20100416 NM 2010 4 16 ABXA201004130058 120100404A5320141T293815 STRUCTURE BOEING767 767232 1385132NM NLG WW CRACKED A ABXAK NONE O OTHER ININSP/MAINT 1 GL23742AX 22217 THE LBL 25 NOSE WHEEL WELL VERTICAL CHORD AT STA 287 IS CRACKED IN THE RADIUS. LOCATED 11.75 INCHES BELOW CEILING STRUCTURE. REMOVED DAMAGED SECTION OF CHORD. REPAIRED IAW B767 SRM CH 51-70-12 FIG 1. 2L72 4F RTA1NM 20100203 NM 2010 2 3 SWAA100461 120100127A531165C22909 FRAME BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED 14Y CHECK, FOUND FRAME CRACKED AT BS 500C, STR 8R. REPAIRED FRAME PER EA. 2L72 4F RTA16WE 20100201 NM 2010 2 1 SWAA100387 120100123A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29343SW 24151 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 515D, STR 16R. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20100419 WP 2010 4 19 FDEA201004061079 120100406A5321SRZ25005187FF FLOORBOARD DOUG DC10 DC1010F 3022111WP CARGO BAY DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21361FE 75748 48260 AFT CARGO COMPARTMENT FLOORBOARD 187 FF IS DELAMINATED AND DENTED AT SEVERAL LOCATIONS. FABRICATED NEW AFT CARGO FLOOR PANEL 187 FF IAW DWG SRZ 25-005, REV "H" AND DWG SRZ 25-011, REV "C". 2L73 4F A22WE 20100416 WP 2010 4 16 EE4Y1004068 120100413A5311 FRAME DOUG DC9 DC915F 3022037WP FUSELAGE DAMAGED B MJYAK NONE O OTHER ININSP/MAINT 1 SO23784TW53952 47014 DURING THE UPPER FUSELAGE, CARGO CABIN AT STA 669 BETWEEN LONG 14R AND LONG 15R INSPECTION, COOPESA FOUND FRAME WITH DOUBLE HOLES. 2L72 4F A6WE 20100125 NM 2010 1 25 SWAA100225 120100112A575465C26602311A SKIN BOEING737 7373H4 1384600NM LE SLAT DELAMINATED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29607SW 27927 DURING SCHEDULED 2HC2 CHECK, FOUND LT WING NR 2 SLAT UPPER WEDGE SKIN DELAMINATED. REMOVED AND REPLACED NR 2 SLAT PER MM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100234 120100114A5330654577677 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29386SW 26601 DURING SCHEDULED MV1 CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT BS 737D, BL 0. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100244 120100117A53306545768 SKIN BOEING737 7373Q8 1384670NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29317WN 24068 DURING SCHEDULED 22Y CHECK, FOUND SKIN CRACKED AT BS 321.5, WL 211.8. REPAIRED SKIN PER EO. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100249 120100118A3350D71701100 BATTERY PACK BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29708SW 27842 DURING SCHEDULED HC1 CHECK, LT EEPLS FAILED CAPACITY CHECK AT ROW 6. REMOVED AND REPLACED BATTERY PACK PER MM. 2L72 4F RTA16WE 20100125 2010 1 25 SWAA100278 420100115A2565D31354 SLIDE BOEING737 7373H4 1384600NM R1 DOOR OUT OF POSITION A SWAAK NONE O OTHER ININSP/MAINT 1 SW29650SW 27720 R1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100282 120100119A53406935352U14 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 3L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100295 120100119A53116546526 FRAME BOEING737 7377H4 1384404NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29704SW 27838 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100308 120100116A3350411A2212 COVER BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29922WN 32461 R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100309 120100117A3350100031 SIGN BOEING737 7377H4 1384404NM CABIN BROKEN A SWAAK NONE O OTHER ININSP/MAINT 1 SW29212WN 32485 L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100310 120100118A335081000 LIGHT BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29282WN 32534 EEPLS LOOSE AT ROW 1. SECURED EEPLS PER MM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100343 120100120A335081000 LIGHT BOEING737 7373H4 1384600NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29315SW 23337 DURING SCHEDULED MV2 CHECK, FOUND RT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100349 120100120A256065C34691 GIRT BAR BOEING737 7373H4 1384600NM EVAC SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED 14Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE GIRT ASSY LOOSE. SECURED GIRT ASSY PER MT. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100351 120100120A575465C26686 SKIN BOEING737 7377H4 1384404NM LE SLAT CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29704SW 27838 DURING SCHEDULED 12Y CHECK, FOUND RT WING NR 7 SLAT LOWER SKIN CRACKED. REPAIRED SKIN PER AAR EA. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100352 120100120A53156546804 FLOORBEAM BOEING737 7377H4 1384404NM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29704SW 27838 DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 18. REPAIRED BEAM PER AAR EA. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100353 120100120A3350D11074 CONNECTOR BOEING737 7377H4 1384404NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29742SW 29278 DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LIGHT CONNECTOR LOOSE. REMOVED AND REPLACED CONNECTOR PER WDM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 UALA2010012200268120100121A361032907706 ISOLATION VALVE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE BLEED SYSTEM MALFUNCTIONED A UALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP29217UA 30550 BLEED ISOLATION VALVE LT STATUS MSG. BLEED ISOLATION VALVE LT LOCKED IN OPEN POSITION. REPLACED LT ISOLATION VALVE. OP CHECKS GOOD. 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 UALA2010012200269120100121A4940S351W200100 CONTROLLER BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE APU INOPERATIVE A UALAK NONE J WARNING INDICATION ININSP/MAINT 1 WP29217UA 30550 APU AIR STARTER APUC DETECTED LOSS OF AIR TURBINE STARTER FUNCTION. STATUS MSG-3610290 LATCHED TA MODE. REPLACED APU AT SCV & AIR TURBINE STARTER & APU SHUTOFF VALVE, ALL NO HELP. APU STILL DOES NOT START PNEUMATICALLY. REPLACED AIR SUPPLY CABIN PRESSURE CONTROLLER, OPS CKS OK. 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 UALA2010012200270120100122A801210011003 START VALVE BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE RT ENGINE MALFUNCTIONED A UALAK NONE J WARNING INDICATION ININSP/MAINT 1 WP29223UA 30224 ENG START VALVE RT STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION. ADVISORY MSG-8061562 INACTV ES MODE. STARTER INOP, NO PARTS STOCKED. RPL'D START VALVE. DRY MOTOR ENGINE, NO MESSAGE. 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 UALA2010012000250120100119A801210011003 START VALVE BOEING777 777222 1385219NM PWA PW4077PW4077 NE RIGHT FAULTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29774UA 70 26936 ENG START VALVE R RT STARTER AIR VALVE POSITION DISAGREES WITH COMMANDED POSITION OR STARTER AIR VALVE POSITION INDICATION IS LOST. REPLACED START VALVE. REPLACED STARTER. MOTORED ENGINE. OPS NORMAL, NO MESSAGES. 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 UALA2010012000252120100120A2910 LINE BOEING777 777222 1385219NM PWA PW4077PW4077 NE HYD SYSTEM LEAKING A UALAK NONE K FLUID LOSS ININSP/MAINT 1 WP29774UA 26936 EVIDENCE OF HYD LEAK NR 2 ENG AT HYD PRESS LINE CONNECTION TO LWR PYLON. NEED TO ACCOMPLISH CLEANING OF BURNT HYD RESIDUE ON DUCTING AND SURROUNDING AREA DUE TO HYD LINES LEAKING, LOCATED UNDER OB REV COWL, AT HYD LINE HOOKUP PYLON AREA. HYD LINES HAVE BEEN REPLACED AND THERE ARE NO LEAKS. NEED A STRONG SOLVENT TO DO CLEAN UP. CLEANED HYD RESIDUE FROM DUCTS. 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 UALA2010012000253120100120A2840921761 TRANSMITTER BOEING777 777222 1385219NM PWA PW4077PW4077 NE FUEL FLOW FAULTY A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29212UA 30218 UNABLE TO DETERMINE FUEL QUANTITY LOSS OF OVER 4200 LBS-800NM. FUEL FLOW TXMTR CHANGED, NEEDS LEAK AND OPS CHECK ON NR 2 ENG. ACP LEAK CHECKED, NO LEAKS DETECTED. COMPLETED FIM 28-41 TASK 825 FQIS AND FMC CHECKED GOOD. REPLACED BOTH NR 1 FUEL FLOW TRANSMITTERS. SUCCESSFUL VERIFICATION FLIGHT ACCOMPLISHED, BOTH L AND R FUEL FLOW SYSTEMS OPERATED NORMALLY. 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 IPXA10558223 120100120A2750 FLAP SYSTEM BOEING757 75724APF 1384969NM TE FLAPS FAILED A IPXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE17432UP 25463 ON CLIMB OUT OF SDF FLAPS FAILED TO OPERATE FROM 1 TO UP. WORKED EMERGENCY CHECKLIST. HAD TO OPERATE FLAPS IN ALTERNATE MODE FOR REST OF FLIGHT BACK. DEFERRED, ACFT FERRIED. PERFORM NR 1 DISPLAYED FAULT MSG 212. AFTER RESETTING C/B C1037 NO FAULTS ON FSEU NR 1 DISPLAYED. OK FOR SERVICE. 2L72 4F RTA2NM 20100126 NM 2010 1 26 JJBA201025751 120100122A3350AD5521981 BATTERY PACK DHAV DHC8 DHC8202 2809007NM EMERGENCY LIGHTSDISCHARGED A JJBAK NONE L NO TEST ININSP/MAINT 1 EA01359PH1950747 514 EMERGENCY LIGHTS WILL NOT COME ON. REMOVED AND REPLACED BATTERY PACK. OPS CHECK SAT. 2H72 4T RTA13NM 20100126 NM 2010 1 26 UALA2010012100256120100120A2622301000223 EXTINGUISHER BOEING777 777222 1385219NM PWA PW4077PW4077 NE LAVATORY MISSING A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29778UA 26940 FIRE EXTINGUISHER - MISSING DR-3L FWD LAV 131. REPLACED EXTINGUISHER. 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 UALA2010012100257120100121A25302610000101 OVEN BOEING777 777222 1385219NM PWA PW4077PW4077 NE GALLEY MALFUNCTIONED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29778UA 26940 BUSS GALLEY OVEN R31 CB R31 POPPED DID NOT RESET. REPLACED R31 OVEN. OPS GOOD . 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 C77A227853 120100115A2741 INDICATION SYS EMB ERJ170ERJ170200LR 3260121NM TRIM SYS INTERMITTENT A C77AC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 EA27629CZ3759 17000236 TAKEOFF CONFIG WARNING ON TAKEOFF, ABORTED TAKEOFF AND RETURNED TO GATE. FOUND PITCH TRIM INDICATION INOP DEFERRED INDICATION SYS. REPLACED HS-ACE NO FURTHER ISSUES WITH THE ACFT 2L72 4F RTA56NM 20100126 CE 2010 1 26 J7SA45205111310 120100113A261274412135 FIRE DETECTOR LEAR 45 45LEAR 5170805CE LT NACELLE FAILED E J7SAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 SW05615FX 452051 CLIMBING THROUGH FL230 LT ENG FIRE WARNING ILLUMINATED. REDUCED POWER TO IDLE AND FIRE LIGHT EXTINGUISHED. IFE DECLARED. AIR RETURN TO DEPARTURE WITH UNEVENTFUL LANDING AND TAXI. SWAPPED LT & RT FIRE DETECT BOXES. INSTALLED A NEW LT ENGINE TAIL PIPE FIRE DETECT ELEMENT. NO DEFECTS NOTED ON GROUND ENGINE RUNS. 2L72 4F RTT00008WI 20100126 NM 2010 1 26 C77A227468 120100114A3350340022 POWER SUPPLY EMB ERJ170ERJ170200LR 3260121NM EMERGENCY LIGHTSFAULTY A C77AK NONE L NO TEST NRNOT REPORTED 1 EA27605CZ5875 17000186 AFT EMERGENCY LIGHTS DID NOT PASS FUNCTIONAL CHECK. REPLACED LT AFT EMERGENCY LIGHT POWER SUPPLY. 2L72 4F RTA56NM 20100126 CE 2010 1 26 DXTA2010011803947120100116A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG WEAK E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07391QS 5600493 DURING "BRAKES CHECK" ON TAXI OUT, CO-PILOT'S RT SIDE BRAKE PEDAL WOULD NOT HOLD PRESSURE, WENT TO THE FLOOR. CHECKED SYS FOR LEAKS UNDER PRESSURE, NONE NOTED. PERFORMED BRAKE BLEEDING OF SYS IAW MM 32-42-00. NO FURTHER DEFECTS NOTED. 2L72 4F RTA22CE 20100126 NM 2010 1 26 C77A230021 120100121A335034002210 BATTERY PACK EMB ERJ170ERJ170200LR 3260121NM EMERGENCY LIGHTSFAILED A C77AK NONE L NO TEST ININSP/MAINT 1 EA27610CZ 17000198 EMERGENCY LIGHT BATTERY FAULTY. 2L72 4F RTA56NM 20100126 WP 2010 1 26 DALA100699876 120100116A5321 FLOOR PANEL DOUG DC9 DC951 3022051WP CABIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27785NC 48110 DURING "H" CHECK FOUND CORROSION ON FLOOR PANEL NR 26. REPAIRED IAW SRM 53-01, SRM 51-10-2, SRM 51-10-3, SRM 51-10-4 AND SRM 51-30-2. 2L72 4F RTA6WE 20100126 WP 2010 1 26 DALA100719876 120100116A5320 FLOOR SUPPORT DOUG DC9 DC951 3022051WP BS 1154 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27785NC 48110 DURING "H" CHECK FOUND CRACK IN FLOOR SUPPORT AT BS 1154, LBL 20. REPAIRED IAW SRM 51-72-01, SRM 51-10-2, SRM 51-10-4, AND SRM 51-10-3 & 51-30-2. 2L72 4F RTA6WE 20100126 WP 2010 1 26 DALA100709876 120100118A5320 INTERCOSTAL DOUG DC9 DC951 3022051WP BS 408 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27785NC 48110 DURING "H" CHECK FOUND CRACK ON INTERCOSTAL AT BS 408 BL 0. REPAIRED IAW SRM 51-10-2, SRM 51-10-3, SRM 51-10-4 AND SRM 51-30-5. 2L72 4F RTA6WE 20100126 WP 2010 1 26 DALA100729876 120100118A5315 FLOORBEAM DOUG DC9 DC951 3022051WP BS 408 DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27785NC 48110 DURING "H" CHECK FOUND CHAFING DAMAGE TO FLOORBEAM AT BS 408, RBL 22 - BL 0. REPAIRED IAW SRM 53-01-20, SRM 51-10-4 & 51-10-3. 2L72 4F RTA6WE 20100126 NM 2010 1 26 AALA20100119DFW06120100117A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21780AN 29956 EMERGENCY LIGHT AT 25C INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2L72 4F RTT00001SE 20100126 NM 2010 1 26 AALA20100119DFW07120100117A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21780AN 29956 EMERGENCY LIGHT AT SEAT 44G INOPERATIVE. REPLACED LAMP. 2L72 4F RTT00001SE 20100126 NM 2010 1 26 AALA20100119DFW08120100117A3350 LIGHT BOEING777 777223 1385213NM CABIN INOPERATIVE A AALAK NONE L NO TEST ININSP/MAINT 1 SW21780AN 29956 EMERGENCY LIGHT AT SEAT 36G INOPERATIVE. REPLACED LIGHT ASSEMBLY. 2L72 4F RTT00001SE 20100126 NM 2010 1 26 AALA20100119DFW09120100117A3350 LENS BOEING777 777223 1385213NM CABIN MISSING A AALAK NONE O OTHER ININSP/MAINT 1 SW21780AN 29956 EMERGENCY LIGHT AT SEAT 10G MISSING LENS. REPLACED LENS. 2L72 4F RTT00001SE 20100126 WP 2010 1 26 AALA20100120TUL01120100120A5347 SEAT TRACK DOUG DC9 DC982 3022082WP FUSELAGE CORRODED A AALAK NONE O OTHER ININSP/MAINT 1 SW21424AA 49336 NUMBER 6 SEAT TRACK INSIDE TRACK CORROSION. REMOVED CORROSION FOUND SEAT TRACK TO BE OUT OF LIMITS. INSTALLED SEAT TRACK REPAIR PLUG PER 53-05 FIG 4A. 2L72 4F A6WE 20100126 EA 2010 1 26 A6WA201040006 120100105A2610 DETECTION SYS CNDAIRCL600 CL6002B19 1900309EA APU BAY MALFUNCTIONED A A6WAO OTHER N FALSE WARNING APAPPROACH 1 GL31406AW 7402 ON APPROACH WHEN TRANSFERRING BLEEDS TO APU RECEIVED APU OVERTEMP WARNING FOLLOWED BY APU FIRE WARNING. SHUT APU DOWN MESSAGES WENT AWAY APU DOOR INHIBIT STATUS MESSAGE DISPLAYED. INSP APU, APU COMPARTMENT FOUND NO EVIDENCE OF FIRE BUT NOTED SLIGHT ODOR. UNINHIBITED DOOR AND RECORDED FAULT CODES 109, 226, 227, AND 230. INSPECTED APU INLET APU FIRE LOOP FOUND NO DEFECTS OPERATED APU FOR 25 MINUTES NO FAULTS NOTED EGT NORMAL IAW AMM 49-10-00. REMOVED FROM MEL. 2L72 4F RTA21EA 20100126 EA 2010 1 26 ASOA201000067 120100116A5710 SKIN CNDAIRCL600 CL6002B19 1900309EA WING CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27904EV 7628 INDICATIONS OF CORROSION NOTED AT WS 55.38 (540BB) ON THE FLAT LANDING SURFACE APRPOX 70 PERCENT FULL SCREEN HEIGHT. AREAS MARKED ON ACFT LOWER WING PLANK. C/W EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030 REV G AND FWDED ALL REQUIRED FORMS TO STRUCTURES ENGINEERING. 2L72 4F RTA21EA 20100126 WP 2010 1 26 AALA20100120TUL02120100120A5320 WEB DOUG DC9 DC982 3022082WP FUSELAGE PUNCTURED A AALAK NONE O OTHER ININSP/MAINT 1 SW21424AA 49336 HOLE IN SUBFLOOR 13 INCHES INBOARD OF FORWARD ENTRY DOOR STATION 200. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16. 2L72 4F A6WE 20100126 NM 2010 1 26 C77A227588 120100114A5210 DOOR EMB ERJ170ERJ170200LR 3260121NM L1 DOOR VENT BINDING A C77AA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA27620CZ4779 17000214 AFTER TAKEOFF FROM MSP CREW RECEIVED A L1 DOOR VENT DOOR UNSAFE MESSAGE RETURNED TO FIELD. MX INSPECTED AND LUBRICATE VENT DOOR WITH NO FURTHER ISSUES. 2L72 4F RTA56NM 20100126 EU 2010 1 26 DALA100563234 120100116A5321 FLOOR PANEL AIRBUS320 A320212 3930322EU CABIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27334NW 339 DURING "H" CHECK FOUND FLOOR PANEL 262FF HAS CORROSION. REPLACED FLOOR PANEL, IAW TASK CARD 2500-6602. 2L72 4F RTA28NM 20100126 NM 2010 1 26 UALA2010012100258120100121A29133031863001 PUMP AIRBUSA319 A319131 3930317NM IAE V2522 V2522A5 NE HYD SYSTEM FAILED A UALAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP29817UA 873 YELLOW SYS HYD LOSS, RTFL. REPLACED HP FILTER ELEMENT. NO EVIDENCE OF DEBRIS. TROUBLESHOT OVERHEAT PROBLEM AND FOUND BAD CHECK VALVE 3083G. REMOVED DEFECTIVE CHECK VALVE. REPLACED AND PERFORMED HIGH POWER RUN FOR 25 MINS. REPLACED TEMP TRANSMITTER 3381GR DUE TO YELLOW SYSTEM OVERHEAT, OVERHEAT MSG DID NOT RE-APPEAR AND ALL INDICATIONS NORMAL. OK FOR RETURN TO SERVICE. 2L72 4F4 FRTA28NM E40NE 20100126 NM 2010 1 26 UALA2010012100263120100119A21508102142 VALVE BOEING777 777222 1385219NM PWA 4084 PW4084 NE RT A/C PACK MALFUNCTIONED A UALAO OTHER J WARNING INDICATION NRNOT REPORTED 1 WP29211UA 30217 RIGHT PACK MODE IN EICAS RT PACK KEEPS TRIPPING OFF. REPLACED THE LOW LIMIT VALVE, OPS CK'D GOOD. 2L72 4F4 FRTT00001SEE46NE 20100126 WP 2010 1 26 DALA100449882 120100115A3350 BATTERY PACK DOUG DC9 DC951 3022051WP EMERGENCY LIGHTSINOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27670MC 47659 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2L72 4F RTA6WE 20100126 WP 2010 1 26 DALA100459755 120100116A3350 BATTERY PACK DOUG DC9 DC941 302207NWP EMERGENCY LIGHTSINOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27755NW 47179 DURING LINE CHECK, MX FOUND THAT 2 OF THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2L72 4F A6WE 20100126 WP 2010 1 26 AALA20100120TUL04120100120A5320 CUSP WEB DOUG DC9 DC982 3022082WP FUSELAGE CRACKED A AALAK NONE O OTHER ININSP/MAINT 1 SW21424AA 49336 CRACK IN RIGHT CUSP, THREE INCHES INBOARD OF CUSP TEE STATION 842. CUT OUT DAMAGE AND INSTALLED DOUBLER PER AARD 53-20-00-16. 2L72 4F A6WE 20100126 EU 2010 1 26 UALA2010012200271120100121A3510MXP80111600U STOWAGE BOX AIRBUS320 A320232 3930326EU IAE V2527 V2527A5 NE OXYGEN MASK MALFUNCTIONED A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29438UA 678 CAN'T SEE YELLOW AIR FLOW INDICATOR ON F-O O2 MASK. REPLACED FO 02 MASK STOWAGE BOX. CHECKS GOOD. 2L72 4F4 FRTA28NM E40NE 20100126 NM 2010 1 26 UALA2010012200278120100122A335020131A CHARGER BOEING747 747422 1384935NM PWA 4056 PW4056 NE EMERGENCY LIGHTSFAULTY A UALAK NONE L NO TEST ININSP/MAINT 1 WP29116UA 26908 EMERGENCY LIGHT SIGN DR4L INOP. REPLACED BATTERY CHARGER. OP CK NORMAL. 