N287AY

Part: HINGE — WORN (LT MLG DOOR) · airframe 26,560 hrs · 4,215 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT MAIN GEAR CENTER HINGE DOOR MOUNT BRACKET WORN. REPLACED BRACKET PER CMM 32-12-61-440-019-A01.

Part: AIR DATA MODULE — UNRELIABLE (NR 1) · airframe 25,860 hrs · 4,122 cycles

AIRCRAFT WAS GROUNDED: FLIGHT AIR RETURNED TO CLT ON ACCOUNT OF NAVIGATION DISAGREE. EMERGENCY WAS DECLARED. SATCOM 1 & 2 WOULD RECEIVE BUT NOT TRANSMIT. ALL 3 ACP'S WERE ATT EMPTED. WORKED INTERMITTENTLY THEN FAILED AGAIN. DURING DEPARTURE AND CLIMBOUT FD 1 & FD 2 SHOWED DIFFERENT COMMANDS NAV ACCURACY CHECKED PERFORMED WHICH SHOWED FD2 TO BE ACCURATE. DURING TAXI OUT AND CLIMB NAV FM/GPS POSITION DISAGREE ECAM MESSAGE APPEARED MULTIPLE TIME. NAV ACCURACY DEGRADED TO LOW THEN RESET BACK TO HIGH. MAINTENANCE PERFORMED OPERATIONAL TEST AND BITE TEST FOR SATCOM 1 & 2 AND FOR TRANSMIT & RECEIVE IAW AMM 23-28-00. OPS CHECK GOOD. RESET FMGEC 1 & 2 IAW TSM 24-0-00. OPS CHECK GOOD FOR FMGEC 1 & 2. BITE TEST GOOD FOR FMGEC 1 & 2, AND FD 1 & 2. PERFORMED SATISFACTORY LAND CAT III CAPABILITY TEST IAW AMM 22-97-00. REMOVED AND INSTALLED #1 ADIRU IAW AMM 34-12-34-0401., TEST OK. ACCOMPLISHED TSM 34-36-00-810-897A/22-13-00-810-801A, PERFORMED AFS/LAND TEST OK IAW AMM 22-96-00-0501/22-97-00-0501.

Part: SIGN — DETACHED (CABIN) · airframe 25,545 hrs · 4,079 cycles

AIRCRAFT WAS NOT GROUNDED: 2L BOARDING DOOR EXIT SIGN WAS DETACHED. MAINTENANCE RESECURED EXIT SIGN PER STANDARD PRACTICES.

Part: CONNECTOR — UNLOCKED (EMERGENCY LIGHT) · airframe 23,722 hrs · 3,814 cycles

MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AFT OF THE L2 DOOR WAS INOPERATIVE. FOUND GALLEY MODULE WITH AN ELECTRICAL CONNECTOR NOT LOCKED. SECURED THE CONNECTOR AND VERIFIED LOCKED. OPS TESTED OKAY IAW AMM 31-51-00-501.

Part: ANGLE — CORRODED (FRAME 76) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON THE ANGLE) AT FRAME 76, STRINGER 26R. REPLACED THE ANGLE IAW SRM 51-72-11, AND DWG F53479335.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 22,968 hrs · 3,659 cycles

BROKEN FLOOR PANEL 242MF BETWEEN FRAMES 31 AND 33, -Y1456 TO -Y1522.5. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARAGRAPH 2, FIGURE 20109.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 22,968 hrs · 3,659 cycles

AIRCRAFT WAS IN BASE MAINTENANCE. DELAMINATED FLOOR PANEL 161CF IN BULK CARGO COMPARTMENT. REPAIRED FLOOR PANEL PER SRM 53-02-00-300-016.

Part: FLOORBEAM — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON FLOOR SUPPORT BETWEEN FRAMES 73 - 74. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING F53478040.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION WAS FOUND ON THE SEAT TRACK BETWEEN FRAMES 73 TO 74, +YC1. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DWG F53478018.

Part: THRESHOLD — CORRODED (FRAMES 73A-75A) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON THE THRESHOLD, BETWEEN FRAMES 73A TO 75A LT SIDE. REPLACED THE THRESHOLD IAW SRM 51-72-11, AND DWG F53479335.

Part: SEAT TRACK — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 73 - 74. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53478007.

Part: SEAT TRACK — CORRODED (FRAMES 71-73) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON THE SEAT TRACK, FRAMES 71+10 TO 73+12, +YB IN THE AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DWG F53478100.

Part: ADAPTER — CORRODED (FRAMES 73-74) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON SEAT TRACK ADAPTER, FRAMES 73 - 74. REPLACED THE ADAPTER IAW 51-72-11, AND DRAWING F53478018.

Part: SEAT TRACK — CORRODED (FRAMES 31-35) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 31-35 IN THE PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DRAWING F53275877.

