N569JB

Part: STRINGER — CORRODED (ZONE 100) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: CORROSION STRINGER 43L BTW FRAME 57 AND FRAME 58 IN AFT CARGO COMPARTMENT (CPCP FINDING ); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00019) PERFORMED PERMANENT REPAIR ON STRINGER 43L BTW FRAME 57 AND FRAME 58 IN AFT CARGO COMPARTMENT IAW A320 SRM 53-00-13-300-001. TOOL USED: CALIPER P/N: 500-197-30, S/N: A21041924, DUE DATE: OCT-16-2024. THIS REPAIR IS CATEGORY B, INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 60,000FC/120,000 FH, SUBSEQUENT INSPECTION AT INTERVALS OF TBD,

Part: SKIN — CORRODED (ZONE 100) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: FUSELAGE/ FWD LOWER SKIN AT NLG/ FR12-13 LH LOWER STGR AT Y520/ CORROSION- TEMPORARY REPAIR (A24-745-01) (CONSIDERED A MAJOR REPAIR)

Part: SHEAR WEB — CRACKED (ZONE 100) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: CRACKED SHEAR WEB LOCATED AT FR 71 BTW STR 27R AND 32R IN THE THS COMPARTMENT; REF AEROMAN WO# 2024-177/1 NR# 2024-298723 FOR ALL WORK ACCOMPLISHED REMOVED DAMAGED SHEAR WEB FABRICATED AND INSTALLED NEW WEB IAW A320 SRM 51-41-2, SRM 51-42-11, 51-42-11, 51-44-11, 51-21-11

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INTERCOSTAL LAYER LOC DOOR STOP 7 FR16RH HOL E H3. CRACK DEPTH 0.063 INCH AND DIRECTION 12 OCLOCK; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00024) REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL OF DOOR STOP 7 FR16 RH IAW A320 SRM 51-72-11, A320 SRM 51-42-11 AND DRAWING # D53114223. TOOL USED: EDDY CURRENT EQUIPMENT PN: NORTEC500D, SN: N500X1693P030457, DUE DATE: OCT-15-2024; SMALL HOLE GAUGES P/N: 154-901, S/N: AE-421357, DUE DATE: FEB -12-2025; CALIPER P/N: 500-196-30, S/N: A22348589, DUE DATE : JUL-12-2024; TORQUE PN: QD1R200A, SN: 0821121264, DUE DATE: SEP-19-2024. THIS REPAIR IS CLASSIFIED AS CATEGORY A AND NO FURTHER INSPECTION IS REQUIRED IAW A320 SRM 53-11-12-300-010 FIG.004 (SHEET 1).DONE BY RII BY J.SERVELLON ON AEROMAN W/O 2024 177/1 N/R 2024-298781 C. PEREZ 8606212.

