N810NW

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 91,158 hrs · 11,978 cycles

FOUND TWO CRACKS ON THE FRAME FR61A FRAME FORK AREA, ONE CRACK ON THE FRAME FORK AREA H-1, ANOTHER CRACK ON THE FRAME FORK AREA H-2, AT BEAM 4 IN THE AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: REPLACED FORK PER DELTA WORK CARDS 5230- 01164-08 REV MAY 09 2025 AND CARD 5230-01164-10. (1374588)

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 91,158 hrs · 11,978 cycles

FOUND TWO CRACKS ON THE AFT CARGO DOOR FRAME 63 - FRAME FORK AREA, ONE CRACK ON THE FRAME FORK AREA H-5, ANOTHER CRACK ON THE FRAME FORK AREA H-6. CORRECTIVE ACTION:FR 63 FRAME FORK REPLACEMENT AS PER CARD 5230- 01164-08 REV MAY 09 2025 08:50 AND CARD 5230-01164-10 REV AUG 08 2023. (1374577)

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 91,158 hrs · 11,978 cycles

FOUND TWO CRACKS ON THE AFT CARGO DOOR FRAME 61 - FRAME FORK AREA, ONE CRACK ON THE FRAME FORK AREA H-5, ANOTHER CRACK ON THE FRAME FORK AREA H-6. CORRECTIVE ACTION: FR61 FRAME FORK REPLACEMENT AS PER CARD 5230- 01164-08 REV MAY 09 2025 AND CARD 5230-01164-10 REV AUG 08 2023

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 91,158 hrs · 11,978 cycles

FOUND TWO CRACKS ON THE AFT CARGO DOOR FRAME 61A - FRAME FORK AREA, ONE CRACK ON THE FRAME FORK AREA H-5, ANOTHER CRACK ON THE FRAME FORK AREA H-6. CORRECTIVE ACTION: FR 61A FRAME FORK REPLACEMENT AS PER CARD 5230- 01164-08 REV MAY 09 2025 08:50 AND CARD 5230-01164-10 REV AUG 08 2023. (1374510)

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 91,158 hrs · 11,978 cycles

FOUND ONE CRACK ON THE FRAME 63 FRAME FORK AREA H-2 AT BEAM 4 ON THE AFT CARGO DOOR. FR 63 FRAME FORK REPLACEMENT AS PER CARD 5230- 01164-08 REV MAY 09 2025 AND CARD 5230-01164-10 REV AUG 08 2023. (1374581)

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 91,158 hrs · 11,978 cycles

FOUND 02 EA CRACKS ON THE FRAME FR61 FRAME FORK AREA, ONE CRACK ON THE FRAME FORK AREA H-1, ANOTHER CRACK ON THE FRAME FORK AREA H-2, AT BEAM 4 IN THE AFT CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: FR 61 FRAME FORK REPLACEMENT AS PER CARD 5230- 01164-08 REV. MAY 09 2025 AND CARD: 5230-01164-10 REV. AUG 08 2023.

Part: SKIN — DAMAGED (ZONE 100) · airframe 90,771 hrs · 11,927 cycles

FUSELAGE / STR 25-26 AND STA 7942-7662 / LIGHTNING STRIKE DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 630330-14 REVISION B. (1293132)

Part: SKIN — DAMAGED (ZONE 100) · airframe 90,771 hrs · 11,927 cycles

STRINGERS 25-26 AND BS 7942-7662 LIGHTNING STRIKE DAMAGE. REPAIRED PER ERA 630330-14 REV A REV 0. (1293332)

Part: LATCH — BROKEN (OXYGEN PANEL) · airframe 90,712 hrs · 11,920 cycles

SHIP 3310 OXYGEN PANEL LATCH BROKEN AT LOCATION 103. CORRECTIVE ACTION: RESET LATCH AND CLOSED PER A330 AMM 35-21. OK FOR SERVICE. (1277133)

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 90,706 hrs · 11,919 cycles

SHIP 3310 EEPLS LIGHT AT SEAT 43 H INOP. CORRECTIVE ACTION: REPAIRED WIRE PER A330 ESWPM 20-45 AND AWM 33-51. OP CHECK GOOD. (7877975)

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 90,519 hrs · 11,895 cycles

SHIP 3310 DURING SVC CHECK FOUND DOORS 1L,1R,2L,4L & 4R ASSIST BOTTLES LOW. CORRECTIVE ACTION: SERVICED DOOR BOTTLES PER A330 AMM 52-15. (7649074)

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 90,275 hrs · 11,863 cycles

FWD CARGO SURROUND SKIN / FR19 STR 37R-39R / IMPACT DAMAGE. COMPLIED WITH ERA 628935- 14 REV ORIG. (1218334)

Part: SKIN — DAMAGED (ZONE 100) · airframe 90,275 hrs · 11,863 cycles

SHIP 3310 LOWER SKIN PANEL P/N F5327060020000 DAMAGED BELOW STRG 39 R/H AT FR 19. REPAIRED PER ERA 629171-14 REV. ORIG. (1218232)

Part: REPAIR — NOT REPORTED (ZONE 100) · airframe 90,275 hrs · 11,863 cycles

FWD FUSELAGE, FR18 & 19, STGR 39RT, LOWER SKIN PANEL, DOUBLER REPAIR. COMPLIED WITH ERA 629171-14. (1217643)

Part: SKIN — GROUND DAMAGE (ZONE 100) · airframe 90,275 hrs · 11,863 cycles

FWD CARGO SURROUND SKIN, FR19, STR 37R - 39R, IMPACT DAMAGE. REPAIRED PER ERA 628935-00. (1217760)

Part: FRAME — DAMAGED · airframe 90,275 hrs · 11,863 cycles

FRAME 19R DAMAGED BETWEEN STRINGER 37R. REPLACED FRAME 19R PER A330 SRM 51-42-11. (1212144)

Part: STRINGER — DAMAGED (ZONE 100) · airframe 90,275 hrs · 11,863 cycles

STRINGER 39R DAMAGED BETWEEN FR 18. REPLACED STRINGER PER A330 SRM 51-42. (1212141)

Part: STRINGER — DAMAGED (ZONE 100) · airframe 90,275 hrs · 11,863 cycles

STRINGER 38R DAMAGED BETWEEN FR 18. REPLACED STRINGER PER A330 SRM 51-42. (1212147)

Part: WIRE — DAMAGED (ZONE 200) · airframe 88,386 hrs · 11,624 cycles

SHIP 3310 EMERGENCY EXIT LIGHTS (FLOOR PATH) AT ROWS 37 AND 41JH ARE INOP. CORRECTIVE ACTION: REPAIRED WIRING PER A330 AMM 33-52. OK TO CONTINUE. (7562405)

Part: WIRE — DAMAGED (ZONE 200) · airframe 88,074 hrs · 11,585 cycles

SHIP 3310 WHITE SEAT MOUNTED EMER PATH LIGHTS INOP AT SEATS 56B, 53H, 44H, 40H. CORRECTIVE ACTION: REPAIRED WIRING PER A330 AMM 33-51. (7128679)

Part: OXYGEN MASK — DISLODGED (ZONE 200) · airframe 87,921 hrs · 11,567 cycles

SHIP 3310 F/A O2 MASK FWD GALLEY FELL OUT ON LANDING. CORRECTIVE ACTION: REPACKED MASKS PER A330 AMM 35-23. OK FOR SERVICE. (7128630)

Part: WIRE — DAMAGED (ZONE 200) · airframe 86,020 hrs · 11,325 cycles

SHIP 3310 ROWS 55B-58B EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: FOUND DAMAGED WIRES AT 55 AND 58 WALL CONNECTORS, REPAIRED PER A330 AWM 33-51. OK FOR SERVICE. (6394086)

Part: DOOR — UNSECURE (OXYGEN PANEL) · airframe 85,427 hrs · 11,253 cycles

SHIP 3310 FOUND PAX OXYGEN MASK COMPARTMENT DOOR AT 49 C/D/F/G BROKEN. CORRECTIVE ACTION: R/R O2 CONTAINER PER A330 AMM 35-21-41. OPS CHECK GOOD. (5564548)

Part: HINGE — DAMAGED (OXYGEN DOOR) · airframe 84,800 hrs · 11,170 cycles

SHIP 3310 FOUND PASSENGER OXYGEN DOOR AT SEAT 42HJ HINGE DAMAGE. CORRECTIVE ACTION: R/R PASSENGER OXYGEN CONTAINER AT SEAT 42HJ PER A330 AMM 35-21. OPS CK OK. (6097813)

