N326US

Part: PANEL — DETACHED (ZONE 200) · airframe 94,142 hrs · 44,472 cycles

SHIP 3226 DISC: FIRST CLASS LAV O2 PANEL FELL DOWN AND NEEDS TO BE SECURED. C/A: UNABLE TO RESECURE FIRST CLASS LAV O2 MASK PANEL - WILL NOT LATCH CLOSED AFTER RESET.DEFERRED PER A320 MEL 35-21-02.MEL AND PLACARD INSTALLED."M" PROCEDURES C/W.DISPATCH APPROVED. R/R'D FWD LAV OXYGEN CONTAINER PER A320 AMM 35-21 RFID INDUCTION COMPLIED WITH. MEL PLACARD REMOVED NO (M) PROC. OK FOR SERVICE. (LP: 6406816)

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 93,752 hrs · 44,278 cycles

SHIP 3226 DISC: NOSE FWD FUSELAGE / FRAMES / FR20LH AT DOOR STOP NO 7 LEVEL / FASTENER HOLE 5 & 6 / CRACK & WEAR - REPLACEMENT. ER/A 558689- 14AD REV E REQUIRES SECTION VII FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. C/A: ER/A 558689-14AD REV E REQUIRES SECTION VII FOLLOW-ON INSPECTIONS ON OR BEFORE BEFORE 3,800 FC FROM SECTION VI REPAIR EMBODIMENT. THEREAFTER, REPEAT SECTION VII WITHIN EVERY 3,800 FC . ASSOCIATED ER/A 00-558689 ADDED FOR AC 3226. (LP: 0666589)

Part: DOOR — ABNORMAL (L2) · airframe 93,640 hrs · 44,209 cycles

SHIP 3226 DISC: 2L DOOR ARMING JAMMED. C/A: EF A320 AMM 25-62. RE-SECURD DOOR AND OPS CK OF SLIDE ARMING GOOD. OK FOR SVC. (LP: 6374688)

Part: NONE — NONE (NONE) · airframe 92,454 hrs · 43,566 cycles

SHIP 3226 DISC: RH MLG DOOR ACTUATOR RIGID HYD LINE REMOVED F.O.M. C/A: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 009-0001:5340-01075-04B/022 00083 REMOVED HYD LINES AND REINSTALLED AFTER MAINTENANCE COMPLETED. REF. A320 AMM 20-21-12. LEAK CHECKS GOOD. (LP: 0383560)

Part: DOOR FRAME — UNKNOWN (FRM 20) · airframe 92,454 hrs · 43,566 cycles

SHIP 3226 DISC: SECTION VI HAS BEEN ISSUED FOR THE REPAIR OF FR 20 LH AT DOOR STOP LEVEL 7, HOLES #5 AND #6. CURRENT ER/A REVISION IS 'D'. C/A: REPAIR APPROVAL IS LIMITED TO 6 MONTHS FROM SECTION VI (4JUN24). AN ER/A REVISION IS REQUIRED, THAT INCLUDES DTA APPROVAL, FOR CONTINUED SERVICE BEYOND THE 6 MONTH THRESHOLD. ASSOCIATED ER/A 32-558689 ADDED FOR AC 3226. (LP: 0376762)

Part: BOTTLE — LEAKING (R1 DOOR ASSIST) · airframe 92,169 hrs · 43,400 cycles

SHIP 3226 DISC: FOUND R1 DOOR ASSIST BOTTLE LEAKING. C/A: REPLACED THE DIAPHRAGM IN THE PERCUSSION MECHANISM OF THE DOOR DAMPER & EMERGENCY OPERATION CYLINDER OF THE PASSENGER/ CREW DOORS IAW A320 AMM 52-10. OPS TEST GOOD. NO LEAKS NOTED. A/C OK FOR SVC. (LP: 5415046)

Part: LINE — LEAKING (HYD SYSTEM) · airframe 91,740 hrs · 43,160 cycles

SHIP 3226 DISC: SLIGHT ODOR DETECTED ON FLIGHT DECK WHEN APU BLEED IN USE. C/A: T/S PER WC 0550-2002 TO ISOLATE ODOR, FOUND HYDRAULIC ON TAIL OF AIRCRAFT. COMPLETED UP TO STEP 4 OF WC 0550-2002 (EL 146456) FOUND LINE LEAKING FROM YAW DAMP SERVO ACTUATOR(3CC2). RMVD LINE PER A320 AMM 27-26. LINE ENDS CAPPED (AA 717885). C/W W/C 2100- 2005 STEPS 1-11 (AM 897688). INSTALLED HYD LINE PER A320 AMM 27- 26. OPS TEST OK. NO LEAKS NOTED. C/W WORK CARD 2100-2005 STEPS 12-34. (LP: 4205418)

Part: OIL SYSTEM — LEAKING (APU) · airframe 91,700 hrs · 43,141 cycles

THERE IS A DEFINITE MYSTY SMELL IN THE FLIGHT DECK IT WAS NOTICED UPON GETTING IN FLIGHT DECK. C/A: CLEANED AND INSPECTED APU FOUND APU COOLING FAN DUCTS WET WITH OIL. R/R FAN ASSY AND CLEANED DUCTS PER A320 AMM 49-52 DURING LEAK CHECK FOUND OIL SEEPING FROM CASE INSIDE THE PLENUM AND GOING INTO COMPRESSOR. WILL REQUIRE APU CHANGE. MCC NOTIFED. ( 417446) REPLACED APU IAW FORECAST 32-0549-8-0062 CW NO GO ODI PREVENTION ON MD LOG 0197698 ECS DECONTAMINATION CW. (LP: 4885688)

Part: OIL SYSTEM — LEAKING (APU) · airframe 91,666 hrs · 43,120 cycles

SHIP 3226 DISC: BOARDING AIRCRAFT IN DCA NOTICED PONGENT DIRTY SOCK SMELL IN FLIGHT DECK. C/A: C/W WORKCARD 4900-2001 (ISOLATE & REPAIR APU LEAKS) STEP 1-6. STEP 7 CANNOT BE C/W UNTILL ECS DECONTAMINATION W/C 2100-2005 IS COMPLETED. C/W ECS DECONTAMINATION W/C 2100-2005 STEP 1-5 WIP BV 877853. COMPLIED WITH REMAINING STEPS OF W/C 2100-2005 STEPS 6-34, DECONTAMINATION IS COMPLETE. UNABLE TO C/W REMAINING STEPS OF WORK CARD 4900-2001 DUE TO APU DEFERED TO MEL FOR OIL LEAK IDENTIFICATION AND REPAIR AND DEEP CLEAN. (LP: 4885668)

Part: UNKNOWN — ODOR (CABIN) · airframe 91,614 hrs · 43,089 cycles

SHIP 3226 DISC: DIRTY SOCK SMELL DURING AND AFTER APU USE. SMELL REDUCED AFTER APU OFF, BUT INCREASED AGAIN ON DESCENT INTO ATL. C/A: INSPECTED APU COMPARTMENT FOUND OIL IN APU. REQUIRES APU CHANGE AND COMPARTMENT CLEANING(555809) FOUND APU ACCESSORY COOLING FAN LEAKING OIL. REMOVED AND REPLACED COOLING FAN ASSEMBLY PER A320 AMM 49-52 TESTS NORMAL. STILL REQ CLEANING OF APU COMPARTMENT AND ADDITIONAL LEAK CHECK(490975) REMOVED THE DIFFUSER AND ELBOW FROM THE RT APU DOOR - CLEANED IT AT THE WASH RACK. REINSTALLED THE DIFFUSER & ELBOW PER A320 AMM 49-16-45. RAN APU - NOTICED ONE B-NUT LOOSE AND LEAKING. TIGHTENED THAT. RUNNING APU TO GET ALL THE RESIDUAL OIL OUT(235172) C/W W/C'S 0550-2002, 4900-2001, 4916-2001 & 2100-2003. (LP: 4885646)

Part: PIN — MISSING (R2 DOOR SLIDE) · airframe 91,614 hrs · 43,089 cycles

SHIP 3226 DISC: SLIDE DISARMING PIN ATTACHING LANYARD MISSING OR DAMAGED. C/A: LANYARD SECURED AT 2R DOOR IAW PER A320 AMM. (LP: 0160641)