2L74 4F4 FRTA20WE E24NE 20100126 WP 2010 1 26 DALA1004079857 120100114A3350 BATTERY PACK DOUG DC9 DC951 3022051WP EMERGENCY LIGHTSINOPERATIVE A DALAK NONE L NO TEST ININSP/MAINT 1 SO27766NC 47739 FLIGHT CREW DISCOVERED THAT THE EMERGENCY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2L72 4F RTA6WE 20100126 NM 2010 1 26 C77A201001170002 120100117A3350340022 BATTERY PACK EMB ERJ170ERJ170200LR 3260121NM EMERGENCY LIGHTSFAILED A C77AK NONE L NO TEST ININSP/MAINT 1 EA27630C 3797 17000238 COCKPIT EMERGENCY LIGHT WOULD NOT TEST. SUSPECT BATTERY PACK 2L72 4F RTA56NM 20100126 NM 2010 1 26 C77A201001170001 120100117A3350340022 BATTERY PACK EMB ERJ170ERJ170200LR 3260121NM EMERGENCY LIGHTSFAILED A C77AK NONE O OTHER ININSP/MAINT 1 EA27628CZ4099 17000233 WITH ACFT POWERED DOWN AND EMERGENCY LIGHT SWITCH IN OFF POSITION, EMERGENCY LIGHTS IN FWD CABIN CAME ON. 2L72 4F RTA56NM 20100126 NM 2010 1 26 C77A230267 120100122A2150 A/C PACK EMB ERJ170ERJ170200LR 3260121NM GE CF34 CF348E5 30061NE CONTAMINATED A C77AC ABORTED TAKEOFF B SMOKE/FUMES/ODORS/SPARKS TOTAKEOFF 1 EA27607CZ 17000192 193537 ACFT ABORTED TAKEOFF, SMOKE AND STRONG ODOR IN THE COCKPIT AND CABIN. THE ACFT HAD COMPRESSOR WASHES PERFORMED DURING OVERNIGHT MX AND RESIDUAL WASH FLUID WAS IN THE AIR CONDITIONING SYS. ENGINE DRY PROCEDURES WERE PERFORMED AND SMOKE AND ODOR WERE REMOVED FROM THE CABIN REF MM 72-00-00-100-001. 2L72 4F4 FRTA56NM E00063EN 20100126 EU 2010 1 26 DALA100933352 120100120A3350 BATTERY PACK AIRBUSA330 A330223 3930374EU EMERGENCY LIGHTSINOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO27852NW 0614 FOUND LDMCR "EXIT" SIGNS DID NOT ILLUMINATE DURING TEST, FOUND BATTERY EPSU (19WL) MESSAGE, REPLACED BATTERY AND TESTS OK. 2L72 4F RTA46NM 20100126 EA 2010 1 26 ASOA201000052 120100115A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 559-567 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 CARGO BAY SEAT TRACK SEGMENT FS 559+95 TO 567.0 LBL 9.0 IS CORRODED. (OPEN) 2L72 4F RTA21EA 20100126 EA 2010 1 26 ASOA201000039 120100112A1100 SIGN CNDAIRCL600 CL6002C10 1390015EA CABIN DETERIORATED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27730EV 10141 EXIT SIGN NEXT TO MAIN DOOR FADED UNABLE TO READ. 2L72 4F RTA21EA 20100126 EU 2010 1 26 DALA100293259 120100120A5321 FLOOR PANEL AIRBUS320 A320212 3930322EU CABIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27359NW 846 DURING "M" CHECK FOUND CORROSION ON FLOOR PANEL 262FF. REPLACED IAW CARD 2500-6002. 2L72 4F RTA28NM 20100126 NM 2010 1 26 F3LA2010012100307120100118A5320D5347112420300 PLATE AIRBUSA319 A319111 3930336NM ZONE 100 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM21942FR 81 2497 DURING C3 C-CHECK INSP NOTED THE RT SHEAR PLATE AT FRAME 70 HAS SURFACE CORROSION AND APPEARS TO BE COMING FROM UNDER GALLEY FLOORBOARD. MX REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11 AND SRM 51-44-11. 2L72 4F RTA28NM 20100126 NM 2010 1 26 F3LA2010012100308120100119A5320D5347112320200 SUPPORT AIRBUSA319 A319111 3930336NM ZONE 100 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM21942FR 81 2497 DURING C3 C-CHECK INSP NOTED THE LT FRAME SUPPORT AT FRAME 70 HAS CORROSION ON THE BOTTOM SIDE AT NUTPLATE HOLES. MX REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-42-11. 2L72 4F RTA28NM 20100126 NE 2010 1 26 UALA2010012200272220100121A73211B7486 EEC BOEING757 757222 1384956NM PWA 2037 PW2037 NE NR 1 ENGINE FAULTY A UALAO OTHER O OTHER NRNOT REPORTED 1 WP29545UA 25323 NR 1 ENG WITH EEC MAINT POWER SELECT SWITCH IN ALTN POSITION. EPCS PAGE DISPLAYS NO CHANNEL SELECTED. CHANNEL SELECT SWITCH HAS NO EFFECT. SQUARE BOX AROUND PRI, SEC, NOT DISPLAYED. THRUST REV WILL NOT DEPLOY. REPLACED EEC. PROBLEM STILL PERSISTS. REPLACED NR1 PDIU SYS OPS, CHECKED OK. 2L72 4F4 FRTA2NM E17NE 20100126 SO 2010 1 26 C2XA10CL008 120100120A21508152915 SWITCH EMB 145 EMB145XR 3260214SO NR 1 PACK FAULTY A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW27141588981 145791 IAH FLT 2124 THE CREW REPORTED A PACK 1 OVERLOAD MESSAGE IN FLT. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED NR 1 PACK OVER TEMP SWITCH. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RT 20100126 NM 2010 1 26 UALA2010012200273120100121A5754 STRUCTURE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE SLAT DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29667UA 29239 RT WING LE STA ISS 308 HAS DAMAGE. CRACKS STOP DRILLED. VERIFIED NO CRACKS BEYOND STOP DRILL. REMOVED CRACKED SECTION AND REPAIRED IAW DWG. ACCOMPLISHED INSPECTION OF REPAIR INSTALLATION IN COMPLIANCE WITH DWG. OK IAW INSPECTOR SIGN OFF. 2L72 4F4 FRTA1NM E24NE 20100126 NM 2010 1 26 UALA2010012200274120100121A2121732591F FAN BOEING747 747422 1384935NM PWA 4056 PW4056 NE CABIN FAILED A UALAO OTHER B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 WP29175UA 24382 EICAS STATUS MSG E&E CLNG EXH FAN. CREW REPORTED SLIGHT BURNING ODOR DETECTED WHEN MSG WAS INITIALLY DISPLAYED, ODOR HAS SINCE CLEARED. CHECKED SYS FOUND CB POPPED FOR FAN. RESET BREAKER AND TESTED SYS IN CMC AFTER A SUCCESSFUL TEST THE CB ON P415 PANEL POPPED AGAIN. SUSPECT FAN FAILED, NIL TIME FOR FURTHER TROUBLESHOOTING. REPLACED EXHAUST FAN. OPS CHECKS OK. 2L74 4F4 FRTA20WE E24NE 20100126 NM 2010 1 26 UALA2010012100259120100121A5532177W31012 PANEL BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE VERTICAL STAB DELAMINATED A UALAK NONE O OTHER ININSP/MAINT 1 WP29794UA 26953 RT VERT STAB LWR FWD BOX PANEL NR 1 HAS A LARGE DELAM AREA. DELAM AREA IS 12" X 7" APP ROX 4" FROM UPPER EDGE OF PANEL AND 14" FROM AFT EDGE OF PANEL. NEED PN 177W3101-2 & 177W3102-5. REPAIRED IAW SMB WU NR K4610E AND R & R NR R13333. REPAIRED ON SMB WU K4598E. 2L72 4F4 FRTT00001SEE46NE 20100126 NE 2010 1 26 UALA2010012100264220100120A7250 TURBINE BLADES BOEING777 777222 1385219NM PWA 4090 PW4090 52119NE ENGINE DAMAGED A UALAK NONE O OTHER ININSP/MAINT 1 WP29222UA 30553 222163 HPT BLADE BURN. DAMAGE AT HPT TURBINE BLADES 2EA HAVING MATERIAL BURN THROUGH IN AREA B BEYOND LIMITS. R & R ENGINE. 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 UALA2010012200265120100122A5210 CASTING BOEING777 777222 1385219NM PWA PW4077PW4077 NE R2 DOOR BROKEN A UALAK NONE O OTHER ININSP/MAINT 1 WP29779UA 26941 DOOR 2R WHEN DOOR IS OPENED ARMING LEVER GOES TO ARM. FOUND BROKEN CASTING. REMOVED CASTING. BROKEN CASTING ON SHELF ON MID GALLEY. CASTING AT LOWER FWD END OF THE NR 2R MAIN CABIN DOOR. BROKEN CASTING ON SHELF ON MID GALLEY. FOUND DOOR 2R ASSIST BOTTLE PRESSURE AT ZERO. 2R ASSIST BOTTLE PARTIALLY INSTALLED. TUBE ASSY AND SQUIB CONNECTOR NEED TO BE INSTALLED. REINSTALLED TUBE AND SQUIB CONNECTOR AND REARMED. REPLACED CASTING AT LWR FWD END OF THE NR 2R MAIN CABIN DOOR. INSPECTED LWR FWD CASTING INSTALLATION. OK FOR SVC. 2L72 4F4 FRTT00001SEE46NE 20100126 NM 2010 1 26 C77A20100124001 120100123A3010 ANTI-ICE SYSTEM EMB ERJ170ERJ170200LR 3260121NM LT WING MALFUNCTIONED A C77AA UNSCHED LANDING J WARNING INDICATION APAPPROACH 1 EA27624CZ4308 17000222 LT WING ANTI-ICE FAIL DURING FLIGHT, DIVERTED, DUE TO ICING CONDITIONS AT DESTINATION, DURING APPROACH HAD SLAT FAIL MESSAGE. 2L72 4F RTA56NM 20100126 EA 2010 1 26 A6WA200940815 120100101A3010 ANTI-ICE SYSTEM CNDAIRCL600 CL6002B19 1900309EA WARNING MESSAGE A A6WAO OTHER J WARNING INDICATION TOTAKEOFF 1 GL31448AW 7814 ANTI ICE DUCT WARNING ON TAKE OFF SYNOPTIC PAGE INDICATES LEFT FUSELAGE, MESSAGE DID NOT CLEAR WHEN 14TH STAGE AIR SELECTED OFF. C/A IN PROGRESS. 2L72 4F RTA21EA 20100126 EA 2010 1 26 ASOA201000076 120100118A5210 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA PAX DOOR CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27834AS 7254 PAX DOOR AFT ANCHOR FITTING CRACKED. R & R AFT ANCHOR FITTING ON PASSENGER DOOR IAW AMM 52-11-17. OPS CHECK GOOD. PERFORMED RII SATISFACTORY IAW SP 607 ON INSTALLATION OF AFT PASSENGER DOOR ANCHOR. R & R AFT ANCHOR FITTING ON PASSENGER DOOR IAW AMM 52-11-17. OPS CHECK GOOD. PERFORMED RII SATISFACTORYON INSTALLATION OF AFT PASSENGER DOOR ANCHOR IAW SP 607. 2L72 4F RTA21EA 20100126 EA 2010 1 26 ASOA201000077 120100118A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 409-559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 RT FLOOR SEAT TRACKS FROM FS 409 TO FS 559 ARE CORRODED. REMOVED CORRODED SEAT TRACK FROM FS 409 TO FS 559 RBL 9.0 IAW AMM 53-01-11000-802, PG 401, STEP 3.B.(1)(2)(3). INSTALLED NEW TRACK FROM FS 409 TO FS 559 RBL 9.0 IAW AMM 53-01-11-400-802 PG 406 STEP 2.B.(1) THRU (8). 2L72 4F RTA21EA 20100126 EA 2010 1 26 ASOA201000078 120100118A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 409-559 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 LT FLOOR SEAT TRACKS FROM FS 409 TO FS 559.0+80 ARE CORRODED. REMOVED CORRODED SEAT TRACK LT FS 409 TO FS 559.0+80 IAW AMM 53-01-11-000-802 STEP 3, B(1)(2)(3). INSTALLED NEW SERVICEABLE SEAT RAIL FS 409 TO FS 559.0+80 LT IAW AMM 53-01-11-400-802, STEP 2B (1)(2)(3)(4)(5)(6)(7) AND (8). 2L72 4F RTA21EA 20100126 SO 2010 1 26 C2XA10IA015 120100113A49304504726 FUEL LINE EMB 145 EMB145XR 3260214SO APU LEAKING A C2XAA UNSCHED LANDING KB FLUID LOSS SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2711127 145697 IAH - FLIGHT 2337, THE CREW REPORTED, SMELLED FUEL AFTER T/O WITH THE APU RUNNING BLEEDS AND AGAIN AFTER STARTING THE APU UPON PARKING AT IAH. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL LINE, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20100126 EA 2010 1 26 ASOA201000053 120100115A5340 ANCHOR FITTING CNDAIRCL600 CL6002B19 1900309EA CARGO BAY CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 CARGO BAY ANCHOR FITTINGS (2) ON LBL 9.0 AND AFT ANCHOR FITTING ON LBL 27.0 ARE CORRODED (3) TOTAL. (OPEN) 2L72 4F RTA21EA 20100126 EA 2010 1 26 ASOA201000054 120100115A5347 SEAT TRACK CNDAIRCL600 CL6002B19 1900309EA BS 614-618 CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 CARGO BAY SEAT TRACK SEGMENT LBL 9.0 FS 614.0 TO FS 618.0 IS CORRODED. (OPEN) 2L72 4F RTA21EA 20100126 NM 2010 1 26 UALA2010011800210120100116A361079027013 PRIORITY VALVE BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE RT ENGINE FAULTY A UALAO OTHER O OTHER TXTAXI/GRND HDL 1 WP29667UA 29239 RIGHT ENG PRV VALVE EICAS ON TAXI IN. UNABLE TO RUN ENGINE IN KOA. LOCKED OUT PRV VALVE. REPLACED RT ENG PRV. 2L72 4F4 FRTA1NM E24NE 20100126 EA 2010 1 26 ASOA201000055 120100115A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 559 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27840AS 7290 FOUND FS 559 BULKHEAD WEB RT SIDE HAS 2 INDICATIONS NOTED: OTBD OF RBL 9.0 WL 58-70 APPROX .2" IN LENGTH 70 PERCENT FSH AND 2) INBD OF RBL 18.0 WL 59.10 APRROX .4" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. REPAIRED PRESSURE BULKHEAD WEB & CAP ANGLES IAW REO 601R-53-41-260 REV D, STEPS 1 THRU 14. C/W EC/TC REO 601R-53-41-260, IAW REO 601R-53-41-260 REV D. 2L72 4F RTA21EA 20100126 EA 2010 1 26 ASOA201000056 120100115A5220 HANDLE CNDAIRCL600 CL6002B19 1900309EA EMERGENCY EXIT OUT OF TOLERANCEA ASOAK NONE L NO TEST ININSP/MAINT 1 SO27844AS 7317 RT EMERGENCY EXIT FAILS FUNCTION TEST, HANDLE RELEASES AT 50-55 LBS. ADJUSTED RT EMERGENCY EXIT DOOR IAW AMM 52-21-00-720-001 SECTION A2 TO A6 AND AMM 51-21-00-863-004. DISPOSITION OF THE LOW GAP CLEARANCE BETWEEN AFT TOP CORNER AND RT SIDE EMERGENCY EXIT DOOR COMPLETED IAW REO 601R-52-21-051 AND MEETS WITH ALL ITS REQUIREMENTS. 2L72 4F RTA21EA 20100126 EA 2010 1 26 ASOA201000057 120100115A5220 PLACARD CNDAIRCL600 CL6002B19 1900309EA ESCAPE HATCH WORN A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 CREW ESCAPE HATCH PLACARDS ARE WORN. (OPEN) 2L72 4F RTA21EA 20100126 SO 2010 1 26 DUFA20100005 220100119A8520642399 CONNECTING ROD CESSNA402 402B 207590PCE CONT O520 TSIO520E 17040SO ENGINE DESTROYED E DUFAA UNSCHED LANDING Y ENGINE STOPPAGE CRCRUISE 1 GL273796C1452 1452 C402B0803 815200R WHILE IN CRUISE FLIGHT, THE PILOT REPORTED THE LT ENG SUDDENLY LOST FUEL FLOW AND RPM. HE ATTEMPTED TO RESTART THE ENGINE SELECTING OTHER FUEL SOURCES WITHOUT SUCCESS. HE THEN FEATHERED THE PROPELLER AND PROCEEDED TO THE NEAREST SUITABLE AIRPORT WHERE HE MADE AN UNEVENTFUL LANDING. UPON ARRIVAL, MX WAS NOTIFIED AND A MECHANIC DISPATCHED TO INVESTIGATE THE POSSIBLE CAUSE. WHEN THE ENG COWLING WAS REMOVED IT WAS DISCOVERED THAT THE NR 5 CONNECTING ROD HAD FAILED AND PUNCTURED A HOLE IN THE TOP OF THE ENG CASE. THE DIPSTICK WAS PULLED AND FOUND TO STILL HAVE TEN QUARTS OF OIL REMAINING. NO DEFINITE CAUSE OF THE ROD FAILURE IS KNOWN AT THIS TIME. 1L72 3O3 O A7CE E8CE 20100126 EA 2010 1 26 ASOA201000047 120100115A2560 FLASHLIGHT CNDAIRCL600 CL6002C10 1390015EA COCKPIT INTERMITTENT A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27713EV 10081 FO'S FLASHLIGHT INTERMITTENT. 2L72 4F RTA21EA 20100126 CE 2010 1 26 DXTA2010012203950120100121A3240 BRAKE ASSY CESSNA500 560CESSNA 2076750CE MLG WEAK E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07318QS 5600418 DURING TAXI FO SIDE RT BRAKE PEDAL WENT ALL THE WAY DOWN WITH NO PRESSURE. BLED RT BRAKE IAW MM 32-42-00. PERFORMED TAXI CHECK. OPS CHECK GOOD IAW MM 32-42-01. 2L72 4F RTA22CE 20100126 CE 2010 1 26 DXTA2010012203951120100121A2820 FUEL TANK CESSNA750 750 2076810CE RT WING OVERSERVICED E DXTAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CRCRUISE 1 GL07928QS 7500418 AFTER BEING ESTABLISHED IN LEVEL FLIGHT FOR 20+ MINUTES AT FL260 - AMBER "WING TANK O'FULL R" EICAS MSG DISPLAYED. FOLLOWED CHECKLIST. NOTICED FUEL VENTING FROM RT WING TIP. DEFUELED RT WING TANK, GAINED ACCESS TO AND INSPECTED VENT HOSE POSITION WITH NO DEFECTED NOTED. REPLACED RT WINGS VENT SYS VENT FLAPPER VALVE AND VENT TANK FLAPPER VALVE WITH NEW VALVES. REFUELED TANK; NO DEFECTS NOTED. LEAK CHECK RT WING FUEL PANELS GOOD IAW MM 28-10-01. 2L72 4J RTT00007WI 20100126 CE 2010 1 26 DXTA2010012203952120100121A5230 SEAL CESSNA750 750 2076810CE CARGO DOOR NICKED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07907QS 7500201 RECEIVED AMBER CABIN ALT CAS MESSAGE & SHORTLY AFTER A RED CABIN ALT CAS MESSAGE. ALSO RECEIVED AN AMBER CARGO SEAL MESSAGE BUT NO PROBLEM WITH CABIN ALTITUDE. HANDLED IAW CHECK LIST. ON POST FLT INSP, CARGO DOOR SEAL LOOKED NICKED. PERFORMED OPS CHK OF CARGO DOOR SEAL, NO MESSAGE ILLUMINATED. NO DEFECTS/LEAKS NOTED. CHKD CORRECT ADJUST OF VALVE. CHK`D CORRECT OPS & CLEANLINESS OF VALVE PLUNGER. OPS CHK GOOD. NO OBSTRUCTIONS NOTED IN WATER SEPARATOR DRAIN ORIFICE. PRESSURIZED ACFT, NO LKS NOTED. VERIFIED CHECK VALVE HOLDING PRESSURE. CHK`D OPS OF CARGO HEAT SOLENOID & CARGO FAN. CHK`D CORRECT SYS PRESSURE TO SEAL. LK & OPS CHK SEAL GOOD. MX PEFORMED IAW SEAL EICAS T/S CHART & MM 52-31-01. 2L72 4J RTT00007WI 20100126 EA 2010 1 26 ASOA201000048 120100115A3350 BATTERY PACK CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27741EV 10155 EMERGENCY LIGHT OVER THE RT EXIT EMERGENCY DOOR INOP. REPLACED BATTERY PACK IAW ASA AMM 33-51-17. OPS CK OK. 2L72 4F RTA21EA 20100126 EU 2010 1 26 DALA100943259 120100121A5320 FLOOR SUPPORT AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27359NW 846 DURING "M" CHECK FOUND CORROSION ON FLOOR SUPPORT AT Y1292. REPAIRED IAW SRM 51-44-11 AND SRM 51-42-11. 2L72 4F RTA28NM 20100126 EA 2010 1 26 ASOA201000068 120100116A5730 SKIN CNDAIRCL600 CL6002B19 1900309EA WING CORRODED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27904EV 7628 INDICATIONS OF CORROSION NOTED AT WS 231.0 (650BB) ON THE FLAT LANDING SURFACE OF LOWER WING PLANK APPROX 70 PERCENT FULL SCREEN HEIGHT. AREAS MARKED ON ACFT. C/W EC/TC EO 600-57-81, C/W IAW REO 601R-57-21-030 REV G AND FWDED ALL REQUIRED FORMS TO STRUCTURE ENGINEERING. 2L72 4F RTA21EA 20100126 NM 2010 1 26 F3LA2010011500301120100106A5311 FRAME AIRBUSA319 A319111 3930336NM ZONE 100 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM21918FR 58 1943 DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 59 HAS EVIDENCE OF CORROSION IN FASTENER HOLES. MX REMOVED AND REPLACED FITTING IAW EA A9-53R-31612 AND EA A9-53R-31625. 2L72 4F RTA28NM 20100126 EA 2010 1 26 ASOA201000069 120100117A5340 ATTACH FITTING CNDAIRCL600 CL6002B19 1900309EA BS 460 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 MAIN CABIN FS 460.00 AT RBL 9.00 INTERCOSTAL ATTACH FITTING CRACKED IN RADIUS ON AFT SIDE. REMOVED INTERCOSTAL FROM ACFT. INSTALLED INTERCOSTAL IAW SRM 51-42-21 AND SRM 51-42-06. 2L72 4F RTA21EA 20100126 NM 2010 1 26 F3LA2010011500300120100114A5320D5347648720000 CHANNEL AIRBUSA319 A319111 3930336NM ZONE 100 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM21918FR 58 1943 DURING C5 C-CHECK INSP NOTED AFT PIT FRAME 59 FWD U CHANNEL CORRODED AT FASTENER HOLES. MX REMOVED AND REPLACED CHANNEL IAW SRM 51-42-11, SRM 51-44-11 AND SRM 51-75-11. 2L72 4F RTA28NM 20100126 NM 2010 1 26 GTIA1000001 120100117A5210 DAMPER AIRBUSA319 A319132 3930340NM IAE V2524 V2524A5 NE L4 DOOR ASSIST DAMAGED A GTIAK NONE O OTHER ININSP/MAINT 1 GL23507NK 2560 L4 DOOR ASSIST DAMPER MISSING INTERNAL SPRING / REMOVED AND REPLACED L4 DOOR ASSIST DAMPER. 2L72 4F4 FRTA28NM E40NE 20100126 WP 2010 1 26 DHLA201000003 120100114A3350 LAMP DOUG DC8 DC873 302199CWP EMERGENCY LIGHTSINOPERATIVE A DHLAK NONE O OTHER ININSP/MAINT 1 GL05807DH 45990 DURING EMERGENCY LIGHTING CHECK, ONLY 2 OF THE 3 REQUIRED LTS ILLUMINATED ON INSTRUMENT PANEL GLARESHIELD. RELAMPED IAW MM 33-50. OPS CK OK IAW MM 33-5. FOUND DURING CHECK, ACFT WAS GROUNDED. 2L74 4F RT4A25 20100126 EU 2010 1 26 DALA100853234 120100120A5310 PROFILE AIRBUS320 A320212 3930322EU EMERGENCY EXIT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27334NW 339 DURING "H" CHECK FOUND CRACK IN RT FWD EMERGENCY EXIT DOOR AFT SIDE PROFILE BEAM CRACKED. REPAIRED IAW SRM 51-42-11 AND SRM 51-44-11. 2L72 4F RTA28NM 20100126 NM 2010 1 26 DALA100926310 120100120A3350 CONNECTOR BOEING747 747451 1384940NM EMERGENCY LIGHTSDISLODGED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27670US 24225 DURING LAYOVER CHECK, MX FOUND THE ZONE 'D' LT SIDE EMERGENCY FLOOR LIGHTS INOPERATIVE. MX RESEATED THE CONNECTOR AT ROW 43ABC. EMERGENCY FLOOR LIGHTING TESTED NORMAL. 2L74 4F RTA20WE 20100126 EU 2010 1 26 DALA100863259 120100120A5315 FLOORBEAM AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27359NW 846 DURING "M" CHECK FOUND CORROSION ON FLOOR SUPPORT BEAM AT Y765 FR66-FR70. REPAIRED IAW SRM 51-44-11. 2L72 4F RTA28NM 20100126 EU 2010 1 26 DALA100873259 120100120A5320 FLOOR SUPPORT AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27359NW 846 DURING "M" CHECK FOUND CORROSION ON FLOOR SUPPORT AT Y765 FWD OF FR66. REPAIRED IAW SRM 51-42-11. 2L72 4F RTA28NM 20100126 WP 2010 1 26 DALA100539751 120100116A5220 PAN DOUG DC9 DC941 302207NWP EMERGENCY EXIT CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27751NW 47115 DURING "L CHECK AND INSPECTION IAW EA 98-89790 FOUND CRACK IN LT FWD EMERGENCY DOOR PAN BEYOND PREVIOUS STOP DRILL. REPLACED LT FORWARD EMERGENCY EXIT DOOR IAW MM 52-21-01. 