N413UA

Part: SDAC — FAULTY (1WV1) · airframe 92,414 hrs · 35,791 cycles

DC ESS BUS SHED DISPLAYED ON UPPER ECAM SCREEN. - EL EC DC ESS BUS SHEDLOW SPEED REJECTREPEAT GRIPE PER TSM TASK 31-55-34-400-001-A, REPLACED NO. 1 SDAC, REF MM24-60-00-810-801-A, GROUND CHECK NORMAL.

Part: CHANNEL — DAMAGED (AFT LH DOOR) · airframe 92,376 hrs · 35,764 cycles

AFT L/H PASS DOOR LOWER INNER LIP DAMAGED/BENT. REPAIRED CHANNEL AT LOWER AREA AFT PASSENGER DOOR IAW A-320 SRM 52-10-00-300-002. EMP: V936039 WC: 76763 STA: ST ENG BFM

Part: PROFILE — CRACKED (LH EMER EXIT) · airframe 92,376 hrs · 35,764 cycles

LH FWD EMERGENCY EXIT HATCH LH LOAD TRANSMITTING PROFIL CRACKED. DOT NO. 17-04 () REMOVED AND REPLACEMENT ANGLE AT LH FWD EMERGENCY EXIT HATCH AND MOBILE AT BFM ON NR#: 77106 APPLIED TOP COAT ON REPAIR PART I.A.W. SRM 51-42--11/001. DRAWI NG D52279020 AND SRM 51-75-12 AND SRM 551-72-11-911 ATTACHED FOR M 44-0008 EMP#: V937309 WORK ACCOMPLISHED AT ST ENGINEERING OF

Part: PROFILE — CRACKED (RH EMER EXIT) · airframe 92,376 hrs · 35,764 cycles

RH FWD EMERGENCY EXIT HATCH LH LOAD TRANSMITTING PROFIL CRACKED. DOT NO. 17-08 () REMOVED AND REPLACEMENT ANGEL AT RH FWD EMERGENCY EXIT HATCH AND MOBILE AT BFM ON NR#: 77110 APPLIED TOP COAT ON REPAIR PART I.A.W. SRM 51-42-11/001, DRAWIN G D52279020 AND SRM 51-75-12 AND SRM 51-72-11-911 ATTACHED FORM 44-0008

Part: PROFILE — CRACKED (EMER EXIT HATCH) · airframe 92,376 hrs · 35,764 cycles

RH FWD EMERGENCY EXIT HATCH RH LOAD TRANSMITTING PROFIL CRACKED. REMOVED AND REPLACED R/H FWD EMERGENCY EXIT HATCH R/H LOAD TRANSMITTING PROFIL IAW SRM 51-42-11 AND 51-72-11. EMP: V934860 WC: 7 7109 STA: ST ENG BFM

Part: PROFILE — CRACKED (EMER EXIT HATCH) · airframe 92,376 hrs · 35,764 cycles

LH FWD EMERGENCY EXIT HATCH RH LOAD TRANSMITTING PROFIL CRACKED. REMOVED AND REPLACED L/H FWD EMERGENCY EXIT HATCH R/H LOAD TRANS MITTING PROFIL IAW SRM 51-42-11 AND 51-72-11.

Part: PROFILE — CRACKED (EMER EXT HATCH) · airframe 92,376 hrs · 35,764 cycles

LH AFT EMERGENCY EXIT HATCH LH LOAD TRANSMITTING PROFIL CRACKED. PERFORMED ON NON ROUTINE 77102 COPY ATTACHED.

Part: PROFILE — CRACKED (EMER EXIT HATCH) · airframe 92,376 hrs · 35,764 cycles

RH AFT EMERGENCY EXIT HATCH RH LOAD TRANSMITTING PROFIL CRACKED. DOT NO. 17-05 () REPLACED PROFILE RH AFT EMERGENCY EXIT HATCH RH IAW SRM 51-72-11 ENGINEERING OF MOBILE AT BFM ON NR#: 77107 AND INSTALLED IAW SRM 51-42-11, P/N D5227902620551 BATCH 000406 1454, RESTORED TOP COAT INSIDE AREA IAW SRM 51-75-12, RESTORED T PS IAW SRM 51-23-12

Part: PROFILE — CRACKED (EMER EXT HATCH) · airframe 92,376 hrs · 35,764 cycles

RH AFT EMERGENCY EXIT HATCH LH LOAD TRANSMITTING PROFIL CRACKED. DOT NO. 17-06 () REPLACED PROFILE RH AFT EMERGENCY EXIT, HATCH LH IAW SRM 51-72-1 ENGINEERING OF MOBILE AT BFM ON NR#: 77108 1 AND INSTALLED IAW SRM 51-42-11, P/N D5227902620451 BATCH 00040 60882, RESTORED TOP COAT INSIDE AREA IAW SRM 51-75-12, RESTORED TPS IAW SRM 51-23-12

Part: PROFILE — CRACKED (EMER EXIT HATCH) · airframe 92,376 hrs · 35,764 cycles

LH AFT EMERGENCY EXIT HATCH LH LOAD TRANSMITTING PROFIL IS CRACKED. DOT NO. 17-01 () REPLACED PROFILE LH AFT EMERGENCY EXIT HATCH LH IAW SRM 51-72-11 T ENGINEERING OF MOBILE AT BFM ON NR#: 77102 AND INSTALLED IAW SRM 51-42-11 P/N D5227902620451 BATCH 0004060 882, RESTORED TOP COAT IAW SRM 51-75-12, RESTORED TPS IAW SRM 51 -23-12 ATTACH FORM 44-0008 EMP#: V936636 WORK ACCOMPLISHED AT S

Part: PROFILE — CRACKED (EMER EXIT HATCH) · airframe 92,376 hrs · 35,764 cycles

LH AFT EMERGENCY EXIT HATCH RH LOAD TRANSMITTING PROFIL CRACKED. DOT NO. 17-02. () REPLACED PROFILE LH AFT EMERGENCY EXIT HATCH RH IAW SRM 51-72-11 RING OF MOBILE AT BFM ON NR#: 77103 AND INSTALLED IAW SRM 51-42-11, P/N D5227902620551 BATCH 0004181 298, RESTORED TOP COAT INSIDE AREA IAW SRM 51-75-12, RESTORED TP S IAW SRM 51-23-12.

Part: PIN — UNKNOWN (NLG) · airframe 92,134 hrs · 35,638 cycles

NOSE GEAR WOULD NOT RETRACT REPORTED BY FLIGHT CREW , AIR RETURN. UPON PARKING AT GATE 17 IN EWR DISCOVERED N/L/G PIN INSTALLED. FLAG WAS FULL OF GREASE. REMOVED N/L/G PIN, CLEANED FLAG, STOWED PIN AND ENSURED ALL GEAR PINS WERE REMOVED AND STOWED IN FLIGHT DECK POUCH.