Part: UNKNOWN — MALFUNCTIONED (L2 DOOR ARMING) · airframe 91,614 hrs · 43,089 cycles

SHIP 3226 DISC: DOOR 2L WILL NOT CLOSE/ ARM. C/A: REPINNED ARMING LEVER, CYCLED DOOR , CHECKED GIRT FITTINGS, NO FINDINGS. CLOSED DOOR DOOR OPERATED NORMALLY. (LP: 4359780)

Part: WIRE — UNKNOWN (WATER HEATER) · airframe 91,543 hrs · 43,046 cycles

.SHIP 3226 DISC: WHILE TROUBLESHOOTING ANOTHER ISSUE, A BURNING POPCORN SMEL. C/A: COMPLIED WITH NO GO ODI 2172 WORK CARDS 0550-2002 + 0550-9001 ( WIP 416340). INSP BEHIND CIRCUIT BREAKER PANELS IN CO WITH NO FINDINGS. SEE LOG 4359774 FOR MAINT. SMELL IDENTIFIED VISUALLY AND OLFACTORILY TO 2754VC. OK FOR SVC. END. (LP: 4359775) REPLACED WIRES, WATER JEATER CONTROL UNIT, AND SWITCH (3MP). RESTORED ALL PANELS. OPERATION CHECKS GOOD. AC OK FOR SERVICE. (LP: 4359774)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,538 hrs · 43,041 cycles

SHIP 3226 DISC: BURNING SMELL IN COCKPIT AND FWD GALLEY. C/A: REF LOG 4359774FOR CORRECTIVE ACTION. (LP: 0152074) FOUND WATER OVERFLOW VALVE HANDLE NOT FULL CLOSED. C/B ON OVERHEAD FWD GALLEY WATER ICE PROT CNTL POPPED, NO RESET. FWD CARGO LOADING LIGHT C/B POPPED. WIP 580952. FOUND BURNT WIRES AT CONNECTOR 2754VC IN FWD CARGO CEILING. REPLACED WATER HEATER CONTROL UNIT. AMM 30-73 (WIP 416340) ALSO FOUND CONNECTOR PLUG 2754VC WIRING DAMAGED + BURNT CAUSE SMELL NOTED IN LOG 4359775. CONNECTOR WILL NEED TO BE REPINNED + REPLACED WIP 660318 PERFORMED WIRING INTEGRITY CHECK OF WIRES COMPLETED + FOUND GOOD WIP 660318 REPINNED AND REPLACED 2754VC JACK SIDE PER A320 ESPM 20-48-21. 793722 WIP. INSTALLED 2754VCA CKS OF SYSTEM / CIRCUITS THROUGH DAMAGED PLUG GOOD. POTABLE WATER ICE PROTECT UNIT TEST GOOD. REF ESPM 20-44, AND A320 AMM 30-73. FWD CARGO REQUIRES CLOSE UP WIP (923516) R/R 3MP DUE TO SWITCH STUCK CLOSED PER A320 AMM 38-14. RESTORED ALL PANELS. OK FOR SVC. (LP: 4359774 C/A)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,199 hrs · 42,861 cycles

SHIP 3226 DISC: EMER LIGHT HOUSING DAMAGED AT ROW 33. C/A: INSTALLED NEW EMER LIGHT HOUSING AT ROW 33 OPS CHECK GOOD OK FOR SVC. (LP 4367894)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,154 hrs · 42,842 cycles

SHIP 3226 DISC: FA COULD NOT CLOSE AND ARM 2L DOOR. C/A: REMOVED DEBRIS FROM GIRT BAR MECHANISM AND 2L DOOR CLOSED NML PER A320 AMM 52-13. (LP: 4367870)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 91,154 hrs · 42,842 cycles

SHIP 3226 DISC: 2L DOOR WOULD NOT ARM/CLOSE. C/A: YCLED 2L DOOR CKS SLIDE STRAPS. CK'S GOOD PER AMM 52-12. (LP: 4367852)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,730 hrs · 42,612 cycles

SHIP 3226 RH DOOR FRM 66 FITTING #6 HOLE #1 (UP INBD) IS .25 DIA AND HAS AN BHEC INDICATION WHICH HASN'T GONE AWAY AFTER CLEANING. AA 5311-01216 AD RELATED, REQUIRES ACTION PRIOR TO FLIGHT. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-41-12. (2971729)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,708 hrs · 42,599 cycles

SHIP 3226 BLUE SYSTEM RUDDER SERVO CONTROL FAILED FREEPLAY CHECK PER WORKCARD 2720-7001. CORRECTIVE ACTION: R/R SERVO ENDS AND ADJUSTED. OK FOR SERVICE. (2959900)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,708 hrs · 42,599 cycles

SHIP 3226 GREEN SYSTEM RUDDER SERVO CONTROL FAILED FREEPLAY CHECK PER WORKCARD 2720-7001. CORRECTIVE ACTION: R/R SERVO ENDS AND ADJUSTED. OK FOR SERVICE. (2959898)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,708 hrs · 42,599 cycles

SHIP 3226 YELLOW SYSTEM RUDDER SERVO CONTROL FAILED FREEPLAY CHECK PER WORKCARD 2720-7001. CORRECTIVE ACTION: R/R SERVO END AND ADJUSTED. OK FOR SERVICE. (2959899)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,708 hrs · 42,599 cycles

SHIP 3226 DURING INSPECTION OF THE AFT AIRCRAFT VIBRATION DISCREPANCY, FOUND THE L/H HORIZONTAL STAB HINGE BEARING LOOSE AND CLUNKING. CORRECTIVE ACTION: R/R THS ACTUATOR ARM ATTACH FITTINGS PER A320 AMM 55-16-34-200-002-A. ALSO CHECK THE INTEGRITY OF THE THS ACTUATOR BALL SCREW SHAFT (PRIMARY AND SECONDARY LOAD PATH) PER A320 AMM 27-44-51-280-001- A. (2933690)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,697 hrs · 42,592 cycles

SHIP 3226 AIRFRAME VIBRATIONS STARTING AT FL260 / 320KTS. HAD TO DIVERT. CORRECTIVE ACTION: REPLACED BLUE SYSTEM ELEVATOR SERVOS. (4770660)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,441 hrs · 42,457 cycles

SHIP 3226 - ATB - DUE TO AIRFRAME VIBRATIONS FELT AFTER LEVELING OFF. CORRECTIVE ACTION: FOUND BLUE HYDRAULIC SYSTEM ACCESS DOOR 197FB LOOSE. ADJUSTED DOOR LATCH. OPS CHECK GOOD. (4858070)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 90,358 hrs · 42,407 cycles

AIRCRAFT 3226 - MISC/DE -ON APPROACH INTO MSP, APPROX. 1800' SELECTING GEAR DOWN GOT 3 RED UNSAFE LIGHTS AND NO GEAR. EXECUTED MISSED APPROACH. AT 3000' CYCLED GEAR AND RECEIVED GEAR UNSAFE WARNING ECAM SHOWED LANDING NOT DOWN LOCKED. FOLLOWED ECAM AND CYCLED ONCE AGAIN AND GEAR EXTENDED ONCE AGAIN, GOT 3 GREEN LIGHTS. CORRECTIVE ACTION: FOUND SENSOR 17GA TOUCHING TARGET. REPLACED PROX SENSOR 17GA, MLG LOCKSTAY ACTUATOR ON MLG LH SIDE STAY ASSEMBLY (2505GM), AND LANDING GEAR CONTROL LEVER. (LP 4858015)

Part: NONE — NONE · airframe 88,443 hrs · 41,350 cycles

SHIP 3226 CABIN PRESSURE LIGHT ON L-1 DOOR FLASHING. CORRECTIVE ACTION: PLACED ON MEL 52-70-02. OK FOR CONTINUED SERVICE. (2494416)

Part: NONE — NONE · airframe 88,365 hrs · 41,304 cycles

SHIP 3226 - DIV - TO IAD DUE TO A BRAKES SYS 1 FAULT. CORRECTIVE ACTION: BRAKES SYSTEM 1 PLACED ON MEL 32-42-03A. TROUBLESHOT SYSTEM. BITE TEST OF BCSU 1 WAS GOOD. NO TROUBLE FOUND. NO HISTORY. OK FOR SERVICE. MEL/PLAC REMOVED. (9192090)

