N505JB

Part: WARNING LIGHT — ILLUMINATED (NLG) · airframe 85,006 hrs · 32,086 cycles

FLT#1247, LGA-TPA. 'UPON GEAR RETRACTION, THE NOSE GEAR SHOWED UNLK AND THE ECAM SHOWED L/G DOORS AND L/G UNLK MESSAGES. GEAR RECYCLED, CLEARED FAULTS.' (SUPPLEMENTAL INFORMATION TO FOLLOW)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 82,868 hrs · 31,142 cycles

FLT#1812, RSW-EWR. (AIRCRAFT DIVERTED TO MCO) 'CLIMBING OUT OF RSW, GOT A "CABPR SYS 1 FAULT, WHILE DOING QRC, GOT A SECOND "CAB PR 1&2 FAULT. FOLLOWED THE ECAM ACTIONS; PERFORMED PRESSURE CONTROL AND MONITORING TESTS, OPS CHECK VIA MCDU, OPS TEST OF MANUAL SELECT, MANUAL PRESSURE CONTROL+ FUNCTIONAL TEST OF MANUAL MODE CABIN ALTITUDE/OUTFLOW VALVE POSITION INDICATION + OUTFLOW CLOSING IN DITCHING CONFIG. ALL OPS TESTS PASSED NO HARD FAULTS. NO PREVIOUS HISTORY ON OUTFLOW VALVE PER AMM 21-31-00.'

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 81,139 hrs · 30,524 cycles

FLT#391, BOS-TPA. EMERG LIGHT BATTERY FIN 12WL FAILED TEST. REMOVED AND REPLACED THE BATTERY 12WL IAW AMM 33-51-38.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 81,139 hrs · 30,524 cycles

FLT#391, BOS-TPA. 'EMERG LIGHT BATTERY FIN10WL FAILED TEST; REMOVED AND REPLACED EMERG LIGHT BATTERY 10WL IAW AMM 33-51-38.'

Part: LIGHT — INOPERATIVE (CABIN) · airframe 80,908 hrs · 30,434 cycles

FLT#1952, MCO-BOS. 'FLOOR PROX EMERGENCY LIGHTS AT ROWS 3, 7, 15, 19, 23, 25 ABC INOPERATIVE. REMOVED AND REPLACED EPSU 11WL REF AMM 33-51-38. MDDR CLEARED. MX-4 UPDATED. PLACARD REMOVED. '

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION UPPER SURFACE OF UPPER SKIN OF THE CENTER WING BOX AT LEVEL+Y1292 AND FR 41 PLUS11 INCHES IN PASSENGER CABIN; ACCOMPLISHES REPAIR ON CENTER WING BOX UPPER SKIN PANEL IAW EC A21-1360-01. WORK ACCOMPLISHED ON AEROMAN NR 2021-491817 (CLASSIFIED A MAJOR REPAIR)

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 52 PLUS 13.375 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492033 (CLASSIFIED A MAJOR REPAIR)

Part: FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 1 ) AND -Y254 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491720 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC STAMP 238.

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 54 PLUS 5 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492034(CLASSIFIED A MAJOR REPAIR)

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION UPPER SURFACE OF UPPER SKIN OF THE CENTER WING BOX AT LEVEL+Y1292 AND FR 41 PLUS 20 INCHES IN PASSENGER CABIN; ACCOMPLISHED REPAIR ON CENTER WING BOX UPPER SKIN PANEL AT+Y1292 BETWEEN STIFFENER 16 AND 17 IAW ECA21-0555-21. WORK ACCOMPLISHED ON AEROMAN NR 2021-491738 (CLASSIFIED A MAJOR REPAIR)

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 51 IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492032 (CLASSIFIED A MAJOR REPAIR)

Part: SHEAR PLATE — CRACKED · airframe 78,180 hrs · 29,405 cycles

DURING HEAVY MAINTENANCE, (E/C A21-1260-01) FUSELAGE/ WFF SUPPORT STRUCTURE/ A320-53-1259 KEEL BEAM SHEAR PLATE & TI ANGLE FR41-42R/ CRACKS- PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)

Part: FLOORBEAM — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 2) AND -Y76 5 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491718 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC STAMP 238.

