N327NW

Part: PANEL — LOOSE (ZONE 200) · airframe 91,125 hrs · 42,746 cycles

SHIP 3227 DISC: OXYGEN PANEL LOOSE / LOCATIONS:103, OXYGEN PANEL IS LOOSE ABOVE THE 2L JUMPSEAT / INTERIOR. C/A: RE-SECURED O2 PANEL ABOVE JUMPSEAT AT 2L IAW A320 AMM 35-21. (LP: 0669183)

Part: IDG — LOW (NR 1) · airframe 89,895 hrs · 42,050 cycles

SHIP 3227 - MISC/DE - DUE TO ELEC IDG 1 OIL LO PR ECAM MESSAGE. CORRECTIVE ACTION: IDG #1 PLACED ON MEL. OK TO CONTINUE. LATER R/R IDG #1. OPS CHECK GOOD. (LP: 6020872)

Part: PICKUP — FAULTED (TE FLAP SYS) · airframe 89,874 hrs · 42,034 cycles

SHIP 3227 - MISC/DE - DUE TO FLAP 3 INDICATION DISAPPEARED ON APPROACH, PERFORMED GO-AROUND AND LANDED WITH FLAPS AT 2. CORRECTIVE ACTION: R/R/ INSTRUMENTATION POSITION PICK-OFF UNIT (3CN). OPS CHECK GOOD.

Part: OXYGEN MASK — DISLODGED (AFT LAVATORY) · airframe 89,743 hrs · 41,967 cycles

SHIP 3227 DISC: AFT CENTER LAV O2 MASK DROPPED. C/A: RESTOWED MASK. OK FOR SVC. REF A320 AMM 35-21. (LP: 5681056)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 89,528 hrs · 41,834 cycles

SHIP 3227 DISC: WHILE CHECKING INTERIOR EMERGENCY LIGHTS FOUND LT FWD EMERGENCY DOOR HANDLE LIGHT INOP. C/A: RELAMPED LT FWD EMERGENCY DOOR HANDLE PER A320 AMM 33-51. OPS CK GOOD. (LP: 5422117)

Part: STOP FITTING — DAMAGED (DOOR FRAME) · airframe 89,177 hrs · 41,647 cycles

SHIP 3227 DISC: LH AND R/H FR 66 STOP FITTINGS #1 TO #7 HOLES 1-4 MEASURE .255". AD RELATED AA 5311-01216. ACTIONS REQUIRED PRIOR TO FURTHER FLIGHT. C/A: REPAIRED PER PRI 616224-14AD REV 0,1,2,3,4,5 AND ERA 616224-14AD REV O SECTION I ASSOCIATED ER/A 14-616224 ADDED FOR AC 3227. (LP: 0245075)

Part: COUNTER — CRACKED (GALLEY) · airframe 89,177 hrs · 41,647 cycles

SHIP 3227 DISC: CRACK INDICATION ABSERVED ON UNDERSIDE OF G5 COUNTERTOP CUTOUTS COMPARTMENT 510 LH. APPROX 1.7 INCHES ACROSS. C/A: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 068-0001:2530-01591-05D/001 00010 REMOVED AND REPLACED G5 TROLLEY BLOCKS AND COMPLY WITH ER/A 616175-14AD REV ORIGINAL AND PRI 626175-14AD REV 0. (LP: 0242887)

Part: STOP FITTING — DAMAGED (DOOR) · airframe 89,177 hrs · 41,647 cycles

SHIP 3227 DISC: ER/A 616224-14 ISSUED FOR DAMAGE ON THE LH AND RH FR66 DOOR STOP FITTINGS (#1-#7). FOLLOW ON ACTION IS REQUIRED. C/A: STAGE III DAMAGE TOLERANCE EVALUATION (DTE) REQUIRED PRIOR TO 31,600 FC THRESHOLD. AN ER/A REVISION IS REQUIRED FOR CONTINUED SERVICE BEYOND THE THRESHOLD ASSOCIATED ER/A CHANGED FROM 00-616224 TO 32-616224 FOR AC 3227

Part: COUNTER — CRACKED (GALLEY) · airframe 89,177 hrs · 41,647 cycles

CRACK INDICATION ABSERVED ON UNDERSIDE OF G5 COUNTERTOP CUTOUTS COMPARTMENT 510 LH. APPROX 1.7 INCHES ACROSS. ORIGINAL DISCREPENCY IS ON NR 10 OF EMPOWER WO P337975820240202. C/A: REMOVED AND REPLACED G5 TROLLEY BLOCKS AND COMPLIED WITH ER/ A616175-14AD REV ORIGINAL SEC 1. GALLEY MPN 601537-1 MSN 4050G ACCOMPLISH POST-REPAIR INSPECTION WITHIN 36 MONTHS AFTER ACCOMPLISHMENT OF SECTION I, AND EVERY 6 MONTHS THEREAFTER. (LP: 0243298)

Part: DOOR — NOT SEATED (FWD CARGO) · airframe 89,115 hrs · 41,622 cycles

SHIP 3227 - ATB - DUE TO DOOR FWD CARGO ECAM MESSAGE. DECLARED EMERGENCY. CORRECTIVE ACTION: INSPECTED FORWARD CARGO DOOR AND FOUND THE DOOR AJAR. CLEARED LATCH AND OPERATIONAL CHECK PERFORMED. OPS CHECK GOOD.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 88,431 hrs · 41,207 cycles

SHIP 3227 DISC: MER EXIT LT LWR FWD R-1 DOOR INOP C/A: UNABLE TO DUPLICATE FAULT LIGHT OPERATES NORMAL (LP: 9626061)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,032 hrs · 40,490 cycles

SHIP 3227 - MISC/DE - DUE TO A F/CTL FLAP SYS 1 FAULT ECAM MSG. CORRECTIVE ACTION: R/R SFCC #1. OPS CHECK GOOD. (9135162)