Part: LATCH — BROKEN (ZONE 200) · airframe 84,769 hrs · 11,165 cycles

SHIP 3310 OXYGEN PANEL LATCH BROKEN / LOCATIONS:206. CORRECTIVE ACTION: R/R LAV 206 OXYGEN CONTAINER ASSY PER A330 AMM 35-21. OK FOR SERVICE. (0463628)

Part: LATCH — BROKEN (OXYGEN PANEL) · airframe 84,673 hrs · 11,153 cycles

SHIP 3310 OXYGEN PANEL LATCH BROKEN / LOCATIONS:206. CORRECTIVE ACTION: RESECURED OXYGEN PANEL PER A330 AMM 35-21. OK FOR SVC. (0460497)

Part: OXYGEN MASK — UNWANTED DEPLOY (AFT LAVATORY) · airframe 84,526 hrs · 11,135 cycles

SHIP 3310 COVER FOR OXYGEN MASK IN 3L AFT LAV CONTINUES TO POP OPEN REVEALING OCYGEN MASK. THEY ARE NOT PHYSICALLY HANGING DOWN BUT ARE EXPOSED BECAUSE THE COVER WILL NOT STAY LATCHED. CORRECTIVE ACTION: REPACKED MASKS PER A330 AMM 35-23. OK TO CONTINUE. (0436812)

Part: LATCH — BROKEN (OXYGEN PANEL) · airframe 84,392 hrs · 11,118 cycles

SHIP 3310 OXYGEN PANEL LATCH BROKEN / LOCATIONS:206. CORRECTIVE ACTION: OPENED AND RE-SET DOOR PANEL PER A330 AMM 35-23. OPS GOOD. (0422395)

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 84,298 hrs · 11,107 cycles

OXYGEN MASKS DEPLOYED IN 4R AND OVER SEATS 32 H+J. RE-PACKED MASKS PER A330 AMM 35-23. OK FOR SERVICE.

Part: OXYGEN PANEL — BROKEN · airframe 84,263 hrs · 11,103 cycles

SHIP 3310 DOOR 4R O2 PANEL BROKEN. CORRECTIVE ACTION: R/R O2 CONTAINER ASSY. AT 4R DOOR REF. A330 AMM 35-21 OPS CHECK GOOD. (5569951)

Part: JUMPSEAT — DETACHED (CABIN) · airframe 83,070 hrs · 10,953 cycles

SHIP 3310 ON ROTATION 3L FA JUMPSEAT CAME DETACHED FROM LAV WALL FA BROKE FALL WITH KNEES. CORRECTIVE ACTION: REINSTALLED DOOR 3L FA SEAT PER A330 AMM 25-22. OPS CHECK GOOD. OK FOR SERVICE. (0250887)

Part: LATCH — BROKEN (OXYGEN PANEL) · airframe 82,939 hrs · 10,934 cycles

SHIP 3310 OXYGEN PANEL LATCH BROKEN / LOCATIONS:45C. CORRECTIVE ACTION: RESECURED PAX O2 PANEL IAW A330 AMM 35-21. OK FOR SVC. (0235117)

Part: CONTROL UNIT — UNKNOWN (DOORS) · airframe 82,599 hrs · 10,891 cycles

SHIP 3310 FAP SHOWS " SLIDE ICE PROT NO DATA" DOOR 4L + 4R. CORRECTIVE ACTION: REMOVED & REPLACED IPCU (16DS). CHECKS GOOD PER A330 AMM 25-27. (4589262)

Part: CONTROL UNIT — UNKNOWN (DOORS) · airframe 82,599 hrs · 10,891 cycles

SHIP 3310 FAP SHOWS "SLIDE ICE PROT NO DATA" DOOR 3L+R. CORRECTIVE ACTION: R/R IPCU 33-3070-9-0005 PER A330 AMM 30-44. (4589261)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR INNER SKIN AT FR63 TO FR63A IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 614061-14, VALIDATED ER/A 614061-14 MATCHES PRI 614061-14. EXISTING REPAIRINSTALLED PER ER/A 550537-14. (0149219)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR AFT LOWER CORNER PASSEN GER CREW DOOR L4 IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WITH PRI 614061-14, VALIDATED ER/A 614061-14 MATCHES PRI 614061-14. EXISTING REPAIRINSTALLED PER A330 SRM 52-13-00. FIGURE 213, WHICH IS CURRENTLY A330 SRM 52-13-00-300-013. (0149283)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR. CORRECTIVE ACTION: COMPLIED WITH PRI 614061-14, VALIDATED ER/A 614061-14 MATCHES PRI 614061-14. EXISTING REPAIR INSTALLED PER A330 SRM 57-40-00, FIGURE 203, WHICH IS CURRENTLY A330 SRM 57-40-00-300-008. REPAIR IS INSTALLED BETWEEN WFX 17315AND 17680; THEREFORE, REPAIR IS CONSIDERED AS CATEGORY A. RII INSPECTION COMPLETE. (0149322)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR INNER SKIN LOCATED FR61 TO FR61A IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 614061-14, VALIDATED ER/A 614061-14 MATCHES PRI 614061-14. EXISTING REPAIRINSTALLED PER ER/A 597679-14, APPROVED AS PER AIRBUS RDAF 81032770/003/2022, ISSUE B. DURING INSPECTION, ONE (1) PULLED RIVETS WAS FOUND. INSPECTION WERE EXECUTED WITH NIL FINDING, AND IT WAS REMOVED AND REPLACED AS PER ER/A 597679-14 WITHOUT DEVIATIONS. (0149250)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK RIB 6 AFT ON RH WING. CORRECTIVE ACTION: COMPLIED WITH PRI 614061-14, VALIDATED ER/A 614061-14 MATCHES PRI 614061-14. EXISTING REPAIRINSTALLED PER EM 5720-01066-04B. REPAIR IS APPROVED PER SB A330-57-3088 R02 ACCORDING TO FAA AD 2006-22-14, PARA. (N)GUIDELINES.EM 5720-01066-04B TERMINATE INSPECTION AND MODIFICATION REQUIREMENTS. RII INSPECTION COMPLETE. (0149289)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,379 hrs · 10,862 cycles

SHIP 3310 DURING CURRENT H CHECK, WHILE EXECUTION OF JC 5310-01461-03 IN ORDER TO PERFORM A330-SB-53-3273 REV 2 AND OVERSIZED HOLE WAS FOUND (G4) BETWEEN FR53.6 AND FR53.7 AT STGR5LH. AS PER MANUALS (A330 SRM 53-31-11-17A), STRUCTURES PRESENT IN THE AFFECTED HOLE ARE PN F5337005121000 (M/F T351, ABS5043A080) AND UPPER STRAP PN F5337007320200 (M/F T351, ABS5044A060). CORRECTIVE ACTION: REF ER/A 614675-14AD. (0149967)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

AHIP 3310 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SLAT 2 EXTERNAL SKIN ON RH WING. CORRECTIVE ACTION: COMPLIED WITH PRI 614061-14, VALIDATED ER/A 614061-14 MATCHES PRI 614061-14. EXISTING REPAIR INSTALLED PER A330 SRM 57-40-00, FIGURE 203, WHICH IS CURRENTLY A330 SRM 57-40-00-300-029. REPAIR IS CONSIDERED AS CATEGORY A. (0149316)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,379 hrs · 10,862 cycles

SHIP 3310 DURING CHECK ESCAPE SLIDE FACILITIES THE MESSAGE CHECK SLIDE PRESSURE WAS NOT DISPLAY ON DOOR R1. CORRECTIVE ACTION: REMOVE AND REPLACE SLIDE AT 1 RH. (0147689)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,379 hrs · 10,862 cycles

