N369NW

Part: MOUNT — BROKEN (EMERGENCY LIGHT) · airframe 75,908 hrs · 35,675 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:10D. SECURED LIGHT TO SEAT WITH TAPE. DEFERRED TO MEL, PLACARDS INSTALLED. (NOTE: MOUNT POINT ON SEAT BROKEN- WILL NEED SEAT SHROUD REPAIR/REPLACE). (LP: 1212089)

Part: OXYGEN PANEL — MISINSTALLED (ZONE 200) · airframe 75,462 hrs · 35,440 cycles

SHIP 3269 AFT LAV OXYGEN PANEL DOOR HAS STRINGS HANGING OUT THE SIDES. LOOKS TAMPERED WITH. SECURED O2 PANEL AND STOWED MASKS OK FOR SVC A320AMM 35-21. (LP: 1106540)

Part: IDG — DAMAGED (ZONE 400) · airframe 75,361 hrs · 35,387 cycles

SHIP 3269 - DIV - TO AUS DUE APU ON MEL AND #2 IDG OIL TEMPERATURE ABOVE 147 DEGREES. CORRECTIVE ACTION: REPLACEMENT OF IDG #2 IN PROGRESS. (LP: 7809135)

Part: STOP — BROKEN (OXYGEN PANEL) · airframe 75,320 hrs · 35,368 cycles

SHIP 3269 DISC: PSU OXYGEN DOOR TEST STOP ASSEMBLY BROKEN / LOCATIONS:103. C/A: RESECURED PARTIALLY OPEN PSU IAW A320 AMM 32-50. NO DAMAGE NOTED. (LP: 1067146)

Part: SHAFT — SHEARED (HYD PUMP) · airframe 75,241 hrs · 35,324 cycles

DECLARED EMERGENCY DUE TO HYDRAULIC G OVERHEAT WITH NO RESTORATION OF HYD G SYSTEM. REQUIRED USE OF L/G GRAVITY GEAR EXTN HANDCRANK. VERIFIED FREE FALL EXTENSION. REFERENCE ODI EVENT LOG 1050057. GREEN EDP SHAFT FOUND SHEARED. R/R SAME AND FILTERS. LK/OPS CK OK. A/C OK FOR SVC.

Part: O-RING — LEAKING (HYD SYSTEM) · airframe 74,474 hrs · 34,933 cycles

SHIP 3269 DISC: ON APPROCH TO GATE, CREW NOTED DIRTY SOCK ODOR IN COCKPIT. CREW DESELECTEED APU BLEED AND ODER GRADUALLY DISAPPEARED CAPT NOTED FA WHO STATED THY DID NOT SMELL THE ODOR IN THE CABIN. C/A: FOUND A HYDRAULIC LEAK FROM THE BRAKE SELECTOR VALVE MANIFOLD. R /R THE O-RINGS ON THE BRAKE SELECTOR VALVE MANIFOLD PER A320 AMM 32-42. OPS AND LEAK CHECK GOOD. FOLLOWED ODI PREVENTION STEPS ON LOG# 0865592. C/W W/C 0550-2002. FOUND APU INGESTED HYDRAULIC PERFORMED CORRECTIVE ACTIVE FOR TYPE 1 APU. C/W W/C 4900-2001 AND AMM 21-00-00-615-803-A AND AMM 36-0-00-615-801-A. DECONTAMINATION OF THE ECS LEVEL B ACCOMPLISHED. APU IS FORWARDED TO MEL. (LP: 6522442)

Part: UNKNOWN — ODOR (CABIN) · airframe 74,301 hrs · 34,830 cycles

SHIP 3269 DISC: DIRTY SOCK ODOR DETECTED MID CABIN FORWARD UPON FINAL APPROACH AND LANDING. C/A: COMPLETED STEPS 1-4 FOR CARD # 0550-2002. (534407). FINISHED REMAINING STEPS OF CARD 0550-2002. C/W AMDS WORK CARD 4916-2001. C/W LEVEL B DECONTAMINATION PER A320 AMM 21-00-00-615-803-A. NO SCENT REMAINING. (LP: 6695160)

Part: INLET — CONTAMINATED (APU) · airframe 74,301 hrs · 34,830 cycles

SHIP 3269 - SMOKE - DECLARED EMERGENCY DUE TO VISIBLE SMOKE IN THE COCKPIT AND MID CABIN DURING LANDING. CORRECTIVE ACTION: FOUND APU INLET CONTAMINATED. DEFERRED APU PER MEL.

Part: BRAKE ASSY — LOW PRESSURE (ZONE 700) · airframe 73,917 hrs · 34,603 cycles

SHIP 3269 DISC: FOUND #4 BRAKE ASSY NOT RELEASING WITH NO BRAKE PRESSURE. C/A: REMOVED AND REPLACED #4 BRAKE ASSY. REF A320 AMM 32-42. BRAKE CK NORMAL. (LP: 6940077)

Part: ARMING LEVER — OUT OF ADJUST (ZONE 800) · airframe 73,886 hrs · 34,587 cycles

SHIP 3269 DISC: 1L DOOR WILL NOT ARM . C/A: UPON INSPECTION FOUND SLIDE ARMING LEVER OUT OF ADJUSTMENT. WHEN SLIDE IS ARMED, ARMING LEVER PAD IS NOT MAKING THE PROX SWITCH. ADJUSTED SLIDE ARMING LEVER PER A320 AMM 52-11. ALL OPS CKS GOOD. SLIDE INDICATION PRESENT ON ECAM. OK FOR SVC. (LP: 6940058)

Part: FILLET — CRACKED (ZONE 100) · airframe 73,216 hrs · 34,261 cycles

SHIP 3269 DISC: A320 / FUSELAGE / RH FR68 AT STGR22 RADIAL FLANGE FILLET LOWER RADIUS / CRACK. ER/A 616977-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. C/A: ER/A 616977-14AD REV A SECTION II FOLLOW-ON INSPECTIONS ARE REQUIRED ON OR BEFORE 53,200 TOTAL AIRFRAME FC. THEREAFTER, REPEAT SECTION II WITHIN EVERY 19,700 FC. ASSOCIATED ER/A 00-616977 ADDED FOR AC 3269. (LP: 0574107)

Part: UNKNOWN — ODOR (ZONE 200) · airframe 72,901 hrs · 34,098 cycles

SHIP3269 DISC: F/A'S REPORT ROTTEN EGG SMELL FROM GALLEY GASPER. GROUND AIR DISCONNECTED, APU RAN FOR 5+ MINUTES BEFORE BLEED SELECTED ON. C/A: PERFORMED INSPECTION PER AMDS 0550-2002 NO SMELL FOUND IN FWD GALLEY GASPER AREA EXCEPT FWD GALLEY DRAIN. CLEANED DRAIN NO SMELL AT THIS TIME. C/W NO-GO ODI STEPS REF LOG 0503697. (LP: 6155022)

Part: ELECTRONIC UNIT — HOT (E/E BAY) · airframe 72,605 hrs · 33,945 cycles

SHIP 3269 DISC: ON TAXI OUT, FA'S REPORTED A SMOKE SMELL FROM VENT @ 1A. NO VISIBLE SMOKE WAS OBSERVED. WAS DESCRIBED AS A PLASTIC SMELL. NO SMELL OBSERVED ELSEWHERE IN CABIN. C/A: T/S PER A320 CARD 0500-2002. FOUND PANASONIC HDD-OML DATA LOADER AND RACK EXTREMELY HOT - L1 CLOSET UPPER COMPARTMENT. FAULT LIGHT ILLUMINATED RED. REF LOG # 6054981 FOR DEACTIVATION AND DEFERRAL. CONFIRMED POWER REMOVED FROM BOX. (LP: 6054980)

Part: CONNECTOR — LOOSE (STEERING HYD MOD) · airframe 72,605 hrs · 33,945 cycles

SHIP 3269 - MISC/DE - DUE TO NOSE WHEEL STEERING FAULT AFTER GEAR EXTENSION FOR APPROACH. CORRECTIVE ACTION: REINSTALLED LOOSE CONNECTOR, 6GC-A, AT STEERING HYDRAULIC MODULE. AIRCRAFT RTS.

