N332NW

Part: UNKNOWN — NONE · airframe 88,325 hrs · 41,588 cycles

SHIP 3232 NEED TO COMPLY WITH INSPECTION AREA FOR WC 5311-01244-01A, SB A320-53-1491 R0, EASA PAD 21-090 (LH SIDE). CORRECTIVE ACTION: COMPLIED WITH. (2500127)

Part: REPAIR — NONE · airframe 88,325 hrs · 41,588 cycles

SHIP 3232 PREVIOUS REPAIR LOCATED IN INSPECTION AREA FOR WC 5311-01244-01B, SB A320-53-1491 R0, EASA PAD 21-090 (RH SIDE). CORRECTIVE ACTION: COMPLIED WITH ERA 603790-14AD. (2499626)

Part: FRAME — NONE · airframe 88,325 hrs · 41,588 cycles

SHIP 3232 AD 2022-15-05, ER/A 603790-14AD SECTION I AND SECTION III ISSUED FOR LH FR68 WEB AT DOOR- STOP FITTING 1. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH ER/A 603790-14AD SECTION I. (2499230)

Part: FRAME — NONE · airframe 88,325 hrs · 41,588 cycles

SHIP 3232 AD 2022-15-05, ER/A 603790-14AD SECTION II AND SECTION IV ISSUED FOR LH FR68 WEB AT DOOR- STOP FITTING 1. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH ER/A 603790-14AD SECTION II. (2499236)

Part: DOOR FRAME — DAMAGED (FRM 68) · airframe 88,325 hrs · 41,588 cycles

SHIP 3232 FITTING REPAIR INSTALLED ON R2 DOOR SURROUND AFT FRAME FR68, LH AT STGR-22 AND DOOR STOP 1 PER ERA 587207-14AD REV A. FOLLOW-ON INSPECTIONS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH INSPECTION. (2495951)

Part: DOOR FRAME — DAMAGED (R2 DOORWAY) · airframe 88,325 hrs · 41,588 cycles

SHIP 3232 FITTING REPAIR INSTALLED ON R2 DOOR SURROUND AFT FRAME FR68, LH AT STGR-22 AND DOOR STOP 1 PER ERA 587207-14AD REV A. FOLLOW-ON INSPECTIONS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH INSPECTION. (2495945)

Part: NONE — NONE · airframe 88,097 hrs · 41,457 cycles

SHIP 3232 2DC PSU O2 PANEL WOULD NOT DROP. CORRECTIVE ACTION: R/R PSU WIRE HARNESS PER DELTA W/C 2527-01041-02. OPS CHK GOOD. (9395863)

Part: NONE — NONE · airframe 87,687 hrs · 41,220 cycles

SHIP 3232 AFT LT LAV O2 PANEL DID NOT DROP DURING TEST. CORRECTIVE ACTION: REPACKED MASKS AND REPLACED STOW SWITCH. OPS CHECK GOOD. (9066639)

Part: HOUSING — BROKEN · airframe 87,462 hrs · 41,083 cycles

SHIP 3232 SEAT MOUNTED EMERG LIGHT HOUSING AT ROW 27 DEF BROKEN. CORRECTIVE ACTION: HOUSING TO BE REPLACED PER A320 AMM 33-51. (9189024)

Part: NONE — NONE · airframe 86,849 hrs · 40,669 cycles

SHIP 3232 DURING TEST SEAT 23 ABC PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8755886)

Part: NONE — NONE · airframe 86,849 hrs · 40,669 cycles

SHIP 3232 DURING TEST SEAT 17 DEF PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (8755887)

Part: LIGHT — INOPERATIVE · airframe 85,616 hrs · 39,903 cycles

SHIP 3232 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT SEAT 19D. CORRECTIVE ACTION: RESUCURED LIGHT ASSY AS SEAT 19D. OK FOR SERVICE. (2008041)

Part: LATCH — LACK OF LUBE (GIRT BAR) · airframe 85,030 hrs · 39,542 cycles

SHIP 3232 ENTRY DOOR ARMING LEVER HARD TO OPERATE. LOCATION: R1. CORRECTIVE ACTION: CLEANED AND LUBRICATED R1 DOOR GIRT BAR LATCHES. LUBED DOOR ARMING LEVER. R1 DOOR ARMS WITH NORMAL EFFORT AND CONSISTENT INDICATION OF ECAM. OK FOR SERVICE.

Part: SKIN — CORRODED (RT WING TE) · airframe 84,794 hrs · 39,354 cycles

SHIP 3232 CORROSION UPPER SURFACE UPPER SKIN LOCATED BTW RIB19 TO RIB20 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER PRI ER/A #592618-14 REV. O AND ER/A 592618-14 REV. ORIGINAL. (1873200)

Part: PANEL — CRACKED (VERTICAL STAB LE) · airframe 84,794 hrs · 39,354 cycles

SHIP 3232 CRACK LEADING EDGE ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 322AL AS PER ER/A 592557-14 REVISION ORIGINAL 07-JUL-21 AND ERA 592257-14 PRI REV.0 AND A320 SRM TASK 55-32-11. (1869484)

Part: WEB — CORRODED (RT NACELLE) · corrosion level 2 · airframe 84,794 hrs · 39,354 cycles

SHIP 3232 CORROSION HORIZONTAL WEB AFT MOVABLE FAIRING ON RH PYLON. CORRECTIVE ACTION: REPLACED HORIZONTAL WEB AFT MOVABLE FAIRING ON RH PYLON AS PER SRM A320 51-72-11. JOB COMPLETE. (1865794)

Part: SKIN — CORRODED (RT WING) · airframe 84,794 hrs · 39,354 cycles

SHIP 3232 CORROSION UPPER SURFACE UPPER SKIN LOCATED BTW RIB24 TO RIB25 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: EVALUATED REWORKED AREA ON UPPER SURFACE UPPER SKIN LOCATED BTW RIB24 TO RIB25 TRAILING EDGE AREA ON RH WING AND FOUND WITHIN LIMITS AS PER A320 SRM 57-21-11. (1860757)

Part: PANEL — NO TEST (SEAT 14ABC) · airframe 84,524 hrs · 39,196 cycles

SHIP 3232 DURING TEST SEAT 14ABC PSU OXYGEN PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7283068)

Part: PANEL — NO TEST (SEAT 22ABC) · airframe 84,524 hrs · 39,196 cycles

SHIP 3232 DURING TEST SEAT 22ABC PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7283069)

Part: LIGHT — DETACHED (SEAT 31D) · airframe 83,842 hrs · 38,890 cycles

SHIP 3232 SEATS 31D 17D 15D EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. CORRECTIVE ACTION: RESECURED LIGHTING. OK FOR SERVICE. (1737306)

Part: FITTING — CRACKED (RT WING) · airframe 84,794 hrs · 39,354 cycles

SHIP 3232 ER/A 588785-14AD IS GENERATED FOR THE RH AFT SPAR TO PINTLE FITTING JOINT AT HOLE 16R. (CRACK) : CORRECTIVE ACTION: PER ER/A #588785-14AD REV.ORIGINAL. OK TO CONTINUE ON MONITOR. REPETITIVE INSPECTION IS REQUIRED 25,200 FLIGHT CYCLES OR 41,400 FLIGHT HOURS, WHICHEVER OCCURS FIRST, JOB COMPLETE. MONITOR CONTINUED. (1681751)

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 83,307 hrs · 38,638 cycles

EMERGENCY ESCAPE PATH LIGHT AT SEAT 19DEF DAMAGED. CORRECTIVE ACTION: R & R EMERGENCY LIGHT HOUSING AND TESTED LIGHTING SYSTEM. OK FOR SERVICE.