SHIP 3310 DONT PASS SLIDE L3 EMERGENCY LIGHT TEST. CORRECTIVE ACTION: REMOVED AND REPLACED SLIDE AT 3 LH EMERGENCY EXIT. PERFORMED OPERATIONAL EMERGENCY LIGHT TEST. (0147682)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 DELAMINATED DOOR L2 SUPPORT ARM IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED DOOR L2 SUPPORT ARM IN PASSENGER CABIN. (0146328)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 CORROSION ELECTRICAL CONNECTOR DOOR R1 IN PASSENGER CABIN (3 EA). CORRECTIVE ACTION: REPLACED ELECTRICAL CONNECTOR 10MJ, 42MJ AND 44MJ ON ACCESS DOOR R1 IN PASSENGER CABIN. PERFORMED OPERATIONAL TESTS OF THE DOOR MONITORING SYSTEM, SLIDE ARMED AND CABIN PRESSURE INDICATIONS. TESTS ARE GOOD. (0146323)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR FUEL TANK RIB6 AFT ON L H WING. CORRECTIVE ACTION: COMPLIED WITH PRI 614061-14, VALIDATED ER/A 614061-14 MATCHES PRI 614061-14. EXISTING REPAIR INSTALLED PER EM 5720-01066-04A. REPAIR IS APPROVED PER SB A330-57-3088 R02 ACCORDING TO FAA AD 2006-22-14, PARA.(N) GUIDELINES. (0146842)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 DURING H CHECK, WHILE EXECUTION OF INSPECTIONS IN THE AVIONICS COMPARTMENT AS PER JOB CARD 5311-2001 (EXECUTION OF A GENERAL VISUAL INSPECTION OF THE FUSELAGE INTERNAL STRUCTURE FROM FR1 TO FR20, RELATED TO MRB 531117-01-1), A CRACK OF 5.85" WAS DETECTED IN A BEAM LOCATED AT -Y790 (RH SIDE), FR7 LEVEL, FLOOR STRUCTURE IN THE FWD AVIONICS COMPARTMENT. A DETAILED VISUAL INSPECTION AS PER NTM 51-90-00 HAS BEEN EXECUTED ON THE ADJACENT AREA OF THE AFFECTED WEB; AS A RESULT, IT HAS BEEN CONFIRMED THAT CRACK IS ONLY PRESENT IN THE WEB, AND THERE IS NO ADDITIONAL DAMAGE TO REPORT. SRM 53-11-14 DOES NOT PROVIDE ADL OR REPAIR INSTRUCTIONS FOR THE CURRENT SITUATION. CORRECTIVE ACTION: ER/A 614476-14 HAS BEEN ISSUED TO PERFORM A REPAIR UNDER AIB´S ASSESSMENT, PRECISELY BY EXECUTING INSPECTIONS AND REPAIR AS PER SB A330-53-3231 R01, R531-15278 ISSUE A AND R531-15270 ISSUE D. REF ER/A 614476-14 FOR REPAIR. (0144852)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 DURING CURRENT H CHECK, WHILE EXECUTION OF JC 5310-01461-03 IN ORDER TO PERFORM A330-SB-53-3273 REV 2 AND OVERSIZED HOLE WAS FOUND (G4) BETWEEN FR53.6 AND FR53.7 AT STGR5LH. CORRECTIVE ACTION: REF ER/A 514675-14AD. (0144774)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 DURING H CHECK AT AEM, WHILE EXECUTION OF A SURVEY TO IDENTIFY ALL REINFORCING REPAIRS TO FATIGUE CRITICAL STRUCTURE AS PER JOB CARD 5100 01848-02B-02 AND ER/A 614061-14, AN EXISTING REPAIR WAS FOUND IN THE AFT CC DOOR, INNER SKIN BETWEEN FR62 AND FR62A. NO RECORDS WERE FOUND OF THE APPROVAL SOURCE/REFERENCE USED TO PERFORM THE REPAIR. THEREFORE, BECAUSE OF THE LACK OF APPROVAL SOURCE, THIS EXISTING REPAIR HAS BEEN REMOVED. CORRECTIVE ACTION: ER/A 614697-14 HAS BEEN ISSUED TO PERFORM A REPAIR UNDER AIB´S ASSESSMENT. REF SAME FOR REPAIR. (0144842)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 DURING H CHECK AT AEM (SAL) WHILE EXECUTION OF JIC 5716-01017-01 REGARDING THE INSPECTION OF FASTENER HOLES AT FR40 VERTICAL WEB (SB A330-57-3115 REV 02 AND A330-57-3131 REV 01: INSPECTION AND COLD EXPANSION OF HOLES 12, 14, 260, 261, 262 AND 263 AT FRAME 40 BETWEEN STGR 37 AND 38) CRACK INDICATION WAS FOUND AT H260 LH. AS PER JC AND AIB SB, WHEN CRACK INDICATION REMAINS AFTER THE FIRST OVZ, AIB MUST BE CONTACTED FOR REPAIR INSTRUCTIONS. CORRECTIVE ACTION: ER/A HAS BEEN ISSUED TO PERFORM A REPAIR UNDER AIRBUS ASSESSMENT. ACCOMPLISHED ER/A 614173-14AD. (0144267)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 CRACK INDICATION FROM 14I HOLE LOCATED AT RH STRG 15A LEVEL AT UPPER FUSELAGE. CRACK DIRECTION IS 11 OCLOCK AND CRACK DEPTH IS 0.083 INCH. FOR AD MANDATED DOCUMENTS AN AMOC MAY BE REQUIRED. REFERENCE EM 5310-01461 AND AIRBUS SB A330-53-3273 REV 02. CORRECTIVE ACTION: ACCOMPLISHED REAMED HOLE 14I TO NEXT OVERSIZE LOCATE ON EXTERNAL SKIN AT RH STR15A LEVEL AT UPPER FUSELAGE AS PER A330 SRM51-44-11-801 AND AMDS 5310-01461-03 STEPS 37, 39 AND 40 (COLD WORKING, OK TO INSTALL, AND FASTENER INSTALLATION). MEASURE OFFINAL DIAMETER OPEN HOLE 14I IS: 0.214 IN. RE-INSPECTION ACCOMPLISHED ON HOLES 14I ONLY ALUMINUM LAYERS AS PER NTM 51-10-01 IN CONJUNCTION WITH AMDS 5310-01461-03. AND CRACK INDICATION WAS NOT FOUND. (0142989)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 CRACK INDICATION FROM 14F HOLE LOCATED AT RH STRG 15A LEVEL AT UPPER FUSELAGE. CRACK DIRECTION IS 9 OCLOCK AND CRACK DEPTH IS 0.078 INCH. COERRECTIVE ACTION: ACCOMPLISHED REAMED HOLE 14F TO NEXT OVERSIZE LOCATE ON EXTERNAL SKIN AT RH STR15A LEVEL AT UPPER FUSELAGE AS PER A330 SRM51-44-11-801 AND AMDS 5310-01461-03 STEPS 37, 39 AND 40 (COLD WORKING, OK TO INSTALL, AND FASTENER INSTALLATION). CRACK INDICATION WAS NOT FOUND. (0142985)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,378 hrs · 10,861 cycles

SHIP 3310 MISSING MID PASSENGER CREW DOOR 842 SLIDE SAFETY PIN AT RESERVOIR ASSY IN PASSENGER CABIN. CORRECTIVE ACTION: INSTALLED MID PASSENGER CREW DOOR 842 SLIDE SAFETY PIN AT RESERVOIR ASSY. (0079855)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 81,180 hrs · 10,711 cycles

SHIP 3310 DURING C-CHECK, ON NOVEMBER 8, 2022, THE FOLLOWING CORROSION FINDING WAS DISCOVERED ON NRC #684 AND IT SHOULD HAVE BEEN CLASSIFIED AS LEVEL 2 CORROSION. "CORROSION AT LEFT I/B SEAT TRACK LBL 47 BETWEEN FRAME 73A AND 74". CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK ASSY. (2947346)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,845 hrs · 10,670 cycles

WHITE EMER FLOOR PATH LIGHTS AT SEAT 51J & 57B INOP. REPLACED PIN IN CONNECTOR. OPS CK OK.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,767 hrs · 10,660 cycles

SHIP3310 EMERGENCY LIGHT INOP AT CEILING PANEL ABOVE ROW 22 LH SIDE. CORRECTIVE ACTION: FOUND EMERGENCY LIGHT CONNECTOR LOOSE, RESEATED. (2896487)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,905 hrs · 10,551 cycles

SHIP 3310 DURING WALK THROUGH FOUND 22H OVERHEAD EMERGENCY LIGHT INOP. CORRECTIVE ACTION: FOUND CEILING EMERGENCY LIGHT AT 22H HOOKED UP BACKWARDS. OPS CHECK OKAY. (4694089)

Part: WARMER — ODOR (GALLEY) · airframe 77,873 hrs · 10,294 cycles

BUN WARMER HAS A BURNING ELECTRICS ODOR WHEN IN USE LOC M2 404. R & R BUN WARMER IN MID GALLEY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,787 hrs · 10,284 cycles

EMERGENCY LIGHT ABOVE DOOR 3 LEFT INOPERATIVE. R & R THE LIGHT ASSY IAW MM 33-51.