Part: FLOORBEAM — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 2 ) AND -Y254 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491721 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC STAMP 238.

Part: FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 1 ) AND Y254 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491722 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC STAMP 238.

Part: FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.200 INCH IN COCKPIT (1 EA); REF AEROMAN N/R 2021-491505, ACCOMPLISH MODIFICATION/REPAIR IN ACCORDANCE WITH AEROMAN 53-0549-21 REV 0 (COVER PLUS PARTS 1-2) AND AIRBUS SB A320-1263 REV 03 ON RH ONLY. EC A21-1328-01, MAJOR REPAIR.

Part: WING — CRACKED · airframe 78,180 hrs · 29,405 cycles

DURING HEAVY MAINTENANCE, (E/C A21-1371-01) WINGS / CENTER WING / FRONT SPAR / FRAME 36 / FLOOR BEAM / VERTICAL STIFFENER / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 60 PLUS 14 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492038(CLASSIFIED A MAJOR REPAIR)

Part: NONE — NONE · airframe 78,180 hrs · 29,405 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 36 PRESSURE DECK PANEL ON OPEN FASTENER HOLE 2 INCH OUTBOARD Y1292, CRACK DIRECTION IS 6 OCLOCK IN FWD CARGO COMPA RTMENT (1 EA); REF AEROMAN N/R 2021-491740, ACCOMPLISHED MODIFICATION/REPAIR IN ACCORDANCE WITH AEROMAN 53-0549-21 REV 0 (COVER PLUS PARTS 1-2) AND AIRBUS SB A320-53-1263 REV 03 AND EC A21-1367-01 ON LH ONLY (CONSIDERED A MAJOR REPAIR)

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION UPPER SURFACE OF UPPER SKIN OF THE CENTER WING BOX BTW +Y1292 AND +Y1732 IN PASSENGER CABIN; ACCOMPLISHED REPAIR ON ON CENTER WING BOX IAW EC A21-1360-21. WORK ACCOMPLISHED ON AEROMAN NR 2021-491731 (CLASSIFIED A MAJOR REPAIR)

Part: PRESSURE PANEL — CRACKED · airframe 78,180 hrs · 29,405 cycles

DURING HEAVY MAINTENANCE, (E/C A21-1367-01) FUSELAGE / CENTER FUSELAGE / CENTER WING BOX / FRAME 35-36 / LHS ONLY / PRESSURE PANEL ATTACHMENT HOLES - MODIFICATION (REPAIR SOLUTION FOR CRACK DAMAGES) (CONSIDERED A MAJOR REPAIR)

Part: FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 ON OPEN HOLE ( ZONE 1 ) AND -Y765 LOCATED ON FLOOR BEAM.; REF AEROMAN NR 2021-491717 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC STAMP 238.

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED BTW FR 47 PLUS 16 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-491810 (CLASSIFIED A MAJOR REPAIR)

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED BTW FR 59 PLUS 2 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 57-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492037 (CLASSIFIED A MAJOR REPAIR)

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED BTW FR 57 PLUS 9.875 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492036 (CLASSIFIED A MAJOR REPAIR)

Part: FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 2 ) AND Y765 LOCATED ON FLOOR BEAM. AEROMAN TECH 8640408 / 8612107 QC STAMP 238; REF AEROMAN NR 2021-491725 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021.

Part: FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.200 INCH IN COCKPIT (1 EA); REF AEROMAN N/R 2021-491504, ACCOMPLISHED THE REPAIR IN ACCORDANCE WITH AEROMAN EA 53-0564-21 REV O (COVER PLUS PARTS 1 AND 2) AND AIRBUS RDAF 80981867/003/2021#A AND EC A21-1328-01, AND R53112919 MAJOR REPAIR

Part: FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 2 ) AND Y254 LOCATED ON FLOOR BEAM; REF AEROMAN NR 2021-491723 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC STAMP 238.