Part: WEB — CRACKED (FRM 68) · airframe 88,325 hrs · 41,588 cycles

SHIP 3232 ER/A 587207-14AD ISSUED FOR LH FR68 WEB AT STOP 1 CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 587207-14AD REV A. (1587431)

Part: DOOR FRAME — DAMAGED (FRM 68) · airframe 88,325 hrs · 41,588 cycles

SHIP 3232 ER/A 587207-14AD ISSUED FOR LH FR68 WEB AT DOOR STOP 1 CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 587207-14AD. (1587429)

Part: BATTERY PACK — NO TEST (EMREGENCY LIGHTS) · airframe 81,928 hrs · 37,889 cycles

EMERGENCY TEST FAILS LT BATTERY, REPLACED LT BATTERY FOR EPSU

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +4 INCH OF RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 11 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FR 36 AND -Y1292+4" OF RT SIDE IN FWD EDGE CARGO COMPARMENT AS PER PRI 580780-14 REV 0 AND #580780-14AD REV ORIGINAL.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292+5 INCH OF RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 11 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FR36 AND -Y1292+5" OF RT SIDE IN FWD CARGO COMPARTMENT ASPER PRI # 580780-14 REV 0 AND ER/A #580780-14AD REV ORIGINAL.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +7 INCH OF THE RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FR36 AND -Y1292+7" OF THE RT SIDE IN FWD CARGO COMPARTMENT ASPER PRI #580780-14 REV 0 AND ER/A #580780-14AD REV ORIGINAL.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +6 INCH OF RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION ARE 6 AND 12 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FRAME 36 AND -Y1292+6 INCH OF RT SIDE IN FWD CARGO COMPARTMENT PRI #580780-14 REV 0 AND ER/A #580780-14AD REV ORIGINAL.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE AT FRAME 36 AND Y1292 + 5 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 AND 7 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC. AT FR.36 AND +Y1292+5" LT SIDE FWD CARGO COMPARTMENT AS PER PRI #580780-14 REV 0 AND ERA #580780-14AD REV ORIGINAL.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FR36 AND -Y1292+3 INCH ON RT SIDE (CRACK INDICATION IS 11 O'CLOCK) IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FR 36 AND -Y1292+3" ON RT SIDE IN FWD CARGO COMPARTMENT AS PER PRI #580780-14 REV 0 AND ER/A #580780-14AD REV ORIGINAL.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION STRINGER 41R LOWER FLANGE, BTW FRAME 25 AND FRAME 28 IN FWD CARGO COMPARTMENT (1 EA), REPLACED STRG 41R LOC BTW FR 24 TO FR 30 IN FWD CARGO COMPARTMENT AS PER SRM 51-72-11 AND DRAWING #D53231586.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FR36 AND -Y1292+2INCH RT SIDE (CRACK DIRECTION IS 10 O'CLOCK) IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DUCT MEMBRANE LOC AT FR 36 AND -Y1292+2 INCH RT SIDE IN FWD CARGO COMPARTMENT AS PER PRI #580780-14 REV 0 AND ER/A #580780-14AD REV ORIGINAL.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON INTERNAL STRUCTURE ON TITANIUM ANGLE LOCATED AT FRAME 36 AND Y1292+ 1 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (2 EA) (CRACK LENGTH 0.923 AND 0.498 INCH APPROX), PERFORMED REPAIR INSTRUCTIONS ON INTERNAL STRUCTURE ON TITANIUM ANGLE LOCATED AT FR.36 AND +Y1292+1" OF LT SIDE IN FWD CARGO COMPARTMENT AS PER PRI #580780-14 REV 0 AND ER/A #580780-14AD REV ORIGINAL.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND Y1292 + 2 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 AND 6 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FSTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FRAME 36 AND Y1292+2 INCH OF LT SIDE IN FWD CARGO COMPARTMENT ASPER PRI # 580780-14 REV 0 AND ER/A #580780-14AD REV ORIGINAL.

Part: SPAR — CORRODED (LT WING) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION FALSE SPAR BOX LOCATED ON FITTING AT RIB 5 INTERNAL AREA ON LT WING, PERFORMED REPAIR INSTRUCTIONS ON FALSE SPAR BOX LOCATED ON FITTING AT RIB 5 INTERNAL AREA ON LT WING AS PER PRI 581186-14 REV 0 AND REV 1 AND ER/A 581186-14 REV ORIGINAL.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND Y1292 +3 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF PRESSURE DECK MEMBRANE LOC AT FR36 AND +Y1292+3" LT SIDE FWD CARGO COMPARTMENT ASPER PRI # 580780-14 REV 0 AND ER/A # 580780-14AD REV ORIGINAL.

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +7 INCH OF THE RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FR36 AND -Y1292+7" OF THE RT SIDE IN FWD CARGO COMPARTMENT ASPER PRI #580780-14 REV 0 AND ER/A #580780-14AD REV ORIGINAL.

Part: SPAR — CORRODED (RT WING) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION FALSE SPAR BOX SKIN LOCATED RIB5 BOTTOM SURFACE ON RT WING, PERFORMED TIME-LIMITED REPAIR FALSE SPAR BOX SKIN LOCATED RIB 5 BOTTOM SURFACE ON RT WING AS PER PRI 581187-14 REV 0 AND ER/A 581187-14 REV ORIGINAL.

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION CLEAT AT LEVEL OF FR31 AND BTW STRG 41R AND STRG 42R IN FWD CARGO COMPARTMENT (1 EA), REPLACED CLEAT AT LEVEL OF FR31 AND BTW STR 41R AND STR 42R IN FWD CARGO COMPARTMENT (1E/A) AS PER SRM 51-42-00, 51-72-11 AND DRAWING D53230514

Part: CLEAT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION CLEAT BTW STR 43L TO 42L AT LEVEL OF FR33 IN FWD CARGO COMPARTMENT (1 EA), REPLACED CLEAT BTW STR 43L TO STR 42L LEVEL FR33 FWD CARGO COMPARTMENT (1E/A) AS PER SRM 51-42-00, 51-72-11 AND DRAWING D5323039820001.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION STRINGER 42L BTW FR27 TO FR31 IN FWD CARGO COMPARTMENT, REPLACED STRINGER LOC. STRINGER 42L BTW FR27 TO FR31 IN FWD CARGO COMPARTMENT AS PER SRM 51-72-11 AND 51-42-11. DRAWING D53231626.

Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION INTERNAL STRUCTURE (SKIN AREA), LOC FRAME 26+3INCH, STRINGER 40R, IN FWD CARGO COMPARTMENT (1 EA), REPLACED STRAP FITTING ON INTERNAL STRUCTURE FR 26 BTW 40R TO STR 41R AS PER SRM 51-72-11 AND SRM 51-42-11 AND DWG #D53231380.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK INDICATION ON FRAME 16 LT IN LOWER INBOARD HOLE OF DOOR STOP FITTING 7 CRACK POSITION 3 O'CLOCK AT FWD GALLEY AREA, REPLACED FITTING LOCATED ON FR 16 ON DOOR STOP FITTING #7 LT SIDE ASPER SRM 51-72-11 AND DWG D53112300.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION SEAT TRACK -Y765 PREVIOUSLY REWORKED AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y765 BTW FR 41 TO FR 47 IN PASSENGER CABIN ASPER SRM 53-31-15-02A AND 51-72-11 AND DWG #D53472554.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION FLOORBEAM -Y1292 AT LEVEL OF FR 68 AT AFT GALLEY AREA, REPLACED FLOORBEAM -Y1292 LOC. FR68 AT AFT GALLEY AREA ASPER SRM 51-72-11 AND 51-42-11, DWG # D53472000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION FLOORBEAM -Y1292 BTW FR 67 AND FR 68 FLOOR STRUCTURE AT AFT GALLEY AREA, REPLACED FLOORBEAM-Y1292 LOC. FR 68 AT AFT GALLEY AREA AS PER SRM 51-72-11 AND 51-42-11, DWG # D53472000.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION FLOORBEAM -Y765 AND FR 20 AT FWD GALLEY AREA, REPLACED FLOORBEAM -765 LOC FR 12 TO FR 24 AT FWD GALLEY AREA ASPER SRM 51-72-11 AND 51-42-11 DWG 53112812.

Part: WEB — CRACKED (FUSELAGE) · airframe 80,973 hrs · 37,404 cycles

CRACK FLOOR STRUCTURE WEB BTW FR 68 TO FR 69 AT LEVEL STR-23L SIDE AT AFT GALLEY AREA, REPLACED FLOOR STRUCTURE WEB BTW FR 68 TO FR 69 AT LEVEL STR 25L SIDE AT AFT GALLEY AREA (1EA) ASPER SRM 51-72-11 AND DWG # D53480020.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION SEAT TRACK Y1292 PREVIOUSLY REWORKED AND EVALUATED WITH CARD 2500-20 31-DE AND FOUND OUT LIMITS, REPLACED SEAT TRACK Y1292 LOCATED BTW FR41 TO FR47 IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG # D57130146.

Part: FLOOR SUPPORT — CORRODED (FRAME 20) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION FLOOR SUPPORT -Y1292 AND FR20 AT FWD GALLEY AREA, REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 TO 24 IAW SRM A320 51-72-11, DRAWING D53212368, AND DWG D53112812.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION SEAT TRACK Y1292 PREVIOUSLY REWORKED AND EVALUATED WITH CARD 2500-2031-DE AND FOUND OUT LIMITS, REPLACED SEAT TRACK Y1292 LOCATED BETWEEN FR36 TO FR41 IN PASSENGER CABIN AS PER SRM 51-72-11 AND DWG # D53371112.

Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORRODED FLOOR SUPPORT, -Y765, FRAME 68 IN THE AFT GALLEY AREA, REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 66 & 70 IAW DWG D534720000, ISSUE AF, AND SRM 51-72-11.

Part: SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 80,973 hrs · 37,404 cycles

CORROSION LOWER SILL LOC AT LEVEL OF FR 68 RH SIDE AT AFT GALLEY AREA, PERFORMED PERMANENT REPAIR LOC ON LOWER SILL AT LEVEL OF FR 68 R /H SIDE AT AFT GALLEY AREA ASPER SRM A320 53-41-14-300-001

Part: BATTERY — INOPERATIVE (CABIN) · airframe 80,865 hrs · 37,353 cycles

L-AFT EPSU BATT INOP, R/R EPSU-BATT.

Part: ARM — NOT REPORTED (VSV ACTUATOR) · airframe 80,386 hrs · 37,102 cycles

DIVERTED DUE TO A NUMBER ONE ENGINE COMPRESSOR STALL. ENGINE HAS RECOVERED. CORRECTIVE ACTION: REPLACED BOTH VSV ACTUATION ARM ASSY PERM56-5A ESM 72-32-00 REV 65 (429382) AND REPLACED HMU AND REPLACED T25 SENSOR

Part: BATTERY — FAILED (CABIN) · airframe 80,230 hrs · 37,029 cycles

EMERGENCY LIGHT TEST FAILED FWD LEFT BATTERY, REPLACED FWD LEFT EMERGENCY BATTERY.

Part: APU — SMOKE (APU BAY) · airframe 78,638 hrs · 36,287 cycles

SMOKE/FUME IN CABIN. MCC REQUESTING APU REPLACEMENT. REPLACED APU.

Part: LIGHT — DAMAGED (SEAT 3C) · airframe 75,711 hrs · 34,838 cycles

SEAT 3C EMERGENCY LIGHT DAMAGED, REPLACED THE LIGHT.

Part: LIGHT — FAULTED (CABIN) · airframe 75,034 hrs · 34,500 cycles

RIGHT EMERGENCY LIGHT EXTERNAL FAULT, REPLACED 1 OVERWING LAMP.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 74,124 hrs · 34,064 cycles

L2 DOOR EMERGENCY LIGHT EXIT SIGN INOPERATIVE, FOUND CONNECTOR PLUG DISCONNECTED BEHIND PANEL RECONNECTED

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 74,096 hrs · 34,050 cycles

EMERGENCY LIGHTS EXT LOADS FWD L FAULT ON CIDS PANEL, FOUND GROUND WIRE BROKEN BETWEEN PIN "B" ON 2871VC TO PIN "K" ON 2819VC, REPLACED WIRE (LOG 7482002)

Part: SLIDE — MALFUNCTIONED (RT OVERWING) · airframe 73,937 hrs · 33,978 cycles

RT OVERWING ESCAPE SLIDE LIGHTING INOPERATIVE. REPLACED THE SLIDE.

Part: WIRE — OUT OF POSITION (CABIN) · airframe 73,409 hrs · 33,716 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. FOUND WIRES AT AREA LIGHT AND EXIT SIGN SWAPPED, CORRECTED.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 73,139 hrs · 33,564 cycles

SCRATCH ON EXTERNAL SKIN OF PASSENGER CREW DOOR FROM BEAM 2 TO BEAM 3 AND BETWEEN XP 820 TO XP 712 AT AFT GALLEY AREA RH SIDE, REPAIRED IAW ER/A 550213-14AD REV. ORIGINAL SECTION I AND PRI REV. 0 AND 1.