Part: FLOOR SUPPORT — CORRODED (FRMS 74-75) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

SHIP 3310 CORROSION ON FLOOR SUPPORT BEAM AROUND SEVERAL FASTENER HOLES LOCATED AT LBL 30 BETWEEN FRAMES C74 AND C75. CORRECTIVE ACTION: REPAIRED AREA REF. ER/A 603869-14. (2511670)

Part: FLOOR SUPPORT — CORRODED (FRMS 74) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

SHIP 3310 CORROSION ON FLOOR SUPPORT BEAM AROUND FASTENER HOLES LOCATED AT RBL 44, AROUND 2EA FASTENERS HOLES, 4.5" AFT OF FRAME C74. CORRECTIVE ACTION: REPAIRED AREA ER/A 603943-14. (2511671)

Part: FLOOR SUPPORT — CORRODED (FRMS 74-75) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

SHIP 3310 CORROSION ON FLOOR SUPPORT BEAM AROUND FASTENER HOLES IN SEVERAL AREAS LOCATED AT RBL 30 BETWEEN FRAMES C74 AND C75. CORRECTIVE ACTION: REPAIRED AREA REF. ER/A 603869-14. (2511668)

Part: SEAT TRACK — CORRODED (FRM 73A) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

SHIP 3310 CORROSION AT RBL82, FRAME 73A,,AFT OF SPLICE SUPPORT (SMALL SEAT TRACK). CORRECTIVE ACTION: REMOVED AND REPLACED PER A330 SRM 51-72-11. (2510409)

Part: SUPPORT FRAME — CORRODED · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION AT FRAME 73A, O/B SUPPORT FRAME. CORRECTIVE ACTION: REPLACED PER A330 SRM 51-72-11. LP 2501871

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION RIGHT O/B SEAT TRACK RBL 64 BETWEEN FRAME 73A AND 74. CORRECTIVE ACTION: REPLACED PER A330 SRM 51-72-11. LP 2501872

Part: FRAME — CORRODED · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION FOUND AT C-78 AIRCRAFT CENTER. CORRECTIVE ACTION: REPLACED C-78 PER A330 SRM 51-72-11. LP 2498884

Part: FRAME — CORRODED (FRM 73A) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION AT FRAME 73A, RBL 82, FWD OF SPLICE SUPPORT FRAME. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 51-72-11. LP 2497429

Part: FRAME — CORRODED (FRM 73A) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION AT FRAME 73A, R/H, I/B SUPPORT FRAME. CORRECTIVE ACTION: REPLACED FRAME PER A330 SRM 51-72-11. LP 2496126

Part: FLOORBEAM — CORRODED (FRM 76 L/RBL 10) · corrosion level 3 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION AT NUT PLATE HOLES ON EACH SIDE OF SUPPORT STRUCTURE FOR AFT GALLEY CENTER FLOORBOARD. LOCATED AT FRAME C76, 14 INCHES OUTBOARD OF CENTER L/H AND R/H AND 10 INCHES FWD ON EACH SIDE OF FLOORBOARD. CORRECTIVE ACTION: REPLACED L/H AND R/H FLOORBOARD SUPPORT BEAMS FROM C75 TO C78 REF A330 SRM 51-41-15. LP 2495111

Part: SEAT TRACK — CORRODED (FRMS 73A-75) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION ON FLOORBOARD FASTENERS AT RBL 18 BETWEEN FRAME 73A AND 75. CORRECTIVE ACTION: REPLACED SEAT TRACK SECTION PER A330 SRM 51-72-11. LP 2496320

Part: FRAME — CORRODED (FRM 73A) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION AT FRAME 73A, RBL62. BETWEEN C73 AND C74 I/B TRACK. REPLACED FRAME PER A330 SRM 51-72-11. LP 2496351

Part: SEAT TRACK — CORRODED (FRMS 73-74 RBL48) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION RIGHT I/B SEAT TRACK RBL 48 BETWEEN FRAME 73A AND 74. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A330 SRM 51-72-11. LP 2494605

Part: SEAT TRACK — CORRODED (FRMS 73-75) · corrosion level 3 · airframe 77,742 hrs · 10,278 cycles

AIRCRAFT 3310, CORROSION ON FLOORBOARD FASTENERS LBL 18 BETWEEN FRAME 73A AND 75A. CORRECTIVE ACTION: REPLACED SEAT TRACK REF A330 SRM 53-00-15. LP 2494989

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

SHIP ROW 26 RIGHT SEAT TRACKS SHOW SIGNS OF CORRASION. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. REPAIRED PER A330 SRM 53-31-15-300-001. (2490701)

Part: SEAT TRACK — CORRODED (FRM 53) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

SHIP 3310 SEAT TRACK Y-1959 @ FR 53.2 FRETTING CORROSION VISIBLE AT SEAT ATTACHMENT AREA. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. REPAIRED PER A330 SRM 53-31-15-300-001 AND A330 SRM 51-42-11. (2490699)

Part: SEAT TRACK — CORRODED (FRM 53) · corrosion level 2 · airframe 77,742 hrs · 10,278 cycles

SHIP 3310 SEAT TRACK Y-2462 @ FR 53.5 FRETTING CORROSION FOUND IN TRACK LUG EXTENDING FORWARD UNDER LAV. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. REPAIRED PER A330 SRM 53-31-15-300-001. (2490698)

Part: RETAINER — DAMAGED (TE FLAPS SYS) · airframe 77,742 hrs · 10,278 cycles

DURING REMOVAL OF LT #3 LINK FOUND PLATE RETAINER (LOCKING KEY) DAMAGED. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. REPLACED PLATE RETAINER (LOCKING KEY) PER AMDS CARD 2754-4003. (2489395)

Part: BOLT — WORN (TE FLAP SYS) · airframe 77,742 hrs · 10,278 cycles

SHIP 3310 DURING REMOVAL OF LT #3 LINK FOUND LOWER HOLLOW BOLT WORN BEYOND LIMITS. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. REPLACED HOLLOW BOLT PER AMDS CARD 2754-4003. (2489396)

Part: NONE — NONE · airframe 77,676 hrs · 10,268 cycles

SHIP 3310 ROW 30,31AB EEPLS LIGHTS INOP. CORRECTIVE ACTION: WIRE BROKEN AT SEAT 31A NEAR SIDEWALL. REPLACED SOCKET AND REINSERTED INTO CONNECTOR. (9444216)

Part: NONE — NONE · airframe 77,258 hrs · 10,218 cycles

SHIP 3310 EMERGENCY LIGHTS INOP AT 40H SEAT, 23B SEAT, 41G CEILING, AND 3L CEILING. CORRECTIVE ACTION: RESEATED CONNECTORS AT LOCATIONS 40H, 41G CEILING AND 3L CEILING . REPLACED LAMP T 23B PER A330 AMM 33-51. (9114257)

Part: NONE — NONE · corrosion level 3 · airframe 77,112 hrs · 10,202 cycles

SHIP 3310 FOUND CANON PLUG 4132KS3-B ON #1 ENG T/R LOWER LEFT LOCKING ACTUATOR BURNED DAMAGE. CORECTIVE ACTION: INSTALLED NEW WIRE BUNDLE PER A330 AMM 20-27. (2401910)

Part: LIGHT — LOOSE · airframe 76,080 hrs · 10,079 cycles

SHIP 3310 EMERGENCY EXIT LIGHT BELOW 16C IS HANGING LOOSE, CORRECTIVE ACTION: REPAIRED EMERGENCY EXIT LIGHT AT 16C OPS CK NORMAL PER A330 AMM 33-52-01A MEL AND PLACARD REMOVED (9187730)

Part: CONNECTOR — PULLED · airframe 75,723 hrs · 10,038 cycles

SHIP 3310 EMER LIGHTS AT 30GH TO 24GH INOP. CORRECTIVE ACTION: FOUND POWER WIRE PULLED AT 30GH CONNECTOR RECONNECTED IAW A330 ESPM 20-43-11. AN GND NOT MAKING GOOD CONTACT FOR SEATS 31-34GH RESECURED GND. (6603571)

Part: NONE — NONE · airframe 75,604 hrs · 10,019 cycles

SHIP 3310 DURING SVC CHECK FOUND AISLE EMERGENCY LIGHT AT 15 JH INOP. CORRECTIVE ACTION: FOUND BROKEN WIRE AT CONNECTOR REPINNED CONNECTOR. (6603505)

Part: NONE — NONE · airframe 74,689 hrs · 9,895 cycles

SHIP 3310 AFT CARGO DOWER LOWER PANEL DAMAGED. CORRECTIVE ACTION: REMOVED DAMAGE BETWEEN FRAMES 62 +61A PER SRM A330 53-32. PERFORMED HFEC INSP OF CUTOUT PER SRM 52-32-00 NO DEFECTS NOTED. REPAIRED PER ERA 597679- 14. RII TASKS C/W. (8481126)

Part: NONE — NONE · airframe 74,529 hrs · 9,870 cycles

SHIP 3310 SEAT 25 JH EMERGY LIGHT INOP. CORRECTIVE ACTION: FOUND BAD SOCKET IN CONNECTOR AT SEAT 25JH. REPLACED SOCKET IAW A330 ESPM 20-44. (8742537)

