N644JB

Part: MOTOR — FAILED (FLAP SYSTEM) · airframe 70,891 hrs · 25,607 cycles

FLT#302, FLL-JFK. (AN EMERGENCY WAS DECLARED) "FLAPS FAULT-ON CLIMB OUT F/CTL FLAP SYS 1 FAULT ON APPROACH F/CTL FLAPS FAULT SLATS EXTENDED TO POSITION 2 FLAPS DID NOT EXTEND AND STAYED AT ZERO. LANDED IN THAT CONFIGURATION @ 157 KTS. BRAKES STAYED BELOW 300 DEGREES; PERFORMED BITE TEST PF FLAP SYS PER AMM 27-51-00. OK FOR SYS. NO FAULT NOTED AT THIS TIME. ACCOMPLISHED OPS CHK OF FLAP SYS. FAULT DUPLICATED. REF TSM 27-51-00-810-810A STEP(B). WITH PTU OFF FLAP SYS 2 PCU HYD MOTOR VERIFIED OPERATIONAL WITH GREEN HYD SYS PRESSURIZED WITH PTU OFF FAILS OP CHK. FOR FLAP SYS 1 MVD MOTOR. REMOVED AND REPLACED FLAP SYS 1 HYD MOTOR IAW AMM 27-54-54. OPS CHK GOOD. NO FAULT NOTED WHEN OPS CHK FLAPS. "

Part: BATTERY — INOPERATIVE (EPSU BATTERY 11W) · airframe 68,924 hrs · 24,844 cycles

FLT#2752, SJU-TPA. 'EPSU BATTERY 11WL FAILED TEST; REMOVED AND REPLACED EPSU BATTERY AT 11WL IAW AMM 33-51-38.'

Part: BATTERY — FAILED (EPSU BATTERY 12W) · airframe 68,924 hrs · 24,844 cycles

FLT#2752, SJU-TPA. 'EPSU BATTERY 12WL FAILED TEST; REMOVED AND REPLACED EPSU BATTERY AT 12WL IAW AMM 33-51-38.'

Part: COMPUTER — UNKNOWN (1WV1) · airframe 66,996 hrs · 24,132 cycles

FLT#1133, MCO-SJU. 'REPEAT WRITE-UP! RIGHT OVERWING EXIT SHOWS NOT ARMED IN FLIGHT, SHOWED ARMED ON THE GROUND; REMOVED AND REPLACED #2 SDAC IAW AMM 31-55-34. OPS CHECK NORMAL. PERFORMED PRESS. CHECK REF. AMM 05-53-00. NO FAULTS NOTED. A/C OK TO CONT. SVC.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,499 hrs · 23,522 cycles

DURING HEAVY MAINTENACE: CRACK INDICATION FOUND IN OPEN UPPER HOLE FROM DOOR STOP FITTING #7; R H FRAME 16; CRACK DIRECTION: 6 CLOCK; D1-D2= 0.095 INCH; REF AERMAN WO 2023 360/1 N/R 2023-692458, PERFORMED REPAIR ON FRAME 16 RH LOCATED UPPER HOLE FROM DOOR STOP FITTING #7. IAW A320 SRM 53-11-12-300-010. THIS REPAIR IS CATEGORY A. COMPLETED BY C. VARELA 8622718 CHECKED BY RII O. COLORADO QC 122.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 65,499 hrs · 23,522 cycles

DURING HEAVY MAINTENACE: CRACK INDICATION FOUND IN OPEN INBOARD LOWER HOLE FROM DOOR STOP FITTIING #7, RH FRAME 16; CRACK DIRECTION: 6 O'CLOCK; D1-D2= 0.125 INCH; REF AEROMAN WO 2023 360/1 N/R 2023-692459, PERFORMED REPAIR ON FRAME 16 RH LOCATED INBOARD LOWER HOLE FROM DOOR STOP FITTING #7. IAW A320 SRM 53-11- 12-300-010. THIS REPAIR IS CATEGORY A.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 65,499 hrs · 23,522 cycles