Part: NONE — NONE · airframe 78,180 hrs · 29,405 cycles

DURING HEAVY MAINTENANCE, (E/C A21-1360-01) WINGS / CENTER WING BOX / UPPER SKIN PANEL / UPPER SURFACE / Y1292/RIB DATUM & STIFF 16-17 / CORROSION DAMAGE - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)

Part: DOOR FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK EMERGENCY EXIT DOOR 833 FWD FRAME SEGMENT 1 IN PASSENGER CABIN (1 EA) (CRACK LENGHT: 0.950 INC; REF AEROMAN N/R 2021-491634, REPLACED SEGMENT (2EA), BEAM (3EA) AND FASTENER LOC ON EMERGENCY EXIT DOOR 833 PASSENGER CABIN IAW SRM A320 51-42-11, THIS JOB WAS DOCUMENTED ON JOB CARD A320-52-1144-01-JB, EC A320-52-1144 MAJOR REPAIR.

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 55 PLUS 16 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492035 (CLASSIFIED A MAJOR REPAIR)

Part: FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK EMERGENCY EXIT DOOR 843 AFT FRAME SEGMENT 1 IN PASSENGER CABIN (1 EA) (CRACK LENGTH: 0.750 INCH); REF AEROMAN N/R 2021-491638, REPLACED SEGMENT (2EA), BEAM (3EA) AND FASTENER LOC ON EMERGENCY EXIT DOOR 843 PASSENGER CABIN IAW SRM A320 51-42-11, THIS JOB WAS DOCUMENTED ON JOB CARD A320-52-1144-02-JB , EC A320-52-1144, MAJOR REPAIR

Part: FRAME — CORRODED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION STRINGER 41L LOCATED NWT FR 28 TO FR 30 INTERNAL AREA IN FWD CARGO COMPARTMENT; REF AEROMABN N/R 2021-491693, - PERFORMED REPAIR OF STRINGER 41L LOCATED BTW FRAME27 AND FRAME 31 IN FORWARD CARGO COMPARTMENT IAW A320 SRM 53-00-13-300-001 FIG 001 (SHEET 2), SEE W/O 1138282, N/R 00040, AND FUR A320-53-00245 FOR SRI.

Part: FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON FRAME 36 IN OPEN HOLE ( ZONE 1 ) AND Y765 LOCATED ON FLOOR BEAM LAYER; REF AEROMAN NR 2021-491724 - REPAIRED PER EA# 53-0548-21 / JB EC# A21-1371-01 AND RDAF 80985768/003/2021. AEROMAN TECH 8640408 / 8612107 QC STAMP 238.

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 49 PLUS 8 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK +Y765 IAW A320 SRM 51-71-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492031 (CLASSIFIED A MAJOR REPAIR)

Part: NONE — NONE · airframe 78,180 hrs · 29,405 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATION FOUND ON LOWEST FASTENER HOLE OF BELLY FAIRING WEB AFT TI ANGLE LOCATION FR 41-42 RH. CRACK LENGTH IS 0.210 INCH ; REF AEROMAN N/R 2021-491794, PERFORMED REPAIR PER AEROMAN EA53-0560-21 COVER RO AND PART 1. JETBLUE EC A21-1260-01. (CONSIDERED A MAJOR REPAIR)

Part: DOOR FRAME — CRACKED · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CRACK EMERGENCY EXIT DOOR 844 FWD FRAME SEGMENT 1 IN PASSENGER CABIN (1 EA) (CRACK LENGTH: 0.700 INCH); REF AEROMAN N/R 2021-491635, REPLACED SEGMENT (2EA), BEAM (3EA), AND FASTENER LOC ON EMERGENCY EXIT DOOR 844 PASSENGER CABIN IAW SRM A320 51-42-11, THIS JOB WAS DOCUMENTED ON JOB CARD A320-52-1144-04-JB, EC A320-52-1144, MAJOR REPAIR

Part: NONE — NONE · corrosion level 2 · airframe 78 hrs · 2,940 cycles

DURING HEAVY MAINTENANCE, CORROSION SEAT TRACK +Y765 LOCATED ON FR 62 PLUS 7.625 INCHES IN PASSENGER CABIN; REMOVED AND REPLACED SEAT TRACK IAW A320 SRM 51-72-11-911-001. WORK ACCOMPLISHED ON AEROMAN NR 2021-492039 (CLASSIFIED A MAJOR REPAIR)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 78,180 hrs · 29,405 cycles