Part: HANDLE — UNSECURE (AFT CARGO DOOR) · airframe 85,738 hrs · 39,768 cycles

ATO AT 65KTS DUE TO AN AFT CARGO DOOR OPEN MESSAGE. FOUND CARGO DOOR HANDLE NOT FULLY STOWED. HANDLE SECURED AND OPS CHECK WAS GOOD. RETURNED TO SERVICE. (9833660)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 NEED TO COMPLY WITH ERA 598894-14 REV A SECT. II. CORRECTIVE ACTION: COMPLIED WITH. (2512505)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 NEED TO COMPLY WITH ER/A 598867-14 REV A SECT. II. CORRECTIVE ACTION: COMPLIED WITH ERA INSP. (2513052)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 NEED TO COMPLY WITH ERA 598894-14 REV A SECT III. CORRECTIVE ACTION: COMPLIED WITH. (2512512)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 NEED TO COMPLY WITH ERA 598776-14 REV A SECTION V MONITOR INSP. CORRECTIVE ACTION: COMPLIED WITH. (2509668)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 FUSELAGE / BULKHEADS / FR35LH BTW STGR28 AND STGR31 / CRACK AT HOLE 6 AND 16 SECTION IV INSPECTION. CORRECTIVE ACTION: COMPLIED WITH INSP. (2509731)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 FUSELAGE / BULKHEADS / FR35LH BTW STGR28 AND STGR31 CRACK AT HOLE 6 AND 16. CORRECTIVE ACTION: COMPLIED WITH ERA 598776-14 REV A SECTION II. (2509692)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 FUSELAGE / BULKHEADS / FR35LH BTW STGR28 AND STGR31 / CRACK AT HOLE 6 AND 16. CORRECTIVE ACTION: COMPLIED WITH ERA 598776-14 REV A SECTION VIII. (2509757)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 REQUIRE 598776-14 REV A SECTION VII MONITOR INSP. CORRECTIVE ACTION: COMPLIED WITH ERA. (2509680)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 FUSELAGE / BULKHEADS / FR35LH BTW STGR28 AND STGR31 / CRACK AT HOLE 6 AND 16. CORRECTIVE ACTION: COMPLIED WITH ERA 598776-14 REV A SECTION VI. (2509745)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,775 hrs · 40,352 cycles

SHIP 3227 FUSELAGE / BULKHEADS / FR35LH BTW STGR28 AND STGR31 / CRACK AT HOLE 6 AND 16- SECTION III INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 598776-14 REV A SECTION III INSPECTION. (2509699)

Part: NONE — NONE · airframe 85,407 hrs · 39,548 cycles

AIRCRAF 3227, DURING OVERNIGHT MAINTENANCE, DOOR 1RT AND 4LT DOOR ASSIST PRESSURE LOW. CORRECTIVE ACTION: SERVICED 1RT AND 4LT DOOR ASSIST BOTTLES PER A320 AMM 52-10 LEAKS NOTED. LP 8919319

Part: NONE — NONE · airframe 84,713 hrs · 39,129 cycles

SHIP 3227 AFT RT CABIN DOOR DIFFICULT TO OPEN/CLOSE. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-12. OK FOR SERVICE. (9295598)

Part: LEVER — OUT OF ADJUST · airframe 84,576 hrs · 39,046 cycles

SHIP 3227 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS:601 /. CORRECTIVE ACTION: ADJUSTED DOOR PER A320 AMM 52-12. OK FOR SERVICE. (2285015)

Part: GIRT BAR — STICKING · airframe 84,526 hrs · 39,023 cycles

SHIP 3227 F/A REPORTS STIFF / DIFFICULT ARMING L1 DOOR. CORRECTIVE ACTION: CLEANED AND LUBED GIRT BAR. OK FOR SERVICE. (9196800)

Part: ARMING LEVER — OUT OF ADJUST · airframe 84,478 hrs · 39,001 cycles

SHIP 3227 L1 DOOR SLIDE ARMING HANDLE NEEDS ADJUSTMENT, MOVES TOO EASILY. CORRECTIVE ACTION: ADJUSTED DOOR ARMING LEVER PER A320 AMM 52-12. OK FOR SERVICE. (6968027)

Part: CONTROL HANDLE — INOPERATIVE · airframe 84,478 hrs · 39,001 cycles

SHIP 3227 SLIDE ARM NOT WORKING CORRECTLY. CORRECTIVE ACTION: PERFORMED ADJUSTMENT OF TRIPLE LEVER RIGGING OF EMERGENCY CONTROL HANDLE 831 PER A320 AMM 52-11-22. OPS TEST GOOD. (2262664)

Part: FRAME — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION ON FRAME 35 LH SIDE AT LEVEL OF STRG30 IN OPEN FASTENER HOLE H16, CRACK DIRECTION IS 5 OCLOCK IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ERA 598776-14AD REV. ORIGINAL. (2259872)

Part: MEMBRANE — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND IN OPEN HOLE OF PRESSURE DECK MEMBRANE LOCATED ON FRAME 36 AND Y1523 MORE 4 INCHES ( HOLE NUMBER 5 ) LH SIDE CRACK DIRECTION ARE 3 AND 7 O CLOCK. CORRECTIVE ACTION: COMPLIED WITH ERA 598894-14AD REV ORIGINAL. (2259922)

Part: STRINGER — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND AT OPEN HOLE LOCATED AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 (-Y254) ZONE 2 AT FRAME 36. CORRECTIVE ACTION: COMPLIED WITH ER/A 598724-14AD.REV ORIGINAL. (2259113)

Part: STRINGER — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND AT OPEN HOLE LOCATED AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 (-Y765) ZONE 1 AT FRAME 36. CORRECTIVE ACTION: COMPLIED WITH ER/A 598724-14AD.REV ORIGINAL. (2259119)

Part: PRESSURE DECK — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND IN OPEN FASTENER HOLE LOCATED ON PRESSURES DECK MEMBRANE ON FRAME 36 AND -Y1523 MORE 7 INCHES ( HOLE NUMBER 7 ) RH SIDE. CRACK DIRECTION IS 12 0 CLOCK . CORRECTIVE ACTION: COMPLIED WITH ERA 598867-14AD REV ORIGINAL. (2260346)

Part: MEMBRANE — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND IN OPEN HOLE OF PRESSURE DECK MEMBRANE LOCATED ON FRAME 36 AND -Y1523 MORE 4 INCHES ( HOLE NUMBER 4 ) RH SIDE CRACK. (2260345)

Part: STRINGER — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND AT OPEN HOLE LOCATED AT CWB FRONT SPAR VERTICAL STRINGER POSITION 5 (-Y765) ZONE 2 AT FRAME 36. CORRECTIVE ACTION: COMPLIED WITH ER/A 598724-14AD.REV ORIGINAL. (2259126)

Part: STRINGER — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND AT OPEN HOLE LOCATED AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 (Y765) ZONE 2 AT FRAME 36. CORRECTIVE ACTION: COMPLIED WITH ER/A 598724-14AD.REV ORIGINAL. OK FOR SERVICE. (2259115)

Part: STRINGER — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 32271 CRACK INDICATION FOUND AT OPEN HOLE LOCATED AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 (Y254) ZONE 2 AT FRAME 36. CORRECTIVE ACTION: COMPLIED WITH ER/A 598724-14AD.REV ORIGINAL. (2259134)

Part: STRINGER — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND AT OPEN HOLE LOCATED AT CWB FRONT SPAR VERTICAL STRINGER POSITION 4 (-Y254) ZONE 1 AT FRAME 36. CORRECTIVE ACTION: COMPLIED WITH ER/A 598724-14AD.REV ORIGINAL. (2259102)

Part: STRINGER — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND AT OPEN HOLE LOCATED AT CWB FRONT SPAR VERTICAL STRINGER POSITION 3 (254) ZONE 1 AT FRAME 36. CORRECTIVE ACTION: COMPLIED WITH ER/A 598724-14AD.REV ORIGINAL. OK FOR SERVICE. (2259133)

Part: STRINGER — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND AT OPEN HOLE LOCATED AT CWB FRONT SPAR VERTICAL STRINGER POSITION 2 (Y765) ZONE 1 AT FRAME 36. CORRECTIVE ACTION: COMPLIED WITH ER/A 598724-14AD.REV ORIGINAL. (2259122)