Part: FUEL CAP — MISSING (RT WING) · airframe 91,953 hrs · 35,547 cycles

BTV OPS REPORTED FUEL CAP IS MISSING. PERFORM CHECK OF COUPLING. STATION UNABLE TO LOCATE CAP. CDL 28A APPLIED. NO DAMAGE TO THE AREA ADJACENT TO THE REFUELING CAP AND FUEL CAP’S SHROUD. REFUEL CAP IS MISSING, VERIFY COUPLING SEAL INTEGRITY (NO FUEL LEAKING FROM COUPLING). APPLIED CDL 28A , INOP STICKER INSTALLED ADJACENT TO REG NUMBER INFLIGHT DECK. ACFT GOOD FOR SERVICE. INSTALLED NEW FUEL CAP IN REF TO AMM 28-25-41-400-005-A AND IPC 28-25-41-02-B. INITIATED DIP FOR PAINTED LINES IN REF EC/RA 2820-02404.

Part: NONE — NONE (AFT EMER LT BATT) · airframe 90,839 hrs · 35,036 cycles

CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - AFT EMERGENCY LIGHT BATTERY TESTED BAD R&RBAD BATTERY IAW AMM 33-51-00. OPS CHECK GOOD

Part: SWITCH — DEFECTIVE (FO) · airframe 88,433 hrs · 33,850 cycles

F/O PTT SWITCH ONSTICK BROKEN ANDCONSTANTLY TRANSMITS, REPLACED FO'S SIDESTICK PUSH TO TALK SWITCH REF. AMM 27-92-41. DDP REVERSED. OPS CK. GOOD. MEL CLEARED

Part: SPOILER — FAULT MESSAGE (#3 AND #4) · airframe 87,998 hrs · 33,650 cycles

F/CTL GRD SPOILER 3+4 FAULT DISPLAYED ON UPPERECAM ON T/O ROLL. POST FLT REPORT SHOWS ''SEC 1 OR INPUT OF R THROTTLE CONTROL UNIT IF NEEDED, THROTTLE CTRL UNIT M&E IS 31-7611-9-9001 (MFR P/N 8KS2''. SOURCE IS EFCS 1. ONE OTHER PREVIOUS HIT WITH SAME 330400M01). FAILURE ON 01/09. REF LOG PAGE 7783215. REF TSM 27-60-00-810-806-A. REMOVED AND REPLACED SEC 1. REF AMM 27-94-34-400-001-A. OPS CK OK. NO FAULTS DISPLAYED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1132908 SN OFF 1354 COMPUTER, SPOIL OFF 31-2794-9-0001 1354 ON 31-2794-9-0001 0918

Part: FRAME — NONE (FR54A) · airframe 87,312 hrs · 33,367 cycles

GENERATE DIP LOG PAGE PER ECRA 5230-02157 PART 1A 3 TO ACCOMPLIS H A PERMANENT REPAIR ON THE AFT CARGO DOOR FR54A PER PART 3 OF L ATEST REV OF ECRA 5230-02157 ON OR BEFORE APRIL 29, 2022. ACCOMPLISH A PERMANENT REPAIR ON THE AFT CARGO DOOR FR 54A PER P ART 3 OF LATEST REV OF ECRA 5230-02157 ON OR BEFORE APRIL 29, 2022.

Part: FUEL CAP — MISSING · airframe 86,611 hrs · 33,040 cycles

PDA 3 REF LOG PAGE 6546614 FOR MISSING FUEL CAP. AS PER GMM 02-30-95 TABLE 1, ITEM FALLS WITHIN CATEGORY 3. PLACED ON CDL. REPLACED FUELING CAP REF AMM.

Part: WARNING LIGHT — FALSE ACTIVATION (AUTOLAND SYS) · airframe 85,985 hrs · 32,773 cycles

AUTOLAND LIGHT ILLUMINATED DURING ATTEMPTED AUTOLAND. PERFORMED TSM TASK 22-11-00-810-838-A AND AMM 22-96-00-710-001, OPERATIONAL TEST OF AFS; TEST PASSED; ALSO PERFORMED LAND CAT 3 CAPABILITY TEST PER AMM 22-97-00-710-001; TEST PASSED- ACFT REMAINS LAND CAT 3.

Part: ACTUATOR — INOPERATIVE (NR 5 SPOILER) · airframe 85,941 hrs · 32,753 cycles

SPOILER SURFACE 5 LEFT INOP - F-CTL F/CTL SPLR FAULT ECAM UPDATED MAA CODE FIX USING VENDOR MAA SCREEN REF TSM 27-60-00-810-848A , ACCOMPLISH EFCS GROUND SCAN AND 27-60-00-866-002 VERIFY IF SPOILER IS IN THE OPERATING POSITION OUTLINED IN AMM GUTIERREZ, HECTOR (V823118) ACCOMPLISHED TSM 27-60-00-810-848 EFCS GROUND SCAN SHOWED NO FAULTS ON SEC ONLY ON LH SPOILER 5, DEFERRED GROUND SPOILER 5 ACTUATOR REF MEL 2764AG LH SPOILER 5 DEACTIVATED REF AMM 27-64-00-040-001 MAC RELATED WORK ORDER 000000003004465 AND PRTR MAC METER INITIATED FOR WITH VENDOR ID V823118 GUTIERREZ, HECTOR (V823118) ACCOMPLISHED TSM 27-60-00-810-848 EFCS GROUND SCAN SHOWED NO FAULTS ON SEC ONLY ON LH SPOILER 5, DEFERRED GROUND SPOILER 5 ACTUATOR REF MEL 2764AG LH SPOILER 5 DEACTIVATED REF AMM 27-64-00-040-001 DEFERRED DIRECTLY BY TOMC COMPLIED WITH AMM 27-64-00-710-001-A. REACTIVATED #5 SPOILER ACTUATOR AND VERIFIED NORMAL OPERATION. FAULT COULD NOT BE DUPLICATED AT THIS TIME. PER TSM 27-60-00-810-845-A. REMOVED AND REPLACED #2 SEC AS PRECAUTIONARY. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1461673 SN OFF 7835 COMPUTER, SPOIL OFF 31-2794-9-0001 7835 ON 31-2794-9-0001 8523

Part: FUEL CAP — MISSING (FUEL SYSTEM) · airframe 84,260 hrs · 32,019 cycles

REFUEL-DEFUEL COUPLING CAP REPORTED MISSING WITH NO FUEL LEAK NO TED. CAP FOUND MISSING ONPREFLIGHT. NO LEAKS NOTED. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN NEED MAINTENANCE TO ACCOMPLISH CHECK AS REQUIRED PER CDL 28A MAC RELATED WORK ORDER 000000002381396 AND PRTR ACCOMPLISHED CHECK AS REQUIRED AND APPLIED CDL 28A, NO LEAKS NOTED AT THIS TIME. MAC METER INITIATED FOR WITH VENDOR ID ACCOMPLISHED CHECK AS REQUIRED AND APPLIED CDL 28A, NO LEAKS NOTED AT THIS TIME. DISPATCH DESK: 31 NAME:

Part: CONTROLLER — FAULTY (CABIN PRESSURE) · airframe 83,761 hrs · 31,807 cycles

CAB PR SYS 2 FAULTECAM DISPLYED ON POST FLIGHT REPORT , FOUND PRESS CONT. 2 21-31-34 MSG . PERFORMED OPERATIONAL TESTS OF CPC 1&2 . ALL TESTS PASSED AFTER RESET OF CPC 2 . REQUEST DEFFERAL OF CPC2 . PULLED C/B FOR CPC 2 . PLACARDED . MEL 2131B PLEASE CHANGE CABIN PRESSURE CONTROLLER 2 THANKS PER TOMC CONTROLLER , REQUEST US CHANGING CPC 2 CONTROLLER .. REMOVED AND REPLACED CABIN PRESSURIZATION CONTROLLER PER TOMC. REF AMM 21-31-34-400-001-A . PERFORMED OPS TEST OF PRESS. CONTROLLERS 1&2 . BOTH TESTS PASSED . P/N ON - 9022-15702-10 S/N 3412. P/N OFF - 20791-02AB S/N 4488. OK FOR SVC . ADD EMP:U221991 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1346753 SN OFF 4488 CONTROLLER, CAB OFF 31-2130-9-0001 4488 ON 31-2130-9-0001 3412

Part: WINDOW — SCRATCHED (CABIN) · airframe 79,249 hrs · 29,810 cycles

WINDOW AT 37A HAS LARGE SCRATCH. REMOVED AND REPLACED CABIN WINDOW REF AMM 56-21-13.