DURING HEAVY MAINTENANCE, CORROSION FLOORBEAM -Y1292 LOCATED BTW FR 66 AND FR 68 AT AFT GALLEY AREA (CPCP RELATED 534195-01) REPORTED BY CERT#: 99999; REMOVED AND REPLACED FLOORBEAM -Y1292 LOCATED BTW FR66 AND FR68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND DRAWING D5347- 2816, TOOL USED DIGITAL CALIPER P/N:500-197-30, S/N: A18135- 097, DUE DATE: JAN-03-2022, CALIPER P/N:500-752-20, S/N: B21- 038251, DUE DATE: AUG-13-2022. MX-220 IS NOT NECESSARY DUE TO FLOOR BEAM -Y1292 IS A SECONDARY STRUCTURE.

Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 75,939 hrs · 28,580 cycles

FT 504, EMERG EXIT LIGHT COVER CAME OFF NEAR L1 DOOR; SECURED EMERGENCY EXIT LIGHT COVER AT L1 DOOR IAW AMM 33-50-00.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 75,205 hrs · 28,304 cycles

PROTECTIVE COVER ON EMERGENCY EXIT LIGHT AT ROW 9D MISSING; REPLACED 9D EMERGENCY LENS. CHECK NORMAL IAW AMM 33-51-00.

Part: ANCHOR FITTING — CORRODED (RT MLG) · airframe 74,813 hrs · 28,155 cycles

DURING HEAVY MAINTENANCE, RMLG ANCHORAGE FITTING HAS PITTING CORROSION ON TOP SIDE OF ACTUATOR BUSHING; REF NR 440572-24027 - REMOVED AND REPLACED RMLG ANCHORAGE FITTING IAW SRM 57-26-13.

Part: ANCHOR FITTING — CORRODED (LT MLG) · airframe 74,813 hrs · 28,155 cycles

DURING HEAVY MAINTENANCE, LMLG ANCHORAGE FITTING HAS PITTING CORROSION AROUND BUSHING; REF NR 440572-24020 - REMOVED BUSHING, REMOVED CORROSION. APPLIED FINISH CUT TO THE BORE AND FACES. FABRICATED AND INSTALLED BUSHING. THIS IS A SAFE LIFE ITEM, 35,000FC. FINISH CUT WAS APPLIED, 35,000FC LIMIT FROM REPAIR EMBODIMENT IAW SRM 57-36-13-300-009 STEP D/E PGS 2/3.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 73,052 hrs · 27,492 cycles

AT THE CURRENT CHECK (11/2018), AIRCRAFT WAS FOUND WITH CRACK DAMAGE ON FASTENER HOLES AT THE FR35 PRESSURE BULKHEAD WEB, AT STR 30L. THE APPROPRIATE SRM SECTIONS WERE CONSULTED AND NO ALLOWABLE DAMAGE LIMITS OR REPAIR WAS LOCATED. CONTACTED FOR DISPOSITION AND SUBSEQUENTLY PROVIDED THE REF. /2/ TD AND REF. /3/ RDAS. THE REPAIR CONSISTS OF A CIRCULAR CUT-OUT OF THE CRACKED AREA IN THE PRESSURE BULKHEAD FR35 WEB AND INSTALLING A REPAIR ANGLE AS PER R533-70269. AFT SKIN AND FWD SKIN PORTION REPLACEMENT AS PER R533-70250. EXISTING FTIS DOUBLER REMOVED AND NEW DOUBLER INSTALLED. EC A18-942-01 ACCOMPLISHES THE REQUIREMENTS OF THE REF. /2/ TD AND REF. /3/ RDAS PER THE REF. /1/ EA. EC A18-942-02 TRACKS THE PERMANENT REPAIR DISPOSITION DUE WITHIN 6 MONTHS PENDING DTA; THIS REPAIR HAS BEEN APPROVED BY AIRBUS VIA THE REF. /2/ TD AND REF. /3/ RDAS AND IS CLASSIFIED AS A “MAJOR”, TEMPORARY REPAIR, AS PER THE GUIDELINES ESTABLISHED IN GMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 71,817 hrs · 26,995 cycles

CABIN EMERGENCY LIGHTS FAILED A BITE TEST. REMOVED AND REPLACED THE POWER SUPPLY BATTERIES AT LOCATION FIN 10WL,11WL AND 13WL IAW AMM 33-51-38. EMERGENCY CABIN LIGHTS CHECKED GOOD.