DURING HEAVY MAINTENACE: CORROSION ANGLE WEB FLOOR STRUCTURE BTW FR69/FR70 AT LEVEL STR23L AFT GALLEY AREA (1 EA) (CPCP RELATED REFER TO MPD TASK 534195-01); REF AEROMAN NR 2023-692366 WO 2023 360/1, REMOVED AND REPLACED WEB LOC ON FLOOR STRUCTURE BETWEEN FR69 TO FR70 AT LEVEL STR 23L AFT GALLEY AREA I.A.W A320 SRM 51-72-11. COMPLETED BY J. ALVAREZ 8615413 CHECKED BY RII I. GARCIA QC 273.(CONSIDERED A MAJOR REPAIR)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 65,499 hrs · 23,522 cycles

DURING HEAVY MAINTENACE: CORROSION ANGLE WEB FLOOR STRUCTURE BTW FR69/FR70 AT LEVEL STR23R AFT GALLEY AREA (1 EA) (CPCP RELATED REFER TO MPD TASK 534195-01); REF AEROMAN N/R 2023-692365 WO 2023 360/1, REMOVED AND REPLACED WEB LOC ON FLOOR STRUCTURE BETWEEN FR69 TO FR70 AT LEVEL STR 23R AFT GALLEY AREA I.A.W A320 SRM 51-72-11 COMPLETED BY J. ALVAREZ 15413 CHECKED BY RII I. GARCIA QC 273. (CONSIDERED A MAJOR REPAIR)

Part: FRAME — CRACKED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 (I/B AND O/B POSITIONS) AT THE OVERWING EMERGENCY EXIT HATCH (AFT RH EEH DOOR 844) L= 0.232 INCH APPROX; REF: ARM W/O 2022 3/1 N/R 2022-163377 EMP# 8610118 CHECKED BY 8603209 PERFORMED REINFORCED DOOR STRUCTURE MODIFICATION OF EMERGENCY DOOR 834 IAW EC NO. A320-52-1144. (SUPPLEMENTAL TO THE JASC/ATA CODE)

Part: FRAME — CRACKED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 (I/B AND O/B POSITIONS) AT THE OVERWING EMERGENCY EXIT HATCH (AFT LH EER DOOR 834) L= 0.157 INCH APPROX; REF: ARM W/O 2022 3/1 N/R 2022-163379 EMP# 8610118 CHECKED BY 8603209 PERFORMED REINFORCE DOOR STRUCTURE MODIFICATION OF EMERGENCY DOOR 834 IAW EC NO. A320-52-1144.

Part: SHEAR TIE — CORRODED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC BTW STR 43R AND STR 44 AT LEVEL OF FRAME 32 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 3/2 N/R 2022-163468 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231060.

Part: SHEAR TIE — CORRODED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC BTW STR 43L AND STR 44 AT LEVEL OF FRAME 31 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 3/1 N/R 2022-163473 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231058.

Part: FRAME — CRACKED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 (I/B AND O/B POSITIONS) AT THE OVERWING EMERGENCY EXIT HATCH (FWD RH EEH DOOR 843) L= 0.236 INCH APPROX; REF: ARM W/O 2022 3/1 N/R 2022-163377 EMP#86101118 CHECKED BY 8603209 PERFORMED REINFORCED DOOR STRUCTURE MODIFICATION OF EMERGENCY DOOR 843 IAW EC NO A320-52-1144.

Part: SHEAR TIE — CORRODED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC. BTW STR 43L AND STR 44 AT LEVEL OF FRAME 32 IN FWD CARGO COMPARTMENT; REF: ARM 2022 3/1 N/R 2022-163469 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231060.

Part: SHEAR TIE — CORRODED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC BTW STR 43R AND STR 44 AT LEVEL OF FRAME 33 IN FWD CARGO COMPARTMENT; REF: ARM W/0 2022 3/1 N/R 2022-163466 EMP# 901069 CHECKED BY 8601415 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231062.

Part: SHEAR TIE — CORRODED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC. BTW STR 43R AND STR44 LEVEL OF FRAME 33 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 3/1 R/R 2022-163466 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231062.