Part: LIGHT — SHORTED (CABIN) · airframe 72,305 hrs · 33,797 cycles

SHIP 3269 DISC: IN SERVICE CHECK FOUND EMERGENCY LIGHTS MSG ON PTP ATA 33-51-38/ EPSU INT LOAD FWD L. C/A: SLAVED IN NEW POWER SUPPLY 10WL. NO HELP. T/S PER TSM A320 33-51 -00-810-807. DID NOT LOCATE ISSUE. CEILING PANELS REMOVED. WIP 530909. FOUND OVERHEAD DOORS 1L AND 2L EMERGENCY LIGHT ASSEMBLIES INTERNAL SHORT. REPLACED BOTH ASSEMBLIES AND PERFORMED SYSTEM TEST. OPS OK. (LP: 5335419)

Part: INLET — CONTAMINATED (APU) · airframe 72,240 hrs · 33,764 cycles

SHIP 3269 DISC: STRONG "DIRTY ODOR " FOUND UPON ENTERING A/C APU & APU BLEED WAS ON. CONTACTED MX. C/A: PERFORMED INSP OF APU FOUND INLET CONTAMINATED WITH OIL. APU PUT ON MEL LOG PAGE 5335417. PERFORMED SMOKE AND/OR OIL SMELL IN CABIN PROCEDURE PER A320 TSM 71-00-00-810-802-A.PERFORMED ECS DECONTAMINATION PER A320 AMM 21-00-00-615-802-A. REPLACED RECIRCULATION FAN FILTERS PER A320 AMM 21-21. CONF. WITH MCC OK FOR SERVICE. (LP: 5335416)

Part: O-RING — CUT (APU OIL SCAV FTR) · airframe 72,176 hrs · 33,732 cycles

SHIP 3269 DISC: WHEN ENTERING THE COCKPIT AT THE GATE @ MSP STRONG "DIRTY SOCK " SMELL THROUGHOUT THE AIRCRAFT. CAPT/FO/MX ALL VERIFIED THE SMELL. POSSIBLE APU OIL LEAK ISSUE. C/A: FOUND ORING CUT ON APU OIL SCAVENGE FILTER HOUSING USING BLACK LIGHT NO OTHER EXTERNAL LEAKS FOUND. REPLACED ORING LEAK CHECK GOOD WASHED APU AND CHANGED CABIN FILTERS DURING PACK BURNOUT, DIRTY SOCK SMELL STILL PRESENT SUSPECT #2 ENGINE. WIP 126605. PERFORMED BORESCOPE PER AMDS 7900-2001 STEPS 14 + 19, OIL WETTING FOUND ENGRG NOTIFIED QC1971. REF LP# 0367027 #2 ENG REMOVED AND REPLACED. STILL REQUIRES ECS DECONTAMINATION WIP 627229. COMPLETED LEVEL A DECONTAMINATION OF ECS PER A320 AMM 21-00-00-615-802-A OK FOR SERVICE. (LP: 5343872)

Part: ELECTRICAL BOX — ODOR (SEAT 20F) · airframe 72,026 hrs · 33,653 cycles

SHIP 3269 - DIV - TO CVG DUE TO ELECTRICAL SMELL IN CABIN. CORRECTIVE ACTION: FOUND SMELL COMING FROM SEB UNDER SEAT 20F. ALSO FOUND PED POWER MODULE INOPERATIVE UNDER SEAT 20E. R/R BOTH SEB AND PED. OPS CHECK GOOD.

Part: WEB — CRACKED (FRM 68 S22R) · airframe 71,798 hrs · 33,526 cycles

RIGHT FUSELAGE AT FR68 STGR 22RH FOUND WEB HORIZONTAL FLANGE CRACKED. C/W STEPS 1-17 AS PER PRI ER/A 616977-14AD C CANTERO 2047692 Q814 2569442 AWAITING PANEL. ALL STEPS COMPLIED AS PER PRI ER/A 616477-14D ORININAL.

Part: WEB — CRACKED (FRM 68 S22L) · airframe 71,798 hrs · 33,526 cycles

L/H FUSELAGE AT FR 68 STGR 22LH FOUND WEB HORIZONTAL FLANGE CRACKED (836-09). COMPLETED STEPS 1-12 AS PER PRI ER/A 616986-14AD REV 00 JJIMENEZ 1764669 Q814 2569442 WAITING FINAL. RECEIVED FINAL ERA 616986- 14AD ALL STEPS OF PRI MATCHES INSTRUCTION OF ERA REV ORIGINAL.

Part: NONE — NONE (NONE) · airframe 71,798 hrs · 33,526 cycles

DAMAGE TOLERANCE EVALUATION (DTE) REQUIRED FOR REPAIR INSTALLED AT FR68RH AND DOOR STOP 1 PER ER/A 616977-14AD. REF ER/A 616977-14AD.

Part: NONE — NONE (NONE) · airframe 71,777 hrs · 33,514 cycles

SHIP 3269 DISC: ER/A 616986-14AD ISSUED FOR REPAIR INSTALLED AT FR68LH AND DOOR STOP 1. FOLLOW ON ACTION IS REQUIRED. C/A: REF. ER/A 616986-14AD. (LP: 0286990)

Part: NONE — NONE (NONE) · airframe 71,777 hrs · 33,514 cycles

SHIP 3269 DISC: DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D AT FR68LH AND DOOR STOP 1 PER ER/A 616986-14AD. LH FR68 AT STGR22 RADIAL FLANGE FILLET LOWER RADIUS - CRACK. C/A: REF. ER/A 616986-14. (LP: 0286985)

Part: NONE — NONE (NONE) · airframe 71,777 hrs · 33,514 cycles

SHIP 3269 DISC: DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D AT FR68LH, DOOR STOP 1 PER ER/A 616986-14AD. / FUSELAGE / LH FR68 AT STGR22 RADIAL FLANGE FILLET LOWER RADIUS - CRACK. C/A: REF. ER/A 616986-14AD. (LP: 0286974)

Part: NONE — NONE (NONE) · airframe 71,777 hrs · 33,514 cycles

SHIP 3269 DISC: DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D AT FR68LH AND DOOR STOP 1 PER ER/A 616986-14AD. LH FR68 AT STGR22 RADIAL FLANGE FILLET LOWER RADIUS - CRACK. C/A: REF. ER/A 616986-14AD. (LP: 0286980)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,713 hrs · 32,942 cycles

SHIP 3269 O2 MASK AT F/A STATION 2L FELL. CORRECTIVE ACTION: REINSTALLED O2 MASK IAW A320 AMM 35-21. OK FOR SERVICE. (9629247)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,523 hrs · 32,859 cycles

SHIP 3269 DAMAGE FR 36-37 ABOVE STRG 6LH. AD 2021-17-03 RELATED. CORRECTIVE ACTION: COMPLIED WITH ERA 597371-14 REV O. (4480471)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,850 hrs · 32,494 cycles