Part: STOP FITTING — CRACKED (ZONE 200) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND DOOR STOP 7 FR20LH HOLE H1. CRACK DEPTH 0.063 I NCH AND DIRECTION 12 OCLOCK; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00023) PERFORMED PERMANENT REPAIR ON DOOR STOP 7 FR20 LH ON HOLE H1 IAW A320 SRM 53-11-12-300-010. TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D, S/N: 60009161631, DUE DATE: MAR-11-2025; SMALL HOLE GAUGES P/N 154-901, S/N: AE-421357, DUE DATE: FEB -12-2025, CALIPER P/N: 500-196-30, S/N: A22348589, DUE DATE : JUL-12-2024; MICROMETER P/N: 293-344-30, S/N: 76014965, DUE DATE : MAR-31-2025; ULTRASONIC THICKNESS GAGE P/N: 45MG, S/N: 221860711, DUE DATE: NOV-21-2024; TORQUE WRENCH P/N: QD1200A, S/N: 0821122921, DUE DATE: OCT-06-2024. THIS REPAIR IS CLASSIFIED AS CATEGORY B, INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT 11,600 FC/ FH NOT RELEVANT, SUBSEQUENT INSPECTION AT INTERVALS (UNTIL 60000 FC/FH NOT RELEVANT) AT 11,600 FC/FH NOT RELEVANT, INSPECTION METHOD: ROTATING PROBE TEST(SRM 53-11-12-300-010 FIG. 009) IAW SRI 53-11-12-205-005 TABLE 001. DONE BY C. PEREZ 8606212 CHECKED BY N. FLORES 279 EMBODIED IN W/O 2024 177/1 N/R 2024-298779 FUR # FUR-A320-53-01388.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: CORROSION LOWER SILL AT LEVEL OF FRAME 60 IN BULK CARGO COMPARTMENT ( CPCP FINDING ); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00020) PERFORMED PERMANENT REPAIR ON LOWER SILL AT LEVEL OF FRAME 60 IN BULK CARGO COMPARTMENT IAW A320 SRM 53-41-49-300-003. TOOL USED: CALIPER P/N:500-197-30 S/N:A23218424, DUE DATE: FEB-14-2025; ELECTRONIC DEPTH P/N: 8645A12, S/N: 72625, DUE DATE: JUL-25-2024; GAGE RADIUS P/N:S167C, S/N: 29044, DUE DATE: AUG-01-2024. THIS REPAIR IS CATEGORY B, INSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT AT 60, 000 FC/120,000 FH; SUBSEQUENT INSPECTION AT INTERVALS OF TBD; INSPECTION METHOD TBD IAW A320 SRI 53-41-49-205-003 TABLE 001. FORM MX-220 IS COMPLETED DONE BY ALL WORK EMBODIED ON WO 2024 177/1 N/R 2024-298963 FUR-A320-53-01382.

Part: FRAME — CRACKED (ZONE 200) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME LOC DOOR STOP 7 FR16RH HOLE H1. CRACK DEPTH 0.063 INCH AND DIRECTION 9 O'CLOCK; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00025) REMOVED AND REPLACED INTERCOSTAL FITTING LOC. AT LEVEL OF DOOR STOP 7 FR16 RH IAW A320 SRM 51-72-11, A320 SRM 51-42-11 AND DRAWING # D53114223. TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D, S/N: 60009161631, DUE DATE: MAR-11-2025; SMALL HOLE GAUGES P/N: 154-901, S/N: AE-421357, DUE DATE: FEB-12-2025; CALIPER P/N: 500-196-30, S/N: A22348589, DUE DATE : JUL-12-2024; TORQUE PN: D1R200A, SN: 0821121264, DUE DATE: SEP-19-2024. THIS REPAIR IS CLASSIFIED AS CATEGORY A AND NO FURTHER INSPECTION IS REQUIRED IAW A320 SRM 53-11-12-300-010 FIG.004 (SHEET 1). WORK DONE BY N.REYES 8608018 RII BY J.SERVELLON 163. ON AEROMAN WO 2024 177/1 NR.

Part: SKIN — CORRODED (ZONE 100) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: CORROSION INTERNAL SKIN BTW FR 12 TO FR 14 LOWER AREA ON LH AVIONIC COMPARTMENT(CPCP FINDING); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00047) REF AEROMAN N/R 2024-29895, PERFORMED REPAIR TO CORROSION AT THE FWD FUSELAGE LOWER SKIN AT NLG FR12-13 LOWER STRG AT Y520 PER AEROMAN EA 53-9008-24 COVER R0 AND PARTS 1-3, RDAF 81405823/003/2024#A, AND TE/81405823/012/2024 ISSUE C AND JETBLUE EC A24-745-01, ACCOMPLISHED BY # 8610712.RII 318.

Part: FUEL TANK — CORRODED (ZONE 100) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: CORROSION ON UPPER SKIN BTW FR41/FR42 LH SIDE CENTER TANK AREA IN PASS ENGER CABIN; (RESOLVED ON W/O: 1308674 TASKCARD: NR-00050) REF AEROMAN N/R 2024-298788, REMOVED CORROSION MECHANICALLY LOCATED ON UPPER SKIN BTW FR41/FR42 LH SIDE CENTER TANK AREA IN PASSENGER CABIN. IAW A320 SRM 51-74-00. EVALUATED REWORK LOC. UPPER SKIN BTW FR41/FR42 LH SIDE CENTER TANK AREA IN PASSENGER CABIN AND FOUND WITHIN LIMITS I.A.W. A320 SRM 57-11-11-283-001 PARAGRAPH 2.A STEP (9) FIG.001. THIS REPAIR IS CLASSIFIED AS CATEGORY A AND NO FURTHER INSPECTION IS REQUIRED.