Part: STRINGER — CORRODED (FRAME 33) · airframe 73,139 hrs · 33,564 cycles

CORROSION ON STRINGER 43L FR 33+6 " IN FWD CARGO BAY. REPAIRED THE STRINGER IAW PRI 521412-14 REV. 1 AND ER/A 521412-14 REV B SECTION III.

Part: SHEAR TIE — DAMAGED (FRAME 24) · airframe 73,134 hrs · 33,562 cycles

ELONGATED HOLE ON SHEAR TIE IN FWD CARGO COMPARTMENT ON FRAME 24A BETWEEN STRINGER 41R TO STRINGER 42R, REPLACED THE SHEAR TIE IAW SRM 51-72-11 AND DRAWING D53231586.

Part: STRUCTURE — CORRODED (FRAMES 67-68) · airframe 73,134 hrs · 33,562 cycles

CORROSION ON LOWER SILL BETWEEN FRAMES 67 TO 68. REPLACED LOWER SILL IAW SRM 51-72-11 AND DRAWING D53480020.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,134 hrs · 33,562 cycles

CORROSION ON FLOORBEAM -Y1225 TO -Y1165 BETWEEN FRAME 66+5" TO FRAME 67+18" AT AFT GALLEY AREA. REPLACED FLOORBEAM -Y1165 BETWEEN FRAME 66+5" TO FRAME 67+18" AT AFT GALLEY AREA AS PER SRM 51-72-11 AND DRAWING D53172000. FLOORBEAM WAS OUT OF LIMITS AS PER SRM 53-41-15 PARAGRAPH 3D MEASURES OF REWORK L=1.570" W=0.625" D=0.040".

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,134 hrs · 33,562 cycles

CORROSION ON FLOORBEAM +Y1225 TO +Y1165 BETWEEN FRAME 66+5" TO FRAME 67+18" AT AFT GALLEY AREA. REPLACED FLOORBEAM +1165 BETWEEN FRAME 66 + 5" TO FRAME 67 + 18" AT AFT GALLEY AREA AS PER SRM 51-72-11 AND DRAWING D5317200.

Part: STRUCTURE — DAMAGED (HORIZONTAL STAB) · airframe 70,235 hrs · 32,120 cycles

THE LT HORIZONTAL STAB L/E WAS DAMAGED IN A HAILSTORM. REPAIRED THE LT L/E.

Part: SKIN — DENTED (NR 4 SLAT) · airframe 70,128 hrs · 32,057 cycles

THE NR 4 RT SLAT WAS FOUND DENTED ALONG THE L/E.

Part: SKIN — CORRODED (FRAMES 25-26) · airframe 69,440 hrs · 31,709 cycles

DURING INSPECTION, FOUND CORROSION WITHIN WIFI AREA FRAME 25 TO 26 STRINGER 44. INSTALLED STR IAW SRM 53-21-13, C/W PRI/ERA 535082-14AD, REV O.

Part: STRINGER — CORRODED (FRAMES 25-26) · airframe 73,438 hrs · 33,735 cycles

STRINGER 43R HAS CORROSION AT FRAMES 25 TO 26. REMOVED AND REPLACED THE STRINGER IAW SRM 53-21-13.

Part: STRINGER — DAMAGED · airframe 73,438 hrs · 33,735 cycles

DURING INSPECTION, FOUND STRINGER 42R DAMAGED. REMOVED AND REPLACED THE STRINGER IAW ER/A.

Part: STRINGER — CORRODED (FRAMES 28-30) · airframe 65,532 hrs · 29,810 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 42R BETWEEN FRAMES 28+11-30+11 IN FWD CARGO BAY. PERFORMED PERMANENT REPAIR, FABRICATION ON SUPPORT STRINGER, DOUBLER IAW ER/A 521427-14.

Part: WEB — CORRODED (FRAME 58-59) · airframe 65,532 hrs · 29,810 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY LOCATED AT STRINGER 38R AND BETWEEN FRAME 58-59. PERFORMED REPAIR ON WEB.

Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · airframe 65,532 hrs · 29,810 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR PLATE BETWEEN FRAME 69-70 AT STRINGER 23R. REPLACED SHEAR PLATE IAW SRM 51-72-11AND DWG D53470100.

Part: WEB — CORRODED (FRAMES 56-57) · airframe 65,532 hrs · 29,810 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY AT STRINGER 38R AND BETWEEN FRAMES 56-57. REPAIRED.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,264 hrs · 33,636 cycles

CORROSION ON STRINGER 31R IN AFT CARGO COMPARTMENT LOCATED BETWEEN FR 64 TO FR 65. REPLACED STRINGER 31R LOCATED BELOW FR 64 TO FR 67 IN AFT CARGO COMPARTMENT AS PER SRM 51-72-11 AND DRAWING D53480505.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,264 hrs · 33,636 cycles

CORROSION ON STRINGER 43L AT FR 33+6" FWD CARGO COMPARTMENT. REPAIR PER ER/A NR 521412-14 REV ORIGINAL SECTION II.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,264 hrs · 33,636 cycles

CORROSION ON STR 41R AT FR31+4" FWD CARGO COMPARTMENT. REPAIR PER ER/A 521412-14 REV ORIGINAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,264 hrs · 33,636 cycles

CORROSION ON STRINGER 41R BETWEEN FR 29 TO FR30+15" FWD CARGO COMPARTMENT. REPAIR PER ER/A 521412-14 REV ORIGINAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,264 hrs · 33,636 cycles

CORROSION ON STR 43R LOCATED BETWEEN FR 24A TO FR 27+7" FWD CARGO COMPARTMENT. REPAIR PER ER/A 521412-14 REV ORIGINAL SECTION II.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,264 hrs · 33,636 cycles

CORROSION ON STR 42R LOCATED BETWEEN FR24A TO FR30+6" FWD CARGO COMPARTMENT. REPAIR ER/A 521412-14 REV ORIGINAL.

Part: WEB — CORRODED (CARGO BAY) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY. STRINGER 38L AND BETWEEN FRAMES 56-57. REPAIRED IAW ER/A 52142014.

Part: STRINGER — CORRODED (FRAMES 56-57) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 43L OF AFT CARGO BAY, BETWEEN FRAMES 56-57. REPAIRED STRINGER IAW SRM 53-00-13, FIG 201 PARA 4.

Part: WEB — CORRODED (FRAMES 28-29) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON WEB LOCATED BETWEEN FRAMES 28-29, STRINGERS 42-44L. REPLACED WEB IAW SRM 51-72-11 AND DWG D53230861.

Part: STRINGER — CORRODED (FRAMES 30-31) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 41L BETWEEN FRAME 30+16 - 31+6. REPAIRED STRINGER IAW SRM 53-00-13, FIG. 201, SHEET 2.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE BETWEEN STRINGERS 42-43 LEFT FRAME 30, REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D532-31212.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE AT FRAME 31 BETWEEN STRINGERS 40-41 LEFT. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231611.

Part: STRINGER — CORRODED (FRAMES 24-30) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 42L BETWEEN FRAMES 24-30+16". REPLACED STRINGER IAW SRM 51-72-11, DWG D53231212, & D53230306.