SHIP 3269 - ATO - AT LESS THAN 5 KNOTS DUE TO F/CTL SEC 2 FAULT ECAM MSG. CORRECTIVE ACTION: RESET PER QRH AND REINITIATED TAKEOFF CONFIGURATION WITH NO FAULTS. OK TO CONTINUE. (4954538)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,775 hrs · 32,457 cycles

AIRCRAFT 3269, ON SVC CHK FOUND BOTH LH EMERG. EXIT HATCH HANDLE LIGHTS INOP. CORRECTIVE ACTION: RELAMPED BOTH LH DOOR HANDLE LIGHTS. (LP 4832589)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,775 hrs · 32,457 cycles

SHIP 3269 - ATB/FCNT - DUE TO AIRCRAFT PITCHING UP WITH AUTO PILOT OFF. AIRCRAFT REQUIRED CONSTANT DOWN PRESSURE TO MAINTAIN ATTITUDE AND WERE UNABLE TO MANUALLY TRIM THE PITCH VIA THE TRIM WHEEL. CORRECTIVE ACTION: REPLACED ELAC-2, PITCH TRIM ACTUATOR, AND THS ACTUATOR. (LP 4732580)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,706 hrs · 32,420 cycles

SHIP 3269 2L DOOR WONT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM DOOR ARMING AREA. OPS CHECK GOOD. (4732538)

Part: NONE — NONE · airframe 68,630 hrs · 31,794 cycles

SHIP 3269 ENTRY DOOR HARD TO OPEN OR CLOSE / LOCATIONS:601. CORRECTIVE ACTION: CLEANED FLOOR FITTING AND CYCLED DOOR CKS GOOD PER A320 AMM 52-10. OK FOR SERVICE. (2627523)

Part: ADIRU — FAULTED · airframe 66,817 hrs · 30,781 cycles

SHIP 3269 - ATB - DUE TO FLIGHT CONTROL AND NAVIGATION FAULTS RELATED TO FAILURE OF ADIRU 3 WITH ADIRU 2 ALREADY ON MEL. CORRECTIVE ACTION: REPLACED ADIRU 2 DC PWR SHED RELAY 17FB AND ADIRU 3. OPS TEST GOOD. (8832091)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 FABRICATE AND REPLACE FLOOR BEAM -Y1292 LOC FR64 TO FR 66 AT AFT GALLEY AREA . (CORROSION) CORRECTIVE ACTION: COMPLIED WITH ER/A 597570-14 REV. ORIGINAL. (2177788)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION OUTBOARD FLAP ECCENTRICAL BEARING CORE ON TRACK 4 OF RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 597971-14 REV. ORIGINAL. (2178393)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 WEAR ON ATTACHMENT BRACKET AILERON INBD ACTUADOR FIXED BUSHING OUTBD LUG ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 597695-14 REV. ORIGINAL. (2178785)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 WEAR ON ATTACHMENT BRACKET AILERON OUTBD ACTUATOR FIXED BUSHING OUTBD LUG ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 597695-14 REV. ORIGINAL. (2178315)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 WINDSHIELD FRAME AND CONTINUITY FITTING LH AND RH AT FRAME 2 TO FRAME 4 COCKPIT NEEDS REPLACING. CORRECTIVE ACTION: COMPLIED WITH ERA 597259-14AD REV. ORIGINAL. (2178518)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 WEAR ON ATTACHMENT BRACKET AILERON INBD ACTUADOR FIXED BUSHING OUTBD LUG ON LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 597695-14 REV. ORIGINAL. (2178775)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION OB FLAP ECCENTRICAL BEARING BORE ON TRACK 3 OF LH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 598067-14 REV. ORIGINAL. (2177778)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 MISSING BUSHING ACTUATOR FITTING KEEL BEAM FWD LUG , UPPER POSITION , R H SIDE IN MAIN WHEEL WELL. CORRECTIVE ACTION: COMPLIED WITH ER/A 597519-14AD REV ORIGINAL. OK FOR SERVICE. (2177777)

Part: WINDOW FRAME — CRACKED · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT AREA CONTINUITY FITTING RH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 597259-14AD REV. ORIGINAL. (2176502)

Part: WINDOW FRAME — CRACKED · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT AREA CONTINUITY FITTING LH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 597259-14AD REV. ORIGINAL. (2176481)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL AREA STARTING FROM UPPER TENSION BOLT RH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 597258-14AD REV. ORIGINAL. (2177023)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL AREA STARTING FROM UPPER TENSION BOLT LH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 597258-14AD REV. ORIGINAL. (2177019)

Part: FRAME — CRACKED · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATIONS FOUND ON FRAME 20 LH SIDE FROM HOLE A, LOCATED AT THE SECOND ROW FROM EDGE AND SECOND HOLE FROM LOWER TO UPPER IN COCKPIT AREA. CORECTIVE ACTION: COMPLIED WITH ERA 545995-14AD REV. B. (2176342)

Part: FRAME — CRACKED · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATION ON FRAME 20 LH SIDE FROM FASTENER LOCATED ON THE SECOND ROW AFTER EDGE AND FOURTH FROM UP TO DOWN. CORRECTIVE ACTION: COMPLIED WITH ERA 545995-14AD REV. B. (2176497)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATION ON RH WINDSHIELD STRUCTURE FROM HOLE LOCATED 29 INCHES FROM BL 0 AT FRAME 4 UPPER ATTACHMENT AREA IN COCKPIT. CORRECTIVE ACTION: COMPLIED WITH ER/A 597258-14AD REV. ORIGINAL. (2176989)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK MAIN DOOR ON RH MAIN LANDING GEAR. CORRECTIVE ACTION: COMPLIED WITH ER/A 597548-14 REV ORIGINAL. (2177226)

Part: ANGLE — CRACKED · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK ANGLE FITTING, FRAME FOOT L/H. CORRECTIVE ACTION: REPLACED ANGLE FITTING FRAME FOOT LH SIDE PER A320 SRM 51-72-11. (2175553)

Part: FRAME — CRACKED · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATION FOUND ON FRAME 16 RH SIDE HOLE 6 LOCATED AT THE FIRST ROW FROM EDGE AND THIRD FROM UPPER TO LOWER IN A COCKPIT. CORRECTIVE ACTION: COMPLIED WITH ER/A 596201-14 REV.ORIGINAL. (2175547)

Part: SUPPORT — CORRODED · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION INTERNAL STRUCTURE INTERCOSTAL SUPPORT LOCATED BETWEEN FR64 TO FR65 AND STR44 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERCOSTAL SUPPORT PER A320 SRM 51-42-11 AND 51-72-11. (2175938)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 NEED TO COMPLY WITH DTA MONITOR INSPECTION LOG REFERENCE ER/A 597259-14 (CRACK) CORRECTIVE ACTION: COMPLIED WITH ERA. (2173525)

Part: SKIN — CORRODED · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION INTERNAL SKIN LOCATED BETWEEN FR65 TO FR66 AND FROM STR31R TO STR32R IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ER/A 597903-14 REV ORIGINAL (2174703)

Part: FRAME — CRACKED (FRM 20) · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATIONS FOUND ON FRAME 20 RH SIDE FROM HOLE D LOCATED AT THE FIRST ROW FROM EDGE AND FIRST HOLE LOWER TO UPPER IN COCKPIT. CORRECTIVE ACTION: COMPLIED WITH ERA 597318-14 REV ORIGINAL. (2174486)