Part: NONE — NONE · airframe 74,319 hrs · 9,830 cycles

SHIP 3310 EMERGENCY FLOOR LIGHTS AT SEAT 20 LEFT AND 25 RIGHT INOP. CORRECTIVE ACTION: FOUND WIRE PULLED OUT OF PLUGS. RETERMINATED WIRE AND REINSTALLED PLUGS. (7946830)

Part: NONE — NONE · airframe 74,188 hrs · 9,807 cycles

SHIP 3310 EMERGENCY EXIT SIGNS ILLUMINATED IN FLIGHT. TURNED ON AT INITIAL DECSENT AT 3L ONLY. NO OTHER EMER EXIT SIGNS ACTIVATED. CORRECTIVE ACTION: PERFORMED CIDS BITE A330 AMM 23-73. NO FAULTS. (8478280)

Part: NONE — NONE · airframe 73,001 hrs · 9,627 cycles

SHIP 3310 OXYGEN PANEL LOOSE LOCATION 901. CORRECTIVE ACTION: RESECURED SAME. MASKS DID NOT DROP. (1978618)

Part: NONE — NONE · airframe 72,766 hrs · 9,591 cycles

SHIP 3310 OXYGEN PANEL MASK DEPLOYED LOCATIONS 4L. CORRECTIVE ACTION: STOWED O2 MASKS. (1952444)

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 70,431 hrs · 9,217 cycles

SHIP 3310 AISLE EMERGENCY LIGHT LENS COVER BROKEN AFT OF 2R DOOR. CORRECTIVE ACTION: R&R AISLE EMERGENCY LIGHT ASSY IAW A330 AMM 33-52. (7687256)

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 70,223 hrs · 9,159 cycles

SHIP 3310 OXYGEN PANEL MASK DEPLOYED / LOCATIONS:206. CORRECTIVE ACTION: STOWED MASKS IAW A330 AMM 35-21. (1726960)

Part: OXYGEN MASK — UNWANTED DEPLOY (CABIN) · airframe 70,223 hrs · 9,159 cycles

SHIP 3310 OXYGEN PANEL MASK DEPLOYED / LOCATIONS:204. CORRECTIVE ACTION: STOWED MASKS IAW A330 AMM 35-21. (1726958)

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 70,129 hrs · 9,145 cycles

SHIP 3310 21HJ ESCAPE PATH LIGHT INOPERATIVE. CORRECTIVE ACTION: RECONNECTED ESCAPE PATH LIGHT. OPS CHKS OK.

Part: SEAT TRACK — CORRODED (AFT GALLEY) · airframe 69,965 hrs · 9,114 cycles

CORROSION SEAT TRACK YC1 LOCATED AT LEVEL FR 73 TO FR 74 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK AND FASTENERS AT AFT GALLEY AREA, AS PER SRM A330 51-72-11-911-001 AND DWG.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 69,906 hrs · 9,106 cycles

DIV/FIRE TO KEF DUE TO COMPRESSOR STALLS FROM THE NBR 1 ENGINE AND ASSOCIATED HIGH ENGINE VIBES. FLAMES EXITING ENGINE EXHAUST. ENGINE WAS NOT SHUT DOWN. CORRECTIVE ACTION: REMOVED AND REPLACED NBR 1 ENGINE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,942 hrs · 8,819 cycles

SUPPLEMENT: EMERGENCY FLOOR PATH LIGHT AT SEATS ROWS 31, 33, AND 35AB POSITIONS INOPERATIVE. DEFERRED PER MEL 33-51-01B-JFK REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEAT 23AB, 31AB, 33AB, AND 35AB. LP 6450669

Part: TAIL CONE — MISSING (FLAP TRACK) · airframe 67,367 hrs · 8,745 cycles

DURING WALK AROUND, FOUND LEFT WING NBR 2 FLAP TRACK FAIRING TAIL CONE MISSING. DEFERRED PER CDL 57-00-04B UNTIL FAIRING TAIL CONE CAN BE PLACED. LP 6573291

Part: BOLT — MISSING (NR 2 ENGINE) · airframe 60,870 hrs · 7,950 cycles

DURING PHASE 1 INSPECTION FOUND 3 BOLTS MISSING AT NR 2 ENGINE ON THE FAN CASE. INSTALLED 3 NEW BOLTS AND SPACERS AT POSITIONS 12, 94, AND 51. LP 4673491

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 56,553 hrs · 7,395 cycles

EMERGENCY EXIT SIGN COVER LOOSE. SECURED EXIT SIGN LENS.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 56,553 hrs · 7,395 cycles

L4 DOOR EMERGENCY EXIT SIGN INOPERATIVE. REPAIRED A BROKEN WIRE.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 56,212 hrs · 7,352 cycles

EMERGENCY ESCAPE PATH LIGHTING INOP AT SEAT 23B, 31B, 33B, AND 21J. RESEATED CONNECTOR AT 4 SEAT LOCATIONS.

Part: SWITCH — FAULTY (COCKPIT) · airframe 55,206 hrs · 7,228 cycles

EMERGENCY LIGHTS STAY ON IN ARM POSITION. REPLACED EMERGENCY LIGHT COCKPIT SWITCH.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 55,114 hrs · 7,217 cycles

EMERGENCY LIGHTS INOPERATIVE AT SEATS 14AB AND 15AB. TERMINATED A WIRE AT SEAT 14AB.

Part: LIGHT — DAMAGED (CABIN) · airframe 54,893 hrs · 7,190 cycles

AFT GALLEY A1 LEFT EMERGENCY LIGHT ASSEMBLY DAMAGED. REPLACED LIGHT ASSEMBLY.

Part: SKIN — DENTED (CARGO DOOR) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, AFT CARGO DOOR INNER LOWER SKIN FOUND DENTED. REMOVED DAMAGED AREA, AND INSTALLED REPAIR FILLER AND DOUBLER PER ER/A 550537-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, SEAT TRACK IN MID CABIN FR 33, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53276407 AND F53276401.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, SEAT TRACK IN MID CABIN FR37.1, Y945 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-42-11 AND DRAWING F73278802 AND F53278800.

Part: FLAP TRACK — CORRODED (LT WING TE FLAP) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, FOUND LEFT WING NR 3 FLAP TRACK CORRODED. REPLACED FLAP TRACK.

Part: DOOR — DAMAGED (CABIN) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, DOOR 4L AFT LOWER CORNER DENTED. REMOVED DAMAGED AND INSTALLED REPAIR DOUBLER AND FILLER.

Part: FLAP TRACK — CORRODED (RT WING TE FLAP) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, RIGHT WING NR 3 FLAP TRACK FOUND CORRODED. REPLACED THE FLAP TRACK.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, THERE IS AN ABRASION LOCATE ON AFTER CARGO DOOR INNER SKIN. REMOVED THE DAMAGE AREA, INSPECTED, AND INSTALLED REPAIR FILLER AND DOUBLERS PER ER/A 550537-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, SEAT TRACK IN MID CABIN FR 33, Y1959 FOUND CORRODED. REPLACED SEAT TRACK FOR SRM 51-42-11 AND DRAWING F53276407 AND F53276401.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, THE SEAT TRACK AT MID CABIN FRAME 33, Y945 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-42-11, AND DRAWINGS F53276502 AND F53276401.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, THE SEAT TRACK AT MID CABIN FRAMES 73-74 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWINGS F53478009 AND F53478209.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, THE SEAT TRACK AT MID CABIN FRAME 73-74 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWINGS F53478009 AND F53478209.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, THE SEAT TRACK AT MID CABIN FRAMES 73-74, -WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWINGS F53478009 AND F53478209.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, THE SEAT TRACK AT MID CABIN FRAME 37, Y2462 WAS FOUND CORRODED. REPLACED SEAT TRACK IAW SRM 51-42-11 AND DRAWINGS F53276408 AND F53276401.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, THE SEAT TRACK AT MID CABIN FRAME 37, -Y2462 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWING F53276408S AND F53276401.

Part: SEAT TRACK — CORRODED (FRAME 74) · airframe 52,884 hrs · 6,923 cycles

DURING CHECK, SEAT TRACK FOUND CORRODED AT FRAME 74, Y450. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWING F53478650 AND F53478040.

Part: SEAT TRACK — CORRODED (FRAMES 33-34) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, SEAT TRACK FOUND CORRODED AT FRAMES 33 - 34, -YC1. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWING F53478007 AND F5347040.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, SEAT TRACK FOUND CORRODED AT FRAMES 73 - 74, YA. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWING F53478239 AND F53478040.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, SEAT TRACK FOUND CORRODED AT FRAME 33, Y1552.5. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWING F53275638.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 52,884 hrs · 6,923 cycles

DURING CHECK, SEAT TRACK FOUND CORRODED AT FRAME 33, -Y1552.5. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWING F53275639 AND 53275677.