Part: NONE — NONE · airframe 87,903 hrs · 41,003 cycles

SHIP 3226 -PRES- EMERGENCY DESCENT DUE TO LOSS OF PACK 2 WITH PACK 1 ALREADY ON MEL. MASKS DID NOT DEPLOY. EMERGENCY DECLARED. CORRECTIVE ACTION: REPLACED RT PACK ANTI-ICE VALVE, RAM AIR INLET ACTUATOR AND MIXER AIR TEMP SENSOR 25HK. LT. PACK OPS CHECKED NORMAL. MEL CLEARED. (9029472)

Part: NONE — NONE · airframe 87,829 hrs · 40,953 cycles

SHIP 3226 -DIV/DE- TO DTW DUE TO GREEN HYDRAULIC SYSTEM LOW QUANTITY. CORRECTIVE ACTION: FOUND PACKING LEAKING FROM ENGINE PUMP PRESSURE SWITCH, R/R PACKING. LEAK CHECK GOOD. OK FOR SERVICE. (9029422)

Part: NONE — NONE · airframe 87,631 hrs · 40,820 cycles

SHIP 3226 PASSENGER CREW DOOR 841 DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: R/R DAMPER PER A320 AMM 52-15. OK FOR SERVICE. (2301462)

Part: NONE — NONE · airframe 87,631 hrs · 40,820 cycles

SHIP 3226 FRAME FOOT 43 LH CRACK INDICATION. CORRECTIVE ACTION: COMPLIED WITH DELTA WORK CARD AMDS 5311-01239-01A. (2300667)

Part: NONE — NONE · airframe 87,631 hrs · 40,820 cycles

SHIP 3226 CORROSION IN FLAP ROTARY ACTUATOR TRACK 2 ON RH WING. CORRECTIVE ACTION: R/R ROTARY ACTUATOR PER DELTA WORKCARD AMDS 2754-4001-RT. (2300645)

Part: CONTROLLER — INOPERATIVE · airframe 87,567 hrs · 40,777 cycles

SHIP 3226 - PRES/DE - DUE TO LOSS OF CPC 1 AND 2 AND EXCESS CABIN ALT MESSAGE. REGAINED CABIN WITH MANUAL CONTROL AT 10K FT. CREW REPORTED THAT MASKS DROPPED AUTOMATICALLY. CORRECTIVE ACTION: REPLACED CABIN PRESSURE CONTROLLER 1 AND 2. ALSO REPLACED OUTFLOW VALVE AND ALL O2 GENERATORS AND MASKS. OPS CHECK GOOD. (8369998)

Part: NONE — NONE · airframe 87,092 hrs · 40,473 cycles

SHIP 3226 NLG R/H MAIN TRUNNION FITTING BEARING MOUNT HOLE ON A/C HAS CORROSION PITTING ON FACE SURFACE TOP AFT SIDE. CORRECTIVE ACTION: COMPLIED WITH ERA 598536-14 SECT. I REV. ORIGINAL. (2187785)

Part: HANDLE — STUCK (L2 DOOR) · airframe 87,055 hrs · 40,458 cycles

SHIP 3226 L2 CABIN DOOR HANDLE IS STUCK. ECAM DOOR PAGES SHOWS DOOR OPEN. CORRECTIVE ACTION: REMOVED DEBRIS FROM DOOR SILL. OPS CK GOOD PER A320 AMM 52-12. OK FOR SVC. (8789404)

Part: NONE — NONE · airframe 86,646 hrs · 40,183 cycles

SHIP 3226 DURING WALK AROUND FOUND CORROSION ON FUSELAGE SKIN AROUND BOTTOM OF LAVATORY FAN EXHAUST. CORRECTIVE ACTION: COMPLIED WITH ERA 596785-14AD REV A. (8476486)

Part: NONE — NONE · airframe 86,645 hrs · 40,182 cycles

SHIP 3226 NEED TO INSPECT REPAIR ER/A 596785-14AD. CORRECTIVE ACTION: COMPLIED WITH INSPECTION. OK TO CONTINUE. (2097699)

Part: NONE — NONE · airframe 85,929 hrs · 39,795 cycles

SHIP 3226 DURING PSU TEST PSU'S DID NOT DROP AT ROWS 12ABC, 21ABC, 26ABC, AND 18 DEF. CORRECTIVE ACTION: REPACKED MASKS, OPS CK GOOD. (7783916)

Part: NONE — NONE · airframe 85,810 hrs · 39,725 cycles

SHIP 3226 AIR ENG 1 BLEED FAULT WHICH CAUSED A DIVERSION. CORRECTIVE ACTION: R/R #1 ENG BLEED PRESSURE REGULATOR VALVE PER A320 AMM 36-11. OP CHECK GOOD AND LEAK CHECK GOOD. PREFORMED VISUAL OF THE SENSE LINE ON ENGINE #1 FOUND NO LOOSE LINE. OK FOR SVC. (5362334)

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 85,460 hrs · 39,470 cycles

SHIP 3226 L1 DOOR EMERGENCY LIGHT COVER MISSING. CORRECTIVE ACTION: REPLACED L1 EMERGENCY LIGHT COVER. OK FOR SERVICE. (7853442)

Part: LATCH — DIRTY (ARMING LEVER) · airframe 85,079 hrs · 39,187 cycles

SHIP 3226 DOOR 1L ARMING LEVER NOT MAKING GOOD INITIAL CONTACT FOR SOLID SLIDE INDICATION ON ECAM AT PRE PUSHBACK. REQUIRES MULTIPLE CYCLING OF ARMING LEVER FOR SOLID INDICATION. CORRECTIVE ACTION: CLEANED DEBRIS FROM LATCHING AREAS IAW A320 AMM 52-12. RE-CHECK. OPS CK GOOD. (7771770)

Part: OXYGEN BOX — INOPERATIVE (RT AFT) · airframe 84,352 hrs · 38,824 cycles

SHIP 3226 RIGHT AFT GALLEY EMERGENCY OXYGEN INOP. CORRECTIVE ACTION: MASK CONTAINER AND DOOR REPLACED PER A320 AMM 35-21. (6691866)

Part: NONE — NONE (NONE) · airframe 92,454 hrs · 43,566 cycles

SHIP 3226 DISC: ER/A 558689-14AD HAS BEEN UPDATED TO REV. 'C' TO INCORPORATE NEW RDAS APPROVAL PER DTE REQUIREMENTS. THE SUBJECT REPAIR IS CLASS IFIED AS CAT. 'B' PERMANENT WITH FOLLOW ON INSPECTION. C/A: ACCOMPLISHED PRI 558689-14AD REV 0, AND 1,2 AND ER/A558689-14AD REV D SECTION V. (LP: 1436644)

Part: BATTERY — DISCHARGED (CABIN) · airframe 83,663 hrs · 38,474 cycles

FOUND EPSU FAULT DURING WORKCARD 3351-2291 TEST, R/R EPSU W/O BATTERY

Part: ANCHOR FITTING — NONE (RT WING) · airframe 83,399 hrs · 38,350 cycles

RT WING ANCHORAGE FITTING REMOVAL REF ER/A 582404-14 REV A PRI REV 3 SEC 2 STEP 4, REMOVED RT MLG ANCHORAGE FITTING, INSPECTED AND REINSTALLED FITTING PER PRI 583025-14 REV O, REV 1, REV 2 AND REV 3, REF ER/A 583025- 14AD REV ORIGINAL ALSO PER PRI 582404-14 REV O, REV 1, REV 2, REV 3, REV 4 AND REV 5, REF ER/A 582404-14AD REV A

Part: ANCHOR FITTING — OUT OF TOLERANCE (RT MLG) · airframe 83,399 hrs · 38,350 cycles

RT MLG ANCHORAGE FITTING HOLE #67 IS OUT OF TOLERANCE. REF PRI 583035-14 REV 1, REPAIRED HOLE #67 IN RT MLG ANCHORAGE FITTING PER PRI 583025-15 REV 3, REF ER/A 583025-14AD REV ORIGINAL

Part: KEEL FITTING — CRACKED · airframe 82,766 hrs · 38,041 cycles

CRACK INDICATION ON HOLES LOC 1,2,3,4 OF FITTING KEEL BEAM ACTUATOR DOOR LH AND RH SIDE IN MLG. PERFORMED PERMANENT REPAIR LOCATED FITTING KEEL BEAM ACTUATOR DOOR LH AND RH SIDE IN MLG ASPER ER/A 580059-14 REV 0, REV 1, REV 2 AND ER/A 580059-14 REV. ORIGINAL SECTION I SEE LOG PAGE 1210465 FOR TIME CONTROLLED ITEMS SECTION DTE ER/A 580059-14 REV. ORIGIANL.