Part: FRAME — CRACKED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CRACK INDICATIONS WERE FOUND IN FRAME SEGMENT 1 (I/B AND O/B POSITIONS) AT THE OVERWING EMERGENCY EXIT HATCH (FWD LH EEH DOOR 833) L= 0.152 INCH APPROX; REF: ARM W/O 2022 3/1 N/R 2022-163378 EMP# 8610118 CHECKED BY 8603209 REFORMED REINFORCED DOOR STRUCTURE MODIFICATION OF EMERGENCY DOOR 833 IAW EC A320-52-1144.

Part: SHEAR TIE — CORRODED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC BTW STR 42R AND STR 43R AT LEVEL OF FRAME 29 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022 3/1 NR 2022-0163472 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11, SRM 51-42-11, DWG D53232542000 AND DWG D53230319000.

Part: FRAME — NONE · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, REF JB A5109057-04-JB. AGING AIRCRAFT PROGRAM. EXITING REPAIR EVALUATION LOC FR27 TO FR28 BTW STR 38R TO 42R AT LOWER FUSELAGE; REF AEROMAN WO 2022 3/1, NR 2022-163236. PERFORMED PERM REPAIR IAW JB EC A22-258-01.

Part: SHEAR TIE — CORRODED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, CORROSION SHEAR TIE LOC. BTW STR 43R AND STR 44 AT LEVEL OF FRAME 32 IN FWD CARGO COMPARTMENT; REF: ARM W/O 2022-3/1 2022-163468 REMOVED AND REPLACED CLEAT IAW A320 SRM 51-72-11 AND DWG D53232542000 AND E53231060.

Part: DOUBLER — DAMAGED · airframe 59,859 hrs · 21,375 cycles

DURING HEAVY MAINTENANCE, ( A22-258-01) FUSELAGE / FWD FUSELAGE / FR 27-28 & STR 38R-42R / EXISTING DOUBLER REPAIR – PERMANENT APPROVAL FOR WV 17. (CONSIDERED AS A MAJOR REPAIR)

Part: RECEIVER — FAILED (40RT1) · airframe 58,892 hrs · 21,015 cycles

FLT 1239, LAS-CUN(DIVERTED TO TPA). GPS PRIMARY LOST IN FLIGHT ; T/S PER TSM 34-52-00-810-847-A. MMR 1& 2 TEST GOOD. ATC 1 & 3 TEST GOOD. GPS VISIBILITY GOOD. R&R MMR1 AS PRECAUTION IAW AMM 34-36-31. BITE TEST GOOD. NO FAULTS NOTED @ THIS TIME

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 55,505 hrs · 19,824 cycles

FLT 1382, IAH-JFK. PER TASK CARD A320-33-51-00-710-003 PERFORMED TEST ESPU BATTER FIN 13WL AFT FAIL. R & R ESPU BATTERY AT FIN 13WL AFT, IAW AMM 33-51-38.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 55,505 hrs · 19,824 cycles

FLT 1382, IAH-JFK. PER TASK CARD A320-33-51-00-710-003 PERFORMED TEST ESPU BATTERY FIN 10WL FWD FAIL. R & R ESPU BATTERY AT FIN 10WL FWD, IAW AMM 33-51-38. OPERATIONS CHECK GOOD.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 51,854 hrs · 18,471 cycles