Part: SEAT TRACK — CORRODED (FRAME 73) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, SEAT TRACK FOUND CORRODED AT FRAME 73, -Y450. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWING F53478650.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 52,884 hrs · 6,923 cycles

DURING M CHECK, SEAT TRACK FOUND CORRODED AT FRAME 33, YC1. REPLACED THE SEAT TRACK IAW SRM 51-42-11 AND DRAWING F53478007.

Part: EXCITER — FAILED (APU) · airframe 51,561 hrs · 6,749 cycles

FAILED APU COLD SOAK START, APU STARTED ON THE FIRST ATTEMPT, BUT DID AN AUTO SHUTDOWN, APU WOULD NOT LIGHT OFF ON ALL 3 ATTEMPTS. REPLACED THE IGNITION EXCITER.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 51,007 hrs · 6,678 cycles

DURING A CHECK, MAINTENANCE FOUND BATTERY CAPACITY TEST FAILED AT THE R3 & 4 DOORS. REPLACED THE BATTERIES.

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 48,356 hrs · 6,332 cycles

DURING SERVICE CHECK, FOUND EPSU, 13WL, DOOR 2 FAULTED. REPLACED DOOR 2 EPSU, 13WL.

Part: FAIRING — CRACKED (WING TO BODY) · airframe 43,731 hrs · 5,753 cycles

FOUND CRACK ON FWD WING TO BODY FAIRING PANEL 191AB. REPAIR PERFORMED IAW SRM.

Part: FAIRING — CRACKED · airframe 43,731 hrs · 5,753 cycles

FOUND CRACK ON FAIRING PANEL 191DB. BODY FAIRING PANEL DB REPAIRED IAW SRM.

Part: SEAT TRACK — CORRODED (FRAME 53) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK Y1959 FRAME 53.3 AND 53 .7 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. EXCEEDS LIMITS IAW SRM 53-31-15, FIG 101, SHEET 2. SEAT TRAC R & R WITH NEW IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 62) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK -Y953, FRAME 62 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 101, SHEET 2. SEAT TRACK R & R IAW SRM 51-42 -11.

Part: SEAT TRACK — CORRODED (FRAMES 31-35) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK Y1456, FRAMES 31-35 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101 (SHEET 2). R & R SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 52-53) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK -Y1959, FRAMES 52, & 53 CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDS LIMITS IAW SRM 53-31-15, FIG 101, SHEET 8. SEAT TRACK R & R WITH NEW IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 33) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK -Y953, FRAME 33 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15 FIG101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 62-67) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK -Y450 FRAMES 62 - 67 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 101, SHEET 2. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 33-36) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK -Y1456, FRAMES 33, 35, & 36 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101 (SHEET 2). R & R SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 49-52) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK Y450 FRAMES 49, 50, & 52 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEEDS LIMITS IAW SRM 53-31-15, FIG 101, SHEET 8. SEAT TRACK R & R WITH NEW IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 26) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK, Y1959, FRAME 26 AND 26.1 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00.

Part: SEAT TRACK — CORRODED (FRAME 40) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK Y450, FRAME 40.2-.3 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101 (SHEET 8). SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 37) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK Y450, FRAME 37.1 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101 (SHEET 2). SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 53-56) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK -Y2462, FRAMES 53.9, 54, & 56 HAS MINOR CORROSION. CORROSION REMOVED IAW SRM 51-74-00. FOUND WITHIN LIMITS IAW SRM 53-31-15, FIG 101.

Part: SEAT TRACK — CORRODED (FRAMES 60-61) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK -Y2462, FRAMES 60 - 61 FOUND MINOR CORROSION. FOUND WITHIN LIMITS IAW SRM 53-00-15, FIG 101.

Part: SEAT TRACK — CORRODED (FRAMES 49-52) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK -Y450 FRAMES 49, 50 AND 52 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101 (SHEET 8). R & R SEAT TRACK.

Part: SEAT TRACK — CORRODED (FRAMES 66-67) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK AT 450, FRAMES 66 AND 67, FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 101, SHEET2, SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 39) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK, Y450, FRAME 39 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 40) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK -Y450, FRAME 40.2-.3 AND FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101 (SHEET 8). R & R SEAT TRACK IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 61) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK Y1959, FRAME 61 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53- 00-15, FIG 101, SHEET 2. SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · airframe 38,881 hrs · 5,145 cycles

SEAT TRACK Y1959, FRAMES 47, 50, 52 AND 53, FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101(SHEET 8). R & R SEAT TRACK IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FRAME 73) · airframe 38,881 hrs · 5,145 cycles

FLOORBEAM AT FRAME 73 BETWEEN YA AND YB1 CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-14, FIG 101. FLOORBEAM R & R IAW SRM 51-42-11.