Part: STRINGER — DAMAGED (FRAMES 63-64) · airframe 82,809 hrs · 38,063 cycles

ELONGATED HOLE ON STRINGER 8L AT LEVEL FR63 TO FR64 ON UPPER FUSELAGE, PERFORMED PERMANENT REPAIR ON STRINGER 8L AT LEVEL FR 63 TO FR 64 ON UPPER FUSELAGE ASPER A320 SRM 53-00-13-300-001

Part: FRAME — CRACKED (FRM 20) · airframe 82,744 hrs · 38,030 cycles

FR20 LHS AT THE DOUBLE JOGGLED AREA CRACK IN HOLE #5 AND WEAR IN HOLE #6, REPLACED FRAME 20 LH SIDE AT FWD GALLEY AREA AS PER PRI 558689-14 REV.0; PRI 558689-14 REV. 1 AND SECTION IV ER/A 558689-14AD REV. B

Part: SKIN — CORRODED (FRAMES 41-42) · airframe 82,744 hrs · 38,030 cycles

CORROSION INTERNAL STRUCTURE UPPER EXTERNAL SKIN CENTER TANK FR 41 TO FR 42 AND +Y1732 TO +Y1292 IN PASSENGER CABIN (1 EA), PERFORMED REPAIR INSTRUCTION ON OINTERNAL SKIN STRUCTURE UPPER EXTERNAL SKIN CENTER TANK FR41 TO FR42 AND + Y1732 TO +Y1292 IN PASSENGER CABIN AS PER PRI 579653-14 REV. 0 AND ER/A 579653- 14 REV. ORIGINAL

Part: FRAME — CRACKED (FRM 36) · airframe 82,744 hrs · 38,030 cycles

CRACK INDICATION ON FRAME 36 PRESSURE DECK PANEL AT EIGHTH HOLE FROM Y+1523 TO I/B IN FWD CARGO COMPARTMENT (2 EA), PERFORMED PERMANENT REPAIR ON FRAME 36 PRESSURE DECK AT EIGHTH HOLE FROM +Y1523 TO I/B IN FWD CARGO COMPARTMENT AS PER PRI 579617-14 REV. 0; PRI 579617-14 REV. 1; PRI 579617-14 REV. 2 AND ER/A 579617-14AD REV. ORIGINAL

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOOR BEAM +Y1292 BTW FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM +Y1292 BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG #D53110920 #D53110984 #D53112812

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOOR STRUCTURE LOCATED BTW FR 68 TO FR 69 +Y1162 IN PASSENGER CABIN, REPLACED FLOOR BEAM +Y1162 IN PASSENGER CABIN BTW FR68 TO FR69 AS PER SRM A320 51-72-11 AND DWG D53472000

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOOR BEAM -Y1137.1 BTW FR66 TO FR68 AT AFT GALLEY, REPLACED FLOOR BEAM -Y1137-1 LOCATED BTW FR66 TO FR68 AT AFT GALLEY AREA AS PER A320 SRM 51-72-11 AND DWG D53472800

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOOR BEAM +Y765 BTW FR12 TO FR24 AT FWD GALLEY AREA, REPLACED FLOOR BEAM +Y765 LOC ON FR12 TO FR24 A1 FWD GALLEY AREA ASPER A320 SRM 51-72-11 AND DWG D53112812

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOOR STRUCTURE LOCATED BTW FR 66 TO FR 68 +Y1292 IN PASSENGER CABIN, REPLACED FLOORBEAM +Y1292 LOC BTW FR66 TO FR68 IN PPASSENGER CABIN AS PER SRM 51-72-11 AND DWG # D53472000.

Part: SEAT TRACK — OUT OF LIMITS (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

REPLACE SEAT TRACK -Y765 LOC BTW FR 41 TO FR 47. PREVIOSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE, WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y765 AND FASTENER LOC BTW FR 41 TO FR 47 IN PASSENGER CABIN AS PER SRM 51-72-11 AND 51-42-11 DRAWING # D53371000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOORBEAM -Y1162.5 BTE FR68 TO FR69 AT AFT GALLEY AREA (1 EA), REPLACED FLOORBEAM -Y1162.5 BTW FR68 TO FR69 AT AFT GALLEY AREA AS PER SRM 51-72-11 AND DRAWING # D53472800.

Part: SEAT TRACK — OUT OF LIMITS (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

REPLACE SEAT TRACK -Y765 BTW FR 36 TO FR 41. PREVIOSLY REWORKED AREA AND EVALUATION WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y765 AND FASTENER LOC. BTW FR36 TO FR41 IN PASSENGER CABIN EA AS PER SRM 51-72-11 AND 51-42-11. DRAWING 57130147.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION LOWER SILL LOCATED AT FR 68 IN PASSENGER CABIN (1 EA), REPLACED LOWER SILL LOCATED BTW FR66 TO FR68 PASSENGER LT CABIN AS PER SRM 51-72-11 AND DWG D53480505. RELEASE DATE: 09-APR -19. ISSUE DG AND DWG D53470150 RELEASE DATE: 11-FEB-04. ISSUE: U AND ERA 579677-14 REV. ORIGINAL.

Part: SEAT TRACK — OUT OF LIMITS (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

REPLACE SEAT TRACK -Y1292 LOC BTW FR 36 TO FR 41. PREVIOSLY REWORKED ARE AND EVALUATED WITH CARD 2500-2031-DE, WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y1292 LOC BTW FR36 TO FR41 AND FASTENERS AS PER SRM 51-72-11 AND DWG D57130146.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOOR STRUCTURE LOCATED BTW FR 64 TO FR 66 +Y 1292 IN PASSENGER CABIN (1 EA), REPLACED FLOORBEAM +Y1292 LOCATED BTW FR64 TO FR66 IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG D53472816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOORBEAM -Y1292 BTW FR64 TO FR66 AT AFT GALLEY AREA (1 EA), REPLACED FLOORBEAM -Y1292 LOCATED BTW FR64 TO FR66 AT AFT GALLEY AREA AS PER SRM 51-72-11 AND IPC 53-41-04-10B.

Part: SEAT TRACK — OUT OF LIMITS (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

REPLACE SEAT TRACK +Y765 LOC. BTW FR 36 TO FR 41 PREVIOUSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE,WAS FOUND OUT LIMITS, REPLACED SEAT TRACK +Y765 LOC. BTW FR 36 TO FR 41 IN PASSENGER CABIN 1EA ASPER SRM 51-72-11 AND DWG D57130147.

Part: SEAT TRACK — OUT OF LIMITS (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

REPLACE SEAT TRACK +Y765 LOC BTW FR 41 TO FR 47 PREVIOSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK +Y765 LOC. BTW FR 41 TO FR 47 IN PASSENGER CABIN 1EA ASPER SRM 51-72-11 AND DWG D53371110.

Part: SEAT TRACK — OUT OF LIMITS (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

REPLACE SEAT TRACK Y+1292 LOC BTW FR 41 TO FR 47. PREVIOSLY REWORKED AREA AND EVALUATED WITH CARD 2500-2031-DE. WAS FOUND OUT LIMITS, REPLACED SEAT TRACK +Y1292 LOC FR 41 TO FR 47 ASPER SRM 51-12-11 DW# 053371000.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

ELONGATED HOLE LOWER SILL CENTER FITTING ENTRY DOOR AT AFT GALLEY AREA (10 EA), REPLACED CONTROL FITTING ENTRY DOOR AT AFT GALLEY AREA AS PER SRM 51-72-11 AND DWG D53480505, AND DWG D53480048.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION LOWER SILL LOC. BTW FR66 TO FR68 AT AFT GALLEY AREA ( 1 EA) RT SIDE, REPLACED LOWER SILL LOC BTW FR 66 TO FR68 AT AFT GALLEY AREA RT SIDE ASPER SRM 51-72-11 AND DRAWINGS D534800200 RELEASE DATE 06 OCT 17 AND D53470150 RELEASE DATE 11 FEB 04 JOB COMPLETE ASSOCIATED ER/A 00-579677.

