 2H72 4T RTA13NM 20081203 SO 2008 12 3 RAIA2008111500001120081112A3350 LIGHT EMB 145 EMB145 3260210SO CABIN INOPERATIVE A RAIAK NONE L NO TEST ININSP/MAINT 1 CE03821HK 145068 PRE FLT INSPECTION REVEALED THAT THE EMERGENCY LIGHT AT SEAT 12A WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE LIGHT ASSEMBLY. SYSTEM OPS CHECKED GOOD. 2L72 4F RTT00011AT 20081203 SO 2008 12 3 RAIA2008112500004120081122A3222 O-RING EMB 145 EMB145EP 3260221SO NLG WORN A RAIAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 CE03809HK 145187 DURING CLIMB, CREW RECEIVED A LG AIR/GND FAIL MESSAGE ON THE EICAS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A LEAKING O-RING ON THE NLG SERVICING PORT. THE O-RING WAS REPLACED, NLG WAS SERVICED, AND AN OPERATIONAL CHECK OF THE EXTENSION AND RETRACTION SYSTEM WAS PERFORMED. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20081203 SO 2008 12 3 RAIA2008112400001120081119A2930300045021 THERMAL SWITCH EMB 145 EMB145LR 3260212SO HYDRAULIC SYS FAULTY A RAIABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CRCRUISE 1 CE03812HK 145373 DURING CRUISE, CREW RECEIVED A HYDRAULIC SYSTEM 1 OVERHEAT MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 1 SYSTEM HYDRAULIC THERMAL SWITCH. SYSTEM OPS CHECKED GOOD. 2L72 4T RTT00011AT 20081203 SO 2008 12 3 RAIA2008112500002120081122A3350 LIGHT EMB 145 EMB145EP 3260221SO CABIN INOPERATIVE A RAIAK NONE L NO TEST TXTAXI/GRND HDL 1 CE03806HK 145112 CEILING EMERGENCY LIGHT IN CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB AT THE CEILING EMERGENCY LIGHT. OPS CHECKED GOOD. 2L72 4F RTT00011AT 20081203 NM 2008 12 3 HNAA2008120200329120081123A33506013211X BATTERY PACK DHAV DHC8 DHC8102 2809003NM CABIN DISCHARGED A HNAAK NONE L NO TEST TXTAXI/GRND HDL 1 EA07846EX37338416 326 UPON ARRIVAL TO A/C, F/A FOUND EMERGENCY LIGHT TO HAVE BEEN LEFT ON. EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERIES, CABIN NUMBER S 3, 4, 5 AND 6 IAW 33-50-05R, OPS CHECK GOOD IAW 33-50-03Q BATTERY S/N SBY-75 , SBY-1, $99088, ORF177. 2H72 4T RTA13NM 20081203 NM 2008 12 3 HNAA2008113000332120081130A31507003652611 DISPLAY DHAV DHC8 DHC8102 2809003NM COCKPIT DEFECTIVE A HNAAK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 EA07808EX228684307 299 DURING GROUND HANDLING WITH APU AND ENGINES RUNNING, THE CREW NOTICED AN ELECTRICAL SMELL IN THE CABIN AND COCKPIT. MAINTENANCE DISCOVERED THE PILOTS ADVISORY DISPLAY PANEL TO BE THE SOURCE OF THE ODORS. THE DISPLAY PANEL WAS PLACED ON THE MEL LIST AND THE AIRCRAFT RELEASED FOR FURTHER FLIGHT. THE DISPLAY PANEL WAS SUBSEQUENTLY CHANGED AND OPS CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. 2H72 4T RTA13NM 20081203 EU 2008 12 3 08FDEA04961 120081122A5347R538D1042201 SEAT TRACK AIRBUS310 A310304 3930339EU FUSELAGE DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21817FD 552 MAIN DECK CARGO COMPT SEAT TRACK NR 2 RT, 12 IN AFT OF FR 43 HAS 2 DAMAGED SCALLOPS. REMOVED DAMAGED SECTION OF SEAT TRACK NR 2 RT. FABRICATED REPLACEMENT SECTION AND INSTALLED BETWEEN FR 40 AND FR 45 IAW A310 SRM 53-10-16 AND SRM 51-40-21. 2L72 4F RTA35EU 20081203 EU 2008 12 3 08FDEA04963 120081124A5270 SWITCH AIRBUS310 A310222 3930315EU AFT CARGO DOOR FAULTY A FDEAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE21455FE 331 AFT CARGO DOOR OPEN LIGHT IN FLIGHT. RETURNED TO KUL. VISUALLY CHECKED CLOSED AND LOCKED. VERIFIED INTEGRITY OF AFT CARGO DOOR CLOSING AND LOCKING MECHANISM. ALL SATISFACTORY. SUSPECT FAULTY MICROSWITCH CAUSING ERRONEOUS DOOR INDICATION. APPLIED MEL 52-71-01. 2L72 4F RTA35EU 20081203 EU 2008 12 3 08FDEA04965 120081124A5320 FITTING AIRBUS300 A300B4622 3930401EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21716FD 358 MAIN CABIN, AT FRAME 49 AND GANTRY 4 LT, SEAT TRACK, "LINKAGE FITTING" IS CRACKED, UNDER FLOOR. REMOVED AND REPLACED THE SEAT TRACK LINK FITTING IAW A300-600 SRM 51-40-21, PARA 5, P/N A5381206720100, PO NR 640729.1. 2L72 4F RTA35EU 20081201 NM 2008 12 1 USAA920082035 120081022A53206545834256 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/015 LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BS312 TO BS328, LBL11. REPLACED INTERCOSTAL BS312 TO BS328, LBL11 IAW B737 SRM 51-10-02. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA920082026 120081106A532050794649 ATTACH ANGLE BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753006/012 INTERCOSTAL ATTACH ANGLE CRACKED AT BS296 BEHIND H STRAP. REPLACED INTERCOSTAL ATTACH ANGLE AT BS296 BEHIND H STRAP IAW B737 SRM 51-10-02. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086597 120081125A33503071BPEGPL LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 23. REMOVED AND REPLACED LAMP PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086627 120081125A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 500, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086600 120081125A53156546804 FLOORBEAM BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54. REPAIRED BEAM PER ER. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086602 120081125A53116546532 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED SPV CHECK, FOUND FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20081201 NM 2008 12 1 DL757081636 120081118A5347694557932 CARGO TRACK BOEING757 757232 1384965NM BS 1400-1405 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 CORROSION ON AFT CARGO TIE DOWN FITTING BS 1400-1405 RBL 25 WL 147 AT DOOR CUTOUT, NO ALLOWABLE LIMIT. REMOVED AND REPLACED PART. 2L72 4F RTA2NM 20081201 NM 2008 12 1 DL757081641 120081118A534769455787 CARGO TRACK BOEING757 757232 1384965NM PWA JT8 JT8D219 52053NE BS 1383 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 725866 CORROSION ON AFT CARGO TIE DOWN FITTING BS 1383 RBL 25 WL 147 AT DOOR CUTOUT, NO ALLOWABLE LIMITS. REMOVED AND REPLACED FITTING PER SRM 51-40-02. 2L72 4F4 FRTA2NM E9NE 20081201 NM 2008 12 1 DL76S081642 120081124A2781 TARGET BOEING767 767332 1382001NM NR 10 SLAT UNSERVICEABLE A DALAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SO27130DL 24080 AFTER TAKEOFF APPROX 200FT AGL, THE STICK SHAKER ACTIVATED. AIRSPEED WAS NML AND FLAPS 15DEG. DURING FLAP RETRACTION RECEIVED LEADING EDGE SLAT ASYM CAUTION MSG. PERFORMED QRH PROCEDURE. FOUND DAMAGED TARGET AT NR 10 SLAT INBD TRACK. REPLACED SAME. REPLACED PROX BOX DUE TO NOT INDICATING TARGET PROBLEM. 2L72 4F RTA1NM 20081201 EA 2008 12 1 SWIA200820467 120081116A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07459SW 7782 AD INSPECTION, ENGINE SUPPORT BEAM INSPECTION PER AD CONFIRMED CRACKS. REPAIRED PER SB60R-53-065. 2L72 4F RTA21EA 20081201 NM 2008 12 1 DLM88081602 120081119A2710 CONTROL CABLE DOUG MD88 MD88 3023688NM FLAP/SLATS FOD A DALAO OTHER WCFINADEQUATE Q C F.O.D. FLT CONT AFFECTED APAPPROACH 1 SO27952DL 49883 WHEN SLATS/FLAPS WERE EXTENDED FROM CLEAN POSITION, THE AIRCRAFT ROLLED APPROXIMATELY 20-30 DEGREES UNCOMMANDED. INSPECTED AIRCRAFT, FOUND SCREWDRIVER STUCK IN CONTROL CABLES ABOVE E/E DOOR AT STA 116. REMOVED TOOL. RAN FLIGHT CONTROLS, FLAPS/SLATS, AILERON AND RUDDER TRIM. ALL CHECKS NORMAL. NO DAMAGE FOUND. OK FOR SERVICE. 2L72 4F RTA6WE 20081201 NM 2008 12 1 DLM88081603 120081120A4920 INLET DOUG MD88 MD88 3023688NM APU CONTAMINATED A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SO27963DL17700 49982 BOTH AFT LAV SMOKE DETECTORS WENT OFF AFTER TAKEOFF FOR BUF BOTH ENG ANTI-ICE ON FOR TAKEOFF, NO SMOKE, SLIGHT ODOR DETECTED, DISSIPATED RAPIDLY. SUSPECT DE-ICE FLUID INGESTION. APU INLET CLEAN PERFORMED ALT DUCT BURNOUT PER AIJC OPN 5090 AND REPLACED WATER SEPARATOR BAGS PER AIJC 7904. ALL CHECKS GOOD. 2L72 4F RTA6WE 20081201 NM 2008 12 1 DL757081612 120081111A5320146N54511 INTERCOSTAL BOEING757 757232 1384965NM PWA 4060 PW4060 52119NE BS 1538 LBL 11.4CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27618DL 22908 724164 CORROSION ON LOWER FLANGE OF INTERCOSTAL COMMON TO SKIN BILGE AREA LBL 11.40 BS 1538. REPAIRED DAMAGE PER DELTA ER/A 471504-14 REV ORIG. 2L72 4F4 FRTA2NM E24NE 20081201 WP 2008 12 1 AALA200810180 120081115A5311 FRAME DOUG DC9 DC982 3022082WP BS 1418 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW217537A 49991 FRAME AT STATION 1418 CRACKED AT LONGERON 2L. REPAIRED PER ESO80559 DATED 11-14-08. 2L72 4F A6WE 20081201 EA 2008 12 1 SWIA200820469 120081123A3350 LAMP CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHT BURNED OUT A SWIAK NONE O OTHER ININSP/MAINT 1 NM07810SK 15093 FLT 4530 - CEILING EMERGENCY LIGHT AFT CABIN INOP. RELAMPED. 2L72 4F RTA21EA 20081201 NM 2008 12 1 AALA200820029 120081028A5315 FLOORBEAM BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21697AN45632 26977 FLOORBEAM CORRODED. REPAIRED IAW EA B757-53-004765 2L72 4F RTA2NM 20081201 EA 2008 12 1 SWIA200820475 120081118A3350 LAMP CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHTSBURNED OUT A SWIAK NONE O OTHER ININSP/MAINT 1 NM07455SW 7760 FLT 4425 - CEILING LEVEL EMERGENCY FLOODLIGHT OVER ROW 2 INOP. RELAMPED. 2L72 4F RTA21EA 20081201 SO 2008 12 1 SWIA200820477 120081117A612330005000052 SIGNAL COND UNIT EMB 120 EMB120ER 3260203SO AUTOFEATHER SYS MALFUNCTIONED A SWIAC ABORTED TAKEOFF RJ PARTIAL RPM/PWR LOSS WARNING INDICATION TOTAKEOFF 1 NM07221SW 120290 FLT 5427 - ABORTED TAKEOFF DUE TO INADVERTENT AUTOFEATHER OF NR 1 ENGINE. REPLACED LEFT TORQUE PROBE AND TORQUE SIGNAL CONDITIONER PN ON 30005-0000-57, PN OFF 30005-0000-52, SN ON MM4720, SN OFF 4225. 2L72 4T RTA31SO 20081201 WP 2008 12 1 AALA200810190 120081118A5320 WEB DOUG DC9 DC983 3022083WP ZONE 200 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21965TW 53615 CANT FRAME 1485 UPPER LEFT WEB CRACKED AFT OF LEFT LOUVER BOX. INSTALLED DOUBLER PER AARD 53-10-00-32. 2L72 4F RTA6WE 20081201 WP 2008 12 1 AALA200810193 120081120A2761 CASTING DOUG DC9 DC982 3022082WP SPOILER ACTUATORCRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21586AA 53249 GROUND SPOILER ACTUATOR CASTING CRACKED FORWARD INBD CORNER, LEFT GROUND SPOILER. INSTALLED REPAIR DOUBLER PER AARD 57-20-00-15. 2L72 4F A6WE 20081201 NM 2008 12 1 AALA200820037 120081028A5320146N8767U48 CHANNEL BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21663AM53392 25297 HAT CHANNEL CORRODED. REPLACED HAT CHANNEL IAW SRM 51-21-03-7. 2L72 4F RTA2NM 20081201 EA 2008 12 1 SWIA200820445 120080827A5320 SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 C-CHECK SUPPORT AND CLIP AT FS 625 CRACKED. REPLACED PER SRM. 2L72 4F RTA21EA 20081104 WP 2008 11 4 UPS08853748 120081002A5320 CUSP WEB DOUG DC8 DC871F 302199DWP FUSELAGE CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:SV EVALUATION REPAIR EFN 70219971243 ORIGINAL NRC 750796 CUSP MEMBRANE CRACKED AT TRACK G FS 1470. PREVIOUSLY REPAIRED IAW 53-02-00 FIG 025. 2L74 4F RT4A25 20081201 EA 2008 12 1 COMA0860463 120081113A5730601R10045 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A COMAK NONE O OTHER ININSP/MAINT 1 SO27784CA 7319 RT WING FUEL ACCESS PANEL CUTOUT AT 640BB HAS PITTING CORROSION AROUND EDGES. REMOVED CORROSION IN THE NON CRITICAL AREA AT FUEL ACCESS PANEL 640BB CUTOUT AND FOUND THAT MATERIAL REMOVED WAS WITHIN LIMITS PER REO 601R-57-21-030 REV G. 2L72 4F RTA21EA 20081201 NM 2008 12 1 SWAA086569 120081124A53156546804 FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, BETWEEN LBL 38 TO RBL 40. REPAIRED BEAM PER SWA EA. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086578 120081124A5311654580744 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND FRAME CRACKED AT BS 291, STR 17R. REPAIRED FRAME PER SWA EA. 2L72 4F RTA16WE 20081201 EA 2008 12 1 SWIA200820472 120081111A5346 SUPPORT BEAM CNDAIRCL600 CL6002B19 1900309EA ENGINE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07913EV 7731 AD INSPECTION, ENGINE SUPPORT BEAM INSPECTION PER AD CONFIRMED CRACKS. REPAIRED PER SB60R-53-065. 2L72 4F RTA21EA 20081201 EA 2008 12 1 SWIA200820458 120080810A7120 MOUNT CNDAIRCL600 CL6002B19 1900309EA RT ENGINE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07959SW 7840 C-CHECK, RIGHT ENGINE AFT THRUST MOUNT FITTING CORRODED. REPLACED PER AMM. 2L72 4F RTA21EA 20081201 EA 2008 12 1 SWIA200820463 120081120A3397 WIRE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY LIGHT BROKEN A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07494CA 7765 FLT 2642 - ENTRY DOOR FLOOR LEVEL EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE. 2L72 4F RTA21EA 20081201 NM 2008 12 1 SWAA086593 120081125A335081000 COVER BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29499WN 32481 DURING SCHEDULED HC2 CHECK, FOUND FWD EEPLS LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086594 120081125A335065C27095 BATTERY PACK BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29499WN 32481 DURING SCHEDULED HC2 CHECK, LT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20081201 2008 12 1 JGV2008F00004 420081104A256182122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531CE LIFE VEST MISSING B JGVRK NONE W INADEQUATE Q C ININSP/MAINT 1 CE09177JB L782069 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECEIVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPECTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTINE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFORMED. (K) 2L72 4F RTA10CE 20081201 2008 12 1 USAAEMB08019 420081113A2565 STITCHING EMB ERJ190ERJ190100IGW3260408NM ESCAPE SLIDE LOOSE A USAAK NONE O OTHER ININSP/MAINT 1 EA19946UW3768 19000072 ORF - MAINTENANCE FOUND THE FORWARD PASSENGER DOOR EVACUATION SLIDE LACING CORD UNRAVELED. MAINTENANCE REMOVED AND REPLACED THE SLIDE. 2L72 4F RTA57NM 20081201 NM 2008 12 1 ASAA0893804 120081117A5320143A751022 INTERCOSTAL BOEING737 737990 NM BS 500K CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02320AS 33680 SIDEWALL SUPPORT INTERCOSTAL CRACKED AT FASTENER HOLE. REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT INTERCOSTAL BETWEEN BS 500J AND 500K IAW SRM 51-40-02 STEP 4B AND C 2L74 4F RTA16WE 20081201 NM 2008 12 1 ASAA0893805 120081119A5320146A8127 SHIELD BOEING737 737990 NM BS 767-787 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02320AS 33680 CORROSION ON SIDEWALL SUPPORT PLATE SHIELD STA 767 787 RBL 23. REMOVED, FABRICATED NEW SUPPORT AND INSTALLED. 2L74 4F RTA16WE 20081201 NM 2008 12 1 ASAA0893815 120081120A5320143A9485Y35 SUPPORT ANGLE BOEING737 737990 NM BS 500L CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02320AS 33680 CORROSION ON THE LOWER BULKHEAD SUPPORT ANGLE. REPLACED LOWER SUPPORT ANGLE AT BS 500L LBL 25 RBL 25 PER SRM 51-20-05 AND 51-40-01. 2L74 4F RTA16WE 20081201 NM 2008 12 1 SWAA086540 120081120A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM BS 461 CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29313SW 23335 DURING SCHEDULED MV1 CHECK, FOUND STRINGER CRACKED AT BS 461, STR 18L. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20081201 CE 2008 12 1 GUUA10100803 120081010A5220 LOCK BEECH 1900 1900D 1154162CE EMERGENCY EXIT LACK OF LUBE A GUUAK NONE O OTHER ININSP/MAINT 1 SO2969549 UE194 AT SCHEDULED ROUTINE MAINT, DISCOVERED RT AFT EMERGENCY EXIT FROZEN AND WILL NOT OPEN, APPLIED LUBRICANT TO RT AFT EMERGENCY EXIT LOCKING ASSY. OPERATIONAL CHECK NORMAL. 2L72 4T RTA24CE 20081201 EA 2008 12 1 SWIA200820447 120080827A5320 SUPPORT CNDAIRCL600 CL6002B19 1900309EA BS 280 CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07918SW 7645 C-CHECK, FS 280 LBL 9 SUPPORT CLIP CRACKED. REPAIRED PER REO. 2L72 4F RTA21EA 20081201 EA 2008 12 1 SWIA200820453 120080830A5340 STRINGER CLIP CNDAIRCL600 CL6002B19 1900309EA BS 625 S14L CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07961SW 7857 C-CHECK, FS 625 LEFT STRINGER CLIP AT STRINGER 14L CRACKED. REPLACED PER SRM. 2L72 4F RTA21EA 20081201 EU 2008 12 1 RMXA11911708 120081031A5302 SKIN AGUSTA AGUSTAA109 A119 0261102EU PWA PT6 PT6B37A 52179NE TAILBOOM CRACKED E RMXAK NONE O OTHER AAAIR AMBULANCE 1 SW05820NA 14011 PU0008 A CRACK DEVELOPED IN THE TAILBOOM SKIN AT APPROXIMATELY STA 9725, WL 1895, LT SIDE EMANATING FROM A RIVET FORE AND AFT WITH A TOTAL LENGTH OF APPROX 79 MM. 1G71 3U4 U H7EU E4EA 20081201 NM 2008 12 1 DL757081619 120081118A5320 ANGLE BOEING757 757232 1384965NM PWA 4060 PW4060 52119NE BS 1480 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 724164 FOUND CORROSION ON INTERCOSTAL UPPER ATTACH ANGLE TO BE OUT OF LIMITS. FABRICATED REPLACEMENT ANGLE AND INSTALLED ANGLE BS 1480-1500 RBL 27. 