Part: TARGET — OUT OF ADJUST (EMERGENCY EXITS) · airframe 77,726 hrs · 29,129 cycles

RIGHT OVERWING EXIT SLIDE SHOWING NOT ARMED. ADJUSTED THE SENSOR TARGET ON BOTH FWD AND AFT RT OVERWING EMERGENCY EXITS, IAW AMM 52-71-00-820-009-A.

Part: WIRE HARNESS — DISCONNECTED (L1 DOOR) · airframe 77,609 hrs · 29,078 cycles

AFTER COMPLETION OF DOOR 1R MAINTENANCE, ACP EMERG LIGHT SYS TEST, FAILED. FOUND DOOR 1L SLIDE WIRING HARNESS NOT CONNECTED. CONNECTED HARNESS, ACP EMERG LIGHT SYS TEST, INSPECTION WITNESSED TESTS OK. VERIFIED CIDS EMERGENCY LIGHT TEST OK.

Part: POST — CRACKED (WINDOW) · airframe 77,527 hrs · 29,028 cycles

LEFT SIDE WINDSHIELD SIDE POST UPPER ATTACHMENT INTERIOR AT FR4. FASTENER HOLE IN UPPER FRAME HAS CRACK INDICATION, REF: HOLE #1 OF A320 NTM 53-11-35-991-001-B SHEET 1. ACCOMPLISHED REPAIR AT L/H SIDE WINDSHIELD SIDE POST UPPER ATTACHMENT INTERIOR AT FR4 IAW ECRA 5310-07298. DIP CREATED TO ACCOMPLISH THE INTIAL INSPECTION PER PART2 OF ECR A 5310-07298 ON OR BEFORE THE AIRCRAFT REACHES 87,628 TOTAL AIRCRAFT FLIGHT CYCLES.

Part: DOOR SILL — CORRODED (R2) · airframe 77,527 hrs · 29,028 cycles

AFTER REMOVAL OF R2 DOOR SILL CORROSION WAS FOUND ON FR68 IN DOOR SILL ATTACH AREA. REPAIRED FR68 JUST ABOVE R2 DOOR SILL IAW ECRA 5310-07297 PART 1 STEPS 1-3. DIP CREATED TO ACCOMPLISH THE INITIAL INSPECTION PER PART 2 OF ECRA 5310-07297 ON OR BEFORE THE AIRCRAFT REACHES 39,728 TOTAL AIRCRAFT FLIGHT CYCLES. PERFORM REPEAT INSPECTION EVERY 10,700 AIRCRAFT FLIGHT CYCLES THEREAFTER.

Part: DOOR FRAME — CRACKED (R2 DOORWAY) · airframe 77,527 hrs · 29,028 cycles

RIGHT AFT PAX DOOR CUTOUT DOOR STOP FITTING HOLES FRAME 68. BOTTOM DOOR STOP, LOWER INBD FASTENER HOLE HAS CRACK INDICATION. REPAIRED THE DOOR FRAME IAW SRM 53- 41-12-300-011, AND SRI 53-41-12-205-009.

Part: DOOR SILL — CORRODED (R2 DOOR) · airframe 77,527 hrs · 29,028 cycles

L2 DOOR SILL IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-72-11-911-001. RESTORED SURFACE PROTECTION IAW SRM 51-75-12-001.

Part: FRAME SPLICE — CRACKED (FRM 68) · airframe 77,527 hrs · 29,028 cycles

LEFT FRAME 68 AFT SPLICE CRACKED. REMOVED AND REPLACED FRAME SPLICE IAW SRM 51-72-11-911-001.

Part: SUPPORT — CORRODED (FRAMES 69-70) · airframe 77,527 hrs · 29,028 cycles

RIGHT SHEAR WEB SUPPORT IS CORRODED. REMOVED AND REPLACED THE SUPPORT FRAMES 69 - 70 IAW SRM 51-72-11-911-001, AND SRM 51-44-11-001.

Part: WIRE — BROKEN (EVAC SLIDE) · airframe 77,518 hrs · 29,023 cycles

DOOR 2L SLIDE HAS BROKEN WIRE HANGING FROM BOTTOM. REPLACED DOOR 2L SLIDE PER AMM 25-62-44-400. OPERATIONAL TEST OF THE ESCAPE FACILITIES COMPLETED AND CHECKED GOOD.

Part: BATTERY — FAILED (CABIN) · airframe 76,434 hrs · 28,538 cycles

EMER EXIT LIGHT TEST FAILS AFT LEFT BATTERY. REPLACED BATTERY REF AMM 33-51-38, OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 73,796 hrs · 27,372 cycles

EMERGENCY BATTERY CAPACITY TEST FAILED DUE TO LT BATTERY MSG 33-51-38. REPLACED EEL POWER SUPPLY AT DR1L, 10WL. OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 71,510 hrs · 26,390 cycles

INTERNAL LOADS EMER L, FAULT MSG WHEN PERFORMING EMER LIGHTS TEST. REPLACED POWER SUPPLY & BATTERY FWD LT IAW AMM 33-51-38-000-001. OPERATIONS CHECKED NORMAL.

Part: BATTERY — DISCHARGED (CABIN) · airframe 69,833 hrs · 25,691 cycles

EMERGENCY LIGHTS OPERATIONAL TEST FAILED. REPLACED LT EMER BATTERY LOCATED BY EMER EXIT IAW AMM 33-51-38, TESTED OK.

Part: STRUT — FAULTY (LT MLG) · airframe 67,197 hrs · 24,668 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. CREW REPORTED HEARING THUMP, THEN GEAR RETRACTED. ACFT DOWN LINKED CFDS FAULT MAG LT LG EXT PROXIMITY SENSOR 23 GA & LT LG EXT SENSOR 21GA. REPACKED LT MLG STRUT, PERFORMED ADJUSTMENT TEST, OPERATIONS CHECKED GOOD IAW AMM 32-11-13.

Part: CONTROL UNIT — FAULTED (NLG STEERING) · airframe 67,182 hrs · 24,661 cycles

ON CLIMB OUT, ACFT ENCOUNTERED A NOSE WHEEL SENSOR FAULT, BRAKE STEERING CONTROL UNIT FAULT. FLIGHT CONTINUED, EMERGENCY DECLARED.