Part: BOLT — BROKEN (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

BROKEN FLOORBEAM -Y1292 BOLT AT LEVEL FR 36 IN PASSENGER CABIN (1EA), REPLACED BOLT ON FLOORBEAM -1292 AT LEVEL FR36 IN PASSENGER CABIN (1EA) AS PER SRM 51-42-11 AND DRAWING # D57130146.

Part: ATTACH BRACKET — CRACKED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

CRACK FLOOR STRUCTURE ACTUATOR ATTACH BRACKET AT FR 54 BTW -Y765 TO -Y1292 IN PASSENGER CABIN (1 EA), REPLACED FLOOR STRUCTURE ACTUATOR ATTACH BRACKET AT FR54 BTW - Y765 TO -Y1292 IN PASSENGER CABIN AS PER SRM 51-42-11, 51- 72-11 AND DRAWING D53472020 REV.K

Part: ACCESS PANEL — CRACKED (LT HORIZ STAB) · airframe 82,744 hrs · 38,030 cycles

CRACK LEADING EDGE TIP 332AB ON LT HORIZONTAL STABILIZER (1 EA). REPAIRED BY WELD ACCESS PANEL 332AB (TIP) AT HORIZONTAL STABILIZER LT AS PER ER/A N. 579687-14.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOOR STRUCTURE BEAM LOCATED BTW FR 12 TO FR 24-Y765 IN PASSENGER CABIN, REPLACED FLOOR STRUCTURE BEAM LOCATED BTW FR12 TO FR24 -Y765 IN PASSENGER CABIN ( 1EA) AS PER SRM 51-72-11 SRM -51-42-11. AND DWG # D53110920

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOORBEAM -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA (1 EA) (SSI 534147). REPLACED FLOORBEAM -Y765 LOC BTW FR 64 TO FR 66 AT AFT GALLEY AREA ASPER SRM 51-72-11 AND DRAWING 14N00031-103.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOORBEAM -Y765 BTW FR66 TO FR70 AT AFT GALLEY AREA (1 EA) (SSI 534147). REPLACED FLOORBEAM -Y765 LOC BTW FR66 TO FR70 AT AFT GALLEY AREA ASPER SRM 51-72-11 AND DRAWING D53472193200.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

CRACK INDICATION ON FRAME 16 LOWER INBD FASTENER HOLE AT DOOR STOP 7 RT SIDE, CRACK DIRECTION 7 AND 9 OCLOCK DEPTH IS 0.170 INCH. AT FWD GALLEY AREA (1 EA). PERFORMED ROTOTEST INSPECTION ON FASTENER HOLES OF INTERCOSTA AT FRAME 16 AND DOOR STOP FITTING #7 RT SIDE AS PER NTM 51-10-01. THE REPLACEMENT OF INTERCOSTAL FITTING IS ACCOMPLISHED ON CARD 89.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOOR STRUCTURE LOCATED BTW FR 12 TO FR 24 -Y 1292 IN PASSEN GER CABIN (1 EA) (SSI 531189). REPLACED FLOORBEAM LOC BTW FR12 TO FR24 -Y1292 IN PASSENGER CABIN ASPER SRM 51-72-11 AND DWG D53112812.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOORBEAM +Y254 BTW FR12 TO FR24 AT FWD GALLEY AREA (1 EA) (SSI 531189). REPLACED FLOORBEAM +Y25A BTW TO FR12 TO FR24 FWD GALLEY AREA AND FASTENER ASPER SRM 51-72-11 AND DWG D53112816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOORBEAM +Y512 BETWEEN FR 12 TO FR 16 AT FWD GALLEY AREA (1 EA) (SSI 531189). REPLACED FLOORBEAM +Y512 LOC BTW FR 12 TO FR 16 AT FWD GALLEY AREA ASPER SRM 51-72-11 AND DRAWING D53110984.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

CRACK INDICATION ON FRAME 16 LOWER INBD HOLE AT DOOR STOP 7 LT SIDE, C RACK DIRECTION IS 5 OCLOCK. DEPTH IS 0.150 INCH. AT FWD GALLEY AREA ( 1 EA). PERFORMED ROTOTEST INSPECTION ON FASTENERS HOLES OF INTERCOSTAL AT FRAME 16 AND DOOR STOP FITTING 7 4H SIDE AS PER NTM 51-10-01 CRACK INDICATION FOUND ONLY ON INTERCOSTAL FITTING TOOL USED PN 500D SN N5001CR0N102020 DUE DATE 03 JAN 20 THE REPLACEMENT OF INTERCOSTAL IS ACCOMPLISHED ON CARD 92.

Part: FITTING — CRACKED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

CRACK INDICATION ON FRAME 16 UPPER INBD FASTENER HOLE AT DOOR STOP 7 RT SIDE, CRACK DIRECTION 7 OCLOCK DEPTH IS 0.140 INCH. AT FWD GALLEY AREA (1 EA), REPLACED INTERCOSTAL FITTING AT FRAME 16 AND DOOR STOP FITTING #7 RT SIDE ASPER SRM 51-72-11 AND DWG D53114223.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 82,744 hrs · 38,030 cycles

CRACK INDICATION ON FRAME 16 UPPER INBD FASTENER HOLE AT DOOR STOP 7 LT SIDE, CRACK DIRECTION 5 AND 6 OCLOCK. DEPTH IS 0.120 INCH. AT FWD GALLEY AREA (1 EA), REPLACED INTERCOSTAL FITTING AT FRAME 16 AND DOOR STOP FITTING #7 LT SIDE AS PER SRM 51-72-11 AND DWG D53114223.

Part: FLOOR PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 82,744 hrs · 38,030 cycles

CORROSION FLOOR PANEL 221FF AT FWD GALLEY AREA, ACCOMPLISHED ON CARD # 2500-0617 REPLACED FLOOR PANEL 221FF AR FWD GALLEY AREA.

Part: CONNECTOR — DISCONNECTED (BRAKE SYSTEM) · airframe 82,657 hrs · 37,985 cycles

NR 3 TIRE BLOWN ON LANDING WITH BRAKES SYS 1 FAULT / BRAKES AUTO BRK FAULT ECAM WARNING. FIRE EMERGENCY WAS AT THE SCENE WITH LOCAL MAINTENANCE, AIRCRAFT TOWED TO THE GATE. FOUND CONNECTOR TO # 3 WHEEL NORMAL BRAKE SERVO VALVE (16GG) OFF THE VALVE AND DANGLING ON THE RT MLG LEG. RE-CONNECTED CONNECTOR, RESET BSCU, REPLACED #3 AND #4 WHEEL ASSY. TESTED ANTI-SKID SYSTEM NORMAL.

Part: LANYARD — OUT OF POSITION (SURVIVAL KIT) · airframe 80,771 hrs · 37,053 cycles

(LP 3999760) RIGHT AND LEFT FORWARD DOOR WHITE LANYARD LOOP ON SURVIVAL KIT ATTACH LANYARDS IMPROPERLY POSITIONED. REPOSITIONED LOOPS ON LEFT AND RIGHT FORWARD DOORS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,799 hrs · 37,067 cycles

ALL FOUR OVERWING DOOR PULL HANDLE LIGHTS INOPERATIVE. RELAMPED. OPERATION CHECKS OKAY.

Part: LANYARD — DETACHED (DOOR SLIDE) · airframe 79,382 hrs · 36,346 cycles

SLIDE DISARMING PIN ATTACH LANYARD DETACHED. ATTACHED THE LANYARD. OPS CHECKED GOOD.