2L72 4F4 FRTA2NM E24NE 20081201 NM 2008 12 1 SWAA086574 120081124A5230002354370 DOOR FRAME BOEING737 7373H4 1384600NM AFT CARGO DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29370SW 26597 DURING SCHEDULED HC2 CHECK, FOUND AFT CARGO DOOR FWD LOWER FRAME CRACKED. REMOVED AND REPLACED DOOR PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086587 120081125A5610141A481018 WINDOW BOEING737 7377H4 1384404NM COCKPIT ARCED A SWAAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW29223WN 32492 R2 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086589 120081125A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29375SW 26583 DURING SCHEDULED MV2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 494, STR 10R. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA2008111792068120081105A5315D53472192200 FLOORBEAM AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19804AW 1043 SAL - MAJOR REPAIR - C7 CHECK - CORROSION ON FLOORBEAM AT FR 69 - FR 70, +Y765. REPLACED FLOORBEAM AT FR 69 - FR 70, +Y765 IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20081201 NM 2008 12 1 ASAA0893849 120081122A5320146A7510 WEB BOEING737 737990 NM BS 500I-500J BENT A ASAAK NONE O OTHER ININSP/MAINT 1 NM02320AS 33680 BAFFLE INTERCOSTAL BENT FWD CARGO BAY STA 500I, 500J LH 26 WL 154. REMOVED 2L74 4F RTA16WE 20081201 NM 2008 12 1 ASAA0843821 120081115A532065479575 INTERCOSTAL BOEING737 7374Q8 138447QNM BS 787-793 CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02760AS 25098 AFT CARGO PIT CORRODED INTERCOSTAL STA 787 TO STA 793 STR 26R AREA. REMOVED DAMAGED INTERCOSTAL, LOCATED, DRILLED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-40-02 AND 51-40-05. 2L72 4F RTA16WE 20081201 2008 12 1 JGV2008F00001 420081104A256182122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531CE GARRTTTFE731TFE731* 01518WP LIFE VEST FAILED B JGVRK NONE O OTHER ININSP/MAINT 1 CE09177JB L782100 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECEIVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPECTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTINE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFORMED. (K) 2L72 4F4 FRTA10CE E6WE 20081201 NM 2008 12 1 SWAA086539 120081122A3350207377 LENS BOEING737 7377H4 1384404NM EMERGENCY LIGHT MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29244WN 34864 DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY LIGHT LENS MISSING AT ROW 1. REPLACED LENS PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086544 120081123A53306547952 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29326SW 23690 DURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT CARGO DOOR CUTOUT UPPER AFT CORNER. REPAIRED SKIN PER SRM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086545 120081123A3350 LAMP BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29337SW 23959 DURING SCHEDULED MV4 CHECK, FOUND R2 DOOR LOWER EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAASB08110 120081116A21216454051 FAN BOEING737 7374B7 138449CNM CABIN NOISY A USAAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19454UW489293122 24996 MIA - FLT 741 - EN ROUTE PHL TO MIA. ON TAXI-OUT, THE FLIGHT CREW NOTICED THAT THE LEFT RECIRCULATION FAN WAS NOISY. THE FAN WAS TURNED OFF AND THE FLIGHT PROCEEDED. DURING THE FLIGHT, THE FLIGHT CREW NOTICED AN OILY ODOR COMING FROM THE COCKPIT GASPER VENT. THE CREW SHUT-OFF THE RIGHT RECIRCULATION FAN, AND THE ODOR DISSIPATED. THE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED AIRCRAFT ON MEL. MAINTENANCE REPLACED THE LEFT RECIRCULATION FAN. OPERATIONALLY CHECKS OK. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA2008112092097120081105A5320D5347112420300 SHEAR PLATE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19804AW 1043 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 & FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 & FR70, S23R IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20081201 CE 2008 12 1 ZESA2008008 120081013A5730 FUEL DOOR CESSNA560 560XL 2076702CE RT WING OPEN E ZESAA UNSCHED LANDING W INADEQUATE Q C TXTAXI/GRND HDL 1 EA03228Y 5342 FUEL DOOR AND CAP WERE NOT SECURED PRIOR TO FLIGHT. UPON TAKE OFF, CREW HEARD A BANGING FROM ACFT AND RETURNED TO POINT OF ORIGIN. INSPECTED AND FERRIED ACFT FOR REPAIRS. REMOVED AND REPLACED RT INBD LEADING EDGE AND POLISHED OUT FUSELAGE PANEL. 2L72 4F RTA22CE 20081201 NM 2008 12 1 USAA920082039 120081022A532065C46812169 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT Q5 MAJOR REPAIR NR 03C10853028/030 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS967 TO BS986,5, RBL17. REPLACED INTERCOSTAL AT BS967 TO BS986.5, RBL17 IAW B737 SRM 51-10-02. 2L72 4F RTA16WE 20081201 WP 2008 12 1 NWAA084969969 120081107A3350 LIGHT DOUG DC9 DC931 3022065WP CABIN INOPERATIVE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL019333 47246 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 8-10 AND THE LT OVERWING EMERGENCY EXIT SIGN WERE INOPERATIVE. 2L72 4F A6WE 20081202 NM 2008 12 2 USAA2008112592123120081123A53306552988 SKIN BOEING737 7374B7 138449CNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - C1 - MAJOR REPAIR - FUSELAGE SKIN CRACKED AT AFT RIGHT SERVICE DOOR LOWER DOOR HINGE CUTOUT AT BS 951 BELOW S14R. REPAIRED FUSELAGE SKIN AT AFT RIGHT SERVICE DOOR LOWER DOOR HINGE CUTOUT AT BS 951 BELOW S14R IAW B737 SRM 53-60-01 REPAIR 7. 2L72 4F RTA16WE 20081202 NM 2008 12 2 USAA2008112692128120081125A2560P4010021 BATTERY AIRBUSA319 A319132 3930340NM FLASHLIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19805AW 1049 FLT 160 - PHX-LAS - EEL - AFT RECHARGEABLE EMERGENCY FLASHLIGHT HAS DEAD BATTERY. REMOVED AND REPLACED EMERGENCY FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20081202 NM 2008 12 2 KCSA081602 120081126A5312 PRESSURE BLKHD BOEING747 747212B 1384886NM ZONE 100 CORRODED A KCSAK NONE O OTHER ININSP/MAINT 1 GL23708CK 21937 CORROSION ON PRESSURE DECK AFT T-CHORD AT BS 1480, WL187, RBL5 TO LBL30. 2L74 4F RTA20WE 20081202 NM 2008 12 2 DXTA2008112403367120081122A3150 WARNING LIGHT GULSTM200 200 4500308NM MULTIPLE FAIL E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07739QS 198 IMMEDIATELY AFTER TAKEOFF POWER SET WE GOT THE RED DITCH LIGHT THE YELLOW AUTO PRESS FAULT LIGHT AND THE FOLLOWING EICAS MESSAGES CABIN ALT HIGH AUTO PRESSURE. 2L72 4F RTA53NM 20081202 EU 2008 12 2 USAA2008112892146120081113A5320D53480043207 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL AT R2 DOOR, FR66, -Y1732. REPAIRED LOWER SILL AT R2 DOOR, FR66, -Y1732 IAW A320 SRM 53-41-14. 2L72 4F RTA28NM 20081202 NM 2008 12 2 USAA2008112892156120081112A5320143N80216 INTERCOSTAL BOEING757 7572S7 1384962NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 WP28904AW 23566 MCN - C12 - MAJOR REPAIR - INTERCOSTAL WEB CRACKED AT BS 550, RBL 54.5. REPAIRED INTERCOSTAL WEB AT BS 550, RBL 54.5 IAW B757 SRM 51-70-10-0G. 2L72 4F RTA2NM 20081202 NM 2008 12 2 YENA200811240119 120081123A27825914054 PDU EMB ERJ190ERJ190100IGW3260408NM LE SLAT FAILED A YENAO OTHER F FLT CONT AFFECTED APAPPROACH 1 EA15247JB1188 190000042 ORD-JFK, SLAT FAIL ON APPROACH TO LANDING, QRH ITEMS COMPLETED. AFTER EMBRAER ANALYZED THE FHDB FOR SLAT FAIL EVENT (REPEAT ITEM) IT WAS DETERMINED THAT THE SLAT SURFACES JAMMED IN FLIGHT DURING APPROACH. FIM TASK 27-81-00-810-802-A. PERFORMED FIM TASK 27-83-00-810-804-A. REPLACED NR 1 SLAT LT ELECTRIC PDU MOTOR. REF AMM 27-83-04. ALSO C/W FIM TASK 27-81-00-810-802-A. OPS CHECK OK. 2L72 4F RTA57NM 20081202 2008 12 2 UALA2008112106605420081119A2565660431 CYLINDER BOEING777 777222 1385219NM PWA PW4077PW4077 NE EVAC SLIDE LOW PRESSURE A UALAO OTHER W INADEQUATE Q C ININSP/MAINT 1 WP29772UA 0113 26930 INFLATION CYLINDER OUT OF GREEN BAND. IMPROPER CYLINDER FILL. TOP OFF CYLINDER. 2L72 4F4 FRTT0001SE E46NE 20081202 NM 2008 12 2 UALA2008111305431120080823A3350363674 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29654UA 25392 ROW 1 LT EEL STRIP INOP. REPLACED LUMINESCENT STRIP. OPS OK. 2L72 4F4 FRTA1NM E24NE 20081202 NM 2008 12 2 UALA2008111305438120080823A3350363674 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29654UA 25392 ROW 5 LT EEL STRIP INOP. FOUND LIGHTS INOP. REPLACED STRIP. OP CHECKS OKAY. 2L72 4F4 FRTA1NM E24NE 20081202 NM 2008 12 2 UALA2008111306324120081030A5220 CABLE BOEING757 757222 1384956NM PWA 2037 PW2037 NE RT ESCAPE HATCH FAULTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29550UA 25398 RT OVERWING ESCAPE HATCH(S) OFFWING MANUAL BACKUP CABLE CHECK FAILED. REPLACED RT OVERWING EXIT PRESSURE BOTTLE MANUAL BACKUP CABLE AND ADJUSTED. 2L72 4F4 FRTA2NM E17NE 20081202 EA 2008 12 2 ASOA200801511 120081115A5320 FLOOR SUPPORT CNDAIRCL600 CL6002C10 1390015EA BS 280 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27713EV 10081 CORROSION DAMAGE ON NUT PLATE SUPPORT ANGLE ATTACHED TO AFT SIDE OF FS 280.00 IN A/E/B (MARKED). REMOVED CORRODED NUT PLATE SUPPORT ANGLE FROM AFT SIDE OF F.S. 280.00 IN A/E/B CORRION ON RADIUS OF ANGLE, ANGLE FOUND TO BE NO GOOD. ALL WORK DONE IAW 51-42-06. PICKED UP EXISTING FASTENER HOLES AND INSTALLED ANGLE FOR FLOORBOARD IN AVIONICS BAY AFT OF FS 280 PER SRM 51-42-06. 2L72 4F RTA21EA 20081203 WP 2008 12 3 AALA200810216 120081105A5320 CUSP WEB DOUG DC9 DC982 3022082WP ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 CORROSION ON RIGHT CUSP AT STATION 1281 TO 1309. REMOVED AND REPLACED CUSP FROM STATION 1250 TO 1309 RIGHT SIDE PER AARD 53-20-00-16. 2L72 4F A6WE 20081203 NM 2008 12 3 AALA200810237 120081120A5343 TRUNNION BOEING737 737800* NM RT MLG CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21948AN 30086 RIGHT MAIN GEAR FORWARD TRUNNION INBOARD LUG FACE HAS CORROSION THAT MEASURES .107 IN DEPTH. REPAIRED PER SRM 57-20-2R-2. 2L72 4F RTA16WE 20081203 NM 2008 12 3 AALA200820044 120081103A5347141N51301 SEAT TRACK BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21604AA43723 27055 LT OUTBOARD SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW SRM 51-10-02. 2L72 4F RTA2NM 20081203 WP 2008 12 3 AALA200810200 120081110A5313 STRINGER DOUG DC9 DC982 3022082WP ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 LONGERON 29 LEFT CORRODED FROM STATION 484 TO 494. INSTALLED LONGERON REPAIR PER ESO 80559 DATED 11/04/2008. 2L72 4F A6WE 20081203 WP 2008 12 3 AALA200802734 120081014A3350 LAMP DOUG DC9 DC982 3022082WP EMERGENCY LIGHT BURNED OUT A AALAK NONE L NO TEST ININSP/MAINT 1 SW21561AA 53091 LGA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23D INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 23D. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20081203 CE 2008 12 3 BSY2008F00011 120080911A3411 PITOT SYSTEM CESSNA208 208B 2073701CE CONTAMINATED E BSYAO OTHER O OTHER TOTAKEOFF 1 GL073RY 208B0436 ON TAKEOFF, PILOTS ALTIMETER AND VSI WERE FLUCTUATING. MAINT FOUND WATER IN PITOT/STATIC SYSTEMS. (K) 1H71 3T A37CE 20081203 SO 2008 12 3 FDKA2008111600297120081116A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A FDKAK NONE O OTHER NRNOT REPORTED 1 SW07840MJ 145429 FRL FLT 6268 JFK-IAD - EMERGENCY LIGHTS INOP. MX REPLACED EMERGENCY BATTERY PACKS 2 AND 3. OPS CHECK GOOD. 2L72 4T RTT00011AT 20081203 SO 2008 12 3 FDKA200811298 120081119A3350 LIGHT EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A FDKAK NONE O OTHER NRNOT REPORTED 1 SW07833MJ 145327 FRL FLT 6265 JFK-RIC - AFT MOST FLOOR ESCAPE PATH LIGHTS INOPERATIVE. MX REMOVED AND REPLACED FLOOR STRIP, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20081203 SO 2008 12 3 FDKA2008111200293120081112A3397 CONNECTOR EMB 145 EMB145LR 3260212SO CABIN LOOSE A FDKAK NONE O OTHER NRNOT REPORTED 1 SW07827MJ 145217 FRL FLT 8910 JFK - LT EMERGENCY EXIT OVERWING DOOR EXIT SIGN OUT. MX RESECURED LOOSE CONNECTOR, OPS GOOD. 2L72 4T RTT00011AT 20081203 SO 2008 12 3 FDKA2008112300299120081123A5241 DOOR EMB 145 EMB145LR 3260212SO GALLEY DOOR LACK OF LUBE A FDKAK NONE O OTHER NRNOT REPORTED 1 SW07860MJ 145773 FRL FLT 6283 CVG-DAY - GALLEY DOOR DIFFICULT TO CLOSE. MX CLEANED AND LUBED DOOR, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20081203 NM 2008 12 3 UALA2008112406626120081122A2797 CONNECTOR BOEING757 757222 1384956NM PWA 2037 PW2037 NE T/E BYPASS VALVEMISINSTALLED A UALAO OTHER O OTHER ININSP/MAINT 1 WP29546UA 25367 CONNECTOR ON T/E BYPASS VALVE V105 ALSO HAS INSULATOR DAMAGE FROM CONNECTOR NOT BEING INSTALLED PROPERLY. REPLACED VALVE ASSY. ALSO FOUND T/E FLAP BYPASS VALVE CONNECTOR D1716 NOT CONNECTED AT LT WHEEL WELL WHILE DOING OPS TEST FOR FLAP AND SLAT ALTERNATE DRIVE SYS ON A-11 CHECK. ALSO CONNECTOR D1716 HAS CRACKS IN INTERNAL SHIELDED AREA. REPLACED CONNECTOR D1716. 2L72 4F4 FRTA2NM E17NE 20081203 NM 2008 12 3 HNAA2008102900321120081017A32338300101 ACTUATOR DHAV DHC8 DHC8102 2809003NM NLG BYPASSING A HNAAL ABORTED APPROACH J WARNING INDICATION LDLANDING 1 EA07815EX41157 321 FLIGHT 4165 LGA TO ROA. THE GEAR WAS SELECTED DOWN ON APPROACH. THE MAIN GEAR INDICATION WAS NORMAL AND THE NOSE GEAR INDICATION WAS RED. THE ALTERNATE INDICATION WAS NOT INDICATING AND THE APPROACH WAS MISSED. THE GEAR WAS THEN CYCLED FOR A SECOND TIME AND ALL INDICATIONS WERE NORMAL. ALL THREE GEAR DOWN AND LOCKED INDICATED WERE ILLUMINATED BY THREE GREEN LIGHTS. THE PLANE LANDED WITHOUT INCIDENT. IN ROA THE NOSE GEAR WAS SWUNG. IT WAS REPORTED THAT THE NOSE GEAR WAS SLOW AND THE DOORS WOULD STUTTER WHEN OPENING. FLUID COULD ALSO BE HEARD BYPASSING IN THE GEAR WELL. THE NOSE RETRACTION ACTUATOR WAS REMOVED AND REPLACED IN ACCORDANCE WITH MM 32-30-31. THE GEAR WAS AGAIN CYCLED AND THE OPERATIONAL CH2H72 4T RTA13NM 20081203 NM 2008 12 3 HNAA2008102900320120081029A532085310346S104A DOUBLER DHAV DHC8 DHC8102 2809003NM NLG WW CRACKED A HNAAL ABORTED APPROACH J WARNING INDICATION APAPPROACH 1 EA07815EX21233 321 UPON GEAR EXTENSION DURING FINAL APPROACH TO RUNWAY 35, NOSE GEAR RED UNSAFE LIGHT INDICATION ILLUMINATED. BOTH MAIN GEARS LOCKED AND ILLUMINATED GREEN INDICATIONS. CREW DISCONTINUED APPROACH AND PERFORMED ALTERNATE GEAR EXTENSION PROCEDURED. GEAR WAS NOT CYCLED PRIOR TO PERFORMING THE ALTERNATE GEAR EXTENSION. THE FLIGHT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. OUT OF SERVICE. THE AIRCRAFT WILL MTC FERRY TO SBY FOR FURTHER INSPECTION. UPON INSPECTION AT SBY AIRCRAFT DAMAGE RECORDING DESCRIPTION: LT SIDEWALL AT J-BEAM DOUBLER CRACKED. LOCATION: X97.00 AND Z110.00 APPROX. DIMENSIONS: WIDTH-N/A, LENGHT-3.5IN, DEPTH-N/A. DISTANCE FROM FASTENER 1.0IN, STRINGER 1.0IN, FRAME 1.0IN. TYPE OF NDT PERFORMED:2H72 4T RTA13NM 20081203 2008 12 3 JRA2008F00000 120081114A2710240723006513 SPRING ASSY CVAC STC STC440 CONTROL CABLES STRETCHED A JRAAO OTHER F FLT CONT AFFECTED TXTAXI/GRND HDL 1 GL11587CA 463 AILERON CONTROL CABLES BINDING TO THE RIGHT FROM FULL LEFT POSITION. INSPECTION OF AILERON CONTROL CABLES REVEALED STRETCHED SPRING AT RUDDER INTERCONNECT. REMOVED AND REPLACED SPRING IAW 440 MM, SEC 8-2, PAGE 26. OPS CHECK OK. (K) 2L72 4R T 6A6 20081203 SO 2008 12 3 BSY2008F00002 120080926A3600CS11C6231951 CLAMP PIPER PA31 PA31350 7103110SO LYC O540 LTIO540J2BD 41533EA INTERCOOLER FAILED E BSYAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL073587P 318052120 L63668A AFTER TAKEOFF AT 4,000 FT RT ENGINE FAILED AND ACFT RETURNED WITH NO PROBLEMS. MAINT FOUND INDUCTION TUBE CAME OFF INTER-COOLER REDUCING MANIFOLD PRESSURE TO A NORMALLY ASPIRATED ENGINE. REPLACED WITH NEW DUCT AND CLAMP. (K) 1L72 3O3 O A20SO E14EA 20081203 NM 2008 12 3 DXTA2008120203382120081201A2780 SLAT SYSTEM GULSTM200 200 4500308NM MALFUNCTIONED E DXTAA UNSCHED LANDING F FLT CONT AFFECTED CLCLIMB 1 GL07705QS 061 FOLLOWING A NORMAL TAKEOFF, SLATS WERE RETRACTED. KRUGERS INDICATED UNBALANCED, IN AMBER. 