Part: FRAME — CRACKED (FRM 20) · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATION FOUND ON FRAME 20 RH SIDE FROM HOLE 6 LOCATED AT THE FIRST ROW FROM EDGE AND THIRD FROM UPPER TO LOWER IN COCKPIT. CORRECTIVE ACTION: COMPLIED WITH ERA 597318-14 REV ORIGINAL. (2174481)

Part: SKIN — CRACKED (FRM 36) · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATION ON SKIN LOCATED AT FR 36 PLUS 9 INCHES AND ABOVE STR 6 LH ON BAY POCKET. CORRECTIVE ACTION: COMPLIED WITH ER/A 597371-14AD REV ORIGINAL. (2173138)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 FAA - AAI FINDING - DURING INSPECTION OF REPAIR PER ER/A 546005- 14AD FOUND THAT FASTENER SPACING / FASTENER COUNT DOES NOT MATCH THE FIGURE AND INSTRUCTIONS PER ER/A IN CENTER FUEL TANK. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON TOP SKIN PANEL EXTERNAL SURFACE ON CENTER WING TANK AS PER ER/A 546005-14 REV A. (2173134)

Part: FRAME — CRACKED (FRM 16) · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CRACK INDICATIONS FOUND ON FRAME 16 LH SIDE FROM HOLE LOCATED AT THE SECOND ROW FROM EDGE AND THE FIRST HOLE FROM LOWER TO UPPER IN COCKPIT. CORRECTIVE ACTION: COMPLIED WITH ER/A 597199-14AD REV ORIGINAL. (2173120)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 NEED TO COMPLY WITH DTA MONITOR INSPECTION LOG REFERENCE ER/A 597258-14 (CRACK). CORRECTIVE ACTION: COMPLIED WITH ERA. (2173489)

Part: NONE — CORRODED (FRMS 33-34) · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION INTERNAL STRUCTURE WEB LOCATED BTW FR33 TO FR34 AT LEVEL STR 38R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL WEB PER A320 SRM 51-72-11. (2171959)

Part: SKIN — CRACKED (FRMS 36-37) · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 FUSELAGE / SKIN / SKIN PANEL AT LEVEL OF FR36-37 & STRG 6LH / CRACK AT SKIN POCKET EDGE. CORRECTIVE ACTION: COMPLIED WITH ERA 597371-14. (2172190)

Part: SKIN — CRACKED (FRMS 36-37) · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 FUSELAGE / SKIN / SKIN PANEL AT LEVEL OF FR36-37 & STRG 6LH / STRG 6LH / CRACK AT SKIN POCKET EDGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 597371-14AD. (2172185)

Part: STRINGER — CORRODED (FRMS 29-30 S41R) · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION STRINGER 41R LOCATED BTW FR29 TO FR30 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-21-13. OK FOR SERVICE. (2171956)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 INSPECT CORROSION PER ERA 598066-14. CORRECTIVE ACTION: COMPLIED WITH ERA 598066-14. (2169754)

Part: SHEAR TIE — CORRODED (FRM 28) · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION IN SHEAR TIE LOCATED FR28 BTW STR43R TO STR43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR PER A320 SRM 51-72-11-911-001. (2169357)

Part: SUPPORT — CORRODED (FRMS 16-20) · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION LOWER SILL LOC BTW FR16 TO FR20 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED LOWER SILL PER A320 SRM 51-72-11. (2169372)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM -Y1162 AT LEVEL OF FR68 AND STRG 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2167631)

Part: UNKNOWN — UNKNOWN · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 BENT INTERNAL STRUCTURE CROSSBEAM LOCATED FR27 BTW STR38L TO STR41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED CROSSBEAM PER A320 SRM 51-72-11. (2167624)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM +Y1292 LOC AT LEVEL FR16 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11 AND 51-42-11. (2167619)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION LOWER SILL LOCATED AT LEVEL OF FR66 AND STRG 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED LOWER SILL PER A320 SRM 5-42-11 AND 51-72-11. (2167654)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM -Y1292 LOCATED AT LEVEL OF FR66 AND STGR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2167651)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM -Y1225 LOCATED BTW FR67 TO FR68 AND STGR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2167637)

Part: UNKNOWN — UNKNOWN · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION WEB FRAME 20 RH SIDE AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB PER A320 SRM 51-42-11 AND 51-72-11. (2167642)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION OB FLAP EXCENTRICAL BEARING ON TRACK 3 AND TRACK 4 ON LH WING REFERENCE AMDS CARD 2750-6020-LT. CORRECTIVE ACTION: REPLACED BEARINGS PER DELTA WORK CARD AMDS 2750-6020-LT. (2166726)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 BENT SUPPORT ANGLE OF FRAME LOCATED FR55 AND BETWEEN STR41L TO STR43L AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SUPPORT ANGLES PER SRM A320 51-72-11 AND 51-42-11. (2166564)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION SHEAR TIE LOCATED FR33 BTW STR 43R TO STR 43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-42-11 AND 51-72-11. (2162818)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION SHEAR TIE LOCATED FR34 BTW STR 43R TO STR 43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11 AND 51-42-11. (2162824)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION SHEAR TIE LOCATED FR32 BTW STR 43R TO STR 43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS PER A320 SRM 51-42-11. (2162822)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION SHEAR TIE LOCATED FR31 BTW STR 43R TO STR 43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11 AND 51-42-11. (2162027)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION LOWER SILL CENTER FITTING LOC BTW FR16 TO FR20 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED LOWER SILL CENTER FITTING PER A320 SRM 51-72-11. (2160947)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION SHEAR TIE LOCATED FR31 BTW STR 39R TO STR 40R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11. (2160960)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION LOWER SILL CORNER FR20 LH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED CORNER FITTING PER A320 SRM 51-72-11. (2160747)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION SHEAR TIE LOCATED FR29 BTW STR 43R TO STR 43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11 AND 51-42-11. (2160957)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION LOWER SILL LOC FR16 TO FR20 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED LOWER SILL AND FASTENERS PER A320 SRM 51-72-11. (2160760)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 FUSELAGE / FRAME/FORMERS / FR16LH AT DOOR STOP NO 7 LEVEL / DOUBLE JOGGLE / HOLE C / CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 597199-14. (2158542)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM +Y765 AT LEVEL FR16 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2155474)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM -Y765 LOC FR20 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2153328)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION LOWER SILL CENTER FITTING LOC BTW FR16 TO FR20 RH SIDE IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED CENTER FITTING PER A320 SRM 51-72-11. (2147426)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION SHEAR TIE LOCATED FR30 BTW STR42R TO STR41R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS PER SRM 51-72-11 AND 51-42-11. (2146499)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION STRINGER SPLICE 43R LOCATED BTW FR27 TO FR28 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SPLICE PER A320 SRM 51-72-11. (2146284)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION CENTER FITTING LOCATED BTW FR66 AND FR68 AND STGR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED CENTER FITTING AS PER A320 SRM 51-72-11. (2146501)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION LOWER SILL LOCATED BTW FR66 TO FR68 AND STRG 23 LH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED LOWER SILL PER A320 SRM 51-72-11. (2144162)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM -Y1292 LOC BTW FR16 TO FR21 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2144170)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM -Y254 LOC BTW FR16 TO FR20 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2144164)