Part: WIRE — MISINSTALLED (EMERGENCY LIGHTS) · airframe 78,966 hrs · 36,179 cycles

ESCAPE SLIDE LIGHTING DURING SERVICE CHECK, EPSU BITE FAIL, WIRES TO CONNECTOR 2819 VC PLUG SIDE IN WRONG HOLES. REPINNED WIRES TO SLOTS J AND K EMERGENCY LIGHTS

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 78,719 hrs · 36,059 cycles

ROW 13CD EMERGENCY LIGHT LENS HANGING DOWN, REPLACED THE LENS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,897 hrs · 35,656 cycles

ELONGATED HOLE EXTERNAL SKIN FR35-36 STR1-L AND STR1-R VHF3 ON UPPER FUSELAGE. PERFORMED SECTION I AS PERMANENT REPAIR AT FR35-36 STR 1L AND STR 1R VHF3 ANTENNA ON UPPER FUSELAGE INSTALL/OVER SIZE AS PER PRI 561810-14 REV 0,1,2,3 AND 4 AND ER/A 561810-14 REV ORIGINAL.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 77,894 hrs · 35,655 cycles

CRACK SEAT TRACK Y1292 IN PASSENGER CABIN FROM FRAME 36 TO FRAME 41. REPLACED SEAT TRACK Y1292 IN PASSENGER CABIN FROM FRAME 36 TO FRAME 41 PER SRM 51-72-11 AND DWG D57130147.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 75,753 hrs · 34,651 cycles

EMERGENCY EXIT SIGN R1 DOOR INOPERATIVE, SECURED THE CONNECTOR.

Part: BEAM — CRACKED (FUSELAGE) · airframe 75,651 hrs · 34,597 cycles

LT SIDE BOX FR 43, BEAM CRACKED AT AFT AND MIDDLE HOLES. SEE NR FOR ADDITIONAL INFORMATION 002-0001:5310-01450-01/003 00017 REPAIR WAS ACCOMPLISHED PER AMDS 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.

Part: PLATE — CRACKED (FUSELAGE) · airframe 75,651 hrs · 34,597 cycles

RT SIDE BOX FR 43 PLATE CRACKED AT FWD HOLE. SEE NR FOR ADDITIONAL INFORMATION 002-0001:5310-01450-01 002 REPLACED PLATE ACCOMPLISHED REPAIR PER AMDS 5310-01450-02 IN ACCORDANCE WITH SB A320-53-1251 REV 1.

Part: CONNECTOR — LOOSE (CABIN) · airframe 75,513 hrs · 34,530 cycles

ON CLIMBOUT FLT ATT REPORTED A MUSTY SMELL WITH HEAT IN LAST 4 ROWS OF CABIN. SHUT OFF PAX SYS/PED PWR AND SMELL WENT AWAY, FOUND CONNECTOR J40 LOOSE AT RECEPTACLE AT FLOOR TO BULKHEAD. RESECURED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,460 hrs · 32,961 cycles

AFT LT EMERGENCY LIGHT FAULT, REPLACED BATTERY.

Part: SKIN — DAMAGED (NR 3 SLAT) · airframe 72,220 hrs · 32,827 cycles

MISSING MATERIAL ON SLAT 3 INBD EDGE AT T/E AREA ON RT WING. PERFORMED REPAIR ON SLAT 3 INBD EDGE AT T/E AREA ON RT WING IAW PRI ER/A 539117-14, REV 0 AND ER/A 539117-14.

Part: SPAR — WORN (LT WING) · airframe 72,220 hrs · 32,827 cycles

WEAR ON BOTTON SKIN REIFORCING PLATE REAR SPAR ON LT WING FROM RIB 7 TO RIB 8. REPLACED REINFORCING PLATE REAR SPAR ON LT WING FROM RIB 7 TO RIB 8 IAW SRM 57-21-11, PARA 5.E, FIG 205.

Part: SPAR — WORN (RT WING) · airframe 72,220 hrs · 32,827 cycles

WEAR ON BOTTON SKIN REINFORCING PLATE REAR SPAR ON RT WING FROM RIB 7 TO RIB 8. REPLACED REINFORCING PLATE REAR SPAR ON RT WING FROM RIB 7 TO RIB 8 IAW SRM 57-21-11 PARA 5.E, FIG 205.

Part: STRUCTURE — CORRODED · airframe 70,970 hrs · 32,245 cycles

DURING INSPECTION, FOUND CORROSION FOUND BETWEEN STR 42L AND 43L BETWEEN 56-57 REF PRI 53-5226-14. INSTALLED DOUBLER IAW PRI 535226-12, VER 1, 2 , 874907.

Part: LIGHT — DAMAGED (CABIN) · airframe 70,829 hrs · 32,178 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE, REINSERTED LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 70,295 hrs · 31,937 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT OUT AT ROW 16 D E F. REPAIRED BROKEN WIRES FOR SEAT EMERGENCY LIGHT AND FUNCTIONAL CHECK WAS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 68,510 hrs · 31,062 cycles

DURING NON ROUTINE CHECK, FOUND SEAT 16C WHITE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND AND REPAIRED LOOSE CONNECTION AT SEAT 16 AND FUNCTIONAL CHECK WAS NORMAL.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 68,185 hrs · 30,888 cycles

EMERGENCY LIGHTS INOPERATIVE ROWS 5, 6, & 7ABC. SEATED CONNECTOR. EMERGENCY LIGHTS CHECKED OK IAW AMM 33-50.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 66,752 hrs · 30,193 cycles

FOUND EMERGENCY LIGHT AT SEAT 15ABC INOPERATIVE. MAINTENANCE REPAIRED WIRES AND FUNCTIONAL TESTED GOOD.

Part: PLATE — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON REFORCING PLATE IN BULK CARGO COMPART. LOCATED BETWEEN FRAMES 65 TO 66 AND STRINGERS 37-43L REPLACED REFORCING PLATE IAW SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR PLATE LOCATED BETWEEN FRAMES 69 AND 70 AT S23R IN PAX CABIN. REPLACED SHEAR PLATE IAW SRM 51-72-11 AND DWG D53470100.

Part: PLATE — CORRODED (FUSELAGE) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON AREA SURROUNDING THE FWD LT PASSENGER DOOR CUT OUT LOCATED AT LEVEL OF FWD FACE FRAME 20 AND STR 23L, REPLACED REINFORCEMENT PLATE IAW SRM 51-72-11, DWG D53112174, D53112350 AND ER/A NR 518745-14,REV ORIGINAL.

Part: PLATE — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON PLATE LOCATED AT FRAME 24A THRESHOLD SHEET AREA FWD CARGO COMPARTMENT. REPLACED PLATE IAW SRM 51-72-11.

Part: STRINGER — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 44 IN AFT CARGO BAY FRAMES 61. PERFORMED PERMANENT REPAIR ON STRINGER 44 IAW SRM 53-00-13, PARA 4A, FIG 201 (SHEET 2) PAG 213/214.

Part: ROD — CORRODED · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON TARGET AND PLAY ON ACTUATOR ROD AND PLAY ON BEARING AT INTERCONNECTING STRUT. LT SIDE. REPLACED INTERCONNECTING STRUT LT SIDE. IS DOCUMENTED ON AMDS CARD 2751-9202/101.

Part: STRUCTURE — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON SECTION CONNECTING IN BULK CARGO COMPART LOCATION. AT STR 27L AND AT FR 67 MEASURE L=0.900", W=0.250", D=0.004". REPLACED SECTION CONNECTING LOCATED AT FR 67 AND STR 27L IN BULK CARGO COMPARTMENT IAW SRM 51-72-11.

Part: SKIN — DENTED (FUSELAGE) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL REAR FUSELAGE SKIN LOCATED FRAME 79+2" AND BETWEEN STR 4 - 5L. PERFORMED PERMANENT REPAIR ON EXTERNAL REAR FUSELAGE SKIN IAW SRM A320 53-00-11, PARA 4W, PAG 579/580, FIG 239.

Part: SHEAR PLATE — CORRODED · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR PLATE LOCATED BETWEEN FRAMES 69 AND 70 AT STR 23L IN PAX CABIN. REPLACED SHEAR PLATE IAW SRM A320 51-72-11 AND DWG D53470100.

Part: WEB — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY, LOCATED BETWEEN FRAMES 58 TO 59 AT STR 38R, REPLACED WEB IN AFT CARGO COMPARTMENT LOCATED BETWEEN FR 58 TO FR 59 AT STR 38R IAW SRM 51-72-11 AND DWG D53470320.