Part: STRINGER — CORRODED (BS 26-34) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ALONG OF STRINGER 40L BETWEEN FRAMES 26-34. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53231212 AND PERFORMED PERMANENT REPAIR IAW SRM 53-00-13.

Part: STRINGER — CORRODED (FRAMES 27-30) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 44, BETWEEN FRAMES 27+15" - 30+17" IN FWD CARGO BAY. REPLACED STRINGER IAW SRM 51-72-11 AND DWG D53231626.

Part: SUPPORT — CORRODED (FRAMES 28-30) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SUPPORT, AT STRINGER 44 BETWEEN FRAMES 28+10" - 30+10 IN FWD CARGO BAY. REPLACED SUPPORT IAW SRM 51-72-11 AND DWG. D53231626.

Part: FITTING — CORRODED (EMERGENCY EXIT) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON LOWER FITTING LOCATION AT FWD CURVE EDGE OF EMERGENCY DOOR. REPLACED LOWER FITTING IAW SRM 51-72-11 AND DWG D52279040.

Part: FLOORBEAM — NOT REPORTED (FUSELAGE) · airframe 73,264 hrs · 33,636 cycles

FLOORBEAM LOCATED FWD PAX CABIN LEVEL Y-254 BETWEEN R16 AND FR20 WITH MEASURE: L=0.020" W=0.010" AND D=0.009". REPAIR PER ER/A 14-521421.

Part: SEAT TRACK — CORRODED (FRAMES 24-35) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK BETWEEN FRAMES 24 TO 35, Y1292. REPLACED SEAT TRACK IAW SRM A320 51-72-11 AND DWG D532131181.

Part: FITTING — CORRODED (FRAME 56) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FITTING AT FRAME 56 STRINGER 44 IN AFT CARGO BAY. REPLACED FITTING IAW 51-72-11 AND DWG D53470260.

Part: STRINGER SPLICE — CORRODED (FRAME 30) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER SPLICE 41L AT FRAME 30+16" IN FWD CARGO BAY. REPLACED STRINGER SPLICE IAW SRM 51-72-11 AND DWG D53231375.

Part: BEAM — GOUGED (EMERGENCY EXIT) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND GOUGE ON INTERNAL STRUCTURE OF AFT EDGE BEAM LOCATED AT EMERGENCY DOOR 843. REPLACED AFT EDGE BEAM LOC AT EMERGENCY DOOR 843 IAW SRM 51-72-11 AND DWG D52279010.

Part: SUPPORT BRACKET — CORRODED (FRAME 29) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SUPPORT BRACKET LOCATED AT FRAME 29, S41R FWD CARGO BAY. REPLACED SUPPORT BRACKET IAW SRM 51-72-11 AND DWG D53231685.

Part: STRINGER — CORRODED (FRAMES 24-30) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 41L, BETWEEN FRAMES 24-30+16 IN FWD CARGO BAY. REPLACED STRINGER IAW SRM A320 51-72-11 AND DWG D53231212.

Part: SUPPORT FITTING — CORRODED (FRAME 65) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SUPPORT FITTING IN AFT CARGO BAY, FRAME 65 BETWEEN S43L-43R. REPLACED SUPPORT FITTING IAW SRM 53-72-11 AND DWG N. D534800 54.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765, FRAMES 47, 51, & 64. FOUND OUT LIMITS2. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472030.

Part: FLOOR SUPPORT — CORRODED (FRAMES 20-23) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-189, BETWEEN FRAMES 20 AND 23. REPLACED FLOOR SUPPORT IAW SRM 51-72-11, DWG D53111406.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE AT FRAME 32 BETWEEN S43-44L IN FWD CARGO BAY. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231626.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 65,531 hrs · 29,809 cycles

DURING SPECTION, FOUND CORROSION ON SHEAR TIE FRAME 31 BETWEEN S42-43R IN FWD CARGO BAY. REPLACED SHEAR TIE AND FASTENERS IAW SRM 51-72-11 AND DWG D532-31611.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE AT FRAME 28 BETWEEN S40-41L IN FWD CARGO BAY. REPLACED SHEAR TIE AND FASTENERS IAW SRM 51-72-11 AND DWG D532-31375.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE AT FRAME 28 BETWEEN S41-42L IN FWD CARGO BAY. REPLACED SHEAR TIE AND FASTENERS IAW SRM A320 51-72-11 AND DWG D532-31375.

Part: STRINGER — CORRODED (FRAMES 30-34) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON STRINGER 42R LOCATED BETWEEN FRAMES 30+6 TO 34 FWD CARGO BAY. REPLACED STRINGER AND FASTENERS IAW SRM 51-72-11 AND DWG D53231212.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE BETWEEN S43-44L FRAME 29 IN FWD CARGO BAY. REPLACED SHEAR TIE AND FASTENERS IAW SRM 51-72-11 AND DWG D53231212.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 31 BETWEEN S43-44L IN FWD CARGO BAY. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231611.

Part: SHEAR TIE — CORRODED (FRAME 29) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 29 BETWEEN S42-43L IN FWD CARGO BAY. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231212.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 31 BETWEEN S40-41R FWD CARGO BAY. REPLACED SHEAR TIE AND FASTENERS IAW SRM 51-72-11 AND DWG D53231611.

Part: SHEAR TIE — CORRODED (FRAME 30) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE BETWEEN S43-44L AT FRAME 30 IN FWD CARGO BAY. REPLACED SHEAR TIE AND FASTENERS IAW SRM 51-72-11 AND DWG. D53231212.

Part: WEB — CORRODED (FRAMES 58-59) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN AFT CARGO BAY STRINGER 38L BETWEEN FRAMES 58 TO 59. REPLACED WEB AND FASTENERS IAW SRM 51-72-11 AND D53470320.

Part: WEB — CORRODED (FRAMES 33-34) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON WEB IN CARGO BAY BETWEEN FRAMES 33 - 34, S38L. REPLACED WEB IAW SRM 51-72-11 AND DWG D53230340.

Part: SHEAR TIE — CORRODED (FRAME 31) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 31 BETWEEN S42-43L IN FWD CARGO BAY. REPLACED SHEAR TIE IAW SRM 51-72-11 DWG. D53231611 AND D53230811 .

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 32 BETWEEN S41-42L. REPLACED SHEAR TIE AND FASTENERS IAW SRM 51-72-11 AND DWG D5323L 212.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 28 BETWEEN S41-42R. REPLACED SHEAR TIE IAW SRM 51-72-11AND DWG D53231582.

Part: WEB — CORRODED (FRAMES 33-34) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON WEB BETWEEN FRAMES 33-34 S38R. REPLACED WEB IAW SRM 51-72-11 AND DWG 0532-30340.

Part: SHEAR TIE — CORRODED (FRAME 32) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 32 BETWEEN S42-43L. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231212.