Part: FRAME — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION ON FRAME 35 LH SIDE AT LEVEL OF STRG30 IN OPEN FASTENER HOLE H6, CRACK DIRECTIONS ARE 3 AND 8 OCLOCK IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ERA 598776-14AD REV. ORIGINAL. (2259876)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 REINSPECT EXISTING REPAIR STOP FITTING 1 ON FRAME 68 RH SIDE AT AFT GALLEY AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 599559-14AD REV ORIGINAL. (2258358)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 NEED TO COMPLY WITH DTA MONITOR INSPECTION LOG REFERENCE ER/A 598867-14 SECTION II. CORRECTIVE ACTION: COMPLIED WITH ERA 598867-14 SECTION II. (2257603)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION FLOORBEAM -Y254 LOC FR20 TO FR24 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11. (2252517)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 NEED TO COMPLY WITH DTA MONITOR INSPECTION LOG REFERENCE ER/A 598776-14 SECTION II. CORRECTIVE ACTION: COMPLIED WITH ERA 598776-14 SECTION II. (2258301)

Part: SUPPORT ANGLE — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK DOOR SUPPORT ANGLE ON PIANO HINGE AREA LOWER SURFACE AT LEVEL FRAME 26 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED DOOR SUPPORT ANGLE PER A320 SRM 51-42-11. (2252868)

Part: NONE — NONE · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION INTERNAL STRUCTURE ON WEB LOC BTW FR69 TO FR70 AT LEVEL STR23L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE ON WEB PER A320 SRM 51-72-11. (2249145)

Part: NONE — NONE · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION FLOOR BEAM -Y765 LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11 AND 51-42-11. (2247828)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 PASSENGER CREW DOOR 831 EMERGENCY DOOR DAMPER CYLINDER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DAMPER PER A320 AMM 52-11-14. OK FOR SERVICE. (2246554)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 PASSENGER CREW DOOR 842 FLEXIBLE EMERGENCY CONTROL CABLE AT AFT GALLEY AREA DEFORMED. CORRECTIVE ACTION: REPLACED CABLE PER A320 AMM 52-13-22. (2242144)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND OPEN HOLE 3 O/B LOWER OF DOOR STOP FITTING 7 FRAME 68 RH. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-41-12. OK FOR SERVICE. (2242521)

Part: NONE — NONE · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION FLOOR BEAM Y1292 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2242138)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND OPEN HOLE 4 I/B LOWER OF DOOR STOP FITTING 1 FRAME 68 RH. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-41-12. OK FOR SERVICE. (2239762)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND OPEN HOLE 3 O/B LOWER OF DOOR STOP FITTING 2 FRAME 68 LH. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-41-12. OK FOR SERVICE. (2239742)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CRACK INDICATION FOUND OPEN HOLE 4 I/B LOWER OF DOOR STOP FITTING 4 FRAME 68 RH. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-41-12. (2235820)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227CRACK INDICATION FOUND OPEN HOLE 4 I/B LOWER OF DOOR STOP FITTING 4 FRAME 68 RH. CORRECTIVE ACTION: PERFORMED REPAIR PER A320 SRM 53-41-12. (2235624)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 IMPROPERLY PACKED SLIDE RAFT PASSENGER CREW DOOR 842 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SLIDE RAFT PER A320 AMM 25-62-44. OK FOR SERVICE. (2233409)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 ELONGATED HOLE INTERNAL STRUCTURE WEB LOCATED BETWEEN FR58 TO FR59 AND STR38L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE WEB PER A320 SRM 51-42-11 AND 51-72-11. (2233488)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION FLOORBEAM LOCATED BTW FR 12 TO FR 24 AND Y765 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM Y765 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11. (2230366)

Part: COUPLING — CORRODED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 NEED TO REPLACE LH FRAME FOOT COUPLING. (CORRODED) CORRECTIVE ACTION: REPLACED LH FRAME FOOT COUPLING PER DELTA WORKCARD AMDS 5311-01239-02A. (2228995)

Part: NONE — NONE · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION STRINGER 31R LOC BTW FR 65 TO FR 66 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-42-11. (2227770)

Part: NONE — NONE · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 BENT INTERNAL STRUCTURE CROSSBEAM AT LEVEL OF FR30 AND BTW STRG38RH AND STRG 44 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED CROSSBEAM PER A320 SRM 51-42-11. (2227785)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 BENT INTERNAL STRUCTURE CROSSBEAM AT LEVEL FR27 AND FROM STRG38LH TO STRG43LH IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED CROSSBEAM PER A320 SRM 51-42-11. (2227778)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION FLOORBEAM -Y1292 BTW FR 12 TO FR 24 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11 AND 51-42-11. (2222923)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 PASSENGER CREW DOOR 842 AT AFT GALLEY DAMPER DOES NOT PASS TEST. CORRECTIVE ACTION: REPLACED DOOR DAMPER CYLINDER PER A320 AMM 52-13-14. (2218961)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION FLOORBEAM +Y1292 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11 AND 51-42-14. (2217603)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION FLOOR5BEAM -Y1292 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11. (2216022)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION FLOORBEAM -Y1162 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11. (2216025)

Part: ROLLER — WORN · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 PASSENGER CREW DOOR 841 LOWER ROLLERS WORN. CORRECTIVE ACTION: R/R DOOR ROLLERS PER A320 AMM 52-11-31. OK FOR SERVICE. (2216049)

Part: FRAME — CRACKED · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 NEED TO REPAIR FRAME 43 R/H (CRACK) CORRECTIVE ACTION: REPAIRED PER DELTA WORKCARD AMDS 5311-01239-01B. OK FOR SERVICE. (2216044)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION FLOORBEAM -Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 51-72-11. (2216046)

Part: NONE — NONE · corrosion level 2 · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 CORROSION WEB INTERNAL STRUCTURE LOC BTW FR69 TO FR70 AT LEVEL STR 23 RH AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB PER A320 SRM 51-72-11 AND 53-41-17. (2214887)

Part: NONE — NONE · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 PASSENGER CREW DOOR 842 AT AFT GALLEY AREA UPPER AND LOWER LINK BUSHINGS WORN. CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 AMM 52-13-21. OK FOR SERVICE. (2213500)

Part: BUSHING — WORN · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 PASSENGER CREW DOOR 831 BUSHINGS WORN BTW UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 AMM 52-11-21. (2212285)

Part: BUSHING — EXCESS PLAY · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 PASSENGER CREW DOOR 841 BUSHINGS HAVE EXCESSIVE PLAY. CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 AMM 52-11-21. (2212280)

Part: FITTING — WORN · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 WEAR INTERNAL STRUCTURE FITTINGS LOCATED AFT BULKHEAD UPPER SIDE AT LEVEL Y 765 TO -Y 765 FR 34 (4EA) IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED INTERNAL STRUCTURE FITTINGS PER A320 SRM 51-72-11. (2212631)