2L72 4F RTA53NM 20081203 CE 2008 12 3 BSY2008F00013 120080926A772110200007 PROBE BEECH 58 58 1152740CE CHT MALFUNCTIONED E BSYAO OTHER N FALSE WARNING NRNOT REPORTED 1 GL0762500 TH1347 LT CYLINDER HEAD TEMP, WENT ABOVE RED LINE ON TAKEOFF, PILOT THEN RETURNED TO DEPARTURE. REMOVED AND REPLACE CHT PROBE. (K) 1L72 3O 3A16 20081203 NM 2008 12 3 DXTA2008120103374120081126A3150 WARNING LIGHT GULSTM200 200 4500308NM ILLUMINATED E DXTAC ABORTED TAKEOFF N FALSE WARNING TOTAKEOFF 1 GL07738QS 204 FLIGHT AIR BRAKE DEPLOYED ANNUCIATOR ILLUMINATED DURING TAKEOFF ROLL CAUSING A TAKE OFF UNSAFE EICAS MESSAGE. THE TAKE OFF WAS ABORTED. 2L72 4F RTA53NM 20081203 NE 2008 12 3 HNAA2008120200327220081121A73103036432 FILTER ELEMENT DHAV DHC8 DHC8311 1386006EA PWA PW120 PW123 NE NR 2 ENGINE CLOGGED A HNAAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA07333EN 221 ON TAKEOFF ROLL NR 2 FUEL FILTER BYPASS CAUTION LIGHT ILLUMINATED. ABORTED TAKEOFF. REMOVED, INSPECTED & REPLACED HP & LP FUEL FILTER REF (WORK) CARD 73-10-02R AND 73-10-04R AND MAINT MANUAL 72-00-01 AND REPLACED HP FILTER BYPASS SWITCH REF P&W MAINT, RUNUP CHECKS GOOD. 2H72 4T4 TRTA13NM E20NE 20081203 SO 2008 12 3 RAIA20081200003 120081130A3350 LIGHT EMB 145 EMB145EP 3260221SO CABIN LOOSE A RAIAK NONE O OTHER TXTAXI/GRND HDL 1 CE03803HK 145077 DURING PRE FLIGHT INSPECTION, EMERGENCY LIGHT AT SEAT 12A WAS FOUND TO BE LOOSE. MAINTENANCE RESECURED THE LOOSE LIGHT ASSEMBLY. 2L72 4F RTT00011AT 20081203 SO 2008 12 3 RAIA2008120100004120081130A2150 A/C PACK EMB 145 EMB145EP 3260221SO NR 1 MALFUNCTIONED A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03804HK 145082 DURING CLIMB, CREW RECEIVED A NR 1 PACK OVERLOAD MESSAGE ON THE EICAS. MAINTENANCE DEFERRED THE NR 1 PACK PER MEL INSTRUCTIONS. 2L72 4F RTT00011AT 20081203 NM 2008 12 3 HNAA2008111800331120081118A6120V319 BETA SWITCH DHAV DHC8 DHC8102 2809003NM NR 2 BROKEN A HNAAA UNSCHED LANDING R PARTIAL RPM/PWR LOSS TOTAKEOFF 1 EA07911HA5851358513 034 DURING TAKEOFF AND AFTER GEAR RETRACTION, THE NR 2 ENGINE STARTED TO SURGE BETWEEN 60 TO 100 PERCENT TORQUE. AFTER TURNING BACK TO FIELD, THE CONDITION CLEARED. MAINTENANCE CLEANED AND RESEATED THE ECU CONNECTOR, GROUND RAN AIRCRAFT AND NOTED NO DEFECTS. AIRCRAFT WAS THEN RELEASED FOR SERVICE AND DURING TAKEOFF AND GEAR RETRACTION, AGAIN THE NR 2 ENGINE TORQUE SURGED BETWEEN 40 AND 100 PERCENT. AFTER RPM REDUCTION, THE CONDITION CLEARED. DURING TROUBLESHOOTING BY MAINTENANCE, THE NR 2 ENGINE BETA BACKUP SWITCH (6141-S4) WAS FOUND TO BE BROKEN. THE SWITCH WAS CHANGED OUT AND THE AIRCRAFT WAS GROUND RUN AND OPS CHECKED GOOD PENDING AN EVALUATION FLIGHT. THE AIRCRAFT FLEW SATISFACTORILY AND WAS THEN RELEASE2H72 4T RTA13NM 20081201 NM 2008 12 1 USAA920082031 120081105A5320507945178 PAN BOEING737 737301 1384611NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT Q3 MAJOR REPAIR NR 03C10552010/012 BOTTOM DOOR PAN BEAM HAS 2 CRACKS, 1 INCH AND 1.5 INCHES AT FORWARD LOWER DOOR STOP AT FORWARD ENTRY DOOR. REPAIRED BOTTOM DOOR PAN BEAM AT FORWARD LOWER DOOR STOP AT FORWARD ENTRY DOOR IAW BOEING DRAWING NR 50-7945 AND B737 SRM 51-10-02. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA920082029 120081105A5210507945178 SKIN BOEING737 737301 1384611NM PAX DOOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT Q3 MAJOR REPAIR NR 03C10552010/007 INTERIOR SKIN CRACKED AT NR 6 STOP PIN CUTOUTS AT FORWARD ENTRY DOOR. REPAIRED INTERIOR SKIN CRACKED AT NR 6 STOP PIN CUTOUTS AT FORWARD ENTRY DOOR IAW US AIRWAYS TYPICAL REPAIR NR 52-10-16. 2L72 4F RTA16WE 20081201 EA 2008 12 1 COMA0860461 120081112A2131 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA CABIN PRESSURE MALFUNCTIONED A COMAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO27938CA 7046 RECEIVED CABIN ALTITUDE WARNING AT 11,500 FT. RETURNED TO BWI, LANDED WITHOUT INCIDENT. PERFORMED OPS TEST OF CABIN PRESSURE CONTROLLER NR 1 AND NR 2 IAW CRJ AMM. NO DEFECTS NOTED. 2L72 4F RTA21EA 20081201 NM 2008 12 1 ASAA0843878 120081029A532065C323946 BEAM BOEING737 7374Q8 138447QNM FUSELAGE CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02760AS 25098 MAIN CABIN STUB BEAM CRACKED RT STA 601 RBL 65. TRIMMED OUT CRACKED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND STIFFENING ANGLE IAW ASA EA 400 53EA 00269. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086624 120081125A533065457665 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND SKIN CRACKED AT BS 500D, BETWEEN STR 12R TO STR 18R. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086604 120081125A532269353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086566 120081124A52106545768 SKIN BOEING737 7373H4 1384600NM L1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29342SW 24133 DURING SCHEDULED 20Y CHECK, FOUND L1 DOOR SKN CRACKED AT BS 305, WL 236. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20081201 NM 2008 12 1 QXEA2008112601199120081121A3397 CONNECTOR BOMBDRDHC8 DHC8402 1390042NM EMERGENCY LIGHTSDISCONNECTED A QXEAK NONE O OTHER ININSP/MAINT 1 NM19400QX 4030 RDM - EMERGENCY EXIT LIGHT AFT REAR SERVICE DOOR INOP. PARTIALLY REMOVED SURROUND TO RT REAR SERVICE DOOR. FOUND CONNECTOR TO EMERGENCY EXIT LIGHT (LOWER) UNPLUGGED. CONNECTED CONNECTOR AND RE-INSTALLED RT REAR SERVICE DOOR SURROUND. OPS CHECK GOOD. RETURNED TO SERVICE. NO PARTS REPLACED. 2H72 4T RTA13NM 20081201 NM 2008 12 1 QXEA2008112601201120081122A33506138001 POWER SUPPLY BOMBDRDHC8 DHC8402 1390042NM EMERGENCY LIGHTSMALFUNCTIONED A QXEAO OTHER O OTHER NRNOT REPORTED 1 NM19400QX1193 802 4030 PDX - EMERGENCY EXIT SIGN LOWER AFT PAX DOOR INOP. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AT WS X692.22, PANEL 245EZ IAW AMM TASKS 33-51-01-000-801, 33-51-01-400-801. OPS CHECK GOOD. NO DEFECTS NOTED. RETURNED TO SERVICE. 2H72 4T RTA13NM 20081201 NM 2008 12 1 SWAA086610 120081125A532269353656 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29359SW 26596 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 14R TO STR 15R. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086616 120081125A5313BAC1498 STRINGER BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29364SW 26575 DURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 362, STR 4R. REPAIRED STRINGER PER SRM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086617 120081125A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29366SW 26577 DURING SCHEDULED 16Y CHECK, FOUND SKIN CORRODED AT BS 515, BETWEEN LBL 2 TO RBL 2. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086583 120081124A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND FUSELAGE SKIN CORRODED AT BETWEEN BS 506D TO 512D, STR 28L. REPAIRED SKIN PER ER. 2L72 4F RTA16WE 20081201 SO 2008 12 1 SWIA200820479 120081121A5210 MECHANISM EMB 120 EMB120ER 3260203SO PAX DOOR LACK OF LUBE A SWIAK NONE O OTHER ININSP/MAINT 1 NM07298SW 120328 FLT 5710 - PASSENGER DOOR DIFFICULT TO OPEN. CLEANED AND LUBE LOCKING MECHANISM. 2L72 4T RTA31SO 20081201 SO 2008 12 1 SWIA200820470 120081107A32331959500007 ACTUATOR EMB 120 EMB120ER 3260203SO MLG FAULTY A SWIAO OTHER O OTHER NRNOT REPORTED 1 NM07584SW1859218592 120352 FLT 5711 - RIGHT MAIN GEAR WOULD NOT RETRACT. REPLACED RIGHT MAIN GEAR ACTUATOR, P/N 1959-000-07, S/N ON 685, S/N OFF: B118. 2L72 4T RTA31SO 20081201 WP 2008 12 1 AALA208810181 120081115A5330 SKIN DOUG DC9 DC982 3022082WP ZONE 200 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW217537A 49991 2 CRACKS IN SKIN AT STATION 1380 RT BETWEEN LONGERON 13R AND 14R. INSTALLED DOUBLER PER SRM 53-01-00. 2L72 4F A6WE 20081201 WP 2008 12 1 AALA200810184 120081121A5320 STRUCTURE DOUG DC9 DC983 3022083WP ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21594AA 53284 CORROSION ON LOWER SIDE OF CABIN SUBFLOOR BELOW G1 GALLEY. INSTALLED REPAIR PER AARD 53-20-00-16. 2L72 4F RTA6WE 20081201 NM 2008 12 1 AALA200820032 120081027A5320 STRUCTURE BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21640A 56247 24597 AFT GUTTER BOX CORRODED. REPAIRED IAW SRM 51-40-02. 2L72 4F RTA2NM 20081201 WP 2008 12 1 AALA200810197 120081112A3350 BATTERY PACK DOUG DC9 DC982 3022082WP EMERGENCY LIGHT WEAK A AALAK NONE O OTHER ININSP/MAINT 1 SW21584AA 53247 EMERGENCY LIGHT BATTERY PACK WEAK AT STATION 160L. INSTALLED NEW BATTERY PACK. 2L72 4F A6WE 20081201 EA 2008 12 1 SWIA200820457 120080810A5420 RISER CNDAIRCL600 CL6002B19 1900309EA NACELLE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07959SW 7840 C-CHECK, FRETTING CORROSION AT RIGHT PRODUCTION RISER. REPAIRED PER REO. 2L72 4F RTA21EA 20081201 NM 2008 12 1 ASAA0893881 120081104A5320147A571235 SHEAR WEB BOEING737 737990 NM FUSELAGE CORRODED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02320AS 33680 CORROSION ON SHEAR WEB BS 986.5 RBL 30 WL 208. REMOVED CORROSION, PERFORMED NDI TO ENSURE NO CRACKS. ALODINED AND PRIMED. NO ESTABLISHED SRM LIMITS REPAIR WAS DONE PER EA 900 53EA 00246. 2L74 4F RTA16WE 20081201 NM 2008 12 1 SWAA086595 120081125A335065C27095 BATTERY PACK BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29499WN 32481 DURING SCHEDULED HC2 CHECK, RT EMERGENCY BATTERY PACK FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086584 120081124A53226546546 SHEAR TIE BOEING737 7373H4 1384600NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29306SW 22946 DURING SCHEDULED 24Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727C BETWEEN STR 26L TO STR 27L. REPAIRED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 DL757081623 120081115A5320146N539148 SUPPORT BOEING757 757232 1384965NM BS 1530 CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27651DL 24391 2 CORROSION ON INBD LOWER FLANGE OF FLOOR TO SIDEWALL SUPPORT COMMON TO LOCK FASTENER, BS 1530, LBL 16.5 OUT OF LIMITS. REPAIRED PER DELTA ER/A 471507-14 REV ORIGINAL. 2L72 4F RTA2NM 20081201 CE 2008 12 1 GUUA10100801 120081010A52601294000321 DOOR BEECH 1900 1900D 1154162CE AIRSTAIR STIFF A GUUAO OTHER O OTHER NRNOT REPORTED 1 SO2981556 UE239 PILOT REPORTED CABIN DOOR HARD TO CLOSE. CLEANED AND LUBRICATED AIRSTAIR DOOR LOCKING CAMS AND ADJUSTED DOOR SUPPORT CABLES. OPS CHECK GOOD. 2L72 4T RTA24CE 20081201 NM 2008 12 1 ASAA0893850 120081122A5320146A7510 INTERCOSTAL BOEING737 737990 NM BS 500K-500L CRACKED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02320AS 33680 BAFFLE INTERCOSTAL CRACKED AT STA 500K 500L LT 26 WL 154. REMOVED FABRICATED NEW AND INSTALLED INTERCOSTAL. 2L74 4F RTA16WE 20081201 NM 2008 12 1 USAASB08113 120081118A27512061141 INDICATOR BOEING737 7374B7 138449CNM COCKPIT DEFECTIVE A USAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA19432US359342842 24554 DCA - FLT 1282 EN ROUTE PBI TO DCA. DURING PREPARATION FOR LANDING, THE TRAILING EDGE FLAPS ONLY DEPLOYED TO TWO DEGREES AND INDICATED UNEVENLY SPLIT. THE CREW EXECUTED A MISSED APPROACH. THE CREW RECYCLED THE FLAPS AND MADE A SECOND APPROACH. THE FLAPS DEPLOYED NORMALLY AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FLAP POSITION INDICATOR. OPERATIONALLY CHECKS OK. 2L72 4F RTA16WE 20081201 2008 12 1 USAASB08111 420081116A2565D31591479 SLIDE BOEING737 737401 138449BNM PAX DOOR LOW PRESSURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US469732626 23885 MCO - THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE PRESSURE WAS FOUND LOW. MAINTENANCE REPLACED THE FORWARD ENTRY DOOR EMERGENCY ESCAPE SLIDE. OK FOR SERVICE. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAASB08112 120081117A2150 UNKNOWN BOEING737 7374B7 138449CNM A/C PACK ODOR A USAAK NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA19430US 24552 FLT 1868. ON TAKEOFF & LANDING, CREW NOTICED AN ODOR COMING FROM A/C PACKS. MX PLACED ACFT ON MEL. ODOR DISSIPATED DURING CLIMB. CLT MX PLACED LT PACK ON MEL 21-01A. WHILE ON MEL, ANOTHER REPORT OF ODOR COMING FROM A/C PACKS DURING HIGH POWER ON TAKEOFF OCCURRED ON 11/21/08, FLIGHT 1159. ODOR AGAIN DISSIPATED DURING CLIMB. MX INSPECTED LT & RT RAM AIR INLETS, LT & RT ENGINE INLETS & AIR MIX CHAMBER. ALL CHECK OK. RAN ENGINES ONE AT A TIME WITH EACH PACK FOR FIVE MINUTES EACH. REACTIVATED LT PACK & ACCOMPLISHED ADJUSTMENT TEST PER MM 21-61-00-5. TESTED NORMAL. CLEARED MEL 21-01A. NO FURTHER ODORS NOTED AS CONFIRMED WITH FLT CREW & MX. ACFT OK FOR SERVICE. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA SB08112 120081117A2120 UNKNOWN BOEING737 737400 138449ANM CABIN ODOR A USAAK NONE B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA19430US 24552 FLIGHT 1868, PBI-CLT - ON TAKEOFF AND LANDING THE CREW REPORTED A SOUR ODOR COMING FORM THE AIR CONDITIONING PACKS. THE ODOR DISSIPATED IN CLIMB. MAINTENANCE INSPECTED THE LEFT AND RIGHT RAM INLET, THE LEFT AND RIGHT ENGINE INLETS AND AIR MIX CHAMBER. ALL CHECK OKAY. MAINTENANCE RAN THE ENGINES ONE AT A TIME WITH EACH SIDE PACK FOR FIVE MINUTES EACH. NO FURTHER ODORS NOTED. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA SB08113 120081118A27512061141 INDICATOR BOEING737 737400 138449ANM COCKPIT FAULTY A USAAL ABORTED APPROACH F FLT CONT AFFECTED LDLANDING 1 EA19432US3593433092 24554 FLIGHT 1282, PBI-DCA - DURING PREPARATION TO LAND IN DCA THE FLAPS STOPPED AT 2 DEGREES WITH ASSEMBLY INDICATION. THE CREW EXECUTED A MISSED APPROACH AND DID A GO AROUND. THE CREW RECYCLED THE FLAPS AND AFTER APPROXIMATELY THREE MINUTES THE FLAPS EXTENDED NORMALLY AND THE INDICATION WENT AWAY. THE FLIGHT LANDED UNEVENTFULLY. MAINTENANCE REMOVED AND REPLACED THE FLAP POSITION INDICATOR. 2L72 4F RTA16WE 20081201 EU 2008 12 1 USAA2008112092095120081112A5347D53371112005 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C07 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR41 & FR47, -Y1292. REPAIRED SEAT TRACK BETWEEN FR41 & FR47, -Y1292 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20081201 NM 2008 12 1 USAA920082036 120081022A53206545834259 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/014 LEVEL 2 GALVANIC CORROSION ON INTERCOSTAL BS328 TO BS344, LBL11. REPLACED INTERCOSTAL BS328 TO BS344, LBL11 IAW B737 SRM 51-10-02. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA920082037 120081019A53206562175133 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT Q3 MAJOR REPAIR NR 03C10753005/011 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL BS294 TO BS312, RBL11. REPLACED INTERCOSTAL BS294 TO BS312, RBL11 IAW B737 SRM 51-10-02. 2L72 4F RTA16WE 20081201 EU 2008 12 1 USAA920082057 120081112A3350 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN MALFUNCTIONED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19649AW 803 LOG PAGE 4458139 FLT NR 157 STL-PHX EEL EMERGENCY LIGHT OPS TEST FAILED (EPSU INT LOAD EMER L). MX RESET THE POWER SUPPLY AT CABIN LT. OPS CHECK GOOD. 2L72 4F RTA28NM 20081201 NM 2008 12 1 NWAA084936309 120081004A3350 POWER SUPPLY BOEING747 747451 1384940NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01669US 24224 DURING OVERNIGHT CHECK FOUND EMERGENCY LIGHTS AT ZONE B RT INOP. MX R&R POWER SUPPLY. OPS CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. 2L74 4F RTA20WE 20081202 NM 2008 12 2 USAA2008112492121120081120A5753654648198 SPINDLE BOEING737 737401 138449BNM TE FLAP CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19422US 23989 PHL - RON - MAJOR REPAIR - CORROSION ON RIGHT WING OUTBOARD MID FLAP CARRIAGE SPINDLE. REPLACED RIGHT WING OUTBOARD FLAP ASSEMBLY IAW US AIRWAYS TASK CARD 03C40727020. 2L72 4F RTA16WE 20081202 EU 2008 12 2 USAA2008112592122120081124A3350321454 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN NO TEST A USAAK NONE L NO TEST ININSP/MAINT 1 EA19603AW3749616334 661 FLT 383 CLT-LAS - EEL - FORWARD LEFT EMERGENCY CABIN POWER SUPPLY UNIT WILL NOT TEST. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT EMERGENCY CABIN POWER SUPPLY UNIT AND BATTERY. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20081202 NM 2008 12 2 USAA2008112492113120081123A5320 STRUCTURE BOEING767 7672B7ER 1385107NM NLG WW CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19255AY 25257 BFM - C3 - MAJOR REPAIR - CRACK ON VERTICAL CHORD ON NOSE WHEEL WELL AT BS 287, RBL 25, WL 173.5. REPAIRED VERTICAL CHORD ON NOSE WHEEL WELL AT BS 287, RBL 25, WL 173.5 IAW B767 SRM 51-70-12. 