Part: SHEAR TIE — CORRODED (FRAME 28) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SHEAR TIE FRAME 28 BETWEEN S43-44L. REPLACED SHEAR TIE IAW SRM 51-72-11 AND DWG D53231375 & D53231616.

Part: SEAT TRACK — CORRODED (FRAMES 24-35) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765, FRAMES 24 TO 35. FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53231181 AND D53210005.

Part: SEAT TRACK — CORRODED (FRAMES 36-41) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y1292 FRAMES 36 TO 41. FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53370500.

Part: SEAT TRACK — CORRODED (FRAMES 24-35) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 BETWEEN FRAMES 24 TO 35. FOUND OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-72-12 AND DWG D53210005.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK Y1292 FRAMES 47, 51, 64. REPLACED SEAT TRACK IAW SRM 51-72-11 AND DWG D53472000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-1292, BETWEEN FRAMES 16 AND 20. REPLACED FLOOR SUPPORT IAW 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y-765, BETWEEN FRAMES 16 AND 20. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53112812.

Part: SEAT TRACK — CORRODED (FRAMES 41-47) · airframe 65,531 hrs · 29,809 cycles

CORROSION FOUND ON SEAT TRACK, Y1292 BETWEEN FRAMES 41 - 47. FOUND OUT OF LIMITS. REPLACED SEAT TRACK.

Part: FITTING — CORRODED (PAX DOOR FRAME) · airframe 65,531 hrs · 29,809 cycles

CORROSION ON AFT LOWER CORNER FRAME 20 OF LT FWD PAX DOOR CUT OUT. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53112109. .

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 65,531 hrs · 29,809 cycles

CORROSION ON SEAT TRACK ON Y765 BETWEEN FRAMES 47-64 EVALUATED AND FOUND OUT LIMITS.

Part: SEAT TRACK — CORRODED (FRAMES 47-64) · airframe 65,531 hrs · 29,809 cycles

CORROSION FOUND ON SEAT TRACK -Y1292 BETWEEN FRAMES 47-64. FOUND OUT OF LIMITS. REPLACED SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 65,531 hrs · 29,809 cycles

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

Part: FLOOR SUPPORT — CORRODED (FRAMES 67-69) · airframe 65,531 hrs · 29,809 cycles

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

Part: FITTING — CORRODED (DOOR FRAME) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING AT FRAMES 17 TO 19 AT S23R PAX CABIN ENTRY CREW DOOR. REPLACED CENTER FITTING IAW SRM A320 51-72-11 AND DWG D53112109.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON RT WING FUEL TANK ACCESS PANEL 640KB. REPLACED ACCESS PANEL IAW SRM 57-27-11.

Part: FITTING — CORRODED (DOOR FRAME) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON CENTER FITTING AT FRAMES 17 TO 19 AT S23L . REPLACED CENTER FITTING IAW SRM A320 51-72-11 AND DWG D53112109.

Part: SEAT TRACK — CORRODED (FRAME 35) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON SEAT TRACK -Y765 UPPER FLANGE AT FRAME 35+7". FOUND OUT LIMITS. REPLACED SEAT TRACK BETWEEN FRAMES 35 TO 36 IAW SRM 51-72-11 AND DWG D53371024.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1225 FRAMES 66+5" TO 67+15". REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D53472395.

Part: FITTING — CORRODED (DOOR FRAME) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON CORNER FITTING AT FRAME 16 AND S23R, FORWARD PAX CABIN ENTRY CREW DOOR. REPLACED FITTING IAW SRM 51-72-11 AND DWG D53112109.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 65,531 hrs · 29,809 cycles

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

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT, Y765 AFT PAX CABIN FLOOR STRUCTURE LOCATED BETWEEN FR 66+5" TO FR 70. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534-72000 AND D534-72093.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y765AT, FRAME 16. REPLACED FLOOR SUPPORT Y765 BETWEEN FRAMES 12 TO 24 IAW SRM 51-72-11 AND DWG D53112812.

Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT, Y1732 BETWEEN FRAMES 65 TO FR 66. REPLACED FLOOR SUPPORT IAW SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (CABIN) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON DUMMY RAIL. REPLACED DUMMY RAIL IAW SRM 51-72-11 AND DWG D531-12828, D531-10984.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT Y1292 BETWEEN FRAMES 64 TO 66 + 5. REPLACED FLOOR SUPPORT IAW SRM A320 51-72-11 AND DWG D53472816.

Part: GIRT BAR — CORRODED (FRAMES 16-20) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON PLATE ASSY BETWEEN FRAMES 16 TO 20 AT S23R OF GIRT BAR FITTING FWD PAX DOOR CUTOUT. REPLACED PLATE ASSY IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y 1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534-72000.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-67) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON FLOOR SUPPORT -Y1225 BETWEEN FRAMES 66+5" TO 67+15". REPLACED FLOOR SUPPORT IAW SRM 51-72-11 AND DWG D534-7200.

Part: DUMMY RAIL — CORRODED (FRAMES 12-16) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ALONG OF RAIL DUMMY BETWEEN FRAMES 12 AND 16, Y503. REPLACED RAIL DUMMY IAW SRM 51-72-11 AND DWG D53112825.

Part: PLATE — CORRODED (FRAMES 16-20) · airframe 65,531 hrs · 29,809 cycles

DURING INSPECTION, FOUND CORROSION ON TWO PLATE ASSEMBLIES, BETWEEN FRAMES 16 TO 20 STRINGER 23L OF GIRT BAR FITTING FWD PASSENGER CREW DOOR CUTOUT. REPLACED PLATE ASSEMBLIES IAW SRM 51-72-11.

Part: FITTING — CORRODED (EMERGENCY EXIT) · airframe 57,895 hrs · 26,061 cycles

LT AFT EMERGENCY EXIT DOOR LWR FWD AND AFT HOOK "T" FITTING HAS CORROSION. REMOVED LOWER SEAL EMERGENCY DOOR LT AFT IAW AMM 52-21-18-401. REMOVED 2 LATCH IAW SRM 51-42-11. REMOVED T FITTING LOWER SECTION IAW SRM 51-42-11 FWD FITTING. REMOVED FITTING LOWER SECTION IAW SRM 51-42-11. INSTALLED 2 LATCHS FWD AND AFT LOWER SECTION. INSTALLED 2 NEW T FITTING LOWER SECTION IAW SRM 51-42-11.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,895 hrs · 26,061 cycles

LWR AFT FUSELAGE SKIN APPROX 3 INCH BY 1.5 INCH AREA OF CORROSION 12 INCH AFT OF FR 69, 3 INCH ABOVE STR 34R LAV VENT EXHAUST. REMOVED CORROSION IAW SRM 53-41-11 OUT OF LIMITS IAW SRM 53-41-11. CUT OUT DAMAGE AREA IAW SRM 53-41-11. FABRICATED DOUBLER AND FILLER IAW SRM 53-41-11. LOCATED AND DRILLED REPAIR PARTS IAW SRM 53-44-11. INSTALLED DOUBLER PER SRM 53-41-11.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 57,895 hrs · 26,061 cycles

RT FWD EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE HAS CRACKS ON FASTENER HOLES EDGE. REMOVED AND REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11.