Part: BATTERY PACK — FAILED (10WL) · airframe 71,817 hrs · 26,995 cycles

CABIN EMERGENCY LIGHTS FAILED A BITE TEST. REMOVED AND REPLACED THE POWER SUPPLY BATTERIES AT 10WL, 11WL, AND 13WL, IAW AMM 33-51-38. EMERGENCY LIGHTS CHECKED GOOD.

Part: BATTERY PACK — FAILED (13WL) · airframe 71,817 hrs · 26,995 cycles

CABIN EMERGENCY LIGHTS FAILED A BITE TEST. REMOVED AND REPLACED THE POWER SUPPLY BATTERIES AT 10WL, 11WL, AND 13WL, IAW AMM 33-51-38. EMERGENCY LIGHTS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (FRAME 19) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

CORROSION WAS DISCOVERED ON SEAT TRACK Y-254, FRAMES 19 R & R THE SEAT TRACK IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 17) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT AT FRAME 17. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 17) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT FR 17. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y940, FRAME 18 +5. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y503.2, FRAMES 17 - 18. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, REV 121, & DWG 53112826.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y503.2, FRAMES 17 -18. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, REV 121, & DWG 53112826.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT AT Y765, FRAME 18. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, REV 121, & DWG 53112813, REV B.

Part: FLOOR SUPPORT — CORRODED (FRAME 17) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT FRAME 17. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FRAME 19) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

CORROSION WAS DISCOVERED ON THE SEAT TRACK, Y-254, FR 19. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAME 17) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y503.2, FRAME 17. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, REV 121, & DWG 53112826, REV D.

Part: FLOOR SUPPORT — CORRODED (FRAME 19) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON FLOOR SUPPORT AT Y-254, FRAME 19. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FRAMES 17-18) · corrosion level 2 · airframe 70,144 hrs · 26,334 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE FLOOR SUPPORT AT Y254, FRAMES 17 - 18. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, REV 121, AND DWG 53112828, REV H.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHTS) · airframe 67,080 hrs · 25,134 cycles

DURING ROUTINE MAINTENANCE, AFT EPSU 13WL SHOWED UNIT FAULT. R & R EPSU & BATTERY PACK IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: WIRE HARNESS — SHORTED (EMERGENCY LIGHTS) · airframe 67,080 hrs · 25,134 cycles

DURING ROUTINE MAINTENANCE, EMERGENCY LIGHTS WILL NOT PASS TEST, SHOWS INT/EXT SHORT. FOUND SEAT HARNESS SHORTED. R & R THE WIRE HARNESS IAW ESPM. EMERGENCY LIGHTS TEST GOOD.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 67,080 hrs · 25,134 cycles

DURING ROUTINE MAINTENANCE, AFT EPSU 13WL SHOWED UNIT FAULT. R & R EPSU & BATTERY PACK IAW AMM 33-51-38. OPS CHECKED GOOD.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 67,009 hrs · 25,111 cycles

DURING ROUTINE MAINTENANCE, AFT EMERGENCY LIGHT ESPU FAILED A CHECK. REPLACED THE POWER SUPPLY. CHECKED OK.