2L72 4F RTA1NM 20081202 NM 2008 12 2 USAA2008112492108120081123A3350 POWER SUPPLY AIRBUSA319 A319132 3930340NM CABIN MALFUNCTIONED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19828AW 1552 FLT 341 - MZT-PHX - EEL - CIDS EMERGENCY LIGHT OPERATIONAL TEST FAILS EMERGENCY POWER SUPPLY UNIT INITIAL LOAD ON FORWARD LEFT. RESET EMERGENCY POWER SUPPLY UNIT FORWARD LEFT AND RIGHT. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20081202 SO 2008 12 2 SIMA200832203 120081115A2120 UNKNOWN EMB 135 EMB135KL 3260302SO CABIN ODOR A SIMAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW21806AE 145503 ON FLIGHT 3055, CREW REPORTED SMOKE DETECTED IN CABIN AND COCKPIT 30 SECONDS AFTER TAKEOFF. SMOKE WAS NOT VISIBLE. SMELLED LIKE PAPER, BREAD TOAST, AND RUBBER. AFTER ONE MINUTE WITH BOTH PACKS TURNED OFF WAS UNABLE TO RESET THEM. CREW DECLARED A EMERGENCY AND LANDED UNEVENTFULLY. FLIGHT ATTENDANT REPORTED ODOR CONTINUED UNTIL JUST PRIOR TO LANDING THEN DISSIPATED. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED ENVIRONMENTAL SLEEVE AT CONTROL UNIT IAW MM 21-51-02. OPERATION CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTT00011AT 20081202 SO 2008 12 2 DJFA2008084 120081125A2120 UNKNOWN EMB 135 EMB135BJ 3260306SO CABIN SMOKE E DJFAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA23910LX 14500952 IMMEDIATELY AFTER DEPARTURE CREW NOTED THE CABIN FILLING WITH SMOKE. MAINT IS EVALUATING. 2L72 4F RT 20081202 SO 2008 12 2 Y9PA663P112508 120081125A2910 HYDRAULIC SYSTEM GULSTMG1159 GIV 3980115SO RROYCETAY TAY6118 EU ZONE 100 LOW PRESSURE E Y9PAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW09663P 3868 1434 1600316369 ENROUTE, THE CREW DECLARED AN EMERGENCY AND LANDED. THE REPORT IS BOTH HYDR SYS QUANTITY WAS INDICATING LOW, LOCATED A LOCAL TECH IAW AIR CARRIER MM SECTION 3.02. CHECKED THE QUANTITY IN THE HYDR RESERVOIRS AND VERIFIED THAT THEY WHERE LOW, SERVICED IAW COMPUTERIZED MAINT PROGRAM (CMP) 291057. ACFT CONTINUED AFTER SERVICING TO FINAL DESTINATION. 2L72 4F4 FRTA12EA E25NE 20081202 2008 12 2 ESPADJ2008-2 220081117A7597 WIRE LEAR 35 35A 5170602CE BLEED SWITCH BROKEN E ESPAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 SO11568PA 205 ON LIFT OFF, CREW NOTED FUMES AND SMOKE IN ACFT, AND THE ACFT PRESSURIZATION SYS WAS IN EMERGENCY. POWER WAS REDUCED AND ENGINE BLEED AIR SWITCHES WERE CYCLED, BUT LT ENGINE REMAINED IN EMERGENCY. CAPTAIN DECLARED AN EMERGENCY TO GET PRIORITY LANDING AND RETURNED WITHOUT INCIDENT. A MECHANIC WAS DISPATCHED, AND TROUBLESHOOTING REVEALED A BROKEN WIRE ON THE LT ENGINE BLEED CONTROL SWITCH LOCATED ON THE CO-PILOT`S INSTRUMENT PANEL. WIRE WAS REPAIRED AND SYS TESTED NORMALLY ON THE GROUND AND SUBSEQUENT TEST FLIGHT. 2L72 4F A10CE 20081202 WP 2008 12 2 IXXA08SMN183S 120080419A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 MISREPAIRED A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11821BX888782984 45811 DURING ROUTINE C-CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1731 LONGERON 35.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FABRICATED REPAIR DOUBLER, FILLER, FINGER DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08197 DATED 04/25/08, SEMAN DRAWING ED-4775 DATED 04/22/08, SRM 51-1-21, 51-1-20D, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, AND 51-3-1. 2L74 4F RT4A25 20081202 EU 2008 12 2 USAA2008112692132120081114A5315D53472772201 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 +5 INCHES TO FR67 +16 INCHES, -Y1195. REPAIRED FLOORBEAM BETWEEN FR66 +5 INCHES TO FR67 +16 INCHES, -Y1195 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20081202 EU 2008 12 2 USAA2008112692135120081112A5320D5311282600100 DUMMY RAIL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON DUMMY RAIL AT FR16, Y503. REPLACED DUMMY RAIL AT FR16, Y503 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20081202 EU 2008 12 2 USAA2008112692137120081113A5320D53480043207 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON R2 DOOR LOWER SILL AT FR68, Y1732. REPAIRED R2 DOOR LOWER SILL AT FR68, Y1732 IAW A320 SRM 53-41-14. 2L72 4F RTA28NM 20081202 EU 2008 12 2 YENA20081114111 120081113A3397 WIRE AIRBUS320 A320232 3930326EU EMERGENCY LIGHTSSHORTED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15580JB20792 2136 EMERGENCY LIGHT AT 13, 17 AND 21 ABC ARE OUT. FOUND SHORTED WIRES TO AISLE LIGHT AT SEAT 25ABC, CAUSING EPSU TO SHORT OUT WHEN EMERGENCY LIGHTS TURNED ON. REPAIRED SHORTED WIRES WITH A SPLICE, TAPED AND SECURED BUNDLE. REMOVED AND REPLACED EPSU PER AMM 33-51-38, OPS CHECK OF EMERGENCY AISLE LIGHTS NORMAL. 2L72 4F RTA28NM 20081202 EU 2008 12 2 USAA2008120192158120081128A3397 WIRE AIRBUS320 A320232 3930326EU CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19619AW 527 FLT 460 PHX-IND - EEL - EMERGENCY EXIT LIGHT SEAT 19 LT INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT EMERGENCY EXIT LIGHT SEAT 19 LT. OPERATIONAL CHECK GOOD. 2L72 4F RTA28NM 20081202 EU 2008 12 2 USAA2008120192159120081128A335032145410 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A USAAK NONE L NO TEST NRNOT REPORTED 1 EA19651AW3362620546 866 FLT 504 ORD-PHX - EEL - EMERGENCY EXIT SIGNS OVER 1L AND 1R DO NOT ILLUMINATE IN THE ARMED POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT AND BATTERY. OPERATIONAL CHECK GOOD. 2L72 4F RTA28NM 20081202 NM 2008 12 2 USAA2008112892140120081112A575465C26601197 REPAIR BOEING737 7373G7 138447JNM LE SLAT DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19307AW 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED ON LEFT WING NR 1 SLAT UPPER SURFACE WS 254.53 TO WS 389. REPAIRED NR 1 SLAT UPPER SURFACE IAW B737 SRM 51-70-10-2R. 2L72 4F RTA16WE 20081202 NM 2008 12 2 USAA2008112892142120081112A552265C557A13 REPAIR BOEING737 7373G7 138447JNM LT ELEVATOR DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19307AW 24634 SAL - C17 - MAJOR REPAIR - EXISTING REPAIR DELAMINATED ON LEFT ELEVATOR UPPER SURFACE AT ELEVATOR STA 53. REPAIRED LEFT ELEVATOR UPPER SURFACE IAW B737 SRM 51-70-03-0G. 2L72 4F RTA16WE 20081202 EU 2008 12 2 USAA2008112892148120081113A5315D5311141420000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y200. REPLACED FLOORBEAM AT FR20, -Y200 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20081202 EU 2008 12 2 USAA2008112892149120081114A5347DAN2001179511 SEAT TRACK AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON RAIL SEAT BETWEEN FR64 TO FR66, -Y1292. REPLACED RAIL SEAT BETWEEN FR64 TO FR66, -Y1292 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20081202 NM 2008 12 2 USAA2008112892138120081126A5755 SPOILER BOEING737 7373G7 138447JNM RT WING DELAMINATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19322AW 25400 CLT - RON - MAJOR REPAIR - RIGHT WING NR 7 SPOILER DELAMINATED AT UPPER TRAILING EDGE APPROX 5 INCHES CIRCULAR DIAMETER. REPLACED NR 7 SPOILER IAW B737 AMM 27-61-11. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086588 120081124A3350417N5213 COVER BOEING737 7377H4 1384404NM CABIN MISSING A SWAAK NONE O OTHER ININSP/MAINT 1 SW29265WN 32522 FOUND FWD EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM. 2L72 4F RTA16WE 20081201 2008 12 1 USAASB08109 420081116A2565D37022101 BOTTLE AIRCRUISERS BOEING737 737401 138449BNM EVAC SLIDE LOW PRESSURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19405US 1227 23885 MCO - MAINTENANCE REPORTED THE FORWARD ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE WAS LOW. MAINTENANCE REMOVED AND REPLACED THE FORWARD ENTRY DOOR ESCAPE SLIDE ASSEMBLY PER MM 25-61-00. 2L72 4F RTA16WE 20081201 NM 2008 12 1 DL777081621 120081122A2530 OVEN BOEING777 777232 1385232NM PWA 4060 PW4060 52119NE GALLEY ODOR A DALAO OTHER B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 SO27863DA 29735 724164 GALLEY 401 OVEN 2 AFTER COOKING 8 MINS MADE HIGH PITCH BUZZ THEN QUIT W/ASSOCIATED BURNT WIRE ODOR NO FAULT LIGHT. 2L72 4F4 FRTT00001SEE24NE 20081201 2008 12 1 JGV2008F00007 420081104A256182122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531CE LIFE VEST MISSING B JGVRK NONE W INADEQUATE Q C ININSP/MAINT 1 CE09177JB L782063 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECEIVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPECTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTINE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFORMED. (K) 2L72 4F RTA10CE 20081201 2008 12 1 JGV2008F00006 420081104A256182122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531CE LIFE VEST MISSING B JGVRK NONE W INADEQUATE Q C ININSP/MAINT 1 CE09177JB L782064 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECEIVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPECTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTINE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFORMED. (K) 2L72 4F RTA10CE 20081201 NM 2008 12 1 USAA BB08169 120081119A3350 BATTERY BOEING767 767201 1385125NM EMERGENCY LIGHTSINOPERATIVE A USAAK NONE O OTHER ININSP/MAINT 1 EA19246AY 23898 CLT - RIGHT EMERGENCY ESCAPE SLIDE SQUIP LIGHT FAILED TO ILLUMINATE DURING TEST ONE. MAINTENANCE REPLACED THE RIGHT OFF WING ESCAPE SYSTEM EMERGENCY BATTERY. 2L72 4F RTA1NM 20081201 EU 2008 12 1 USAA2008112092092120081119A2120 UNKNOWN AIRBUSA321 A321211 3930370EU CABIN FUMES A USAAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA19179UW 1521 FLT 904 CLT-ORD - RETURN TO FIELD - APPROXIMATELY 10 MINUTES INTO FLIGHT, FUMES WERE REPORTED IN THE REAR OF THE AIRCRAFT. THE CREW BEGAN A RETURN TO CLT AND WHEN AIRCRAFT STOPPED CLIMBING, THE FUMES DISSIPATED. IT WAS DECIDED TO CONTINUE TO ORD, BUT WHEN AIRCRAFT BEGAN TO CLIMB AGAIN, THE FUMES RETURNED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO CLT. THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT PER THE TSM (TROUBLESHOOTING MANUAL) 71-00-00-810-802 WITH NO FAULTS NOTED. RAN BOTH ENGINES AND APU BLEEDS AND PACKS TO TAKEOFF POWER. NO SMOKE OR SMELL NOTED. 2L72 4F RTA28NM 20081201 CE 2008 12 1 ZESA2008014 120080925A77128184873 SENSOR CESSNA500 560CESSNA 2076750CE PWA 530 PW535A NE RT ENGINE OUT OF LIMITS E ZESAK NONE O OTHER TOTAKEOFF 1 EA03511TH 5600561 PCEDC0044 CREW IDENTIFIED DURING TAKEOFF THAT THE THROTTLE POSITION WHEN MATCHED SHOWED THE LT ENGINE AT 88 PERCENT AND THE RT ENGINE AT 37 PERCENT. RT ENGINE TOOK APPX 4-5 SECONDS TO CATCH UP TO THE LT. MAINT TROUBLESHOT AND REPLACED THE RT ENGINE T1 SENSOR. OPS CHECKS SATISFACTORY. 2L72 4F4 FRTA22CE E00053EN 20081201 NM 2008 12 1 USAA920082070 120081020A53206546812169 INTERCOSTAL BOEING737 7373G7 138447JNM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19158AW 23780 SAL C21 MAJOR REPAIR NR 6136496 CORROSION ON INTERCOSTAL BETWEEN BS967 TO BS986.5, WL208.1, RBL17.5 IN PASSENGER CABIN. REPAIRED INTERCOSTAL BETWEEN BS967 TO BS986.5, WL208.1, RBL17.5 IAW B737 SRM 51-40-02-0G. 2L72 4F RTA16WE 20081201 NM 2008 12 1 NWAA084986310 120081108A3350 POWER SUPPLY BOEING747 747451 1384940NM CABIN DISCHARGED A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01670US 24225 DURING OVERNIGHT FOUND 2 EACH RT OVER WING EMERGENCY LIGHTS INOP. MX R&R POWER SUPPLY. OPS CHECKED GOOD, AND ACFT WAS RETURNED TO SERVICE. 2L74 4F RTA20WE 20081202 NM 2008 12 2 USAA2008112492109120081114A5320 SUPPORT ANGLE AIRBUSA319 A319132 3930340NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19804AW 1043 SAL - C7 - MAJOR REPAIR - CORROSION ON SUPPORT ANGLE AT INTERNAL STRUCTURE OF FORWARD CARGO COMPARTMENT FR29 + 2.5 INCHES, S43R. REPLACED SUPPORT ANGLE AT INTERNAL STRUCTURE OF FORWARD CARGO COMPARTMENT FR29 + 2.5 INCHES, S43R IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20081202 NE 2008 12 2 ASMF 20081102 220081121A7230JT8D219 FAN BLADE DOUG DC9 DC987 3022087WP PWA JT8 JT8D219 52053NE RT ENGINE NICKED W ASMFK NONE O OTHER ININSP/MAINT 1 SW23754RA4396410798 49641 718193 DURING OVERNIGHT CHECK, FOUND A NICK OF 0.005 INCHES DEPTH ON THE LEADING EDGE OF ONE FAN BLADE AT .4375 INCHES FROM THE ROOT, AND A NICK OF 0.0035 INCHES OUT OF LIMITS ON THE LEADING EDGE OF THE OTHER FAN BLADE AT .7500 INCHES FROM THE ROOT. RT ENG WAS REPLACED AND OPERATIONAL TEST WAS PERFORMED IAW MM 71-00-02 AND CM 71-00-01, ALL CORRECT. 2L72 4F4 FRTA6WE E9NE 20081202 EU 2008 12 2 USAA2008112692134120081114A5315D5347279220000 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR68, Y765. REPLACED FLOORBEAM AT FR68, Y765 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20081202 NM 2008 12 2 YENA200811260121 120081125A2120 UNKNOWN EMB ERJ190ERJ190100IGW3260408NM CABIN ODOR A YENAHA DEACTIVATE SYST/CIRCUITSUNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 EA15279JB 190000090 FLT 623, JFK-HOU - AFTER TAKEOFF CALL RECEIVED FROM FLIGHT ATTENDANT AT 1500FT , A STRONG SMELL OF SMOKE IN THE CABIN. BELIEVED TO BE ELECTRICAL SMELL. AT THAT TIME CREW COULD SMELL SMOKE IN COCKPIT BUT NOT AS STRONG. PERFORMED QRH SMOKE COCKPIT/CABIN SMOKE/FUMES PROCEDURE. RETURNED TO JFK FOR EMERGENCY LANDING. THE SMOKE WAS NEVER VISIBLE TO THE FLIGHT OR INFLIGHT CREW. AFTER PERFORMING THE QRH PROCEDURE WHICH LEAD TO SHUTTING OFF THE BLEEDS AND RECIRCULATION FAN, NO LONGER COULD SMELL THE BURNING ODOR. THERE WAS NO FURTHER INCIDENT AFTER TOUCHDOWN. TAXIED TO GATE NORMALLY WITH ARFF VEHICLES FOLLOWING AS PRECAUTION. PERFORMED TASK 21-20-00-810-801A SMOKE AND/OR ABNORMAL SMELL IN PASSENGER COMPARTMENT 2L72 4F RTA57NM 20081202 NM 2008 12 2 NWAA084996624 120081107A3350 BATTERY PACK BOEING747 747251B 1384892NM EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01624US 21706 DURING OVERNIGHT FOUND EMERGENCY EXIT SIGNS AT DOOR 2 RT INOP. MX R&R BATTERY PACK. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE. 2L74 4F RTA20WE 20081202 NE 2008 12 2 UALA2008112106611220081121A7397 CONNECTOR BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE FUEL FLOW BROKEN A UALAO OTHER J WARNING INDICATION DEDESCENT 1 WP29648UA 25285 CREW REPORTED FUEL CONFIGURATION EICAS ON DESCENT. FOUND ENTIRE CONNECTOR BROKEN AT THE DIFFERENTIAL PRESSURE SWITCH, D11000. REPLACED NR 1 ENG FUEL FLOW CONNECTOR. NR 1 ENGINE, 5 MINUTE IDLE RUN ACCOMPLISHED. NO LEAKS NOTED. 2L72 4F4 FRTA1NM E24NE 20081202 EU 2008 12 2 YENA200811240117 120081123A3350312431 POWER SUPPLY AIRBUS320 A320232 3930326EU CABIN FAILED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15570JB1627 2099 EMERGENCY LIGHT TEST FAILED FWD EPSU. REMOVED AND REPLACED EPSU, OPS CHECK NORMAL IAW AMM 33-51-38-04. 2L72 4F RTA28NM 20081202 WP 2008 12 2 NWAA085029881 120081009A4930 O-RING DOUG DC9 DC951 3022051WP APU FUEL SYS LEAKING A NWAAO OTHER KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 GL01676MC 47652 SHORTLY AFTER TAKEOFF FLIGHT ATTENDANT REPORTED STRONG FUEL ODOR IN CABIN. A SLIGHT FUEL ODOR WAS NOTICED IN THE COCKPIT. FLIGHT CREW LANDED AT DESTINATION. MX NOTICED APU INTAKE PLENUM WET WITH FUEL AND ALSO A FUEL LEAK AT THE APU FUEL HEATER. THE APU AND AN O-RING ON THE APU FUEL HEATER WERE REPLACED. PACK BURNOUT AND COALESCER BAG REPLACEMENT COMPLIED WITH. 2L72 4F RTA6WE 20081202 NM 2008 12 2 NWAA085006743 120081108A3350 BATTERY PACK BOEING747 747249F 1384849NM EMERGENCY LIGHT INOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01643NW 22245 DURING LINE CHECK FOUND UPPER DECK EMERGENCY LIGHT INOP. MX R&R BATTERY PACK. OPS CHECKED GOOD AND ACFT WAS RETURNED TO SERVICE. 2L74 4F RTA20WE 20081202 NM 2008 12 2 USAA920082072 120081116A53306545775 SKIN BOEING737 7373G7 138447JNM ZONE 100 CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19155AW 23777 PHX RON MAJOR REPAIR NR 4451797 FUSELAGE SKIN CRACKED BETWEEN BS727E TO BS747, S23R. REPAIRED FUSELAGE SKIN BETWEEN BS727E TO BS747, S23R IAW SRM 53-00-01-2R31. 