Part: BUSHING — WORN · airframe 84,477 hrs · 39,000 cycles

SHIP 3227 EXCESSIVE PLAY PASSENGER CREW DOOR 832 BTW UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED BUSHINGS PER A320 AMM 52-10-00 AND 52-13-21. OK FOR SERVICE. (2204074)

Part: LIGHT — DAMAGED (SEAT 13D) · airframe 84,113 hrs · 38,820 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED, RESECURED EMERGENCY LT MOUNT ON SEAT 13D

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 83,235 hrs · 38,373 cycles

EPSU FAULT INT. LOADS EMER R, INSTALLED SERVICEABLE EPSU W/O BATTERY

Part: SDAC — FAULTY (NR 2) · airframe 82,474 hrs · 37,977 cycles

SHIP 3227 - HYD - GREEN AND YELLOW HYDRAULIC SYSTEM OVERHEAT MESSAGES. SYSTEM SHUTDOWN AND GRAVITY GEAR EXTENSION REQUIRED PER QRH. DURING LANDING #3 AND #4 MAIN TIRES FLAT SPOTTED AND BLOWN. CORRECTIVE ACTION: FOUND SDAC #2 TO BE CAUSING ERRONEOUS INDICATIONS. REPLACED SDAC #1 AND #2. REPLACED #3 AND #4 WHEEL AND BRAKE ASSEMBLIES.

Part: LIGHT — INOPERATIVE (SEAT 11D) · airframe 82,366 hrs · 37,920 cycles

SEAT 11D EMERGENCY LIGHT INOP, REPLACED LIGHT

Part: COVER — MISSING (LT WING TE FLAP) · airframe 82,273 hrs · 37,875 cycles

FOUND LH FLAP TRACK MOVABLE FAIRING PIVOT COVER MISSING, INSTALLED NEW LH #3 FLAP FAIRING INBD PIVOT COVER

Part: EPSU — INOPERATIVE (CABIN) · airframe 81,146 hrs · 37,339 cycles

EPSU (13WL) IN PASSENGER CABIN INOPERATIVE. REMOVED AND REPLACED SAME. OPERATION CHECKS GOOD.

Part: WEB — CRACKED (EMERGENCY EXIT) · airframe 81,082 hrs · 37,306 cycles

CRACKED WEB EMERGENCY EXIT DOOR 844 INTERNAL AREA IN PASSENGER CABIN. REPLACED SEGMENT ANGLE IAW SRM 51-72-11 AND DWG 52279010.

Part: BATTERY — FAULTED (CABIN) · airframe 79,915 hrs · 36,714 cycles

AFT LEFT EMERGENCY LIGHT BATTERY FAULT. REMOVED AND REPLACED AFT LEFT EMERGENCY LIGHT BATTERY. OPERATION CHECKS GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 79,293 hrs · 36,415 cycles

AFT LEFT LAVATORY SMOKE DETECTOR ALARM SOUNDED TWICE. STOPPED BY ITSELF. THE FLIGHT DECK LAVAVATORY SMOKE LIGHT AND BELL SOUNDED ONCE THEN STOPPED. REMOVED AND REPLACED SDCU IAW MM. REPLACED AFT LEFT LAVATORY SMOKE DETECTOR. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 77,307 hrs · 35,501 cycles

EMERGENCY ESCAPE PATH LIGHT AT SEAT 1C BROKEN, REPLACED 01C EMERGENCY ESCAPE PATH LIGHT ASSY.

Part: SKIN — DENTED (FRAMES 53-54) · airframe 77,053 hrs · 35,363 cycles

DENTS AND PULL IN RIVETS FOUND ON EXTERNAL SKIN BETWEEN FRAMES 53 - 54 AND STRINGER 41L, REPAIR ON EXTERNAL SKIN BTW FR 53 TO FR 54 AND STR 37L TO STR 42L ON LOWER FUSELAGE IAW ER/A 554926-14AD REV. ORIGINAL

Part: SKIN — DAMAGED (FUSELAGE) · airframe 75,301 hrs · 34,480 cycles

LIGHTNING STRIKE DAMAGE, FWD INBD MOUNT HOLE FOR FWD WATER DRAIN MAST. REMOVED DAMAGE PER SRM 53-00-11 FIG 231 SHT 3. REPAIR PER ERA 553223-14AD REV ORIG SECT I.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 75,122 hrs · 34,383 cycles

14L EMERGENCY LIGHT INOPERATIVE, CONNECTED THE LIGHT

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,161 hrs · 32,369 cycles

FOUND EMERGENCY LIGHT TEST WOULD NOT PASS. REPLACED THE POWER SUPPLY AND FUNCTIONAL CHECKED NORMAL.

Part: SKIN — DENTED (FRAME 65) · airframe 70,086 hrs · 31,852 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED AT FRAME 65 AND BETWEEN STR 43L TO STR 44 AFT FUSELAGE. EVALUATED DENT ON EXTERNAL SKIN LOCATED AT FRAME 65 AND BETWEEN STR 43L AND STR 44 IAW ER/A 532995-14 REV ORIGINAL AND PRI 532995-14, REV 0, 1, 2, 3, 4, 5.

Part: SKIN — DENTED (FRAMES 67) · airframe 70,086 hrs · 31,852 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED AT FRAME 67+6" AND STR 32R AFT FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED AT FRAME 67+6" AND STR 32R AFT FUSELAGE IAW ERA 532995-14, REV ORIGINAL AND PRI 532995-14.

Part: SKIN — DENTED (FRAME 68) · airframe 70,086 hrs · 31,852 cycles

DURING INSPECTION, FOUND DENTS ON EXTERNAL SKIN LOCATED AT FRAME 68 AND BETWEEN STR 43L TO STR 32R AFT FUSELAGE. EVALUATED DENTED AREA ON EXTERNAL SKIN LOCATED AT FRAME 68 AND BETWEEN STR 43L TO STR 32R AFT FUSELAGE IAW ER/A 532995-14, REVISION ORIGINAL AND PRI 532995-14, REVISION 0, 1, 2, 3, 4, 5.

Part: SKIN — DENTED (FRAME 67) · airframe 70,086 hrs · 31,852 cycles

DURING INSPECTION, FOUND DENTS ON EXTERNAL SKIN LOCATED AT FRAME 67 AND BETWEEN STR 32L TO STR 32R AFT FUSELAGE. EVALUATED DENT ON EXTERNAL SKIN LOCATED AT FRAME 67 AND BETWEEN STR 32L TO STR 32R AFT FUSELAGE IAW ER/A 532995-14, REV ORIGINAL AND PRI 532995-14 REV 0, 1, 2, 3, 4, 5.

Part: SKIN — DENTED (FRAME 69) · airframe 70,086 hrs · 31,852 cycles

DURING INSPECTION, FOUND DENTS ON EXTERNAL SKIN LOCATED AT FRAME 69 AND BTW STR 32R TO STR 37R AFT FUSELAGE. EVALUATED DENT ON EXTERNAL SKIN LOCATED AT FRAME 69 AND BETWEEN STR 32R TO STR 37R AFT FUSELAGE IAW ER/A 532995-14, REV ORIGINAL AND PRI 532995-14, REVISIONS 0, 1, 2, 3, 4, 5.

