N342NB

Part: STRUCTURE — DAMAGED (FWD GALLEY) · airframe 62,080 hrs · 32,578 cycles

FWD GALLEY LAMINATE IS COSMETICALLY DAMAGED. REPLACED GALLEY LAMINATED AMM 25-31. (1357443).

Part: STRUCTURE — DAMAGED (ZONE 900) · airframe 62,080 hrs · 32,578 cycles

AFT GALLEY LAMINATE IS COSMETICALLY DAMAGED. REPLACED AFT GALLEY LAMINATE PER A319 AMM 25-31. (1357446).

Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 61,908 hrs · 32,488 cycles

EXIT LIGHTS ABOVE OVERWING EXITS KEPT FLICKERING THROUGHOUT FLIGHT. EXIT SIGNS CURRENTLY OPS CK NORMAL. UNABLE TO DUPLICATE FLICKERING. REF AMM 33-51. (8171861).

Part: APU — ODOR (ZONE 100) · airframe 61,009 hrs · 32,023 cycles

DIRTY SOCK SMELL WHEN APU AIR TURNED ON. R/R APU IAW A319 AMM 49-11-11.

Part: APU — ODOR (ZONE 100) · airframe 61,049 hrs · 32,045 cycles

DIRTY SOCK ODOR WHEN APU BLEED SELECTED ON. R/R APU PER W/C 4900-9002.

Part: O-RING — LEAKING (APU) · airframe 60,828 hrs · 31,920 cycles

SHIP 3142, FUMES SMELL IN FLIGHT DECK AFTER RUNNING PACKS ON APU AT GATE DURING BOARDING. COMPLETED LEAK CHECK OF AIR OIL SEPERATOR PER AMM 49-26-54. NO LEAKS FOUND. REPLACED GENERATOR SCAVENGE FILTER AND O-RING REF AMM 49-91-41.

Part: ECS — CONTAMINATED (ZONE 100) · airframe 60,695 hrs · 31,841 cycles

SHIP 3142 UPON ENTERING THE FLIGHT DECK NOTICE A BAD OLD SOCK ODOR AND INCREASINGLY GOT WORSE. CORRECTIVE ACTION: C/W ECS DECONTAMINATION PER A319 AMM 36-10-00-615-802-A. (7290386).

Part: SCREW — UNSECURE (ZONE 600 SLAT) · airframe 60,575 hrs · 31,781 cycles

SHIP 3142 RIGHT WING #3 SLAT T/E DAMAGED BY SCREW STICKING UP. CORRECTIVE ACTION: BLENDED TO WITHIN LIMITS OF SRM 57-40-00-283-004. (6635837)

Part: FRAME — DAMAGED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 ELONGATED HOLE 19 LOCATED ON FR16LH. CORRECTIVE ACTION: COMPLIED WITH ER/A 625906-14AD. (0987933).

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 TWO CRACKS WERE FOUND AFFECTING THE HOLE #1 & #3 AT DOOR STOP #7 ON FR16 RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 579971-14AD. (0987881).

Part: SKIN — GOUGED (ZONE 100) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 GOUGE EXTERNAL SKIN LOCATED BTW FR54 TO FR55 AND BTW STR43L TO STR41L BELLY FAIRING AREA LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 626599-14AD. (0986962).

Part: DOOR FRAME — DAMAGED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 HOLE #19 WAS FOUND ELONGATED AT FR16LH, DOOR STOPS #1 & #7, DOUBLE JOGGLE AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 625906-14AD. (0987409).

Part: DOOR FRAME — DAMAGED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 TWO CRACKS WERE FOUND AFFECTING THE HOLE #1 & #3 AT DOOR STOP #7 ON FR16 RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 579971-14AD. (0987566).

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CRACK FOUND ON FR4 RH WINDSHIELD SIDE POST. CORRECTIVE ACTION: COMPLIED WITH ER/A 561852-14AD. (0984757).

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CRACK INDICATION FOUND ON FRAME 20 RH DOUBLE JOGGLE AREA HOLE 5 DOOR STOP FITTING 7. CORRECTIVE ACTION: COMPLIED WITH ER/A 625653-14AD. (0984755).

Part: PANEL — CRACKED (ZONE 100) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 SECONDARY FINDING CRACK WASTE TANK PANEL 172AR AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 626048-14. (0984872).

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CRACK FOUND AT HOLE #5 AT RH FR20 PAX DOOR DOUBLE JOGGLE AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 625653-14AD. (0983903).

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CORROSION INSERT ON FLOOR PANEL 261PF AT PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH ER/A 625738-14. (0983179).

Part: POST — CORRODED (ZONE 900) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CORROSION ON LATERAL POST FWD RH LOWER SIDE AT LAV A. CORRECTIVE ACTION: COMPLIED WITH ER/A 625666-14. (0983383).

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CRACK INDICATION WAS FOUND AT RH (CENTER POST, UPPER AREA) FRONT WINDSHIELD FRAMING. CORRECTIVE ACTION: COMPLIED WITH ER/A 625715-14AD. (0984352).

Part: POST — CRACKED (ZONE 100) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CRACK INDICATION FOUND ON CENTER POST FR 4 UPPER TENSION BOLT POSITION RH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 625622-14AD. (0984340).

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 DELAMINATED FLOOR PANEL 261DF IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH ER/A 625694-14. (0983393).

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 DURING M2 AND WHILE INSPECTING PER EM 5311-01226-01 CRACK INDICATION FOUND IN RH CENTER WINDSHIELD FRAME LWR NODE AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 625622-14. (0981077)

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 DTE* DURING M2 AND WHILE INSPECTING PER EM 5311-01226-01 CRACK INDICATION FOUND IN RH CENTER WINDSHIELD FRAME LWR NODE AREA. CORRECTIVE ACTION: REPAIRED PER ER/A 625622-14AD. (0981067)

Part: STIFFENER — CRACKED (WINDOW FRAME) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CRACK WAS FOUND IN THE LOWER VERTIC AL STIFFENER OF THE RHS LATERAL WINDOW FRAME. CORRECTIVE ACTION: REPAIRED PER ER/A 561852-14. (0979253)

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CRACK INDICATION FOUND IN RH CENTER WINDSHIELD FRAME LWR NODE AREA. CORRECTIVE ACTION: REPLACED PER ER/A 625715-14AD. (0980552)

Part: WEB — MECHANIC ERROR (ZONE 100) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 DISC: IMPROPERLY INTERNAL STRUCTURE MISS DRILL ON WEB LLOWER SILL AREA BTW F R26 TO FR28 IN FWD CARGO COMPARTMENT. C/A: REPLACED WEBS (2EA) AND FASTENERS LOC. LOWER SILLAREA BTW FR26 TO FR28 IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-42-11,SRM:51 -72-11 AND DWG: D53231685, ISSUE: H00, RELEASE DATE: 24-DEC-14. MATERIAL USED SEALANT P/N: 0870B1-2BM012PT, PO:2025-119491/001 SEE INDIVIDUAL SIGN-OFF ON ORNRC 133/100 RII INSPECTION COMPLETE 0943462 AE362QC JOB COMPLETE. (LP: 0966363)

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 DISC: CORROSION STRINGER 44 BETWEEN FR59 TO FR60 AFT CARGO COMPARTMENT (SSI 534107). C/A: REPLACED STRINGER 44 LOC BTW FR59 TO FR64 AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11, SRM 51-72-11 AND DWG D53476345 RELEASE DATE 08-NOV-99 ISSUE N AND DWG D53476318 RELEASE DATE 07-FEB-00 ISSUE N. SEE ORNRC 153/100 FOR INDIVIDUAL SIGN-OFF RII INSPECTION COMPLETE 0512801 AE135QC JOB COMPLETE. (LP: 0955739)

Part: FLOOR SUPPORT — ABNORMAL (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142, CORROSION FLOOR BEAM +Y765 LOCATED BTW FR 15 TO FR 16 AT FWD GALLEY AREA (SSI 531189). REPLACED FLOOR BEAM Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11-801 AND A319 SRM 51-72-11 DWG D53110984, DWG D43110920, DWG D53112812. ORNRC 22/220 FOR INDIVIDUAL SIGN-OFF RII INSPECTION COMPLETE 0512801 AE135QC JOB COMPLETE. (LP: 0946979)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CORROSION FLOOR BEAM -Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED FLOOR BEAM -Y1292 LOC. AT FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-72-11 AND DWG D53112812 AND DWG D53110920. SEE ORNRC 25/220 FOR INDIVIDUAL SIGN-OFF RII INSPECTION COMPLETE, JOB COMPLETE. (LP: 0945319)