Part: VALVE — FAULTY (AC BAY) · airframe 66,471 hrs · 24,378 cycles

COND HOT AIR FAULT. ACFT IS FAULTING TRIM AIR VLV. REPLACE TRIM AIR VLV IAW AMM 21-63-52 FOR R &R OF VLV. VLV PCN IS 644-0100. R & R TRIM AIR VLV IAW AMM, OPERATIONS CHECKED GOOD. MEL CLEARED PLA REMOVED.

Part: PA SYSTEM — INOPERATIVE (CABIN) · airframe 66,241 hrs · 24,283 cycles

FLIGHT ATTENDANT`S PA AT 1L INOPERATIVE.

Part: SCREW — MISSING (FUSELAGE) · airframe 66,160 hrs · 24,250 cycles

SCREW MISSING AT FWD PANEL CORNER RT SIDE OF ACFT IMMEDIATELY AFT OF GEAR WELL JUST BELOW WING. REPLACED MISSING SCREW.

Part: BOLT — LOOSE (HYDRAULIC SYS) · airframe 65,685 hrs · 24,074 cycles

RAMP REPORT AT DEPARTURE LEAK AT LT MAIN GEAR WW DOOR. FOUND DRIP LEAK BRAKE HYD PACKAGE PARTING SURFACE LOCATED ON AFT LT WING SPAR. TIGHTENED MOUNT BOLTS LEAKAGE CEASED.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,631 hrs · 24,055 cycles

ON INITIAL LIGHTNING STRIKE INSPECTION FOUND FOUR STRIKES ALL INDICATING CRACK USING EDDY CURRENT. TWO EACH STRIKES IN RT FWD FUSELAGE RVSM AREA & TWO EACH IN SKIN LAP BELOW DOOR 1R. BLENDED IAW SRM 53-00-11. ACCOMPLISHED HFEC INSPECTION AT BLEND REPAIR AREA IAW SRM 53-00-11, NO CRACK INDICATIONS FOUND.

Part: DAMPER — FAULTY (R1 DOOR) · airframe 65,635 hrs · 24,056 cycles

DOOR 1R DAMPER CYLINDER WILL NOT ALLOW DOOR TO OPEN FULLY & LOCK. R & R DOOR 1R EMERGENCY DAMPER CYLINDER IAW AMM, OPERATIONS CHECKED NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 65,631 hrs · 24,055 cycles

ON INITIAL LIGHTNING STRIKE INSPECTION FOUND FOUR STRIKES ALL INDICATING CRACK USING EDDY CURRENT. TWO EACH STRIKES IN RT FWD FS RVSM AREA & TWO EACH IN SKIN LAP BELOW DOOR 1R. BLENDED IAW SRM. ACP HFEC INSP AT BLEND REPAIR AREA IAW SRM, NO CRACKS INDICATIONS FOUND. AFTER BLENDED, REPAINTED IAW SRM 51-75-12.

Part: ACM — FAULTY (AC BAY) · airframe 65,618 hrs · 24,051 cycles

A-C PACKS NOT ABLE TO KEEP PLANE COOL ON GROUND. PUTTING OUT AMBIENT AIR. R & R LT ACM IAW AMM, OPERATIONS CHECKED NORMAL.

Part: ACM — FAULTY (AC BAY) · airframe 65,618 hrs · 24,051 cycles

A-C PACKS NOT ABLE TO KEEP PLANE COOL ON GROUND. PUTTING OUT AMBIENT AIR GOT TO 88 DEGREES. R & R LT ACM IAW AMM, OPERATIONS CHECKED NORMAL.

Part: SKIN — BENT (L1 DOOR) · airframe 65,400 hrs · 23,966 cycles

L1 DOOR LOWER AFT CORNER SKIN BENT OUTWARD AND ANGLE BROKEN. REMOVED BROKEN ANGLE. AWAITING NEW ANGLE.

Part: SOLENOID VALVE — FAILED (OXYGEN SYS) · airframe 65,271 hrs · 23,913 cycles

LOW PRESSURE OXYGEN INDICATION FAILED TEST IAW 2SVC REQUIREMENT. REMOVED LP O2 SUPPLY SOLENOID VALVE IAW AMM. REPLACEMENT PART DAMAGED AWAITING NEW VALVE. INSTALLED NEW SOLENOID VALVE IAW MM, VALVE TESTS OK.

Part: ACOUSTIC LINER — DAMAGED (NR 2 ENGINE) · airframe 65,252 hrs · 23,906 cycles

NR 2 ENGINE ACOUSTIC LINING ON OTBD FAN SECTION BEHIND BLOCKER DOOR PEELING UP 2 TO 3 FEET. APPROXIMATELY 30 SQUARE INCHES. MEASURED DELAMINATION TO OB "C" DUCT WALL TO BE 24 INCHES LONG AND 2 INCHES WIDE. TO BE WITH IN MT-78-010 LIMITS. TRIMMED OFF LOOSE MATERIAL AND COVERED WITH SPEED TAPE.

Part: BOTTLE — READS LOW (L2 DOOR) · airframe 65,010 hrs · 23,801 cycles

L2 DOOR OPEN ASSIST BOTTLE PRESSURE NOT IN LIMITS, HIGH. SERVICED ASSIST BOTTLE.

Part: BOTTLE — READS LOW (R1 DOOR) · airframe 65,010 hrs · 23,801 cycles

R1 DOOR DOOR ASSIST BOTTLE PRESSURE NOT IN LIMITS, LOW. SERVICED ASSIST BOTTLE.

Part: CONTROL PANEL — FAULTY (FUEL SYSTEM) · airframe 65,010 hrs · 23,801 cycles

FUEL MIGRATING FROM WING TANKS TO CENTER TANK. FOUND CHANNEL 2 OF FQIC INTERMITTENTLY BLANKING ALL X'S. ALSO INCORRECT ECAM DISPLAY WITH ONE CHANNEL FAILURE. BITE CHECKED OK. REPLACED FQIC.

Part: TAT PROBE — FAILED (NR 1) · airframe 64,833 hrs · 23,727 cycles

ADR 1 FAULTED, FLT DIVERTED. REPLACED NR 1 TAT PROBE.

Part: OXYGEN MASK — LEAKING (COCKPIT) · airframe 64,796 hrs · 23,713 cycles

FIRST OFFICER`S OXYGEN HARNESS FAILED TO INFLATE. SWAPPED F/O`S MASK WITH OBSERVERS MASK . CHECKED OK. REPLACED OBSERVERS MASK.

Part: CONTACTOR — FAULTY (DC ESS BUSS) · airframe 64,622 hrs · 23,643 cycles

WITH NO APU POWER OR GROUND POWER. HEN BATTERY'S ARE SWITCHED ON NO OVERHEAD LIGHTS OR VHF RADIO POWER. SUSPECT ESSENTIAL DC BUS NOT POWERED BY HOT BATTERY BUSS WHEN POWERED BY APU IS BEING POWERED BY STATIC INVERTERS. NO LOUD CLUNK BY CONTACTORS IN 120VU PANEL, TASK 24-38-00-8 10-850-A. REPLACED BATTERY LINE CONTACTOR 6PB2, AMM 24-38-55-000 -001-A, 24-38-55-400-001-A. CFDS BCL TEST 24-38-00-10-001-A OK. REPLACED DC ESS BUS CONTACTOR 4PC FOR TROUBLESHOOTING 27551, AMM 24-35-55-00-002-A, 24-35-55-400-002-A. OPS TEST OF DC GENERATION SWITCHING, AMM 24-32-00-710-001-A, OK.