2L72 4F A6WE 20100126 NM 2010 1 26 F3LA2010012100306120100118A5320D53480043206 SILL AIRBUSA319 A319111 3930336NM ZONE 100 CORRODED A F3LAK NONE O OTHER ININSP/MAINT 1 NM21942FR 81 2497 DURING C3 C-CHECK INSP NOTED THE L2 DOOR SILL INBD FLANGE FASTENER HOLE CORRODED. MX REPAIRED IAW SRM 53-41-14, SRM 51-23-11 AND SRM 51-42-11. 2L72 4F RTA28NM 20100125 NM 2010 1 25 SWAA100266 120100118A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500C, STR 8L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100273 120100114A3350207377 LENS BOEING737 7377H4 1384404NM CABIN CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29440LV 29835 DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS LENS CRACKED AT ROW 10. REMOVED AND REPLACED LENS PER MM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100284 120100119A52406516300 DOOR FRAME BOEING737 7373H4 1384600NM R1 DOOR CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR AFT SIDE FRAME CRACKED. REPAIRED FRAME PER SRM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100287 120100119A53226546546 SHEAR TIE BOEING737 737301 138447RNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100291 120100115A53306545774 SKIN BOEING737 737301 138447RNM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29660SW 23230 DURING SCHEDULED 2HC2 CHECK, FOUND SKIN CRACKED AT BS 786, STR 19L. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100298 120100119A53116558280 FRAME BOEING737 7377H4 1384404NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29704SW 27838 DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100306 120100116A5743115A5211 FITTING BOEING737 7377H4 1384404NM LT MLG TRUNNION CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29775SW 30590 DURING SCHEDULED MV2 CHECK, FOUND LT MLG TRUNNION FITTING LUG FACES CORRODED. REPAIRED FITTING PER EA. 2L72 4F RTA16WE 20100125 NM 2010 1 25 SWAA100314 120100117A53306545767 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29388SW 26591 DURING SCHEDULED MV2 CHECK, FOUND SKIN CRACKED AT BS 1000, STR 5R. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20100125 2010 1 25 SWAA100350 420100120A2565D31354 SLIDE BOEING737 7373H4 1384600NM L1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29651SW 27721 L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT. 2L72 4F RTA16WE 20100126 WP 2010 1 26 DALA100519751 120100116A5530 FORMER DOUG DC9 DC941 302207NWP VERTICAL STAB LOOSE A DALAK NONE O OTHER ININSP/MAINT 1 SO27751NW 47115 DURING "L" CHECK FOUND 3 EA BLIND FASTENERS LOOSE IN VERTICAL STABILIZER FORMER. REPAIRED IAW SRM 55-30-0, SRM 55-31-0 & SRM 51-30-8. 2L72 4F A6WE 20100126 EU 2010 1 26 DALA100893259 120100120A5321 FLOOR PANEL AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27359NW 846 DURING "M" CHECK FOUND CORROSION ON FLOOR PANEL 262FF. REPLACED IAW CARD 2500-6002. 2L72 4F RTA28NM 20100126 NM 2010 1 26 DALA100496309 120100117A5310 BEAM BOEING747 747451 1384940NM FUSELAGE DAMAGED A DALAK NONE O OTHER ININSP/MAINT 1 SO27669US 24224 DURING "L" CHECK FOUND SHORT EDGE MARGIN ON SHEAR BEAM AT MAIN DECK CREW REST. REPAIRED IAW ERA 473036-14AD AND CARD 5300-01047-01B. 2L74 4F RTA20WE 20100126 NM 2010 1 26 DALA100506309 120100117A5347 CARGO TRACK BOEING747 747451 1384940NM BS 1862 CRACKED A DALAK NONE O OTHER ININSP/MAINT 1 SO27669US 24224 DURING "L" CHECK FOUND CRACK IN RT OTBD CARGO TRACK AT BS 1862 RT. REPAIRED IAW SRM 53-00-52. 2L74 4F RTA20WE 20100126 EA 2010 1 26 A6WA200940816 120100101A30107858062 CONTROLLER CNDAIRCL600 CL6002B19 1900309EA ADHC MALFUNCTIONED A A6WAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL31450AW16538 7823 JUST AFTER TAKEOFF RECEIVED TAT PROBE HEAT RT AOA HEAT, RT STATIC HEAT, RT PITOT HEAT CAUTION MESSAGES CW QRH MESSAGES PERSISTED. R & R NR 2 AIR DATA HEAT CONTROLLER IAW AMM 30-31-15. OPS CHECK GOOD. 2L72 4F RTA21EA 20100126 EA 2010 1 26 A6WA201040021 120100111A2797 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA TE FLAPS SYS CONTAMINATED A A6WAO OTHER J WARNING INDICATION LDLANDING 1 GL31453AW 7838 ON ARRIVAL THE FLAPS FAILED AT 20 DEGREES WHEN ATTEMPTED TO SELECT 30 DEGREES. INITIATED A GO-AROUND AND COMPLIED WITH THE QRH THEN MADE A 20 DEGREE FLAP LANDING. AN EMERGENCY WAS DECLARED. AS PART OF FLAP FAIL TROUBLESHOOTING: MEGOHM CKD TRANSDUCER CIRCUIT FOR THE LT AND RT BPSU WIRING HARNESSES. NO FAULTS FOUND AT THIS TIME. FOUND FLUID IN LT BPSU CONNECTOR PLUG. CLEANED AND REAPPLIED SUPER CORR B. ALSO CLEANED RT BPSU CONNECTOR PLUG AND APPLIED SUPER CORR B. CKD BOTH FLAP POSITION TRANSMITTER CONNECTOR PLUGS AND NO DEFECTS NOTED. ALSO CLEANED CONNECTOR NR 1 P5CE AT STA 559 IAW FIM 27-50-00, ITEM 20, PG 136. 2L72 4F RTA21EA 20100126 SO 2010 1 26 C2XA10IA016 120100114A799723061442 WIRE HARNESS EMB 145 EMB145XR 3260214SO NR 1 ENGINE FAULTY A C2XAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 SW2734111 145659 IAH - FLIGHT 2333, THE CREW REPORTED ABNORMAL OIL PRESSURE NUMBER ONE ENGINE AT CRUISE ALTITUDE FL350 WITH 135 PSI. THE OIL PRESSURE REMAINED IN THE AMBER RANGE FOR 8 MINUTES, AND DURING DESCENT AT 6000FT THE OIL PRESSURE WENT BACK INTO THE AMBER RANGE FOR SIX MINUTES & 130 PSI, AND NOTED THAT THE OIL PRESSURE NEVER WENT INTO THE RED RANGE. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE EIS HARNESS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20100126 SO 2010 1 26 C2XA10IA017 120100115A21208151133 DUCT EMB 145 EMB145XR 3260214SO AC BAY LOOSE A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2711119 145677 IAH - FLIGHT 2160, THE CREW REPORTED THAT THE PACK TWO VALVE WOULD NOT OPEN AFTER TAKEOFF AND COULD NOT GET IT OPEN AFTER MULTIPLE RESETS. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED A DUCT ON THE NR 2 PACK DUAL TEMP CONTROL VALVE, OPERATIONAL AND LEAK CHECKS COMPLETED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20100126 SO 2010 1 26 C2XA10IA019 120100115A36107276045 FILTER EMB 145 EMB145LR 3260212SO BLEED AIR SYS DIRTY A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2713997 145298 IAH - FLIGHT 2992 THE CREW REPORTED A BLD 1 OVERTEMP MESSAGE ON EICAS AT 1000FT ON T/O IN ICING CONDITIONS. THE MESSAGE CLEARED IN LESS THAN ONE MINUTE, THE QRH WAS ACCOMPLISHED WITH NORMAL OPS AFTER THAT. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 FAN AIR VALVE FILTER, LEAK AND OPERATIONAL CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20100126 SO 2010 1 26 C2XA10IA020 120100116A36208166248 SENSOR EMB 145 EMB145LR 3260212SO BLEED AIR SYS INOPERATIVE A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW2713997186211375 145298 IAH - FLIGHT 2573, THE CREW REPORTED A NR 1 BLEED OVERTEMP INDICATION WITH WING ANTI-ICE ON. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 FAN AIR SENSOR, AND NR 1 PRE-COOLER. OPERATIONAL AND LEAK CHECKS WERE ACCOMPLISHED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20100126 SO 2010 1 26 C2XA10IA022 120100117A335020131A BATTERY PACK EMB 145 EMB145LR 3260212SO CABIN DISCHARGED A C2XAK NONE L NO TEST ININSP/MAINT 1 SW27139905929 425 145277 IAH - FLIGHT 2314, DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ARM. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE AND NUMBER TWO EMERGENCY LIGHT BATTERY PACKS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20100126 SO 2010 1 26 C2XA10IA024 120100117A33507287103507 CONTROL PANEL EMB 145 EMB145LR 3260212SO CABIN INOPERATIVE A C2XAK NONE O OTHER ININSP/MAINT 1 SW2713990 145277 IAH - DURING PREFLIGHT INSPECTION THE CREW REPORTED THAT THE EMERGENCY LIGHTS WOULD NOT ARM. MAINTENANCE REMOVED AND REPLACED THE CABIN / EMERGENCY LIGHT CONTROL PANEL, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20100126 NM 2010 1 26 SWAA100323 120100119A53406546541 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663, STR 10R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100324 120100119A53406546541 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 663.75, STR 10L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100325 120100119A53406546541 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100326 120100119A53406546541 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 578, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100327 120100118A53306545765 SKIN BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29383SW 26589 DURING SCHEDULED MV1 CHECK, FOUND SKIN CRACKED BS 513C, STR 6L. REPAIRED SKIN PER EA. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100328 120100119A335065C27093 COVER BOEING737 7373H4 1384600NM CABIN LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29387SW 26602 DURING SCHEDULED MV1 CHECK, FOUND L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100329 120100118A335081000 LIGHT BOEING737 7377H4 1384404NM CABIN INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29402WN 29814 DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS INOP AT ROW 1. RELAMPED PER MM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100330 120100118A3350D71701100 BATTERY BOEING737 7377H4 1384404NM CABIN FAILED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29454WN 29851 DURING SCHEDULED HC1 CHECK, EMERGENCY EXIT BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM. 2L72 4F RTA16WE 20100126 2010 1 26 SWAA100331 420100119A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29454WN 29851 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100332 120100118A25606557463 FITTING BOEING737 7377H4 1384404NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29497WN 32479 DURING SCHEDULED SPV CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100333 120100118A25606557463 FITTING BOEING737 7377H4 1384404NM GIRT BAR LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29497WN 32479 DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100334 120100119A256065C34691 GIRT BAR BOEING737 7373H4 1384600NM EVAC SLIDE LOOSE A SWAAK NONE O OTHER ININSP/MAINT 1 SW29630WN 27705 DURING SCHEDULED 14Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT MATERIAL LOOSE. REMOVED AND REPLACED GIRT ASSY PER MT. 2L72 4F RTA16WE 20100126 NM 2010 1 26 SWAA100335 120100119A53226545776 SHEAR TIE BOEING737 737301 138447RNM FUSELAGE CORRODED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29659SW 23229 DURING SCHEDULED SPV CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 27R TO STR 27L. REMOVED AND REPLACED SHEAR TIE PER SRM. 2L72 4F RTA16WE 20100126 SO 2010 1 26 C2XA10010 120100121A2120 UNKNOWN EMB 145 EMB145XR 3260214SO CABIN ODOR A C2XAK NONE B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2711119 145677 CLE FLT 2181 THE CREW REPORTED A ABNORMAL SMELL ASSOCIATED WITH THE NR 2 PACK IN ICING CONDITIONS. MAINTENANCE INSPECTED AND PERFORMED OPERATIONAL CHECKS OF THE NR 2 PACK AND NO DEFECTS OR SMELLS WERE FOUND. 2L72 4F RT 20100202 SO 2010 2 2 C2XA10CL011 120100125A26123601133500230C90FIRE DETECTOR EMB 145 EMB145LR 3260212SO NR 1 NACELLE FAULTY A C2XAO OTHER N FALSE WARNING NRNOT REPORTED 1 SW271399417885 145291 BWI FLT 2718 THE CREW REPORTED A FIRE DETECTION NR 1 FAIL MESSAGE. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE FIRE DETECTOR. OPERATIONAL CHECKS WERE GOOD. 2L72 4T RTT00011AT 20100126 2010 1 26 C2XA10IA029 420100118A34311978 ANTENNA EMB 145 EMB145XR 3260214SO ILS INOPERATIVE A C2XAA UNSCHED LANDING O OTHER APAPPROACH 1 SW27311312651 2651 145705 TUL - FLIGHT 2415, THE CREW REPORTED THAT ON APPROACH INTO MCI THE ILS SYSTEM WAS INOPERATIVE. THE AIRCRAFT DIVERTED TO TUL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED THE ILS ON MEL 34-32-00/1 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED BOTH VOR/ILS ANTENNAS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20100126 SO 2010 1 26 C2XA10IA032 120100121A26973601133500230C90CONNECTOR EMB 145 EMB145XR 3260214SO FIRE LOOP DIRTY A C2XAO OTHER J WARNING INDICATION CRCRUISE 1 SW27111091685516855 145657 IAH - FLIGHT 2758 THE CREW REPORTED THAT THE NUMBER TWO ENGINE FIRE DETECTOR FAIL MESSAGE CAME ON INTERMITTENTLY DURING FLIGHT. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE CLEANED AND RE-SECURED THE CONNECTOR ON THE ENGINE ONE FIRE LOOP, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20100126 SO 2010 1 26 C2XA10IA033 120100122A2120 CLAMP EMB 145 EMB145EP 3260221SO AC SYSTEM LOOSE A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2716944 145045 IAH - FLIGHT 2165, THE CREW REPORTED THAT THE PACK 2 VALVE CLOSED TWICE DURING CLIMB. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT, RE-SECURED SEVERAL CLAMPS, OPERATIONALLY TESTED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20100126 SO 2010 1 26 C2XA10IA034 120100122A3610 CLAMP EMB 145 EMB145EP 3260221SO BLEED AIR SYS LOOSE A C2XAO OTHER J WARNING INDICATION CLCLIMB 1 SW2716944 145045 IAH - FLIGHT 2165, THE CREW REPORTED THAT THE BLEED 1 VALVE CLOSED FROM T/O TO 10'000 FEET. THE AIRCRAFT CONTINUED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND RE-SECURED SEVERAL CLAMPS, OPERATIONAL AND LEAK CHECKS WERE ACCOMPLISHED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20100126 SO 2010 1 26 C2XA10IA036 120100122A21208151133 SLEEVE EMB 145 EMB145XR 3260214SO NR 2 PACK BURNED A C2XAA UNSCHED LANDING B SMOKE/FUMES/ODORS/SPARKS CLCLIMB 1 SW2714162 14500808 IAH - FLIGHT 2857 THE CREW REPORTED A BURNING SMELL AFTER TAKE OFF. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, AND REMOVED AND REPLACED A BURNT SLEEVE ON THE NUMBER TWO PACK DUAL TORQUE MOTOR, OPERATIONALLY AND LEAK CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RT 20100126 2010 1 26 SWIA201023386 420100101A3120 UNKNOWN CNDAIRCL600 CL6002B19 1900309EA COCKPIT MALFUNCTIONED A SWIAO OTHER N FALSE WARNING APAPPROACH 1 NM06507CA 7796 ON APPROACH, NUMEROUS COCKPIT INSTRUMENT WARNINGS AND FLAGS DISPLAYED, EMERGENCY DECLARED. (FLT 6830) POWERED DOWN AIRCRAFT, ALL OPERATIONAL AND FUNCTIONAL CHECKS NORMAL. 2L72 4F RTA21EA 20100126 EA 2010 1 26 SWIA201023387 120100103A5210 ROLLER CNDAIRCL600 CL6002B19 1900309EA CABIN DOOR LACK OF LUBE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06943SW 7762 UNABLE TO OPEN MAIN CABIN DOOR. (FLT 6472) LUBED INNER DOOR HANDLE ROLLER. 2L72 4F RTA21EA 20100126 EA 2010 1 26 SWIA201023392 120100101A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN SATURATED A SWIAK NONE O OTHER UKUNKNOWN 1 NM06955SW 7817 EMERGENCY LIGHT OPERATION ABNORMAL. (FLT 6438) REPLACED RELAY AND REMOVED WATER FROM CONNECTOR. 2L72 4F RTA21EA 20100126 EA 2010 1 26 SWIA201023393 120100101A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06614SK 10051 NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 4556) RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100126 EA 2010 1 26 VNAA2010010600003120100101A2750860D10018 ECU CNDAIRCL600 CL6002B19 1900309EA TE FLAP FAILED A VNAAA UNSCHED LANDING O OTHER TOTAKEOFF 1 GL05250PS 662 7929 CREW REPORTED FLAPS FAILED ON RETRACTION AT 12°. AIRCRAFT RETURNED TO PNS LANDING WITHOUT INCIDENT. USING THE AIRCRAFT MAINTENANCE MANUAL AND FAULT ISOLATION MANUAL MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20100127 SO 2010 1 27 SWIA201023406 120100101A3350 LIGHT EMB 120 EMB120ER 3260203SO CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06583SW 120351 EMERGENCY LIGHT AT FORWARD DOOR INOP. (FLT 6299) RELAMPED EMERGENCY LIGHT. 2L72 4T RTA31SO 20100127 NM 2010 1 27 ZZDA2010008 120100110A3350 LIGHT BOEING737 7377BD 1384511NM CABIN BROKEN A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37296AT 34861 LEFT EMERGENCY LIGHT STRIP IN ROW 1 BROKEN. REPLACED LIGHT STRIP IAW 737 AMM CH 33-51. 2L72 4F RTA16WE 20100127 EA 2010 1 27 SWIA201023414 120100106A7120 MOUNT CNDAIRCL600 CL6002B19 1900309EA GE CF34 CF34* 30015NE LT ENGINE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM06913SW 7597 LEFT ENGINE FORWARD LINK AND BUSHING PITTED. (ENG CHANGE) REPLACED YOKE LINK AND BUSHING. 2L72 4F4 FRTA21EA 20100127 EA 2010 1 27 SWIA201023415 120100105A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06906SW 7510 EMERGENCY CEILING LIGHT NR 2 INOP. (FLT 6757) RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100127 EA 2010 1 27 SWIA201023417 120100103A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06453SW 7743 OVERWING EMERGENCY LIGHT INOP. (FLT 4778) RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100127 EA 2010 1 27 SWIA201023420 120100103A7120 MOUNT CNDAIRCL600 CL6002C10 1390015EA LT ENGINE CORRODED A SWIAK NONE O OTHER ININSP/MAINT 1 NM06752SK 10209 LEFT ENGINE MOUNT UPPER YOKE LINK AND BUSHING CORRODED. (ENG CHANGE) REPLACED LEFT ENGINE MOUNT UPPER YOKE LINK AND BUSHING. 2L72 4F RTA21EA 20100127 EU 2010 1 27 FDEA201001210207 120100121A276031059321 ACTUATOR AIRBUS310 A310222 3930315EU SPEEDBRAKES DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21453FE 267 DURING T/S FOUND RT NR 2 SPEEDBRAKE ACTUATOR'S ROD END BROKEN ALSO THE INBD FLAP NEAR THE SPEEDBRAKE ACTUATOR DAMAGED ABOUT 2IN X 1.5 IN. R & R RT INBD FLAP VANE IAW AMM 27-50-11-4. OPS CHECK NORMAL . REF DISCREPANCY 2760 9380 FOR SPEEDBRAKE ACTUATOR CHANGE CHECKED FOUND RT NR 2 SPEEDBRAKE ACTUATOR'S ROD END BROKEN ALSO THE INBD FLAP NEAR THE SPEEDBRAKE ACTUATOR DAMAGED ABOUT 2 IN X 1.5 IN . 2L72 4F RTA35EU 20100127 NM 2010 1 27 FDEA201001140194 120100114A5315652082761 FLOORBEAM BOEING727 727227 1384078NM BS 560 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21489FE 21492 CABIN FLOORBEAM BS 560 LBL 24- 45 UPPER FLANGE LOWER SURF HAS CORROSION AT N/P'S. REMOVED CORROSION IAW SRM 51-10-6, UT INSPECTED AREA IAW NDTM 51-00-00 FIG 3 PART 4, FOUND OUT OF LIMITS IAW PF SRM (ER 01-049) 53-10-1 FIG 4B REV C, REMOVED STIFFENER FOR ACCESS IAW 51-30-2 CUT OUT DAMAGED AREA IAW SRM 53-10-8 FIG 8 DETAIL II, FABRICATED REPAIR PARTS IAW SRM 53-10-8 FIG 8, TREATED AND PRIMED REPAIR PARTS IAW SRM 51-10-2, INSTALLED REPAIR PARTS AND STIFFENERS AT CABIN FLOORBEAM BS 560 LBL 24-45 IAW SRM 53-10-8 FIG 8. 2L73 4F A3WE 20100127 EA 2010 1 27 SWIA201023424 120100103A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06706SK 10149 OVERHEAD EMERGENCY LIGHT NR 6 INOP. (FLT 6366) RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100127 EA 2010 1 27 SWIA201023425 120100103A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06774SK 10240 OVERHEAD EMERGENCY FLOODLIGHT INOP. (FLT 5876) RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100127 NM 2010 1 27 FDEA201001210209 120100121A323026702887 VALVE BOEING757 75728A 1384976NM MLG FAILED A FDEAO OTHER J WARNING INDICATION LDLANDING 1 CE21912FD 24260 ON APPROACH, PUT GEAR LEVER DOWN. GOT NO NOSE GEAR INDICATION. HAD GEAR DISAGREE MESSAGE, GEAR AND DOOR LIGHTS. RAN CHECKLIST AND LOWERED GEAR WITH ALT IXT SWITCH. COULD HEAR NOSE GEAR EXTENDING. GOT 3 GREEN INDICATIONS AND DOOR LIGHT. LANDED NORMALLY. RELEASED FOR SERVICE IAW MEL: 32-30-01. 