Part: POST — DAMAGED (ZONE 100) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 SECONDARY FINDING ELONGATED HOLE VERTICAL POST INTERNAL STRUCTURE AT LEVEL FR60 RH SIDE IN AFT CARGO COMPARTMENT. REPLACED VERTICAL POST INTERNAL STRUCTURE AT LEVEL FR60 RH SIDE IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11, A319 SRM51-72 -11 AND DRAWING D53476977. SEE ORNRC 160/100 FOR INDIVIDUAL STEPS RII INSPECTION COMPLETE 0512801 AE135QC JOB COMPLETE. (LP: 0945327)

Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP DISC: CORROSION FLOOR BEAM +Y254 LOCATED AT FR 16 AT FWD GALLEY AREA ( SSI 531189). C/A: REPLACED FLOOR BEAM Y254 AND FASTENERS LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG: D53110984, DWG: D53112816, DWG: D53110920 JOB COMPLETE. (LP: 0940344)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 DISC: CORROSION LOWER SILL LOCATED AT FR 68 LH SIDE AT AFT GALLEY AREA (SSI 534147 ). C/A: PERFORMED REPAIR LOWER SILL LOC ON FR68 LH SIDE AT AFT GALLEY AREA AS PER A319 SRM 53-41-14-300-001 STEP 2, FIGURE 001, SHEET 4,PRINCIPLE 7 AND A319 SRM 51-42-11 TOOK MEASURES OF CORROSION ARE: L= 0.987IN, W= 0.167IN, TOOL USED DIGITAL CALIPER PN:500-197-30, SN: B2312374, DUE DATE: 03/SEP/25 RECHECK IS NOT REQUIRED DUE TO THIS REPAIR IS CONSIDERED AS CATEGORY A. SEE INDIVIDUAL SIGN- OFF ON ORNRC 27/260 RII INSPECTION COMPLETE AE206QC JOB COMPLETE. (LP: 0936342)

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CORROSION UNDERFLOOR STRUCTURE FRAME WEB LOC FR69 T0 FR70 AT LEVEL ST R 23L AT AFT GALLEY AREA. REPLACED FRAME WEB AND FASTENERS LOCATED FR69 TO FR70 AT LEVEL STR23L AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AND DWG: D53474180 ISSUE: AA RELEASE DATE: 09/SEP/24 TOOK MEASURE OF CRACK IS L= 0,742 INCH W= 0.416 INCH D= 0.027 INCH. REFER TO ORNRC 38/260 FOR INDIVIDUAL SIGN-OFF RII INSPECTION COMPLETE 2304886 AE388QC JOB COMPLETE. (LP: 0932889)

Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CORROSION UNDERFLOOR STRUCTURE FRAME WEB LOC FR69 TO FR70 AT LEVEL ST R23R AT AFT GALLEY AREA. REPLACED FRAME WEB AND FASTENERS LOCATED FR69 TO FR70 AT LEVEL STR23R AT AFT GALLEY AREA AS PER A 319 SRM 51-42-11 AND DWG: D53474180 RELEASE DATE: 09/SEP/24 ISSUE AA TOOK MEASURE CORROSION IS L= 1.412 INCH W= 0.563 INCH D= 0.008 INCH TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A23325701 DUE DATE: 05-FEB -26 SEE INDIVIDUAL SIG-OFF ON ORNRC 37/260 RII INSPECTION COMPLETE 2255748 AE452QC JOB COMPLETE. (LP: 0932899)

Part: FITTING — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CORROSION CENTER FITTING LOCATED BTW FR 66 TO FR 68 LH SIDE CUT OUT AT AFT GALLEY AREA (SSI 534136). REPLACED CENTER FITTING LOCATED BTW FR 66 TO FR68 LH SIDE CUT OUT AT AFT GALLEY AREA AS PER A319 SRM 51-72-11, A319 SRM 51-42- 11, DWG D53480048, ISSUE: F, RELEASE DATE: 05-NOV-93, DWG D53480505, ISSUE: FE, RELEASE DATE:09-JAN-25, TOOK MEASURE OF CORROSION ON CENTER FITTING ARE: L: 0.842 INCHES, W: 0,510 INCHES, D: 0,016 INCHES.

Part: PLATE — CRACKED (ZONE 100) · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 DISC: CRACK PLATE LOCATED BTW FR 68 TO FR 69 LEVEL STR 23R AT AFT GALLEY AREA. C/A: REPLACED PLATE LOCATED BTW FR 68 TO FR 69 LEVEL STR 23R AT AFT GALLEY AREA AS PER A319 SRM 51-72-11, A319 SRM 51-42-11, DWG D53480505, ISSUE: FE, RELEASE DATE :09-JAN-25 AND DWG D53474250, ISSUE: V, RELEASE DATE: 11-FEB-04 TOOK MEASURE OF CRACK IS L: 0.780 INCHES TOOL USED CALIPER PN: 500-193-30 SN: 0051663 DUE DATE: 16-SEP-25 SEE INDIVIDUAL SIGN-OFF ON ORNRC 23/260 RII INSPECTION COMPLETE 1715948 AE403QC JOB COMPLETE. (LP: 09329113)

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CORROSION FLOOR BEAM -Y1292 LOCATED BTW FR 65 TO FR 66 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM LOC -Y1292 BTW FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11 AND DWG D53472816 RELEASE DATE 18-DEC-06 ISSUE F, MEASURES OF CORROSION ARE: L=2.235 INCH W=0.385 INCH D=0.051 INCH.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 CORROSION FLOOR BEAM +Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA ASPER A319 SRM 51-72-11, A319 SRM 51-42-11 AND DWGD53472780 RELEASE DATE: 26-APR-18 ISSUE K AND DWG D53474250 RELEASE DATE 11-FEB-04 ISSUE V. MEASURE OF CORROSION ARE: L= 0.105IN W= 0.100 IN D=0.025 IN

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

CORROSION FLOOR SUPPORT -Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY A REA (SSI 534147). REPLACED FLOOR SUPPORT -Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWG D53472780, DWG D53472816 ISSUE F AND DWG D53474250 ISSUE V. MEASURES OF CORROSION ARE: L: 0.478 IN, W: 0.449 IN, D: 0.0510 IN.

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

SHIP 3142 DISC: CORROSION FLOOR SUPPORT +Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11, DWG D53472092 AND DWG D53472815. MEASURES OF CORROSION ON FLOOR SUPPORT Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY AREA ARE: L: 3.074 IN, W: 0.832 IN, D:0.076 IN,

Part: BELLCRANK — OUT OF ADJUST (ZONE 800) · airframe 60,496 hrs · 31,733 cycles

OUT OF ADJUSTMENT DOOR RIGGING POINT (K) IN THE TORSION BAR BELLCRANK AT PASSENGER CREW DOOR 831 AT FWD GALLEY (REFERENCE RII AMDS CARD 5210 -7089-LF-DE). C/A: PERFORMED ADJUSTMENT DOOR RIGGING POINT (K) IN THE TORSION BAR BELLCRANK AT PASSENGER CREW DOOR 831 AT FWD GALLEY AS PER A320 FAM AMM 52-11-21-400-001-A. STEP 4.L(7) THRU (9). THE ADJUSTMENT IS CORRECT.

Part: DAMPENER — NO TEST (ZONE 800) · airframe 60,496 hrs · 31,733 cycles

DID NOT PASS OPERATIONAL FUNCTIONAL TEST EMERGENCY DOOR DAMPER ON PASSENGER CREW DOOR 832 (REFER TO AMDS CARD 5210-7089-LA RII). REMOVED DOOR DAMPER ON PASSENGER CREW DOOR 832 PER A320 FAM AMM 52-13-14-000- 001-B STEP 1 THRU 4 EXCEPT STEP 3.D. REPLACED DOOR DAMPER ON PASSENNGER CREW DOOR. 832 RII C/W. DONT PASS OPERATIONAL FUNCTIONAL TEST EMERGENCY DOOR DAMPER ON PASSENGER CREW DOOR 832 (REFER TO AMDS CARD 5210-7089-LA RII). C/A: REMOVED DOOR DAMPER ON PASSENGER CREW DOOR 832 PER A320 FAM AMM 52-13-14-000- 001-B STEP 1 THRU 4 EXCEPT STEP 3.D.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

CORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLE Y AREA (SSI 534147). REPLACED FLOOR BEAM -Y1162.5 LOCATED BETWEEN FR68 TO FR69 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AS PER A319 SRM 51-72-11, AND DWG- D53472780 RELEASE DATE 26-APR-18 ISSUE K AND DWG D53472089 RELEASE DATE 12-DEC-24 ISSUE M. MEASURE OF CORROSION ARE: L=0.279 IN W= 0.210 IN D= 0.030IN

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 60,496 hrs · 31,733 cycles

CORROSION FLOOR BEAM -Y1292 LOCATED BTW FR 66 TO FR 68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM -Y1292 AND FASTENERS LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM51-72 -11 AND DWG D53472816 RELEASE DATE: 18-DEC-06 ISUE F ,AND DWG- D53472780 RELEASE DATE 26-APR-18 ISSUE K MEASURES OFCORROSION ARE: ARE:L= 0.373 IN W= 0.113 IN D= 0.031 IN.