Part: CONTROLLER — INOPERATIVE (AFT CARGO HEAT) · airframe 64,597 hrs · 23,634 cycles

COND AFT CARGO HEAT FAULT AFT CARGO ISOLATION VALVE. REPLACED PER MM 21-43-52.

Part: FASTENER — MISSING (NR 1 NACELLE) · airframe 64,291 hrs · 23,510 cycles

TWO RIVETS MISSING ONE POPPED ALONG UPPER INBOARD OF NR 1 ENGINE TAILCONE. INSTALLED NEW RIVETS PER MT 78-001.

Part: HYDRAULIC LINE — LEAKING (CARGO BAY) · airframe 63,748 hrs · 23,296 cycles

FLUID LEAK - DISCOVERED IN AFT PIT BY BAG LOADER. AFT PIT NESTING SYSTEM WET WITH HYD FLUID DUE TO CRACKED HYD LINE REF SMC6, NESTING SYSTEM OPS NORMAL.

Part: STRUCTURE — DAMAGED (THRUST REVERSER) · airframe 63,646 hrs · 23,256 cycles

NR 2 ENGINE THRUST REVERSER INNER SKIN HAS PREVIOUS REPAIR FALLING OFF AT THE AFT END 3:00 POS. SKIN ALSO HAS SEVERAL AREAS OF SEALANT DETERIORATION AND SMALL HOLES. REPAIRED AREA AND RESEALED ALL AREAS OF DETERIORATION REF 54-30-00 AND MT 78-018.

Part: COMPUTER — WARNING LIGHT (NR 1) · airframe 63,504 hrs · 23,196 cycles

FCTL SEC 1 FAULT ECAM. RESET PER FLT MANUAL, RESTORED. REPLACED SEC NR 1, OPS CHECKED GOOD.

Part: CHECK VALVE — FAULTY (FUEL SYSTEM) · airframe 62,447 hrs · 22,755 cycles

UNWANTED TRANSFER. ACCOMPLISHED MM 28-21-00-720-004-A TEST OF CENTER TANK FUEL PUMP CANISTER CHECK VALVE. LEFT CENTER FUEL PUMP FAILED. NEXT STEP IS PARA 4.A. IN TSM 28-21-810-840-A. REF LOG 1. REPLACED THE CENTER TANK LEFT BOOST PUMP CHECK VALVE, CHECKS NORMAL.

Part: APU — INOPERATIVE · airframe 62,272 hrs · 22,694 cycles

ECAM MESSAGE, APU AUTO SHUTDOWN DISPLAYED ON UPPER ECAM SCREEN. WOULD NOT START. FLAP DID NOT OPEN. TRIED THREE TIMES, CREW ATTEMPTED SECOND START. AFTER EXT POWER WAS APPLIED, FLAP OPENED. OK TO CONTINUE.

Part: SEAT — FAULTED (COCKPIT) · airframe 61,904 hrs · 22,560 cycles

COCKPIT JUMPSEAT WILL NOT SLIDE TO STOWED POSITION. REPAIRED SEAT TO SLIDE AND LOCK. SEAT OPS NORMAL.

Part: SEAL — BROKEN (THRUST REVERSER) · airframe 61,878 hrs · 22,546 cycles

UPPER AFT SECTION OF STAINLESS STEEL REV TO PYLON SEAL BROKEN AND MISSING, 2.5 IN LONG BY 3 IN SECTION OF SEAL AFT END. NUMBER 2 ENGINE INBOARD SIDE. REPLACED SEAL SECTION.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 61,678 hrs · 22,480 cycles

EMERGENCY LIGHT TEST FAILS BOTH FWD AND AFT LEFT BATTERY PACKS. REPLACED BATTERY PACK AND GROUND CHECKED OKAY.

Part: SCREW — LOOSE (SCUFF PLATE) · airframe 60,702 hrs · 22,142 cycles

DOOR 2R HAS LOUD SQUEAL. PRESSURIZED ACFT, FOUND FWD SCREW OF CENTER SCUFF PLATE LOOSE. SECURED SCREW. ALSO FOUND AIR LEAKAGE AT FWD CORNER OF SCUFF PLATE INBOARD TOP SCREW LOOSE, UNABLE TO TIGHTEN. TAPED OVER SCREW. WILL REQUIRE SCUFF PLATE REMOVAL, RESEALING, AND INSTALLATION PER AMM WITHIN 20 DAYS. SQUEAL NOISE SUBSIDED AFTER THE TIGHTENING OF CTR SCREW AND TAPING OVER THE FWD CORNER LOOSE SCREW. REPAIRED DOOR SILL AND FASTENER. PRESSURIZED AC NO LEAKS NOTED.

Part: STRAP — LOOSE (EVAC SLIDE) · airframe 60,441 hrs · 22,055 cycles

DOOR 2R HAS SLIDE PACK STRAPS LOOSE AND STUCK IN DOOR. REPOSITIONED AND ADJUSTED STRAPS. ALL CKS NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 60,151 hrs · 21,944 cycles

DENT IN FUSELAGE SKIN BETWEEN FR9 AND FR10 AT STR 22L. DOUBLER REPAIR INSTALLED PER SRM. RPR REQ'S INSPECTION AT 60000 CYC AFTER REPAIR EMBODIMENT WITH SUBSEQUENT INSP'S TBD PER SRI 53-11-11 PAGE 213-214 TABLE 204. FIRST INSP REQ'D AT PTC 81944.

Part: FILTER — NOISY (CABIN) · airframe 59,567 hrs · 21,731 cycles

LOUD AIR LEAK SOUND IN BACK HALF OF CABIN NOT AROUND GALLEY OR DOORS - ENTIRE FLIGHT. DURING TROUBLESHOOTING CONFIRMED AIR NOISE AND FOUND A AMBER FAN ECAM WARNING ON THE COND. A TEST OF THE TEMP CTL HAD A RECIRC FAN 1 OR SPLY FAILURE MSG. REPLACED FAN 1 RECIRC FILTER. THE FAULT CLEARED AND NO AIR NOISE NOTED.

Part: EXTINGUISHER — LEAKING (AFT CABIN) · airframe 59,259 hrs · 21,604 cycles

WATER FIRE EXTINGUISHER IN AFT CABIN LEAKING. REMOVED AND REPLACED LEAKING WATER FIRE EXTINGUISHER IN AFT CABIN OVERHEAD BIN.

Part: ELECTRICAL BOX — FAULTY (SEAT) · airframe 59,259 hrs · 21,604 cycles

AUDIO INOPERATIVE AT SEAT 26D, 29A. 26E 26F ALSO SEATS 26D 26E AND 26F OK 29, 'A' BAD. TROUBLESHOT. REPLACED SEAT BOX. OPS CHECKED GOOD.