Part: BOTTLE — LOW PRESSURE (R1 DOOR SLIDE) · airframe 66,885 hrs · 25,055 cycles

R1 DOOR SLIDE PRESSURE INDICATION AT RED MARK. R & R THE R1 DOOR SLIDE IAW AMM 25-62-44.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 56,865 hrs · 21,468 cycles

DURING MAINTENANCE, EMERGENCY LIGHT FAILS TEST, R & R BATTERY PACK 13WL. EMERGENCY LIGHTS OPS CHECK GOOD IAW AMM 33-51-38.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 56,865 hrs · 21,468 cycles

DURING MAINTENANCE, EMERGENCY LIGHT FAILED TEST. R & R BATTERY PACKS AT 12WL. EMERGENCY LIGHTS CHECKS GOOD IAW AMM 33-51-38.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 44,153 hrs · 16,968 cycles

FLT 263 SMF-LGB, AT FL390 HYD BLUE ELECTRIC PUMP LOW PRESSURE IN ECAM. THE CREW ADVISED ATC TO HAVE EMERGENCY EQUIPMENT STANDING BY AND APPLIED LANDING DISTANCE PROCEDURE. THE TECHNICIAN REMOVED AND REPLACED BLUE ELECTRIC HYDRAULIC PUMP AS PER AMM 29-12-51. OPS AND LEAK CHECK OK.

Part: EPSU — FAILED (CABIN) · airframe 43,678 hrs · 16,813 cycles

FLT 780 MBJ-JFK DURING MAINTENANCE, EPSU RT FAULT. FOUND BATTERY FAULTING ON RT MID EPSU. REMOVED AND REPLACED IAW AMM 33-51-38. OPS CHECK OK.

Part: TARGET — OUT OF ADJUST (R1 DOOR) · airframe 40,521 hrs · 15,673 cycles

FLT 392 MCO-LGA, CREW DECLARED EMERGENCY DUE TO RIGHT FWD DOOR R1 SHOWS ECAM MESSAGE R1 DOOR ON CLIMB OUT (ECAM DOOR PG IND PASSENGER DOOR OPEN). CREW FOLLOWED QRH AND IT WAS DETERMINED THAT CABIN DOOR WAS NOT OPEN AND IT WAS SAFE TO PROCEED TO LGA. FLIGHT PROCEED TO LGA AND LANDED WITHOUT FURTHER INCIDENT. TECHNICIAN ADJUSTED DOOR HANDLE TARGET PER AMM 52-71-11. OPS CHECK NORMAL.

Part: BATTERY — FAILED (CABIN) · airframe 40,377 hrs · 15,631 cycles

FLT 529 EWR-MCO, ON GROUND MAINTENANCE CHECK FWD LT EMERGENCY BATTERY FAILED. REMOVED AND REPLACED BATTERY IAW AMM 33-51-38. OPS CHECK GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG DOOR) · airframe 32,577 hrs · 12,809 cycles

FLT 119, JFK-MSY, UPON LANDING GEAR RETRACTION, RECEIVED "L/G DOORS NOT CLOSED" ECAM. LANDING GEAR WHEELS IND NORMAL, BUT GEAR DOOR IND OPEN. DID NOT CLEAR UPON RECYCLE. RETURNED TO DEPARTURE AIRFIELD. REMOVED AND REPLACED L/G DOOR SELECTOR VALVE (41GA) IAW AMM 32-31-34, OPS CHECK OK, LEAK CHECK OK.

Part: BLEED VALVE — FAULTY (NR 2 ENGINE) · airframe 25,810 hrs · 10,357 cycles

PRESSURE PROBLEM. PRESSURE UNCONTROLLABLE, DIVERTED TO CLT. ON LANDING AT GATE WITH DOOR OPEN SHOWS MINUS -900 & .4 PSI. PFR SHOWS HISTORY OF NR 2 ENG BLEED PRESSURE REG VALVE/SOLENOID SENSE LINE FAULT. REMOVED & REPLACED NR 2 ENG BLEED VALVE (4001 HA2) IAW MM 36-1152 DUE TO SUSPECT FLUCTUATING BLEED PRESSURE OPS & LEAK CHECK OK. PERFORMED CABIN PRESSURE CHECK IAW AMM 05-53-00. OPS CHECK OK.

Part: POWER SUPPLY — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 15,695 hrs · 6,867 cycles

DURING EMERGENCY LIGHT TEST, FAULT INDICATION OF LEFT EPSU UNIT. FOUND WIRE HARNESS D9299200900200 AT SEAT 3C CHAFED CAUSING FAULT DURING TEST OF THE EMERGENCY LIGHTING SYSTEM IAW 33-51-00-710-001. ITEM PLACED ON MEL UNTIL PART CAN BE REPLACED. REMOVED AND REPLACED HARNESS & LT EPSU OVERWING EXIT.