DURING HEAVY MAINTENANCE, REPORTED THAT DURING THE ACCOMPLISHMENT OF THE REF /3/ SB FOR INSPECTION OF THE TI- ANGLES BETWEEN THE BELLY FAIRING & KEEL BEAM SIDE PANEL (AS REQUIRED BY THE REF /4/ AD)– THAT ON THE RT SIDE THE TI-ANGLE AT FR 41-42 AND SHEAR PLATE WAS CRACKED. PER THE REF /3/ SB & REF /4/ AD INSTRUCTIONS – THIS CRACKED ANGLE WAS REPLACED, BUT DUE TO THE CRACK IN THE SHEAR PLATE WAS CONTACTED FOR FURTHER INSTRUCTIONS. PROVIDED THE REF /3/ TD – WHICH PROVIDES INSTRUCTIONS TO PERFORM CUTOUT IN THE SHEAR PLATE TO REMOVE THE CRACK DAMAGE, PERFORM NDT INSPECTIONS, MANUFACTURE AND INSTALL DOUBLER/FILLER, AND RESTORE SURFACE PROTECTION. ALL OTHER REQUIREMENTS OF THE REF /3/ SB AND REF /4/ AD REMAIN AND MUST BE COMPLETED. PROVIDED THE REF /2/ RDAS WHICH APPROVES THESE REPAIR INSTRUCTIONS, WITH A 6 MONTH LIMITATION FOR FURTHER DAMAGE TOLERANCE ANALYSIS (DTA) TO BE ACCOMPLISHED. THIS EC ACCOMPLISHES THE PERMANENT REPAIR PER THE REF /1/ EA AND COMPLIES WITH REF /2/ RDAS WITHOUT DEVIATION. THIS EC A19-519-01 PROVIDES THE TIME LIMITED REPAIR INSTRUCTIONS. EC A19-519-02 IS ISSUED TO TRACK THE DTA, DUE WITHIN 6 MONTHS FROM REPAIR ACCOMPLISHMENT; THIS TIME LIMITED REPAIR HAS BEEN APPROVED VIA REF /2/ RDAS, IS VALID FOR 6 MONTHS, AND IS CLASSIFIED AS MAJOR.

Part: UNKNOWN — MALFUNCTIONED (FUEL SYSTEM) · airframe 51,371 hrs · 18,248 cycles

FLT 170, FLL-BOS. DIVERTED TO JFK. OUTER TANK TO INNER TANK TRANSFER VALVE INOP ( INTER CELL TRANSFER VALVES-LH WING-BOTH LATCH CLOSED ); PERFORMED OPERATIONAL TEST OF INDIVIDUAL TRANSFER VALVES IAW AMM 28-15-00-710-002A WITH NO FAULTS NOTED. ALL INTERCELL TRANSFER VALVES AT L & R WINGS PERFORMED WITHOUT FAILURE OF ANY KIND. MX-4 UPDATED PLACARD REMOVED.

Part: BATTERY — FAILED (CABIN) · airframe 49,030 hrs · 17,397 cycles

DURING HEAVY MAINTENANCE, EPSU BATRERY PACKS 10WL, 11WL, 12WL, 13WL FAILED OPERATIONAL CHECK; REF IAC N/R 13147-5802, R&R EPSU BATTERIES IAW AMM TASK 33-51-38-000-002, 33-51-38-400-002 OPS CHECK GOOD. 10WL: P/N OFF & ON 3214-31, S/N OFF 781924, S/N ON 811574 11WL :P/N OFF & ON 3214-31, S/N OFF 052637, S/N ON 838999 12WL : P/N OFF &ON 3214-31, S/N OFF 780620, S/N ON 834596 13WL : P/N OFF &ON 3214-31, S/N OFF 777451, S/N ON 834607.

Part: BATTERY — FAILED (CABIN) · airframe 49,030 hrs · 17,397 cycles

DURING HEAVY MAINTENANCE, EPSU BATRERY PACKS 10WL, 11WL, 12WL, 13WL FAILED OPERATIONAL CHECK; REF IAC N/R 13147-5802, R&R EPSU BATTERIES IAW AMM TASK 33-51-38-000-002, 33-51-38-400-002 OPS CHECK GOOD. 10WL: P/N OFF & ON 3214-31, S/N OFF 781924, S/N ON 811574 11WL :P/N OFF & ON 3214-31, S/N OFF 052637, S/N ON 838999 12WL : P/N OFF &ON 3214-31, S/N OFF 780620, S/N ON 834596 13WL : P/N OFF &ON 3214-31, S/N OFF 777451, S/N ON 834607.