Part: NONE — NONE · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 IMPROPERLY PACKED SLIDE RAFT PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SLIDE RAFT. OK FOR SERVICE. (2142061)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR STRUCTURE WEB LOCATED BTW FR69 TO FR70 AND STRG 23RH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE WEB PER A320 SRM 51-72-11. (2142689)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM +Y1162 AT LEVEL OF FR68 AND STRG 23LH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2141539)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM +Y1225 BTW FR67 TO FR68 AND STGR 23LH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2141535)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR STRUCTURE WEB LOCATED FROM FR69 TO FR70 AND STRG23 LH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR STRUCTURE WEB PER A320 SRM 51-72-11. (2140075)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM -Y465 LOCATED AT LEVEL OF FR68 AND STGR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2140082)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM +Y254 AT LEVEL FR20 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2138889)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM +Y765 AT LEVEL FR68 AND STRG 23LH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 53-41-14 AND 51-72-11. (2138087)

Part: NONE — NONE · corrosion level 2 · airframe 66,203 hrs · 30,424 cycles

SHIP 3269 CORROSION FLOOR BEAM -Y765 AT LEVEL FR68 AND STGR 23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 53-41-14 AND 51-72-11. (2134434)

Part: NONE — NONE · airframe 65,758 hrs · 30,163 cycles

SHIP 3269 ER/A 572550-14 HAS BEEN REVISED TO 'A'. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH REVISION IN ERA 572550-14 (LIGHTNING STRIKE DAMAGE) (1998118)

Part: NOT REPORTED — NOT REPORTED · airframe 65,496 hrs · 29,990 cycles

SHIP 3269 DURING ALI INSP OF FWD CARGO DOOR CUTOUT FOUND POSSIBLE DAMAGE ON FR24A NEAR BOTTOM OF CUTOUT. SSI 532135-02-1 CARD 5321-2016. CORRECTIVE ACTION: COMPLIED WITH ERA 594800-14 REV ORIGINAL. (1990823)

Part: NONE — NONE · airframe 65,409 hrs · 29,930 cycles

SHIP 3269 CRACK INDICATIONS LEFT FR 16 FITTING 7 HOLE # 1. CORRECTIVE ACTION: COMPLIED WITH ERA 594387-14 REV O. (1965309)

Part: NONE — NONE · airframe 65,409 hrs · 29,930 cycles

SHIP 3269 CRACK INDICATIONS RIGHT FR 16 FITTING 7 HOLE #3. CORRECTIVE ACTION: COMPLIED WITH ERA 594388-14 REV O. (1965313)

Part: NONE — NONE · airframe 65,409 hrs · 29,930 cycles

SHIP 3269 CRACK INDICATIONS RIGHT FR 16 FITTING 7 HOLE # 1. CORRECTIVE ACTION: COMPLIED WITH ERA 594388-14 REV O. (1965311)

Part: NONE — NONE · airframe 65,409 hrs · 29,930 cycles

SHIP 3269 FORWARD LEFT PASSENGER DOOR HAS CRACK INDICATIONS AT LEFT FR 16 FITTING 7 HOLE # 3. CORRECTIVE ACTION: COMPLIED WITH ERA 594387-14 REV O. (1965390)

Part: PSU — NO TEST (SEAT 20ABC) · airframe 64,473 hrs · 29,369 cycles

SHIP 3269 SEAT 20ABC PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7483561)

Part: PANEL — INOPERATIVE (SEAT 17DEF) · airframe 64,464 hrs · 29,365 cycles

SHIP 3269 SEAT 17DEF PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7483560)

Part: LIGHT — BROKEN (SEAT 14D) · airframe 64,464 hrs · 29,365 cycles

SHIP 3269 EMER EXIT LIGHT ON THE BOTTOM OF SEAT 14D IS BROKEN. CORRECTIVE ACTION: SECURED LOOSE LIGHT HOLDING TRIM PER A320 AMM 33-52. LIGHT WORKS. (7483556)

Part: SLIP JOINT — DETACHED (ACM) · airframe 63,908 hrs · 29,112 cycles

SHIP 3269 - DIV - TO GSP DUE TO LOSS OF PRESSURIZATION. O2 MASKS DID NOT DEPLOY. PACK 2 ALREADY ON MEL. CORRECTIVE ACTION: DEFERRED AUTO PRESSURE CONTROL PER MEL 21-31-01A AND FERRIED TO ATL. FOUND PACK 1 SLIP JOINT FROM PRIMARY HEAT EXCHANGER TO ACM PARTIALLY OFF DUCT. FLOW CONTROL VALVE HAS HEAVY INTERNAL BYPASS. RE-SECURED CONNECTION PER A320 AMM 21-51. OPS CHECK OK.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 63,874 hrs · 29,092 cycles

SHIP 3269 ENROUTE TO KCLE @ FL350 WHILE OPERATING ON A SINGLE PACK, CABIN ALTITUDE EXCEEDED 9000' WITH A CABIN DIFFERENTIAL OF 8.6. DECENDED TO FL 310 AND CABIN ALTITUDE CONTINUED TO CLIMB TO A MAX ALTITUDE OF 9500 FEET. DESCENDED TO FL 250 AND CABIN ALTITUDE RETURNED TO NORMAL VALUES. CORRECTIVE ACTION: R&R CPC PER A320 AMM 21-31. OPS CK GOOD AFTER PART REPLACEMENT. (7689030)

Part: LIGHT — DAMAGED (SEAT 14D) · airframe 63,812 hrs · 29,066 cycles

SHIP 3269 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS: SEAT 14D. CORRECTIVE ACTION: RESECURED EMERGENCY SEAT LIGHT AT 14D. OK FOR SVC. (1736343)

Part: ARMING LEVER — DRAGGING (ENTRY DOOR) · airframe 63,719 hrs · 29,024 cycles

SHIP 3269 ENTRY DOOR ARMING LEVER HARD TO OPERATE AT LOCATIONS 608. CORRECTIVE ACTION TIGHTENED HANDLE. OPS CHK OK.

Part: PSU — NO TEST (SEAT 14ABC) · airframe 63,670 hrs · 28,999 cycles

DURING TEST PSU/O2 PANEL IN SEAT 14ABC DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE.

Part: PSU — NO TEST (SEAT 18ABC) · airframe 63,670 hrs · 28,999 cycles

DURING TEST PSU/O2 PANEL IN SEAT 18ABC DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE.

Part: PSU — NO TEST (SEAT 23FED) · airframe 63,670 hrs · 28,999 cycles

DURING TEST PSU/O2 PANEL IN SEAT 23FED DID NOT DROP. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE.

Part: DOOR — NO TEST (SEAT 27ABC PSU) · airframe 63,708 hrs · 29,018 cycles

SHIP 3269 DURING TEST FOUND SOLENOID WAS BAD AT THE PSU AT SEAT 27ABC. CORRECTIVE ACTION: R & R OVERHEAD PASSENGER OXYGEN ASSEMBLY PER A-320 AMM 35-21. OPS CK GOOD.

Part: RELEASE MECH — OUT OF ADJUST (R2 DOOR) · airframe 63,462 hrs · 28,907 cycles

AT CRUISE 2R DOOR SHOWS DISARMED ON FLT DECK ECAM. CORRECTIVE ACTION: REMOVED AND STOWED LOCK PIN FROM R2 DOOR SLIDE REGULATOR VALVE ASSEMBLY, PER A320 AMM 25-62. VERIFIED R2 DOOR SLIDE REGULATOR SAFETY PIN REMOVED AND STOWED, IAW AMM 25-62. ADJUSTED RELEASE MECHANISM OF THE EMERGENCY SLIDE, PER A320 AMM 52-13. MCO PLACARD REMOVED. NO M PROCEDURES AC. OK FOR SERVICE.