Part: STRINGER — CORRODED (43 LEFT) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L IN AFT CARGO BAY BETWEEN FRAMES 56 TO 57. REPAIRED STRINGER.

Part: SILL — CORRODED (CABIN) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL LOCATED BETWEEN FRAMES 66 AND 68 STRINGER 23L. REPLACED LOWER SILL IAW SRM 51-72-11.

Part: STRUCTURE — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON SECTION CONNECTING IN BULK CARGO BAY, STRINGER 29L AND FRAME 67 MEASURE. REPLACED SECTION CONNECTING IN BULK CARGO BAY IAW SRM 51-72-11.

Part: STRUCTURE — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON SECTION CONNECTING IN BULK CARGO BAY STRINGER 26L FRAME 67. REPLACED SECTION IAW SRM 58-72-11 AND DWG D53480505.

Part: FITTING — CORRODED (CABIN) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON CENTER FITTING BETWEEN FRAMES 66 AND 68 STR 23L. REPLACED FITTING.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON FLOOR SUPPORT -Y1162 LOCATED BETWEEN FRAMES 67+15" AND 69+3". REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 66,483 hrs · 30,040 cycles

IMPROPERLY HOLE ON FLOOR SUPPORT +Y1292 LOCATED AT FRAME 66 IN PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472230.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON FLOOR SUPPORT AT +Y1225 BETWEEN FRAMES 66+4" AND 67+15". REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472000 AND REPLACED SPLICE IAW SRM 51-72-11, LOCATION FR 66+4" UPPER INBD POSITION IAW DWG D53472230.

Part: FLOOR SUPPORT — CORRODED (PAX CABIN) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON FLOOR SUPPORT -Y1292 LOCATED BETWEEN FRAMES 64 AND 66+4". REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472230.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON LOWER CORNER FITTING AT FRAME 68 LEVEL OF STR 23R IN PAX CABIN. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53480505.

Part: UPPER SHEET — CORRODED (FUSELAGE) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON COVER SHEET LOCATED BETWEEN FRAMES 24A TO 28 FWD CARGO BAY. REPLACED COVER SHEET IAW SRM 51-72-11 AND DWG D53230315.

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON FLOOR SUPPORT +Y1162 LOCATED BETWEEN FRAMES 67+15" - 69+3". REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000 AND REPLACED SPLICE IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 66,483 hrs · 30,040 cycles

CORROSION FOUND ON FLOOR SUPPORT -Y1225 LOCATED BETWEEN FRAMES 66+4" - 67+15" IN PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: THRESHOLD — CORRODED · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON THRESHOLD SHEET LOCATED BETWEEN FR 24A TO FR 28 FWD CARGO COMP SSI 532180. MEASURES ARE: L=0.890", W=0.425", D=0.001". REPLACED THRESHOLD SHEET LOCATED BETWEEN FR 24A TO FR 28 FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D53231264.

Part: SILL — CORRODED (L1 DOOR) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER L1 DOOR SILL LOCATED BETWEEN FR 16 TO FR 20 AND STR 23L. REPLACED LOWER SILL IAW SRM 51-72-11.

Part: WEB — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY BETWEEN FR 58 TO FR 59 AT STR 38L. REPLACED WEB AND FASTENER IAW SRM 51-72-11 AND DWG D53470321.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING AFT FACE FR 16 AT LEVEL OF STRG 23R. REPLACED CONER FITTING IAW SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 LEVEL OF STR 23R IN PAX CABIN. REPLACED CENTER FITTING LOCATED BETWEEN FR 66 AND FR 68 LEVEL OF STR 23R IN PAX CABIN IAW SRM 51-72-11 AND DWG D53480505.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING FWD FACE FR 20 AT LEVEL OF STRG 23R. REPLACED CORNER FITTING IAW SRM 51-72-11 AND DWG D53112225 JOB COMPLETE.

Part: CLEAT — CORRODED (FWD CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON CLEAT AT FRAME 28 BETWEEN STRINGERS 41-42R IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231586.

Part: WEB — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

CORROSION FOUND ON WEB IN AFT CARGO BAY, BETWEEN FRAMES 54 - 55 STRINGER 38L. REPLACED WEB IAW SRM 51-72-12 AND DWG D53470321.

Part: CLEAT — CORRODED (FWD CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON CLEAT AT FRAME 28 BETWEEN STRINGERS 42 AND 43R IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231626.

Part: CLEAT — CORRODED (FWD CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

CORROSION ON CLEAT AT FRAME 31, BETWEEN STRINGERS 39 AND 40L IN FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231626.

Part: CLEAT — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 32, BETWEEN S40-41L FWD CARGO BAY. REPLACED CLEAT IAW SRM A320 51-72-11 AND DWG D53231626.

Part: SPLICE — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON SPLICE LOCATED BETWEEN FRAMES 30 AND 31, STRINGER 41L FWD CARGO BAY. REPLACED SPLICE IAW SRM 51-72-11 AND DWG D53231375.

Part: WEB — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN BULK CARGO BAY BETWEEN FRAMES 69 & 70 S23L. REPLACED WEB IAW SRM 51-72-11.

Part: WEB — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN BULK CARGO BAY BETWEEN FRAMES 69 TO 70 AT S23R. REPLACED WEB IAW SRM 51-72-11 AND DWG D53470100.

Part: CLEAT — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FRAME 32 BETWEEN S41-42R FWD CARGO BAY. . REPLACED CLEAT IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y81 FWD PAX CABIN BETWEEN FRAMES 12 AND 16. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112828.

Part: CLEAT — CORRODED (ZONE 100) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 32 S42-43R FWD CARGO BAY. REPLACED CLEAT IAW SRM AND DWG D53231626.

Part: CLEAT — CORRODED (ZONE 100) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 32 BETWEEN STR 42-43L FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231626.

Part: CLEAT — CORRODED (ZONE 100) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT AT FRAME 31 BETWEEN S40-41L, FWD CARGO BAY. REPLACED CLEAT IAW SRM A320 51-72-11 AND DWG D53231626.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT, +Y765 BETWEEN FRAMES 66+4" AND 70 IN PAX CABIN. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: CLEAT — CORRODED (ZONE 200) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT FRAME 32 BETWEEN S42-43R FWD CARGO BAY. REPLACED CLEAT IAW SRM 51-72-11 AND DWG D53231626.

Part: CLEAT — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT LOCATED AT FR 32 BETWEEN STR 40-41R FWD CARGO BAY. REPLACED CLEAT IAW SRM A320 51-72-11 AND DWG D53231586.

Part: CLEAT — CORRODED (CARGO BAY) · airframe 66,483 hrs · 30,040 cycles

DURING INSPECTION, CORROSION ON CLEAT LOCATED AT FR 33, BETWEEN STR 41-42R FWD CARGO BAY. REPLACED CLEAT IAW SRM A320 51-72-11 AND DWG D53231586.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 66,067 hrs · 29,828 cycles

ON SERVICE CHECK, FOUND RT EMERGENCY BATTERY PACK FAIL ON LIGHT TEST. REPLACED 12WL EMERGENCY BATTERY AMM 33-51-38. OK FOR SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 65,913 hrs · 29,740 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT ROW 2AB. MX INSTALLED NEW SPLICE CONNECTOR AND OPS CHECK WAS NORMAL.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 64,541 hrs · 29,062 cycles

DURING NON ROUTINE CHECK, FOUND AISLE EMERGENCY LIGHT INOPERATIVE AT ROW 14. INSPECTED AND FOUND WIRES PULLED OUT OF CONNECTOR. INSTALLED NEW PINS AND CONNECTOR. OPS CHECK WERE NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 64,260 hrs · 28,940 cycles

DURING NON ROUTINE CHECK AND WHILE WORKING JIC 2561-4002-RF RECEIVED EPSU BATTERY EMERGENCY RT FAILURE MESSAGE ON CIDS PANEL. REPLACED EPSU BATTERY AT RIGHT AND FUNCTIONAL CHECK WAS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,750 hrs · 28,197 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT SYSTEM FAILED TEST AT AFT L. MAINTENANCE RELAMPED SEVERAL CABIN EXIT SIGNS AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: SLIDING WINDOW — MALFUNCTIONED (COCKPIT) · airframe 59,563 hrs · 26,688 cycles

DURING CLIMB FLIGHT CREW EXPERIENCED STRONG ELECTRICAL SMELL FOLLOWED BY A SMALL AMOUNT OF SMOKE COMING FROM THE FORWARD PORTION OF FIRST OFFICER WINDOW. PULLED W14CB CIRCUIT BREAKER FOR WINDOW ANTI ICE. AIRCRAFT CONTINUED ON SAFELY TO DESTINATION. MAINTENANCE REPLACED FIRST OFFICER SLIDING WINDOW PER AMM 56-12-11 AND CONTROLLER PER AMM 30-42-00 TESTS OK AND AIRCRAFT HAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 5,917 hrs · 126,507 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT ROW 21 INOPERATIVE. REPAIRED BROKEN WIRING AND TESTS OK.