Part: SEAT TRACK — CORRODED (FRAME 33) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION ON THE SEAT TRACK, -Y1456, FRAME 33. REPAIRED THE SEAT TRACK IAW SRM 53-21-15-300-002, PAR 2A, FIG 20102.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 22,968 hrs · 3,659 cycles

DELAMINATION FOUND ON FLOOR PANEL 272JF IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW EA 286929, SRM 53-02-00-300-009, AND IRM 9701, REVISION I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 22,968 hrs · 3,659 cycles

DELAMINATION FOUND ON FLOOR PANEL 272HF, BETWEEN FRAMES 72 - 77. REPLACED THE FLOOR PANEL IAW EA 286929, SRM 53-02-00-300-009, AND IRM 9701, REVISION I.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 22,968 hrs · 3,659 cycles

FLOOR PANEL 232KG WAS CRACKED FROM FRAMES 25 TO 29, Y-1959 TO Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2, FIGURE 20109, AND IRM 9701 REV.I.

Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 22,968 hrs · 3,659 cycles

DELAMINATION FOUND ON FLOOR PANEL 272KF, FRAMES 72 TO 77, -YA -TC, IN THE AFT GALLEY AREA. FABRICATED AND INSTALLED A NEW FLOOR PANEL IAW EA 286929, SRM 53-02-00-300-009, AND IRM 9701, REV I.

Part: SEAT TRACK — CORRODED (FRAMES 25-37) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 25+12 - 37.4+12. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DRAWINGS F53328090, AND F5397939.

Part: SEAT TRACK — CORRODED (FRAMES 31-35) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 31 - 35.

Part: SEAT TRACK — CORRODED (FRAMES 38-39) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 38-39.2 IN THE PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53311114.

Part: SEAT TRACK — CORRODED (FRAMES 47-53) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 47 - 53.2 IN THE PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-42-11, 51-72-11, DRAWING F53325687 AND F53325686.

Part: SEAT TRACK — CORRODED (FRAMES 26-37) · corrosion level 2 · airframe 22,968 hrs · 3,659 cycles

CORROSION FOUND WAS ON THE SEAT TRACK, FRAMES 26 - 37.4+9", Y1959. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DWG F53276421.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 22,443 hrs · 3,583 cycles

WHILE ACCOMPLISHING JC 33C22033002, THE L1 DOOR EMERGENCY LIGHT POWER SUPPLY BATTERY FAILED. MAINTENANCE REPLACED THE BATTERY AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: PROFILE — WORN (ZONE 100) · airframe 21,457 hrs · 3,444 cycles

DURING CCC VISIT, EDGE CHAFING WAS FOUND COMMON TO THE BULK CARGO DOOR LOWER AFT CORNER PROFILE. THE AIRCRAFT WAS GROUNDED. REPLACED THE PROFILE IAW EA 279851D, AND DRAWING A523,78040.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,237 hrs · 3,414 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND FLASHLIGHT AT DOOR 4R INOPERABLE. MAINTENANCE REPLACED FLASHLIGHT AT DOOR 4R WITH SERVICEABLE UNIT AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,510 hrs · 3,139 cycles

EMERGENCY LIGHT IN AISLE ABOVE THE L3 DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT.

Part: BOTTLE — LOW PRESSURE (L4 DOOR ASSIST) · airframe 19,376 hrs · 3,116 cycles

L4 DOOR BOTTLE PRESSURE LOW. SERVICED DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 18,789 hrs · 3,021 cycles

L4 DOOR DAMPER EMERGENCY CYLINDER HAD LOW PRESSURE. SERVICED L4 DOOR CYLINDER.

Part: CYLINDER — LOW PRESSURE (L4 DOOR) · airframe 18,575 hrs · 2,987 cycles

4L DOOR ASSIST BOTTLE PRESSURE IN THE YELLOW ON GAGE. SERVICED 4L DOOR ASSIST BOTTLE IAW AMM.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 17,725 hrs · 2,868 cycles

L4 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED THE ASSIST BOTTLE.

Part: LENS — DETACHED (EXIT SIGN) · airframe 17,451 hrs · 2,828 cycles

AIRCRAFT WAS NOT GROUNDED. EXIT SIGN COVER DETACHED FROM BASE. REATTACHED EXIT SIGN AT DOOR L1.

Part: LIGHT — LOOSE (L3 DOOR) · airframe 17,088 hrs · 2,774 cycles

L3 EXIT SIGN LOOSE AND A SCREW MISSING. REPLACED LIGHT FRAME ASSY.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 16,470 hrs · 2,688 cycles

EMERGENCY LIGHT BATTERY FAILED AT DOOR 4. REPLACED THE BATTERY. AIRCRAFT WAS GROUNDED.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 16,316 hrs · 2,667 cycles

EXIT SIGN COVER FELL OFF NEAR SEAT 23C. REINSTALLED COVER.