2L72 4F RTA2NM 20100127 EU 2010 1 27 USAA20100113SB004220100110A73219387M15P12 MEC BOEING737 7374B7 138449CNM CFMINTCFM56 CFM563B2 13802EU NR 2 ENGINE UNRESPONSIVE A USAAE ENGINE SHUTDOWN O OTHER DEDESCENT 1 EA19433US463445658 24555 725142 CLT - ON DESCENT INTO CLT, THE NR 2 ENGINE WAS UNRESPONSIVE TO THROTTLE MOVEMENT / WOULD NOT ACCELERATE FROM IDLE THRUST. CREW ACCOMPLISHED ENGINE NO RESPONSE QRH CHECKLIST AND SHUT DOWN THE NR 2 ENGINE. CAPTAIN DECLARED AN EMERGENCY. FLIGHT LANDED NORMALLY AND TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. APPROXIMATE TOTAL SINGLE ENGINE TIME WAS 15 TO 22 MINUTES. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE MEC. ALSO, REPLACED THE NR 2 ENGINE FUEL PUMP. THRUST RESPONSE NORMAL AT ALL POWER SETTINGS. AIRCRAFT OK FOR SERVICE. 2L72 4F4 FRTA16WE E21EU 20100127 WP 2010 1 27 FDEA201001220219 120100122A53476010964 SEAT TRACK DOUG DC10 DC1030F 3023504WP BS 1431-1531 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 CE21306FE5754157541 48287 MCD CARGO COMPT. SEAT TRACK BETWEEN F.S. 1431 TO F.S. 1531 AT LBL 47.5 HAVE 6 EACH WORN LOBES. REMOVED AND REPLACED SEAT TRACK FROM F.S. 1431 TO F.S. 1531 AT LBL 47.5 IAW SRM 51-31-01 AND SRM 53-70-00, CLASSIED AS MAJOR REPAIR. 2L73 4F RTA22WE 20100127 EU 2010 1 27 FDEA201001180171 120100118A5247A5247132501200 SKIN AIRBUS300 A300F4605R 3930327EU APU DOOR CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21681FE 799 APU COMPARTMENT; RT ACCESS DOOR; AFT INBD CORNER; SKIN IS CRACKED AND A RIVET IS SHEARED. DRILLED OUT FASTENER IAW SRM 51-40-21, PARA 6. CUT OUT DAMAGE IAW SRM 52-41-41, PG 210. IAW SRM 52-41-11, FIG 202. FABRICATED REPAIR PARTS IAW SRM 52-41-11, FIG 202, PGS 210, 213, 214. PRIMED & PAINTED IAW SRM 51-25-10. INSTALLED REPAIR PARTS, FILLER AND DOUBLER, IAW SRM 51-40-21, PARA 7. 2L72 4F RTA35EU 20100127 NM 2010 1 27 FDEA201001150182 120100115A5347652363737 SEAT TRACK BOEING727 727227 1384078NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21489FE 21492 CABIN SEAT TRACK AT STA 720B LBL 45 OUTBD FLANGE UPPER SURF. HAS CORROSION. REMOVED SEAT TRACK SECTION LBL 45 BETWEEN STA 690 TO 740 AND 1EA SPLICER IAW SRM 51-30-2, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 53-10-5 FIG 1 TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED NEW SEAT TRACK & SPLICER IAW SRM 51-30-2. 2L73 4F A3WE 20100127 EA 2010 1 27 VNAA2010011400005120100108A2750855D10015 BPSU CNDAIRCL600 CL6002B19 1900309EA TE FLAP FAILED A VNAAA UNSCHED LANDING O OTHER CLCLIMB 1 GL05250PS120371836 7929 CREW REPORTED FLAPS FAILED AT 8° WHEN THE FLAP LEVER WAS MOVED TO 0° AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED OVERWEIGHT, BUT WITHOUT INCIDENT. USING THE AIRCRAFT MAINTENANCE MANUAL AND FAULT ISOLATION MANUAL, MAINTENANCE REMOVED AND REPLACED THE RT BRAKE AND POSITION SENSOR UNIT (BPSU). CHECKS WERE MADE AND AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED PER THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20100127 2010 1 27 USAA2010011490101420100113A2565D31516317 SLIDE AIRBUSA319 A319132 3930340NM R1 DOOR DEFECTIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19830AW35425209 1565 FLT 152 - PDX - PHX - EMERGENCY LIGHTS - FORWARD EMERGENCY POWER SUPPLY UNIT (EPSU) FAILED PERFORMANCE OF TEST OF EMERGENCY LIGHTS. INDICATES EXTERIOR LIGHTS FAULT STEP 7. REMOVED AND REPLACED R1 SLIDE PACK ASSEMBLY IAW TASK CARD R1C25305. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20100127 NM 2010 1 27 USAA2010011490102120100113A335032145410 POWER SUPPLY AIRBUSA319 A319132 3930340NM CABIN INOPERATIVE A USAAK NONE L NO TEST ININSP/MAINT 1 EA19830AW3013030130 1565 FLT 152 - PDX - PHC - EMERGENCY LIGHTS, FORWARD EMERGENCY POWER SUPPLY UNIT (EPSU) FAILED TEST. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU). OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20100127 NE 2010 1 27 USAA20090114BB001220100113A7230LK84177 LOCK PLATE BOEING757 75723N 1384973NM RROYCERB211 RB211535E4 54555NE RT ENGINE DETACHED A USAAEA ENGINE SHUTDOWN UNSCHED LANDING A FLAME/FIRE CLCLIMB 1 EA19205UW 30887 31743 FLT 1556 EN ROUTE AT 26,000 FT, CAPTAIN FELT A YAW & HEARD A COMPRESSOR STALL COMING FROM RT ENGINE. ENGINE READINGS NORMAL. HOWEVER, A PASSENGER SAW FIRE COMING FROM RT ENGINE DURING STALL. CAPTAIN DECLARED AN EMERGENCY & FLT DIVERTED. DURING TAXI TO GATE, RT ENGINE OIL PRESSURE DROPPED & OIL TEMP CLIMBED TO RED. CREW SHUTDOWN RT ENGINE & TAXIED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED RT ENGINE. REPAIR SHOP REPORTED THE COMBINATION OF HEAVY SPALLING OF ATTRITION LINING OF HPC CASES & IOD OF HPC BLADES CAUSED REPORTED HPC SURGE. IOD CAUSED BY THE LIBERATION OF STAGE 2 LOCK PLATE. 2L72 4F4 FRTA2NM E12EU 20100127 NM 2010 1 27 WRLA20100105330 120100105A5753ARC4125502 STOP FITTING DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE TE FLAP CRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11275WA 48631 DURING 01C CHECK FOUND RIGHT WING OUTBOARD FLAP STOP RIB (P/N:ARC4125-502) CRACKED AT XOF 563.244. NRC U05078 ISSUED. PER EI:W2010A57B-072 REV00 AND AMM REV66, RMV THE FLAP, RPL THE LEADING EDGE RIB, RE-INST THE FLAP. PFM AMM SUBTASK 27-50-30-830-003 TO ADJ THE OUBD FLAPS, PFM AMM SUBTASK 27-50-30-830-004 TO MAKE SURE THE FLAP DOWNSTOP IS ADJUSTED CORRECTLY, PFM SUBTASK 27-50-30-220-010 TO DO AN INSPECTION OF THE OUTBD FLAP CONTROL SURFACES. PFM SUBTASK 27-50-30-710-004 TO TEST OF THE FLAP SYSTEM OPERATION/RANGE OF MOVEMENT. ALL COND SATI'S. 2L73 4F4 FRTA22WE E24NE 20100127 EU 2010 1 27 YENA20100113007 120100113A3350321431 BATTERY AIRBUS320 A320232 3930326EU CABIN DISCHARGED A YENAK NONE L NO TEST ININSP/MAINT 1 EA15612JB19186 2447 FLT JB21 JFK-TPA DURING RON MX OPS CHECK OF EMERGENCY LIGHTS, EMERGENCY LIGHT BATTERY TEST FOUND FWD/LT FAULT. REMOVED AND REPLACED FWD/LT EMERGENCY LIGHT BATTERY AS REQUIRED IAW AMM 33-51-38-000-001, OPS CHECK NORMAL. 2L72 4F RTA28NM 20100127 NM 2010 1 27 WRLA20100105331 120100105A5343ACA7017502 FITTING DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE NLG TRUNNION CRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11275WA 48631 DURING 01C CHECK FOUND NOSE GEAR TRUNNION LT FITTING P/N ACA7017-502 CRACKED. 2L73 4F4 FRTA22WE E24NE 20100127 NM 2010 1 27 ZZDA2010009 120100110A5320 CUSP WEB BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 RIGHT CABIN CUSP PANEL LIGHTENING HOLE, STA 490, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP PANEL LIGHTENING HOLE DOUBLER AND FILLER REPAIR PER BOEING DWG 09530003. SEE NR 5186. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010010 120100110A5320 FLOOR SUPPORT BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 CABIN FLOOR SUPPORT BEAM, STA 147 TO 200, RBL7, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-01. SEE NR 5194. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010011 120100110A5313 LONGERON BOEING717 717200 1383700NM FUSELAGE CRACKED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 LEFT LONGERON FINGER WEB, STA 200, LONG L15L, CRACKED. ACCOMPLISHED LONGERON FINGER WEB DOUBLER AND FILLER REPAIR PER B717 SRM 51-70-10 FIG 201 REPAIR 1. SEE NR 5180. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010012 120100110A5320 FLOOR SUPPORT BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 CABIN FLOOR SUPPORT BEAM, STA 200, LBL 5 TO RBL 5, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-01. SEE NR 5193. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010013 120100110A5320 CUSP WEB BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 RIGHT CABIN CUSP PANEL, STA 665, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP PANEL DOUBLER AND FILLER REPAIR PER BOEING DWG 09530003. SEE NR 5188. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010014 120100110A5320 FITTING BOEING717 717200 1383700NM CABIN CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 RIGHT CABIN CUSP GRILL CLIP, STA 500, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP GRILL CLIP REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5185. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010015 120100110A5320 FITTING BOEING717 717200 1383700NM CABIN CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 RIGHT CABIN CUSP GRILL CLIP, STA 460, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP GRILL CLIP REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5184. 2L72 4F TRA6WE 20100127 NM 2010 1 27 FDEA201001150160 120100115A5313655457512 STRINGER BOEING727 727227 1384078NM BS 720B S15R CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21489FE 21492 CABIN STRINGER 15 RT BS 720B PLUS 15" HAS END CRACKED AT FASTENER. REMOVED FASTENERS AND CUTOUT DAMAGED AREA, FABRICATED REPAIR "U" CHANNEL, FILLER AND FILLER TAPER. INSTALLED IAW SRM 51-30-2, 53-10-3, AND 51-10-2. 2L73 4F A3WE 20100127 NM 2010 1 27 ZZDA2010016 120100110A5320 FITTING BOEING717 717200 1383700NM CABIN CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 RIGHT CABIN CUSP GRILL CLIP, STA 610, LONG L18R, CORROSION. ACCOMPLISHED CABIN CUSP GRILL CLIP REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5187. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010017 120100112A5320 FLOOR SUPPORT BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 CABIN FLOOR SUPPORT BEAM, STA 200, LBL 11, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5192. 2L72 4F TRA6WE 20100127 NM 2010 1 27 FDEA201001160163 120100116A575465172769 RIB BOEING727 727227 1384078NM NR 4 SLAT CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21481FE 21463 NR 4 SLAT HAS 1 CRACKED RIB ON THE OTBD SIDE OF ACTUATOR FWD MOUNT. REMOVED ACCESS PANELS ON NR 4 SLAT IAW SRM 51-30-2. REMOVED (2) RIBS INBD AND OTBD FOR ACCESS & TWO (2) RIBS DAMAGED IAW SRM 51-30-2. LOCATED & DRILLED NEW RIBS INBD AND OTBD IAW SRM 51-30-5. INSTALLED NEW RIBS & RIBS FOR ACCESS IAW SRM 51-30-2. INSTALLED ACCESS PANELS IAW SRM 51-30-2. 2L73 4F A3WE 20100127 NM 2010 1 27 ZZDA2010018 120100112A5730 RUB STRIP BOEING717 717200 1383700NM LT WING CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 LEFT WING UPPER ACCESS PANEL 520DT RUB STRIP, CORROSION. ACCOMPLISHED WING UPPER ACCESS PANEL 520DT RUB STRIP REPLACEMENT PER B717 SRM 57-10-01. SEE NR 1070. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010019 120100112A5320 FLOOR SUPPORT BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 CABIN FLOOR SUPPORT BEAM, STA 256, LBL 22 TO RBL 22, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5206. 2L72 4F TRA6WE 20100127 NM 2010 1 27 NOCA00810 120100122A5320 SILL BOEING757 75728A 1384976NM BS 1674 CORRODED A NOCAK NONE O OTHER ININSP/MAINT 1 EA15753NA 28174 4L DOOR SILL CORROSION AT BS 1674 LBL 56. REPLACED GUTTER SUPPORT BRACKET PER SRM 51-10-02. 2L72 4F RTA2NM 20100127 NM 2010 1 27 ZZDA2010020 120100114A5347 SEAT TRACK BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 CABIN SEAT TRACK, STA 200 TO 247, RBL 45, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F. SEE NR 5204. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010021 120100114A5347 SEAT TRACK BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 CABIN SEAT TRACK, STA 200 TO 256, RBL 22, CORROSION. ACCOMPLISHED SEAT TRACK SPLICE REPAIR PER DC9 SRM 53-05 FIG 4F. SEE NR 5195. 2L72 4F TRA6WE 20100127 NM 2010 1 27 ZZDA2010022 120100114A5320 FLOOR SUPPORT BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37935AT 55069 CABIN FLOOR SUPPORT BEAM, STA 256, LBL 22 TO RBL 22, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02. SEE NR 5206. 2L72 4F TRA6WE 20100127 EA 2010 1 27 U5QA06023 120100113A3620 SENSOR CNDAIRCL600 CL6002B16 1900305EA WING SHORTED E U5QAO OTHER N FALSE WARNING CRCRUISE 1 GL07895CC 5177 AIRCRAFT WAS EN ROUTE FROM KSDL TO MDSM, HAD DUCT FAIL LIGHT ILLUMINATE. CREW ELECTED TO RETURN TO BLOCK. MAINTENANCE DISCOVERED SAFETY WIRE SHORTING INTERMITTENTLY AGAINST WING DUCT TEMP SENSOR. 2L72 4F RTA21EA 20100127 EU 2010 1 27 FDEA201001200196 120100120A5321 FLOOR PANEL AIRBUS300 A300F4605R 3930327EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21681FE 15457 799 MAIN CABIN FLOOR PANEL 231 YG IS DAMAGED. REPAIRED MAIN CAB CARGO COMPARTMENT FLOOR PANEL 231 YG BY FABRICATING NEW FLOOR PANEL USING OLD FLOOR PANEL 231 YG AS TEMPLATE IAW DWG SRZ 25-005, REV "H". 2L72 4F RTA35EU 20100127 EU 2010 1 27 USAA20100119BA002120100116A5210 CYLINDER AIRBUS330 A330323 3940030EU L3 DOOR ASSIST LOW PRESSURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19276AY 0375 PHL - L3 DOOR LOW PRESSURE PER SERVICE REPORT. SERVICED L3 DOOR CYLINDER. 2L72 4F RTA46NM 20100127 NM 2010 1 27 USAA20100115SB006120100114A2450 CIRCUIT BREAKER BOEING737 7373B7 138447FNM COCKPIT OVERHEATED A USAAO OTHER MB OVER TEMP SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19532AU 24479 CREW REPORTED THE COCKPIT LIGHTING GOES FROM BRIGHT TO EITHER DIM OR OFF. AT OVERHEAD & FORWARD PANEL, THERE IS AN ODOR OF SOMETHING ELECTRICALLY HOT. HOT ODOR WAS ALSO REPORTED BY FLT ATTENDANT IN FIRST CLASS CABIN. MAINTENANCE CONFIRMED FAILURE FOR LIGHT ANOMALY & REPLACED DISCREPANT APU GENERATOR BREAKER C889 PER MM 24-21-41. AS FOR THE HOT ODOR, MAINTENANCE FOUND THE L1 AND R1 WINDOW CIRCUIT BREAKERS C228 AND C394 LOAD TERMINALS OVERHEATED. REPLACED C228 AND C394 IN ASSOCIATION WITH SWPM 20-30-00. REPLACED AFFECTED TERMINALS IN ASSOCIATION WITH 20-30-11. WINDOW HEAT SYSTEM CHECKS SATISFACTORY IAW 30-41-00. FLIGHT DECK LIGHTING CHECKS SATISFACTORY IAW 33-11-00. 2L72 4F RTA16WE 20100127 EU 2010 1 27 USAA2010011590113120100114A5220FE240004 CYLINDER AIRBUSA319 A319112 3930323EU EMERGENCY EXIT LOW PRESSURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19745VJ267465577 1289 FLT NR 1888 - EMERGENCY EGRESS SYSTEM - L1 DOOR EMERGENCY CYLINDER NEEDS SERVICE. SERVICED L1 DOOR EMERGENCY CYLINDER PER AMM 52-10-00-614. 2L72 4F RTA28NM 20100127 EU 2010 1 27 USAA2010011590114120100114A2560 BATTERY AIRBUSA319 A319112 3930323EU FLASHLIGHT DISCHARGED A USAAK NONE L NO TEST ININSP/MAINT 1 EA19747UW 1301 FLT NR 1869 - EMERGENCY EQUIPMENT - FLASHLIGHT FORWARD FLIGHT ATTENDANT STATION INOPERATIVE. REMOVED AND REPLACED BATTERY AND STRAP. OPERATIONAL CHECK WAS GOOD. 2L72 4F RTA28NM 20100127 NM 2010 1 27 USAA2010011590115120100114A33502514303 LENS AIRBUSA319 A319132 3930340NM EMERGENCY LIGHT MISSING A USAAK NONE O OTHER ININSP/MAINT 1 EA19819AW 1395 FLT NR 468 - EMERGENCY EQUIPMENT, EMERGENCY EXIT LENS MISSING AT LEFT SIDE OVERWING DOOR. INSTALLED NEW EMERGENCY LIGHT LENS AT LEFT SIDE OVERWING DOOR. 2L72 4F RTA28NM 20100127 EA 2010 1 27 SWIA201023469 120100109A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A SWIAK NONE L NO TEST ININSP/MAINT 1 NM06756SK 10221 FLT 6716, NR 1 AND NR 4 EMERGENCY CEILING LIGHTS INOP. OPERATIONAL CHECK NORMAL. 2L72 4F RTA21EA 20100127 EA 2010 1 27 SWIA201023470 120100109A3350 LAMP CNDAIRCL600 CL6002C10 1390015EA EMERGENCY LIGHT BURNED OUT A SWIAK NONE L NO TEST ININSP/MAINT 1 NM06776SK 10241 FLT 6251 - NR 3 CEILING EMERGENCY LIGHT INOP. RELAMPED. 2L72 4F RTA21EA 20100127 NM 2010 1 27 USAA2010011990125120100115A5240FE240007 CYLINDER AIRBUSA321 A321231 3940032NM R4 DOOR LOW PRESSURE A USAAD RETURN TO BLOCK J WARNING INDICATION TXTAXI/GRND HDL 1 EA19519UW3063 3063 3881 FLT NR 401 - AFTER PUSHBACK, FLIGHT ATTENDANT WARNING FOR DOOR 4R, RETURNED TO GATE. MAINTENANCE SERVICED 4R DOOR ASSIST BOTTLE PER MM 52-10-00. 2L72 4F RTA28NM 20100127 NM 2010 1 27 FDEA201001230229 120100123A5347 SEAT TRACK DOUG MD10 MD1030F 3024020NM BS 879-1019 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 CE21306FE 48287 UPPER CARGO COMPARTMENT SEAT TRACK LBL 47.5. FS 1019 TO 879 HAS 3 EA WORN LOBES- OUT OF LIMITS. R & R SEAT TRACK SECTION IAW SRM 53-70-00, STA. 869 TO STA 1009 LBL 47.5. SEAT TRACK SECTION FABRICATED ON MAE TRAVELER T10/816283. REPAIR CLASSIFIED AS MAJOR REPAIR. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001240230 120100124A5347S492915018 SEAT TRACK DOUG MD10 MD1030F 3024020NM BS 1015-1159 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 CE21306FE 48287 MCD CARGO COMP SEAT TRACK BETWEEN F.S. 1015 TO F.S. 1159 AT LBL 47.5 HAVE 8 EACH WORN LOBES. REMOVED AND REPLACED SEAT TRACK SECTION FROM FS 1015 TO FS 1159 AT LBL 47.5 IAW SRM 51-31-01 AND SRM 53-70-00, REPAIR CLASSIFIED AS MAJOR, SEAT TRACK SECTION FABRICATED ON MAE TRAVELLER NR T10/817049 IAW SRM 51-10-01. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001240231 120100124A5347607158 SEAT TRACK DOUG MD10 MD1030F 3024020NM BS 1511-1521 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 CE21306FE5754157541 48287 MCD CARGO COMPT SEAT TRACK BETWEEN F.S. 1511 TO F.S. 1521 HAS 2 EACH WORN LOBES AT LBL 8. MCD CARGO COMPT SEAT TRACK BETWEEN FS 1511 TO FS 1521 AT LBL 8 HAS BEEN REPLACED ON NON-ROUTINE NR N00389 IAW SRM 53-70-00 SHEET 1 AND 2, SRM 51-31-01, REPAIR CLASSIFIED AS MAJOR. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001240232 120100124A5347601096418 SEAT TRACK DOUG MD10 MD1030F 3024020NM BS 979-1085 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 CE21306FE5754157541 48287 MCD CARGO COMPT. SEAT TRACK BETWEEN F.S. 979 TO FS 1085 AT RBL 47.5 HAVE 8 EACH WORN LUGS. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-70-00, SEAT TRACK FABRICATED IAW SRM 51-10-01, REPAIR CLASSIFIED AS MAJOR. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001240233 120100124A53476010964 SEAT TRACK DOUG MD10 MD1030F 3024020NM BS 1179-1311 WORN A FDEAK NONE O OTHER ININSP/MAINT 1 CE21306FE5754157541 48287 MCD CARGO COMPT. SEAT TRACK BETWEEN FS 1179 TO FS 1311 AT LBL 47.5 HAVE 5 EACH WORN LOBES. REPAIRED SEAT TRACK AND FOUND WITHIN LIMITS IAW SRM 57-70-00 FIG. 5, REMOVED AND REPLACED SEAT TRACK IAW SRM 51-31-01 AND SRM 57-70-00 FIG 5, SEAT TRACK FABRICATED IAW SRM 51-10-01, REPAIR CLASSIFIED AS MAJOR. 2L73 4F RTA22WE 20100127 NM 2010 1 27 R61A20100025 120100118A3240 SENSOR EMB ERJ170ERJ170200LR 3260121NM RT BRAKE FAULTY A R61AO OTHER N FALSE WARNING LDLANDING 1 GL11107HQ 17000165 CREW REPORTED RT MLG BRAKES OVERTEMP DURING LANDING, DECLARED EMERGENCY AT IAH AND ENDED FLIGHT WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT TO TROUBLESHOOT. MAINTENANCE FOUND THE NR 4 BRAKE TEMP SENSOR TO BE AT FAULT, AND REPLACED IT PER EMB AMM. A/C WAS THEN RETURNED TO SERVICE. 2L72 4F RTA56NM 20100127 2010 1 27 WRLA20100120332 420100120A2565 SLIDE DOUG MD11 MD11 3023602NM PWA 4462 PW4462 NE R4 DOOR DAMAGED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11273WA 48519 R4 EVAC SLIDE FELL FROM CONTAINER AND IS DAMAGED. REMOVED AND REPLACED R4 SLIDE. 