Part: OIL SYSTEM — LEAKING (APU) · airframe 60,254 hrs · 31,609 cycles

SHIP 3142 - SMKE - SMOKE REPORT IN FLT DECK JUST AFTER LANDING. DECLARED EMERGENCY AND DONNED O2 MASKS. FAS ALSO REPORTED LIGHT HAZE IN AFT CABIN. CORRECTIVE ACTION: FOUND APU INLET CONTAMINATED WITH OIL. APU DEFERRED TO MEL. REVERSE DUCT BURN AND LEVEL B ECS DECONTAMINATION PERFORMED. REPLACED RECIRC AND OZONE FILTERS. (LP: 6694416)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 60,102 hrs · 31,532 cycles

SHIP 3142 STRONG SMELL WAS NOTICED IN THE COCKPIT. IT ALMOST SMELLS LIKE OVEN CLEANER OR BURNING IT WAS NOTICED AROUND THE MIDPOINT OF THE CABIN AS WELL. CORRECTIVE ACTION: COMPLIED WITH W/C 0550-2002 AND ER/A 568923-14TR. (6021516)

Part: NONE — NONE (NONE) · airframe 60,029 hrs · 31,498 cycles

SHIP 3142 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A 570263-14. (1224604)

Part: TIRE — OUT OF ROUND (ZONE 700) · airframe 59,326 hrs · 31,166 cycles

SHIP 3142 NOSEWHEEL HAD EXCESSIVE SHIMMY DURING TAKEOFF FOR APPROXIMATELY 15 SEC AFTER GREAR RETRACTION. CORRECTIVE ACTION: INSPECTED BOTH NLG WHEEL ASSEMBLE FOUND RT LNG SLIGHTLY OUT OF ROUND RETORQUE BOTH NLG TIRES PER A319 AMM 32-41-12. (6460302)

Part: PANEL — BULGED (ZONE 800) · airframe 59,245 hrs · 31,116 cycles

SHIP 3142 AFT CARGO COVER PANEL BULGE LOWER EDGE AFT CARGO DOOR ACCESS COVER PANEL. CORRECTIVE ACTION: REPLACED PANEL IAW A319 AMM 52-32. OPS NORMAL. A/C OK FOR SVC. (6489524)

Part: DOUBLER — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,156 hrs · 31,064 cycles

WASTE BOX HAS CORROSION ON INNER SIDE OF DOUBLER ON FWD R/H CORNER. CORRECTIVE ACTION: COMPLIED WITH PRI 621280-14. (0610881) - ERA 621280-14 IS CONNECTED TO SHIP 8142 WHICH IS AN A220-100 NOT SHIP 3142 WHICH IS AN A319. THE CROSS-REFERENCE LOG NUMBER IS 0603970. SHIP 3142 IS INCORRECT AND SHIP 8142 IS CORRECT.

Part: ECS — FUMES (ZONE 200) · airframe 59,117 hrs · 31,040 cycles

SHIP 3142 FUME EVENT DURING DESCENT. REPORTED A HYDRAULIC/FUEL SMELL. CORRECTIVE ACTION: C/W AMDS W/C 0550-2002. PERFORMED ECS DECOMANITAION IAW W/C 2100-2005. (6659272)

Part: UNKNOWN — FUMES (CABIN) · airframe 59,091 hrs · 31,028 cycles

SHIP 3142 SMOKE/FUMES ON DESCENT. CORRECTIVE ACTION: PERFORMED WORKCARD 2100-2005. ACCOMPLISHED WORK CARD 0550-9001-A320FAM. (0591238)

Part: INLET — CONTAMINATED (APU) · airframe 58,843 hrs · 30,897 cycles

SHIP 3142 - DIV/FUMES - DIVERTED TO RIC FOR OILY SMELL IN CABIN. CORRECTIVE ACTION: FOUND OIL ON APU EXTERIOR, NO OIL INGESTION FOUND IN INLET OR BLEED DUCT USING UV LIGHT. NO OIL FOUND BEHIND ENGINE SPINNERS. COMPLIED WITH DUCT BURNS AND ECS DECONTAMINATION. CLEANED APU DOOR. RAN APU AND PACKS FOR EXTENDED TIME. NO SMELLS. (LP 5713218, 5713220)

Part: ECS — CONTAMINATED (ZONE 100) · airframe 58,739 hrs · 30,834 cycles

SHIP 3142 DIRTY SOCK SMELL WHEN APU BLEED AIR TURNED ON. CORRECTIVE ACTION: PERFORMED LEVEL B REMOVAL OF THE CONTAMINATION OF THE ECS IAW A319 AMM 21-00-00-615-803-A. (0507876)

Part: UNKNOWN — UNKNOWN (STEERING SYSTEM) · airframe 58,444 hrs · 30,684 cycles

SHIP 3142 AIRCRAFT PULLS TO THE LEFT, REQUIRES EXCESSIVE PEDAL PRESSURE TO STEER A/C. CORRECTIVE ACTION: T/S PER A319 TSM TASK 32-51-00-810-823-A. INSPECTED NLG TIRE PSI'S. CHKS GOOD. JACKED NLG AND INSPECTED TIRES & ASSY FOR ANY PLAY. NO EXCESSIVE PLAY FOUND. UNABLE TO DUPLICATE FAULT. OK FOR SVC. (6192870)

Part: RADOME — DAMAGED (NOSE) · airframe 57,785 hrs · 30,313 cycles

SHIP 3142 RADOME HAS IMPACT DAMAGE. CORRECTIVE ACTION: REMOVED AND REPLACED RADOME PER A319 AMM 53-15-11. (5402312)

Part: FAIRING — DAMAGED (NR 4 FLAP TRACK) · airframe 57,768 hrs · 30,301 cycles

SHIP 3142 #4 FLAP TRACK FAIRING ON LEFT WING DAMAGED BY DEPARTURE OF PANEL 575GB. CORRECTIVE ACTION: REPAIRED PER A319 SRM 57-51-37-400-004-A. (5402308)

Part: PANEL — INFLT SEPARATION (WING) · airframe 57,768 hrs · 30,301 cycles

SHIP 3142 PANEL 575GB DEPARTED A/C. CORRECTIVE ACTION: INSTALLED PANEL 575 GB REF. A319 AMM 57-51-37. (5402306)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 56,519 hrs · 29,624 cycles

SHIP 3142 AFT. GALLEY TROLLEY RETAINER BLOCKS SHOW SIGNS OF BULGING, CORROSION AND DELAMINATION IN COMPARTMENTS 510, 511, AND 512. CORRECTIVE ACTION: REPAIRED PER A.A WORK CARD 2530-01591-04D. (0007069)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 56,428 hrs · 29,573 cycles

SHIP 3142 DAMAGE TO BELLY FAIRING PANEL 191KB. CORRECTIVE ACTION: REPAIRED PER ERA 612263-14. (2981962)

Part: FILTER — ODOR · airframe 52,898 hrs · 27,680 cycles

SHIP 3142 - DURING DESENT DIRTY SOCK SMELL FROM PACK. CORRECTIVE ACTION: REMOVED + REPLACED BOTH OZONE FILTERS PER A319 AMM 21-51-41, CABIN RECIRC FILTERS PER A319 AMM 21-21. C/W WORKCARDS 0550-2002, 0550-9001-A320FAM, 4900-2001, 2100-2005. APU PLACED ON MEL.(9245048)

Part: NONE — NONE · airframe 52,114 hrs · 27,230 cycles

SHIP 3142 - LMLG RETRACT ACTUATOR ANCHORAGE FITTING SPHERICAL BEARING BORE HAS CORROSION. CORRECTIVE ACTION: REPAIRED WITH REF A319 SRM 57-26-13-300-025. (2101412)