Part: PROFILE — CORRODED (EMERGENCY EXIT) · airframe 57,895 hrs · 26,061 cycles

LT FWD EMERGENCY EXIT DOOR RT LOAD TRANSMITTING PROFILE HAVE CRACKS ON FASTENER HOLES EDGE. REMOVED CRACKED ANGLE AND CENTER SUPPORT ANGLE FOR ACCESS TO REPAIR IAW SRM 51-42-11. LOCATED AND DRILLED ANGLE IAW SRM 51-44-11. INSTALLED ANGLE AND CENTER SUPPORT ANGLE IAW SRM 51-42-11. FILLET SEAL AROUND ANGLE IAW SRM 51-24-00. APPLIED CIC TO REPAIR AREA IAW AMM SUBTASK 51-21-00-916-053-000-NWA.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 57,895 hrs · 26,061 cycles

FORWARD CARGO COMPT FLOORBOARD PNL 131EF HAS BROKEN WASHERS SEVERAL PLACES, AS MARKED. REMOVED FLOOR PANEL IAW AMM 53-22-14 PB401. FABRICATED FLOOR PANEL ON STAM TRAVELER NR T11/881688 IAW DWG 3D25-37705 MAT. A40 2AB-60X144. INSTALLED FLOOR PNL 131EF IAW AMM 53-22-14 PB401.

Part: FLOOR PANEL — PUNCTURED (CARGO BAY) · airframe 57,895 hrs · 26,061 cycles

FORWARD CARGO COMPT FLOORBOARD PNL 131AF UPPER SURFACE HAS PUNCTURED AND DENTED SEVERAL PLACES APPROXIMATELY 2 TO 3 INCHES, AS MARKED. REMOVED FLOOR PANEL IAW AMM 53-22-14 PB401 FABRICATED FLOOR PANEL ON STAM TRAVELER NR T11/881687 IAW DWG3D25-37705 MAT. A40 2AB-60X144, BATCH NR 1886727. INSTALLED FLOOR PNL 131AF IAW AMM 53-22-14 PB401.

Part: FLOOR PANEL — BROKEN (CARGO BAY) · airframe 57,895 hrs · 26,061 cycles

FORWARD CARGO COMPT FLOORBOARD PNL 131HF HAS BROKEN WASHERS SEVERAL PLACES, AS MARKED. REMOVED FLOOR PANEL 131HF IAW AMM53-22-14 PB401 FABRICATED FLOOR PANEL ON STAM TRAVELER NR T11/881682 IAW DWG 3D25-37705 MAT A402AB-60X144, BATCH NR 1886727. INSTALLED FLOOR IAW AMM 53-22-14 PB401.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 57,895 hrs · 26,061 cycles

AFT CARGO COMPARTMENT FLOOR BOARD PNL NR 151DF HAS SEVERAL BROKEN WASHERS AS MARKED. REMOVED FLOOR PANEL 151DF IAW AMM 53-42-14-000-001. FABRICATED FLOOR PANEL 151DF ON STAM TRAVELER T11/881685 IAW DWG NR 3D25-3770 5. MATERIAL TYPE: A402AB-60X144 BATCH 1886727. INSTALLED 151DF PNL IAW AMM 53-42-12.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 357,985 hrs · 26,061 cycles

AFT CARGO COMPT FLOOR BOARD PNL NR 151AF HAS SEVERAL PLACES DAMAGED AND PUNCTURED APPROXIMATELY 3 TO 4 INCHES AS MARKED. REMOVED FLOOR PANEL 151AF IAW AMM 53-42-14-000-001. FABRICATED FLOOR PANEL 151AF ON STAM TRAVELER T11/881686 IAW DWG NR 3D25-37705. MATERIAL TYPE: A402AB-60X144 BATCH 1886727. INSTALLED 151AF PNL IAW AMM 53-42-14.

Part: FLOORBOARD — DAMAGED (CARGO BAY) · airframe 57,895 hrs · 26,061 cycles

AFT CARGO COMPARTMENT FLOORBOARD PNL 151GF HAS BROKEN WASHERS AT SEVERAL PLACES. REMOVED FLOORBOARD PNL 151GF IAW AMM 53-42-14-000-001. FABRICATED FLOORBOARD PNL 151GF ON STAM TRAVELER T11/881684 IAW DWG NR 3D25-37705 MATERIAL TYPE: A402AB-60X144 BATCH 1886727. INSTALLED FLOORBOARD PNL 151GF IAW AMM 53-42-14.

Part: FLOORBOARD — PUNCTURED (CARGO BAY) · airframe 57,895 hrs · 26,061 cycles

AFT CARGO COMPT FLOOR BOARD PNL 151GF HAS BROKEN WASHERS AT SEVERAL PLACES. REMOVED FLOORBOARD PNL 151GF IAW AMM 53-42-14-000-001. FABRICATED FLOORBOARD PNL 151GF ON STAM TRAVELER T11/881684 IAW DWG NR 3D25-37705 MATERIAL TYPE:A402AB-60X144 BATCH 1886727. INSTALLED FLOORBOARD PNL 151GF IAW AMM 53-42-14.

Part: FITTING — CORRODED (EMERGENCY EXIT) · airframe 57,895 hrs · 26,061 cycles

RT AFT EMER EXIT DOOR FWD AND AFT LWR HOOK "T" FITTINGS HAVE CORROSION. REMOVED FASTENERS IAW SRM 51-42-11. REMOVED CORROSION IAW SRM 51-74-00, FITTING FWD MAT= .080" L=1.6" W=1.1" D=.010", FITTING AFT MAT= .080" L=1.3" W=1.0" D=.011"OUT OF LIMITS IAW SRM 51-73-11, LOCATED AND DRILLED 2 HOOK "T" FITTINGS IAW SRM 51-44-11, INSTALLED HOOK "T" FITTINGS IAW SRM 51-42-11, PAINTED FASTENERS IAW SRM 51-75-12.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 57,895 hrs · 26,061 cycles

RT WING INBD FLAP L/E PUNCTURED REMOVED DAMAGED SKIN AND CORE, FABRICATED INNER SKIN AND BONDED, FABRICATED CORE AND BONDED, FABRICATED REPAIR PLIES AND BONDED, SANDED SMOOTH TO CONTOUR, SEALED EXPOSED FIBERS, CLEANED AREA, APPLIED PRIMER AND PAINT, WORK PERFORMED IAW SRM 57-52-00 PARA 8 A FIG 201. REQUIRED INSPECTION COMPLETED BY SAN NR 489916.

Part: SIGN — BROKEN (CABIN) · airframe 55,724 hrs · 25,117 cycles

EMERGENCY EXIT SIGN AT FWD OVER WING EXIT SEAT 10F BROKEN, REPLACED AND TESTS OK.

Part: HINGE — DAMAGED (L1 DOOR) · airframe 53,944 hrs · 24,399 cycles

DURING GROUND OPERATIONS DOOR 1L ATTACH HINGE AND BEARINGS WERE DAMAGED . REPLACED IAW AMM 20-21-11.