Part: FITTING — CORRODED (ZONE) · airframe 77,507 hrs · 27,885 cycles

DURING HEAVY MAINTENANCE: CORROSION ON FITTING BTW FR13- FR14 INTERNAL STRUCTURE LOWER AREA ON LH AVIONICS COMPARTMENT (CPCP FINDING); (RESOLVED ON W/O: 1308674 TASKCARD: NR-00051) REF AEROMAN NR 2024-298984 WO# 2024-177/1 REMOVED AND REPLACED FITTING AND FASTENERS LOC. BTW FR13 AND FR14 AT LEVEL OF Y520 ON INTERNAL STRUCTURE I.A.W A320 SRM 51-72-11 AND A320 SRM 51-42-11.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,802 hrs · 26,461 cycles

FLT#87, ALB-FLL. 'DURING DESCENT ( 8000 MSL ) COCKPIT ODOR ( FUME EVENT ) WAS NOTED UNTIL LANDING. X BLEED & PACK 1 OFF UNTIL PARKING; PERFORMED INSPECTION OF APU COMP NO LEAK ( OIL / FUEL ) FOUND AT THIS MOMENT. PERFORMED INFO NOTE 2017-T015J. ACCOMPLISHED PACK BURNS, NO ODOR IS PRESENT IN THE CABIN / AND OR FLIGHT DECK. A/C OK TO CONTINUE SERVICE.'

Part: VENT — CORRODED (LAVATORY EXTRACT) · airframe 72,323 hrs · 25,923 cycles

DURING HEAVY MAINTENANCE: FOUND CORROSION ON LAV VENT EXTRACT; REF FLIGHT STARV W/O FS220088. N/R 00004, PERFORMED DOUBLER REPAIR IAW A320 SRM 53-41-00, SEE FS 220088 N/R 00004 FOR WORK ACCOMPLISHED. MAJOR REPAIR.

Part: NONE — NONE · airframe 71,139 hrs · 25,460 cycles

FLT#837, JFK-STI. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO JFK) ' DURING TAKEOFF ROLL AT ROTATION SPEED, AIRCRAFT JERKED HARD LEFT. AFTER LIFT-OFF A SIGNIFICANT VIBRATION WAS FELT. SUSPECTED BLOWN TIRE. DECIDED NOT TO RETRACT LANDING GEAR. PROCEEDED WITH A LOW APPROACH FOR JFK TOWER TO VISUALLY INSPECT GEAR. ALL APPEARED NORMAL. PROCEEDED TO BURN FUEL FOR NORMAL LANDING. ROLL OUT FELT A WOBBLE.' (SUPPLEMENTAL TO FOLLOW)

Part: SLIDE — FAILED · airframe 65,629 hrs · 23,527 cycles

DURING HEAVY MAINTENANCE, REF AEROM 2020- 42075 WO 12/1 PERFORMED CREW DOOE CONTROLLED DEPLOYMENT 832 IAW AMM 25-62-00-710-001-A & REPLACED SLIDE 832 IAW AMM 25-62-44-400-007-A; SUPPLEMENTAL INFORMATION TO FOLLOW

Part: SKIN — DENTED (NR 1 SLAT) · airframe 65,629 hrs · 23,527 cycles

DURING HEAVY MAINTENANCE, ENT SLAT 1 LOWER SKIN RH WING; REF AEROMAN NR 2020-42151 WO 2020 12/1 PERFORMED REPAIR ON SLAT #1 LOWER SKIN RH WING IAW EA # 57-0116-20 PART 1.