Part: LANYARD — OUT OF POSITION (R2 GIRT BAR) · airframe 63,449 hrs · 28,898 cycles

2R DOOR ARM DISARM SYSTEM NOT WORKING PROPERLY. CORRECTIVE ACTION: REPOSITIONED LAYNARD ON GIRT BAR AND CLEANED. OPERATIONS CHECKS GOOD, PER A-320 AMM- 52-73-00.

Part: LATCH — DIRTY (GIRT BAR) · airframe 63,439 hrs · 28,893 cycles

2R DOOR SHOWS UNARMED INFLIGHT UNLESS HELD DOWN. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR LATCHES. PERFORMED OPERATIONAL TEST OF 2R DOOR WARNING SYSTEM, PER A320 AMM 52-73-00. OPERATIONS CHECK OK.

Part: ARMING LEVER — MALFUNCTIONED (R2 DOOR) · airframe 63,365 hrs · 28,854 cycles

DURING CRUISE R2 DOOR SLIDE ARMING HANDLE DISARMED AND WON'T REARM DOOR INDICATOR CLOSED AND PRESSURIZATION NORMAL. CORRECTIVE ACTION: PERFORMED OPERATIONS CHECK, NO DEFECTS NOTED UPON TEST.

Part: FRAME — DAMAGED (FRM 36) · airframe 63,334 hrs · 28,839 cycles

BOLT HOLES NEEDED COLD WORKING ( 2EA) HOLE LOCATED ON FRAME 36 RT SIDE INTERFACING LONGITUDINAL BEAM AND PRESSURE PANEL. CORRECTIVE ACTION: PERFORMED COLD EXPANSION IN OPEN (2 EA) HOLE LOCATED ON FRAME 36 RT SIDE INTERFACING LONGITUDINAL BEAM AND PRESSURE PANEL. OK FOR SERVICE.

Part: FRAME — DAMAGED (FRM 36) · airframe 63,334 hrs · 28,839 cycles

BOLT HOLES (2 EA) NEEDED TO BE COLD WORKED AT FRAME 36 LT SIDE INTERFACING LONGITUDINAL BEAM AND PRESSURE PANEL. CORRECTIVE ACTION: COLD WORKED BOLT HOLES AT FRAME 36 LT SIDE INTERFACING LONGITUDINAL BEAM AND PRESSURE PANEL. OK FOR SERVICE.

Part: LIGHT — DETACHED (SEAT 17D) · airframe 62,858 hrs · 28,601 cycles

17D SEAT MOUNTED FLOOR PROXIMITY LIGHT BROKEN OFF, INSTALLED NEW LIGHT ASSY

Part: EPSU — FAULTED (CABIN) · airframe 62,798 hrs · 28,569 cycles

DURING SVC FOUND L EPSU FAULTING, REPLACED L EPSU W/ BATTERY.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 61,690 hrs · 27,985 cycles

GALLEY CLOSET SIDE WALL EMER. LIGHT MISSING COVER, REPLACED FWD GALLEY CLOSET WALL EMERGENCY LIGHT COVER

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,447 hrs · 27,857 cycles

RT FORWARD AND AFT OVERWING EXIT DOOR PULL HANDLE LIGHTS HAVE BULBS INOP, RELAMPED RT FORWARD AND AFT OVERWING EXIT DOOR PULL HANDLE LIGHTS.

Part: SKIN — DAMAGED (AFT CARGO DOOR) · airframe 64,983 hrs · 29,675 cycles

SHIP 3269 DAMAGE ON SKIN LOWER AFT CORNER OF AFT CARGO DOOR. CORRECTIVE ACTION: COMPLIED WITH GENERAL VISUAL INSPECTION OF SKIN ON LOWER AFT CORNER OF AFT CARGO DOOR AS PER A320 SRM 53-41-11. OK AT THIS TIME. CONTINUE ON MONITOR. (5542517)

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 58,364 hrs · 26,357 cycles

FINAL APPROACH, AFTER GEAR EXTENSION, GOT MASTER CAUTION WITH BL SYS LO PRES INDICATION. FOLLOWED QRH/ECAM PROCEDURE. DECLARED EMERGENCY. MAINTENANCE TROUBLESHOT. REPLACED O-RING ON PLUG FOR BLUE HIGH PRESSURE MANIFOLD. LEAK CHECKS GOOD. CLEANED APU INLET AND COMPARTMENT.

Part: BOTTLE — LOW PRESSURE (LT OVRWG SLIDE) · airframe 58,159 hrs · 26,262 cycles

LOW PRESSURE FOR THE OVERWING SLIDE RESERVOIR, LEFT SIDE, REMOVED AND REPLACED RESERVOIR.

Part: LENS — DAMAGED (EMERGENCY LIGHTS) · airframe 55,283 hrs · 24,950 cycles

EMERGENCY LIGHT LENS DAMAGED. REPLACED THE LENS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,580 hrs · 24,198 cycles

CABIN EMERGENCY ROW EXIT LIGHTS AND EMERGENCY ISLE LIGHTS ILLUMINATED W/EMER EXIT LIGHT SWITCH IN AUTO. ONLY SOME LIGHTS ILLUMINATED MIDDLE OVERHEAD EXIT SIGN AND EXIT SIGNS AT 1., 1R, 2L/2R ILOLUMINTED. SOME PATHWAY LIGHTS ALSO, REPLACED EPSU 12WL W/O BATTERY

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,552 hrs · 24,185 cycles

EMERGENCY EXIT LIGHTS OVERWINGS ON - OFF DURING FLIGHT. STOPPED THEN OFF & ON AFTER LANDING, REPLACED THE RELAY 8WL ON 103VU.

Part: SKIN — CRACKED (LT AILERON) · airframe 53,283 hrs · 24,056 cycles

LEFT AILERON UPPER SKIN CRACKED. REPAIRED PER ERA 549842-14

Part: SKIN — DAMAGED (FRAMES 42-) · airframe 52,187 hrs · 23,548 cycles

CORROSION FOUND ON WING CENTER TANK TOP SKIN EXTERNAL SURFACE BETWEEN FRAME 42 AND STR 16, RIB 1 DATUM AND 1292. PERMANENT REPAIR ON UPPER SKIN BETWEEN FRAME 41 TO FRAME 42 AND 1292 TO 1732 PASSENGER CABIN ON CENTER WING BOX IAW ERA 546005-14AD REVISION ORIGINAL.

Part: WEB — CORRODED (FRAMES 42-43) · airframe 52,187 hrs · 23,548 cycles

CORROSION FOUND ON CENTER FUSELAGE LT SIDEBOX SHELL UPPER PLATE WEB PANEL BETWEEN FRAME 42-43, PERMANENT REPAIR ON SIDE BOX UPPER SURFACE BETWEEN FRAME 42 AND FRAME 43 LT SIDE IN PASSENGER CABIN IAW PRI 546001-14, REV 0 AND ER/A 546001-14, REV B.

Part: SEAT TRACK — CORRODED (FRAMES 12-24) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON SEAT TRACK -765 FOUND OUT LIMITS IN PASSENGER CABIN FROM FRAMES 12 - 24, REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53110900 AND D53110984.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON SHEAR TIE FRAME 31 BETWEEN STR 40 - 42R IN FWD CARGO BAY. REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DWG NR D53231712 AND D53231586.