Part: NONE — NONE · airframe 52,114 hrs · 27,230 cycles

SHIP 3142 - RMLG RETRACT ACTUATOR ANCHORAGE FITTING SPHERICAL BEARING BORE HAS CORROSION. CORRECTIVE ACTION: REPAIRED RMLG ANCHORAGE FITTING BORE REF A319 SRM 57-26-13-300-025. CORROSION LEVEL 2. (2101415)

Part: NONE — NONE · airframe 51,869 hrs · 27,102 cycles

LIGHT ATTENDANT REPORT- SEAT 11D FLOOR PROXIMITY EVERGENCY ESCAPE PATH MARKING SYSTEM LIGHT ASSY MISSING/INOP. FWD TO MCO AND PLACARD PER MEL 33-50-03A. NEEDS LIGHT ASSY AND SEAT SIDE PLASTIC COVER REPAIR. CONNECTOR IS STOWED. REPLACED EMERGENCY LIGHT AT 11D REF A319 CMM 25-22-53. OPS CHECK GOOD. MEL PLACARD REMOVED . M PROCEDURES REVERSED. (LP# 7977858)

Part: UNKNOWN — ODOR (COCKPIT) · airframe 51,231 hrs · 26,753 cycles

SHIP 3142 - SMELL OF A DIRTY SOCK ODOR IN COCKPIT. CORRECTIVE ACTION: PERFORMED CHECK ENGINE OIL ODOR CARD 7900-2001 STEPS 1-22. COMPLETED WORK CARD 7900-2001. C/W W/C 0550-2002, W/C 4900-2001 AND DECONTAMINATION W/C 2100-2005 C/W. NO TROUBLE FOUND. (7913243)

Part: APU — ODOR · airframe 50,942 hrs · 26,617 cycles

SHIP 3142 - UPON START OF APU AT ENGAGE OF PACKS. WE GOT THE "DIRTY SOCK SMELL". CORRECTIVE ACTION: ACCOMPLISHED AMDS WC 0550. FOUND APU AT FAULT. ACCOMPLISHED DECONTAMINATION OF ECS PER AMDS WORK CARD 2100-2005. ALL LEAK AND OPS CHECKS GOOD. (7971088)

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 50,349 hrs · 26,322 cycles

SHIP 3142 - EMERGENCY ESCAPE FLOOR PATH MARKING LIGHT HOUSING AT SEAT 19DEF DAMAGED. CORRECTIVE ACTION: C/W SECTION II ERA 591510-14, REV ORIG. PERMANENT REPAIR. (6308068)

Part: PROXIMITY SENSOR — OUT OF LIMITS (MLG) · airframe 50,309 hrs · 26,302 cycles

SHIP 3142 - GEAR HANDLE DIFFICULT TO MOVE TO THE UP POSITION AFTER TAKEOFF. CORRECTIVE ACTION: CHECKED PROX SENSORS RESISTANCE. FOUND 20GA OUT OF LIMITS. ADJUSTED PER A319 AMM. ADJUSTED 24GA & 25GA TO WITHIN LIMITS PER A319 AMM 32-31. CYCLED LANDING GEAR & PERFORMED OPS CHECK OF RETRACTION INHIBITION BAULK PER A319 AMM 32-31. NO FAULTS FOUND. LANDING GEAR HANDLE OK. (6308044)

Part: CONTROL LEVER — BINDING (MLG) · airframe 50,309 hrs · 26,302 cycles

SHIP 3142 - GEAR HANDLE DIFFICULT TO RAISE. CORRECTIVE ACTION: R&R LANDING GEAR NORMAL CONTROL LEVER PER A319 AMM 32-31. SYSTEM CKS NORMAL. (6308042)

Part: APU — ODOR · airframe 50,295 hrs · 26,292 cycles

SHIP 3142 - ODOR WITH APU BLEED ON (GROUND). INFLIGHT ODOR WAS NOT AS PRONOUNCED (CRUISE) ON DESCENT ODOR RETURNED. CORRECTIVE ACTION: T/S SMOKE AND FUMES IN COCKPIT PER AMDS W/C. R/R APU. (6308026)

Part: PSU — NO TEST (SEAT 14ABC) · airframe 49,794 hrs · 26,018 cycles

SHIP 3142 DURING TEST PSU OXYGEN PANEL SEAT 14ABC PANEL DID NOT DEPLOY. CORRECTIVE ACTION: R/R PSU PANEL. OPS CK GOOD. (6464595)

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 49,276 hrs · 25,719 cycles

AUTOMATIC CABIN PRESSURE CONTROL SYSTEM NR 1. CORRECTIVE ACTION: R & R NR 1 CPC, PER A319 AMM 21-31. OPERATIONS CHECK NORMAL, PER AB 319 AMM 21 -31-00-710. OK FOR SERVICE.

Part: VALVE — FAILED (LT ENGINE) · airframe 48,735 hrs · 25,407 cycles

ATB - DUE TO A LEFT ENGINE BLEED FAULT CORRELATED TO A FAV FAILURE. ICING CONDITION DURING THE FLIGHT PREVENTED CONTINUATION TO BDA. CORRECTIVE ACTION: REPLACED L FAN AIR VALVE. RAN ENGINES CHECKS OK.

Part: UNKNOWN — MALFUNCTIONED (EXIT SIGN) · airframe 47,856 hrs · 24,937 cycles

EXIT SIGN FLASHES DURING FLIGHT" CHECKED EMERGENCY LIGHT OPERATION FROM FLT DECK & FAP. OPS NORMAL. INSPECTED EXIT SIGNS - NORMAL. NO HISTORY.

Part: ACCESS PANEL — CRACKED (HORIZONTAL STAB) · airframe 46,589 hrs · 24,206 cycles

CRACK ACCESS PANEL 332AB ON LH HORIZONTAL STABILIZER. REPAIRED ACCESS PANEL 332AB ON LH HORIZONTAL STABILIZER ASPER PRI # 580392-14 REV 0 ER/A # 580392-14 REV ORIGINAL. ASSOCIATED ER/A 00-580392 ADDED FOR AC 3142.

Part: FRAME — CRACKED (FRM 20) · airframe 46,589 hrs · 24,206 cycles

CRACK INDICATION ON FRAME 20 (RH) FROM THE UPPER I/B HOLE COMMON TO DO OR STOP FITTING 7 AT FWD GALLEY AREA (1 EA) (CRACK DIRECTION IS 7 O'C LOCK LOOKING AFT) (THE CRACK LENGTH IS 0.058 INCHES). PERFORMED PERMANENT REPAIR LOC ON FRAME 20 RH COMMON TO DOOR STOP FITTING 7 AT FWD GALLEY AREA ASPER PRI REV 0-1 AND ERA 579968-14AD REV ORIGINAL.

Part: FRAME — CRACKED (FRM 68) · airframe 46,589 hrs · 24,206 cycles

CRACK INDICATION ON FRAME 68 BTW STRINGER 8 TO STRINGER 9 TO HOLE AT RADIUS AREA LH SIDE AT AFT GALLEY AREA (CRACK LENGHT= 0.250 INCH APPROX). PERFORMED PERMANENT REPAIR LOC ON FRAME 68 BTW STR 8 TO STR 9 LH SIDE AT AFT GALLEY AREA ASPER PRI REV 0 AND ERA 580121-14AD REV ORIGINAL. IDENTIFIED REPAIR LOC ON FRAME 68 BTW STR 8 TO STR 9 LH SIDE AT AFT GALLEY AREA ASPER PS 900-5-1 #4 FOR SECTION DTE SEE LOGPAGE 1222733 JOB COMPLETE ASSOCIATED ER/A 00-580121 ADDED FOR AC 3142 LOG-PAGE.

Part: FRAME — CRACKED (FRM 16) · airframe 46,589 hrs · 24,206 cycles

CRACK INDICATION ON FRAME 16 (RH) FROM THE UPPER I/B HOLE COMMON TO THE DOOR STOP FITTING 7 AT FWD GALLEY AREA (1EA) (CRACK DIRECTION IS BETWEEN 10 & 11 O'CLOCK LOOKING FORWARD) (THE CRACK LENGTH IS 0.085 INCHES). PERFORMED REPAIR ON FRAME 16 (RH) FROM THE UPPER I/B HOLE COMMON TO THE DOOR STOP FITTING 7 AT FWD GALLEY AREA PER PRI 579971-14 REV.0 AND REV.1 ER/A 579971-14AD REV.ORIGINAL, FOR SECTION II SEE LOG PAGE 1223876 JOB COMPLETE.