2L72 4F RTA16WE 20081202 NM 2008 12 2 YENA200811200115 120081117A27821703909 ACTUATOR EMB ERJ190ERJ190100IGW3260408NM LE SLAT FAILED A YENAB EMER. DESCENT F FLT CONT AFFECTED APAPPROACH 1 EA15193JB7987 190000017 FLT 1219, BOS-BUF, AOA FAIL EICAS MESSAGE, SLAT FAIL EICAS MESSAGE QRH COMPLIED WITH EMERGENCY LANDING ACCOMPLISHED. T/S PER FIM TASK 27-81-00-810-802-A. FOUND NR 6 RT SLAT ACTUATOR TRIPPED DUE TO PREVIOUS HISTORY, REMOVED & REPLACED NR 6 RT SLAT ACTUATOR PER 27-81-01-000-801-A AND 27-81-01-400-801-A, PERFORMED MECHANICAL RIG OF NR 567 RT SLAT ACTUATORS PER 27-80-820-801-A. NO ADJUSTMENT NEEDED. PERFORMED ELECTRICAL RIGGING PER 27-80-00-820-802-A. OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME. PERFORMED FIM TASK 27-03-00-810-89L-A. NO FAULTS NOTED AT THIS TIME. 2L72 4F RTA57NM 20081202 NM 2008 12 2 DXTA2008120103378120081129A2612 WARNING LIGHT GULSTM200 200 4500308NM APU FIRE FALSE ACTIVATIONE DXTAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 GL07745QS 170 15 MINS AFTER APU SHUTDOWN APU FIRE CAS MSG CAME ON IN FLIGHT. NO INDICATION OF FIRE VISIBLE ON GROUND. 2L72 4F RTA53NM 20081202 NM 2008 12 2 DXTA2008120103379120081130A3230 LANDING GEAR GULSTM200 200 4500308NM INOPERATIVE E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07712QS 073 ON DEPARTURE APA, UNABLE TO GET LT AND RT MAIN TO RETRACT. 2L72 4F RTA53NM 20081202 CE 2008 12 2 BSY2008F00015 120081020A2421649305R ALTERNATOR BEECH 58 58 1152740CE ENGINE INTERMITTENT E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL07696BD TH352 LT ALTERNATOR INTERMITTENT, COULD NOT DUPLICATE, CHANGED AS PRECAUTIONARY MEASURE, OPS GOOD. (K) 1L72 3O 3A16 20081202 CE 2008 12 2 BSY2008F00016 120081029A3060353801327 SWITCH BEECH 58 58 1152740CE PROP HEAT BURNED E BSYAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 GL079044V TH216 ACFT ENROUTE, WHEN PILOT SMELLED SMOKE AND SAW FLAMES COMING OUT OF PROPELLER HEAT CIRCUIT BREAKER SWITCH. PILOT THEN DIVERTED TO AIRPORT WITH NO OTHER PROBLEMS. (K) 1L72 3O 3A16 20081202 NE 2008 12 2 BSY2008F00005 220081003A7200 ENGINE CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE FAILED E BSYAA UNSCHED LANDING YJ ENGINE STOPPAGE WARNING INDICATION NRNOT REPORTED 1 GL071115M 208B0356 PCE17008 ACFT ENROUTE, WHEN THE ENGINE FAILED. PILOT WAS ABLE TO LAND ON A HIGHWAY WITH NO PROBLEMS. CAUSE UNKNOWN AT THIS TIME. (K) 1H71 3T3 T A37CE E4EA 20081202 CE 2008 12 2 BSY2008F00006 120080927A5210 DOOR BEECH 58 58 1152740CE UNSECURE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL072064V TH1004 ACFT ENROUTE, WHEN THE CABIN DOOR POPPED OPEN, PILOT THEN LANDED. SECURED DOOR AND CONTINUED. (K) 1L72 3O 3A16 20081202 NM 2008 12 2 UALA2008111306307120081029A3610 REGULATOR BOEING777 777222 1385219NM PWA PW4077PW4077 NE BLEED AIR SYSTEMBLOCKED A UALAA UNSCHED LANDING W INADEQUATE Q C CRCRUISE 1 WP29777UA 26916 LOSS OF ALL WATER PRESSURE. FLIGHT DIVERTED. FOUND BLEED AIR PRESSURE REGULATOR BLOCKED. CLEANED AND NOW WATER PRESSURE TO LAV AND GALLEY NORMAL. 2L72 4F4 FRTT0001SE E46NE 20081202 CE 2008 12 2 BSY2008F00007 120081016A5210 DOOR BEECH 58 58 1152740CE UNSECURE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL072064V TH1004 ACFT ENROUTE, HAD TO LAND AT BECAUSE CABIN DOOR POPPED OPEN SECURED DOOR AND CONTINUED TO DEPARTURE. (K) 1L72 3O 3A16 20081202 NM 2008 12 2 UALA2008111306361120081103A496032908144 CONTROLLER BOEING777 777222 1385219NM PWA PW4077PW4077 NE APU FAULTY A UALAO OTHER W INADEQUATE Q C NRNOT REPORTED 1 WP29213UA 30219 APU BLEED AIR APUC DETECTED LOSS OF ABILITY TO PNEUMATICALLY LOAD APU. MESSAGE IS TRIGGERED BY IGV OR SURGE CONTROL SYSTEM FAULTS. STATUS MSG01- NOT ACTIVE ENGINE START MODE DEPENDENT; SURGE CONTROL VALVE (PNEUMATIC CLUSTER) DOES NOT FOLLOW COMMAND. DB- APU CONTROLLER (APUC) MSG-4911180 INACTIVE MODE. REPLACED APU CONTROLLER. 2L72 4F4 FRTT0001SE E46NE 20081202 EU 2008 12 2 YENA200811200116 120081117A2120 UNKNOWN AIRBUS320 A320232 3930326EU CABIN ODOR A YENAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 EA15597JB 2307 FLT 760, SJU-BOS, 30 MINUTES AFTER TAKEOFF F/A REPORTED A BURNING PLASTIC ODOR. COUNTING FROM THE LAST THREE ROWS, TURNED OFF (LIVE TV) AND THE ODOR WENT AWAY. COMPLIED WITH TSM 24-00-00-810-823. NO DAMAGE FOUND. PERFORMED INSPECTION PER TSM 23-39-00-819-801 SECTION B. NO ABNORMALITIES FOUND. MONITORED FOR 2 HOURS. OPS NORMAL. 2L72 4F RTA28NM 20081202 NM 2008 12 2 UALA2008112406618120081121A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAO OTHER O OTHER ININSP/MAINT 1 WP29552UA 26641 AFT PIT AT STA 1560, STR 26R, FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF FRAME AND INSTALLED DOUBLER REPAIR. 2L72 4F4 FRTA2NM E17NE 20081202 NM 2008 12 2 UALA2008112406620120081121A5315 FLOORBEAM BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE CORRODED A UALAK NONE O OTHER ININSP/MAINT 1 WP29552UA 26641 MAIN CABIN FLOORBEAM STA 1640, RBL 57 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SECTION OF T-CAP, RBL 0 TO RBL 64. FAB NEW SECTION AND SPLICES. 2L72 4F4 FRTA2NM E17NE 20081202 CE 2008 12 2 BSY2008F00004 120081007A8011 STARTER CESSNA208 208B 2073701CE PWA PT6 PT6A114A 52043NE ENGINE NOISY E BSYAA UNSCHED LANDING O OTHER CLCLIMB 1 GL07105AN 208B0956 PCEPC0911 AFTER TAKEOFF, AT 5,000 FT, ENGINE STARTER TO MAKE A SQUEALING NOISE WITH A RISE IN EGT, LOW TORQUE AND NO. PILOT THEN RETURNED TO DEPARTURE NO PROBLEMS. CAUSE UNKNOWN AT THIS TIME. (K) 1H71 3T3 T A37CE E4EA 20081203 NM 2008 12 3 AALA200820043 120081103A5347141N51301 SEAT TRACK BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21604AA43723 27055 LT INBOARD SEAT TRACK CORRODED, REPLACED SEAT TRACK IAW SRM 51-10-02. 2L72 4F RTA2NM 20081203 CE 2008 12 3 BSY2008F00000 120081015A3010442CLU12 PLUG BEECH 58 58 1152740CE CONT O520 IO520* 17032SO VACUUM PUMP MISSING E BSYAK NONE O OTHER ININSP/MAINT 1 GL07525GW417 TH557 ACFT WING BOOTS WON`T INFLATE TO FULL PRESSURE. FOUND INSP PLUG MISSING CAUSING PREMATURE PUMP FAILURE. (K) 1L72 3O3 O 3A16 E5CE 20081203 SO 2008 12 3 FDKA2008111500295120081115A5610163500115 WINDSHIELD EMB 145 EMB145LR 3260212SO COCKPIT CRACKED A FDKAB EMER. DESCENT O OTHER CRCRUISE 1 SW07830MJ 145259 FDL FLT 6173 JFK-PIT - EMERGENCY DECLARED DUE TO LT WINDSHIELD SHATTERED. MX REMOVED AND REPLACED WINDSHIELD, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20081203 NM 2008 12 3 AALA200820040 120081103A5320146N5318 PLATE BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21604AA43723 27055 AFT MAIN DECK PLATE CORRODED. REPAIRED IAW SRM 53-60-51-2R. 2L72 4F RTA2NM 20081203 NE 2008 12 3 AALA200802731 220081013A7261 OIL SYSTEM DOUG DC9 DC982 3022082WP PWA JT8 JT8D217 52053NE NR 1 ENGINE LOW PRESSURE A AALAEA ENGINE SHUTDOWN UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SW21441AA 49460 728218 PHL INFLIGHT JFK TO DFW - DURING CLIMB NUMBER ONE ENGINE OIL PRESSURE LOW LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO ZERO ON GAUGE AND OIL TEMPERATURE DROPPED. CREW SHUT DOWN ENGINE AS PRECAUTION. LANDED PHL WITHOUT INCIDENT. SINGLE ENGINE TIME 15 MINUTES. FOUND METAL IN FILTER. REPLACED NUMBER ONE ENGINE ON 13 OCT AT PHL DUE TO OIL PRESSURE OUT OF LIMITS. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F4 F A6WE E9NE 20081203 2008 12 3 UALA2008112406627420081122A2565H2052K3833 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EVAC SLIDE DOOR FAULTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 RT OVERWING ESCAPE SLIDE COMPARTMENT DOOR LATCHES FAIL TORQUE CHECK AT 225 IN LBS. REMOVED AND REPLACED 4 EA LATCHES AT RT OVERWING SLIDE COMPT DOOR. PRELIMINARY ADJUSTMENT AND LATCHING SYSTEM ADJUSTMENT CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20081203 2008 12 3 UALA2008112406628420081122A2565H2052K3833 LATCH BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE EVAC SLIDE WORN A UALAK NONE O OTHER ININSP/MAINT 1 WP29660UA 27115 LEFT OVERWING ESCAPE SLIDE DOOR LATCH NR 3 SLIDER WORN. REMOVED AND REPLACED NR 3 LATCH. OP CHECKS GOOD. 2L72 4F4 FRTA1NM E24NE 20081203 EU 2008 12 3 AALA200802730 120081012A3350 BATTERY PACK AIRBUS300 A300B4605R 3930308EU EMERGENCY LIGHTSDISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW2150051 459 MIA - EMERGENCY LIGHTS AT SEAT ROWS 1G TO 5G INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 1G TO 5G. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F RTA35EU 20081203 WP 2008 12 3 AALA200810198 120081110A5311 FRAME DOUG DC9 DC982 3022082WP ZONE 200 CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 FRAME AT STA 1418 L-2L TO L-2R HAS CRACKS. INSTALLED DOUBLER AND RADIUS BLOCK PER AARD 53-10-00-17. 2L72 4F A6WE 20081203 NM 2008 12 3 AALA200820048 120081105A5320141N5160U46 FLOOR SUPPORT BOEING757 757223 1384957NM ZONE 100 CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21666A 52891 25300 FLOORBOARD SUPPORT HAT CHANNEL CORRODED. REPLACED FLOOR SUPPORT HAT CHANNEL IAW SRM 53-10-51-01. 2L72 4F RTA2NM 20081203 2008 12 3 BSY2008F00017 220080925A7261 DIPSTICK LEAR 35 35LEAR 5170600CE LT ENGINE UNSECURE E BSYAO OTHER O OTHER NRNOT REPORTED 1 GL07900JC 178 ACFT DEPARTED, WHEN PILOT NOTICED HIS LT ENGINE OIL PRESSURE DROPPING, HE THEN NOTIFIED TOWER AND RETURNED TO DEPARTURE. FOUND OIL DIP STICK NO SECURED CAUSING OIL LOSS. (K) 2L72 4F A10CE 20081203 NM 2008 12 3 HNAA2008112300324120081121A2611PU90461S SMOKE DETECTOR DHAV DHC8 DHC8102 2809003NM LAVATORY MALFUNCTIONED A HNAAD RETURN TO BLOCK N FALSE WARNING TXTAXI/GRND HDL 1 EA07908HA* 59520 015 LAV SMOKE DETECTOR SOUNDED ABOUT 10 TIMES AND STOPPED, NO EVIDENCE OF SMOKE OR FUMES. LAV SMOKE DETECTOR DEACTIVATED IAW SP 26.2 REFERENCE LP 279923 ITEM 2. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW 26-12-05 AND REACTIVATED SYSTEM OPS CHECK GOOD. P/N ON/OFF PU90-461S S/N OFF 08243 S/N ON 09254. 2H72 4T RTA13NM 20081203 SO 2008 12 3 RAIA2008112500003120081122A3297 WIRE EMB 145 EMB145EP 3260221SO LANDING GEAR BROKEN A RAIABA EMER. DESCENT UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03805HK 145096 DURING CLIMB, CREW RECEIVED A LG AIR/GROUND FAILURE MESSAGE ON THE EICAS. MAINTENANCE REPAIRED WIRING AT THE LT AFT A/G SWITCH. SYSTEM OPS CHECKED GOOD FOLLOWING REPAIR. 2L72 4F RTT00011AT 20081203 SO 2008 12 3 RAIA2008120100001120081126A3260 PROXIMITY SENSOR EMB 145 EMB145EP 3260221SO LT MLG OUT OF ADJUST A RAIAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 CE03809HK 145187 DURING CLIMB FROM TAKEOFF, CREW RECEIVED AN AIR/GROUND FAIL MESSAGE ON THE EICAS AND GEAR WOULD NOT RETRACT. MAINTENANCE INSPECTED AND FOUND THAT THE LT MLG WOW PROXIMITY SENSOR REQUIRED ADJUSTMENT. ADJUSTMENT WAS MADE AND LANDING GEAR SYSTEM, OPS CHECKED GOOD. 2L72 4F RTT00011AT 20081203 SO 2008 12 3 RAIA2008120100002120081130A3610 DUCT EMB 145 EMB145LR 3260212SO BLEED AIR SYS LOOSE A RAIAAD UNSCHED LANDING RETURN TO BLOCK J WARNING INDICATION CLCLIMB 1 CE03840HK 145341 DURING CLIMB FROM TAKEOFF, CREW RECEIVED A BLEED NR 1 AND NR 2 LEAK MESSAGE ON THE EICAS. MAINTENANCE RESECURED LOOSE A NR 2 BLEED LINE DUCT UNDER THE CARGO FLOOR. BLEED SYSTEM, OPS CHECKED GOOD. 2L72 4T RTT00011AT 20081203 EU 2008 12 3 08FDEA04957 120081121A5321 FLOOR PANEL AIRBUS300 A300B4622 3930401EU CARGO BAY PUNCTURED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21716FD 358 THE BULKPIT FLOOR PANEL 161 BF IS PUNCTURED. REPAIRED PUNCTURE ON FLOOR PANEL 161 BF IN REF TO A300-600 SRM 53-10-20, STEP 10A. 2L72 4F RTA35EU 20081203 NM 2008 12 3 08FDEA04960 120081122A5320651633512 BRACKET BOEING727 7272D4 138407UNM RT MLG WW CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21287FE 21849 RT MLG W/W CUTOUT SEAL BEAM (STR 19R), AREAS OF CORROSION ON TOP SIDE OF BEAM FROM FS 906 TO FS 930, RBL 74, WL 105 REMOVED CORROSION FROM BRACKET, STA 920 ORIG T .094, REMAINING T .071, .023 MATERIAL LOSS OUT OF LIMITS. REPLACED BRACKET STA 920. REMOVED CORROSION FROM BEAM, ORIG T .080' REMAINING T .076. .004 MATERIAL REMOVED WITHIN ALLOWABLE DAMAGE. REF SRM 51-30-2 PG 1-7, SRM 53-10-1 PG 2A, AMM 51-20-021-7 PG 1-3, AMM 51-20-151-7 PG 1, THIS IS CLASSIFIED AS A MINOR REPAIR. 2L73 4F A3WE 20081203 EU 2008 12 3 FDEA200812015032 120081201A5321A4600003434100 FLOORBOARD AIRBUS300 A300B4622 3930401EU CABIN BROKEN A FDEAK NONE O OTHER ININSP/MAINT 1 CE21716FD 358 CABIN FLOOR BOARD BROKEN IN 3 PIECES, BETWEEN FR 47 - 51, 4TH BOARD FROM LEFT. FABRICATED NEW FLOOR BOARD USING OLD BOARD AS TEMPLATE IAW FEDEX DWG SRZ 25- 005 REV G. 2L72 4F RTA35EU 20081203 NM 2008 12 3 FDEA200812025037 120081202A5270 ACTUATOR BOEING727 7272S2F 1384O81NM DOOR WARNING BROKEN A FDEAA UNSCHED LANDING O OTHER CLCLIMB 1 CE21204FE 22926 AFT AIRSTAIR LIGHT ILLUMINATED IN-FLIGHT CLIMBING THROUGH 4,500 FEET. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B. AMBER AFT AIRSTAIR DOOR WARNING LIGHT INOP." REPLACED WARN RT HAND UPLOCK ROLLER FITTING PER SMP, FOUND SWITCH S395 ROLLER ACTUATOR BROKEN AND SWITCH INOP. REPLACED S395 AND ROLLER ACTUATOR PER WDM 52-71-01 AFT AIRSTAIR OPERATION AND ALL INDICATIONS CK OK PER MM 52-62-001-5 2L73 4F A3WE 20081203 EU 2008 12 3 FDEA200812025039 120081202A5230A5237416020800 SKIN AIRBUS300 A300B4622R 3930312EU AFT CARGO DOOR CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21722FD 479 AFT CARGO DOOR INTERNAL SKIN CORRODED AT FWD LWR CORNER. THIS SDR IS GEN TO REFLECT CORRECTIONS MADE IN CORRECTIVE ACTION BLOCK FROM ORIG SDR 08-4756. REMOVED CORROSION IAW A300-600 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 51-30-00. ORIGINAL MATERIAL 0.063. REMAINING MATERIAL 0.051. MATERIAL REMOVED 0.011. USED UT GAUGE T8225Q. REMOVED AND RE-INSTALLED PANELS 812 AR AND BR; 154 AR; BR; CR IAW A300-600 AMM 52-72-11-5. REMOVED AND RE-INSTALLED SEAL RETAINER IAW A300-600 AMM 52-30-18-4. REMOVED AND REINSTALLED CAPS AND INSTALLED NEW SKIN IAW A300-600 SRM 51-72-10. MATERIAL ID 2024-T3, 0.063, PO 633758.6 IAW A300-600 SRM 52-32-00. ALODINED IAW A300-600 SRM 51-21-10. PRIMED IAW A300-6002L72 4F RTA35EU 20081203 NM 2008 12 3 FDEA200812025042 120081202A5320141N5160322 FLOOR SUPPORT BOEING757 75723A 1384967NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21918FD 24290 CABIN FLOOR, BS 297, RBL 20-36.2, CHANNEL IS CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT AT BS 297, RBL 20-36.2, IAW SRM 51-40-02. FABRICATED NEW SUPPORT ON MAE TRAVELER T8/759390. TREATED, PRIMED AND TOP COATED SUPPORT IAW SRM 51-20-01 AND AMM 51-21-00. LOCATED AND DRILLED NEW SUPPORT IAW SRM 51-40-05. INSTALLED NEW SUPPORT, BS 297, RBL 20-36.2, IAW SRM 51-40-02. CORROSION WAS DETERMINED TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3 (L=1.9 INCH, W=1.0 INCH, D=.033 INCH). THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR. 2L72 4F RTA2NM 20081203 WP 2008 12 3 FDEA200812025047 120081202A3260 WARNING SYSTEM DOUG MD10 MD1010F 3022112WP COCKPIT ACTIVATED A FDEAK NONE J WARNING INDICATION LDLANDING 1 CE21556FE 46710 LANDING MEM, 18R 3 UNSAFE (RED) GEAR LIGHTS WITH GEAR HANDLE DOWN, 3 UNSAFE ON CONFIG PAGE, QRH PROCEDURE DEPLOY ALT GEAR EXTENSION AND RECEIVED 3 GREEN SAFE (CONFIG AND GEAR). NOSEWHEEL STEERING RIGHT LIMITED TO 25 DEG. 2L73 4F RTA22WE 20081203 WP 2008 12 3 AALA200810218 120081106A5320 INTERCOSTAL DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 CABIN FLOOR SUPPORT, INTERCOSTAL CRACKED AT STATION 1287 TO 1209. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-00. 2L72 4F A6WE 20081203 NM 2008 12 3 08FDEA04968 120081124A571264834219 RIB BOEING727 7272D4 138407UNM LT WING CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21287FE 21849 LT WING L/E RIB LWR CHORD HAS 2 CRACKS AT 5 INCH AND 18 INCH FROM SPAR, FSS 122. REMOVED PNL 6301 TO FOM. FABRICATED ANGLE REF DWG 64-8342-19 DRILLED-UP, TREATED, PRIMED, AND INSTALLED ANGLE REF SRM 51-30-5, MM 51-20-021, MM 51-20-051, AND SRM 51-30-2. INSTALLED PANEL 6301 REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR. 2L73 4F A3WE 20081203 NM 2008 12 3 08FDEA04970 120081124A5347BAC1592792 SEAT TRACK BOEING757 75728A 1384976NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21912FD 24260 SEAT TRACK BS 418-440, RBL 24, GOUGED AND CORRODED. AFTER EVALUATION, DAMAGE ON SEAT TRACK, RBL 24, BS 418-440, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED SEAT TRACK IAW SRM 51-40-02. RECEIVED NEW SEAT TRACK ON MAE TRAVELER NR T8/769432. LOCATED AND DRILLED NEW SEAT TRACK, TREATED AND PRIMED AND PAINTED NEW SEAT TRACK IAW SRM 51-20-01. INSTALLED NEW SEAT TRACK, BS 418-440, RBL 24, IAW SRM 51-40-02/53-00-52. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING. 2L72 4F RTA2NM 20081203 EU 2008 12 3 FDEA200811244967 120081124A5320A5381206720000 FITTING AIRBUS300 A300B4622 3930401EU FUSELAGE CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21716FD 358 MAIN CABIN, AT FRAME 48 AND GANTRY 4 RT, SEAT TRACK, "LINAGE FITTING" IS CRACKED, (UNDER FLOOR) REMOVED SEAT TRACK SPLICES AND DAMAGED LINKAGE FITTING IAW A300-600 SRM 51-30-00. LOCATED AND DRILLED NEW LINKAGE FITTING IAW A300-600 SRM 51-30-40. INSTALLED NEW LINKAGE FITTING AND OLD SEAT TRACK SPLICES IAW A300-600 SRM 51-30-00 PART NR A5381206720000 PO NR 640729.3. 2L72 4F RTA35EU 20081203 WP 2008 12 3 FDEA200811254972 120081125A521062963 SOLENOID DOUG MD10 MD1010F 3022112WP L1 DOOR DEFECTIVE A FDEAK NONE O OTHER ININSP/MAINT 1 CE21397FE 46631 L-1 DOOR TORQUE TUBE SOLENOID NOT OPERATING PROPERLY. REMOVED AND REPLACED L-1 DOOR TORQUE TUBE SOLENOID AND ADJUSTED. OPS CHECKED GOOD IAW FEDEX MD 10 AMM 52-11-13-2 AND 52-11-00-5. 2L73 4F RTA22WE 20081203 EU 2008 12 3 FDEA200811264980 120081126A5712A5724196000400 RIB AIRBUS300 A300B4622R 3930312EU RT WING DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21722FD 479 RIGHT WING RIB 5; HOLE "E", THE EXISTING HOLE SIZE IS LARGER THAN THE FINAL HOLE SIZE CALLED OUT IN FEDEX EO 6-5710-7-5005 P1. COMPLIED WITH FEDEX EA 6-5710-123672, WINGS - AD 99-16-01 - EO 6-5710-7-5005, RT WING REAR SPAR MLG FWD PICK-UP FITTING BOLT "E". 2L72 4F RTA35EU 20081203 NM 2008 12 3 AALA200820042 120081103A5347141N51301 SEAT TRACK BOEING757 757223 1384957NM FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21604AA43723 27055 LT OUTBOARD SEAT TRACK CORRODED, REPLACED SEAT TRACK IAW SRM 51-10-02. 2L72 4F RTA2NM 20081203 NM 2008 12 3 FDEA200812025044 120081202A5320141N5160188 FLOOR SUPPORT BOEING757 75723A 1384967NM FUSELAGE CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21918FD 24290 CABIN FLOOR, BS 297-310.5, RBL 30, CHANNEL CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT, BS 301-310.5, RBL 30, IAW SRM 51-40-02. FABRICATED NEW FLOOR SUPPORT (CHANNEL) ON MAE TRAVELER T8/759040. TREATED, PRIMED AND TOP COATED NEW SUPPORT/CHANNEL IAW SRM 51-20-01 AND AMM 51-21-00. LOCATED AND DRILLED NEW SUPPORT/CHANNEL IAW SRM 51-40-05. INSTALLED NEW SUPPORT/CHANNEL, BS 301-310.5, RBL 30, IAW SRM 51-40-02. CORROSION WAS 100 PERCENT EXFOLIATED THRU PART AND OUT OF LIMITS IAW SRM 53-00-51, FIG 101. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR. 2L72 4F RTA2NM 20081203 EU 2008 12 3 FDEA200812025045 120081202A5711A5724453123200 ANGLE AIRBUS300 A300B4622 3930401EU LT WING GOUGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21716FD 358 LT WING AFT OF REAR FALSE SPAR APPROX RIB 6A AREA HAS VERTICAL WEB GOUGED AND DOUBLE DRILLED HOLES. REMOVED LOWER SKIN PANEL AND DAMAGED ANGLE REF SRM 51-40-21 PARA 6 AND 13. FABRICATED NEW ANGLE REF SRM 57-51-11 AND DWG A57244531. ALODINED REF SRM 51-21-10. PRIMED AND PAINTED REF SRM 51-23-10. PARTS MARKED REF GMM 7-0-1000. INSTALLED NEW ANGLE AND LOWER SKIN REF SRM 51-40-21 PARA 6, 7, AND 13. 2L72 4F RTA35EU 20081203 NM 2008 12 3 ZZDA2008172 120081117A2421 PCDU BOEING717 717200 1383700NM RIGHT MALFUNCTIONED A ZZDAK NONE H ELECT. POWER LOSS-50 PC APAPPROACH 1 SO37947AT 55010 ON DESCENT LOST RT GEN TRIED ONE RESET - STARTED APU BUS AC BUS TIE WOULD NOT CLOSE. REMOVED AND REPLACED RT PCDU, GEN CONTROL RELAY & EXT PWR MAIN BTR REF AMM 24-21. APU BUS, OPS CHECK GOOD. 2L72 4F TRA6WE 20081203 NM 2008 12 3 ZZDA2008173 120081113A2120 UNKNOWN BOEING737 73776N 13844CHNM CABIN ODOR A ZZDAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 SO37168AT 32653 BURNING RUBBER SMELL VERY STRONG IN AFT CABIN. UPON INITIAL OBSERVATION NO SMOKE, FUMES, OR RUBBER SMELL IN AFT CABIN. ACCOMPLISHED CHECK OF CABIN EQUIPMENT, IFE SYSTEM AT PAX SEATS, RECIRC FANS, LIGHTING, CARGO COMPARTMENTS. PERFORMED VISUAL INSPECTION OF ENGINE INLETS AND EXHAUSTS. NO DEFECT NOTED. CANNOT DUPLICATE BURNING RUBBER SMELL REF FIM 21-00 TASK 806. 2L72 4F RTA16WE 20081203 EA 2008 12 3 VNAA2008111700003120081116A2742 BOLT CNDAIRCL600 CL6002C10 1390015EA HORIZ STAB LOOSE A VNAAK NONE O OTHER ININSP/MAINT 1 GL05718PS 10175 DURING ROUTINE MAINTENANCE ON THE HORIZONTAL STABILIZER TRIM ACTUATOR (HSTA), LOOSE BOLTS WERE FOUND IN THE UPPER BOLT LOCATIONS OF THE UPPER HSTA FITTING ASSEMBLIES (LT AND RT). THE BOLTS WERE RETORQUED TO THE PROPER SPECIFICATION. CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20081203 EA 2008 12 3 MASA2008111600777120081116A3230 PRIORITY VALVE CNDAIRCL600 CL6002B19 1900309EA NLG MALFUNCTIONED A MASAK NONE J WARNING INDICATION CLCLIMB 1 SW0727314 7314 ASH FLT 7263 ABE-ORD. GEAR DISAGREE ON DEPARTURE AND NLG DOOR WARNING. MX REPLACED NLG PRIORITY VALVE. 2L72 4F RTA21EA 20081203 NM 2008 12 3 MASA2008111400774120081114A5210 STRUT DHAV DHC8 DHC8202 2809007NM PAX DOOR BROKEN A MASAK NONE O OTHER NRNOT REPORTED 1 SW07437YV 437 ASH FLT 2896 PHX-DRO. PASSENGER DOOR AFT SUPPORT STRUT BROKEN. MX REMOVED AND REPLACED AFT SUPPORT STRUT. 2H72 4T RTA13NM 20081203 WP 2008 12 3 UPS08853910 120081025A5320 STRUCTURE DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE:SV EVALUATION EFN 70019951018 ORGINIAL NRC 282430. REPAIRED SRM 53-02-03 FIG 6. 2L74 4F RT4A25 20081203 WP 2008 12 3 UPS08853911 120081024A5320 STRUCTURE DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE:SV EVALUATION REPAIR ESN 70019951009 ORIGINAL NRC 282404. REPAIRED DC8 SRM 53-02-03 FIG 6. 2L74 4F RT4A25 20081203 WP 2008 12 3 AALA200810222 120081124A3350 BATTERY PACK DOUG DC9 DC983 3022083WP CABIN UNSERVICEABLE A AALAK NONE O OTHER ININSP/MAINT 1 SW219401W 53137 WITH ELECTRICAL POWER OFF THE EMERGENCY LIGHTS IN THE AFT ACCESSORY BAY ARE ON. TURNING MAIN AIRCRAFT BATTERY SWITCH ON CAUSES LIGHTS TO GO OFF. LIGHT RETURNS ON WHEN BATTERY SWITCH IS OFF. INSTALLED SERVICEABLE 8130 BATTERY PACKS IN B5-27 AND B5-28 POSITIONS, SYSTEM OPERATIONS TESTS GOOD. 2L72 4F RTA6WE 20081203 WP 2008 12 3 AALA200810225 120081108A5320 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 CORROSION ON CUSP BETWEEN STATION 256 TO 275 LEFT SIDE. INSTALLED NEW CUSP MEMBRANE FROM STATION 237 TO 313. 2L72 4F A6WE 20081203 NM 2008 12 3 AALA200810244 120081120A3211 TRUNNION BOEING737 737823 13844BZNM RT MLG CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21948AN 30086 RIGHT MAIN GEAR FORWARD TRUNNION LUG BORE HAS CORROSION AT OUTBOARD LOWER LUG. REPAIRED PER SRM 57-20-90-2R-2. 2L72 4F RTA16WE 20081203 WP 2008 12 3 AALA200810203 120081103A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 CRACKED TANG ON WEB AFT OF THE FWD ENTRY DOOR STATION 208 AT LONGERON 11 LEFT. FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-11. 2L72 4F A6WE 20081203 SO 2008 12 3 CHQA200800231 120081122A2610JEHX0520150B REGULATOR EMB 135 EMB135KL 3260302SO ALLSN AE3007AE3007A 03030GL NR 2 BLEED SYS CLOGGED A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11371SK 145535 CAE311660 FLIGHT 5374, STL TO DSM - DURING CLIMB IN ICING CONDITIONS THE FLIGHT CREW RECEIVED A BLD 2 LOW TEMP MESSAGE ON EICAS SHORTLY AFTER THE ANTI-ICING SYSTEM TURNED ON. THE QRH WAS FOLLOWED AND IT WAS DECIDED TO RETURN TO STL DUE TO WEATHER CONDITIONS AT THE DESTINATION AIRPORT. MAINTENANCE TROUBLESHOT THE FAULT TO A CLOGGED PNEUMATIC REGULATOR FOR THE BLEED 2 THERMOSTAT. THE REGULATOR WAS REPLACED AND THE SYSTEM OPERATED NORMALLY. 2L72 4F4 FRTT00011ATTE6CH 20081203 SO 2008 12 3 CHQA200800228 120081118A3350RPS1B BATTERY PACK EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007A 03030GL CABIN DISCHARGED A CHQAK NONE L NO TEST ININSP/MAINT 1 GL11270SK9494 9494 145304 CAE311866 DURING INSPECTION MAINTENANCE FOUND THAT THE FLOOR EMERGENCY LIGHTS FROM SEATS 7A TO 12A WERE INOPERATIVE WHEN TESTED. 2L72 4T4 FRTT00011ATTE6CH 20081203 EA 2008 12 3 SWIA200820481 120080909A5320 BEAM CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07604SK 10249 DURING C-CHECK, LEFT SIDE OF BEAM AT FS 280 CORRODED. REPAIRED PER REO. 2L72 4F RTA21EA 20081203 EA 2008 12 3 SWIA200820486 120080912A5320 FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07905SW 7437 DURING C-CHECK, FS 280 RBL9 OUTBOARD CLIP CRACKED. REPLACED PER REO. 2L72 4F RTA21EA 20081201 2008 12 1 JGV2008F00003 420081104A256182122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531CE LIFE VEST MISSING B JGVRK NONE W INADEQUATE Q C ININSP/MAINT 1 CE09177JB L782101 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECEIVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPECTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTINE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFORMED. (K) 2L72 4F RTA10CE 20081201 2008 12 1 JGV2008F00002 420081104A256182122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531CE LIFE VEST MISSING B JGVRK NONE W INADEQUATE Q C ININSP/MAINT 1 CE09177JB L782065 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECEIVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPECTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTINE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFORMED. (K) 2L72 4F RTA10CE 20081201 NM 2008 12 1 SWAA086541 120081121A335065C27095 BATTERY PACK BOEING737 7373H4 1384600NM EMERGENCY LIGHT INOPERATIVE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED MV3 CHECK, FOUND L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086542 120081120A575465C2660297 SKIN BOEING737 7373H4 1384600NM NR 2 SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT LOWER T/E WEDGE DELAMINATED. REMOVED AND REPLACED SLAT PER MM. 2L72 4F RTA16WE 20081201 NM 2008 12 1 SWAA086543 120081120A3350PL22300 LIGHT BOEING737 7373H4 1384600NM CABIN WORN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29323SW 23344 DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY LIGHT STRIP WORN BETWEEN ROW 8 TO ROW 13. REMOVED AND REPLACED STRIP PER MM. 2L72 4F RTA16WE 20081201 2008 12 1 USAA BB08170 420081119A2565 BATTERY BOEING767 767201 1385125NM ZONE 200 DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19246AY 23898 CLT - LEFT EMERGENCY ESCAPE SPOILER SQUIB LIGHT FAILED TO ILLUMINATE DURING TEST TWO. MAINTENANCE REPLACED THE LEFT ESCAPE SYSTEM EMERGENCY BATTERY. 2L72 4F RTA1NM 20081201 NM 2008 12 1 USAASB08114 120081119A3397 WIRE BOEING737 7373G7 138447JNM CABIN BROKEN A USAAK NONE L NO TEST ININSP/MAINT 1 EA19154AW 23776 PHX - SEAT TWO, LEFT FORWARD ESCAPE PATH LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONALLY CHECKS OK. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA2008112092094120081119A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM CABIN FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19816AW3134317067 1350 FLT 548 - PHX-DFW - EEL - EMERGENCY BATTERY PACK FAULTING ON LEFT OVERWING EMERGENCY EXIT LOCATION 11WL. REMOVED AND REPLACED POWER SUPPLIES 11WL AND 12WL. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20081201 NM 2008 12 1 USAA2008112192101120081119A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM CABIN FAULTY A USAAK NONE O OTHER ININSP/MAINT 1 EA19816AW283391443 1350 FLT 548 - PHX-DFW - EEL - EMERGENCY BATTERY PACK FAULTING ON LEFT OVERWING EMERGENCY EXIT LOCATION 11WL. REMOVED AND REPLACED POWER SUPPLIES 11WL AND 12WL. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20081201 NM 2008 12 1 USAA2008111992089120081116A552365C2638428 TRIM TAB BOEING737 7374B7 138449CNM RT ELEVATOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - RON - MAJOR REPAIR - RIGHT ELEVATOR TRIM TAB HAS CRACKS COMING FROM HINGE CUTOUTS (2 PLACES). REPLACED RIGHT ELEVATOR TRIM TAB IAW US AIRWAYS TASK CARD 03C71227004. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA2008111992090120081116A552365C2638427 TRIM TAB BOEING737 7374B7 138449CNM LT ELEVATOR CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19439US 24781 CLT - RON - MAJOR REPAIR - LEFT ELEVATOR TRIM TAB DELAMINATED AT NR 2 HINGE CUTOUT AREA AND HAS CRACKS AT THE NR 1 HINGE CUTOUT. REPLACED LEFT ELEVATOR TRIM TAB IAW US AIRWAYS TASK CARD 03C71127007. 2L72 4F RTA16WE 20081201 EU 2008 12 1 USAA920082066 120081116A335032145410 POWER SUPPLY AIRBUS320 A320214 3930316EU CABIN FAILED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19123UW265083581 1310 LOG PAGE 4440750 FLT NR 1145 PHL-SAN EEL L3 EMERGENCY LIGHT POWER SUPPLY FAILED OPS CHECK. MX R&R THE L3 EMERGENCY POWER SUPPLY UNIT. OPS CHECK WAS GOOD. 2L72 4F RTA28NM 20081201 EU 2008 12 1 USAA920082067 120081114A3350321454 POWER SUPPLY AIRBUSA319 A319112 3930323EU CABIN FAULTY A USAAK NONE L NO TEST ININSP/MAINT 1 EA19746UW 1297 LOG PAGE 4394365 FLT NR 1458 PIT-CLT EEL DURING EMERGENCY LIGHT TEST CFDS FAULT MSG EMERGENCY POWER SUPPLY UNIT BATTERY FORWARD LT. R&R BATTERY. OPS TEST WAS GOOD. 2L72 4F RTA28NM 20081201 NM 2008 12 1 USAA920082040 120081023A532065C10592146 INTERCOSTAL BOEING737 737301 1384611NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19574US 23739 CLT Q3 MAJOR REPAIR NR 03C10853028/025 LEVEL 2 EXFOLIATION CORROSION ON INTERCOSTAL AT BS964, BETWEEN RBL25 TO RBL8. REPLACED INTERCOSTAL AT BS964, BETWEEN RBL25 TO RBL8 IAW B737 SRM 53-60-15. 2L72 4F RTA16WE 20081201 WP 2008 12 1 NWAA084979862 120081109A3397 CONNECTOR DOUG DC9 DC951 3022051WP CABIN LOOSE A NWAAK NONE L NO TEST ININSP/MAINT 1 GL01771NC 47769 DURING LINE CHECK MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-18 OF THE CABIN WERE INOPERATIVE. MX CORRECTED A LOOSE CONNECTION AND THEN OPS CHECKED THE SYSTEM. 2L72 4F RTA6WE 20081202 NM 2008 12 2 USAASB08115 120081122A27512061141 INDICATOR BOEING737 7374B7 138449CNM COCKPIT FAULTY A USAAL ABORTED APPROACH F FLT CONT AFFECTED APAPPROACH 1 EA19460UW2054 1575 25024 CREW REPORTED A SPLIT FLAP CONDITION WHEN EXTENDING FLAPS FROM 10 TO 15 UNITS. AFTER GO-AROUND, FLAPS CORRECTED TO NORMAL. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT CLT. CLT MAINTENANCE REMOVED AND REPLACED THE TRAILING EDGE FLAP POSITION INDICATOR PER MM 27-58-41. ACCOMPLISHED SATISFACTORY FLAP ASYMMETRY CHECK AND TEST OF THE TRAILING EDGE POSITION INDICATION SYSTEM. 2L72 4F RTA16WE 20081203 EA 2008 12 3 SWIA200820487 120080912A5320 FITTING CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 DURING C-CHECK, FS 280 RBL9 INBOARD AND OUTBOARD CLIPS CRACKED. REPLACED PER SRM. 2L72 4F RTA21EA 20081203 EA 2008 12 3 SWIA200820488 120080912A5320 FLOOR SUPPORT CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 DURING C-CHECK, FS 280 RBL9 UPPER FLOOR SUPPORT CRACKED. REPAIRED PER REO. 2L72 4F RTA21EA 20081203 EA 2008 12 3 SWIA200820489 120080912A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07903SW 7425 DURING C-CHECK, FS 621 BULKHEAD WEB CRACKED ABOVE LINTEL FITTING. REPAIRED PER REO. 2L72 4F RTA21EA 20081203 EA 2008 12 3 SWIA200820491 120080913A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07471CA 7655 DURING C-CHECK, LEFT AND RIGHT OBLIQUE ANGLES AT FS 625 CRACKED. REPLACED PER SRM. 2L72 4F RTA21EA 20081203 EA 2008 12 3 SWIA200820494 120080913A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA RT WING CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07471CA 7655 DURING C-CHECK, RIGHT WING PLANK AT WS 136 HOLE NR 8 CORRODED. REPAIRED PER REO. 2L72 4F RTA21EA 20081203 EA 2008 12 3 SWIA200820497 120080913A7120 FITTING CNDAIRCL600 CL6002B19 1900309EA LT ENGINE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07471CA 7655 DURING C-CHECK, LEFT ENGINE AFT THRUST FITTING CORRODED. REPLACED PER AMM. 2L72 4F RTA21EA 20081203 EA 2008 12 3 SWIA200820499 120080919A3213 TORQUE LINK CNDAIRCL600 CL6002C10 1390015EA RT MLG CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM07716SK 10180 DURING C-CHECK, RIGHT MLG OUTER CYLINDER UPPER TORQUE LINK CORRODED. REPAIRED PER CMM. 2L72 4F RTA21EA 20081203 WP 2008 12 3 AALA200810210 120081104A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 SUB FLOOR WEB CORRODED, STATION 160-200, JUST INBOARD OF THE FORWARD SERVICE DOOR. INSTALLED DOUBLER STATION 160-200 PER AARD 53-20-00-16. 