Part: EPSU — FAULTY (CABIN) · airframe 50,466 hrs · 22,909 cycles

EMERGENCY EGRESS LIGHTING TEST FAILS, FAULTING EPSU EMER R. REPLACED EPSU 12WL, CHECKS OK.

Part: OIL COOLER — LEAKING (APU) · airframe 44,042 hrs · 19,727 cycles

AFTER TAKEOFF AT 25,000FT AFT LAV SMOKE MASTER WARNING ILLUMINATED. FLIGHT ATTENDENT INVESTIGATION REVEALED NO SMOKE OR FIRE BUT ABNORMAL ODOR WAS DETECTED. FLIGHT CREW ELECTED TO RETURN TO DEPARTURE AIRPORT. MAINTENANCE FOUND THE APU INLET SOAKED WITH OIL AND OIL LEAK AT APU OIL COOLER. APU PLACED ON MEL. Â

Part: ODOR — DETECTED (CABIN) · airframe 40,519 hrs · 18,059 cycles

DURING DESCENT INTO MEM, EXPERIENCED BURNING ODOR AND OBSERVED WHITE SMOKE IN COCKPIT. DECLARED AN EMERGENCY AND PROCEEDED TO MEM AND LANDED UNEVENTFULLY. INSPECTED ALL AVIONICS BAYS AND BEHIND CIRCUIT BREAKER PANELS, OVENS, AND COFFEEMAKERS WITH NO PROBLEMS FOUND AND NO ODOR PRESENT. RAN BOTH PACKS WITH NO SMOKE NOTED. PERFORMED TEST FLIGHT WITH NO SMOKE OR ODOR PRESENT. AIRCRAFT RETURNED TO SERVICE.

Part: POWER SUPPLY — SHORTED (EMERGENCY LIGHT) · airframe 38,907 hrs · 17,296 cycles

DURING FLIGHT, FUMES WERE REPORTED IN THE CABIN AND COCKPIT. NO SMOKE OR HEAT SOURCE WAS IDENTIFIED. THE OZONE FILTER WAS REPLACED, THEN ROW 11F EMERGENCY LIGHTS POWER SUPPLY SHORTED. REPLACED THE POWER SUPPLY AND TESTED OK.

Part: FITTING — CRACKED (RT MLG) · airframe 28,852 hrs · 12,764 cycles

DURING L-CHECK FOUND CRACK ON RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING. REPAIRED PER EA 32-181770.

Part: ACTUATOR — LEAKING (NR 1 YAW DAMPER)

DURING CRUISE, CREW NOTICED GREEN HYDRAULIC FLUID QUANTITY DECREASING. DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 YAW DAMPER ACTUATOR, OPERATIONAL CHECK OK.

Part: SLIDE — DEFECTIVE (PAX DOOR)

DURING INSPECTION OF PASSENGER DOOR EVACUATION SLIDE PACK RELEASE CABLE, FOUND DEFECTIVE CABLES ON SLIDES AT FORWARD RIGHT, AFT RIGHT, AND LEFT DOORS. REPLACED CABLES ON SLIDES AT AFT DOORS AND REPLACED SLIDE ASSEMBLY AT FORWARD DOOR.

Part: SEAL — LEAKING (HYD PWR CONTL)

DURING CRUISE, CREW NOTED GREEN HYDRAULIC SYSTEM QUANTITY DECREASING AND RECEIVED HYD G RSVR LO LVL MESSAGE. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE, DECLARED EMERGENCY, DIVERTED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING O-RING SEAL ON POWER CONTROL UNIT VALVE BLOCK FILTER (24CV) AND RESERVICED HYDRAULIC SYSTEM. LEAK CHECK OK.

Part: WIRE — SHORTED (CABIN)

DURING LINE MAINTENANCE, THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 14, 15, 16, 19, 20, 21,25, 26, AND 27 WERE FOUND INOPERATIVE. REPAIRED SHORTED WIRE IN SEAT TRACK AT ROW 26 AND REPLACED EPSU (110WL2), OPERATIONAL CHECK OK.

Part: BATTERY — DISCHARGED (CABIN)

DURING THRU-FLIGHT CHECK, THE EMERGENCY LIGHTS SYSTEM FAILED TO TEST. REPLACED EPSU (13WL) AT DOOR 3L, OPERATIONAL CHECK OK.

Part: ACTUATOR — RUPTURED (NR 3 SPOILER)

SHORTLY AFTER LIFT OFF, RECEIVED F/CTL SPLR 3 FAULT MESSAGE FOLLOWED BY THE BLUE HYDRAULIC SYSTEM QUANTITY AND PRESSURE DECREASING TO ZERO. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LEFT HAND NR 3 SPOILER ACTUATOR RUPTURED. REPLACED ACTUATOR. LEAK AND OPERATIONAL CHECK OK.

Part: SENSOR — FAILED (RT MLG DOOR)

DURING CLIMBOUT AFTER LANDING GEAR RETRACTION, LANDING GEAR DOOR INDICATED UNLOCKED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOOR PROXIMITY SENSOR AND OPERATIONAL CHECK OK.

Part: AIR DATA COMP — MALFUNCTIONED (AVIONICS BAY)

WHILE CLIMBING THROUGH 15,000 FEET MSL, RECEIVED F/CTL ADR DISAGREE AND F/CTL ALTN LAW (PROT LOST) MESSAGES. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND CONTINUED ON TO ORIGINAL DESTINATION WHERE AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING ACCOMPLISHED. MAINTENANCE REPLACED THE NR 1 AIR DATA COMPUTER. OPERATIONAL CHECK OK.

Part: THRUST LINK — WORN (NR 1 ENGINE)

DURING C-CHECK, THE NR 1 ENGINE FORWARD ENGINE MOUNT THRUST LINKS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-22-07. THE MAXIMUM DEPTH OF THE DAMAGED AREAS WAS 0.002 INCH. REPAIRED PER NWA EA 32-96336.

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

DURING C-CHECK, THE NR 1 ENGINE FORWARD ENGINE MOUNT THRUST LINKS AND THE NR 2 ENGINE FORWARD INBOARD THRUST LINK WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREAS AS DEFINED BY ROHR CMM 71-21-06, FIG 803. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.001 INCH TO 0.002 INCH. REPAIRS ACCOMPLISHED PER NWA EA 32-96336 AND EA 32-96337.

Part: ANGLE — CRACKED (BELLY FAIRING)

DURING 'C' CHECK, FOUND THE LEFT FUSELAGE BELLY FAIRING CONNECTING ANGLE FOR PANEL 193B CRACKED. THE CRACK, EMINATES FROM THE FORWARD MOST EDGE TO THE 3RD FASTENER HOLE APPROXIMATELY 6 INCHES AFT OF THE FORWARD EDGE. THE ANGLE IS ATTACHED TO THE LEFT OVERWING EMERGENCY SLIDE PACK. REPAIRED PER NWA EA 32-095314.