Part: SLIDE — NO TEST (CREW DOOR) · airframe 65,629 hrs · 23,527 cycles

DURING HEAVY MAINTENANCE, REF AEROM 2020- 42075 WO 12/1 PERFORMED CREW DOOE CONTROLLED DEPLOYMENT 832 IAW AMM 25-62-00-710-001-A & REPLACED SLIDE 832 IAW AMM 25-62-44-400-007-A; SUPPLEMENTAL INFORMATION TO FOLLOW

Part: SKIN — DENTED (NR 2 SLAT) · airframe 65,629 hrs · 23,527 cycles

DURING HEAVY MAINTENANCE, REF AEROMAN W/O 2020-12/1 WCC 2020-42059, WEIGHT VARIANT UPGRADE FOR ACFT N569JB - SRM REPAIR SURVEY - LEFT WING - SLAT #2 DENT DAMAGE - LEADING EDGE; REF AEROMAN W/O 2020-12/1 WCC 2020-42059, PERFOEMED PERMANENT REPAIR ON LEFT WING SLAT #2 15.5 INCHES FROM INBOARD EDGE OF SLAT NOSE AREA IAW EA #57-0105-20 REV 0 AND PART I AND EC # A20-120-01. THIS REPAIR IS CLASSIFIED AS CATEGORY A AND NO FURTHER ACTION IS REQUIRED.

Part: STRUCTURE — BROKEN (RUDDER) · airframe 65,629 hrs · 23,527 cycles

DURING HEAVY MAINTENANCE, PER AEROMAN WORK ORDER 2020-12/1, WCC# 2020-42019, FOUND BROKEN RUDDER TIP (326AT) ON VERTICAL STABILIZER; PER AEROMAN WORK ORDER 2020-12/1, WCC# 2020-42019, PERFORMED PERMANENT REPAIR ON RUDDER TIP (326AT) ON VERTICAL STABILIZER IAW A320 SRM 55-44-00-300-008. THIS IS A CAT A REPAIR AND NO FURTHER ACTION IS REQUIRED.

Part: SKIN — CORRODED (LT WING) · airframe 65,629 hrs · 23,527 cycles

DURING HEAVY MAINTENANCE, REF AEROMAN W/O 2020-12/1 WCC 2020-42262, CORROSION ON TOP SKIN, LOWER SURFACE, TRAILING EDGE, REAR SPAR, RIB 16 PLUS 20 INCHES ON LH WINGL; REF AEROMAN W/O 2020-12/1, WCC 2020-42262, EVALUATED EXISTING REWORK LOCATED RIB 16 + 20, TOP SKIN LOWER SURFACE TRAILING EDGE REAR SPAR LH WING AND FOUND WITHIN LIMITS AS CATEGORY A IAW SRM 57-21-11-283-007 TABLE 002. REPAIRED WITH REPAIR INSSTRUCTIONS ON DRAWING # R57258998. NOMINAL SKIN THICKNESS ON REQORKED AREA IS 0.0197 INCH. MINIMUM REMAINING THICKNESS ON REWORKED AREA IS 0.178 INCH. NO FURTHER ACTION IS REQUIRED.

Part: BATTERY PACK — FAILED (CABIN) · airframe 61,741 hrs · 22,048 cycles

FLT 2066, RSW-BOS. FDW BATTERY PACK FAIL ( ESPU); R & R FWD (EPSU) EMERGENCY BAT LIGHT IAW AMM 35-51-00. OPS CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 59,616 hrs · 21,193 cycles

RIGHT OVERWING EXIT, TWO EMERGENCY EXIT SIGN COVERS WERE MISSING. REPLACED THE COVERS IAW AMM 33-51-15. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT CABIN FLOORBEAM Y464 1 INCH FWD OF FRAME 66. REMOVED CORROSION ORIG MAT .140" REMAINING MAT .088" MAT LOSS .052" L 2.5" W 1.3". FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM Y464 AT AFT CABIN FR 64 TO 67 IAW SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT FLOOR SUPPORT 1 INCH OF FRAME 20 IN FRONT OF R2 DOOR CUTOUT. REMOVED AND REPLACED WEB AND ANGLE PN D5311278520301 AND D5311278620101 IAW SRM 51-72-11 AND GMM 5-169.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT CABIN R2 DOOR I/B SILL 1 INCH AFT OF FRAME 66. REMOVED AND REPLACED R2 DOOR SILL PN D5348004320701 PO 1041397.7 IAW SRM 51-72-11-911-001.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT DADO PANEL SUPPORT FLOOR BEAM AT FR 66 3" FWD OF GIRT BAR FITTING HAS BIG AREA OF CORROSION. REMOVED CORROSION ON L2 DOOR SILL, FOUND TO BE OUT OF LIMITS IAW 53-00-14-283-002 FIG 101 PG 4, REQUIRED NEW L2 DOOR SILL AND INSTALLED IAW SRM 51-42-11 PG, 17 PARA 4 51-72-11 PG2-C.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON LT AFT CABIN FLOORBEAM Y1292 FR66 +1" STR23L. REMOVED AND REPLACED FLOORBEAM Y1292 AT FR66 +1" STR23L IAW SRM 51-72-11.