Part: SKIN — DENTED (NR 4 SLAT) · airframe 35,853 hrs · 4,768 cycles

RT WING L/E NR 4 SLAT UPPER SURFACE FOUND WITH DENTED. FOUND EXCEED LIMIT IAW SRM 57-40-00, FIG 102. REPAIR CARRIED OUT IAW SRM 57-40-0 0, FIG 203.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK, Y-2462, FR37 CORRODED. CORRODED AT ZN 250 SEAT TRACK Y-2462, FR37. REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMIT. ORG THK 0.180", MAT'L REMOVED 0.042" (L=2"XW=0.5") IAW SRM 53-00-15, FIG 102. REPAIR CARRIED OUT IAW PRI 490911-14, REV O. COMPARED WITH ER/A 490911-14 REV O. FOUND IN COMPLIANCE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y2462 FR 37 CORRODED. CORR AT ZN 250 SEAT TRACK Y2462, FR 37. REMOVED IAW SRM 51-74-00 FOUND OUT LIMIT. ORG THK 0.120" MAT'L REMOVED 0.041 (L=2"XW=0.5") IAW SRM 53-00-15 FIG 102. REPAIR CARRIED OUT IAW PRI ER/A 490911-14 REV O DATED 21APR11 1701 HRS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y2462 FR 57.4-58 CORRODED. CORROSION REMOVED IAW SRM 51-74-00. ORG THK: 0.180", THK REMOVED: 0.042" (L=1"XW=0.5") FOUND EXCEED LIMITS IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK R & R IAW PRI 490898-14, REV 0. PRI 490898-14 REV 0 COMPARED WITH ER/A 490898-14, REV 0. FOUND IN COMPLIANCE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y1959, FR 57.1-57.2, FR 57.4-58 CORRODED. CORROSION REMOVED IAW SRM 51-74-00. ORG THK: 0.180", THK REMOVED AT FR57.1-57.2: 0.039", L=1"XW=0.5" AND FR 57.4-58: 0.041", L=1"XW=0. 5". FOUND EXCEED LIMITS IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK R & R IAW PRI 490898-14, REV 0. PRI 490898-14, REV 0 COMPARED WITH ER/A 490898-14, REV 0. FOUND IN COMPLIANCE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y2462 FR59-60 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMITS. ORG THK 0.180", MAT'L REMOVED AT FR59: 0.041" (L=1"XW=0.5") AND FR60: 0.040"(L=1"XW=0.5") AS PER SRM 53-00-15 FIG 102. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-450 FR53.4-53.5 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 (EMMA) AND FOUND OUT OF LIMIT. ORG THK: 0.180", MAT'L REMOVED 0.044" (L=2"XW=0.5") AS PER SRM 53-00-15 FIG 102. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-2462 FR41, FR41-42, FR42-43 CORRODED. CORROSION REMOVED PER SRM 51-74-00. ORIGINAL THK 0.180", FR41 MATERIAL REMOVED 0.039" (L-2"XW-0.5"), FR41-FR42 MATERIAL REMOVED 0.042" (L-1.5"XW-1.5"), FR42-43 MATERIAL REMOVED 0.044" (L-1"XW-0.5") FOUND OUT OF LIMIT PER SRM 53-31-15. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1959 FR 48-49, FR 50, FR 53.1 CORRODED. CORROSION REMOVED AS PER SRM 51-74-00 AND FOUND EXCEED LIMITS. ORG THK 0.18 0", THK REMOVED AT FR48-49: 0.038" (L=1.5"XW=0.5"), FR 50: 0.041 (L=1"XW=0.5") AND FR53.1: 0.040" (L=1"XW=0.5") AS PER SRM 53-31-15 FIG 101. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1959 FR37.1-37.2, FR37.3 CORRODED. CORROSION REMOVED AS PER SRM 51-74-00 AND FOUND EXCEED LIMITS. ORG THK: 0.180", THK REMOVED AT FR37.1-37.2: 0.040" (L=1"XW=0.5") AND FR37.3: 0.042" (L=1"XW=0.5") AS PER SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1959 FR29, FR33 CORRODED. CORROSION REMOVED AS PER SRM 51-74-00. FR29 MATERIAL REMOVED 0.042" (L-1"XW-0.5"), FR33 MATERIAL REMOVED 0.040" (L=1"XW-0.5"). ORG THK 0.180" FOUND OUT OF LIMIT PER SRM 53-00-15 FIG 102. DAMAGED SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y2462 FR 38, FR 39 CORRODED. CORROSION REMOVED PER SRM 51-74-00. ORIGINAL THK 0.180", FR 38 MATERIAL REMOVED: 0.043" (L-1"XW-0.5"), FR 39 MATERIAL REMOVED: 0.039"(L-1"XW-0.5") FOUND OUT OF LIMIT PER SRM 53-31-15 FIG 101. DAMAGED SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y1959 FR33, FR36, FR37 CORRODED. CORROSION REMOVED PER SRM 51-74-00. FR33 MATERIAL REMOVED 0.040" (L-1"XW-0.5"), FR36 MATERIAL REMOVED 0.041" (L-0.5"XW-0.5"), FR37 MATERIAL REMOVED 0.040" (L-1"XW-0.5"). ORG THK 0.180" FOUND OUT LIMITS PER SRM 53-00-15 FIG 1 02. DAMAGED SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1552 FR33 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 AND FOUND OUT OF LIMITS. ORG THK 0.180". MAT'L REMOVED 0.043" (L=1"XW=0.5") AS PER SRM 53-00-15 FIG 102. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y1959 FR 48-49, FR 53, FR 53.1-53.2 CORRODED. CORROSION REMOVED PER SRM 51-74-00. ORIGINAL THK 0.180", FR 48-49 MATERIAL REMOVED 0.042" (L-1"XW-0.5"), FR 53 0.044" (L-0.5"XW-0.5"), FR 53.1-53.2 MATERIAL REMOVED 0.040" (L-1"XW-0.5") FOUND OUT OF LIMIT PER SRM 53-31-15 FIG 101. DAMAGED SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1959 FR58-59, FR59-60, FR61 CORRODED. CORROSIONREMOVED AS PER SRM 51-74-00 AND FOUND EXCEED LIMIT. ORG THK: 0.180", THK REMOVED AT FR58-59: 0.039" (L=1"XW=0.75"), 0.042" (L=1.5"XW=0.5") AND FR61: 0.040" (L=1"XW=0.5") AS PER SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-2462 FR53.9 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 (EMMA) AND FOUND OUT OF LIMIT. ORG THK 0.180", MAT'L RE MOVED 0.042" (L=1"XW=0.5") AS PER SRM 53-00-15 FIG 102 (EMMA). DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1959 FR40.2, FR45-46, FR46-47 CORRODED. CORROSION BLENDED OUT FOUND OUT LIMITS PER SRM 53-31-15 FIG 101 (L=0.5"XW=0.5") D=0.040" AT FR45-46, AND (L=1"XW=0.5") D=0.045" AT FR40.2 AND D=0.041" AT FR46-47 AND SEAT TRACK REPLACEMENT CARRIED OUT AS PER SRM 51-42-11 AND SRM 51-49-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-2462 FR37.2-37.3 CORRODED. CORROSION REMOVED PER SRM 51-74-00. ORIGINAL THK 0.180" FR37.2-37.3 MATERIAL REMOVED 0.043" (L-1"XW-0.5") FOUND OUT OF LIMITS PER SRM 53-00-15 FIG 102. DAMAGED SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-2462 FR58-59, FR61 CORRODED. REMOVED CORROSION AS PER SRM 51-74-00 (EMMA) AND FOUND OUT OF LIMIT. ORG THK 0.180", MAT'L REMOVED AT FR58-59: 0.040" "XW=0.5"), FR61: 0.039" (L=1"XW=0.75") AS PER SRM 53-00-15 FIG 102. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-2462 FR 47-48, FR 50-51, FR 53.1 CORRODED. CORROSION REMOVED PER SRM 51-74-00. ORIGINAL THK 0.180", FR 47-48 MATERIAL REMOVED 0.042" (L-1" XW-0.5"), FR 50-51 MATERIAL REMOVED 0.039" (L-1.5"XW-0.5"), FR 53. 1, MATERIAL REMOVED 0.040" (L-1"XW-0.5") FOUND OUT OF LIMITS PER SRM 53-31-15 FIG 101. DAMAGED SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y2462 FR37-37.1 CORRODED. CORROSION REMOVED AS PER SRM 51-74-00. ORG THK: 0.180", THK REMOVED: 0.042" (L=1"XW=0.5") FOUND EXCEED LIMITS AS PER SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y1959 FR59-60, FR60-61 CORRODED. CORROSION REMOVED AS PER SRM 51-74-00 (EMMA) AND FOUND EXCEED LIMIT.ORG THK: 0.180", THK REMOVED AT FR59-60: 0.040" L=1.5"XW=0.5" AND FR60-61: 0. 043" (L=1"XW=0.5") AS PER SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y1959 FR37.1, FR37.2, FR37.3 CORRODED. CORROSION REMOVED PER SRM 51-74-00. ORIGINAL THK 0.180", FR37.1 MATERIAL REMOVED 0.042" (L-1"XW-0.5"), FR37.2 MATERIAL REMOVED 0.039" (L-0.5"XW-0.5"), FR37.3 MATERIAL REMOVED 0.043" (L-1"XW-0.5") FOUND OUT OF LIMITS PER SRM 53-00-15 FIG102. DAMAGED SEAT TRACK REMOVED AND REPLACED PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1959, FR53.9 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 FOUND OUT OF LIMITS. ORG THK 0.180", MATERIAL REMOVED 0.042" (L=1"XW=0.5") IAW SRM 53-31-15 FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK, Y1959 FR41-42, FR44-45 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK FR41-42: 0.043" (L=1"XW=0.5") AND FR44-45: 0.039" (L=1"XW=0.5") IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

LONGITUDINAL SUPPORT BETWEEN HEATED PANELS 271KF AND 27 1JF CORRODED. REMOVED CORROSION IAW SRM 51-74-00. MATERIAL REMOVED 0.100" (L=2"XW=1"). ORG THK 0.165" FOUND OUT OF LIMIT IAW SRM 53-41-14, FIG 101. DAMAGED SUPPORT R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

LONGITUDINAL SUPPORT Y450 FR76-77 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.080", MATL REMOVED 0.040" (L=2.5"XW=1") IAW SRM 53-41-14, FIG 103. DAMAGED SUPPORT R & R IAW SRM 51-42-11, COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-2462, FR55-56, FR56-57, FR57.1-57.2 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.180", MATERIAL REMOVED AT FR55-56: 0.040" (L=1"XW=0.5"), FR56-57: 0.042" (L=1"XW=0.5") AND FR57.1-57.2: 0.039" (L=0.5"XW=0.5") IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11, COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y2462 FR40.3, FR41, FR42-43 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.180", MATERIAL REMOVED AT FR40.3: 0.041" (L=1.5"XW=0.5"), FR41: 0.040" (L=1"XW=0.5") AND FR42-43: 0.043" (L=1.25"XW=0.5") IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK, Y2462, FR49-50, FR53.1 CORRODED. REMOVED CORROSIONAS IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.180", MATERIAL REMOVED AT FR49-50: 0.040" (L=1.5"XW=0.5") AND FR53.1:0.042" (L=1"XW=0.5") IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y1456, FR16-16A CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.080", MATERIAL REMOVED 0.020" (L=2"XW=1") IAW SRM 53-11-15, FIG 101. REPAIR CARRIED OUT IAW ER/A 483291-14MA, REV O. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1959 FR64, FR68, FR70 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.1 80", MAT'L REMOVED AT FR64: 0.040" (L=1"XW=0.5"), FR68: 0.042" (L=1"XW=0.5") AND FR70: 0.040" (L=1"XW=0.5") ASPER SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

LONGITUDINAL SUPPORT Y-450, FR76-77 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.080", MATERIAL REMOVED 0.039" (L=2"XW=1") IAW SRM 53-44-14, FIG 103. DAMAGED LONGITUDINAL SUPPORT R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y450 FR61, FR63, FR67 CORRODED. REMOVED CORROSION IAW SRM 51-74-00. FR61 MATERIAL REMOVED: 0.043", L=1", W=0.5". FR63 MATERIAL REMOVED: 0.043", L=1", W=0.5". FR67 MATERIAL REMOVED: 0.045", L=1", W=0.5". ORG THK: 0.180" FOUND EXCEED LIMIT IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y2462 FR65-66 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.180", MAT'L REMOVED AT FR65-66: 0.041" (L=1"XW=0.5") IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y450 FR53.4-53.5 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.180", MAT'L REMOVED: 0.041" (L=1"XW=0.5") IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-450 AT FR70, FR71 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.180", AT FR70 MAT'L REMOVED 0.043" (L=1"XW=0.5") AND FR71 MAT'L REMOVED 0.046" (L=1"XW=0.5") IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y450 FR38 CORRODED REMOVED CORROSION IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.180", MATERIAL REMOVED 0.044" (L=1"XW=0.5") IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-74-00, FR37.1. FOUND OUT OF LIMIT IAW SRM 53-00-15, FIG 102. DAMAGED SEAT-TRACK, R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-450, FR34, FR36-37 CORRODED. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED..