2L72 4F A6WE 20081203 WP 2008 12 3 AALA200810212 120081105A5320 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 CRACK IN CUSP MEMBRANE STATION 219 UNDER SEAT TRACK NUMBER 5. FABRICATED AND INSTALLED DOUBLER. 2L72 4F A6WE 20081203 WP 2008 12 3 AALA200810213 120081105A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE SEPARATED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 FUSELAGE SKIN SEPARATED AT BOTTOM FORWARD CORNER OF THE AFT LAVATORY SERVICE PANEL. INSTALLED DOUBLER ON BOTTOM HALF OF SKIN AT AFT LAVATORY SERVICE PANEL CUT-OUT PER ESO 80559 DATED 11/05/2008. 2L72 4F A6WE 20081203 WP 2008 12 3 AALA200802738 120081015A335060030451 BATTERY PACK DOUG DC9 DC982 3022082WP CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21427AA 49339 LGA - EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT LEFT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. 2L72 4F A6WE 20081203 NM 2008 12 3 KCSA081603 120081129A5315 FLOORBEAM BOEING747 747249F 1384849NM FUSELAGE CRACKED A KCSAK NONE O OTHER ININSP/MAINT 1 GL23706CK 21827 STA 330 FLOORBEAM WEB CRACKED 3.5 INCHES AT LBL 63. 2L74 4F RTA20WE 20081203 NM 2008 12 3 KCSA081589 120081118A5730 SKIN BOEING747 747212B 1384886NM LT WING CORRODED A KCSAK NONE O OTHER ININSP/MAINT 1 GL23708CK 21937 LT WING UPPER SURFACE ILES-472 AT L/E RIB HAS CORROSION. 2L74 4F RTA20WE 20081203 NM 2008 12 3 KCSA081597 120081120A5414 SKIN BOEING747 747212B 1384886NM NR 1 PYLON CHAFED A KCSAK NONE O OTHER ININSP/MAINT 1 GL23708CK 21937 NR 1 PYLON HAS CHAFING ON O/B SKIN UPPER SURFACE AT NAC STA-215 TO 220. 2L74 4F RTA20WE 20081203 NM 2008 12 3 KCSA081598 120081120A5210 WEB BOEING747 747212B 1384886NM L5 DOOR CORRODED A KCSAK NONE O OTHER ININSP/MAINT 1 GL23708CK 21937 L-5 DOOR INNER WEB CORRODED STA 2226. 2L74 4F RTA20WE 20081203 NM 2008 12 3 KCSA081601 120081121A5311 FRAME BOEING747 747212B 1384886NM FUSELAGE DAMAGED A KCSAK NONE O OTHER ININSP/MAINT 1 GL23708CK 21937 FORWARD BILGE FUSELAGE FRAME IS DAMAGED AT STA 820, RBL 27. 2L74 4F RTA20WE 20081203 NM 2008 12 3 KCSA081591 120081118A3350 SIGN BOEING747 747122 1384872NM CABIN INOPERATIVE A KCSAK NONE L NO TEST ININSP/MAINT 1 GL23712CK 19754 EMERGENCY EXIT SIGN ABOVE UPPER DECK ESCAPE DOOR INOP. 2L74 4F RTA20WE 20081203 NM 2008 12 3 KCSA081599 120081120A5414 SKIN BOEING747 747212B 1384886NM NR 4 PYLON WORN A KCSAK NONE O OTHER ININSP/MAINT 1 GL23708CK 21937 NR 4 PYLON LOWER EDGE SKIN ON I/B AT NAC STA 180 TO 220 SIDE IS WORN. 2L74 4F RTA20WE 20081203 NM 2008 12 3 KCSA081590 120081118A5313 STRINGER BOEING747 747212B 1384886NM FUSELAGE DENTED A KCSAK NONE O OTHER ININSP/MAINT 1 GL23708CK 21937 STR 49R AT STA 2614 DENTED. 2L74 4F RTA20WE 20081203 NM 2008 12 3 KCSA081608 120081202A5411 RIB BOEING747 747212B 1384886NM NR 2 NACELLE CRACKED A KCSAK NONE O OTHER ININSP/MAINT 1 GL23708CK 21937 NR 2 NAC STA 211 I/B RIB CRACKED 1 INCH, BELOW MIDSPAR. 2L74 4F RTA20WE 20081204 SO 2008 12 4 C2XA08RI171 120081111A2120 UNKNOWN EMB 145 EMB145XR 3260214SO GALLEY SMOKE A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SW2711194 14500940 FLIGHT 2756 - EWR - FLIGHT ATTENDANT AND PASSENGER IN SEAT 2A REPORTED WHAT THEY THOUGHT WAS SMOKE COMING FROM AFT TRASH BIN IN GALLEY. FLIGHT ATTENDANT DISCHARGED HALOGEN FIRE EXTINGUISHER INTO BIN AND PASSENGERS WERE EVACUATED. EWR MX INSPECTED THE AREA NO SIGNS OF BURNING OR SMOKE FOUND. MX REMOVED AND REPLACED FIRE EXTINGUISHER. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RT 20081204 SO 2008 12 4 C2XA08CL125 120081129A323221180100401 ACTUATOR EMB 145 EMB145LR 3260212SO NLG DOOR FAULTY A C2XAK NONE J WARNING INDICATION DEDESCENT 1 SW271292219584 145338 CLE - FLIGHT 2775 - THE CREW REPORTED A LANDING GEAR LEVER DISAGREE MESSAGE ON THE EICAS AFTER SELECTING GEAR DOWN. THE MESSAGE CLEARED IMMEDIATELY AND NO OTHER INDICATIONS WERE NOTICED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT NOSE GEAR DOOR ACTUATOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20081204 NE 2008 12 4 COMA2008111970002220081119A7230 FAN BLADE CNDAIRCL600 CL6002C10 1390015EA GE CF34 CF348C1 30049NE LT ENGINE DEFECTIVE A COMAA UNSCHED LANDING E VIBRATION/BUFFET CRCRUISE 1 SO27369CA 10079 965504 EN ROUTE ATL-MKE THE LEFT ENGINE VIBRATION INDICATION REACHED 1.8 AMBER, REDUCED THRUST TO INDICATE GREEN. CREW DIVERTED TO MKE AND LANDED WITHOUT INCIDENT. REPLACED ALL FAN BLADES ON THE LEFT ENGINE. 2L72 4F4 FRTA21EA E00063EN 20081204 NM 2008 12 4 UPS08M53895 120081110A5720 DOUBLER DOUG MD11 MD11F 3023600NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01254UP 48406 INSPECTION TYPE:1C RT WING FIXED L/E COMPT AT XORS 506 HAS CRACK 4 EA AROUND FASTENERS HOLE ON BEADED DOUBLER. REMOVED DAMAGE, FABRICATED FILLER, ANGLES, AND DOUBLER, AND INSTALLED IAW MD-11 SRM 57-10-00 VOL 1 FIG 2. 2L73 4F RTA22WE 20081204 NM 2008 12 4 UPS08M53916 120081113A71602242101567 ACOUSTIC PANEL DOUG MD11 MD11F 3023600NM NR 1 ENGINE DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01254UP 48406 INSPECTION TYPE:1C 2 EA DENTS AT 6 O'CLOCK POSITION 6 INCHES AND 18 INCHES FROM NOSE LIP IN NR 1 ENG INLET ACOUSTIC PANEL. REMOVED DAMAGE, FABRICATED AND INSTALLED PLUGS AND APPLIED FIBERGLASS IAW MD-11 SRM 54-10-00 REPAIR 18 STEPS C-F AND G-O. 2L73 4F RTA22WE 20081204 EU 2008 12 4 UPS08153919 120081029A5751A57661001179 AILERON AIRBUSA300 A300F4622R 3930360EU RT WING DENTED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01142UP 0825 INSPECTION TYPE:1C3C RT WING ALL SPEED AILERON UPPER T/E NUMEROUS DENTS. REPAIRED RT WING ASA UPPER T/E REF EO C-5750-31147-A AND EA 300- 5751-01-A1554. 2L72 4F RTA35EU 20081204 WP 2008 12 4 UPS08853925 120081106A5730 SKIN DOUG DC8 DC871F 302199DWP LT WING DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE:SV LT WING LEADING EDGE AT STA 700 DOES NOT HAVE REPAIR DOUBLER INSTALLED AS PER APPENDIX H (3)(4) OF EO DC8 5100 30418. INSTALLED DOUBLER AS IAW 57-02-01 FIG 38 2L74 4F RT4A25 20081204 NE 2008 12 4 UPS08B53921 220081114A7321 HMU BOEING747 74745E 1384947NM GE CF6 CF680C2B2 30025NE NR 1 ENGINE MALFUNCTIONED A IPXAO OTHER XJ ENGINE FLAMEOUT WARNING INDICATION APAPPROACH 1 SO01579UP 26062 704664 INSPECTION TYPE:N/A ENG NR 1 FAILURE ON FINAL WITH SUCCESSFUL AUTO RELIGHT. NR 1 FAILED AGAIN ON GROUND WITH ENG 1 CONTROL MESSAGE. WIND ON FINAL APPROACH TO 26L WAS OUT OF NORTH UP TO 50 KNOTS. REMOVED AND REPLACED NR 1 ENG HMU IAW MM 73-21-14, REMOVED AND REPLACED ECU IAW MM 73-21-15. REF Q141548 & K141559. OPS CK GOOD. 2L74 4F4 FRTA20WE E13NE 20081204 NM 2008 12 4 UPS08M53926 120081109A5330ADA70301 DOUBLER DOUG MD11 MD11F 3023600NM FUSELAGE GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01254UP 48406 INSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-004 OF MD11-5100-30530 APPENDIX C SECTION C ITEM 3, FOUND 2 GOUGES ON FWD EDGE OF DOUBLER REPAIR STA 999 L-39R- L-42R. REMOVED PREVIOUS REPAIR DOUBLER, FABRICATED, AND INSTALLED NEW REPAIR DOUBLER 1 AND REPAIR DOUBLER 2 IAW MD11 SRM 53-50-00 VOL 1 FIGURE 17 SHEETS 1-5. 2L73 4F RTA22WE 20081204 NM 2008 12 4 UPS08M53927 120081106A5712 ATTACH FITTING DOUG MD11 MD11F 3023600NM LT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01254UP 48406 INSPECTION TYPE:1C LT WING AT STA XORS 562 FIXED L/E RIB ATTACH STRAP CRACKED. REMOVED, FABRICATED, AND INSTALLED STRAP IAW MD11 SRM 51-33-01 AND DWG ARB3954. 2L73 4F RTA22WE 20081204 NM 2008 12 4 UPS08M53934 120081116A3350 LIGHT DOUG MD11 MD11F 3023600NM CABIN INOPERATIVE A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01296UP 48474 INSPECTION TYPE:N/A EMERGENCY LIGHTING SYSTEM INOP. PERFORMED ADJUSTMENT / TEST IAW 33-50-00-5. SYSTEM OPERATIONAL TEST CHECKED GOOD. THIS CLEARS M388756. 2L73 4F RTA22WE 20081204 NM 2008 12 4 UPS08M53936 120081116A33506044115 BATTERY PACK DOUG MD11 MD11F 3023600NM COCKPIT DISCHARGED A IPXAK NONE L NO TEST ININSP/MAINT 1 SO01295UP 48475 INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP. REMOVED & REPLACED EMERGENCY LIGHTS BATTERY PACK IN REF TO MD11 MM 33 51, NO HELP. CYCLED C/B B1-382 SYSTEM. OPS OK PER AMM 33 51 01. 2L73 4F RTA22WE 20081202 EU 2008 12 2 USAASB08116 220081123A7230 COMPRESSOR BOEING737 7374B7 138449CNM CFMINTCFM56 CFM563B2 13802EU LT ENGINE LEAKING A USAAO OTHER J WARNING INDICATION TOTAKEOFF 1 EA19430US 24552 ON TAKEOFF FROM ORD, EN ROUTE TO CLT, CREW REPORTED A STRONG ODOR WITH SMOKE DETECTORS SOUNDING OFF. NO VISUAL INDICATION OF SMOKE WAS NOTED. FLIGHT LANDED WITHOUT FURTHER INCIDENT AT CLT. CLT MAINTENANCE FOUND OIL RESIDUE IN APU DISTRIBUTION DUCT. CLEANED AND BURNED OUT SMELL. ALSO, DUE TO AIRCRAFT HISTORY FOR STRONG ODORS, CLT MAINTENANCE BOROSCOPED THE NR 1 ENGINE FOR OIL IN THE HPC STAGES 1-3 PER MM 71-00-00-6. OIL WAS FOUND IN THE HPC STAGES 1-3. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE PER JOB CARD. OPERATIONAL CHECK AND LEAK CHECK GOOD. 2L72 4F4 FRTA16WE E21EU 20081202 NM 2008 12 2 USAA2008112492112120081106A5315BAC1518399 FLOORBEAM BOEING737 7373G7 138447JNM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19307AW 24634 SAL - C17 - MAJOR REPAIR - CORROSION ON FLOORBEAM AT BS 986.5 BETWEEN RBL 43 TO LBL 8. REPLACED FLOORBEAM AT BS 986.5 BETWEEN RBL 43 TO LBL 8 IAW B737 SRM 53-00-51 2R2. 2L72 4F RTA16WE 20081202 NM 2008 12 2 USAA2008112492116120081122A533065C32355 SKIN BOEING737 7374B7 138449CNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - C1 - MAJOR REPAIR - CRACK ON FUSELAGE SKIN AT BS 484.5, S1R. REPAIRED FUSELAGE SKIN AT BS 484.5, S1R IAW B737 SRM 53-00-01. 2L72 4F RTA16WE 20081202 NM 2008 12 2 USAA2008112492117120081121A57526546845521 TAB BOEING737 7374B7 138449CNM AILERON DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19442US 24841 CLT - C1 - MAJOR REPAIR - LEFT AILERON TAB DISBONDED ON LOWER SIDE 1.5 INCHES FROM OUTBOARD END AND 1 INCH FROM TRAILING EDGE. REPLACED LEFT AILERON TAB IAW US AIRWAYS TASK CARD 03I30627002L. 2L72 4F RTA16WE 20081202 EA 2008 12 2 SIMA200833602 220081125A7200 ENGINE EMB 135 EMB135KL 3260302SO RROYCEAE3007AE3007A1 54165EA NR 1 SMOKE A SIMAC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 SW21830AE 162 145615 CAE311351 ON FLIGHT 4553, AFTER 80 KTS ON TAKEOFF ROLL COCKPIT BECAME HAZY WITH SMOKE ACCOMPANIED BY ODOR. ABORTED TAKEOFF. SMOKE DISSIPATED FAIRLY RAPIDLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. 2L72 4F4 FRTT00011ATTE6CH 20081202 CE 2008 12 2 DXTA2008112403366120081122A3150 WARNING LIGHT RAYTHNDH125 HAWKER800XP 7150012CE NR 1 COMPUTER ILLUMINATED E DXTAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 GL07893QS 258393 NR 1 COMPUTER LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROX 60KTS. ABORTED TAKEOFF. 2L72 4F RTA3EU 20081202 2008 12 2 SIMA200832901 420081123A3420 DISPLAY EMB 145 EMB145LR 3260212SO COCKPIT MALFUNCTIONED A SIMAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 SW21630AE 145132 ON FLIGHT 4286, DURING DESCENT CREW RECEIVED A PFD FAILED MESSAGE FOLLOWED BY SLIGHT ELECTRICAL BURNING ODOR. CREW PULLED PFD NR 1 CB AND ODOR SLOWLY EXTINGUISHED. ACFT REMOVED FROM SERVICE, ISSUED MEL 34-01. REMOVED AND REPLACE NR 1 PFD IAW EMB-145 MM 34-22-01. OPERATIONAL CHECK GOOD MEL ITEM RESTORED. AIRCRAFT RETURNED TO SERVICE. 2L72 4T RTT00011AT 20081202 WP 2008 12 2 IXXA08SMN186S 120080605A5310 FINGER DOUBLER DOUG DC8 DC871F 302199DWP ZONE 700 CORRODED A IXXAK NONE O OTHER ININSP/MAINT 1 SW11823BX918102850 46064 DURING ROUTINE D CHECK INSPECTION, FOUND TOP SURFACE OF MAIN LANDING GEAR WHEEL WELL PRESSURE PANEL FINGER DOUBLER CORRODED AT STATION 941.000 TO STATION 958.000 LEFT BOTTOM LINE 5 TO RIGHT BOTTOM LINE 5. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FINGER DOUBLER. FABRICATED FINGER DOUBLER. CLEANED TREATED AND PRIMED AREA AND FINGER DOUBLER. INSTALLED NEW FINGER DOUBLER IAW SRM 51-1-21, SRM 51-1-8 PAGES 17-18, SRM 53-2-0 PAGE 2P, SRM 51-1-21, SRM 53-7-1 PAGE 21 FIGURE 10, AND SRM 51-1-8B. 2L74 4F RT4A25 20081202 WP 2008 12 2 IXXA08SMN182S 120080419A5330 SKIN DOUG DC8 DC871F 302199DWP ZONE 100 MISREPAIRED A IXXAK NONE W INADEQUATE Q C ININSP/MAINT 1 SW11821BX888782984 45811 DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 1694 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8100-9 DATED 05-09-08, AD 2007-02-02, SB DC8-53A080 DATED 06-22-04, DRAWING SR08530032, MESSAGE 1-819144906-11 DATED 05/07/08, 1-819144906-13 DATED 05-05-08, AND DRAWING ED-4754 DATED 05-10-08. 2L74 4F RT4A25 20081202 EA 2008 12 2 MALA080197 120081123A3350 BATTERY PACK CNDAIRCL600 CL6002D24 1390016EA EMERGENCY LIGHTSINOPERATIVE A MALAO OTHER O OTHER CRCRUISE 1 GL15933XJ 15196 CABIN EMERGENCY LIGHTS CYCLING INTERMITTENTLY DURING FLIGHT. REPLACED BATTERY AND RELAY. 2L72 4F RTA21EA 20081202 EU 2008 12 2 USAA2008120192160120081128A3350 LIGHT AIRBUS320 A320232 3930326EU CABIN INOPERATIVE A USAAK NONE L NO TEST NRNOT REPORTED 1 EA19642AW 584 FLT 687 PHX-EWR - EEL - LAV D ALL LIGHTS INOPERATIVE INCLUDING EMERGENCY LIGHTS. CYCLED LAV POWER SWITCH ON FORWARD ATTENDANT PANEL WITH NO HELP. MAINTENANCE RELAMPED LIGHTS AND RECONNECTED MIRROR LIGHT CONNECTOR. OPERATIONAL CHECK GOOD. 2L72 4F RTA28NM 20081202 EU 2008 12 2 USAA2008112892154120081114A5320D53471124200 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1340. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1340 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20081202 NM 2008 12 2 UALA2008112106606120081120A5311 FRAME BOEING757 757222 1384956NM PWA 2037 PW2037 NE FUSELAGE DENTED A UALAK NONE O OTHER ININSP/MAINT 1 WP29552UA 26641 AFT PIT AT STA 1500, STR 26L FRAME DENTED AT INBOARD FLANGE. MAJOR REPAIR ACCOMPLISHED. INSTALLED FRAME REPAIR. 2L72 4F4 FRTA2NM E17NE 20081202 NM 2008 12 2 UALA2008112106608120081121A3510MC1019101 OXYGEN MASK BOEING757 757222 1384956NM PWA 2037 PW2037 NE COCKPIT DEFECTIVE A UALAO OTHER W INADEQUATE Q C ININSP/MAINT 1 WP29564UA 26666 PILOTS O2 MASK HAS DEFECTIVE AIRFLOW. REPLACED MASK & OP CHECKS OK. 2L72 4F4 FRTA2NM E17NE 20081202 WP 2008 12 2 NWAA084959867 120081106A3397 CONNECTOR DOUG DC9 DC951 3022051WP EMERGENCY LIGHT LOOSE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01776NC 47786 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FROM ROWS 22 AND AFT WERE INOPERATIVE. MX FOUND AND CORRECTED A LOOSE CONNECTION AND THEN OPS CHECKED THE SYSTEM. 2L72 4F RTA6WE 20081201 NM 2008 12 1 USAA2008111992091120081118A5315 SUPPORT ANGLE BOEING767 7672B7ER 1385107NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19253AY 24894 BFM - C4 - MAJOR REPAIR - FLOORBEAM SUPPORT ANGLE CRACKED AT BS 287, LBL 82. REPAIRED FLOORBEAM SUPPORT ANGLE AT BS 287, LBL 82 IAW B767 SRM 51-40-02. 2L72 4F RTA1NM 20081204 NM 2008 12 4 K11A2008120372213120080808A5310 WINDOW POST BOEING727 7272H3 138368NNM FUSELAGE CRACKED A K11AK NONE O OTHER UKUNKNOWN 1 GL23722CK 20948 THE E-H WINDOW POST CRACKED 4 INCHES ABOVE LOWER CORNER. 2L73 4F RTA3WE 20081204 NM 2008 12 4 R61A20080049 120080401A5311 FRAME EMB ERJ170ERJ170100SU 3260403NM FUSELAGE DAMAGED A R61AK NONE O OTHER ININSP/MAINT 1 GL11802MD 17000013 DENT/SCATCH ON FUSELAGE FRAME 32 TO 34. PERFORMED MAJOR REPAIR PER EMBRAER ENGINEERING INSTRUCTION. 2L72 4F RTA56NM 20081204 WP 2008 12 4 UPS08853945 120081010A5330 SKIN DOUG DC8 DC871F 302199DWP FUSELAGE MISREPAIRED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01702UP 45902 INSPECTION TYPE:SV FUSELAGE SKIN REPAIR AT BS 55- BS61 L25R-L26R DOES NOT MEET SRM CRITERIA REF UPS EO REPAIR EVAL SURVEY SEQ 702-F1-11. REPAIRED DC SRM 53-203 AND SRM 53-2-0 FIG 7 SHT 5. 2L74 4F RT4A25 20081204 NM 2008 12 4 UPS08M53930 120081116A5210ACA3822511V DOUBLER DOUG MD11 MD11F 3023600NM NR 2 DOOR MISREPAIRED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01254UP 48406 INSPECTION TYPE:1C SURVEY SEQUENCE NUMBER 254-F1-002 OF MD11-5100-30530 APPENDIX E SECTION D REPAIR DOES NOT CONFORM TO MD11 VOL 1 SRM 52-00-01 FIG 4 SHEET 2. REMOVED EXTERNAL DOUBLER, FABRICATED AND INSTALLED 1 EXTERNAL DOUBLER 1 INTERNAL DOUBLER, AND 1 FILLER IAW MD11 SRM 52-10-00 VOL 1 FIG 1. 