2L73 4F4 FRTA22WE E24NE 20100127 NM 2010 1 27 QXEA2010011100028120100107A27313094301 SWITCH BOMBDRDHC8 DHC8402 1390042NM ELEVATOR TRIM MALFUNCTIONED A QXEAC ABORTED TAKEOFF J WARNING INDICATION TOTAKEOFF 1 NM19401QX 4031 AT APPROX 50 KTS TAKE WARNING HORN ACTIVATED CONTINUOUSLY. ABORTED TAKEOFF. POST ABORT CHECK SHOWED ACFT PROPERLY CONFIGURED. PRE TAKEOFF T/O WARN TEST OK. POST ABORT T/O WARN TEST OK. PERFORMED FUNCTIONAL TEST OF T/O WARNING SYS AND THEN INTROGRATED CDS FOUND FAULT "PILSW FAULT". REMOVED AND REPLACED HANDWHEEL ELEVATOR-TRIMSWITCH IAW AMM TASK 27-32-18-000-801 & 27-32-18-400-802. PERFORMED OPS TEST OF ELEVATOR PITCH TRIM SYS IAW AMM TASK 27-32-00-710-802 AND RIL 84-27-057. RETURNED TO SERVICE. 2H72 4T RTA13NM 20100127 NM 2010 1 27 R61A20100027 120100118A2560 GLOWSTRIP EMB ERJ170ERJ170100SU 3260403NM CABIN UNSERVICEABLE A R61AK NONE O OTHER NRNOT REPORTED 1 GL11874RW 17000148 THE EMERGENCY EXIT MARKING ON GLOW STRIPS ON RIGHT FRONT IS MISSING RED DOTS. MAINTENANCE CONTROL PLACED THIS ON DEFERRAL PER MEL 33-50-21-1 CAT C TICKET 28801. 2L72 4F RTA56NM 20100127 NM 2010 1 27 HALA2010011200014120100112A2612 FIRE LOOP BOEING767 76733A 1385209NM LT NACELLE FALSE ACTIVATIONA HALAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP35580HA 28140 ETOPS SIGNIFICANT SYS - EICAS MSG L ENG FIRE LP 2 DISPLAYED. T/S IAW FIM 26-11-00/101 INSPECTED FIRE LOOPS ON ENG NO TROUBLE FOUND- MSG CLEARED AND DID NOT RETURN SYS CHECKS OK. 2L72 4F RTA1NM 20100127 2010 1 27 HALA2010010900015420100109A3442 DISPLAY BOEING767 76733A 1385209NM MALFUNCTIONED A HALAO OTHER N FALSE WARNING NRNOT REPORTED 1 WP35580HA 28140 ETOPS SIGNIFICANT SYS - STATUS PG DISPLAYS EICAS MSG "WXR SYS" W/L SYS SELECTED. RECYCLED NR 1 WXR C/B. OPS CK OK IAW MM 34-53-00."WXR SYS" MESSAGE CLEARED. 2L72 4F RTA1NM 20100127 NM 2010 1 27 FDEA201001250234 120100125A5320146N53183 PLATE BOEING757 7572T7 1384914NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21936FD 23293 CORROSION ON DECK PLATE AT STA 1715, LBL 25. CORROSION REPAIR CARRIED OUT ON DECK PLATE AT STA 1715 IAW EA F-5320-135812 (BS 1715, LBL 25 AFT DECK PLATE CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100. 2L72 4F RTA2NM 20100127 NM 2010 1 27 FDEA201001150193 120100115A534765196018 SEAT TRACK BOEING727 727227 1384078NM BS 950A-960 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21489FE 21492 CABIN SEAT TRACK BS 960-950A RBL 24 IB UPPER FLANGE IS CORRODED AT FASTENERS. REMOVED SEAT TRACK SECTION IAW SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK SECTION AND FABRICATED SPLICE FOR 2EA ANGLES AND 1EA STRAP IAW SRM 53-10-5 FIG1. TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED SEAT TRACK SECTION AND SPLICE IAW SRM 51-30-2 REV 102. 2L73 4F A3WE 20100127 NM 2010 1 27 FDEA201001200202 120100120A5755 SKIN DOUG MD11 MD11F 3023600NM NR 4 SPOILER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21574FE 48499 RT WING NR 4 SPOILER TOP SURFACE FOUND DENTED. DENTED AREA FOUND CRACKED AFTER REPAIR IAW SRM 51-21-01 REV 42. CRACKED SKIN REPAIRED IAW SRM 51-71-00, PARAGRAPH 19 REV 2. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001200203 120100120A5755 SKIN DOUG DOUG MD11 MD11F 3023600NM NR 3 SPOILER CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21574FE AA102 48499 RT WING NR 3 SPOILER TOP SURFACE FOUND CRACKED. RT WING NR 3 SPOILER R & R IAW AMM 27-60-30-4 REVISION 64. FUNCTIONAL TEST OF THE SPOILER LATERAL CONTROLS CARRIED OUT IAW AMM 27-61-00-730-801 REVISION 64. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REVISION 109. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001200204 120100120A5751 SKIN DOUG DOUG MD11 MD11F 3023600NM RT WING AILERON DELAMINATED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21574FE 0120 48499 RT WING OTBD AILERON T/E LOWER SURFACE FOUND DELAMINATED. RT WING OTBD AILERON R & R IAW AMM 27-10-30-4 REVISION 64. OPS TEST OF THE AILERON NEUTRAL AND RANGE OF MOVEMENT CARRIED OUT IAW AMM 27-10-00-710-802 REVISION 64. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REVISION 109. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001210205 120100121A33102632EDC DIMMER DOUG MD11 MD11F 3023600NM COCKPIT LIGHTS FAILED A FDEAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 CE21585FE1356 1356 48481 500 HRS INTO FLT AT CRUISE FL 360. CREW HEARD AN ARCING SOUND BY THE RT OBSERVERS POSITION, LIGHT SMOKE AND AN ACRID SMELL WERE ALSO NOTED. THE OVER-HEAD SWITCH PANEL LTG (C-30) CIRCUIT BREAKER POPPED AND SMOKE AND FUMES DISAPATED. OVERHEAD PANEL LIGHTS WERE OUT THE REMAINDER OF FLIGHT. NO OTHER MALFUNCTIONS ON AC BUS 3 NOTED. T/S IAW FIM 33-11, FOUND OVERHEAD LAMP DIMMER (U1-13 0) R & R O/H LAMP DIMMER IAW MM 33-11-03-2. ACFT OK FOR SERVICE, CLEARS PIREP. PREMATURE REMOVAL/INSTALLATION. 2L73 4F RTA22WE 20100126 NE 2010 1 26 C8GA201000002 220100120A751069171314 DUCT BOEING727 727227 1384078NM PWA JT8 JT8D9 52048NE ANTI ICE CRACKED A C8GAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SO2989427 21365 DURING CLIMB OPERATION THE LOWER AFT BODY OVERHEAT ILLUMINATED IN FLIGHT. CREW PERFORMED APPROPRIATE CHECKLIST AND DIVERTED, WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP REVEALED THAT THE NR 3 ENGINE ANTI-ICE DUCT WAS CRACKED. REMOVED AND REPAIRED DAMAGED DUCT. INSTALLED REPAIRED DUCT AND PERFORMED OPS AND LEAK CHECKS. NO DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE. 2L73 4F4 F A3WE E2EA 20100126 EU 2010 1 26 IPXA10158224 120100114A5753 SKIN AIRBUSA300 A300F4622R 3930360EU RT WING TE FLAP GOUGED A IPXAK NONE O OTHER ININSP/MAINT 1 CE17133UP 0816 INSPECTION TYPE:4/C, SMALL GOUGE ON UPPER SURFACE OF RT WING MID FLAP AT 40 IN INBD OF OTBD EDGE REPAIRED SA IAW SRM 57-50-00 PARA 4.E, FIG. 205 REF. UPS RCD 385048. 2L72 4F RTA35EU 20100126 NM 2010 1 26 UALA2010010700078120100105A2550181RA71R206C PDU BOEING767 767322 1385200NM PWA 4060 PW4060 52119NE AFT CARGO BAY FAULTY A UALAK NONE B SMOKE/FUMES/ODORS/SPARKS ININSP/MAINT 1 WP29652UA 25390 AFT CARGO PIT, AFT CARGO LOADING SYS CHECK. DURING CHECK SMOKE WAS COMING OUT FROM UNDER CARGO PIT FLOOR PANELS ON LT SIDE FWD OF CARGO DOOR. 2 EACH PDU CONTROL C-B. REPLACED PDUS AT 3L AND 7L, OPS CHECKED GOOD. 2L72 4F4 FRTA1NM E24NE 20100126 SW 2010 1 26 KY7A15462 120100107A53442724147003 HINGE SWRNGNSA226 SA226TC 8780404SW PAX DOOR CRACKED E KY7AK NONE O OTHER ININSP/MAINT 1 NM0362Z 31817 TC237 CABIN DOOR DIFFICULT TO CLOSE. FOUND HINGE CRACKED 2L72 4T RTA8SW 20100126 NM 2010 1 26 IPXA10658233 120100114A5753113T220129A PANEL BOEING767 76734AF 1385212NM LT WING TE FLAP CHIPPED A IPXAK NONE O OTHER ININSP/MAINT 1 CE17315UP 27743 INSPECTION TYPE:7C, LT WING INBD MAIN FLAP OTBD EDGE MID AREA CHIPPED. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5H REV 45. 2L72 4F RTA1NM 20100126 EA 2010 1 26 MALA100008 120100122A5330 SKIN CNDAIRCL600 CL6002B19 1900309EA FUSELAGE DENTED A MALAD RETURN TO BLOCK W INADEQUATE Q C TXTAXI/GRND HDL 1 GL15834AY 8034 THE ACFT WAS PUSHED BACK INTO A BAGGAGE CART WHICH CAUSED A DENT TO THE LT FUSELAGE SKIN 9.75" LONG X 8.0" WIDTH WITH A MAX DEPTH OF 0.125 INCH. THE DENT WAS SMOOTH, WITH NO EVIDENCE OF SKIN CRACKING AND THE INTERNAL STRUCTURE WAS DISPLACED, BUT THERE WAS NO BUCKLING OR CRACKING. EVEN SO, BBD DETERMINED THE DAMAGE WAS BEYOND FLYABLE LIMITS. ACCOMPLISH REPAIR IAW REO 601R-53-51-105 DATED 21JAN2010. 2L72 4F RTA21EA 20100126 NM 2010 1 26 IPXA10M58232 120100112A5754NRB6224513 SKIN DOUG MD11 MD11F 3023600NM SLAT MISREPAIRED A IPXAK NONE O OTHER ININSP/MAINT 1 CE17290UP 48456 INSPECTION TYPE:2C REPAIR SURVEY SEQ NR 290-W3-01 PREVIOUS REPAIR DOUBLER INSTALLED SOLID R IVETS IN LIEU OF BLIND RIVETS APPROX BETWEEN STA XIS 151- 180 REF SRM 57-40-01 FIG 201 REPAIR 7. REMOVED EXISTING REPAIR ON LT INBD SLAT, SLAT SKIN BETWEEN XIS 151 AND XIS 180. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD11-5750-36304-A AND EA 011-5730-01-A2121. 2L73 4F RTA22WE 20100126 NM 2010 1 26 UALA2010011800207120100116A2751S256T00717 TRANSMITTER BOEING767 767322 1385200NM PWA 4052 PW4052 52119NE FLAPS FAULTY A UALAK NONE O OTHER ININSP/MAINT 1 WP29665UA 29237 FLAP-SLAT ELEC LIGHT INTERMITTENT ON TAXI IN. UNABLE TO VERIFY THE PROBLEMS, REPLACED FSEU AS PRECAUTION AND SYS CHECKED NORMAL. PROBLEM RECURRED. ACCOMPLISHED BITE ON FSEU AND HAD M489 FAULT. RPLC'D NR 8 FLAP POSITION TRANSMITTER. SYS CHECKS OK AT THE PRESENT TIME. 2L72 4F4 FRTA1NM E24NE 20100126 NM 2010 1 26 UALA2010011800208120100116A5753 SKIN BOEING757 757222 1384956NM PWA 2037 PW2037 NE L WING IB FLAP CHAFED A UALAK NONE O OTHER ININSP/MAINT 1 WP29502UA 24623 LT WING IB FLAP OTBD SIDE CHAFING ON NR 5 SPOILER. MAJOR REPAIR ACCOMPLISHED: REPAIRED FLAP UPPER SKIN. ACP RII INSPECTION ON FLAP SKIN REPAIR. 2L72 4F4 FRTA2NM E17NE 20100126 NM 2010 1 26 AALA20100119DFW10120100117A3350 BATTERY PACK BOEING777 777223 1385213NM CABIN DISCHARGED A AALAK NONE L NO TEST ININSP/MAINT 1 SW21780AN 29956 EMERGENCY LIGHT AT SEAT 36G AND LEFT NUMBER TWO OVERHEAD DOOR IS INOPERATIVE. REPLACED BATTERY PACK M33096 AT LEFT NUMBER TWO DOOR. 2L72 4F RTT00001SE 20100126 WP 2010 1 26 AALA20100120TUL03120100120A5330 SKIN DOUG DC9 DC982 3022082WP FUSELAGE DENTED A AALAK NONE O OTHER ININSP/MAINT 1 SW21424AA 49336 DENT AND SEVERAL SCRATCHES ON RIGHT SIDE OF FUSELAGE, AT LONGERON 20, STATION 285. BLENDED SCRATCHES AND INSTALLED INTERNAL DOUBLER PER SRM 53-04 FIGURE 38, SHEET 20. 2L72 4F A6WE 20100126 SO 2010 1 26 C2XA10CL009 120100120A361040303920SD O-RING EMB 145 EMB145 3260210SO BLEED AIR SYS DETERIORATED A C2XAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 SW2713994 145291 CLE FLT 2610 THE CREW REPORTED A BLEED 1 LEAK INDICATION DURING CLIMBOUT FROM CMH. THE AIRCRAFT DIVERTED INTO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE BLEED AIR O-RINGS AT JOINTS 13, 15, 17, 21, 25, 30 AND 32. OPERATIONAL CHECKS WERE GOOD. 2L72 4F RTT00011AT 20100126 SO 2010 1 26 C2XA10IA031 120100121A3320BR900022 BALLAST EMB 145 EMB145EP 3260221SO CABIN MALFUNCTIONED A C2XAO OTHER B SMOKE/FUMES/ODORS/SPARKS UKUNKNOWN 1 SW2714947 145054 DFW - FLIGHT 2324 THE CREW REPORTED A FAINT ELECTRICAL BURNING SMELL IN FLIGHT. THE AIRCRAFT LANDED AT DFW WITHOUT INCIDENT, WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PLACED SIDEWALL LIGHTS 2A & 3A ON MEL 33-20-00/1 CAT C, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. THE AIRCRAFT LANDED AT IAH WHERE MAINTENANCE REMOVED AND REPLACED THE FORWARD CABIN LIGHT BALLAST, OPERATIONALLY TESTED WITH NO DEFECTS, REMOVED THE MEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4F RTT00011AT 20100126 EA 2010 1 26 SWIA201023384 120100101A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06978SW 7953 OVERHEAD EMERGENCY CEILING LIGHT NR 3 INOP. (FLT 6394) RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100126 EA 2010 1 26 SWIA201023394 120100104A2170 COALESCER BAG CNDAIRCL600 CL6002B19 1900309EA AC BAY DIRTY A SWIAA UNSCHED LANDING J WARNING INDICATION TOTAKEOFF 1 NM06934SW 7722 SMOKE TOILET CAUTION ON TAKEOFF. (FLT 6014) REPLACED RIGHT PACK COALESCER BAG. 2L72 4F RTA21EA 20100126 EA 2010 1 26 SWIA201023400 120100101A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06417SW 7400 CEILING EMERGENCY FLOOD LIGHT AT ROW 10 INOP. (FLT 4626) RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100127 EU 2010 1 27 FDEA201001220215 120100122A5320A5361235620100 FLOOR SUPPORT AIRBUS300 A300F4605R 3930327EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21681FE 15457 799 AVIONICS COMPARTMENT FLOOR SUPPORT INTERCOSTAL ATTACH ANGLE IS CRACKED AT FRAME 10. REMOVED ATTACH ANGLE. LOCATED AND DRILLED ANGLE. INSTALLED ATTACH ANGLE IAW SRM 51-72-10 2L72 4F RTA35EU 20100127 WP 2010 1 27 22AA201000035 120100122A2910 LINE DOUG DC10 DC1030 3023501WP GE CF6 CF650* 30018NE HYD SYSTEM LEAKING A 22AAA UNSCHED LANDING KJ FLUID LOSS WARNING INDICATION CLCLIMB 1 SO19524MD 46999 530149 DURING CLIMB OUT, NR 1 HYD SYS START LOOSING FLUID, INITIATION PROCEDURE ON ALT PROCEDURES CHECK LIST, HYD FLUID LOST, DURING CLIMB OUT TO CRUISE NR 2 ENG FAIL, SECURED ENGINE IAW CHECK LIST. DUMP FUEL TO MAX LANDING WEIGHT TO LANDING, DURING POST FLIGHT FOUND LARGE FLUID LEAK IN AREA OF TAIL SECTION. DURING INSP TO HOR/STAB AREA FOUND HYD LINE TO RT MAINT S/O VALVE CRACKED, REBRIRED LINE IAW MM 20-10-01, PG 206 TYPE 3 REPAIR, LEAK CHECKED NORMAL, REMOVED MAIN OIL FILTER & CHIP DETECTOR OF TAIL ENG FOR INSP, FOUND CONTAMINATED WITH METAL PARTICLES & CONTAMINATION MM 79-30-01. ACCOMPLISHED RB NR 026363 ACCOMPLISHED NR 2 ESN 530-149, REMOVAL & INSTALLATION OF ESN 528-313 IAW W/C NR 142R7101M. 2L73 4F4 F A22WE E23EA 20100127 EU 2010 1 27 FDEA201001220216 120100122A5320A2551002700000 SUPPORT AIRBUS300 A300F4605R 3930327EU ZONE 100 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21681FE 15457 799 E & E COMPARTMENT BATTERY RACK TARP COVER BRACE; FWD INBD LEG IS CRACKED IN THE RADIUS. REPAIRED COVER BRACE IAW DWG A25510027. 2L72 4F RTA35EU 20100127 NM 2010 1 27 FDEA201001150180 120100115A5347652363726 SEAT TRACK BOEING727 727277 138408SNM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21489FE 21492 CABIN SEAT TRACK AT STA 695 RBL 24 INBD FLANGE AND SPLICE CORRODED REMOVED SEAT TRACK SECTION BETWEEN STA 690 TO 740 RBL24 AND 1 EA SPLICER IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK SECTION FROM BAE 1526-729-7178 T6 511 PO NR 9006020, DIM 172" LONG IAW SRM 53-10-5 FIG. 1 REV 102. TREATED AND PRIMED IAW SRM 51-10-2, INSTALLED SEAT TRACK SECTION AND 1 EA SPLICER IAW SRM 51-30-2. 2L73 4F RTA3WE 20100127 NM 2010 1 27 FDEA201001190183 120100119A5511185N70011 SPAR BOEING757 75723A 1384967NM HORIZONTAL STAB DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21921FD 24924 LT HORZ STAB L/E DAMAGED. REPAIR WAS ACCOMPLISHED IAW MAE EA NR 757-5510-16 A1923. CLASSIFIED AS A, "INTERIM" REPAIR, MAJOR. 2L72 4F RTA2NM 20100127 EA 2010 1 27 SWIA201023413 120100103A2130 SHUTOFF VALVE CNDAIRCL600 CL6002B19 1900309EA AC BAY FAILED A SWIAK NONE O OTHER CLCLIMB 1 NM06986SW 7967 UNABLE TO CONTROL CABIN ALTITUDE. (FLT 6551) REPLACED LEFT PACK PRSOV AND RIGHT PACK DUAL BYPASS VALVE. 2L72 4F RTA21EA 20100127 EA 2010 1 27 SWIA201023418 120100101A3350 LIGHT CNDAIRCL600 CL6002D24 1390016EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06814SK 15100 CENTER OVERHEAD EMERGENCY LIGHT AFT SECTION INOP. (FLT 4519) RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100127 EA 2010 1 27 SWIA201023419 120100107A5753 SEALANT CNDAIRCL600 CL6002B19 1900309EA TE FLAP OUT OF POSITION A SWIAO OTHER F FLT CONT AFFECTED APAPPROACH 1 NM06866AS 7517 UNCOMMANDED ROLL WHEN FLAPS DEPLOYED TO 45 DEGREES. (FLT 4773) REMOVED PROTRUDING PAINT AND SEALANT ON RIGHT OUTBOARD LEADING EDGE FLAP VANE. 2L72 4F RTA21EA 20100127 EA 2010 1 27 SWIA201023423 120100104A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06748SK 10203 NR 3 EMERGENCY LIGHT INOP. (FLT 6375) RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100127 EA 2010 1 27 VNAA2010011500007120100108A4990 OIL SYSTEM CNDAIRCL600 CL6002B19 1900309EA APU LOW A VNAAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL05260JS 7957 CREW REPORTED AN APU OIL TEMP AMBER MESSAGE DURING CRUISE EN ROUTE FROM CLT TO XNA. AIRCRAFT DIVERTED TO BNA BECAUSE THE RT ENGINE INTEGRATED DRIVE GENERATOR (IDG) WAS ALREADY DEFERRED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE APU OIL LEVEL AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20100127 NM 2010 1 27 ZZDA2010007 120100105A5320 STRUCTURE BOEING737 73776N 13844CHNM FUSELAGE TORN A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37278AT 32665 TEAR IN FUSELAGE BY L1 DOOR. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR PER B737 SRM 53-00-01. SEE NR 6581 AND 6583. 2L72 4F RTA16WE 20100127 NM 2010 1 27 WRLA20100105329 120100105A5320ABA7202117 MEMBRANE DOUG MD11 MD11F 3023600NM PWA 4462 PW4462 NE FUSELAGE CRACKED A WRLAK NONE O OTHER ININSP/MAINT 1 SO11275WA 48631 DURING 01C CHECK FOUND Y=360 X=-2 Z=-10 MEMBRANE ABA 7202-117 DEFORM AND 2EA CRACK, L=0.9" AND L=1.2" ON LIGHTENING HOLE. NRCU05014 ISSUED. ACCOMPLISHED THE REPAIR PER EI: W2010A53B-050 REV 00, 01,02: CUT THE DAMAGED AREA AS SHOWN IN W2010A53B-050 FIG 1, FABRICATE REPAIR PARTS AS SHOWN IN FIG 1, ASSEMBLE THE REPAIR PARTS WITH FAYING SURFACE SEALANT AND THE FASTENER PATTERN AS SHOWN IN FIG 1 SHEET 1 AND 2. CONDITION CHECK SATISFACTORY. 2L73 4F4 FRTA22WE E24NE 20100127 2010 1 27 YENA20100117008 420100117A3444066011534001 TRANSCEIVER EMB ERJ190ERJ190100IGW3260408NM RADAR ALTIMETER FAILED A YENAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 EA15178JB109906224 19000004 FLT JB1207 HPN-RSW CREW DIVERTED TO JFK DUE TO UNCOMMANDED LANDING GEAR ORAL WARNING AT 7000/9000/13000/17000 FT, COULD NOT CANCEL WARNING IT WOULD CONTINUE FOR SEVERAL MINUTES EACH OCCURRENCE. JFK MX RETRIEVED FHDB AND DVDR DATA, DATA NOTED NR 2 RADAR ALTIMETER SYSTEM FAULTED AT APPROX 400 FT CAUSING A/C TO BELIEVE IT WAS AT 400 FT AND ASKED FOR THE GEAR TO BE EXTENDED. PERFORMED AMM FIM 34-31-00-810-810, VERIFIED TRANSMIT COAX OF SYS NR 2 HAS GOOD INSULATION AND GOOD CONTINUITY. REMOVED AND REPLACED NR 2 RADAR ALTIMETER TRANSCEIVER IAW AMM 34-31-01, ALL OPS CHECK GOOD. 2L72 4F RTA57NM 20100127 SO 2010 1 27 RAIA2009120600001120100106A5210 SUPPORT EMB 145 EMB145LR 3260212SO MAIN DOOR OUT OF ADJUST A RAIAO OTHER O OTHER TXTAXI/GRND HDL 1 CE03835HK 145670 CREW REPORTED THAT THE MAIN DOOR COULD NOT BE OPENED FROM THE OUTSIDE. MAINTENANCE ADJUSTED THE LOWER DOOR SUPPORT BAR AND FORWARD UPPER ROLLER. AN OPERATIONAL CHECK OF THE DOOR IAW AMM PROCEDURE WAS PERFORMED FOLLOWING THE ADJUSTMENT WITH NO OTHER DEFECTS NOTED AT THE TIME. 2L72 4T RTT00011AT 20100127 NM 2010 1 27 ZZDA2010023 120100115A5311 FRAME BOEING717 717200 1383700NM FUSELAGE DAMAGED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37982AT 55041 EO 17-5310-2937 AFT LEFT STA 1178 CANTED FRAME INSPECTION IDENTIFIED CONFIGURATION 1 CONDITION 3. ACCOMPLISHED REPAIR TO AFT FUSELAGE FRAME CAP, CANTED STA 1178.225, LEFT SIDE IAW AIRTRAN TASK CARD 17-5310-2975. 2L72 4F TRA6WE 20100127 SO 2010 1 27 CHQA201000004 120100116A3297 CONNECTOR EMB 135 EMB135KL 3260302SO LANDING GEAR CONTAMINATED A CHQAA UNSCHED LANDING N FALSE WARNING CRCRUISE 1 GL11375SK 145569 CAE311837 JUST AFTER TAKEOFF FROM KSTL THE CREW RECEIVED A LG AIR/GND FAIL MESSAGE AND AN ENG 1/2 REVERSER DISAGREE MESSAGE. THE FLIGHT RETURNED TO THE FIELD AND LANDED UNEVENTFULLY. UPON A VISUAL INSPECTION BY MAINTENANCE OF THE AIR/GROUND SYSTEM IT WAS FOUND THAT THE RT WOW NR 2 PROX SWITCH HAD A CRACKED FACE AND THE CONNECTOR WAS FULL OF WATER. THE RT WOW NR 1 PROX SWITCH CONNECTOR WAS ALSO FOUND FULL OF WATER AND THE NOSE LANDING GEAR HARNESS CHAFED THROUGH TO THE WIRE, AND THE CONNECTOR CORRODED. AT THIS TIME THE NOSE LANDING GEAR PROX SWITCH WIRE W019 HARNESS AND NOSE LANDING GEAR PROX SWITCH WERE REPLACED PER EMB AMM 32-63-02-4. THE RT MLG PROX SWITCH WOW NR 1 AND NR 2 WERE REPLACED AS WELL PER AMM 32-63-01. 