Part: FLOOR SUPPORT — CORRODED (FRAME 16-20) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOORBEAM 1292 LOCATED BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA, REPLACED FLOORBEAM 1292 LOCATED BETWEEN FRAME 12 TO FRAME 24 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWGS D53112812 AND D53110900.

Part: WEB — CORRODED (FRAME 20) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON WEB ON FLOOR STRUCTURE AT LEVEL STR 23L, FRAME 20 AT FWD GALLEY AREA, REPLACED WEB ON FLOOR STRUCTURE AT LEVEL STR 23L, FRAME 20 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53112784.

Part: WEB — CORRODED (FRAMES 20) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON WEB ON FLOOR STRUCTURE AT LEVEL STR 23R AND FRAME 20 AT FWD GALLEY AREA REPLACED WEB ON FLOOR STRUCTURE AT LEVEL STR 23R AND FRAME 20 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53112784.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOORBEAM 1162 BETWEEN FRAME 68 TO FRAME 69 AT AFT GALLEY AREA. REPLACED FLOORBEAM 1162 BETWEEN FRAME 68 TO FRAME 69 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472780 MEASURES OF REWORKED AREA: L=5.054", W=2.132", D=0.041".

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON LOWER SILL LOCATION FRAME 66 TO FRAME 68 RT SIDE AT AFT GALLEY AREA . REPLACED LOWER SILL LOCATED FRAME 66 TO FRAME 68RT SIDE AT AFT GALLY AREA IAW SRM 51-72-11 AND DWG D53480019.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON LOWER SILL LOCATION FRAME 66 TO 68 LT SIDE AT AFT GALLEY AREA, REPLACED FLOOR SILL LOCATION FRAME 66 TO 68 LT SIDE AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOOR SUPPORT 1589 BETWEEN FRAMES 65 TO 66 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53474250.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOOR SUPPORT 1589, FRAMES 65 TO 66 IN AFT GALLEY. REWORKED AND EVALUATED OUT OF LIMITS IAW SRM 53-00-14, TABLE 101, PARA 4.B, FIG 102, SHEET 1. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53474250.

Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOORBEAM 1162 BETWEEN FRAME 68 TO FRAME 69 AT AFT GALLEY AREA. REPLACED FLOOR BEAM 1162 BETWEEN FRAME 68 TO FRAME 69 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472780.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOORBEAM 1225 BETWEEN FRAME 66 TO FRAME 68 AT AFT GALLEY AREA L=1.256", W=0.978", D=0.004". REPLACED FLOORBEAM 1225 BETWEEN FRAME 66 TO FRAME 68 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472780, MEASURES OF REWORKED AREA: L=1.790", W=1.180", D=0.060".

Part: FITTING — CORRODED (FRAME 68) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON CORNER FITTING FRAME 68 LT SIDE AT AFT GALLEY AREA. REPLACED CORNER FITTING FRAME 68 LT SIDE AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOORBEAM 465, FRAME 64 TO FRAME 66 AT AFT GALLEY AREA L= 1.300", W=0.786", D=0.005". REPLACED FLOORBEAM 465 LOCATED, FRAME 64 TO FRAME 67+10 AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53472816; MEASURES OF CORROSION ARE L=1.315", W=1.000", D=0.007".

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOORBEAM +1292 LOCATION BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA, REPLACED FLOORBEAM +1292 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53110920.

Part: FRAME — CRACKED (FRM 68) · airframe 52,187 hrs · 23,548 cycles

CRACK SECTION FRAME 68 AND STR 23L ON CROSSBEAM AT AFT GALLEY AREA, REPLACED SECTION FRAME 68 LOCATED AT STR 23L ON CROSSBEAM AT AFT GALLEY AREAS IAW SRM 51-72-11, SRM 51-42-11, D53474250, MEASURES OF CRACK IS L=0.350".

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOORBEAM -Y765, LOC FR 66 TO FR 70 AT AFT GALLEY AREA, L=2.500", W=1.500", D=0.005, REPLACED FLOORBEAM 765 LOCATED BETWEEN FRAME 66 TO FRAME 70 AT AFT GALLEY AREA SRM 51-72-11, DWS D53472093 AND D53472780, REWORKED AREA MEASURES L=1.931", W=1.333", D=0.033".

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOORBEAM 254 LOCATED BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA, REPLACED FLOORBEAM 254 LOCATED BETWEEN FRAME 16 TO FRAME 20 AT FWD GALLEY AREA IAW SRM 51-72-11 AND DWG D53110984.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON FLOOR SUPPORT -254 BETWEEN FRAMES 16 TO 20. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53111461.

Part: DUMMY RAIL — CORRODED (FRAMES 12-16) · airframe 52,187 hrs · 23,548 cycles

CORROSION ON RAIL DUMMY Y503.2 BETWEEN FRAME 12 TO FRAME 16 AT FWD GALLEY AREA. REPLACED RAIL DUMMY Y503.2 LOCATED BETWEEN FRAME 12 TO FRAME 16 AT FWD GALLEY ARE AS IAW SRM 51-72-11 AND DWG D53112825.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,110 hrs · 23,505 cycles

FWD LT EMERGENCY LIGHTS PSU FAILED SELF TEST, UNIT FAULT LIGHT ON. REPLACED EPSU IAW AMM 33-51. TEST PASSED. OPS NORMAL.

Part: STRINGER — CORRODED (FAMES 56-57) · airframe 51,941 hrs · 23,429 cycles

CORROSION ON STRINGER 43L BETWEEN FRAMES 56-57. R & R BAD PORTION OF S43L BETWEEN FR 55 AND 58 IAW SRM 53-00-13, FIG 201.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 51,941 hrs · 23,429 cycles

EMERGENCY LIGHTS INOPERATIVE ON SEAT ROWS 5, 7, AND 22, FOUND LOOSE CONNECTOR AT SEAT 7 AND 22. REPLACED LIGHT ASSY AT ROW 5.

Part: WIRE HARNESS — UNSECURE (EMERGENCY LIGHTS) · airframe 47,879 hrs · 21,535 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT WIRE HARNESS UNSECURED ON SEAT ROWS 6AB AND 7 AB. MAINTENANCE SECURED EMERGENCY LIGHT WIRE HARNESS AT SEAT ROWS 6AB AND 7 AB AND FUNCTIONAL CHECK WAS NORMAL.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 45,149 hrs · 20,269 cycles

DURING INSPECTION, FOUND SEAT ROW 2AB EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND LOOSE CONNECTOR. SECURED CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL.

Part: CONNECTOR — FAILED (TE FLAPS) · airframe 44,311 hrs · 19,863 cycles

DURING APPROACH FOR LANDING AND AFTER COMMANDING FLAPS 2 DEG, 30 SEC LATER FLT/CTL FLAPS FAULT APPEARED ON THE UPPER ECAM SCREEN. CREW FOLLOWED QRH PROCEDURE, DECLARED EMERGENCY AND LANDING WAS UNEVENTFUL. MAINTENANCE REPLACED CONNECTOR 7541VC, 7505VC, 7543VC AND 7503VC. LUBED RT FLAP SYS CARRIAGES, LT FLAP SYS AND FUNCTIONAL CHECK WERE NORMAL. ACFT RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,692 hrs · 18,602 cycles

DURING EMERGENCY LIGHTS TEST, FOUND EPSU BATTERY PACK RT MESSAGE. APPLIED TSM 33-51-00-810-802A. PERFORMED OPS TEST OF THE EMERGENCY LIGHT SYS. FAULT CONTINUES. PERFORMED OPS TEST OF THE BATTERY PSEU. BATTERY FAULT APPEARS. R & R BATTERY IAW AMM 33-51. TEST OK.