2L73 4F RTA22WE 20081204 NM 2008 12 4 R61A20080040 120081117A27811702288A SENSOR EMB ERJ170ERJ170100SU 3260403NM LE SLAT DEFECTIVE A R61AO OTHER N FALSE WARNING APAPPROACH 1 GL11806MD8344 17000019 CREW REPORTED SLAT FAIL/AOA LIMIT FAIL ON FINAL APPROACH, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT HAND OUTBOARD SKEW SENSOR AND COMPLETED OPERATIONAL CHECK SYSTEM OPERATIONAL CHECK GOOD AND A/C WAS RETURNED TO SERVICE. 2L72 4F RTA56NM 20081204 NM 2008 12 4 R61A20080041 120081113A2780 SLAT EMB ERJ170ERJ170200LR 3260121NM WING MALFUNCTIONED A R61AO OTHER J WARNING INDICATION APAPPROACH 1 GL11106HQ 17000164 CREW REPORTED SLAT/FLAP FAIL MESSAGE ON EICAS. CREW DECLARED AN EMERGENCY, FOLLOWED QRH PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT TROUBLESHOT CLEARED INHIBITS AND COMPLETED AND OPERATIONAL CHECK, SYSTEM CHECK GOOD. RETURNED A/C TO SERVICE. 2L72 4F RTA56NM 20081204 NM 2008 12 4 R61A20080042 120081113A2782 ACTUATOR EMB ERJ170ERJ170200LR 3260121NM LE SLAT MALFUNCTIONED A R61AO OTHER O OTHER APAPPROACH 1 GL11106HQ 17000164 CREW REPORTED FLAP/SLAT FAIL ON APPROACH. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 2 AND NR 3 ACTUATOR TRIPPED. MAINTENANCE RESET ACTUATORS AND SYSTEM OPERATIONAL CHECK COMPLETED, SYSTEM OPERATIONAL CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA56NM 20081204 NM 2008 12 4 UPS08M53946 120081117A5730ARB2886503 SKIN DOUG MD11 MD11F 3023600NM RT WING CRACKED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01254UP 48406 INSPECTION TYPE:1C RT WING ON TELESCOPIC ANTI-ICE DUCT AT SLAT NR 3 HAS CRACK ON DOOR CUTOUT UPPER LEFT CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD11 VOL 1 SRM 57-10-00 FIG 43. 2L73 4F RTA22WE 20081203 WP 2008 12 3 AALA200810202 120081103A5320 STRAP DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21954U 49426 TEE STRAP CRACKED STATION 207 AT LONGERON 11 LEFT. FABRICATED AND INSTALLED DOUBLER PER AARD 53-10-00-011. 2L72 4F A6WE 20081203 NM 2008 12 3 R61A20080039 120081113A2752 LIMITER EMB ERJ170ERJ170200LR 3260121NM FLAP ACTUATOR TRIPPED A R61AO OTHER J WARNING INDICATION DEDESCENT 1 GL11106HQ 17000164 CREW REPORTS ON DESCENT AT FLIGHT LEVEL 7000 FEET CREW RECEIVED A FLAP FAIL MESSAGE FOLLOWED QRH PROCEDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO AIRCRAFT TROUBLESHOT. FOUND NR 2 LEFT AND NR 3 RIGHT ACTUATOR TORQUE LIMITER TRIP PINS TRIPPED. RESET PINS, OPERATIONAL CHECK WAS GOOD. ALSO PERFORMED FLAP LUBE, RETURNED AIRCRAFT TO SERVICE. 2L72 4F RTA56NM 20081203 EA 2008 12 3 MASA2008111400773120081114A5270 PROXIMITY SENSOR CNDAIRCL600 CL6002D24 1390016EA EMERGENCY EXIT DIRTY A MASAK NONE N FALSE WARNING NRNOT REPORTED 1 SW07923FJ 15023 ASH FLT 2719 PHX-SBA. LT AFT EMERGENCY DOOR CAUTION MESSAGE INTERMITTENT. MX CLEANED PROXIMITY SENSOR. 2L72 4F RTA21EA 20081203 WP 2008 12 3 UPS08853908 120081025A5347 SEAT TRACK DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE:SV EVALUATION REPAIR EFN 70019951020 TRACK 8 AFT END COMPARTMENT 2. REPAIRED TRACK SPLICE AT STA 338 SRM 53-02-03 FIG 6. 2L74 4F RT4A25 20081203 WP 2008 12 3 UPS08853909 120081025A5320 STRUCTURE DOUG DC8 DC871F 302199DWP FUSELAGE DAMAGED A IPXAK NONE O OTHER ININSP/MAINT 1 SO01700UP 45900 INSPECTION TYPE:SV EFN 7001199510 NEEDS EVALUATION ORGINIAL NRC 282432. REPAIRED IAW DC8 SRM 53-02-03 FIG 6. 2L74 4F RT4A25 20081203 SO 2008 12 3 CHQA200800226 120081118A2750 FLAP EMB 135 EMB135LR 3260305SO ALLSN AE3007AE3007A 03030GL WING FAILED A CHQAO OTHER J WARNING INDICATION APAPPROACH 1 GL11840RP 145725 CAE311921 FLIGHT 6054, CMH TO LGA - ON APPROACH, FLAPS 9 WERE SELECTED AND CREW RECEIVED A FLAP FAIL MESSAGE AND FLAPS REMAINED AT ZERO. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RESET POWER TO THE FLAP SYSTEM AND THE FLAPS OPERATED NORMALLY. 2L72 4F4 FRTT00011ATTE6CH 20081203 SO 2008 12 3 C2XA08RI169 120081110A2611FAU751A4 PANEL EMB 145 EMB145XR 3260214SO SMOKE DETECTION DEFECTIVE A C2XAK NONE N FALSE WARNING CLCLIMB 1 SW2714204 14500968 FLIGHT 2761 - EWR - FLIGHT CREW REPORTED LAV SMOKE INDICATION ON EICAS DURING CLIMBING, BUT NO SMOKE NOTICED. EWR MX REMOVED AND REPLACED LAV SMOKE DETECTION PANEL AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. MX ALSO PERFORMED BORESCOPE INSPECTION THROUGH ENGINE INLET AND NO OIL NOR WETNESS NOTICED. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RT 20081203 SO 2008 12 3 C2XA08TY135 120081126A335082301 SIGN EMB 145 EMB145 3260210SO CABIN INOPERATIVE A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2726545 145558 FWD CEILING EXIT LIGHT LOCATOR SIGN IS NOT FULLY LIT. REMOVED AND REPLACED FWD EXIT LOCATOR SIGN ASSEMBLY IAW EMB 145 AMM 33-50-15. OPS CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE. 2L72 4F RTT00011AT 20081201 2008 12 1 JGV2008F00005 420081104A256182122Z CARTRIDGE AIRCRUISERS LEAR 35 31A 5170531CE LIFE VEST MISSING B JGVRK NONE W INADEQUATE Q C ININSP/MAINT 1 CE09177JB L782066 161 DURING ROUTINE INSP OF NINE (9) LIFE VESTS FOUND MISSING CO2 CARTRIDGES ON ALL NINE (9) VESTS. ALL LIFE VESTS WERE RECEIVED IN SEALED, SEWN-SHUT BAGS WITH SIGNED MAINT RELEASE DOCUMENTS FROM PREVIOUS INSP ACCOMPANYING THEM. PREVIOUS INSPECTION ACCOMPLISHED NOVEMBER 2003. CO2 CARTRIDGES ARE NORMALLY REMOVED FOR WEIGHT CHECK AND REINSTALLED AS PART OF ROUTINE INSPECTION REQUIREMENTS. PROBABLE CAUSE FOR FAILURE TO RE-INSTALL IS LAPSE OF FOCUS ON DETAILS OF MAINT BEING PERFORMED. (K) 2L72 4F RTA10CE 20081201 NM 2008 12 1 DU4R2008264 120081123A5711111A1141 REPAIR BOEING737 737800* NM LT WING CRACKED B DU4RK NONE O OTHER ININSP/MAINT 1 SO15171LF 30637 DURING SCHEDULED INSPECTION, FOUND A TEMPORARY REPAIR AT LBL 33 AND LBL 41 CRACKED AND REQUIRING REPAIR. 2L72 4F RTA16WE 20081201 NM 2008 12 1 USAA2008112092096120081114A5320 FLOOR SUPPORT BOEING767 7672B7ER 1385107NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19253AY 24894 BFM - C4 - MAJOR REPAIR - CABIN FLOOR SUPPORT INBOARD ANGLE IS CRACKED IN HALF AT BS 303, RBL 54.75. REPAIRED CABIN FLOOR SUPPORT INBOARD ANGLE AT BS 303, RBL 54.75 IAW B737 SRM 51-40-02 & 51-21-01. 2L72 4F RTA1NM 20081201 CE 2008 12 1 ZESA2008007 120081016A3243CV02259AND9R3864CHECK VALVE CESSNA500 550 2076604CE NLG WW CHATTERING E ZESAK NONE E VIBRATION/BUFFET CLCLIMB 1 EA03824CB 0824 VIBRATION EVIDENT WITH CHANGES IN AIRSPEED, PRESSURIZATION AND GEAR RETRACTION. TROUBLESHOT SYS WITH TECH REP AND FOUND BRAKE RESERVOIR PRESSURIZATION CHECK VALVE VIBRATING DURING OPERATION. CHANGED CHECK VALVE AND RELIEF VALVE THEN PRESSURIZED CABIN. NO FAULTS NOTED. OPS CHECK FLIGHT PERFORMED AND ALL SYS CHECKED GOOD. 1L72 4F A22CE 20081202 NM 2008 12 2 USAA2008112492114120081122A53306545776 SKIN BOEING737 7374B7 138449CNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19427US 24549 CLT - RON - MAJOR REPAIR - CRACK FUSELAGE SKIN AT BS 727E +9 INCHES, S26R. REPAIRED FUSELAGE SKIN IAW B737 SRM 53-00-01 REPAIR 31. 2L72 4F RTA16WE 20081202 CE 2008 12 2 AWKA7741118 120081114A215073838433 ACM CESSNA750 750 2076810CE ZONE 200 LEAKING E AWKAA UNSCHED LANDING BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION CLCLIMB 1 WP25774XJ 28 7500274 SHORTLY AFTER TAKEOFF, 3 TO 5 MINUTES. A PASSENGER REPORTED STEAM/SMOKE VAPOR WAS ACCUMULATING IN THE CABIN. THE COCKPIT CREW BEGAN DETECTING ODOR AND LOOKING BACK IN THE CABIN SEEING INCREASING SMOKE/VAPOR LEVELS. THE PILOTS DECIDED TO RETURN AND NOTIFIED DEPARTURE OF INTENTIONS. WHILE ON VECTORS FOR RETURN, THE CREW PLACED BOTH PACKS IN MANUAL TEMP CONTROL AND WERE ABLE TO CONTROL BOTH PACKS MANUALLY. THE SMOKE BEGAN TO DIMINISH AS ENGINE POWER WAS REDUCED FROM CLIMB TO IDLE FOR DECENT. AN EMERGENCY WAS NOT DECLARED DUE TO SMOKE DIMINISHING, BUT, A RETURN FOR PRECAUTIONARY REASONS WAS DECLARED. THE COCKPIT AIRCYCLE MACHINE WAS FOUND TO BE FAULTY AND WAS REPLACED. OPS CHECKS NORMAL, NO SMOKE WAS DETECTED 2L72 4J RTT00007WI 20081202 CE 2008 12 2 DJFA2008081 120080710A324142901 CONTROL UNIT BEECH MU300 400A 1155402CE ANTI-SKID SYSTEMFAILED E DJFAH DEACTIVATE SYST/CIRCUITS O OTHER LDLANDING 1 EA23464LX RK453 ON LANDING BRAKES DID NOT RESPOND WHEN INITIALLY APPLIED. BRAKES ENGAGED AFTER A FEW MOMENTS BUT FAILED AGAIN WHILE DECELERATING BETWEEN 10 AND 15 KNOTS. CREW DISENGAGED THE ANTI-SKID SYS AND BRAKING RETURNED TO NORMAL. MAINT FOUND THE ANTI-SKID CONTROL BOX FAILED. THE UNIT WAS REPLACED. 2H72 4F RTA16SW 20081202 NM 2008 12 2 YENA200811180112 120081111A215017018554401 SUPPORT EMB ERJ190ERJ190100IGW3260408NM NR 2 PACK BROKEN A YENAA UNSCHED LANDING S AFFECT SYSTEMS CLCLIMB 1 EA15289JB3090 19000002 FLT 1114, MCO-RIC, AIR RETURN TO MCO AT FL 390, HEARD LOUD NOISE SIMILAR TO NOISE REDUCTION HEADSETS TURNING ON AND OFF. FLIGHT ATTENDANTS REPORTED LOUD BANG COMING FROM AFT OF AIRPLANE. CABIN ALT WAS RISING RAPIDLY WITH A HIGH CABIN RATE OF CLIMB. SHORTLY EICAS SHOWED CABIN ALT HIGH WITH MASTER WARNING. OFC WAS FULL CLOSED AND PACK (PSI) WAS NORMAL WITH GREEN LINES ON MFD ECS PAGE. PERFORMED QRH CABIN ALTITUDE HI PROCEDURES. CABIN ALT REACHED APRX 13,500 FT. REACHING 10,000 MSL, FLIGHT ALT CABIN PRESSURIZATION STABILIZED AND STARTED TO PRESSURIZE TO APRX 500 FT. FOUND NR 2 PACK OUTLET DUCT BELLOWS SLIPPED OFF AND A BROKEN PACK OUTLET DUCT SUPPORT ROD ASSY. RESECURED NR 2 PACK BELLOWS AND REMOVED AND R2L72 4F RTA57NM 20081202 NM 2008 12 2 YENA200811190113 120081111A212019055782401 DUCT EMB ERJ190ERJ190100IGW3260408NM NR 2 PACK CRACKED A YENAA UNSCHED LANDING O OTHER CLCLIMB 1 EA15289JB3091 19000002 FL 662, MCO-BUF, AIR RETURN TO MCO. CLIMBING THROUGH 32,000 CABIN ALT WAS 8400 AND CLIMBING. CREW EXECUTED CABIN ALT HIGH PROCEDURE. CABIN ALT HIT 10,000 WITH A CABIN ALT EICAS. OUTFLOW VALVE WAS CLOSED. NO NOISES. PACK INDICATION NORMAL. ON DESCENT CABIN ALT STAYED BELOW 10,000 THROUGH THE REMAINDER OF THE FLIGHT. THE CABIN ALT AND CABIN RATE FLUCTUATED. PERFORMED FIM TASK 21-31-00-810-818-A. FOUND NR 2 PACK OUTLET DUCT CRACKED AND CONDITIONER AIR CHECK VALVE BELLOWS RUPTURED. REMOVED AND REPLACED NR 2 PACK OUTLET DUCT AND CHECK VALVE BELLOWS PER AMM 21-51. OPS CHECKS AND LEAK CHECKS OK. PRESSURIZATION CHECKS GOOD. REF 21-31-00. 2L72 4F RTA57NM 20081202 EU 2008 12 2 USAA2008112692133120081114A5320D5348004320 SILL AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL OF L2 DOOR AT FR66 , Y1732. REPAIRED LOWER SILL OF L2 DOOR AT FR66, Y1732 IAW A320 SRM 53-41-14. 2L72 4F RTA28NM 20081202 EU 2008 12 2 USAA2008120192162120081118A5320D53471124201 SHEAR PLATE AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19654AW 1050 SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1732 IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20081202 WP 2008 12 2 NWAA084849853 120081103A3350 BATTERY PACK DOUG DC9 DC951 3022051WP EMERGENCY LIGHTSINOPERATIVE A NWAAK NONE O OTHER ININSP/MAINT 1 GL01762NC 47710 DURING LINE CHECK MX FOUND THAT THE RT SIDE EXTERIOR EMERGENCY FLOOD LIGHT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OP CONDITION. 2L72 4F RTA6WE 20081202 NM 2008 12 2 UALA2008111305437120080823A3350363674 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN LOOSE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29654UA 25392 ROW 1 RT EEL STRIP INOP. FOUND LOOSE LIGHTS. ADJUSTED LOOSE LIGHTS. OP CHECKS OKAY. 2L72 4F4 FRTA1NM E24NE 20081202 NM 2008 12 2 UALA2008111305439120080823A3350363674 LIGHT BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE CABIN INOPERATIVE A UALAK NONE L NO TEST ININSP/MAINT 1 WP29654UA 25392 ROW 5 RT EEL STRIP INOP. FOUND LIGHTS INOP. SPLICED IN EEL POWER STRIP. OPS CHECK GOOD. 2L72 4F4 FRTA1NM E24NE 20081202 NM 2008 12 2 DXTA2008120103380120081130A2700 UNKNOWN AMD FALC50FALCON2000 2730170NM UNKNOWN E DXTAA UNSCHED LANDING F FLT CONT AFFECTED DEDESCENT 1 GL07275QS 075 ACFT WAS DESCENDING THROUGH FL 380 WHEN FLYING PILOT MOMENTARILY LOST PITCH CONTROL. 2L72 4F RTA50NM 20081202 CE 2008 12 2 DXTA2008120103381120081130A2120 UNKNOWN CESSNA560 560XL 2076702CE COCKPIT ODOR E DXTAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 GL07639QS 5605139 WITH APU OPERATING AND AVIONICS SWITCH ON I NOTICED A BURNING ODOR. 2L72 4F RTA22CE 20081203 SO 2008 12 3 C2XA08TY137 120081126A3350251005 FUSE EMB 145 EMB145LR 3260212SO BATTERY BLOWN A C2XAK NONE L NO TEST ININSP/MAINT 1 SW2726545 145558 RT & LT OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY TRAY FUSE IAW RADIANT POWERCORP VCMM 25-60-03. OPS CHECK GOOD AND AIRCRAFT RELEASE FOR SERVICE. 2L72 4T RTT00011AT 20081203 SO 2008 12 3 C2XA08RI174 120081104A32608005701 PROXIMITY SWITCH EMB 145 EMB145XR 3260214SO LANDING GEAR DEFECTIVE A C2XAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW2723139 145731 FLIGHT 2859 - EWR - FLIGHT CREW REPORTED LANDING GEAR AIR GROUND FAIL MESSAGE ON EICAS AND ENGINE 1/2 REV DISAGREE AFTER SELECTING GEAR UP. CREW PERFORMED AIR RETURN AND LANDED AIRCRAFT UNEVENTFULLY. MESSAGES DISAPPEARS WHEN SELECTED GEAR DOWN. EWR MX REMOVED AND REPLACED PROXIMITY SWITCH AND SERVICED NOSE LANDING GEAR. MX PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RT 20081203 SO 2008 12 3 C2XA08SH 120081202A554412033817005 ATTACH FITTING EMB 145 EMB145LR 3260212SO RUDDER DAMAGED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713955 145075 SHV - DURING C-CHECK RUDDER 1 UPPER ACTUATOR ATTACHMENT LOWER HINGE UPPER HAT BUSHING MIGRATED. 2L72 4T RTT00011AT 20081203 SO 2008 12 3 C2XA08SH154 120081203A551214552201402 SKIN EMB 145 EMB145XR 3260214SO HORIZ STAB CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2724103 145645 RT HORIZONTAL STAB L/E HAS CORROSION AROUND RIVETS. RT HORIZONTAL STAB L/E WAS REPAIRED IAW EC 5510-01195. THE AIRCRAFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4F RT 20081204 SO 2008 12 4 C2XA08TY134 120081123A4920M4504113A APU EMB 145 EMB145LR 3260212SO MALFUNCTIONED A C2XAF ACTIVATE FIRE EXT. J WARNING INDICATION ININSP/MAINT 1 SW2716976 145171 BNA - MX WAS IN THE COCKPIT OF THE A/C TROUBLESHOOTING THE APU, AND RECEIVED AN APU FIRE MESSAGE AND DISCHARGED THE FIRE BOTTLE. THE APU FIRE BOTTLE WAS REMOVED AND REPLACED IAW EMB 145 AMM 26-22-01 AND OPS CHECKED GOOD. THE APU WAS REMOVED AND REPLACED IAW T/C 6849001 AND THE OPS AND LEAK CHECK WERE GOOD. A/C HAS BEEN RELEASED TO SERVICE. 2L72 4T RTT00011AT 20081204 NM 2008 12 4 R61A20080048 120081119A5320 STRUCTURE EMB ERJ170ERJ170100SU 3260403NM FUSELAGE DENTED A R61AK NONE O OTHER ININSP/MAINT 1 GL11821MD 17000042 DENT AT FRAME 91 TO FRAME 92, STRINGER 21 RT AND 23 RT. PERFORMED MAJOR REPAIR PER EMBRAER ENGINEERING INSTRUCTION. 2L72 4F RTA56NM 20081204 NM 2008 12 4 SWAA086732 120081202A256025270017 GLOWSTRIP BOEING737 7377H4 1384404NM CABIN DETERIORATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29788SA 30603 DURING SCHEDULED 8Y CHECK, FOUND CABIN FLOOR PHOTOLUMINESCENT LIGHT STRIP IN POOR CONDITION. REMOVED AND REPLACED STRIP PER SWA DWG. 2L72 4F RTA16WE 20081204 NM 2008 12 4 SWAA086661 120081126A53126517582 BULKHEAD BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29621SW 28037 DURING SCHEDULED SPV CHECK, FOUND LT VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17, WL 232. REPAIRED WEB PER SRM. 2L72 4F RTA16WE 20081204 NM 2008 12 4 SWAA086662 120081126A2560P4010021 BATTERY BOEING737 7373H4 1384600NM FLASHLIGHT DISCHARGED A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29631SW 27706 AFT I/B FLASHLIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20081204 NM 2008 12 4 SWAA086663 120081126A53306545768 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 370, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20081204 NM 2008 12 4 SWAA086664 120081126A53306545767 SKIN BOEING737 7373A4 1384585NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29678AA 23290 DURING SCHEDULED MV4 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 400, STR 15L. REPAIRED SKIN PER SWA EA. 2L72 4F RTA16WE 20081204 NM 2008 12 4 SWAA086669 120081127A3350417N5213 COVER BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29902WN 36615 DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT COVER BROK