Part: SKIN — DENTED (FRAME 66) · airframe 70,086 hrs · 31,852 cycles

DURING INSPECTION, FOUND DENT ON EXTERNAL SKIN LOCATED AT FR66 AND BETWEEN STG 42R TO STG 43R AFT FUSELAGE. EVALUATED DENT ON EXTERNAL SKIN LOCATED AT FR 66 AND BETWEEN STR 42R TO STR 43R AFT FUSELAGE IAW ER/A 532995-14, REV ORIGINAL AND PRI 532995-14.

Part: SLAT — UNKNOWN · airframe 70,098 hrs · 31,856 cycles

DURING INSPECTION, FOUND CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR ON SLAT NR 2 RT WING LOCATED T/E UPPER SURFACE AT 12" FROM INBD EDGE AND 7.5" FROM L/E OF SLAT. REPLACED SLAT 2 RT, PERFORMED ADJUSTMENT OF SLAT 2 RT IS GOOD AND PERFORMED OPS TEST OF SLAT POWER TRANSMISSION IS GOOD IAW AMM 27-84-64-400-002-A AND AMM 27-84-00-710-001-A.

Part: SKIN — CORRODED (FRAMES 69-70) · airframe 70,086 hrs · 31,852 cycles

DURING INSPECTION, FOUND CORROSION ON EXTERNAL SKIN LOCATED BETWEEN FRAME 69 TO FRAME 70 AND STR31R TO STR32R AFT FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BETWEEN FRAME 69 TO FRAME 70 AND BETWEEN STR 30R TO STR 33 RT REAR FUSELAGE IAW SRM 53-41-11, PARAGRAPH 5D, FIG 205, PAGES 259/260.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,582 hrs · 35,651 cycles

DENTS AND CREASES WERE FOUND ON FWD FUSELAGE SKIN BETWEEN STRINGERS 14L-15L AND DOOR STOP BEAM , REPAIRED IAW ERA 533192-14, AND PRI 533192-14.

Part: BRACKET — CORRODED (RT AILERON) · airframe 75,224 hrs · 34,435 cycles

RIGHT AILERON JACK 1 AND 2 AND HINGE 4 BRACKETS WERE CORRODED. THE BRACKETS WERE REPAIRED PER ER/A.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 75,224 hrs · 34,435 cycles

CORROSION ON FLOOR SUPPORT -Y254 BETWEEN FRAMES 12 - 24. REPAIRED THE FLOOR SUPPORT IAW ER/A.

Part: STRUCTURE — CORRODED · airframe 75,224 hrs · 34,435 cycles

DURING M CHECK, SEVEN CORROSION SPOTS WERE FOUND ON THE UPPER SURFACE OF THE COVERSHEET LOCATED AT AFT CARGO BAY AREA. DAMAGED AREAS WERE REWORKED IAW IAW SRM AND ER/A.

Part: BOLT — WORN (SPOILER) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND WEAR ON STOP BOLT OF CENTER FITTING LOCATED SPOILER 2, LT PERFORMED PERMANENT REPAIR ON STOP BOLT OF CENTER FITTING LOCATED ON SPOILER 2 LT WING IAW SRM 57-70-00, PARA 5.C, FIG 201.

Part: STRINGER — CORRODED (FRAMES 55-56) · airframe 75,224 hrs · 34,435 cycles

CORROSION ON STRINGER 44 IN THE AFT CARGO BAY BETWEEN FRAMES 55 AND 56. REPAIRED THE STRINGER.

Part: STRINGER — CORRODED (FRAME 56) · airframe 75,224 hrs · 34,435 cycles

CORROSION ON STRINGER 43R IN AFT CARGO BAY FRAME 56+1. REPAIRED THE STRINGER.

Part: WEB — CRACKED (FRAMES 23-24) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CRACK ON WEB LOCATED BETWEEN FRAME 23 TO FRAME 24 LEVEL STR 34L AFT AVIONIC COMPARTMENT. REPLACED WEB LOCATED BETWEEN FRAME 23 TO FRAME 24 AT STR 34L LEVEL, AVIONIC COMPARTMENT, IAW SRM 51-72-11 AND DWG D53911363.

Part: NONE — NONE (NONE) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, CONFIRM AT EVALUATION FOR POSSIBLE FCS REPAIR. ON EXTERNAL SKIN LT PAX DOOR LOCATION BETWEEN XP 662 AND XP 297 AND BETWEEN BEAM 7 AND BEAM 6. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN L1 PAX DOOR LOCATED BETWEEN XP 662 AND XP 297 AND BETWEEN BEAM 7 AND BEAM 6 IAW SRM 52-10-00; PARA 5.F FIG 206, SHEET 1.

Part: SKIN — DAMAGED (FRAME 24) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND NICK ON EXTERNAL FUSELAGE SKIN LOCATED FR 24+9" AND BETWEEN STR 42L AND STR 43L. PERFORMED REPAIR ON EXTERNAL FUSELAGE SKIN LOCATED FRAME 24+9" AND BETWEEN STR 42L TO STR 43L IAW SRM 53-00-11, PARA 4W REPAIR 7, FIG 240.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON TIE CLIP LOCATED ON FR 31 BETWEEN STR 38R AND STR 39R IN FWD CARGO COMPARTMENT REPLACED TIE CLIP LOCATED ON FR 31 BETWEEN STR 38R AND STR 39R IN FWD CARGO COMPARTMENT IAW SRM 51-72-11 AND DWG D52231533.

Part: WEB — CORRODED · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON VERTICAL WEB OF THE LT MOVABLE FAIRING. REPLACED VERTICAL WEB OF THE LT MOVABLE FAIRING IAW SRM 51-72-11 AND 51-42-11 AND DWG D545-30391.

Part: BOLT — WORN (SPOILER) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND WEAR ON STOP BOLT OF CENTER FITTING LOCATED SPOILER NR 4 LT WING. PERFORMED PERMANENT REPAIR ON STOP BOLT CENTER HINGE FITTING LOCATED ON SPOILER NR 4 LT WING IAW SRM 57-70-00, PARA 5.C, FIG 201, SHEET 2.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, -Y1292 LOCATED BETWEEN FR 47 TO FR 64. EVALUATED AND FOUND OUT LIMITS ON JC 2500-2032. REPLACED SEAT TRACK, -Y1292 LOCATED BETWEEN FRAME 47 TO FRAME 64 AFT PAX CABIN IAW SRM 51-72-11 AND DWG N D53472000.

Part: WEB — CORRODED · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON VERTICAL WEB OF RT MOVABLE FAIRING. REPLACED VERTICAL WEB ON RT MOVABLE FAIRING IAW SRM 51-72-11 AND 51-42-11 AND DWG D545-30391.