Part: PANEL — DENTED (NACELLE) · airframe 57,189 hrs · 20,806 cycles

PANEL 423BL HAS 2 DENTS IN PYLON SKIN PANEL. TOP DENT IS 4X 2.75D-.0625 DEEP, LOWER DENT IS 4 X 3-. 0125 DEEP. BOTH DENTS WERE WITHIN RATIO FOR CARRY FORWARD TO THE NEXT 'C' CHECK 26SEPT2012 BUT NOT TO EXCEED 04NOV, 2012 (20 MONTH LIMIT OR PTC 25306) PER SRM.

Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 56,838 hrs · 20,667 cycles

DOOR 1L SLIDE WILL NOT ARM. FOUND AFT GIRT FITTING CONTACTING NEW FLOOR PLATE. FILED PLATE AT CONTACT POINT TO ALLOW FOR SMOOTH OPERATION. OPS CHECKS OK. ON ACCOUNT OF DOOR 1L DOOR SLIDE ARMING PROBLEMS, ARMING SAFETY PIN INSTALLED.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 56,834 hrs · 20,665 cycles

EXISTING EXTERNAL SKIN DOUBLER 18 INCHES FWD OF ACCESS DOOR 314AR AND 3" RIGHT OF APU INLET REQUIRES REPLACEMENT PER AGING AIRCRAFT REPAIR SURVEY INSPECTION (JC 410003010). MAJOR REPAIR ACCOMPLISHED: DOUBLER REPAIR ACCOMPLISHED. REPAIR WAS ACCOMPLISHED ON NR D3640Y BY MAE MECH 02969 AND INSP 140.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 56,834 hrs · 20,665 cycles

FUSELAGE EXTERNAL SKIN HAS A GOUGE AND DENT AT STR 21 - 22L, 3 INCHES AFT OF FR 23. MAJOR REPAIR ACCOMPLISHED: -DOUBLER REPAIR WAS ACCOMPLISHED PER SRM, ON NR P2158W BY MAE MECH 46093, AND INSP 30.

Part: MICROPHONE — FAILED (OXYGEN MASK) · airframe 55,808 hrs · 20,199 cycles

MICROPHONE IN F/O O2 MASK INOP ON INTERCOM. REPLACED OXYGEN MASK STOWAGE BOX, OPS OK.

Part: CYLINDER — FAULTY (R1 DOOR) · airframe 55,808 hrs · 20,199 cycles

NR 1 RIGHT EMERGENCY POWER ASSISTANT BOTTLE IS FAULTY. REPLACED NR 1 RT DOOR DAMPER CYLINDER AND SECURED. ALSO WASHER WAS REPLACED AND OPS CHECKED GOOD ON WU J5523D.

Part: BELLCRANK — BROKEN (PAX DOOR) · airframe 55,808 hrs · 20,199 cycles

NR 1 RT PAX ENTRY DOOR - ACTUATING LEVER FOR THE EMERGENCY POWER ASSIST BOTTLE DIAPHRAGM PLUNGER BROKE OFF AT THE ACTUATING LEVER CASTING SUPPORT. REPLACED BELLCRANK ON DOOR.

Part: PANEL — DAMAGED (WING) · airframe 55,449 hrs · 20,078 cycles

VIBRATION NOISE ENCOUNTERED IN FLIGHT. ACP VIBRATION CK AND FOUND PANEL 191DT HAS EROSION DAMAGE ON L/E OF PANEL. ACP QUICK DISPATCH SPEED TAPE REPAIR. A PERMANENT REPAIR MUST BE ACCOMPLISHED WITHIN 300 FLT HOURS. FLT 225-25 CREW REPORTS NO VIB-NOISE FELT IN ALL PHASES OF FLT, CHECKED PANEL 191DT SPD TAPE STILL INTACT. REPAIRED 191DT ON R & R R39124, SMB W-U S4793P. REPAIRED 192DT ON R & R NR R38207 ON SMB W-U K1805.

Part: CONTROL UNIT — FAULTY (SMOKE DETECTION) · airframe 55,549 hrs · 20,112 cycles

SDCU MAINTENANCE STATUS CLASS II MESSAGE DISPLAYED ON LOWER ECAM. SUPPLEMENTAL DATA UPDATE SDCU PREVIOUS FLT LEGS SHOWED INTERMITTANT FAULT MSG "SDCU CHANNEL 1 (10WQ)". REPLACED SCDU UNIT. OP TESTS OKAY.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 55,060 hrs · 19,900 cycles

LT WING OTBD T/E FLAP, AFT FLAP HAS LOOSE SHEET METAL REPAIR ON UPPER SURFACE AFT OF NR 3 SPOILER. AFT INBD CORNER HAS BECOME DISBONDED. WILL REQUIRE METAL BOND REPAIR. STARTNG REPAIR AFTER CONSULTING WITH EG ON ETCHING PRIMER TO BE USED AS MATERIAL LISTED IN SRM DID NOT CROSS. REMOVED DELAMINATED DOUBLER. ORIGINAL DAMAGE IS TOO CLOSE TO L/E OF PANEL TO ACCOMPLISH REPAIR. REMOVED DAMAGED AREAS AND HONEYCOMB FOR EG EVALUATION. CUT OUT (PARTIAL). REPAIRED, PRIMED AND PAINTED FLAP AREA. AWAITING ENGINEERING APPROVAL OF REPAIR. APPROVED EVA COMPL AND RECEIVED.

Part: BYPASS VALVE — FAULTY (MLG DOOR) · airframe 54,993 hrs · 19,869 cycles

LT MLG DOOR WILL NOT CLOSE. WHILE TROUBLE SHOOTING PROBLEM FOUND 2 SHEARED BOLT HEADS ON MLG DOOR BYPASS VALVE. BYPASS VALVE ON AOG, AOG M2464. REPLACED LT MLG DOOR GROUND OPENING BYPASS VALVE. DOOR OPENS AND CLOSES OK.

Part: SLIDE — FAULTY (DOOR 1L) · airframe 53,748 hrs · 19,350 cycles

EMERGENCY LIGHT TEST HAS FAULT EXT LOADS FWD L. INSTALLED TEST SHUNT ON DOOR. VERIFIED SLIDE PACK IS BAD. NEED NEW SLIDE. NEW SLIDE INSTALLED. OP CHKS NORMAL.

Part: ENGINE — MAKING METAL (RIGHT) · airframe 53,423 hrs · 19,184 cycles

NR 2 ENG STALL, FLIGHT DIVERTED. COMPLIED WITH TSM AND CHECKED ALL CHIP DETECTORS. FOUND METAL ON ALL DETECTORS WITH LONG TAILS ON THE MAIN OIL FILTER AND THE MAIN OIL CHIP DETECTORS AND EXHAUST ALL WHITE. REPLACED ENGINE.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 53,216 hrs · 19,084 cycles

AC SKIN PUNCTURED 18 FORWARD OF ACCESS DOOR 314AR & 3 INCHES RIGHT OF APU INLET. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE, LAID OUT RIVET PATTERN AND CUT DOUBLER. REPAIRED DAMAGE WITH DOUBLER.