Part: BATTERY — FAILED (CABIN) · airframe 49,030 hrs · 17,397 cycles

DURING HEAVY MAINTENANCE, EPSU BATRERY PACKS 10WL, 11WL, 12WL, 13WL FAILED OPERATIONAL CHECK; REF IAC N/R 13147-5802, R&R EPSU BATTERIES IAW AMM TASK 33-51-38-000-002, 33-51-38-400-002 OPS CHECK GOOD. 10WL: P/N OFF & ON 3214-31, S/N OFF 781924, S/N ON 811574 11WL :P/N OFF & ON 3214-31, S/N OFF 052637, S/N ON 838999 12WL : P/N OFF &ON 3214-31, S/N OFF 780620, S/N ON 834596 13WL : P/N OFF &ON 3214-31, S/N OFF 777451, S/N ON 834607.

Part: BATTERY — FAILED (CABIN) · airframe 49,030 hrs · 17,397 cycles

DURING HEAVY MAINTENANCE, EPSU BATRERY PACKS 10WL, 11WL, 12WL, 13WL FAILED OPERATIONAL CHECK; REF IAC N/R 13147-5802, R&R EPSU BATTERIES IAW AMM TASK 33-51-38-000-002, 33-51-38-400-002 OPS CHECK GOOD. 10WL: P/N OFF & ON 3214-31, S/N OFF 781924, S/N ON 811574 11WL :P/N OFF & ON 3214-31, S/N OFF 052637, S/N ON 838999 12WL : P/N OFF &ON 3214-31, S/N OFF 780620, S/N ON 834596 13WL : P/N OFF &ON 3214-31, S/N OFF 777451, S/N ON 834607.

Part: DOOR SILL — CORRODED (FRAME 61) · corrosion level 2 · airframe 45,649 hrs · 16,085 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR LOWER SILL FRAME 61 + 19. REPAIRED THE DOOR SILL IAW EC A17-1084-01.

Part: DOOR SILL — CORRODED (FRAME 61) · corrosion level 2 · airframe 45,649 hrs · 16,085 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR LOWER SILL FR 61 + 9"; REPAIRED SILL IAW EC A17-1084-01.

Part: DOOR SILL — CORRODED (FRAMES 61-62) · corrosion level 2 · airframe 45,649 hrs · 16,085 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON BULK CARGO DOOR SILL FRAME 61 TO 62. REPAIRED THE DOOR SILL IAW EC A17-1084-01.

Part: SEAT TRACK — CORRODED (FRAME 44) · corrosion level 2 · airframe 45,649 hrs · 16,085 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED THE SEAT TRACK, FR 44 + 12, -Y765. REPLACED THE SEAT TRACK IAW SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FRAME 16) · corrosion level 2 · airframe 45,649 hrs · 16,085 cycles

DURING HEAVY MAINTENANCE, CORROSION WAS DISCOVERED ON THE DUMMY RAIL Y503.2, FRAME 16 IN THE FWD GALLEY AREA. REPLACED THE DUMMY RAIL.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 41,226 hrs · 14,413 cycles

FLT 365 SMF-LGB. DURING A MAINTENANCE INSPECTION, THE OVERHEAD EMERGENCY LIGHT WAS DISCOVERED TO BE INOPERATIVE AT ROW 18. LIGHT ASSEMBLY WAS FOUND TO BE DISCONNECTED. REINSTALLED CONNECTOR, OPS CHECK PASSED. SUPPLEMENTAL INFORMATION TO FOLLOW.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 38,618 hrs · 13,487 cycles

FORWARD LT EMERGENCY LIGHT BATTERY FAILED CAP TEST. REPLACED BATTERY FIN 10WL IAW AMM 33-50-00, GROUND CHECKS OK.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 37,503 hrs · 13,085 cycles

DURING WEEKLY CHECK, EMERGENCY LIGHTS ON RT OVERWING EXIT FAILED. REMOVED RT SIDE OVERWING BATTERY ON THE EPSU AND PERFORMED OPS TEST IAW 33-51-38.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 34,952 hrs · 12,173 cycles

ON MAINTENANCE CHECK FOUND ROW 1 ABC EMERGENCY LIGHT INOPERATIVE. R & R HARNESS TO LIGHT ASSY IAW AMM 33-51-19. OPS CHECK GOOD.