Part: CLEAT — CORRODED (FRAME 29) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON TIE CLEAT ON FR 29 AND BETWEEN STR 42L TO STR 43L FWD CARGO COMPARTMENT, SSI 532180. REPLACED TIE CLEAT LOCATED FRAME 29 AND BETWEEN STR 42L TO STR 43L FWD CARGO COMPARTMENT IAW SRM 51-42-11 AND DWG D53231626 AND DWG D53230319.

Part: BOLT — CORRODED (SPOILER) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND WEAR ON STOP BOLT OF CENTER FITTING, LOCATED ON SPOILER 3 LT WING. PERFORMED PERMANENT REPAIR ON STOP BOLT OF CENTER FITTING LOCATED ON SPOILER 3 LT WING IAW SRM 57-70-00, PARA 5.C, FIG 201.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CRACK ON SEGMENT ANGLE RT, IN EMERGENCY EXIT DOOR. REPLACED THE ANGLE IAW SRM 51-72-11.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON CURVE EDGE RT LOWER CORNER IN EMERGENCY EXIT DOOR. REPLACED THE STRUCTURE IAW SRM 51-72-11.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CRACK ON SEGMENT FRAME IN RT EMERGENCY EXIT DOOR. REPLACED THE FRAME IAW SRM 51-72-11 AND DWG D52279010.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON STRUCTURE IN THE RT EMERGENCY EXIT DOOR. REPLACED THE STRUCTURE IAW SRM 51-72-11.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND A CRACK ON SEGMENT ANGLE IN EMERGENCY EXIT DOOR . REPLACED THE ANGLE IAW SRM 51-72-11.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CRACK ON FRAME IN THE EMERGENCY EXIT DOOR. REPLACED THE FRAME IAW SRM 51-72-11 AND DWG D52279010.

Part: FLOOR SUPPORT — CRACKED (FRAME 29) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CRACK ON FLOOR SUPPORT Y-254, FRAME 29. REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 24 - 35 IAW SRM 51-72-11 AND DWG.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 BETWEEN FRAMES 36 - 41. FOUND OUT LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130146.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 BETWEEN FRAMES 35 - 36. FOUND TO BE OUT OF LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370000.

Part: STRUCTURE — CORRODED (FRAMES 66-68) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER SILL BETWEEN FRAMES 66 - 68. REPLACED THE SILL IAW SRM 51-72-11 AND DWG D534-80019.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CRACKED ANGLE ON RT EMERGENCY EXIT DOOR. REPLACED THE ANGLE IAW SRM 51-72-11, DWGS D52279036, AND D52279010.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND A CRACK ON THE ANGLE IN THE LEFT EMERGENCY EXIT DOOR. REPLACED THE ANGLE IAW SRM 51-72-11, DWGS D52279036, AND D52279010.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND A CRACK ON THE FRAME IN THE LT EMERGENCY EXIT DOOR. REPLACED THE FRAME IAW SRM 51-72-11, DWGS D52279040, AND D52279010.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765 BETWEEN FRAMES 47 - 64 . FOUND TO BE OUT OF LIMITS IAW JC NR 2500-2032. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND 53-41-15, FIG 202.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CRACK ON FRAME IN THE RIGHT EMERGENCY EXIT DOOR. REPLACED THE FRAME IAW SRM 51-72-11, DWGS D52279040, AND D52279010.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CRACK ON ANGLE IN THE RIGHT EMERGENCY EXIT DOOR. REPLACED THE ANGLE IAW SRM 51-72-11 AND DWG D52279010.

Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND A CRACK ON ANGLE IN EMERGENCY EXIT DOOR. REPLACED ANGLE IAW SRM 51-72-11 AND DWG D52279010.

Part: CLEAT — CORRODED (FRAMES 28-29) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON CLEAT BETWEEN FRAMES 28 AND 29 STRINGERS 40-41L. REPLACED THE CLEAT IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 30 AND BETWEEN STRINGERS 41-42L. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231626.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 BETWEEN FRAMES 35 - 36. FOUND OUT LIMITS ON JC 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371024.

Part: SPAR — CORRODED (RT PYLON) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON RT PYLON UPPER SPAR SPIGOT RECEPTACLE. PERFORMED PERMANENT REPAIR IAW SRM 54-51-12, CONFIG 1, PARA 5A FIG 201.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR PANEL 261FF AT AFT GALLEY AREA. REPLACED FLOOR PANEL 261FF AT AFT GALLEY AREA AND INSTALLATION IS DOCUMENTED IN AMDS 2500-6602.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 BETWEEN FRAMES 41 - 47. FOUND OUT OF LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371000.

Part: SEAT TRACK — CORRODED (FRAMES 35-36) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 BETWEEN FRAMES 35 - 36. FOUND OUT OF LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371034.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y765, BETWEEN FRAMES 36 - 41. FOUND OUT LIMITS ON JC 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130146.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, -Y765 BETWEEN FRAMES 41 - 47. FOUND OUT LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, Y765 BETWEEN FRAMES 41 - 47. FOUND OUT LIMITS ON JC 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D53371000.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, -Y1292 BETWEEN FRAMES 36 - 41. FOUND OUT LIMITS ON JC NR 2500-2031. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D57130146.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1292 BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1162 BETWEEN FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72000.

Part: STRUCTURE — CORRODED (FRAMES 66-68) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SILL BETWEEN FRAMES 66 - 68. REPLACED THE SILL. IAW SRM 51-72-11 AND DWG D53480019.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PANEL 640RB RT WING. REPLACED FUEL ACCESS PANEL 640RB RT WING IAW AMM 57-27-11-400-002-A AND THE INSTALLATION IS DOCUMENTED IN AMDS CARD 5730-6013.

Part: STRUCTURE — CORRODED (FRAME 66) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER FRAME 66 AND STRINGER 23L . REPLACED IAW SRM 51-72-11 AND DWG D53480009.

Part: FLOOR SUPPORT — DAMAGED (FRAMES 68-70) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND EVIDENCE OF REWORK ON FLOOR SUPPORT Y-160 BETWEEN FRAMES 68 AND 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG NR D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG: D53112812, D53110984.

Part: STRUCTURE — CORRODED (FRAME 68) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER FRAME 68 STRINGER 23L. REPLACED LOWER CORNER IAW SRM 51-72-11 AND DWG D5348009.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT, Y1292 BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-67) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-465 BETWEEN FRAMES 64 AND 67+10. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, Y1292, BETWEEN FRAMES 47 TO 64. FOUND OUT LIMITS ON JC NR 2500-2032. REPLACED THE SEAT TRACK IAW SRM 53-41-15. PARA 5.B, FIG 202, SRM 51-72-11 AND DWG D53470080, D5347200.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y254, BETWEEN FRAMES 12 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112816;

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-70) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y512.5 BETWEEN FRAMES 64-70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534 72000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1225 BETWEEN FRAMES 66+5 - 67+15. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG 53472000.

Part: WEB — CORRODED (FRAMES 20-24) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON WEB Y1732 LOCATED BETWEEN FRAMES 20 TO 24 . REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53114392.