Part: TRACK — OBSTRUCTED (EVAC SLIDE) · airframe 52,604 hrs · 18,819 cycles

F/A REPORTED DOOR HARD TO ARM ON GROUND. GOOD FOR TAKEOFF DISARMED IN FLT. F/A ABLE TO REARM. PER CREW THIS IS DOOR 2L. REMOVED BOBBY PIN LODGED IN SLIDE TRACK. TESTED DOOR ARMING OPERATION. OPS CHECK OKAY FORCE LOAD ON CONTROL HANDLE WAS 16 LBS WITHIN LIMITS. OBSERVED DOOR OPERATION PRESSURE & OPERATION OF ARMING MECHANISM NORMAL.

Part: BATTERY — FAILED (CABIN) · airframe 51,796 hrs · 18,509 cycles

DURING EMERGENCY LIGHT TEST ON CIDS PANEL, BATTERY FWD LEFT INDICATED FAILURE. REPLACED LT FWD BATTERY, CHKS OKAY.

Part: BYPASS VALVE — DAMAGED (NLG) · airframe 51,786 hrs · 18,504 cycles

LOSS OF HYDRAULICS. RTFL. FOUND FACE PLATE ON NOSE GEAR BYPASS VALVE WITH 3 OF 4 BROKEN BOLT HEADS. FOUND FLUID FLOWING FROM FACE PLATE ON OLD VALVE. REPLACED NOSE GEAR BYPASS VALVE. NEW VALVE OPS CHECKS GOOD-NO LEAKS NOTED.

Part: WIRE — DAMAGED (CABIN) · airframe 49,922 hrs · 17,768 cycles

EMERGENCY LIGHTS INOP ROWS 24, 25, 26. REPAIRED WIRING AT SEATS AND RELAMPED. CHECKS OKAY.

Part: APU — SMOKE · airframe 49,643 hrs · 17,660 cycles

GROUND CREW REPORTED SMOKE FROM APU EXHAUST AREA. FIRE DEPARTMENT RESPONDED. OPENED APU COMPARTMENT. NO OIL ON THE EXTERIOR. APU EXHAUST IS OK. PER FIRE DEPARTMENT NO FIRE AGENT REQUIRED, SMOKE ONLY. CLOSED APU COMPARTMENT. NO OIL IN SITE GLASS. REPLACED APU AS PRECAUTIONARY.

Part: SENSOR — FAILED (A/C BAY) · airframe 48,765 hrs · 17,344 cycles

PRESSURIZATION PROBLEM, RTFL. PACK 2 OVERHEATED AND WOULD NOT RESET FULLY, AND PACK 1 WAS ON DEFFERAL. RTFL, UNABLE TO PRESSURIZE AC. REPLACED ACM DISCHARGE TEMP SENSOR NR 2 PACK, OPS CHECK NORMAL.

Part: CONTROL SERVO — FAILED (NLG STEERING) · airframe 48,325 hrs · 17,177 cycles

PER CREW, AIRCRAFT PULLS TO LEFT AT TAXI SPEED, REQUIRES 2 DEGREES OF TILLER DEFLECTION. SUPPLEMENTAL DATA UPDATE, NOSE WHEEL STEERING CONTROL SERVO FAILING. REPLACED NOSE WHEEL STEERING CONTROL SERVO, TAXI TEST GOOD.

Part: COMPUTER — MALFUNCTIONED (FLT MANAGEMENT) · airframe 47,208 hrs · 16,790 cycles

RTFL WITH A FLIGHT MANAGEMENT COMPUTER FAILURE. *S/D* RESET FMGC 1 AND 2 AND CROSS LOADED, OK- UPDATED FMS DATA UA30801001 17JAN TO 24FEB. OPS CHECKING NORMALLY.

Part: POWER SUPPLY — FAULTY (EMERGENCY LIGHTS) · airframe 46,259 hrs · 16,465 cycles

EMERGENCY LIGHT TEST MESSAGE, INT LOADS EMER L ATA 33-51-38. 10-26-07 FOUND FAULTY POWER SUPPLY. REPLACED LEFT OW POWER SUPPLY.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,027 hrs · 16,372 cycles

THREE SERVICE CABIN EMERGENCY LIGHT TEST FAILED, MESSAGE INT LOADS EMER L.

Part: BATTERY — DISCHARGED (L1 DOOR) · airframe 45,815 hrs · 16,281 cycles

FOUND FWD 1L BATTERY AT FAULT FOR EMERGENCY LIGHTS. FOUND FAULTY BATTERY. REPLACED DOOR 1L LIGHT BATTERY,

Part: A/C PACK — INOPERATIVE (NR 2) · airframe 45,652 hrs · 16,225 cycles

CAPTS EMERGENCY AUTHORITY USED TO OPERATE PACK 1 DUE TO FAILURE OF PACK 2 TO COOL AC. PACK 2 WEAK AIRFLOW AND OUTLET TEMP (REPORTED BY CREW) ACTUAL CAUSE NEVER DETERMINED. ALL TESTS PERFORMED ON BOTH PACKS ON GROUND WERE NORMAL. COULD NOT DUPLICATE ON GROUND. REPORT: PACK 2 UNABLE TO COOL CABIN. COMPRESSOR OUTLET TEMP 115 PACK OUTLET TEMP 15. POST FLIGHT, NO FAULTS. BITE CK NO FAULTS. OP CK BOTH PACKS,TEMP INDICATIONS SAME ON GRND . VISUAL INSP CK OK.

Part: FUEL FEED — INOPERATIVE · airframe 45,446 hrs · 16,141 cycles

AUTO FUEL FEED SYSTEM INOPERATIVE. FAULTY LOW LEVEL FUEL SENSORS IN RT WING TANK CAUSING LOGIC FAULT IN FQIC. REPLACED TWO LOW LEVEL SENSORS IN RT WING TANK.

Part: HORN — INTERMITTENT (EVAC) · airframe 44,951 hrs · 15,961 cycles

EVAC HORN INTERMITTENTLY SOUNDING WHILE ACFT AT GATE. NO JOY WITH RESET BUTTON ON F/A PANEL'S. PERFORMED SEVERAL RESETS OF THE SYSTEM AND PUT A/C BACK INTO SERVICE. THERE HAVE BEEN NO REPEATS OF THIS PARTICULAR ISSUE SINCE THE ORIGINAL.

Part: BATTERY — FAULTY (AFT LEFT) · airframe 43,576 hrs · 15,462 cycles

LEFT AFT BATTERY FAULTED DURING NR 3 SERVICE EMERGENCY LIGHT CHECK. REPLACED BATTERY.

Part: FAN — FAULTED (E/E BAY) · airframe 42,392 hrs · 15,040 cycles

FLIGHT DIVERTED DUE TO AN AVIONICS COOLING FAN FAULT. REPLACED AVIONICS EQUIPMENT VENTILATION COMPUTER. ALL TEST NORMAL WITH NO FAULTS. AVIONICS EQUIPMENT VENTILATION COMPUTER TEST OK. REPLACED FILTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,281 hrs · 14,646 cycles

EMERGENCY ESCAPE PATH MARKING WHITE LIGHT AT ROW 1AB INOP. REPLACED ASSEMBLY, EMERGENCY ESCAPE PATH LIGHT TEST NORMAL.