Part: EPSU — FAILED (EMERGENCY LIGHTS) · airframe 41,461 hrs · 18,503 cycles

DURING SERVICE CHECK, FOUND LEFT ESPU BATTERY FAIL TEST. MX REPLACED LT ESPU AND FUNCTIONAL CHECKED NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 40,997 hrs · 18,273 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 1B INOPERATIVE. MAINTENACE SECURED LIGHT ASSEMBLY AND FUNCTIONAL CHECKED NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,509 hrs · 18,046 cycles

EMERGENCY LIGHT TEST FAULTS EPSU BATTERY FORWARD LEFT. REMOVED AND REPLACED BATTERY PACK AT 10WL L-1 DOOR PER AMM 33-51-58. NOW TESTED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,396 hrs · 17,993 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 1B INOPERATIVE. MAINTENANCE REPAIRED ASSEMBLY AND RELAMPED. OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: STRUCTURE — DENTED (L2 DOOR) · airframe 40,381 hrs · 17,987 cycles

NR 2 LEFT MAIN ENTRY DOOR DENTED AT LOWER AFT CORNER. MAINTENANCE REMOVED DAMAGE AND FABRICATED REPAIR PARTS PER ERA 504635-14 REV O. PERFORMED DETAILED VISUAL INSPECTION. NO FURTHER DAMAGE NOTED. INSTALLED REPAIR AND RESTORED ACCESS PER SECT 2 PERM REPAIR ERA 504635-14 REV ORIG. ALL STEPS COMPLIED, ERA 504635-14 REV ORIG PERM REPAIR.

Part: EPSU — INOPERATIVE (CABIN) · airframe 5,622 hrs · 2,505 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT SYSTEM TEST FAULTS "EPSU EXIT LOAD L". MAINTENANCE REPLACED LT EPSU AND BATTERY PACK. FUNCTIONAL CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 36,866 hrs · 16,373 cycles

DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT ON SEAT 5C AND 6C INOPERATIVE. MAINTENANCE RECONNECTED BROKEN WIRE AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHT) · airframe 36,846 hrs · 16,362 cycles

DURING A NON ROUTINE CHECK, FOUND THE EPSU FAULTED FOR THE RIGHT AND LEFT EMERGENCY LIGHTS. MAINTENANCE REPLACED THE EPSU AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 36,411 hrs · 16,159 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT ROW 6C INOP. LOOSE CONNECTOR SECURED AND TESTS OK.

Part: CONNECTOR — LOOSE (CABIN) · airframe 36,411 hrs · 16,159 cycles

DURING EMERGENCY LIGHT TEST FOUND SEAT ROW 4B INOP. LOOSE CONNECTOR SECURED AND TESTS OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 35,722 hrs · 15,683 cycles

DURING NON A ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT L2 DOOR INOPERATIVE. MX REPLACED THE POWER SUPPLY AND LIGHT ASSY. FUNCTIONAL CHECK WAS NORMAL AND ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 35,488 hrs · 15,753 cycles

DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 5C AND 8C INOPERATIVE. MX RESECURED WIRING CONNECTORS AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 34,538 hrs · 15,340 cycles

PILOT REPORTED EMERGENCY PATH LIGHT AT SEAT 5C INOP, SECURED CONNECTOR AND CHECKS OK.

Part: SKIN — DENTED (FUSELAGE) · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND RIGHT FUSELAGE SKIN DENTED AT FR3. REPAIRED PER ERA 483384-14 & SRM 51-42-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON AFT CABIN RT FRAME SUPPORT BETWEEN FR69 & FR70. REPAIRED PER SRM 51-42-11 & SRM 51-44-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON R2 DOOR SILL AT FR 66. REPAIRED PER ERA 483379-14.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CLEAT CORRODED AT FR33 BETWEEN S41L & S42L. REPAIRED PER SRM 51-42-11 & SRM 51-44-11.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON AFT CABIN LT FRAME SUPPORT AT +Y1732 BETWEEN FR69 & FR70. REPAIRED PER SRM 51-42-11.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 131EF. REPLACED FLOOR PANEL PER DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 131AF. REPLACED FLOOR PANEL PER DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 151GF. REPLACED FLOOR PANEL PER DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 131HF. REPLACED FLOOR PANEL PER DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 151AF. REPLACED FLOOR PANEL PER DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 151DF. REPLACED FLOOR PANEL PER DWG 3D25-37705.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND DAMAGE TO FLOOR PANEL 261PF. FABRICATED AND REPLACED FLOOR PANEL PER DWG 3D25-37498.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON SEAT TRACK AT +Y1292 BETWEEN FR66 & FR68. REPAIRED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON SEAT TRACK AT +Y1292 BETWEEN FR68 & FR69. REPAIRED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON SEAT TRACK AT Y765 BETWEEN FR66 & FR70. REPAIRED PER SRM 51-42-11, SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON SEAT TRACK AT Y765 BETWEEN FR64 & FR66. REPAIRED PER SRM 51-44-11, SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON SEAT TRACK AT Y1292 BETWEEN FR66 & FR68. REPAIRED PER SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON SEAT TRACK AT Y1292 BETWEEN FR68 & FR69. REPAIRED PER SRM 51-42-11 & SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON SEAT TRACK AT +Y765 BETWEEN FR64 & FR66. REPAIRED PER SRM 51-42-11, SRM 51-44-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON SEAT TRACK AT Y765 BETWEEN FR66 & FR70. REPAIRED PER SRM 51-44-11, SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON SEAT TRACK AT +Y512 FR66. REPAIRED PER SRM 51-42-11, SRM 51-44-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION ON FLOOR SUPPORT AT Y1732 FR20. REPAIRED PER SRM 51-44-11, SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,150 hrs · 15,177 cycles

DURING M-CHECK FOUND CORROSION OF SEAT TRACK AT +Y503.2 FR16. REPAIRED PER SRM 51-42-11, SRM 51-44-11.

Part: DISPLAY — FAILED (NR 2 PFD) · airframe 32,621 hrs · 14,590 cycles

F/OS NR 2 PFD CIRCUIT BREAKER TRIPPED, FOLLOWED BY SMOKE IN THE COCKPIT. DIVERTED, LANDING UNEVENTFULLY. REPLACED F/OS PFD AND DMC, CHECKS OK.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 23,790 hrs · 10,565 cycles

FLIGHT ATTENDANT REPORTED LARGE WATER MESS IN AFT GALLEY, THEN ODOR OF ELECTRICAL FUMES AND SMOKE. FLIGHT CREW REMOVED POWER FROM GALLEY, OBSERVATION REVEALED THAT ODOR STILL PERSISTED, NO SMOKE. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED INTO DTW. AIRCRAFT LANDED UNEVENTFULLY. CORRECTIVE ACTION WAS TO REPLACE AFT GALLEY COFFEEMAKER.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,917 hrs · 7,902 cycles

DURING H-CHECK FOUND CORROSION ON AFT RT AND LT DOOR SILLS. REPAIRED PER EA 32-202563.

Part: PACKING — LEAKING (HYD MANIFOLD) · airframe 5,249 hrs · 2,344 cycles

DURING CLIMB, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES. RETURNED TO DEPARTURE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING O-RING ON PTU QUICK DISCONNECT COUPLING. LEAK CHECK OK.