2L72 4F RTT00011AT 20100127 NM 2010 1 27 YENA20100116009 120100116A3620354910 PIN EMB ERJ190ERJ190100IGW3260408NM BLEED AIR SYS CORRODED A YENABA EMER. DESCENT UNSCHED LANDING N FALSE WARNING CLCLIMB 1 EA15231JB10090 19000033 FLT JB111 BUF-JFK DURING TAKEOFF CLIMBOUT FROM BUF "BLEED 1 LEAK" EICAS MESSAGE ILLUMINATED, QRH COMPLETED, BLEED LEAK STILL ILLUMINATED. CREW DECLARED EMERGENCY AND RETURNED TO BUF AND LANDED SAFELY. BUF MX TROUBLESHOOTING PER AMM FIM 36-21-00-81-801-A FOUND CORRODED CERAMIC PIN ON CHANNEL 2 PYLON LOOP AT CONNECTOR J1045, CLEANED CONNECTOR AND REPLACED CERAMIC PIN IAW AMM 36-20-01. OPS CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. 2L72 4F RTA57NM 20100127 NM 2010 1 27 FDEA201001200195 120100120A5321146N543112 SPLICE BOEING757 7572T7 1384914NM FLOOR PANEL CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21936FD 23293 AFT CARGO RT SIDE PANEL SPLICE AT STA 1530 FOUND CORROSION. CORRODED SPLICE AT AFT CARGO STA 1530, RT PANEL REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA. 2L72 4F RTA2NM 20100127 SO 2010 1 27 CHQA201000005 120100117A2130 UNKNOWN EMB 145 EMB145LR 3260212SO CABIN PRESSURE MALFUNCTIONED A CHQAA UNSCHED LANDING O OTHER CLCLIMB 1 GL11279SK 145379 CAE312622 DURING CLIMBOUT OF KCLE THE CREW NOTICED THE CABIN ALTITUDE INDICATOR WAS DISPLAYING AMBER DASHES. THE AUTO PRESSURIZATION SYSTEM WAS ALREADY DEFERRED AND THE PROCEDURES WERE REVIEWED. THE MEL ALLOWED CONTINUED FLIGHT IF THE MANUAL SYSTEM WAS OPERATING NORMALLY. HAVING NOW LEVELED OFF AT 14,000FT MSL THE DIFFERENTIAL PRESSURE WAS ALREADY APPROACHING THE LIMIT OF 7.8. THE CREW FELT THAT WITH THE PRESSURIZATION LIMIT APPROACHING THE LIMIT AND WITHOUT THE ABILITY TO SEE THE CABIN ALTITUDE THAT THE SYSTEM WAS NOT NORMAL. THE APPROPRIATE CHECKLISTS WERE RUN AND THE FLIGHT ATTENDANT AND PASSENGERS NOTIFIED OF THE SITUATION. THE FLIGHT THEN RETURNED TO KCLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE2L72 4T RTT00011AT 20100127 SO 2010 1 27 C2XA10IA21 120100116A361014530609401 PRECOOLER EMB 145 EMB145LR 3260212SO BLEED AIR SYS LEAKING A C2XAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 SW271399719434894 145298 IAH - FLIGHT 2573, THE CREW REPORTED A NR 1 BLEED OVERTEMP INDICATION WITH WING ANTI-ICE ON. THE AIRCRAFT RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 FAN AIR SENSOR, AND NR 1 PRE-COOLER. OPERATIONAL AND LEAK CHECKS WERE ACCOMPLISHED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20100127 EU 2010 1 27 COEA2010011801819120100118A5711S57112081202 SPAR AEROSPATR72 ATR72212 8680945EU LT WING CHAFED A COEAK NONE O OTHER ININSP/MAINT 1 NM13819FX 359 HEAVY CHECK COE: MAJOR REPAIR: LT WING REAR SPAR UPPER SLAT STRIP FLANGE BETWEEN RIBS 2 & 4, UPPER AND LOWER SURFACES OF FLANGE ARE CHAFED IN 3 LOCATIONS, TITANIUM BONDING STRIPS ARE WORN THROUGH. BLENDED DAMAGE IAW STRUCTURAL REPAIR INSTRUCTIONS DO/TS-299/10-12830 AND SRM ATR72 CHAPTER 57-12-20 FIG 402. WO 91979 NR 601009. 2H72 4T RTA53EU 20100127 WP 2010 1 27 WX0A070511 120100118A49204034242974 APU DOUG DC9 DC982 3022082WP APU BAY MALFUNCTIONED A WX0AK NONE B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 WP19407NV 53244 FLIGHT CREW REPORTED WHILE TAXING TO GATE AFTER LANDING IN SGF AND SWITCHING AIR CONDITIONING PACK TO THE APU THE CABIN FILLED WITH HAZE AND STENCH. MAINTENANCE DEPARTMENT PERSONNEL INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE APU ASSY, IAW ALLEGIANT AIR TASK CARD R0594902. SYSTEM OPS CHECKS NORMAL AND THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F A6WE 20100127 SO 2010 1 27 C2XA10SH031 120100121A532014530645403 FLOOR SUPPORT EMB 145 EMB145LR 3260212SO FUSELAGE CORRODED A C2XAK NONE O OTHER ININSP/MAINT 1 SW2722971 145149 SHV - DURING C-CHECK, CENTER OMEGA BEAM HAS CORROSION AT FR 44. REPAIRED CENTER OMEGA BEAM IAW EC5310-01466. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. 2L72 4T RTT00011AT 20100127 NM 2010 1 27 NOCA00410 120100116A33508100022601 LIGHT BOEING757 75728A 1384976NM CABIN INOPERATIVE A NOCAK NONE L NO TEST ININSP/MAINT 1 EA15754NA 29381 EMERGENCY LIGHT AT SEAT 1C (FLOOR PATH) 1 LIGHT INOP. REPLACED 1 EA LIGHT ASSEMBLY AMM 33-51-1, OPS OK. 2L72 4F RTA2NM 20100127 NM 2010 1 27 NOCA00510 120100116A3350S41N50915 LIGHT BOEING767 76739H 1385311NM CABIN BROKEN A NOCAK NONE O OTHER ININSP/MAINT 1 EA15760NA 26257 EMERGENCY TRACK LIGHTING AT SEAT 5H BROKEN. REMOVED AND REPLACED EMERGENCY TRACK LIGHT ASSY AT 5HG PER AMM 33-51-10, OPS CHECK NORMAL. 2L72 4F RTA1NM 20100127 NM 2010 1 27 NOCA00610 120100116A33978100022608 WIRE BOEING767 76739H 1385311NM CABIN BROKEN A NOCAK NONE O OTHER ININSP/MAINT 1 EA15760NA 26257 AFT GALLEY PHOTO LUMINESCENT E-PATH LIGHT ON RIGHT SIDE HAS BROKEN WIRES. REMOVED AND REPLACED LIGHT ASSY AND OPS CHECKS NORMAL PER AMM 33-51-00. P/N 81000-22608 2L72 4F RTA1NM 20100127 NM 2010 1 27 QXEA2010011200031120100108A5753 SKIN BOMBDRDHC8 DHC8402 1390042NM TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM19407QX 4049 C5 CHECK -OTBD FLAP UPPER SURFACE HAS LIGHT CHAFE DAMAGE ON PREVIOUS PATCH REPAIR. REMOVED OLD DOUBLER IAW SRM 51-23-00-02-01, HFEC INSPECTED ENTIRE SKIN SURFACE IAW NDTM PART 6,51-00-01, NO CRACKS NOTED. FABRICATED AND INSTALLED NEW DOUBLER, ALL WORK PERFORMED IAW T/C 6-57-444A. 2H72 4T RTA13NM 20100127 NM 2010 1 27 QXEA2010011200032120100108A5753 FLAP TRACK BOMBDRDHC8 DHC8402 1390042NM RT WING TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM19407QX 4049 C5 CHECK - RT NR 4 FLAP TRACK INBD FACE HAS A CHAFE APPROX 5' LONG JUST ABOVE WHERE THE INBD SIDE ROLLER WOULD TRAVEL AND IT STARTS APPROX 21' AFT OF THE WINGS AFT SPAR. MAPPED FOR ENGINEERING. LOCALLY POLISHED AREA TO REMOVE LOOSE MATERIAL AND BREAK SHARP EDGES AND FOUND AREA OF REPAIR TO BE WITHIN LIMITS IAW RD 8/4-57-1238. HFEC INSPECTED POLISHED AREA FOR CRACKS IAW NDTM PART 6, 51-00-01 NO CRACKS NOTED. 2H72 4T RTA13NM 20100127 NM 2010 1 27 FDEA201001250235 120100125A5410AJC759351 FRAME DOUG MD11 MD11F 3023600NM NR 2 PYLON CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21609FE 48549 CRACK INDICATION FOUND APPROX 0.5" IN LENGTH DURING HFEC INSP ON THE NR 2 PYLON CARRY THRU STRUCTURE ACCESS PANEL NR 363ML CUTOUT. REPAIR CARRIED OUT IAW EA NR 1-5530-137547. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001160168 120100116A4920GTCP8598 APU BOEING727 727233 138408ANM ZONE 100 MALFUNCTIONED A FDEAF ACTIVATE FIRE EXT. BJ SMOKE/FUMES/ODORS/SPARKS WARNING INDICATION TXTAXI/GRND HDL 1 CE21285FE40807261 22622 SHORTLY AFTER APU SHUTDOWN, AFT LOWER CARGO SMOKE ILLUMINATED, BOTTLE NR 1 DISCHARGED, (JUST BEFORE BOTTLE NR 1 DISCHARGED, TUG DRIVER CONFIRMED SMOKE AROUND BELLY OF ACFT) SUBSEQUENTLY FORWARD LOWER CARGO SMOKE LIGHT ILLUMINATED, THEN DISCHARGED BOTTLE NR 2. ACCOMPLISHED THE EMERGENCY EVAC CK LIST AND EGRESSED. OPENED SHROUDS AT EITHER END AND GVI FOR OBVIOUS CAUSES, CONDITION AND SECURITY OF 'B' NUTS, WIRING AND COMPONENTS. FOUND OIL TANK QTY OVER SERVICED - DRAINED TO NORMAL. APU FUEL VLV OPS CHK GOOD. MOTORED APU -NORMAL ROTATION IAW JRH STARTED APU, NOTING STONG IGN, NORMAL ACCEL TIME AND EGT. OPERATED BLEED LOADS - OK. ELEC OK. AFTER 40 MIN RUN W/ NO ABNORMAL NOISES SHUTDOWN NOTING SMOOTH COAST2L73 4F RTA3WE 20100127 EU 2010 1 27 FDEA201001180170 120100118A5230A5237050220000 SKIN AIRBUS300 A300F4605R 3930327EU FWD CARGO DOOR DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21681FE 799 FWD CARGO DOOR; UPPER AFT CORNER HAS A SHEARED FASTENER AND SKIN SEPARATION. REPAIRED IAW SRM 52-31-00, FIG 203, SHEET 3. ALODINE, PRIME AND TOPCOAT IAW SRM 51-21-10, PG 4 AND SRM 51-23-10, PGS 2 & 3. INSTALLED DOUBLER IAW SRM 52-31-00, FIG 203, SHEET 3. 2L72 4F RTA35EU 20100127 NM 2010 1 27 FDEA201001110172 120100111A324026094724 BRAKE DOUG MD11 MD11F 3023600NM MLG DAMAGED A FDEAO OTHER MJ OVER TEMP WARNING INDICATION CLCLIMB 1 CE21603FE7726 7726 48459 BRAKE DIFF TEMP ALERT CLIMBOUT. TEMPS ON LT MAIN TRUCK WERE : NR1-72, NR 2-387, NR 3-95, NR 4-127 DEGREES. NR 2 BRAKE TEMP WAS CONTINUING TO INCREASE. GEAR EXTENDED TO EXPEDITE COOLING. WHEN TEMP DECREASED TO 225, GEAR WAS RETRACTED. INSPECTED NR 2 BRAKE, FOUND BRAKE DISK BROKEN AND VERY HARD TO SPIN WITH AXLE ON JACK. R & R NR 2 BRAKE ASSY IAW AMM 32-43-20-4. OPS CHECK SATISFACTORY. ACFT OK FOR SERVICE. PREMATURE REMOVAL/INSTALLATION OFF MFG 2609472-4, POS 2 SRL B2857, TAG 3758C4 ON MFG 2609472-4 SRL B0591, TAG 44218B INSPECTED NR 2 BRAKE, FOUND BRAKE DISK BROKEN AND VERY HARD TO SPIN WITH AXLE ON JACK. R & R NR2 BRAKE ASSY IAW AMM 32-43-20-4. OPS CHECK SATISFACTORY. ACFT OK FOR SERVICE. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001180173 120100118A5753 SKIN BOEING BOEING757 7572B7 1384964NM RT WING TE FLAP CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21909FD 27200 RT WING INBD UPPER FLAP L/E STRUCTURE HAS CHAFINGS. REMOVED CHAFE FROM RT WING INBD FLAP IAW SRM 57-53-01, FIG 101 DETAIL VI. FOUND TO BE OUT OF LIMITS. ORIG MATERIAL 0.055 AFTER REWORK 0.049. CUT OUT DAMAGE AREA IAW SRM 57-53-01 FIG 201 REPAIR 2. REMOVED PANEL IAW SRM 51-40-02. FABRICATED 2EA DOUBLERS AND REPAIR PLATE. FABRICATED STRAPS IAW SRM 57-53-01 FIG 201. LOCATED AND DRILLED HOLES IAW SRM 51-40-05. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED ALL REPAIR PARTS IAW SRM 51-40-02. REINSTALLED PANEL IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR 2L72 4F RTA2NM 20100127 NM 2010 1 27 QXEA2010011200033120100108A5540 CASTING BOMBDRDHC8 DHC8402 1390042NM RUDDER WORN A QXEAK NONE O OTHER ININSP/MAINT 1 NM19407QX 4049 C5 CHECK - FWD RUDDER BOTTOM PCU ATTACH POINT CASTING UPPER SURFACE HAS WEAR APPROX .007 DEEP FROM THE PCU FORK AND A GOUGE ON THE CORNER OF THE UPPER OUTTER RADIUS. CLEANED UP FWD RUDDER BOTTOM PCU ATTACH POINT CASTING DAMAGED AREAS. REF SRM 51-14-00-02-03 PARA 1-4 AND PARA 5B(2)(A) THRU (E). NO REPAIRS ALLOWED IAW SRM 55-41-20-00-01 ITEM 7. HFEC INSPECTED DAMAGED AREAS FOR CRACKS IAW NDTM PART 6, 51-00-01, NO CRACKS NOTED. UT THICKNESS CHECKED DAMAGED AREA IAW NDTM PART 1, 51-00-04. MAPPED DAMAGE FOR ENGINEERING. INSPECTED AREA OF BLEND AND FOUND BLENDED AREA TO BE WITHIN LIMITS IAW RD 8/4-55-506. ALODINED AND PRIMED BARE AREA TO COMPLETE REPAIR IAW RD 8/4-55-506. 2H72 4T RTA13NM 20100127 NM 2010 1 27 QXEA2010011200034120100108A5753 SKIN BOMBDRDHC8 DHC8402 1390042NM LT WING TE FLAP DAMAGED A QXEAK NONE O OTHER ININSP/MAINT 1 NM19407QX 4049 C5 CHECK -LT INBD FLAP UPPER SURFACE HAS 3 SPOTS OF CHAFE DAMAGE ON THE INBD END APPROX 20' FWD OF THE T/E. BLENDED AFFECTED AREA TO SMOOTH AND REMOVED DAMAGE. HFEC INSP BLENDED AREAS FOR CRACKS IAW NDTM PART 6, 51-00-01-250-801. NO CRACKS NOTED. UT THICKNESS CHECKED BLENDED AREAS IAW NDTM PART 1, 51-00-01. FLAP SKIN FOUND TO BE OUT OF LIMITS REF 57-51-30 PG 102. MAPPED FOR ENGINEERING. INSPECTED AREAF BLEND AND FOUND IT TO BE WITHIN LIMITS IAW RD 8/4-57-1295. ALODINED, PRIMED AND PAINTED BARE AREA IAW RD 8/4-57-1295. 2H72 4T RTA13NM 20100127 NM 2010 1 27 FDEA201001150186 120100115A531465182333 KEELBEAM BOEING727 727227 1384078NM BS 872 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21489FE 21492 LT KEELBEAM CRACKED BS 872 BETWEEN FASTENERS. TRIMMED OUT DAMAGE, FABRICATED REPAIR DOUBLER, CAD PLATED DOUBLER, HEAT TREATED DOUBLER AND INSTALLED IAW EA 7-5310-137782. 2L73 4F A3WE 20100127 NM 2010 1 27 FDEA201001190188 120100119A534753FX20617 SEAT TRACK BOEING727 727227 1384078NM BS 640-660 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21489FE 21492 CABIN SEAT TRACK BS 640 -660 LBL 56 IB FLANGE HAS SEVERAL SPOTS OF CORROSION. CORROSION FOUND OUT OF LIMITS. REMOVED SEAT TRACK SUPPORT FLANGE. FABRICATED NEW SEAT TRACK SUPPORT FLANGE AND INSTALLED IAW SRM 51-30-2, 51-20-1 AND 51-10-2. 2L73 4F A3WE 20100127 NE 2010 1 27 RU3A1002 220100112A7510 TUBE BEECH 300 300BEECH 1152930CE PWA PT6 PT6A60A 52043NE LT ENGINE BROKEN E RU3AK NONE B SMOKE/FUMES/ODORS/SPARKS LDLANDING 1 SW1574 FF9 ON GROUND WHEN ENGINES STARTED (WITH BLEEDS IN ENVIRONMENTAL) STRONG EXHAUST SMELL IN CABIN. SMELL GOES AWAY ONCE AIRCRAFT PRESSURIZES. WHEN AIRCRAFT STARTED WITH BLEEDS OFF (PNEUMATIC AND ENVIRONMENTAL) NO EXHAUST SMELL IN CABIN. ON TOUCHDOWN IMMEDIATELY GOT THE ODOR DURING ROLLOUT. WROTE UP DISCREPANCY. INSPECTION OF LT ENGINE FOUND INBOARD EXHAUST FLEX TUBE BROKEN. 2L72 4T4 T A24CE E4EA 20100127 SO 2010 1 27 CHQA201000009 120100117A361040303920SD O-RING EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007A 03030GL BLEED AIR SYS BLOWN A CHQAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL11566RP 145691 CAE312019 THE FLIGHT CREW REPORTED A BLEED 1 LEAK MESSAGE ON EICAS UPON ENTERING ICING CONDITIONS DURING CLIMB. THE CREW DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE BLEED SYSTEM AND FOUND A LEAK AT JOINT 15 UNDER THE CARGO COMPARTMENT FLOOR. THE O-RINGS AND COVER BOOT WERE REPLACED IAW EMB145 MM 36-11-09. OPS AND LEAK CHECKS GOOD. 2L72 4T4 FRTT00011ATTE6CH 20100127 WP 2010 1 27 FDEA201001160161 120100116A2760APH72721 SPRING DOUG MD10 MD1010F 3022112WP SPOILERS DAMAGED A FDEAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 CE2168051 47805 AT FL 340 APPROX 50 MIN INT FLT W/ PNEU SYS 2 MEL(ED) INOP (SYS CONFIGURED W/ 1-2 ISOL ON & NR 2 PACK & BLEED OFF) GOT AIR SYS 2 OFF FOLLOWED BY LVL 3 AIR MANF 2 FAIL. AIR MANF 2 FAIL SOON CLEARED BUT PNEU SYS 2 SCHEMATIC & OVERHEAD MANF LIGHT REMAINED RED EVEN AFTER SHUTDOWN. R & R CAM FOLLOWER SPRING ON 2&3 SPOILER LATERAL CONTROL MIXER IAW SRM. NO ADJUST OR CHANGES TO CABLE/PUSHROD RIGGING MADE TO FACILITATE REPAIR. PERFORMED VISUAL INSP OF SPOILER LATERAL CONTROL MIXER ASSY`S (2) & CONTROL SECTORS; NO FURTHER DISCREPANCIES NOTED. PERFORMED A LATERAL FLT CONTROL FUNCTION/SYMMETRY CHECK IAW AMM 27-60-00-5 STEP 3D48 A-E; LATERALS FUNCTIONED NORMAL IN CLEAN WING & TAKEOFF CONFIG. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001160164 120100116A5347A5A70829 SEAT TRACK DOUG MD11 MD11F 3023600NM ZONE 200 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21609FE 48549 CABIN - LT STA 1536 X = 47 SEAT TRACK FOUND CORROSION. REMOVED IAW SRM 51-33-01 REV 42 AND NEW SEAT TRACK REWORKED IAW DWG A5A7082 REV B. NEW SEAT TRACK INSTALLED IAW SRM 53-00-52 REPAIR 1 FIGURE 201 REVISION 42. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 109. 2L73 4F RTA22WE 20100127 NM 2010 1 27 FDEA201001170165 120100117A5410112N700223 BUSHING BOEING757 7572B7 1384964NM ZONE 400 MISALIGNED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21909FD 52338 27200 STRUT NR 1 DIAG BRACE WING FITTING OTBD BUSHING HAS MIGRATED. REMOVED BUSHINGS IAW SOPM 20-50-03. RECEIVED REPAIR BUSHINGS ON TRAV NR T9/811726. INSTALLED 2EA REPAIR BUSHINGS IAW EA F-5740-131560. CATEGORY "A". MAJOR REPAIR. 2L72 4F RTA2NM 20100127 NM 2010 1 27 FDEA201001170166 120100117A5753ARC70541 TEE FITTING DOUG MD11 MD11F 3023600NM LT WING TE FLAP CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21609FE 48549 LT WING OTBD FLAP VANE TEE FITTING (NR 2 FROM INBD) HOLE CORROSION. REPAIR CARRIED OUT IAW EA NR 1-5750-137545. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109. 2L73 4F RTA22WE 20100127 SO 2010 1 27 C2XA10RI015 120100119A2130 UNKNOWN EMB 145 EMB145LR 3260212SO CABIN PRESSURE MALFUNCTIONED A C2XAK NONE O OTHER CRCRUISE 1 SW2718556 145595 FLIGHT 2504 - EWR - FLIGHT CREW REPORTED CABIN RATE WOULD NOT CLIMB/DESCEND FROM 200 TO 1500 FT PER MIN IN CRUISE. CABIN ALTITUDE CLIMBED UP TO 8500 FT IN CRUISE. EWR MX PERFORMED VISUAL INSPECTION OF STATIC PORTS AND PERFORMED PRESSURIZATION TEST OF THE ACFT SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. 2L72 4T RTT00011AT 20100127 EU 2010 1 27 USAA2010012090152120100104A5730D5725270600000 PANEL AIRBUS320 A320231 3930325EU LT WING DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19637AW 99 SAL - BC7 - MAJOR REPAIR - DEBOND ON LEFT WING CLOSING PANEL 540CZ. REPLACED LEFT WING CLOSING PANEL 540CZ IAW A320 AMM 57-27-11. 2L72 4F RTA28NM 20100127 EU 2010 1 27 USAA2010012090156120100103A5754D5746002720200 ATTACH BOLT AIRBUS320 A320231 3930325EU LE SLAT CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19637AW 99 SAL - BC7 - MAJOR REPAIR - CORROSION ON LEFT WING NR 4 SLAT NR 9 SLAT TRACK ATTACH BOLT. REPLACED LEFT WING NR 4 SLAT NR 9 SLAT TRACK ATTACH BOLT IAW A329 AMM 27-84-62. 2L72 4F RTA28NM 20100127 EU 2010 1 27 USAA2010012090145120100118A499038761451 HEATER AIRBUS320 A320232 3930326EU APU DEFECTIVE A USAAK NONE B SMOKE/FUMES/ODORS/SPARKS NRNOT REPORTED 1 EA19659AW 1166 FLT 373 - CLT - CABIN ODOR - STRONG "DIRTY SOCK" ODOR THROUGHOUT CABIN. ODOR ALSO NOTED ON JETWAY AFTER OPENING CABIN DOOR. MAINTENANCE REPLACED APU OIL HEATER PER AIRBUS MAINTENANCE MANUAL 49-96-51. 2L72 4F RTA28NM 20100127 2010 1 27 SWAA100356 420100120A256563550 SLIDE BOEING737 7377H4 1384404NM R1 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29218WN 32489 DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20100127 2010 1 27 SWAA100357 420100120A256563550 SLIDE BOEING737 7377H4 1384404NM R2 DOOR OUT OF ADJUST A SWAAK NONE O OTHER ININSP/MAINT 1 SW29218WN 32489 DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2L72 4F RTA16WE 20100127 NM 2010 1 27 SWAA100360 120100120A335081000 LIGHT BOEING737 7373H4 1384600NM EXTERIOR INOPERATIVE A SWAAK NONE L NO TEST ININSP/MAINT 1 SW29339SW 24090 DURING SCHEDULED MV2 CHECK, FOUND AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM. 2L72 4F RTA16WE 20100127 NM 2010 1 27 SWAA100362 120100121A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100127 NM 2010 1 27 SWAA100363 120100121A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 685, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100127 NM 2010 1 27 SWAA100364 120100121A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 559, STR 11L. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100127 NM 2010 1 27 SWAA100365 120100121A534065C27314 STRINGER CLIP BOEING737 7373H4 1384600NM FUSELAGE CRACKED A SWAAK NONE O OTHER ININSP/MAINT 1 SW29382SW 26588 DURING SCHEDULED 16Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 597, STR 11R. REMOVED AND REPLACED CLIP PER SRM. 2L72 4F RTA16WE 20100128 NM 2010 1 28 ASAA1047257 120100119A5755654645170A SKIN BOEING737 737490 1384715NM SPOILER DAMAGED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 NUMBER 2 SPOILER LOWER SURFACE DENTED AND GOUGED. INSTALLED FILLER AND DOUBLER. 