Part: FRAME — CRACKED (FRM 16) · airframe 46,589 hrs · 24,206 cycles

CRACK INDICATION ON FRAME 16 (RH) FROM THE LOWER I/B HOLE COMMON TO THE DOOR STOP FITTING 7 AT FWD GALLEY AREA (1 EA) (CRACK DIRECTION IS BETWEEN 10 & 11 O'CLOCK LOOKING FORWARD) (THE CRACK LENGTH IS 0.047 INCHES). PERFORMED REPAIR ON FRAME 16(RH) FROM THE LOWER I/B HOLE COMMON TO BE DOOR STOP FITTING 7 AT FWD GALLEY AREA (1E/A) AS PER ER/A 579971-14AD REV.ORIGINAL AND PRI REV 0, PRI REV "1" FOR SECTION III SEE LOG PAGE 1223883.

Part: FRAME — CRACKED (FRM 36) · airframe 46,589 hrs · 24,206 cycles

CRACK INDICATION ON FRAME 36 FASTENER HOLES LOCATED 1 INCH INBD FROM Y +1292.0, 2 INCH OUTBD FROM Y+1292.0 AND 3 INCH OUTBD FROM Y+ 1292.0. "A CRACK(S) THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR35LH AND FR36LH. MODIFY IN ACCORDANCE WITH WORK CARD 5311-01171-04A PRIOR TO FURTHER FLIGHT". AA 5311-011 71' SB A320-53-1263, AD-2018-06-04. IN FWD CARGO COMPARTMENT (3 EA). REPAIRED PRESSURE PANEL AREA (PRESSURE PLATE) LOC. BTW FR.35LH AND FR.36LH Y+12920 AS PER A319 WORK CARD 5311-01171-04A.

Part: FRAME — CRACKED (FRM 36) · airframe 46,589 hrs · 24,206 cycles

CRACK INDICATION ON FRAME 36 IN HOLE A AT THE INTERFACE OF THE PRESSUR E PANEL AND LONGITUDINAL BEAM Y+1292 IN FWD CARGO COMPARTMENT ( 1 EA) (REPAIR IN ACCORDANCE WITH WORK CARD 5311-01171-04A PRIOR TO FURTHER F LIGHT.) REPAIRED PRESSURE PANEL AND LONGITUDINAL BEAM Y+1292 LOC. ON FR .36 IN FWD CARGO COMPARTMENT AS PER A319 WORK CARD #5311-01171-01A.

Part: HINGE FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 46,589 hrs · 24,206 cycles

CORROSION LEVEL: 2. CORROSION ELEVATOR HINGE FITTING 4 ON LH HORIZONTAL STABILIZER. PERFORMED REPAIR ON ELEVATOR HINGE FITTING 4 ON LH HORIZONTAL STABILIZER AS PER A319 SRM 55-26-41-300-002 FIGURE 01 TAB LUGS ZONE 04 ELEVATOR HINGE FTG REPAIR-SHEET 1.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 46,589 hrs · 24,206 cycles

CRACK INDICATION ON INTERCOSTAL FROM THE TWO INBOARD HOLES COMMON TO T HE DOOR STOP FITTING 7 AND FR 16 (RH) AT FWD GALLEY AREA (2 EA). REPLACED INTERCOSTAL FROM THE TWO INBOARD HOLES COMMON TO THE DOOR STOP FITTING 7 AND FR 16 (R/H) AT FWD GALLEY AREA AS PER SRM A319 51-72-11-401 AND DRAWING D53112331.

Part: INTERCOSTAL — CRACKED (DOOR FRAME) · airframe 46,589 hrs · 24,206 cycles

CRACK INDICATION ON INTERCOSTAL FROM THE UPPER INBOARD HOLE COMMON TO THE DOOR STOP FITTING 7 AND FR20 (RH) AT FWD GALLEY AREA (1 EA). REPLACED INTERCOSTAL FROM THE UPPER INBOARD HOLE COMMON TO THE DOOR STOP FITTING 7 AND FR 20(RH) AT FWD GALLEY AREA AS PER SRM A319 51-72 -11-401 AND DRAWING D53112331.

Part: COMBUST CHAMBER — CRACKED (NR 1 ENGINE) · airframe 46,589 hrs · 24,206 cycles

CRACK COMBUSTION SECTION PLATE INBOARD SIDE LOC AT 6 OCLOCK APROX ON ENGINE 1. REPAIRED AND INSTALLED COMBUSTION SECTION PLATE INBOARD SIDE LOC AT 6 OCLOCK APROX ON ENGINE 1 AS PER ERA 564620-14MA REV. ORIGINAL AND CFM56-5A ESM 71-00-01-440-024-0.

Part: DUMMY RAIL — CORRODED (FRAME 12) · corrosion level 2 · airframe 46,589 hrs · 24,206 cycles

CORROSION LEVEL: 2. CORROSION RAIL DUMMY -Y1379.5 LOC. FR 16 AT FWD GALLEY AREA. REPLACED RAIL DUMMY -Y1379.5 LOC ON FR 12 TO FR 16 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG D53112831, ISSUE=D RELEASE DATE 24DEC96 AND DWG D53110984, ISSUE=B, RELEASE DATE 25 JUN 05 TOOK MEASURES OF CORROED AREA ARE= L=0.517", W=0.905" D=0.042.

Part: DAMPER — NO TEST (PAX DOOR) · airframe 46,589 hrs · 24,206 cycles

CHK H2. WILL NOT PASS OPERATIONAL TEST FINGER DOOR DAMPER PASSENGER CREW DOOR 831 HARD IMPACT DURING CLOSING OPERATION AT FWD GALLEY AREA (1 EA). REPLACED DOOR DAMPER PASSENGER CREW DOOR 831 AT FWD GALLEY AREA AS PER A320 FAM 52-11-14-400-001-B.

Part: FLOOR SUPPORT — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 46,589 hrs · 24,206 cycles

CORROSION FLOOR BEAM +Y1292 LOC.BTW FR 16 TO FR 20 AT FWD GALLEY AREA. REPLACED FLOOR BEAM +Y1292 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DWG D53110920, ISSUE=D, AND DWG D53110984, ISSUE=B, AND DWG D53112812, ISSUE =E.

Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 46,589 hrs · 24,206 cycles

CORROSION FLOOR BEAM -Y765 BTW FR 66 TO FR 70 AT AFT GALLEY AREA (1EA). REPLACED FLOOR BEAM -Y765 BTW FR 66 TO FR 70 AT AFT GALLEY AREA (1EA) AS PER A319 SRM 51-72-11 AND DWG D53472093, ISSUE D, AND DWG D53472816, ISSUE A,

Part: SEAT TRACK — CORRODED (FRAMES 47-51) · corrosion level 2 · airframe 46,589 hrs · 24,206 cycles

CORROSION SEAT TRACK FLANGE FROM FR47/51 + 15.5 IN IN PASSENGER CABIN. REPLACED SEAT TRACK Y765 BTW FR 47/51 TO FR 64 IN PASSENGER CABIN AS PER A319 SRM 51-72-11 AND AIRBUS A319 DWG 53472554 REV G AND DWG D53476977 REV A.

Part: FLOOR SUPPORT — CORRODED (FRAME 16) · corrosion level 2 · airframe 46,589 hrs · 24,206 cycles

CORROSION FLOOR BEAM +Y254 LOC. ON FR 16 AT FWD GALLEY AREA. REPLACED FLOOR BEAM +Y254 LOC ON FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND DWG D53110920, ISSUE=D, RELEASE DATE 07 DEC 99, DWG D53110984. ISSUE=B, RELEASE DATE 25 JUN 05 DWG D53112816.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,589 hrs · 24,206 cycles

CORROSION LEVEL: 2 CORROSION FLOORBEAM -Y160 BTW FR66 TO FR 68 AT AFT GALLEY AREA (1 EA). REPLACED FLOORBEAM -Y160 BTW FR 66 AND FR 68 AT AFT GALLEY AREA (1 EA) ASPER SRM 51-42-11, 51-72-11 AND DWG #D5347278000.

Part: LENS — UNSECURE (CABIN) · airframe 45,204 hrs · 23,456 cycles

EMERGENCY FLOOR LIGHT DAMAGE AT 2C. RESECURED LENS AT 2C. OK FOR SVC.