Part: NOT REPORTED — CRACKED (FUSELAGE) · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CRACKS WERE FOUND. REFER EC A18-414-01. FUSELAGE/ CENTER FUSELAGE/ ALI 521110-01/ FR16LT & FR20LT FASTENER HOLES/ MULTIPLE CRACKS- PERMANENT REPAIR; APPROVED THIS REPAIR PER REF /3/ RDAS AND IS CLASSIFIED AS MAJOR CATEGORY 'B'.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON AFT CABIN FLOORBEAM Y465 5 INCHES AFT OF FRAME 66. REMOVED AND REPLACED FLOORBEAM Y464 F66 IAW SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON MAIN CABIN AT FR68 FLOORBEAM Y-1292 (RT) ON UPPER SURFACE. REMOVED AND REPLACED MAIN CABIN AT FR68 FLOORBEAM Y-1292 (RT) PN D5347218920400 PO 1036857.5 IAW SRM 51-72-11 AND 51-42-11 PER 2.F AND 2.D.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT CABIN R2 DOOR I/B SILL 1 INCH AFT OF FRAME 66. REMOVED AND REPLACED R2 DOOR SILL PN D5348004320701 PO 1041397.7 IAW SRM 51-72-11-911-001.

Part: SHEAR WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,220 hrs · 21,042 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON RT AFT CABIN CORNER SHEAR WEB. REMOVED AND REPLACED RT AFT CABIN CORNER SHEAR WEB IAW SRM 51-72-11-911-001.

Part: BULB — BROKEN (CABIN) · airframe 58,606 hrs · 20,803 cycles

DURING APPROACH, A STRONG ODOR IN THE COCKPIT AND CABIN, OF ELECTRICAL ODOR, LIKE A BALLAST IN A FLUORESCENT LIGHT BURNING OUT. TURNED OFF THE COMMERCIAL BUTTON ON OVHD ELEC PANEL AND THE AFT AVIONICS COMP. SWITCH. THE ODOR SUBSIDED BUT CHANGED TO THE ODOR ASSOCIATED WITH THE DIRTY SOCKS AND THEN WENT AWAY ALMOST COMPLETELY FOR THE LAST 5 MINUTES OF THE FLIGHT. THEN AFTER LANDING, THE ELECTRICAL ODOR RETURNED BUT NOT AS STRONG AS IN FLIGHT. THE TWO SWITCHES REMAINED OFF UNTIL PARKED AT THE GATE. PERFORMED AN INSPECTION OF THE CENTRAL ELECTRICAL CIRCUITS IAW 24-00-00-200-003A. FOUND 2A SIDEWALL LAMP BURNED OUT AND GLASS CAUSING BROKEN EXPOSING INSIDE OF BULB AND GLASS . CLEARED DEBRIS & REPLACED THE BULB AS REQUIRED. TROUBLESHOT IAW INFO NOTICE 2017-T015C. NO DUPLICATED EVIDENCE OF ODOR, INSPECTED APU BLEED DUCT AT BLEED VALVE FOR CONTAMINATION AND APU INLET. NO DEFECT NOTED. COMPLIED WITH INFO NOTICE 2017-T015B. ACFT OK FOR SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 55,665 hrs · 19,703 cycles

EMERGENCY LIGHTING FORWARD PARTION RED LIGHT INOPERATIVE. FOUND A DAMAGE WIRE AT FIN 361WL1. REPAIR THE WIRE IAW ESPM 20-53-51. OPS CHECKED GOOD.