Part: DIAPHRAGM — PUNCTURED (DOOR DAMPER) · airframe 13,939 hrs · 6,241 cycles

AFT SEVICE DOOR DAMPER AND EMMERGENCY OPERATION CYLINDER PUNCTURED DIAPHRAM IN PERCUSSION MECHANISM. REPLACED DIAPHRAM IAW AMM 52-10-00, OPERATIONAL CHECK PER 52-10-00 GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 12,610 hrs · 5,790 cycles

SMELLED ODOR DESENDING THROUGH FL300; F/A CONFIRMED. SWITCHED OVER TO APU BLEED AT LOWER ALT, F/A CONTINUED TO SMELL & FELT SICK. CREW DID NOT SMELL ANYMORE. F/A NR 2 USED PORTABLE OXYGEN BOTTLE. ON ARRIVAL CHECKED NR 1 & 2 ENGINE INLET & EXHAUST AREA, CHECKED NR 1 & 2 PACK INLETS & EXHAUST AREA, CHECK APU INLET & EXHAUST AREA. ALL CHECK CLEAN & NO LEAKS DETECTED. REMOVED AND REPLACED NR 1 PACK'S OZONE FILTER PER 21-51-41-401. FILTER CHECKED CLEAN (REINSTALLED SAME FILTER). GAIN ACCESS TO RECIRCULATION FILTER PER 21-21-41, CK'D GOOD. CHECK LAV AND GALLEY FILTER, CHECK CLEAN. RAN PACKS FOR 2 HRS, SYSTEM CHECKED NORMAL. NO ODOR DETECTED. REMOVED AND REPLACED FWD / LT POB PER 35-11-41. LEAK CHECK GOO

Part: DOOR — FOD (CARGO BAY) · airframe 12,623 hrs · 5,795 cycles

A/C DIVERTED TO FLL DUE RIGHT AFT DOOR MAKING LOUD HUMMING SOUND LIKE VACUUM. PERFORMED DETAILED VISUAL INSPECTION OF RT AFT DOOR SEAL, NO DAMAGE FOUND. CLEANED SEAL IAW 52-13-00. THE CONDITION REPEATED NEXT FLIGHT. REMOVED FOD FROM BULK CARGO DOOR, INSPECTED R2 DOOR AREA. PERFORMED PRESSURIZATION CHECK ON GROUND. OPS CHECK GOOD IAW MM 21-33-00. NO DEFECT NOTED.

Part: CAPACITOR — FAILED (ELECTRICAL BOX) · airframe 10,874 hrs · 5,093 cycles

ELECTRICAL ODOR MID CABIN ON FINAL APPROACH. AREA INSPECTED WITH NO NOTICEABLE DEFECTS. LIVE TV CIRCUIT BREAKER PULLED AND COLLARED AS PERCAUTIONARY. ISSUED MEL 25-22-03 CAT D, ENTIRE LIVETV. PRELIMINARY FINDING: SEAT ELECTRONICS BOX, INTERNAL POWER SUPPLY CAPACITOR C12 APPEARS TO HAVE FAILED.

Part: CONNECTOR — NOT SEATED (CABIN)

DURING EMERGENCY LIGHT TEST, PER WEEKLY CHECK DOC, STEP 5&7 EMERGENCY TEST FAILED. RESET CANNON PLUG ON ESPU FIN 10WL. PERFORMED OPS CK OF EMERGENCY LIGHT SYSTEM AS PER AMM 33-51-00. OPS CKS GOOD.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 7,914 hrs · 3,894 cycles