Part: TRUNNION — WORN (TE FLAP) · airframe 41,886 hrs · 21,755 cycles

WEAR ON IB FLAP TRACK 1 TRUNNION ON RT WING, REPLACED INBOARD FLAP TRACK 1 TRUNNION ON RT WING AS PER PRI 561855-14 REVISION 0 AND ER/A 561855-14AD REVISION ORIGINAL.

Part: CONTROL UNIT — NO TEST (EMERGENCY LIGHTS) · airframe 40,743 hrs · 21,229 cycles

AFT EPCU WON'T TEST. REPLACED THE AFT EPCU.

Part: STRINGER — DAMAGED (FRAMES 51-52) · airframe 39,962 hrs · 20,825 cycles

DAMAGE ON STRINGER 4R BETWEEN FRAMES 51 & 52, INSTALLED A NEW STRINGER IAW SRM 53-00-13-300-001.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 46,045 hrs · 23,912 cycles

RT FRACTAL ANTENNE LOCATED 1 ROW FWD OF DWG LOCATION, REPAIR PER ER/A 554888-14 SECTION 1.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,300 hrs · 20,487 cycles

LEFT AFT EXIT FAULT WHEN CHECKING EMERGENCY LIGHTS, REPLACED AFT EPSU WITH BATTERY

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 36,440 hrs · 19,033 cycles

ROW 23 D, E, F EMERGENCY LIGHT INOPERATIVE, SECURED LOOSE CONNECTION.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 36,263 hrs · 18,940 cycles

RIGHT ELEVATOR NR 6 HINGE FITTING BOLT HOLE WORN AT INBD SIDE, REPLACED NR 6 HINGE FITTING ON RT ELEVATOR AND INBD & OTBD BUSHINGS.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 36,263 hrs · 18,940 cycles

AFT CARGO FLOOR PANEL 161NF IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW DWG NW3025-40532.

Part: PANEL — DAMAGED (AFT CARGO BAY) · airframe 36,263 hrs · 18,940 cycles

AFT CARGO SLOPE PANEL 152XG IS DAMAGED, PUNCTURED & DELAMINATED PANEL FOUND TO BE DELAMINATED, 11" X 10", FABRICATED NEW PANEL 152XG ON VT MAE TRAVELER T15/1166324 IAW DWG NW3025-40532.

Part: PANEL — DAMAGED (AFT CARGO BAY) · airframe 36,263 hrs · 18,940 cycles

AFT CARGO SLOPE PANEL 161 FF IS DAMAGED, DELAMINATED & PUNCTURED. PANEL FOUND TO BE DELAMINATED, 10" X 12". FABRICATED NEW PANEL 161FF ON VT MAE TRAVELLER T15/1166319 IAW DWG NW 3025-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 36,263 hrs · 18,940 cycles

AFT CARGO FLOOR PANEL 151ZG IS DAMAGED, PUNCTURED & DELAMINATED PANEL FOUND TO BE DELAMINATED, 10" X 11", FABRICATED NEW PANEL 151ZG ON VT MAE TRAVELER T15/1166315 IAW DWG NW3025-40532.

Part: PANEL — DAMAGED (AFT CARGO BAY) · airframe 36,263 hrs · 18,940 cycles

AFT CARGO SLOPE PANEL 151AE IS DAMAGED, PUNCTURED & DELAMINATED PANEL FOUND TO BE DELAMINATED 9" X 15", FABRICATED NEW PANEL 151AE ON VT MAE TRAVELER T15/1166325 IAW DWG NW3025-40532.

Part: PANEL — DAMAGED (AFT CARGO BAY) · airframe 36,263 hrs · 18,940 cycles

AFT CARGO SLOPE PANEL 151CE IS DAMAGED, DELAM 70 PERCENT, PANEL FOUND TO BE DAMAGED 70 PERCENT, DELAMINATION, FABRICATED NEW PANEL 151CE ON VT MAE TRAVELER T15/1166317 IAW DWG NW3025-46532.

Part: PANEL — DAMAGED (AFT CARGO BAY) · airframe 36,263 hrs · 18,940 cycles

AFT CARGO SLOPE PANEL 151DE IS DAMAGED, PUNCTURED. PANEL FOUND TO HAVE SEVERAL PUNCTURES, OVER 60 PERCENT, FABRICATED NEW PANEL 151DE ON VT MAE TRAVELER T15/1166316 IAW DWG NW3025-405832.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 36,263 hrs · 18,940 cycles

AFT CARGO FLOOR PANEL 151VG IS DAMAGED, PUNCTURED & DELAMINATED PANEL FOUND TO BE DAMAGED/DELAMINATED, 10" X 10", FABRICATED NEW PANEL 151VG ON VT MAE TRAVELER T15/1166314 IAW DWG NW3025-40532.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 36,263 hrs · 18,940 cycles

CABIN FLOOR PANEL 241KF, DELAMINATED, 2" X 10", FABRICATED NEW PANEL 241KF ON VT MAE TRAVELER T15/1166326 IAW DWG NW3D25-40640.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 36,263 hrs · 18,940 cycles

FLOOR PANEL FOUND TO BE DELAMNATED, 13" X 9", REPLACED PANEL 261 DF IAW SRM 51-72-11.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 36,263 hrs · 18,940 cycles

FLOOR PANEL 161DF HAS EDGE DAMAGE, 6.5"X .500". FABRICATED FLOOR PANEL IAW DWG NR NW3D25-40640.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 36,263 hrs · 18,940 cycles

AFT CABIN FLOOR PANEL 252JG IS DELAMINATED, 14" X 7", FABRICATED NEW PANEL IAW DWG NW3D25-40640.

Part: FLOOR PANEL — DELAMINATED (AFT CABIN) · airframe 36,263 hrs · 18,940 cycles

AFT CABIN FLOOR PANEL 251YF IS DELAMINATED, 12" X 6". FABRICATED NEW FLOOR PANEL IAW DWG NW3D25-40640.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 35,800 hrs · 18,652 cycles

EMERGENCY SEAT MOUNTED LIGHTING DAMAGED INOPERATIVE LOCATIONS:01B. RE-CONNECTED EMERGENCY LIGHT AND FUNCTIONAL CHECK WAS NORMAL.

Part: SKIN — CORRODED (FRAMES 59-60) · airframe 33,073 hrs · 17,118 cycles

CORROSION FOUND ON SKIN AT STRINGER 43L, BETWEEN FRAMES 59 - 60. FABRICATED COUPLING. INSTALLED REPAIR IAW SRM 53-00-13.

Part: STRINGER — CORRODED (FRAMES 59-60) · airframe 33,073 hrs · 17,118 cycles

CORROSION FOUND AT STRINGER 42L, BETWEEN FRAMES 59-60. REMOVED CORROSION IAW SRM 53-00-13, FIG 202, SHEET 4 MSIP 81196, PERFORMED HFEC OF BLENDED AREA IAW NDTM 51-00-08, PG 1. NO CRACKS FOUND AND PERFORMED UT THICKNESS MEASSUREMENT IAW NDTM 51-10-04 PB4. FABRICATED COUPLING. INSTALLED REPAIR IAW SRM 53-00-13.

Part: WIRE — EXPOSED (EMERGENCY LIGHTS) · airframe 31,597 hrs · 16,333 cycles

22 ABC EMERGENCY LIGHT WIRES EXPOSED. SEATED WIRES INTO FLOOR CONDUIT IN SEAT TRACK.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,215 hrs · 16,139 cycles

FUSELAGE SKIN DENTED SEVEN INCHES FWD OF FRAME 77, 3.75 INCHES BELOW S28R. DENT WITHIN LIMITS IAW SRM 53-51-11 FIG 103.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 162CF HAS MULTIPLE DENTS, EDGE DAMAGED & CRACKED. SLOPE PANEL FABRICATED IAW AMM 25-50-00-340-007-A, SRM 53-02-00, FIG 209 & DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 151BE HAS MULTIPLE DENTS & DISBONDED. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL HAS FOUR PREVIOUS REPAIRS & MULTIPLE DENTS. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 161BF HAS TWO PREVIOUS REPAIRS, MULTIPLE DENTS, SCRATCHES PUNCTURED & EDGE DAMAGED. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR SUPPORT — GOUGED (CABIN) · airframe 31,203 hrs · 16,131 cycles

FOUND SUPPORT FITTING GOUGED AND HAS AN ELONGATED HOLE. REMOVED DAMAGE IAW SRM 51-73-00.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 151GE HAS PREVIOUS REPAIRS, SCRATCHES & MULTIPLE DENTS. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 151GE HAS PREVIOUS REPAIRS, SCRATCHES & MULTIPLE DENTS. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 161CF HAS MULTIPLE DENTS, SCRATCHES & PUNCTURED. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 31,203 hrs · 16,131 cycles

FWD CARGO BAY SLOPE PANEL 131EG HAS MULTIPLE DENTS & CRACKED. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 152WG HAS THREE PREVIOUS REPAIRS, MULTIPLE DENTS & PUNCTURED. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY FLOOR PANEL 151CE HAS PREVIOUS REPAIR, MULTIPLE DENTS & DISBONDED. FLOOR PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR SUPPORT — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 151FE HAS MULTIPLE DENTS, PUNCTURED & CRACKED. SLOPE PANEL FABRICATED IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.