Part: WARNING LIGHT — FAULTED (NR 1) · airframe 45,783 hrs · 16,029 cycles

AIRCRAFT DIVERTED DUE TO LGCIU 1 FAULT. LANDING GEAR GEAR AURAL, INDICATED ALL THREE UNLOCKED. PERFORMED INDICATION CHECK AND GEAR WAS UP AND LOCKED. WHEELS -SD- SHOWED AMBER XX ALL GEARS. R & R LGCIU (5GA1) IAW AMM 32-31-71 AS A PRECAUTION. LANDING GEAR CONTROL LEVER WAS ALSO REPLACED. PERFORMED LANDING GEAR LEVER CHECK IAW MM 32-31-11 AND LANDING GEAR SWING IAW MM 32-31-00, FOUND OK.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 45,302 hrs · 15,861 cycles

DURING MAINTENANCE CHECK OF CABIN EMERGENCY LIGHTS, FOUND AFT BATTERY PACK SHOWING EXTERIOR LIGHT FAULT AND BATTERY FAULT. R & R BATTERY PACK IAW AMM CH 33-51-38. OPS CHECKED GOOD.

Part: OXYGEN MASK — NOT SEATED (COCKPIT) · airframe 33,846 hrs · 11,898 cycles

FLT 824 SDQ-JFK, AIRCRAFT DIVERTED TO SJU DUE TO OXYGEN APPEARS TO BE LEAKING, DEPARTED WITH 550 PSI AFTER 30 MIN OF FLIGHT O2 WAS 360 PSI AND DECREASING. RESET ALL MASK BEFORE DEPARTURE. SERVICED CREW O2 BOTTLE IAW AMM 12-14-35 AND PERFORMED FIM TASK 35-10-00-810-813. RESEATED CREW OXYGEN MASK. NO FURTHER LEAKS NOTED, CREW O2 NOW AT 1340 PSI.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,868 hrs · 10,398 cycles

FLT 6403 JFK-SAL, ON MAINTENANCE CHECK FOUND EPSU UNIT FAULT IN FWD AREA GALLEY. REPLACED BATTERY PACK IN FWD AREA GALLEY. TEST OK IAW AMM 33-51-38.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 27,535 hrs · 9,577 cycles

FLT 762 CUN-JFK DIVERTED TO MCO, SMOKE LAV / CRG DET FAULT. REMOVED AND REPLACED FWD LAV SMOKE DET UNIT IAW MM 26-17-15. OPS CHECK ALL NORMAL.

Part: BLEED VALVE — FAILED (NR 2 ENGINE) · airframe 21,245 hrs · 7,280 cycles

FLT 785, MCO-BON, DIVERTED TO FLL, ENG NR 2 BLEED FAULT. ACCOMPLISHED ECAM QRH, NO PRESSURIZATION IN CABIN. LOST BOTH (1&2) EMERGENCY DESCENT REQUIRED. REMOVED AND REPLACED NR 2 ENG PRESSURE REGULATING VALVE 4001HA PER AMM 36-11-52. OPS CHECK OK.

Part: COMPRESSOR — STALLED (NR 1 ENGINE) · airframe 21,066 hrs · 7,213 cycles

FLT 1262, LGB-SMF, AIR RETURN TO LGB, ENG NR 1 COMPRESSOR STALL (ECAM) THRUST LEVERS AT CL DETENT LEVEL AT FL230 "BANG" AND YAW AND VIBRATION SAW ZERO EPR, THEN WENT BACK TO NORMAL. DID NOT SHUT DOWN IAW QRH 6-26. PERFORMED TSM 71-00-00-710-013-A, GVI, BLEED VVALVE CK, VSV LUBE, BOROSCOPE OK. HI POWER TEST NR 11, ALL TEST OK, CHECK OK, ALL ENG PARAMETERS NORMAL. ACFT OK FOR SERVICE. (S)

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE) · airframe 555 hrs · 200 cycles

L2 SLIDE RAFT BOTTLE PRESSURE LOW FOUND DURING WEEKLY CHECK. REMOVED AND REPLACED L2 SLIDE RAFT IAW 25-62-44.