2L72 4F RTA16WE 20100128 CE 2010 1 28 GLBA20100118A 120100118A3060 BOOT BEECH 1900 1900D 1154162CE PROP DE ICE SPARKS A GLBAH DEACTIVATE SYST/CIRCUITS B SMOKE/FUMES/ODORS/SPARKS CRCRUISE 1 NM21237YV UE237 SPARKS WERE COMING FROM NR 1 PROP WHEN DE-ICE WAS ENGAGED HAD LARGE BURN MARK ON BOOT. MX R & R THE LT PROPELLER IAW TASKCARD 1900-6110.00. THE OPS CHECK AND LEAK CHECK WERE GOOD PN HC-E4A-3J SN ON HJ2050, SN OFF HJ1695. RII INSPECTIONS WAS SATISFACTORY IAW TASKCARD 1900-6110.00. 2L72 4T RTA24CE 20100128 WP 2010 1 28 DALA100969996 120100125A3397 CONNECTOR DOUG DC9 DC931 3022065WP EMERGENCY LIGHTSDISCONNECTED A DALAK NONE O OTHER ININSP/MAINT 1 SO278932E 47141 DURING LINE CHECK, MX FOUND THAT THE RT AFT RED EMERGENCY PATHWAY LIGHTING WAS INOPERATIVE. MX FOUND A CONNECTOR IN THE WIRE HARNESS UNPLUGGED, RECONNECTED IT, AND FUNCTIONALLY CHECKED THE SYS. 2L72 4F A6WE 20100128 CE 2010 1 28 GLBA20100113G 120100113A5754 SKIN BEECH 1900 1900D 1154162CE RT WING SLAT CRACKED A GLBAK NONE O OTHER ININSP/MAINT 1 NM21245GL UE245 MAJOR REPAIR - DURING A ROUTINE DE-ICE REPLACEMENT, A CRACK WAS FOUND ON THE RT WING AT WS 190.74 AT THE WING BOOT TUBE CONNECTION HOLE, PROTRUDING INBD. CRACK LENGTH APPROX 1.250" IN LENGTH. MX REPAIRED THE CRACK IAW EO 10-1900-87-001. RII INSPECTIONS COMPLIED WITH IAW EO 10-1900-87-001. MATERIALS UTILIZED ARE INCLUDED IN THE EO. 2L72 4T RTA24CE 20100128 EU 2010 1 28 DALA101513305 120100125A5347 SEAT TRACK AIRBUS330 A330323 3940030EU CABIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27805NW 0552 DURING "H" CHECK FOUND CORROSION ON SEAT TRACK Y1959 AT FR 61. REPAIRED IAW 53-00-15. 2L72 4F RTA46NM 20100128 WP 2010 1 28 DALA101359926 120100111A3097 WIRE DOUG DC9 DC932 3022066WP COCKPIT WINDOW SHORTED A DALAH DEACTIVATE SYST/CIRCUITS A FLAME/FIRE NRNOT REPORTED 1 SO27926NW 47425 SPARKS AND A SMALL FIRE EMANATED FROM THE LOWER AREA OF THE F/O SLIDING WINDOW AT THE TIME THE COMMUNICATIONS HEADSET WAS PLUGGED IN. FLIGHT CREW STATED THAT BOTH THE WINDOW AND ANTI-ICE AND ANTI-FOG SWITCH WERE IN THE "ON" POSITION. NO MENTION OF QRH COMPLIANCE. MX INITIALLY DEFERRED THE SYS AND SIX DAYS LATER FOUND WIRE BROKEN AT TERMINAL BLOCK AND ARC DAMAGE TO WINDOW FRAME FOR CAPTAIN'S WINDOW ANTI-FOG SYSTEM. MX REPLACED BOTH THE CAPTAIN & F/O CLEAR VIEW WINDOW TERMINAL BLOCKS. 2L72 4F A6WE 20100128 EA 2010 1 28 ASOA201000079 120100122A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA EXTERNAL EMERG INOPERATIVE A ASOAK NONE L NO TEST ININSP/MAINT 1 SO27751EV 10163 RT REAR EXTERNAL EMERGENCY LIGHT INOP. R & R RT REAR EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECK GOOD. 2L72 4F RTA21EA 20100128 EA 2010 1 28 ASOA201000080 120100122A5210 DOOR CNDAIRCL600 CL6002B19 1900309EA MAIN PAX STUCK A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 UPON REACHING GATE MAIN PAX DOOR WOULD NOT OPEN. AFTER SEVERAL ATTEMPS WE WERE ABLE TO OPEN DOOR. LUBE PAX DOOR HANDLE TRACKS, OPS CHECK GOOD, OK FOR SERVICE IAW AMM 52-10-00. 2L72 4F RTA21EA 20100128 EA 2010 1 28 ASOA201000081 120100122A5210 CYLINDER CNDAIRCL600 CL6002B19 1900309EA MAIN PAX DOOR OUT OF RIG A ASOAK NONE O OTHER ININSP/MAINT 1 SO27839AS 7284 CREW REPORTED PAX DOOR HARD TO OPEN. TROUBLESHOT PAX DOOR FOUND FWD GAS SPRING OUT OF RIG AND SUPPORT WHEEL DRAGGING ON DOOR FRAME. RIGGED PAX DOOR FWD GAS SPRING AND SUPPORT WHEEL IAW AMM 52-11-17 AND 52-11-13. 2L72 4F RTA21EA 20100128 EA 2010 1 28 ASOA201000083 120100122A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27843AS 7310 LT MID FS 625 OBLIQUE ANGLE IS CRACKED AT BL 45, STR LT WL 97.5. R & R LT MID FS 625 OBLIQUE ANGLE IAW SRM 51-42-21. PAINTED OBLIQUE ANGLE IAW SRM 51-25-16. 2L72 4F RTA21EA 20100128 EA 2010 1 28 ASOA201000084 120100122A5320 ANGLE CNDAIRCL600 CL6002B19 1900309EA BS 625 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27843AS 7310 RT MID FS 625 OBLIQUE ANGLE IS CRACKED AT BL 45, STR R14 WL 97.5. R & R RT MID FS 625 OBLIQUE ANGLE IAW SRM 51-42-21. PAINTED OBLIQUE ANGLE IAW SRM 51-25-16. 2L72 4F RTA21EA 20100128 EA 2010 1 28 ASOA201000085 120100122A1100 PLACARD CNDAIRCL600 CL6002B19 1900309EA PAX DOOR PEELING A ASOAK NONE O OTHER ININSP/MAINT 1 SO27843AS 7310 PAX DOOR "EXIT" PLACARD IS PEELING. REMOVED PAX DOOR EXIT PLACARD IAW AMM 11-20-00-000-801. INSTALLED NEW PAX DOOR EXIT PLACARD IAW AMM 11-20-00-400-801. 2L72 4F RTA21EA 20100128 NM 2010 1 28 ASAA1047259 120100119A5755654645262A SKIN BOEING737 737490 1384715NM SPOILER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 LEFT I/B GROUND SPOILER CLUSTER OF SMALL DENTS AFT OF I/B ACTUATOR LOWER SURFACE. INSTALLED FILLER AND DOUBLER. 2L72 4F RTA16WE 20100128 EA 2010 1 28 ASOA201000086 120100122A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA BS 621 CRACKED A ASOAK NONE O OTHER ININSP/MAINT 1 SO27844AS 7317 FS 621.00 PRESSURE BULKHEAD FWD FACE HAS AN 80 PERCENT FSH HFEC INDICATION NOTED APPROX 0.50" LONG EXTENDING FROM THE UPPER CORNER OF THE AFT CARGO DOOR TRACK AT LBL 27.50 APPROX WL 131.00. COMPLIED WITH EC/TC REO 601R-53-61-1541. 2L72 4F RTA21EA 20100128 WP 2010 1 28 FDEA201001250240 120100125A5311AEA04394 FRAME DOUG DC10 DC1030F 3023504WP BS 1501 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21320FE 47835 RT MLG WHEEL WELL, FOUND CRACK ON FRAME. TRIMMED OUT DAMAGED SECTION OF FRAME IAW SRM 53-30-00 FIG.5 VOL.1. INSTALLED NEW SECTION OF FRAME & SPLICE IAW SRM 53-00-01 FIG.10 SH.5 VOL.1 2L73 4F RTA22WE 20100128 NM 2010 1 28 ASAA1047261 120100120A57536546430190 SKIN BOEING737 737490 1384715NM FOREFLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 RIGHT WING I/B FOREFLAP LOWER SKIN HAS A DENT CLUSTER WITH OVERLAPPING DAMAGE WBL 80 TO WBL 95. INSTALLED FILLER AND DOUBLER. 2L72 4F RTA16WE 20100128 NM 2010 1 28 ASAA1047268 120100111A575465C26603202A SKIN BOEING737 737490 1384715NM LE SLAT CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 NUMBER 4 SLAT LOWER SURFACE I/B AFT EDGE IS CHAFED. REMOVED DAMAGED ARE, FABRICATED REPAIR DOUBLER AND FILLER AND BONDED. 2L72 4F RTA16WE 20100128 EU 2010 1 28 FDEA201001250248 120100125A5321SRZ25005252UH FLOORBOARD AIRBUS300 A300F4605R 3930327EU ZONE 200 DAMAGED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21681FE 15457 799 MAIN CABIN CARGO COMPARTMENT FLOORBOARD NR 252 UH IS PUNCTURED. REPAIRED MAIN CAB CARGO COMPARTMENT FLOOR PANEL NR 252 UH BY FABRICATING NEW FLOOR PANEL USING OLD FLOOR PANEL NR 252 UH AS TEMPLATE IAW DWG SRZ 25-005, REV "H". 2L72 4F RTA35EU 20100128 NM 2010 1 28 ASAA1047269 120100111A575465C26602312A SKIN BOEING737 737490 1384715NM LE SLAT DELAMINATED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 NR 5 SLAT UPPER SURFACE O/B CORNER DELAMINATED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F RTA16WE 20100128 NM 2010 1 28 ASAA1047270 120100111A575465C26603202A SKIN BOEING737 737490 1384715NM LE SLAT CHAFED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 NR 4 SLAT LOWER SURFACE I/B AFT EDGE IS CHAFED. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER. 2L72 4F RTA16WE 20100128 NM 2010 1 28 ASAA1047278 120100112A57536546486149 SKIN BOEING737 737490 1384715NM TE FLAP DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 LEFT I/B MID FLAP T/E WEDGE HAS CLUSTER OF SMALL DENTS ON LOWER SURFACE. REPAIRED LEFT I/B MID FLAP T/E WEDGE. 2L72 4F RTA16WE 20100128 WP 2010 1 28 FDEA201001250241 120100125A5347ADA7321503 CARGO TRACK DOUG DC10 DC1030F 3023504WP BS 755 CRACKED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21320FE 47835 FWD CARGO COMPT FOUND CRACK ON TRACK. REMOVED AND REPLACED SECTION OF TRACK IAW SRM 53-70-00 FIG.1 SH.1 VOL.1. 2L73 4F RTA22WE 20100128 NM 2010 1 28 ASAA1047280 120100112A5755654645268A SKIN BOEING737 737490 1384715NM SPOILER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 RIGHT WING INBOARD NR 5 SPOILER UPPER SKIN DENTED WITHIN CRITICAL AREA 3 INCHES FROM LEADING EDGE 19 INCHES FROM OUTBOARD END. REPAIRED DENT DAMAGE ON UPPER SURFACE OF SPOILER NR 5. 2L72 4F RTA16WE 20100128 NM 2010 1 28 ASAA1047282 120100112A5755654645268A SKIN BOEING737 737490 1384715NM SPOILER DENTED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02709AS 28896 RIGHT WING NR 5 SPOILER LWR SKIN HAS CLUSTER OF DENTS AT I/B END FROM LEADING EDGE TO TRAILING EDGE. REPAIRED DENT DAMAGE. 2L72 4F RTA16WE 20100128 EU 2010 1 28 DALA101533305 120100125A5347 SEAT TRACK AIRBUS330 A330323 3940030EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27805NW 0552 DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y450 BETWEEN FR 37.3 AND FR 37.4. REPAIRED IAW SRM 53-31-15. 2L72 4F RTA46NM 20100128 EU 2010 1 28 DALA100993259 120100122A5320 FLOOR SUPPORT AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27359NW 846 DURING "M" CHECK FOUND CORROSION ON FLOOR SUPPORT BETWEEN FR 65 AND FR 66 Y732. REPAIRED IAW SRM 51-42-11. 2L72 4F RTA28NM 20100128 EU 2010 1 28 DALA101003259 120100122A5320 FLOOR SUPPORT AIRBUS320 A320212 3930322EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27359NW 846 DURING "M" CHECK FOUND CORROSION ON RT FLOOR SUPPORT BETWEEN FR 69 AND FR 70. REPAIRED IAW SRM 51-44-11 AND SRM 51-42-11. 2L72 4F RTA28NM 20100128 EU 2010 1 28 DALA101013259 120100123A5320 SILL AIRBUS320 A320212 3930322EU AFT PAX DOORWAY CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27359NW 846 DURING "M" CHECK FOUND CORROSION ON LT AFT PASSENGER DOOR SILL. REPAIRED IAW SRM. 51-42-11. 2L72 4F RTA28NM 20100128 EU 2010 1 28 DALA101373355 120100123A3397 CONNECTOR AIRBUSA330 A330223 3930374EU EMERGENCY LIGHTSDISCONNECTED A DALAK NONE L NO TEST ININSP/MAINT 1 SO27855NW 0621 TEST OF EMERGENCY LIGHTING FOUND CEILING LIGHT ABOVE SEAT 3G-H NOT ILLUMINATED, CORRECTED PLUG INSTALLATION AND CHECKED OK. 2L72 4F RTA46NM 20100128 2010 1 28 ASAA1057262 420100120A2310 UNKNOWN BOEING737 737890 1384527NM HF COMM MALFUNCTIONED A ASAAK NONE O OTHER NRNOT REPORTED 1 NM02585AS 35683 BOTH HF RADIOS CUTTING OUT DURING TRANSMISSION. TRIED BOTH STATIONS (CAPT AND F/O) AS WELL AS HANDHELD MIC WITH TRANSMISSIONS STILL CUTTING OUT. OTHER RADIOS APPEAR NORMAL. SWITCHED FREQS AND HF APPEARS TO BE OPERATING NORMALLY. RADIO WAS CUTTING ON FREQ 5574 BUT APPEARS TO OPERATE NORMALLY ON 3413 AND 6673. NR 1 AND 2 HF'S OPS AND SYSTEM TEST NORMAL USING FREQ 5.574 (SFO ARINC) COULD NOT DUPLICATE FAULT. NO HISTORY, SYSTEM OK FOR SERVICE REF M/M 23 11 0. 2L72 4F RTA16WE 20100128 WP 2010 1 28 DALA101389855 120100125A3397 WIRE DOUG DC9 DC951 3022051WP EMERGENCY LIGHT BROKEN A DALAK NONE L NO TEST ININSP/MAINT 1 SO27764NC 47717 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 4C IN THE FIRST CLASS CABIN WAS INOPERATIVE. MX FOUND A BROKEN WIRE AT THE CONNECTOR UNDER SEAT 4D. THE WIRE WAS RE-PINNED TO THE CONNECTOR AND THE SYS RETURNED TO NORMAL OPERATION. 2L72 4F RTA6WE 20100128 CE 2010 1 28 DXTA2010012703957120100126A3243991205018 MASTER CYLINDER CESSNA500 560CESSNA 2076750CE MLG WEAK E DXTAD RETURN TO BLOCK S AFFECT SYSTEMS TXTAXI/GRND HDL 1 GL07318QS4426 5600418 COPILOT SIDE, RT BRAKE PEDAL GOES SOFT DURING TAXI. AFTER PEDAL WAS ALMOST TO THE FLOOR, RELEASED PRESSURE, AND BRAKING WAS RESTORED. THIS HAPPENED 5 TIMES ON A 2 MILE TAXI. R & R COPILOTS RT MASTER CYLINDER IAW MM CHP 32-42-01. BLEED SYS IAW MM CHP 32-42-20. BRAKE SYS, OPS AND LEAK CHECKS GOOD. 2L72 4F RTA22CE 20100128 WP 2010 1 28 DALA101719936 120100126A3350 BATTERY PACK DOUG DC9 DC931 3022065WP EMERGENCY LIGHT INOPERATIVE A DALAK NONE O OTHER ININSP/MAINT 1 SO271799U 47370 DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING FOR THE CATWALK IN THE TAIL COMPARTMENT WAS INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION. 2L72 4F A6WE 20100128 EU 2010 1 28 DALA101573305 120100125A5347 SEAT TRACK AIRBUS330 A330323 3940030EU CABIN CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27805NW 0552 DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y2462 FR 50. REPAIRED IAW ERA 478947-14. 2L72 4F RTA46NM 20100128 EU 2010 1 28 DALA101583305 120100125A5320 FLOOR SUPPORT AIRBUS330 A330323 3940030EU FUSLEAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27805NW 0552 DURING "H" CHECK FOUND CORROSION ON FLOOR STRUCTURE AT Y1456 FR 15-16. REPAIRED IAW ERA 478937-14. 2L72 4F RTA46NM 20100128 NM 2010 1 28 ASAA1057273 120100122A3350D71702001 BATTERY PACK BOEING737 737890 1384527NM CABIN FAILED A ASAAK NONE O OTHER ININSP/MAINT 1 NM02569AS 35184 BATTERY PACK M1673 AFT LEFT FAILS DEEP CYCLE TEST. REMOVED AND REPLACED DEFECTIVE BATTERY PACK. 2L72 4F RTA16WE 20100128 EU 2010 1 28 DALA101593305 120100125A5347 SEAT TRACK AIRBUS330 A330323 3940030EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27805NW 0542 DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y950 FR 17. REPAIRED IAW ERA 478936-14. 2L72 4F RTA46NM 20100128 NM 2010 1 28 ASAA1057275 120100121A499038762983 SENSOR BOEING737 737890 1384527NM APU FAULTY A ASAAK NONE N FALSE WARNING ININSP/MAINT 1 NM02579AS2634 2634 35187 DURING CHECK FOUND APU FAULT MAINT MSG 49 94304 OIL LEVEL SENSOR SHOW CIRCUIT FAILURE. ACCOMPLISHED FIM TASK 49 90 00 810 811. WIRE HARNESS CHECK GOOD. REMOVED AND REPLACED OIL LEVEL SENSOR AS PRECAUTION REF MM 49 94 11. VERIFIED PART. SEAMC CONTACTED. OPS CHECK APU, NO LEAKS. OK FOR SERVICE AT THIS TIME. 2L72 4F RTA16WE 20100128 EU 2010 1 28 DALA101133305 120100123A5347 SEAT TRACK AIRBUS330 A330323 3940030EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27805NW 0552 DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 35. REPAIRED IAW SRM 53-00-15. 2L72 4F RTA46NM 20100128 EA 2010 1 28 COMA2010012550023120100123A492038004883 APU CNDAIRCL600 CL6002B19 1900309EA APU BAY SEIZED A COMAO OTHER B SMOKE/FUMES/ODORS/SPARKS TXTAXI/GRND HDL 1 SO27958CA18322 7111 DURING TAXI APU SEIZED AND SHUT DOWN WITH A PUNGENT ELECTRICAL SMELL. SMOKE EXITING FROM APU DOOR. RECEIVED APU FAULT CAUTION MSG. REMOVED AND REPLACED APU. 2L72 4F RTA21EA 20100128 NM 2010 1 28 MASA2010012300064120100123A3350 LIGHT DHAV DHC8 DHC8202 2809007NM CABIN INOPERATIVE A MASAO OTHER O OTHER UKUNKNOWN 1 SW07456YV 456 FLOOR E-LIGHTS 2 FWD RED LIGHTS OUT. FLOOR LIGHTS, OPS GOOD. 2H72 4T RTA13NM 20100128 EA 2010 1 28 MASA2010012300070120100123A3350 LIGHT CNDAIRCL600 CL6002D24 1390016EA CABIN INOPERATIVE A MASAO OTHER O OTHER UKUNKNOWN 1 SW07917FJ 15017 THE 3RD AFT OVERHEAD EMERGENCY FLOOD LIGHT INOP. RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100128 EA 2010 1 28 MASA2010012400058120100124A3350 LIGHT CNDAIRCL600 CL6002B19 1900309EA CABIN INOPERATIVE A MASAO OTHER O OTHER UKUNKNOWN 1 SW0775993 7372 CREW REPORTED ON PREFLIGHT, BOTH EXT FWD WING EMERGENCY FLOOD LIGHT ARE INOPERATIVE. FAULT WAS PLACED ON MEL WITH THE CREW. RELAMPED EMERGENCY LIGHT. 2L72 4F RTA21EA 20100128 EA 2010 1 28 MASA2010012400059120100124A3397 CONNECTOR CNDAIRCL600 CL6002B19 1900309EA CABIN LOOSE A MASAO OTHER O OTHER UKUNKNOWN 1 SW0787353 7353 HNL - REPORTED EMERGENCY EXIT PATH LIGHTING THAT FAILED TO ILLUMINATE. MX FOUND AND SECURED A LOOSE WIRING CONNECTION AT THE LIGHTING ASSEMBLY. 2L72 4F RTA21EA 20100128 NM 2010 1 28 NOCA01210 120100125A5345415N40029 MOUNT FITTING BOEING757 75728A 1384976NM GALLEY CORRODED A NOCAK NONE O OTHER ININSP/MAINT 1 EA15752NA 28174 AFT GALLEY RIGHT AFT TIE DOWN FITTING CORRODED. REPLACED MOUNT FITTING PER SRM 51-10-02. 2L72 4F RTA2NM 20100201 NM 2010 2 1 FDEA201001260262 120100126A5347451N570081 CARGO TRACK BOEING757 7572T7 1384914NM ZONE 100 CORRODED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21936FD 23293 AFT CARGO COMPARTMENT FLOOR SIDE PANEL TIE DOWN FOUND WITH SURFACE CORROSION AS MARKED, STA 1377 LT. CORRODED TIE-DOWN FITTING AT STA 1377 IN AFT CARGO COMPARTMENT REMOVED AND REPLACED IAW SRM 51-40-02 REV 99. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA. 2L72 4F RTA2NM 20100201 2010 2 1 CHQA201000015 420100124A34527510700766 TRANSCEIVER EMB 145 EMB145LR 3260212SO ALLSN AE3007AE3007A 03030GL NR 2 FAULTY A CHQAA UNSCHED LANDING O OTHER CLCLIMB 1 GL11265SK2364 145226 CAE311953 CREW REPORTED THAT AFTER TAKEOFF TRANSPONDERS 1 AND 2 WERE INOP WITH NO TCAS INFORMATION. ATC RECEIVERS HAD PRIMARY RADAR TARGET ONLY AND NO ALTITUDE INFORMATION. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 COMMUNICATIONS UNIT WITH NO FURTHER DEFECTS NOTED. 2L72 4T4 FRTT00011ATTE6CH 20100201 EU 2010 2 1 DALA101433305 120100125A5347 SEAT TRACK AIRBUS330 A330323 3940030EU FUSELAGE CORRODED A DALAK NONE O OTHER ININSP/MAINT 1 SO27805NW 0552 DURING "H" CHECK FOUND CORROSION ON SEAT TRACK AT Y1959 FR 36 AND FR 37. REPAIRED IAW SRM 53-00-15. 2L72 4F RTA46NM 20100201 WP 2010 2 1 FDEA201001220214 120100122A5330 SKIN DOUG DC10 DC1030F 3023504WP ZONE 100 CHAFED A FDEAK NONE O OTHER ININSP/MAINT 1 CE21306FE5754157541 48287 FUSELAGE EXTERNAL SKIN IS CHAFED AND GOUGED AT LWR CTR CARGO DOOR LWR AFT JAMB BELOW SEAL RETAINER. REPAIRED FUSELAGE EXTERNAL SKIN AT CTR CARGO DOOR LOWER AFT JAMB BELOW SEAL RETAINER IAW SRM 53-50-00.MAJOR REPAIR. 2L73 4F RTA22WE 20100201 EU 2010 2 1 NSVA2010018 120100121A5330 SKIN SAAB SF340 340B 7860101EU FUSELAGE DAMAGED A NSVAK NONE O OTHER ININSP/MAINT 1 EA27321CJ 340B321 ACFT REQUIRES MAJOR REPAIR FOR PERM REPAIR OF PUNCTURE DAMAGE TO RT FUSELAGE AT STA 360.25 IAW TD 340-53-09-85. 2L72 4T RTA52EU 20100201 EU 2010 2 1 NSVA201022 120100121A5420 STRUCTURE SAAB SF340 340B 7860101EU NACELLE DAMAGED A NSVAK NONE O OTHER ININSP/MAINT 1 EA27191MJ 340B191 ACFT REQUIRES MAJOR REPAIR FOR PER REPAIR FOR MISC RIVET DEVIATION ON RT INBOARD NACELLE IAW TD 340-54-09-82. 2L72 4T RTA52EU 20100201 NM 2010 2 1 R61A20100030 120100125A5320 GUSSET EMB ERJ170ERJ170100SU 3260403NM FUSELAGE CORRODED A R61AK NONE O OTHER ININSP/MAINT 1 GL11803MD14939 17000015 WHILE AC WAS IN FOR HEAVY CHECK, LEVEL TWO CORROSION WAS FOUND ON GUSSET FOR RT SEAT TRACK AT FR 90. MAINTENANCE REQUESTED EMB ENGINEERING SUPPORT AND RECEIVED ETD 2009/170-00325 FOR REMANUFACTURE OF GUSSET. REPLACED AS REQUIRED PER SRM AND AC RELEASED AFTER CHECK WAS COMPLETE. 2L72 4F RTA56NM 20100201 NE 2010 2 1 HALA2010011500033220100115A7510 ANTI-ICE VALVE BOEING767 76733A 1385209NM PWA PW4062PW4062 NE LT ENGINE MALFUNCTIONED A HALAO OTHER J WARNING INDICATION CRCRUISE 1 WP35583HA 25531 ETOPS SIGNIFICANT SYSTEM, LEFT ENG ANTI ICE STICKS IN THE ON POSITION. EXERCISED VALVE MANUALLY FOR LEFT ENG ANTI ICE VALVE. REMOVED, INSPECTED, CLEANED AND REINSTALLED C/P FOR ANTI ICE VALVE. ALL INDICATIONS NOW NORMAL. OK FOR FURTHER SERVICE. 