Part: FLOOR SUPPORT — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 151AE HAS MULTIPLE DENTS, SCRATCHES, PUNCTURED & DISBONDED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR SUPPORT — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 151TG HAS MULTIPLE DENTS & PUNCTURED. SLOPE PANEL FABRICATED IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY FLOOR PANEL 161PF HAS PREVIOUS REPAIR & DISBONDED. FLOOR PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 162FF HAS MULTIPLE DENTS & CRACKED. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 151DE HAS MULTIPLE DENTS & DISBONDED. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 152UG HAS PREVIOUS REPAIR, MULTIPLE DENTS & CRACKED. SLOPE PANEL FABRICATED IAW SRM 53-02-00 FIG 209, AMM 25-50-00-340-007-A AND DWG 3D25-40532.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,203 hrs · 16,131 cycles

DURING VISUAL INSPECTION, FOUND A DENT THAT IS OUT OF LIMITS FRAMES 23-24 S22L IAW SRM 53-11-11 DIAGRAM 103. CUT OUT DAMAGE SKIN, FABRICATED & INSTALLED DOUBLER & FILLER IAW SRM 51-42-11 & SRM 53-00-11 FIG.231.

Part: FLOOR SUPPORT — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 151UG HAS TWO PREVIOUS REPAIRS, MULTIPLE DENTS & CRACKED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 31,203 hrs · 16,131 cycles

FWD CARGO BAY SLOPE PANEL 132EG HAS FOUR PREVIOUS REPAIRS, MULTIPLE DENTS, PUNCTURES & DISBONDED. SLOPE PANEL FABRICATED IAW DWG 3D25-40532 AND SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 31,203 hrs · 16,131 cycles

FWD CARGO BAY FLOOR PANEL 131AF HAS FOUR PREVIOUS REPAIR & MULTIPLE DENTS WITH CRACKED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 31,203 hrs · 16,131 cycles

FWD CARGO BAY SLOPE PANEL 132DG HAS MULTIPLE DENTS, PUNCTURED, CRACKED & DISBONDED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY SLOPE PANEL 152TG HAS MULTIPLE DENTS & PUNCTURED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 31,203 hrs · 16,131 cycles

FWD CARGO BAY SLOPE PANEL 131DG HAS SIX PREVIOUS REPAIRS, MULTIPLE DENTS & CRACKED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY FLOOR PANEL 151ZG HAS THREE PREVIOUS REPAIRS, MULTIPLE DENTS & PUNCTURED. FLOOR PANEL FABRICATED IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 31,203 hrs · 16,131 cycles

FWD CARGO BAY FLOOR PANEL 131CG HAS FOUR PREVIOUS REPAIRS, MULTIPLE DENTS, PUNCTURED & DISBONDED. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 31,203 hrs · 16,131 cycles

FWD CARGO BAY SLOPE PANEL 131CF HAS MULTIPLE DENTS, PREVIOUS REPAIR & PUNCTURED. SLOPE PANEL FABRICATED IAW SRM 53-02-00, FIG 209 AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (AFT CARGO BAY) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY FLOOR PANEL 151VG HAS MULTIPLE DENTS, PUNCTURED & CRACKED. FLOOR PANEL FABRICATED IAW AMM 25-50-00-340-007-A AND DWG 3D25-40532.

Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY FLOOR PANEL 161NF HAS MULTIPLE DENTS & PUNCTURED. FLOOR PANEL FABRICATED IAW AMM 25-50-00-340-007-A AND DWG 3D25-4032.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 31,203 hrs · 16,131 cycles

DURING CLEANING, FOUND FWD CABIN FLOOR SUPPORT Y503.2 AT FRAME 16 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-11-14, FIG 106. R & R FLOOR SUPPORT IAW TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 31,203 hrs · 16,131 cycles

FORWARD UTILITY AREA FLOOR SUPPORT Y-765 BETWEEN FRAMES 16-20 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, FIG 101. REMOVED & INSTALLED FLOOR SUPPORT IAW TRM 53-21-01. CUT OUT DAMAGED AREA IAW 53-11-15, FIG 207. FABRICATED REPAIR FILLER & TWO REPAIR SPLICES IAW SRM 53-11-15, FIG 207. MACHINED REPAIR SPLICES IAW SRM 53-11-15. INSTALLED REPAIR FILLER AND REPAIR SPLICES IAW SRM 53-11-15, FIG 207.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT Y765 BETWEEN FRAMES 66-69 UPPER FLANGE CORRODED.BLENDED AREA IAW SRM 51-74-00 AND FOUND OUT OF LIMIT IAW SRM 53-00-14, FIG 102. R & R FLOOR SUPPORT IAW SRM 51-42-11 & DWG D53472815.

Part: FLOOR PANEL — CORRODED (AFT CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR PANEL 261FF CORRODED. INSTALLED NEW FLOOR PANEL.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT Y1292 BETWEEN FRAMES 66 - 68 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT Y1292 BETWEEN FRAMES 68-69 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 31,203 hrs · 16,131 cycles

FORWARD UTILITY AREA FLOOR SUPPORT Y-254, BETWEEN FRAMES 16 - 20 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT Y1292 BETWEEN FRAMES 64-66 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: HINGE PIN — CORRODED (AILERON) · airframe 31,203 hrs · 16,131 cycles

RIGHT WING AILERON HINGE PIN CORRODED. NEW HINGE PIN INSTALLED ON JIC 5760-1010S-RT.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT Y765 BETWEEN FRAMES 64-66 UPPER FLANGE & HARDPOINT HOLES CORRODED. BLENDED AREA IAW SRM 51-74-00. FOUND OUT OF LIMIT IAW SRM 53-00-14, FIG 102. R & R FLOOR SUPPORT IAW SRM 51-42-11 & DWG D53472815.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 252GF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 241MF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 252MF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 231XG UPPER SURFACE DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 222EF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 261HG DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 231CF HAS CORRODED INSERTS. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 261HG DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT Y-1292, BETWEEN FRAMES 68 - 69 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 221DF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 241CF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 241HF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 251JF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 251TF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT Y-1292 BETWEEN FRAMES 66 - 68 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 232FF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 241JF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG.102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 231LF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 242KF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR SUPPORT — CORRODED (AFT CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT Y-1292, BETWEEN FRAMES 65-66 UPPER FLANGE CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 232YG DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 251LF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG.102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 31,203 hrs · 16,131 cycles

LT AFT PASSENGER/CREW DOOR SILL BEAM AT AFT INBD FRAME 66 NUTPLATE HOLES CORRODED. REPAIRED IAW SRM 53-41-14, FIG 201.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 241KF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 241AF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 221EF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW 3SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 232YG DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY FLOOR PANEL 261PF DELAMINATED AND HAS SEVERAL PUNCTURES. FOUND OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 261HG DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 31,203 hrs · 16,131 cycles

FORWARD UTILITY AREA FLOOR SUPPORT Y254 BETWEEN FRAMES 16-21 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 105. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: STRUCTURE — CORRODED (LT WING) · airframe 31,203 hrs · 16,131 cycles

LEFT WING MANUAL REFUEL OPENING INTERFACE CORRODED. REMOVED CORROSION IAW SRM 57-21-11, PAR 5E. FOUND TO BE IN LIMITS IAW SRM 57-21-11, FIG 205. PERFORMED FPI IAW NTM 51-80-00, NO DEFECTS NOTED. APPLIED CHEMICAL CONVERSION COATING IAW SRM 57-21-11, PAR 5-E.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT Y-765 BETWEEN FRAMES 64-66 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: SHEAR PLATE — CORRODED (CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA STRINGER 23R BETWEEN FRAMES 69-70, SHEAR PLATE UPPER SURFACE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. NO ESTABLISH LIMITS FOUND IN SRM 53-41-14, TABLE 101. R & R SHEAR PLATE IAW SRM 51-42-11 & DWG D53474180.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 31,203 hrs · 16,131 cycles