Part: LIMITER — FAILED (RUDDER) · airframe 37,390 hrs · 13,279 cycles

BOTH RUDDER LIMITERS FAILED. MAINTENANCE FOUND FAULT "AFS: FAC2-RTL ACTR 4CC". ELECTRONIC MODULE OF RUDDER TRAVEL LIMITATION UNIT (RTLU) WAS SUBSEQUENTLY REPLACED. OPERATIONAL CHECK WAS NORMAL.NO FURTHER ANOMALY WAS REPORTED. SUBSEQUENT SHOP FINDING FOUND A SIDE BOARD BURNED. MULTIPLE INTERMITTENT FAILURES WERE FOUND ON THE B-SIDE BOARD OF THE ELECTRONIC MODULE.

Part: DAMPER — LEAKING (NR 1) · airframe 33,481 hrs · 11,979 cycles

GREEN HYDRAULIC SYSTEM FAILURE. QUANTITY ZERO, PRESSURE LOW. *S/D* YAW DAMPER NR 1 SEAL WAS FOUND LEAKING. THE FAULTY YAW DAMPER WAS REPLACED.

Part: BYPASS VALVE — FAILED (NR 2 A/C PACK) · airframe 24,617 hrs · 8,658 cycles

UNABLE TO CONTROL CABIN TEMPERATURE.*S/D* REPLACED NR 2 PACK TURBINE BYPASS VALVE DUE TO FAILURE FAULTED BY CFDS. IN ADDITION REPLACED NUMEROUS LEAKING DUCT SEALS IN RT PACK, NO FURTHER FAILURES REPORTED.

Part: SLIDE — TORN (LOWER TUBE) · airframe 21,005 hrs · 7,432 cycles

SLIDE/RAFT MR25612-032, MANUFACTURERS PART NUMBER D30665-105, SERIAL NUMBER A5824, MANUFACTURE DATE 12/93, DEVELOPED A SEAM TEAR OF OVER 3 FEET IN LENGTH. THE TEAR WAS IN THE LOWER TUBE ON THE MID SPAN CROSSOVER TUBE RIGHT HAND SIDE. THIS TEAR HAPPENED DURING SHOP OVERHAUL PROOF TEST AFTER ABOUT 2.5 MINUTES. *S/D* UNIT IS BEING SENT TO VENDOR FOR EVALUATION AND REPAIR.

Part: TUBE — CHAFED (LT WING) · airframe 17,402 hrs · 6,280 cycles

FUEL FLOW ON LEFT ENGINE 80 LB/HR MORE THAN RIGHT. FUEL WENT OUT OF BALANCE ON 3 SEPARATE OCCASIONS, WITH THE WORST BEING 900 LBS, IE LEFT SIDE LOW. FUEL BURN WAS 1500 LBS, MORE THAN PLANNED. *S/D* FUEL LEAK FROM LINE TO ACOC AIR MODULATING VALVE. CLAMPS HAD CHAFED THRU FUEL LINE. TWO FUEL TUBES (P/N: 5R8128 AND 5R8129) REPLACED. INVESTIGATION REVEALED THIS FAILURE TO BE AN ISOLATED EVENT. OUR PLAN OF ACTION IS TO CONTINUE TO MONITOR THESE TUBES BY INSTITUTING AN MAINTENANCE PROGRAM INSPECTION REQUIREMENT TO REMOVE CLAMPS AND INSPECT TUBES FOR FRETTING WEAR AND TO REPLACE TUBES AS NECESSARY.

Part: B NUT — CROSS THREAD (OIL PRESS LINE)

FLIGHT DIVERTED TO CUU DUE TO LOSS OF OIL PRESSURE AND OIL QUANTITY IN NR 2 ENGINE. ENGINE NR 2 OIL QUANTITY SHOWS 4.5 QT, FLASHING, ALL OTHER INDICATIONS NORMAL. OIL PRESSURE LINE FITTING WAS FOUND LOOSE AT T-FITTING ABOVE PRESSURE SWITCH, CAUSING OIL LEAKAGE AT CRUISE POWER SETTINGS. B-NUT APPEARED TO BE CROSS THREADED. THE DAMAGED TUBES HAVE BEEN RETURNED TO LUFTHANSA, THE V2500 REPAIR SHOP, FOR QUALITY ASSURANCE INVESTIGATION. NOTIFIED ENGINE REPAIR VENDOR TO ENSURE TUBES ARE PROPERLY INSTALLED AT FUTURE ENGINE SHOP VISITS.

Part: LIGHT — INOPERATIVE (ROW 6, 10 & 15)

EMERGENCY ESCAPE PATH LIGHTS INOP AT SEATS 6C, 10C, AND 15C. *S/D* REPLACED LIGHT ASSY, OPS CK NORMAL.

Part: BATTERY — DISCHARGED (CABIN)

RIGHT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY AND POWER SUPPLY.

Part: COWL DOOR — UNLATCHED (NR 1 ENGINE)

AIRCRAFT RETURNED TO IAD FOR PRECAUTIONARY LANDING DUE TO NUMBER 1 ENGINE FAN PANELS DEPARTING AIRCRAFT AFTER TAKEOFF. *S/D* FAN COWLS WERE NOT CORRECTLY LATCHED FOLLOWING ENGINE MAINTENANCE.

Part: WHEELS — OUT OF BALANCE (NLG)

EXPERIENCED SIGNIFICANT VIBRATION ON TAKEOFF FROM ROTATION UNTIL AFTER LANDING GEAR UP. SUSPECT NOSEWHEEL. *S/D* REPLACED BOTH NOSE WHEELS AND INSPECTED NOSE GEAR. NO FAULTS FOUND.

Part: IDG BOLTS — LOOSE (NR 1 ENGINE)

RETURNED TO ORD UNDER AMBER ALERT WITH NR 1 ENGINE GENERATOR FAILURE. *S/D* IDG DID NOT DISCONNECT. ROOT CAUSE WAS DUE TO IDG SCAVENGE PUMP/GOVERNOR HOUSING BOLTS COMING LOOSE. THIS ALLOWED VIBRATION WHICH BROKE THE WIRE STRANDS TO THE DISCONNECT SOLENOID. ALSO, LOOSE BOLTS CAUSED IDG PUMP GEAR TO DISENGAGE AND IDG TO LOOSE OIL PRESSURE CAUSING HIGH OIL TEMP PROMPTING CREW TO SHUT DOWN THE ENGINE.

Part: SWITCH — FAILED (GREEN HYD SYST)

GREEN HYDRAULIC SYSTEM RESERVOIR INDICATED LOW FOLLOWED BY ECAM ALERT, SYSTEM GREEN PRESSURE LOW. CREW FOLLOWED ECAM PROCEDURES FOR LANDING WITH MANUAL GEAR EXTENSION ACCOMPLISHED. *S/D* FAILED LOW LEVEL SWITCH GENERATED ECAM MESSAGE. CREW PROCEDURE IS TO SHUT OFF HYDRAULIC PUMP. THIS ACTION GENERATED A LOW PRESSURE MESSAGE AND THE NEED TO GRAVITY EXTEND GEAR. SWITCH WAS REPLACED AND OPERATIONALLY CHECKED NORMAL.

Part: EEL — FAILED (CABIN)

EEL LIGHT OUT AT SEAT 2B. REPLACED LIGHT ASSEMBLY AND OPERATIONALLY CHECKED NORMAL.