2L72 4F4 FRTA1NM E24NE 20100201 NM 2010 2 1 HALA2010011300019120100113A2913887673 PUMP BOEING767 7673G5 1385126NM HYD SYSTEM LEAKING A HALAK NONE K FLUID LOSS ININSP/MAINT 1 WP35586HA3047 3047 24259 ETOPS SIGNIFICANT SYSTEM - ON WALK AROUND FOUND NR 1 ENG HYDRAULIC PUMP LEAKING. REMOVED AND REPLACED HYDRAULIC PUMP AT NR 1 ENG PER AMM 29-11-5. LEAK CHECK AND SECURITY CHECK OK. 2L72 4F RTA1NM 20100201 SO 2010 2 1 RAIA2010012000002120100120A3412102AU1AF PROBE EMB 145 EMB145EP 3260221SO TAT FAULTY A RAIAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE03803HK 145077 DURING CLIMBOUT OF ORD, THE CREW REPORTED RECEIVING A NR 1 TAT PROP HEAT INOP MESSAGE ON THE EICAS. MAINTENANCE REMOVED AND REPLACED THE NR 1 TAT PROBE AND OPS CHECKED IT GOOD IAW AMM PROCEDURES. 2L72 4F RTT00011AT 20100201 EA 2010 2 1 REXA201000013 120100124A7932 SENSOR CNDAIRCL600 CL6002B19 1900309EA LT ENGINE FAILED A REXAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 CE218837B 7837 DURING CLIMBOUT OF KRDU THE FLIGHT CREW NOTICED THE LT ENGINE OIL TEMPERATURE WAS INDICATING HIGH. THE FLIGHT CREW REDUCED POWER ON THE ENGINE WHICH CAUSED A REDUCTION IN THE OIL TEMPERATURE TO THE TOP OF THE AMBER LIMIT. THE FLIGHT CREW PERFORMED THE QRH AND REQUESTED TO DIVERT TO TYS. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KTYS. COMPANY MAINTENANCE DETERMINED THAT THE ENGINE OIL WAS OVERSERVICED DUE TO A FAILED HIGH LEVEL SENSOR IN THE REMOTE OIL SERVICING SYSTEM. THE REMOTE SERVICING SYSTEM WAS DEFERRED, ENGINE OIL DRAINED TO NORMAL LEVEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE. 2L72 4F RTA21EA 20100201 EA 2010 2 1 SIMA201002204 120100122A531267053110521 BULKHEAD CNDAIRCL600 CL6002C10 1390015EA FUSELAGE CORRODED A SIMAK NONE O OTHER ININSP/MAINT 1 SW21503AE18432 10021 DURING MAINTENANCE BASE VISIT FOUND THE LEFT WEB CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED SERVICEABLE LEFT LOWER BULKHEAD WEB IAW AE EO CR-53MR-174. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20100201 EA 2010 2 1 SIMA201002504 120100124A3250530133 TILLER CNDAIRCL600 CL6002C10 1390015EA NLG STEERING INOPERATIVE A SIMAK NONE J WARNING INDICATION TOTAKEOFF 1 SW21521AE14782 10142 ON FLIGHT 4217 DURING THE CLIMBOUT THE CREW REPORTED, RECEIVED A STEERING INOPERABLE CAUTION MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND CONTINUED TO ABQ. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED HAND WHEEL CONTROL ASSEMBLY IAW CRJ IAW AMM 32-51-00. THE NOSE WHEEL OPERATIONAL TEST WERE NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. 2L72 4F RTA21EA 20100201 NM 2010 2 1 ZZDA2010031 120100123A5320 CUSP WEB BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37934AT 55070 RIGHT CABIN CUSP WEB, STA 522 TO 541, CORROSION. ACCOMPLISHED CABIN CUSP WEB DOUBLER REPAIR PER B717 SRM 51-41-02. 2L72 4F TRA6WE 20100201 NM 2010 2 1 ZZDA2010034 120100124A5320 FLOOR SUPPORT BOEING717 717200 1383700NM FUSELAGE CORRODED A ZZDAK NONE O OTHER ININSP/MAINT 1 SO37934AT 55070 CABIN FLOOR SUPPORT BEAM, STA 204 TO 243, LBL 15, CORROSION. ACCOMPLISHED FLOOR SUPPORT BEAM REPLACEMENT PER B717 SRM 51-41-02 AND B717 SRM 51-41-01. 2L72 4F TRA6WE 20100202 NM 2010 2 2 YENA20100124012 120100124A531517003264001 FLOORBEAM EMB ERJ190ERJ190100IGW3260408NM FUSELAGE CORRODED A YENAK NONE O OTHER ININSP/MAINT 1 EA15193JB11211 190000017 DURING 12K C CHECK AT EMBRAER AIRCRAFT MAINTENANCE SERVICES BNA FOUND FLOORBEAM CORROSION AT TWO LOCATIONS. FWD GALLEY AREA ON LT FLOORBEAM FROM FRAME 13 TO FRAME 19 HAS 7 AREAS OF CORROSION AND RT FLOORBEAM FROM FRAME 14 TO FRAME 17 HAS 9 AREAS OF CORROSION CLASSIFIED AS LEVEL 1 FIRST FINDING, REMOVED AND REPLACED FLOORBEAMS IAW SRM 51-40-02, 51-21-00, 51-41-01. REF EAMS N/R'S 2541 AND 2542 WO H1302. 2L72 4F RTA57NM 20100202 NM 2010 2 2 USAA2010012290171120100121A53306545774 SKIN BOEING737 737401 138449BNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US 23886 CLT - C6 - MAJOR REPAIR - CRACK IN FUSELAGE SKIN AT BS 727F, S25L. REPAIRED FUSELAGE SKIN AT BS 727F, S25L IAW B737 SRM 53-00-01 REPAIR 31. 2L72 4F RTA16WE 20100202 EU 2010 2 2 USAA2010012590186120100114A5315D5347207500000 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW 929 PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM BETWEEN FR65 TO FR66, S23L, Y1732. REPLACED FLOORBEAM BETWEEN FR65 TO FR66, S23L, Y1732 IAW A319 SRM 51-72-11. 2L72 4F RTA28NM 20100202 NM 2010 2 2 USAA2010012590180120100121A5755654645262A MOUNT BRACKET BOEING737 7373G7 138447JNM SPOILER CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19303AW3359433594 24010 PHX - B4 - MAJOR REPAIR - CRACK ON NR 5 GROUND SPOILER INBOARD SPOILER MOUNT BRACKET AT PIVOT ARM, RSS179.56. REPLACED NR 5 GROUND SPOILER IAW B737 AMM 27-62-12-4. 2L72 4F RTA16WE 20100202 EU 2010 2 2 USAA2010012290164120100110A3211D3215303000800 PIN AIRBUS320 A320231 3930325EU RT MLG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19637AW 99 SAL - BC7 - MAJOR REPAIR - CORROSION ON THREADS OF RIGHT MAIN LANDING GEAR REAR PINTLE PIN. REPLACED RIGHT MAIN LANDING GEAR REAR PINTLE PIN IAW JOB CARD R4M32304. 2L72 4F RTA28NM 20100202 EU 2010 2 2 USAA2010012290165120100111A3211D3215303000600 PIN AIRBUS320 A320231 3930325EU LT MLG CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19637AW 99 SAL - BC7 - MAJOR REPAIR - CORROSION ON LEFT MAIN LANDING GEAR REAR PINTLE PIN LOCATED AT INTERNAL CAVITY. REPLACED LEFT MAIN LANDING GEAR REAR PINTLE PIN IAW JOB CARD R4M32304. 2L72 4F RTA28NM 20100202 NM 2010 2 2 USAA2010012290168120100119A5313654658599 STRAP BOEING737 7374B7 138449CNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19450UW 24933 SAL - Q4 - MAJOR REPAIR - CRACK ON FUSELAGE STRINGER STRAP AT BS 1138, S12L. REPAIRED FUSELAGE STRINGER STRAP AT BS 1138, S12L IAW EA 132791. 2L72 4F RTA16WE 20100202 NM 2010 2 2 USAA2010012590181120100121A5752654645528BF TAB BOEING737 7373G7 138447JNM AILERON DEBONDED A USAAK NONE O OTHER ININSP/MAINT 1 EA19303AW 24010 PHX - B4 - MAJOR REPAIR - DISBOND AREA ON RIGHT AILERON TAB AT WBL 422.8. REPLACED RIGHT AILERON TAB IAW JOB CARD R3M27014. 2L72 4F RTA16WE 20100202 EU 2010 2 2 USAA2010012590183120100115A5320D53480020343 PLATE AIRBUS320 A320232 3930326EU FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19652AW 953 SAL - S5 - MAJOR REPAIR - CRACK ON PLATE BETWEEN FR68 TO FR69, S23R. REPLACED PLATE BETWEEN FR68 TO FR69, S23R IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20100202 EU 2010 2 2 USAA2010012590184120100113A5315D53111450202 FLOORBEAM AIRBUSA319 A319112 3930323EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19705UW 929 PIT - S4 - MAJOR REPAIR - LEVEL 2 CORROSION ON FLOORBEAM AT FR20, S23R, -Y254. REPAIRED FLOORBEAM AT FR20, S23R, -Y254 IAW A319 SRM 53-00-14. 2L72 4F RTA28NM 20100202 NM 2010 2 2 USAA2010012790216120100123A5340 MOUNT FITTING EMB ERJ190ERJ190100IGW3260408NM CARGO BAY CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19949UW 19000102 PHL - MAJOR REPAIR - CRACK AT BASE OF AFT CARGO DOOR FITTING AFT MOUNT HOLES. REPLACED AFT CARGO DOOR AFT MOUNT FITTING IAW E190 AMM 53-23-29. 2L72 4F RTA57NM 20100202 NE 2010 2 2 USAA20100128BA004220100126A726152G388 SEAL AIRBUS330 A330323 3940030EU PWA 4168 PW4168A NE ENGINE ODOR A USAAO OTHER B SMOKE/FUMES/ODORS/SPARKS DEDESCENT 1 EA19275AY 0370 SJU FLT 1071 EN ROUTE PHL TO SJU. ON DESCENT THROUGH 9000 FT, DETECTED VERY STRONG ODOR THROUGHOUT CABIN AND COCKPIT. ODOR SIMILAR TO TURBINE OIL. PASSENGERS AND FLIGHT ATTENDANTS COMPLAINED OF ODOR. ODOR WENT AWAY AT 2000 FT. MAINTENANCE REPLACED THE NUMBER TWO ENGINE. THE 1.5 BEARING SEAL WAS DISCREPANT. 2L72 4F4 FRTA46NM 20100202 NM 2010 2 2 USAA2010012690188120100122A5755654645262A ATTACH FITTING BOEING737 737401 138449BNM SPOILER BROKEN A USAAK NONE O OTHER ININSP/MAINT 1 EA19404US164646354 23886 CLT - C6 - MAJOR REPAIR - NR 4 GROUND SPOILER BOARD ATTACH FITTING AT OUTBOARD ACTUATOR IS BROKEN AS VIEWED FROM UPPER SURFACE OF LEFT WING. REPLACED NR 4 GROUND SPOILER IAW JOB CARD 03C30057003/040. 2L72 4F RTA16WE 20100202 EU 2010 2 2 USAA2010012990218120100111A5522D5528000100500 SKIN PANEL AIRBUS320 A320232 3930326EU ELEVATOR SATURATED A USAAK NONE O OTHER ININSP/MAINT 1 EA19652AW 953 SAL - S5 - MAJOR REPAIR - TRAPPED WATER IN RIGHT ELEVATOR SKIN PANEL UPPER SURFACE & HONEY COMB CORE BETWEEN ELEV STA 131 TO ELEV STA 466. REPAIRED RIGHT ELEVATOR UPPER SKIN PANEL IAW A320 SRM 51-77-13 & 55-21-11. 2L72 4F RTA28NM 20100202 NM 2010 2 2 USAA2010012990224120100116A53116546548 FRAME BOEING737 7374B7 138449CNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19452UW 24979 CLT - Q1 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 747 BETWEEN S8L TO S9L. REPAIRED FUSELAGE FRAME AT BS 747 BETWEEN S8L TO S9L IAW TYPICAL REPAIR 53-10-20E. 2L72 4F RTA16WE 20100202 NM 2010 2 2 USAA2010012990227120100116A531165C32395 FRAME BOEING737 7374B7 138449CNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19452UW 24979 CLT - Q1 - MAJOR REPAIR - CRACK ON FUSELAGE FRAME AT BS 727F BETWEEN S8L TO S9L. REPAIRED FUSELAGE FRAME AT BS 727F BETWEEN S8L TO S9L IAW TYPICAL REPAIR 53-10-20E. 2L72 4F RTA16WE 20100202 NM 2010 2 2 USAA2010012990228120100126A5320 ATTACH ANGLE BOEING737 7374B7 138449CNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19452UW 24979 CLT - Q1 - MAJOR REPAIR - CRACK ON VERTICAL BEAM ATTACH ANGLE WEB AT BS 188, RBL 24. REPAIRED VERTICAL BEAM ATTACH ANGLE WEB AT BS 188, RBL 24 IAW B737 SRM 53-10-08 REPAIR 12. 2L72 4F RTA16WE 20100202 NM 2010 2 2 USAA2010012790201120100116A5320140N250532 FITTING BOEING757 7572G7 1384963NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - CRACK IN CLIP BETWEEN BS 860 TO BS 880, WL 208, BL 0. REPLACED CLIP BETWEEN BS 860 TO BS 880, WL 208, BL 0 IAW B757 SRM 51-40-02 & BOEING DRAWING 140N2505. 2L72 4F RTA2NM 20100202 EU 2010 2 2 USAA2010012590174120100124A5210FE240004 BOTTLE AIRBUS320 A320232 3930326EU L1 DOOR LOW PRESSURE A USAAK NONE O OTHER ININSP/MAINT 1 EA19665AW3060930609 1644 FLT 614 - ATL - EES - L-1 DOOR ASSIST BOTTLE REQUIRES SERVICE. MAINTENANCE SERVICED L-1 DOOR ASSIST BOTTLE. 2L72 4F RTA28NM 20100202 NM 2010 2 2 USAA2010012790212120100112A5320146N876948 STIFFENER BOEING757 7572G7 1384963NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON STIFFENER AT BS 1655, S17R, WL 208. REPLACED STIFFENER AT BS 1655, S17R, WL 208 IAW B757 SRM 51-40-02. 2L72 4F RTA2NM 20100202 NM 2010 2 2 USAA2010012790213120100112A5320146N876948 STIFFENER BOEING757 7572G7 1384963NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON STIFFENER AT BS 1670, S17R, WL 207. REPLACED STIFFENER AT BS 1670, S17R, WL 207 IAW B757 SRM 51-40-02. 2L72 4F RTA2NM 20100202 NM 2010 2 2 USAA2010012990229120100126A531165C22908 FRAME BOEING737 7374B7 138449CNM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19452UW 24979 CLT - Q1 - MAJOR REPAIR - CRACK IN FUSELAGE FRAME AT BS 500B, S20L. REPAIRED FUSELAGE FRAME AT BS 500B, S20L IAW B737 SRM 53-00-07 REPAIR 13. 2L72 4F RTA16WE 20100202 EU 2010 2 2 USAA2010012790196120100115A5315D53472195200 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19652AW 953 SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 TO FR70, -Y465. REPLACED FLOORBEAM BETWEEN FR67 TO FR70, -Y465 IAW A320 SRM 51-72-11& AIRBUS DRAWING D53472000. 2L72 4F RTA28NM 20100202 EU 2010 2 2 USAA2010012790197120100115A5315D53472173201 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19652AW 953 SAL - S5 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y160. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y160 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000. 2L72 4F RTA28NM 20100202 EU 2010 2 2 USAA2010012790198120100115A5315D5347218820800 FLOORBEAM AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19652AW 953 SAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 + 15 INCHES TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR67 + 15 INCHES TO FR69, Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000. 2L72 4F RTA28NM 20100202 EU 2010 2 2 USAA2010012790199120100119A5320D53470492002 WEB AIRBUS320 A320232 3930326EU FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19652AW 953 SAL - S5 - MAJOR REPAIR - CORROSION ON WEB BETWEEN FR58 TO FR59, S38L. REPLACED WEB BETWEEN FR58 TO FR59, S38L IAW A320 SRM 51-72-11. 2L72 4F RTA28NM 20100202 NM 2010 2 2 USAA2010012790204120100116A5320143N52601 ANGLE BOEING757 7572G7 1384963NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - CRACKS IN ANGLE BETWEEN BS 540 TO BS 560, WL 208, BL 0. REPLACED ANGLE BETWEEN BS 540 TO BS 560, WL 208, BL 0 IAW B757 SRM 51-40-02. 2L72 4F RTA2NM 20100202 NM 2010 2 2 USAA2010012790205120100116A5320143N52601 ANGLE BOEING757 7572G7 1384963NM FUSELAGE CRACKED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - NR # 6167458 - CRACK IN ANGLE BETWEEN BS780 TO BS800, WL208, BL0. REPLACED ANGLE BETWEEN BS780 TO BS800, WL208, BL0 IAW B757 SRM 51-40-02. 2L72 4F RTA2NM 20100202 NM 2010 2 2 USAA2010012790206120100119A5320146N524020 ANGLE BOEING757 7572G7 1384963NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON ANGLE AT BS 1716, WL 207, LBL 14. REPLACED ANGLE AT BS 1716, WL 207, LBL 14 IAW B757 SRM 51-40-02 & BOEING DRAWING 146N5240. 2L72 4F RTA2NM 20100202 NM 2010 2 2 USAA2010012790207120100118A5310146N83261 CREASE BEAM BOEING757 7572G7 1384963NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CREASE BEAM INNER CHORD AT BS 1343, WL 208, LBL 61. REPLACED CHORD AT BS 1343, WL 208, LBL 61 IAW B757 SRM 51-40-02. 2L72 4F RTA2NM 20100202 NM 2010 2 2 USAA2010012790208120100111A5320146N53183 PLATE BOEING757 7572G7 1384963NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON DECK PLATE AT BS 1716, WL 208 BETWEEN BL 0 TO LBL 14. REPAIRED DECK PLATE AT BS 1716, WL 208 BETWEEN BL 0 TO LBL 14 IAW B757 SRM 53-60-51. 2L72 4F RTA2NM 20100202 NM 2010 2 2 USAA2010012790209120100112A5320146N876947 CHANNEL BOEING757 7572G7 1384963NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CHANNEL AT BS 1670, S17L, WL 207. REPLACED CHANNEL AT BS 1670, S17L, WL 207 IAW B757 SRM 51-40-02. 2L72 4F RTA2NM 20100202 NM 2010 2 2 USAA2010012790210120100112A5320146N876947 CHANNEL BOEING757 7572G7 1384963NM FUSELAGE CORRODED A USAAK NONE O OTHER ININSP/MAINT 1 EA19909AW 24522 MCN - C4 - MAJOR REPAIR - LEVEL 2 EXFOLIATION CORROSION ON CLIP CHANNEL AT BS 1655, S17L, WL 207. REPLACED CLIP CHANNEL AT BS 1655, S17L, WL 207 IAW B757 SRM 51-40-02. 2L72 4F RTA2NM 20100202 CE 2010 2 2 TIMA201000002 120100114A711050910275691 COWLING BEECH 99 99 1154002CE ENGINE OPEN E TIMAA UNSCHED LANDING E VIBRATION/BUFFET TOTAKEOFF 1 NM0724BH 3051876 U67 COWL OPENED AFTER TAKEOFF. PILOT STATED THAT HE LATCHED THE COWL, BUT THERE IS NO WAY TO VISUALLY CONFIRM THAT THE LATCHES WERE CONNECTED. COWL WAS SUBSTANTIALLY DAMAGED BY BUFFETING. 1L72 3T A14CE 20100202 EA 2010 2 2 SWIA201023530 120100111A5312 BULKHEAD CNDAIRCL600 CL6002B19 1900309EA FUSELAGE CRACKED A SWIAK NONE O OTHER ININSP/MAINT 1 NM06443SW 7638 FS 621 AFT BULKHEAD CRACKED AT CARGO DOOR ROLLER GUIDE TRACK. (C CHECK) REPAIRED PER REO. 2L72 4F RTA21EA 20100202 SO 2010 2 2 SWIA201023531 120100120A7712 SIGNAL COND UNIT EMB 120 EMB120ER 3260203SO RT ENGINE FAILED A SWIAC ABORTED TAKEOFF S AFFECT SYSTEMS TOTAKEOFF 1 NM06579SW 120347 RIGHT TORQUE GAUGE FLUCTUATED ON TAKEOFF CAUSING AN AUTO FEATHER. (FLT 6549) REPLACED RIGHT TORQUE SIGNAL CONDITIONER AND RIGHT TORQUE SENSOR. 2L72 4T RTA31SO 20100202 CE 2010 2 2 2010F00010 120100122A2841 INDICATOR CESSNA560 560XL 2076702CE FUEL QTY MALFUNCTIONED E DXTAA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 GL07627QS 5605227 AFTER TAKE OFF (L) FUEL GUAGE ANNUNCIATOR ILLUMINATED. FUEL LOAD INITIALLY SHOWED 1000 LBS HIGH, THEN STABILIZED SHOWING 1000 LBS LOW AND REMAINED THERE. 2L72 4F RTA22CE 20100202 EU 2010 2 2 JBZA38RXTB11910 120100118A2612 FIRE DETECTOR UROCOPEC135 EC135P2 5620027EU ZONE 400 FALSE ACTIVATIONE JBZAA UNSCHED LANDING N FALSE WARNING CLCLIMB 1 WP2738RX 711 0749 SHORTLY AFTER TAKEOFF, EXPERIENCED AN ENGINE FIRE WARNING BELL WITH NO CAUTION LIGHT, WARNING LIGHT OR OTHER SECONDARY INDICATIONS. MADE THE DECISION TO ABORT FLIGHT AND PERFORM A PRECAUTIONARY LANDING BACK AT DEPARTURE. LANDED WITHOUT INCIDENT. NO INDICATION OF ACTUAL FIRE. SUSPECT FAULTY FIRE DETECTION SYS. TROUBLESHOOTING INDICATED A FAULTY TEST ON THE NR 2 SYS. FIRE WARNING LIGHT WOULD ILLUMINATE BUT THE AUDIO WAS ABSENT. REPLACED FAULTY INBD RT ENGINE COMPARTMENT FIRE DETECTOR. 1G72 3U H88EU 20100202 GL 2010 2 2 I06B2010 01 18 JF220100118A7200 ENGINE EMB 135 EMB135ER 3260203SO ALLSN AE3007AE3007A 03030GL CONTAMINATED I I06BA UNSCHED LANDING J WARNING INDICATION CLCLIMB 1 WP25325JF 145499 311965966 AFTER TAKEOFF AT APPROX 400 FT, PILOTS RECEIVED "LAV SMOKE" EICAS INDICATION. DECLARED EMERGENCY & RETURNED FOR LANDING AT DEPARTURE. ACFT GROUNDED UNTIL MX DETERMINES ROOT CAUSE. F/A INVESTIGATED ACFT LAV - OBSERVING NO FUMES OR SMOKE. ONCE ON THE GROUND FIRE DEPARTMENT COMPLETED EXTERNAL INSPECTION " NO INDICATION OF SMOKE OR FUMES". AFTER ALL PASSENGERS DEPLANED, FIRE DEPARTMENT BOARD TO INVESTIGATE LAV "NO INDICATION OF SMOKE OR FUMES". ACFT WAS TAKEN OUT OF SERVICE FOR MX EVALUATION. RESIDUAL ENG CLEANER IN BLEED AIR SYS & ASSOCIATED COMPONENTS. MX CONDUCTED ENG CORE WASHES DURING WEEKEND. 2L72 4F4 FRTT00011ATTE6CH 20100202 CE 2010 2 2 DXTA2010F00013 120100122A3080 WARNING LIGHT CESSNA560 560XL 2076702CE TAIL DE ICE ILLUMINATED E DXTAA UNSCHED LANDING J WARNING INDICATION CRCRUISE 1 GL07602QS 5605518 ENROUTE, LT TAIL DEICE FAIL LIGHT ILLUMINATED. SELECTED OFF THEN MANUAL IAW THE ABNORMAL CHECKLIST WITH NO CHANGE . ACFT WAS AT FLT 270 DURING FAILURE. 2L72 4F RTA22CE 20100202 SO 2010 2 2 SWIA201023519 120100116A5210 DOOR EMB 120 EMB120ER 3260203SO CABIN DOOR LACK OF LUBE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06295SW 120322 MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. (FLT 6840) LUBED MAIN CABIN DOOR. 2L72 4T RTA31SO 20100202 SO 2010 2 2 SWIA201023525 120100120A5210 PIVOT EMB 120 EMB120ER 3260203SO CABIN DOOR LACK OF LUBE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06295SW 120322 MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 6237) LUBED OUTSIDE HANDLE AT SHAFT PIVOT POINT. 2L72 4T RTA31SO 20100202 SO 2010 2 2 SWIA201023549 120100118A5210 HANDLE EMB 120 EMB120ER 3260203SO CABIN DOOR LACK OF LUBE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06296SW 120325 MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. (FLT 6817) LUBED MAIN CABIN DOOR HANDLE. 2L72 4T RTA31SO 20100202 SO 2010 2 2 SWIA201023550 120100120A5210 MECHANISM EMB 120 EMB120ER 3260203SO CABIN DOOR LACK OF LUBE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06270YV 120270 MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 7735) LUBED DOOR LATCHING MECHANISM. 2L72 4T RTA31SO 20100202 EA 2010 2 2 SWIA201023551 120100125A3350 LIGHT CNDAIRCL600 CL6002C10 1390015EA CABIN INOPERATIVE A SWIAK NONE O OTHER UKUNKNOWN 1 NM06701SK 10133 EMERGENCY EXIT LIGHT AT SERVICE DOOR INOP. (FLT 6701)