AFT UTILITY AREA FLOOR SUPPORT, Y-765, BETWEEN FRAMES 66-69 HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. R & R FLOOR SUPPORT IAW SRM 51-42-11 & TRM 53-21-01.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 241BF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: SILL — CORRODED · airframe 31,203 hrs · 16,131 cycles

RIGHT AFT PASSENGER/CREW DOOR SILL BEAM AT INBD FRAME 68 UPPER SURFACE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14. R & R SILL IAW SRM 51-42-11 & DWG D53480020.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 31,203 hrs · 16,131 cycles

MAIN CABIN FLOOR PANEL 251WF DELAMINATED OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 31,203 hrs · 16,131 cycles

FORWARD UTILITY AREA FLOOR SUPPORT, Y-1292 BETWEEN FRAMES 16-20 UPPER FLANGE HAS CORROSION. BLENDED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, FIG 101. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. LOCATED & DRILLED NEW FLOOR SUPPORT IAW SRM 51-44-11. INSTALLED NEW FLOOR SUPPORT IAW TRM 53-21-01.

Part: BLANKING PLATE — CORRODED (R2 DOOR) · airframe 31,203 hrs · 16,131 cycles

R2 DOOR FWD BLANKING PLATE HAS EDGE DAMAGE. NO ALLOWABLE LIMITS IAW SRM 53-02-00, FIG 101. REPLACED BLANKING PLATE IAW SRM 51-72-11.

Part: BLANKING PLATE — CORRODED (R1 DOOR) · airframe 31,203 hrs · 16,131 cycles

R1 DOOR FWD BLANKING PLATE HAS EDGE DAMAGE. NO ALLOWABLE LIMITS IAW SRM 53-02-00, FIG 101. REPLACED BLANKING PLATE IAW SRM 51-72-11.

Part: SILL — CORRODED (PAX DOORWAY) · airframe 31,203 hrs · 16,131 cycles

LEFT AFT PAX DOOR SILL AT FWD INBD FR 68 HAS NUTPLATE HOLES CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-41-14, FIG 101. CUT OUT DAMAGE. FABRICATED REPAIR ANGLE AND FILLER. INSTALLED IAW SRM 53-41-14, FIG 201 & SRM 51-42-11.

Part: WEB — CORRODED (CABIN) · airframe 31,203 hrs · 16,131 cycles

FORWARD UTILITY AREA STRINGER 23R BETWEEN FRAMES 20-21, UPPER SURFACE WEB & ANGLE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00. NO ESTABLISH LIMITS IAW SRM 53-11-14. R & R WEB & ANGLE IAW SRM 51-42-11 AND DWG D53004332.

Part: BLANKING PLATE — CORRODED (L2 DOOR) · airframe 31,203 hrs · 16,131 cycles

L2 DOOR AFT BLANKING PLATE HAS EDGE DAMAGE. NO ALLOWABLE LIMITS IAW SRM 53-02-00, FIG 101. REPLACED BLANKING PLATE IAW SRM 51-72-11.

Part: SKIN — DENTED (FWD FUSELAGE) · airframe 31,203 hrs · 16,131 cycles

LOWER FWD FUSELAGE SKIN BETWEEN FRAMES 26 & 27, STRINGERS 41 & 42R DENTED. FOUND WITHIN LIMITS IAW SRM 53-21-11, DIAGRAM 103. HFEC INSPECTED INTERNAL & EXTERNAL AREA IAW NTM 51-10-08, NO CRACK INDICATION NOTED.

Part: FLOOR SUPPORT — CORRODED (FWD CABIN) · airframe 31,203 hrs · 16,131 cycles

FORWARD CABIN FLOOR SUPPORT Y-189 BETWEEN FRAMES 20-24 UPPER FLANGE HAS CORROSION. R & R FWD CABIN FLOOR SUPPORT IAW TRM 53-21-01 & SRM 51-42-11. BLENDED AREA IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 107.

Part: FLOOR SUPPORT — CORRODED (MAIN CABIN) · airframe 31,102 hrs · 16,083 cycles

MAIN CABIN FLOOR PANEL 221PF DELAMINATED AND FOUND OUT OF LIMITS IAW SRM 53-02-00, FIG 102. FLOOR PANEL FABRICATED IAW SRM 53-02-00, FIG 9 AND DWG NW3D25-40640.

Part: SKIN — DENTED (FUSELAGE) · airframe 31,203 hrs · 16,131 cycles

NOTIFIED BY GROUND CREW OF SMALL DENT JUST AFT AND BELOW OF MAIN L1 DOOR. FOUND DENT TO BE WITHIN LIMITS PER SRM 53-11-11.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 27,997 hrs · 14,404 cycles

HOLE IN FWD CARGO FLOOR PANEL. REPAIRED IAW SRM 53-02-00 BLK 201. AIRCRAFT OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 5,134 hrs · 2,842 cycles

AIRCRAFT 3142. DURING MAINTENANCE FOUND 10WL EMERGENCY LIGHT BATTERY POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED 10WL BATTERY. TESTS OK PER AMM. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,931 hrs · 11,237 cycles

DURING A MAINTENANCE VISIT, THE GALLEY 3 FORWARD CENTER EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT ASSEMBLY WAS REPLACED.

Part: WIRE — BROKEN (CABIN) · airframe 25,801 hrs · 13,203 cycles

DURING NON ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE PATH LIGHT AT ROW 9 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 23,731 hrs · 11,970 cycles

DURING A NON-ROUTINE CHECK, THE EMERGENCY LIGHT SYS FAILED A EPSU LOAD TEST. MX FOUND A LOOSE CONNECTOR AT AFT LT SLIDE. RE-SEATED CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: SLIDE — MALFUNCTIONED (LT PAX DOOR) · airframe 22,289 hrs · 11,195 cycles

DURING A NON ROUTINE CHECK, FOUND THE EPSU EXIT LOAD AT AFT L FAULT. MX REPLACED AFT LT DOOR SLIDE, SLIDE COVER AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: LUG — GOUGED (DOOR SILL) · airframe 31,203 hrs · 16,131 cycles

AFT CARGO BAY DOOR SILL NR 5 LOCK FITTING AFT LUG GOUGED. BLENDED DAMAGE AND FOUND WITHIN LIMITS IAW SRM 53-46-11, FIG 101. WORKED AREA IAW SRM 51-29-11, PG 10 & 11..

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 19,363 hrs · 9,850 cycles

EMERGENCY EGRESS LIGHTING AT ROWS 11, 15, 16, 19, 20 INOP. REPAIRED WIRE AND REPLACED EPSU 11WL. LIGHTS CHECK GOOD.

Part: LIGHT — INTERMITTENT (CABIN) · 9,662 cycles

F/A REPORTED VARIOUS EMERGENCY EGRESS LIGHTING ( WINDOW EXITS, FLOOR AND SEAT MOUNTED) FLICKER ON AND OFF (UNREADABLE) REPLACED EPSU 11 WL, CHECKS GOOD. (K)

Part: EPSU — DISCHARGED (CABIN) · airframe 18,879 hrs · 9,616 cycles

EMERGENCY EGRESS LIGHTING, OVERWING, AFT FACING AISLE EXIT SIGN DOES NOT ILLUMINATE. REPLACED EPSU BATTERY PACK AT ROW 9ABC, OPS GOOD. (K)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 16,855 hrs · 8,595 cycles

EMERGENCY ESCAPE LIGHTING EPSU LEFT EXIT INOP. REPLACED LEFT EXIT EPSU, CHECKS GOOD.

Part: APU — LEAKING · airframe 3,729 hrs · 1,813 cycles

DURING CLIMB AND CRUISE, FLIGHT ATTENDANT REPORTED AN ODOR IN THE CABIN. EVENTUALLY COCKPIT CREW ALSO NOTICED THE ODOR. FLIGHT CONTINUED TO DESTINATION AND AN UNEVENTFUL LANDING WAS PERFORMED. MAINTENANCE FOUND AN APU OIL LEAK. REPLACED THE APU, PACK BURNOUT PERFORMED, AND OZONE CONVERTERS AND RECIRCULATION FILTERS WERE REPLACED.