Part: FLOOR SUPPORT — CRACKED (FRAMES 25-29) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND A CRACK IN THE FLOOR SUPPORT Y+254, BETWEEN FRAMES 25-29.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 LOCATED BETWEEN FRAMES 47-64 . FOUND OUT LIMITS ON NR 2500-2032. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DWG D534 72000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT, Y1162 FRAMES 67+15 - 69. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND EVIDENCE OF REWORK ON UPPER FLANGE OF FLOOR SUPPORT Y-1379.5 FRAME 16 FWD PAX CABIN. REPLACED FLOORB SUPPORT IAW SRM 51-72-11 AND DWG D53112831.

Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND DELAMINATION ON FLOOR PANEL 222FF IN THE GALLEY AREA. REPLACED THE FLOOR PANEL IAW AMDS 2500-6617.

Part: DOOR FRAME — CORRODED (FRAMES 17-19) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FWD PAX CABIN CENTER FITTING OF R1 DOOR CUT OUT LOCATED BETWEEN FRAME 17 TO FRAME 19 AT LEVEL OF STR 23R, SSI 531163. REPLACED CENTER FITTING OF R1 DOOR LOCATED BETWEEN FR 17 TO FR 19 AT LEVEL STR 23R IAW SRM 51-42-11 AND DWG D53112109.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON JOINT COVER LOCATED ON FLOOR SUPPORT -Y81 BETWEEN FRAMES 12-16.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66- 70) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765 BETWEEN FRAMES 66+5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: FITTING — CORRODED (FRAME 68) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER CORNER IN AFT PAX CABIN LOCATED AT FRAME 68 AND AT STRINGER 23R. REPLACED THE FITTING IAW SRM 51-72-11 AND DWG D534-80020.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1292 BETWEEN FRAMES 12-24 . REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112821.

Part: SUPPORT BRACKET — CORRODED (FRAME 26) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND A CRACK ON SUPPORT BRACKET FOUR THE FWD CARGO DOOR ACTUATOR BETWEEN Y-1292 AND Y-765 FRAME 26 . REPLACED THE SUPPORT BRACKET IAW SRM 51-72-11 AND DWG D53230321.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-24) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1292 LOCATED BETWEEN FRAMES 12 TO 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, DRAWINGS D53112812, D53110920, AND D53110984.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK, Y1292 LOCATED BETWEEN FR 36 TO FR 41. EVALUATED AND FOUND OUT LIMITS ON JC 2500-2031. REPLACED SEAT TRACK Y1292 LOCATED BETWEEN FR 36 TO FR 41 FLOOR STRUCTURE PAX CABIN IAW SRM 51-72-11 AND DWG D53370500.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 LOCATED BETWEEN FRAMES 41 TO 47. EVALUATED AND FOUND OUT LIMITS ON JC 2500-2031. REPLACED SEAT TRACK Y1292 BETWEEN FR 41 TO FR 47 FLOOR STRUCTURE PAX CABIN IAW SRM 51-72-11 AND DWG D53370500.

Part: WEB — CORRODED (FRAMES 20-24) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON WEB -Y1732 LOCATED BETWEEN FRAMES 20 - 24. REPLACED THE WEB IAW SRM 51-72-11 AND DWG D53112783.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT AT Y-1732 BETWEEN FRAMES 65 - 66. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG NR D53470150.

Part: FRAME — CRACKED (FRM 68) · airframe 70,045 hrs · 31,830 cycles

PERFORM VISUAL INSPECTION ON AREA AND FOUND CRACK ON SECTION CONNECTION LOCATED ON FRAME 68 AND STR 23L AFT PAX CABIN. REPLACED SECTION CONNECTION LOCATED ON FR 68 AND STR 23L AFT PAX CABIN IAW SRM 51-72-11 AND DWG D53470150.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-24) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y189 BETWEEN FRAMES 20 - 24. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112834.

Part: FLOOR SUPPORT — CORRODED (FRAMES 12-16) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT Y503.2 BETWEEN FRAMES 12 - 16. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112825.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON THE FLOOR SUPPORT Y765 BETWEEN FRAMES 66+5 - 70. REPLACED THE FLOOR SUPPORT IAW SRM 320 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 70,045 hrs · 31,830 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765 BETWEEN FRAMES 64 - 66+5. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472000.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,986 hrs · 31,344 cycles

DURING EMERGENCY SYSTEM TEST, RECEIVED BATTERY EMERGENCY LIGHT MESSAGE. MAINTENANCE REPLACED EMERGENCY LIGHT BATTERY PACK AT LT EMERGENCY EXIT. FUNCTIONAL CHECKED NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 66,216 hrs · 29,991 cycles

DURING NON ROUTINE CHECK, FOUND FWD LT EMERGENCY BATTERY FAILED. REPLACED BATTERY AND FUNCTIONAL CHECKED NORMAL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,472 hrs · 29,569 cycles

DURING SERVICE CHECK, FOUND CIDS FAULT AT AFT LT UNIT, MANY ESCAPE PASSNGER LIGHTS INOPERATIVE. MX REPLACED 13WL EPSU AND OPS CHECKED NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,737 hrs · 29,190 cycles

DURING NON ROUTINE CHECK, FOUND AFT RED ESCAPE PATH LIGHT AT 9C INOPERATIVE. MX REPLACED AFT LIGHT ASSY AT 9C AND OPS CHECK WAS NORMAL.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,940 hrs · 28,815 cycles

EMERGENCY EXIT SIGNS DID NOT ILLUMINATE WHEN GEAR DOWN ON LANDING. MX REPLACED EPSU AND BATTERY AT 2L DOOR AND FUNCTIONAL CHECKED NORMAL.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHT) · airframe 63,945 hrs · 28,817 cycles

DURING INSPECTION, FOUND FLOOR/AISLE EMERGENCY ESCAPE PATH LIGHT AT 14C INOPERATIVE. INSPECT WIRE HARNESS FOR DAMAGE FLAT SPOTS CRIMPS OR SHARP BENDS, CHECK BULB AND REPLACE, MAY NEED 32-3300-3-0586. FOUND BROKEN WIRE ALONG WIRE HARNESS. TERMINATED NEW QUICK DISCONNECT MODULE ASSY IAW EPSM 20-48. PERFORMED OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,803 hrs · 28,749 cycles

EMERGENCY OVERHEAD LIGHTS AFT INOPERATIVE. R & R EPSU AND BATTERY PACK IAW AMM 33-51-38. OPS CHECK NORMAL. TEST GOOD. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,755 hrs · 28,726 cycles

DURING LANDING, F/A REPORTS LIGHTS OVER REAR EXIT DOORS FAILED TO COME ON WHEN GEAR COMES DOWN. MX REPLACED EPSU AT 13WL, BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 63,592 hrs · 28,641 cycles

ROW 17 AB SEAT EMERGENCY INOPERATIVE. WIRE CONNECTOR PULLED APART IN OUTER SEAT TRACK . REPAIRED WIRING AT SEAT ROW 17A & B. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,287 hrs · 28,486 cycles

DURING NON ROUTINE, EMERGENCY LIGHTS TEST IAW SERVICE CHECK FAULTS "INT LOADS EMERGENCY L" MX REPLACED INOPERATIVE BULBS AND RESET FWD ESPU. FUNCTIONAL CHECK WAS NORMAL.