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y450 AT FR73 CORRODED. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK, R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y450, FR41, FR44, FR47 CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMIT IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK CORRODED. CORROSION. REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y450 FR49, FR51, FR53 CORRODED. REMOVED CORROSION IAW SRM 51-74-00 FR49 MATERIAL. REMOVED: 0.043",L=1", W=0.5". FR51 MATERIAL. REMOVED: 0.046", L=1", W=0.5". FR53 MATERIAL REMOVED: 0.041", L=1", W=0.5". ORIGINAL THK 0.180" FOUND EXCEED LIMITS IAW SRM 53-31-15 (FIG 101). SEAT TRACK R & R IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK, R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK CORRODED. CORROSION REMOVED IAW SRM 51-74-0 0 AND FOUND OUT OF LIMITS IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK, R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y-450 FR49, FR51, FR53 CORRODED. CORROSION AT ZN 250 SEAT TRACK Y-450 REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.180", MAT'L REMOVED AT FR49: 0.045" (L=2"XW=0.5"), FR51: 0.040" (L=1"XW=0.5") AND FR53: 0.042" (L=1"XW=0.5") IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y1959 FR65, FR67, FR70 CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND OUT OF LIMIT IAW SRM 53-00-15, FIG 102. DAMAGED SEAT TRACK. R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y-450 FR41, FR44, FR47 CORRODED. CORROSION REMOVED IAW SRM 51-74-00 AND FOUND OUT OF LIMITS IAW SRM 53-31-15, FIG 101. DAMAGED SEAT TRACK, R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y1552, FR33 CORRODED. CORROSION REMOVED IAW SRM 51-74-00 AND 53-00-15 FIG 102. DAMAGED SEAT TRACK, R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1959, FR18, FR22 CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FOUND EXCEED LIMITS IAW SRM 53-00-15, FIG 102. SEAT TRACK R & R AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-450 FR37.1, FR37.4 CORRODED. REMOVED CORROSION IAW SRM51-74-00, FR37.1 MATERIAL REMOVED: 0.040",L=1", W=0.5". FR37.4 MATERIAL REMOVED: 0.039", L=1", W=0.5".ORIGINAL THK: 0.1 80" FOUND EXCEED LIMITS IAW SRM 53-00-15 (FIG 102). SEAT TRACK R & R IAW SRM 51-42-11 COMPLETED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y-1959 FR56, FR57, FR58 CORRODED. CORROSION AT ZN260 SEAT TRACK Y-1959 REMOVED AS PER SRM 51-74-0 0 AND FOUND OUT OF LIMIT. ORG THK 0.180", MAT'L REMOVED AT FR56 MAT'L REMOVED: 0.040" (L=1"XW=0.5"), FR57 MAT'L REMOVED 0.042" (L=1.5"XW=0.5") AND FR58 MAT'L REMOVED 0.043" (L=1"XW=0.75") AS PER SRM 53-00-15 FIG 102. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK -YB1 FR74 CORRODED. CORROSION AT ZN 270 SEAT TRACK -YB1 REMOVED AS PER SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.180" MAT'L REMOVED AT FR74 0.042" (L=1"XW=0.5") AS PER SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y-450 FR61, FR63, FR67 CORRODED. CORROSION AT ZN 260 - SEAT TRACK Y-450 FR61, FR63, FR57 REMOVED AS PER SRM 51-74-00. FR61 MATERIAL REMOVED: 0.044", L=1", W=0.5". FR63 MATERIAL REMOVED: 0.044", L=1", W=0.5". FR67 MATERIAL REMOVED: 0.045", L=1", W=0.5". ORG THK: 0.180" FOUND EXCEED LIMITS AS PER SRM 53-00-15 FIG 102. SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y953 FR16-16A CORRODED. CORROSION AT ZN 220 SEAT TRACK Y953 FR16-16A REMOVED AS PER SRM 51-74-00 AND FOUND OUT OF LIMIT. ORG THK 0.071" MAT'L REMOVED 0.042" (L=2"XW=1") AS PER SRM 53-11-15 FIG 101. REPAIR CARRIED OUT AS PER ER/A 483241-14MA REV O.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK Y450 AT FR70, FR71 CORRODED. CORROSION AT ZN 260 SEAT TRACK Y450 FR70, FR71 REMOVED AS PER SRM 51-74-00 FOUND OUT OF LIMIT. ORG THK 0.120", FR70 MATL REMOVED 0.047" (L=1"XW=0.5") AND FR71 MAT'L REMOVED 0.040" (L=1 "XW=0.5") AS PER SRM 53-00-15 FIG 102. DAMAGED SEAT TRACK REMOVED AND REPLACED AS PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y-450 FR53.9 CORRODED. CORROSION AT SEAT TRACK AT Y-450, FR53.9 REMOVED IAW SRM 51-74-00. FR 53.9 MATERIAL REMOVED: 0.042", L=2", W=0.5". ORIGINAL THK: 0.120" FOUND EXCEED LIMITS IAW SRM 53-31-15 (FIG 101). SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y450 FR53.9 CORRODED. CORROSION AT SEAT TRACK AT Y450, FR53.9 REMOVED IAW SRM 51-74-00 FR53.9, MATERIAL REMOVED: 0.040", L=2", W=0.5". ORIGINAL THK: 0.120" FOUND EXCEED LIMITS IAW SRM 53-00-15 (FIG 102). SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

SEAT TRACK AT Y450 FR55, FR57.1, FR57.3 CORRODED. CORROSION REMOVED IAW SRM 51-74-00. FR55, MATERIAL REMOVED: 0.039",L=1", W=0. 5". FR57.1, MATERIAL REMOVED: 0.047", L=2", W=0.5". FR 57.3, MATERIAL REMOVED: 0.040", L=2", W=0.5" FOUND EXCEED LIMITS IAW SRM 53-00-15 (FIG 102). SEAT TRACK R & R IAW SRM 51-42-11. COMPLETED AND INSPECTED.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

LT Z-PROFILE AT FR80 CRACKED. DAMAGED Z-PROFILE AT ZN 270, FR 80 LT. R & R IAW SRM COMPLETED AND INSPECTED. ASSOCIATED AA 5322-01022 ADDED FOR AC 3310.

Part: PROFILE — CRACKED (FUSELAGE) · airframe 26,938 hrs · 3,593 cycles

RT Z-PROFILE AT FR80, CRACKED, DAMAGED Z-PROFILE AT ZN 270, FR80 RT R & R IAW IAW SRM 51-42-11. COMPLETED AND INSPECTED. ASSOCIATED AA 5322-01022 ADDED FOR AC 3310.

Part: SLIDE — FAULTED (1L DOOR) · airframe 26,721 hrs · 3,565 cycles

DURING EMERGENCY LIGHT TEST, SLIDE DOOR 1 LEFT SHOWED LOAD FAULT. REPLACED SLIDE 1L AND CHECKED OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,688 hrs · 3,048 cycles

DOOR 3 FAILED SYSTEM CHECK, REPLACED BATTERY AND TESTS OK.

Part: SLIDE — FAULTY (CABIN) · airframe 20,987 hrs · 2,818 cycles

DURING TEST OF THE EMERGENCY LIGHT SYSTEM THE ESCAPE SLIDE EPSU (18WL) DOOR NR 4 RIGHT FAULTED. REMOVED AND REPLACED ESCAPE SLIDE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)

DURING SCHEDULED SLIDE DEPLOYMENT, THE SLIDE EMERGENCY LIGHTS DID NOT ILLUMINATE. WRUNG OUT WIRING AND REPLACED EMERGENCY POWER SUPPLY UNIT (EPSU) 16WL. (K)

Part: GROUND WIRE — BROKEN (EMERGENCY LIGHTS)

EPSU (71WL) FAULTS TEST, FOUND BROKEN GROUND WIRE AND REPAIRED AND REPLACED EPSU AND TESTS, OK. (K)