Part: LIGHT — MISSING (SEAT 5C) · airframe 58,387 hrs · 26,189 cycles

FLIGHT CREW REPORTED EMERGENCY PATH FLOOR LIGHT SEAT 5C MISSING AND WIRES ARE EXPOSED, INSTALLED COVER AND TESTS OK.

Part: HYDRAULIC SYSTEM — LOW (GREEN) · airframe 55,567 hrs · 24,996 cycles

AFTER FLAP RETRACTION, ACFT LOSS GREEN HYD QUANTITY. GEAR WAS RETRACTED NORMAL. CREW DIVERTED AND LANDED WITHOUT INCIDENT.

Part: LINE — RUPTURED (HYD SYSTEM) · airframe 55,567 hrs · 24,996 cycles

AFTER TAKEOFF, ACFT LOSS GREEN HYD QUANTITY. GEAR WAS RETRACTED NORMAL. CREW DIVERTED AND LANDED WITHOUT INCIDENT. FOUND DOWN LOCK ACTUATOR LINE RUPTURED. REPLACED LOCK STAY ACTUATOR HOSE AND OPS CHECK WAS NORMAL.

Part: MANIFOLD — LEAKING (HYD SYSTEM) · airframe 49,857 hrs · 22,433 cycles

SHORTLY AFTER TAKEOFF THE HYD G RSVR LO LVL FAULT ANNUNCIATED. AIRCRAFT RETURNED TO MEM, LANDING GEAR GRAVITY EXTENDED. AIRCRAFT LANDED UNEVENTFULLY AND WAS TOWED TO GATE. REPLACED GREEN GROUND LEAK MEASUREMENT MANIFOLD AND NR 1 ENGINE DRIVEN GREEN PUMP.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 47,671 hrs · 21,315 cycles

LEFT FORWARD EMERGENCY LIGHT POWER SUPPLY INOP. REPLACED LEFT FORWARD EMERGENCY LIGHT POWER SUPPLY, CHECKS OK.

Part: LINE — CHAFED (HYD SYSTEM) · airframe 36,983 hrs · 16,170 cycles

IN MODERATE TURBULENCE, AUTOPILOT KICKED OUT AND RECEIVED YELLOW HYDRAULIC SYSTEM RESERVOIR LOW LEVEL MESSAGE ON ECAM. FOLLOWED COM PROCEDURE AND LANDED AT DTW UNEVENTFULLY. FOUND YELLOW SYSTEM COMPLETELY EMPTY. FOUND SPOILER HYDRAULIC PRESSURE LINE CHAFED ON WIRING RACEWAY. REPAIRED LINE WITH RING-LOK REPAIR PER AMM. SERVICED YELLOW HYDRAULIC RESERVOIR. SYSTEM LEAK CHECK OIK. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — BURNED OUT (E/E BAY) · airframe 35,942 hrs · 15,712 cycles

DURING CRUISE EXPERIENCED RUMBLING/VIBRATION SEEMING TO COME FROM AVIONICS COMPARTMENT. ALSO EXPERIENCED ELECTRICAL BURING ODOR (NO SMOKE). DIVERTED TO BHM AND LANDED UNEVENTFULLY. VERIFIED AVIONICS BLOWER FAN FAULTY AND APPLIED MEL PROVISIONS. RAN PACK AND VERIFIED ABSENCE OF ODOR AND SMOKE. RETURNED A/C TO SERVICE.

Part: HYDRAULIC SYSTEM — LOW (YELLOW SYSTEM) · airframe 29,590 hrs · 12,939 cycles

FOLLOWING APPLICATION OF TAKEOFF POWER, RECEIVED HYD Y RSVR LO LVL MESSAGE. ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE SERVICED THE YELLOW HYDRAULIC SYSTEM BUT NO LEAKS WERE FOUND. OPERATIONAL CHECK OK.

Part: SLIDE — DEPLOYED (PAX DOOR) · airframe 28,279 hrs · 12,342 cycles

AFTER PARKING AT THE GATE, THE AFT LEFT DOOR WAS INADVERTENTLY OPENED WITH THE SLIDE ARMED. THE SLIDE FULLY DEPLOYED REACHING THE GROUND BUT DID NOT INFLATE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY AND RESERVICED THE DOOR ASSIST BOTTLE.

Part: BATTERY PACK — DISCHARGED (CABIN)

NUMEROUS FLOOR ESCAPE PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING EMERGENCY LIGHT TEST, INT LOADS EMER R FAULT DISPLAYED. MAINTENANCE REPLACED PSEU BATTERY PACK. OPERATIONAL CHECK OK.

Part: RELAY — INTERMITTENT (E/E COMP)

AFTER TAKEOFF, RECEIVED ECAM WARNING ELEC ESS BUSSES ON BAT. RETURNED TO YVR AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RELAY 16XC, OPERATIONAL CHECK OK.

Part: CASTING — CRACKED (CARGO DOOR)

DURING LINE CHECK, FOUND THAT THE FORWARD CARGO DOOR HANDLE ATTACH MECHANISM CASTING WAS BROKEN. REPLACED CASTING.

Part: ACTUATOR — LEAKING (NR 2 SPOILER)

DURING CLIMBOUT, THE YELLOW HYDRAULIC SYSTEM FLUID DECREASED TO ZERO ACCOMPANIED BY A RIGHT WING NR 2 SPOILER ECAM INDICATION. THE SPOILER WAS DEPLOYED AT APPROXIMATELY 45 DEGREES. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT WING NR 2 SPOILER ACTUATOR, LEAK AND OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILED THE LEFT FORWARD BATTERY. REPLACED BATTERY PACK, OPERATIONAL CHECK OK.

Part: SENSOR — MALFUNCTIONED (LT MLG)

AFTER TAKEOFF THE LANDING GEAR DID NOT RETRACT, CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT MAIN LANDING GEAR PROXIMITY SENSOR 20GA, OPERATIONAL CHECK OK.

Part: UPLOCK IND — MALFUNCTIONED (LANDING GEAR)

DURING CLIMBOUT, RECEIVED LANDING GEAR NOT UPLOCKED MESSAGE. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED NO DISCREPANCY.

Part: EEL POWER SUPPLY — INOPERATIVE (CABIN)

DURING CRUISE, THE AFT CABIN EMERGENCY PATH LIGHTS REMAINED ILLUMINATED, RESETTING THE SYSTEM DID NOT HELP. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT, 11WL AND OPERATIONAL CHECK OK.

Part: GENERATOR — MALFUNCTIONED (NR 2 ENGINE)

DURING TAKEOFF ROLL, RECEIVED ELEC IDG 2 OIL LOW PRESSURE MESSAGE. THE TAKEOFF WAS ABORTED AT APPROXIMATELY 40 KNOTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 2 IDG, LEAK AND OPERATIONAL CHECK OK.

Part: HYD FLUID — LOW LEVEL (B-HYD SYST)

AFTER APPLYING T/O THRUST FOR TAKEOFF ROLL, RECEIVED HYD B RSVR LO LVL MESSAGE. THE TAKEOFF WAS ABORTED AT 60 KNOTS. MAINTENANCE SERVICED THE BLUE HYDRAULIC SYSTEM. LEAK AND OPERATIONAL CHECK OK.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

DURING APPROACH INTO SAN, RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT WHEN FLAP 3 WAS SELECTED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DESCREPANCIES.