Part: CONTROL UNIT — FAILED (EMERGENCY LIGHTS) · airframe 62,729 hrs · 28,194 cycles

DURING EMERGENCY LIGHT TEST, THE AFT LT UNIT FAULT. MAINTENANCE REPLACED UNIT AND FUNCTIONAL CHECK WAS NORMAL.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 62,483 hrs · 28,078 cycles

FOUND FLOOR EMERGENCY LIGHT AT ROW 19 INOPERATIVE. REMOVED AND REPLACED WIRE HARNESS PER ESPM. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,275 hrs · 27,963 cycles

DURING NON ROUTINE CHECK, FOUND SEVERAL EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RELAMPED AND FUNCTIONAL CHECKED NORMAL. AIRCRAFT RETURNED TO SERVICES.

Part: WIRE — BROKEN (CABIN) · airframe 6,247 hrs · 2,727 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 16 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT FLOOR CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 5,854 hrs · 2,547 cycles

DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 17 ABC INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 4,924 hrs · 2,129 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHTS AT ROWS 13-15, 18-20 AND 24-26 INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY UNIT 13WL AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: EPSU — INOPERATIVE (CABIN) · airframe 4,908 hrs · 2,119 cycles

DURING NON ROUTINE CHECK, FOUND THREE SECTIONS OF EMERGENCY LIGHTS AT AFT CABIN INOPERATIVE. MAINTENANCE REPLACED LEFT AFT EPSU AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED SERVICE.

Part: EPSU — INOPERATIVE (CABIN) · airframe 60,291 hrs · 27,060 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY PATH LIGHTS INOPERATIVE. MAINTENANCE REPLACED AFT LEFT ESPU. OPERATIONALCHECK GOOD.

Part: EPSU — INOPERATIVE (CABIN) · airframe 60,198 hrs · 27,014 cycles

FLIGHT CREW REPORTED NUMEROUS EMERGENCY SEAT PATH LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE EPSU (13WL) AND SYSTEM NOW CHECKS OK.

Part: EPSU — INOPERATIVE (CABIN) · airframe 59,833 hrs · 26,836 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT ROWS 18, 19, 20, 24, 25, AND 26 WOULD NOT TEST. MAINTENANCE REPLACED EPSU UNIT AND FUNCTIONAL TEST WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 59,657 hrs · 26,758 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY PATH LIGHTS INOPERATIVE AT DIFFERENT LOCATION SEAT (13 - 16, 18 - 20 AND24 - 26). MAINTENANCE REPLACED AFT LEFT EMERGENCY POWER SUPPLY AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (CABIN) · airframe 55,235 hrs · 24,899 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 18 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT FLOOR CONNECTION AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 55,235 hrs · 24,899 cycles

DURING NON-ROUTINE CHECK, FOUND EMERGENCY LIGHT AT SEAT 16 INOPERATIVE. MX REPAIRED BROKEN WIRE AT FLOOR CONNECTION AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,804 hrs · 23,909 cycles

DURING "H" CHECK, FOUND CORROSION ON AFT CARGO COMPARTMENT BILGE SKIN AT FR 64 BETWEEN S43R AND S44R. REPAIRED PER EA 32-215807.

Part: UPLOCK SENSOR — MALFUNCTIONED (LT MLG) · airframe 46,338 hrs · 20,804 cycles

AT FLIGHT LEVEL 370, ECAM MSG: L/G DOORS NOT CLOSED, WHEELS PAGE INDICATED ALL THREE GEAR DOORS OPEN. ECAM THEN INDICATED ALL GEAR DOORS OPEN AND LEFT GEAR UNSAFE. AIRCRAFT DESCENDED TO FLIGHT LEVEL 200 AND 215 KNOTS, TO PERFORM COM RECYCLE PROCEDURE. BEFORE ATTEMPTING COM, THE GEAR DOORS CLOSED AND INDICATIONS WERE NORMAL. FLIGHT CONTINUED TO MSP AT LOWER THAN PLANNED ALTITUDE, UNDER EXPEDITED ATC HANDLING DO TO INCREASED FUEL USAGE. FLIGHT LANDED UNEVENTFULLY WITHOUT FURTHER INCIDENT. CORRECTED BY REPLACING LEFT LANDING GEAR UPLOCK SENSOR, AND NR 2 LGCIU.

Part: POWER SUPPLY — INOP (CABIN)

DURING LINE CHECK, FOUND EMERGENCY LIGHTS AT SEAT ROWS 5, 9-13, 17, 18, AND 22-24 INOPERATIVE. REPLACED POWER SUPPLY UNIT. OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING TEST OF EMERGENCY LIGHT SYSTEM, FORWARD LEFT EMERGENCY LIGHT BATTERY FAILED. MAINTENANCE REPLACED BATTERY, OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT TEST ON FLIGHT ATTENDANT'S PANEL WOULD NOT TEST. REPLACED BATTERY PACK AT AIRCRAFT RIGHT CENTER EMERGENCY EXIT DOOR, OPERATIONAL CHECK OK.

Part: BATTERY — DISHCARGED (CABIN)

DURING LINE MAINTENANCE, THE LEFT AND RIGHT EMERGENCY LIGHTS BATTERIES FAILED TO TEST. REPLACED BATTERIES, OPERATIONAL CHECK OK.

Part: ACM — SEIZED (NR 1)

FUMES PRESENT IN COCKPIT AND CABIN FOLLOWED BY A PACK ONE OVERHEAT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND THE FUMES CEASED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT AT THE ORIGINAL DESTINATION. MAINTENANCE FOUND THE NR 1 PACK AIR CYCLE MACHINE SEIZED AND A CLAMP ON THE PACK OUTLET DUCT BROKEN. REPLACED THE AIR CYCLE MACHINE AND CLAMP. LEAK AND OPERATIONAL CHECK OK.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAILS THE AFT LEFT POWER SUPPLY UNIT. REPLACED EPSU, OPERATIONAL CHECK OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING LINE MAINTENANCE, CABIN EMERGENCY LIGHTS TEST FAULTS BATT 12WL. REPLACED BATTERY PACK, OPERATIONAL CHECK OK.

Part: THRUST LINKS — WEAR MARKS (FWD ENG MOUNT)

DURING OVERNIGHT MAINTENANCE, THE NR 1 ENGINE INBOARD AND OUTBOARD FORWARD ENGINE MOUNT THRUST LINKS AND THE NR 2 ENGINE OUTBOARD FORWARD ENGINE MOUNT THRUST LINKS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-21-06, FIG 803. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.003 INCH TO 0.005 INCH. REPAIRS ACCOMPLISHED PER NWA EA 32-095306 AND EA 32-095307.