DEPARTING PBI, FLIGHT 74, PBI TO JFK, GEAR WOULD NOT RETRACT WITH GEAR LEVER IN UP POSITION. BOTH GREEN DOWNLOCK AND RED UPLOCK LIGHTS WERE OBSERVED ON LANDING GEAR PANEL. NO ECAM WAS OBSERVED. AFTER RECYCLE OF GEAR HANDLE, NORMAL GEAR RETRACTION AND SYSTEM STATUS NORMAL WAS OBSERVED. PERFORMED DETAIL VISUAL INSPECTION OF NOSE LANDING GEAR AS PER AMM 32-21-00. FOUND PROX SENSOR OUT OF ADJUSTMENT. REPLACED TARGET BUSHED LEVER, CLEVIS AND LINK ASSY AND ATTACHING HARDWARE AS PER AMM 32-21-27. PERFORMED TSM TASK 32-21-00-810-815, NO FAULT FOUND, REPLACED PROX SENSOR 25GA AS PER AMM 32-31-73, OPS CHECK OK.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 6,992 hrs · 3,515 cycles

AFTER TAKEOFF LANDING GEAR FAILED TO RETRACT, L/G SHOCK ABSORBER FAULT, AIR RETURN TO JFK, OVERWEIGHT LANDING APPROX 160,000 LBS AT 3-400 FPM. ON INSPECTION FOUND FOD (UNSERVICEABLE TAXI LAMP) IN AREA OF SCISSORS LINK CAUSING TARGET FOR EXTENSION TO FAIL, REMOVED FOD, PERFORMED EXTENSION AND RETRACTION TEST PER AMM TASK 32-31-00-501, NLG FAILED TO RETRACT, INSPECTED NOSE STRUT ASSY, FOUND PROX SENSORS 24GA AND 25GA OUT OF ADJUSTMENT. ADJUSTED, OPS CHECK PROX SENSORS. PERFORMED RETRACTION TEST, OPS CHECK OK.

Part: STRUCTURE — TORN · airframe 6,860 hrs · 3,454 cycles

At JFK arrival, Flt 67, Ground damage from jetway impact, found a (6" x 4") tear between Frames 23/24 and Stringers 22/23.Fuselage skin repair at Frame 24, between Stringers 21 and LHS 24 as per JetBlue Engineering Order 5301242. Repair consisted in: cutting out the damaged area, installing a repair doubler (clad-2024T3) thickness=0.09". The original alu rivets (diameter 4mm) have been replaced by HL11VF6, The original Hi lock fasteneres (diameters 4.8mm) have been replaced by HL411VF6. The other fasteners have been installed according to the E.O 5301242 drawing and Airbus repair design approval sheet. No cracks, deformations have been detected on the frame 24 and holes.

Part: SMOKE — DETECTED (POWER CORD)

FLT 25 - JFK-TPA - WHILE CLIMBING THROUGH FL240, FLIGHT CREW HEARD A LOUD POP AND SAW SMOKE TO THE RIGHT REAR OF THE F/O SEAT. AFTER CLOSE CHECK OF THE COCKPIT, BELIEVE THE SOURCE WAS THE POWER CHORD THAT PROVIDES POWER TO PILOT LAPTOP COMPUTER. SMOKE WAS MINOR AND CLEARED RAPIDLY. C/B DID NOT POP. SMOKE GOGGLES/OXYGEN MASKS WERE USED AS PER PROCEDURES. AS PER AMM 5-56, INSPECTED AREA BEIND F/O''S SEAT FOR SOURCE OF NOISE AND SMOKE, FOUND DAMAGE AND BURN MARKS ON CORD FOR LAPTOP POWER SOURCE. INSPECTED ELECTRICAL PLUG BEHIND FLIGHT OFFICERS SEAT, CHECKED OK. AIRCRAFT OK FOR CONTINUED SERVICE. (M)

Part: ACTUATOR — LEAKING (NR 4 SPOILER)

JFK/FLL - FLT 11 - AIR TURN BACK TO JFK DUE HYDRAULIC YELLOW RESERVOIR LOW LEVEL ON ECAM. ON INSPECTION, FOUND RT WING NR 4 SPOILER ACTUATOR LEAKING. REMOVED NR 4 SPOILER ACTUATOR REF AMM 27-64-51, INSTALLED SPOILER ACTUATOR PER AMM 27-64-51, OPS CHECK AND LEAK CHECK C/W, ADJ AND TEST PER AMM 27-64-00. OK. (X)