Part: COMPUTER — FAILED (FLAPS) · airframe 32,947 hrs · 11,527 cycles

FLIGHT CONTROL FLAPS LOCKED WING TIP BRAKE ON DESCENT. R & R APU AND PERFORMED CHECKS IAW AMM 27-51-00, OPS CHECKED NORMAL.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 32,720 hrs · 11,454 cycles

DURING FINAL APPROACH, SELECTED FLAPS 2 AND RECEIVED A F/CTRL FLAPS LOCKED WING TIP BRAKE ON ECAM. ACCOMPLISHED FLAPS/SLATS SYS RESET IAW AMM 27-50-00. NO FAULTS NOTED ON FLAP/SLATS, OPS CHECK NORMAL.

Part: SLIDE — MISREPAIRED (OVERWING) · airframe 32,096 hrs · 11,258 cycles

DISCREPANCY ON THE OVERWING SLIDE. DURING THE SCHEDULED RESTORATION OF OVERWING SLIDE, IT WAS FOUND THAT A VACUUM ADAPTER TOOL WAS STILL ATTACHED TO THE SLIDE ASPIRATOR. TOOL SHOULD HAVE BEEN REMOVED DURING THE FOLDING/PACKING PROCESS.

Part: RELEASE CABLE — FAILED (EVAC SLIDE) · airframe 21,796 hrs · 7,711 cycles

ON HEAVY MAINTENANCE CHECK FOUND RT EMERGENCY EXIT SLIDE RELEASE CABLE FAILED OPS CHECK. REPLACED CABLE AS PER TASK CARD A320-1227-02.

Part: RELEASE CABLE — FAILED (EVAC SLIDE) · airframe 21,796 hrs · 7,711 cycles

ON HEAVY MAINTENANCE CHECK FOUND LT EMERGENCY EXIT SLIDE RELEASE CABLE FAILED OPS CHECK. REPLACED CABLE AS PER TASK CARD A320-53-1227-01.

Part: PRESSURE SWITCH — LEAKING (HYDRAULIC SYS) · airframe 21,700 hrs · 7,674 cycles

FLT 830 SDQ-JFK, CREW DECLARED EMERGENCY AND AIRCRAFT DIVERTED TO SJU DUE TO AT CRUISE OF 34000, RECEIVED A GREEN HYD RESERVOIR LEVEL LOW ECAM INDICATING A LOSS OF GREEN HYD FLUID. THE TECHNICIAN REMOVED AND REPLACED NR 1 ENGINE HYD PRESSURE SWITCH IAW AMM 29-11-17.

Part: CONTROL HANDLE — DAMAGED (MLG) · airframe 2,694 hrs · 936 cycles

FLT 61, AFTER TAKEOFF SYR TO JFK, GEAR FAILED TO RETRACT. GEAR HANDLE WOULD NOT MOVE. GEAR HANDLE PANEL DISPLACED OUT APPRROX .5 INCH. ACCOMPLISHED TSM 32-31-00-30-885. LANDING GEAR RETRACTION/EXTENSION DONE 4 TIMES. NO FAULT NOTED. NO FAULT FOUND ON PFR FAULT REPORT. FOUND L/G CONTROL LEVER UNIT DISPLACED. INSPECTED CONNECTOR & REINSTALLED L/G CONT LEVER UNIT. OPS CHECK NORMAL PER 32-31-71-00-001. OK FOR SERVICE.

Part: CONTROL LEVER — FAULTY (COCKPIT) · airframe 2,540 hrs · 883 cycles

FLT 937, ORD-LGB, ON TAKEOFF SELECTED GEAR HANDLE UP, WOULD NOT MOVE. LEFT GEAR DOWN. RETURNED TO ORD. REMOVED AND REPLACED LANDING GEAR CONTROL LEVER IAW 32-31-11-04. SYSTEM OPS CHECK GOOD.