Part: SMOKE WARNING — FALSE INDICATION (LAVATORY) · airframe 15,964 hrs · 2,599 cycles

LAVATORY SMOKE ECAM ACTIVATED. FOLLOWED ECAM PROCEDURES AND FOUND NO EVIDENCE OF SMOKE. PERFORMED BSCU BITE WITH NO FAULTS.

Part: ACTUATOR — FAILED (FUEL TRIM) · airframe 15,508 hrs · 2,482 cycles

TRIPPED FUEL TRIM TANK INLET VALVE M61 CIRCUIT BREAKER. MAINTENANCE REPLACED TRIM TANK FUEL INLET VALVE ACTUATOR IAW AMM 28-27-52.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 14,997 hrs · 2,389 cycles

EMERGENCY POWER SUPPLY UNIT FAILS TEST. REPLACED THE BATTERY AT 15WL IAW 33-51-38-401.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 14,997 hrs · 2,389 cycles

EMERGENCY POWER SUPPLY UNIT FAILS TEST. REPLACED BATTERY AT 18WL IAW 33-51-38-401.

Part: GAUGE — UNKNOWN (L4 DOOR SLIDE) · airframe 14,997 hrs · 2,389 cycles

CIDS FAP SHOWS CHECK SLIDE PRESSURE ON THE L4 DOOR. DOOR SLIDE PRESSURE IN OPERATIONAL LIMITS. CHECKS OK AT GAUGE ON SLIDE. REPLACED THE L4 DOOR ESCAPE SLIDE IAW TASK CARD 33L00025001 AND FAULT MESSAGE CLEARED.

Part: LIGHT — BROKEN (SEAT 1H) · airframe 14,249 hrs · 2,248 cycles

PASSENGER SEAT 1H EMERGENCY LIGHT HAS BROKEN CONTACT PIN. REPLACED LIGHT IAW AMM 33-51-12-00-814-A, AMM 33-51-12-400-814-A AND ACCOMPLISHED SATISFACTORY CHECK.

Part: DIAPHRAGM — BLOWN (R4 DOOR) · airframe 14,631 hrs · 2,297 cycles

AIRCRAFT IN BASE MAINTENANCE. LOW PRESSURE ON 4R DOOR ASSIST BOTTLE, CAUSED BY BLOWN DIAPHRAGM. REMOVED AND REPLACED R4 DOOR ASSIST BOTTLE DIAPHRAGM IAW AMM 52-10-00-860-803-A. SERVICED BOTTLE IAW AMM 52-10-00-600-802-A. LEAK CHECK GOOD.

Part: LENS — UNSECURE (CABIN) · airframe 13,087 hrs · 2,093 cycles

AIRCRAFT WAS NOT GROUNDED: 3L EXIT LIGHT LENS IS NOT SECURED. RE-SECURED EXIT SIGN LENS AT 3L AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — MISSING (CABIN) · airframe 12,605 hrs · 2,017 cycles

AIRCRAFT WAS GNDED. LENS COVER EMER EXIT MISSING AT L3 DOOR. INSTALLED NEW LENS COVER AT L3 DOOR EXIT SIGN IAW AMM 33-51-11.

Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 12,025 hrs · 1,909 cycles

AIRCRAFT WAS NOT GNDED. ESPRESSO MAKER NR 2 SMELLS LIKE ELEC SMOKE WHEN IN USE. REPLACED ESPRESSO MAKER NR 2 & ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK IAW AMM 25-35-15-000-802-A & 25-35-15-400-802-A.

Part: SIGN — BROKEN (CABIN) · airframe 11,925 hrs · 1,880 cycles

AIRCRAFT WAS NOT GNDED. EXIT SIGN ON CEILING AT 3R BROKEN. INSTALLED NEW EXIT SIGN.

Part: AIR FILTER — DEFECTIVE (CABIN) · airframe 11,782 hrs · 1,842 cycles

AIRCRAFT WAS GNDED. FLIGHT ATTENDANT REPORTED A STRONG ODOR IN THE FWD CABIN DURING TAKEOFF & LANDING THAT CAUSED BURNING EYES, IRRITATED THROAT & A METALLIC TASTE IN THE FLIGHT ATTENDANTS MOUTH. ACCOMPLISHED JC 33L00021001 REPLACED TWO EACH OVENS & ALL 8 HEPA FILTERS IAW AMM 25-35-19 & 21-21-41. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. PLEASE SEE AALA201602229002 FOR ADDITIONAL PART.

Part: OVEN — DEFECTIVE (GALLEY) · airframe 11,782 hrs · 1,842 cycles

AIRCRAFT WAS GNDED. FLIGHT ATTENDANT REPORTED A STRONG ODOR IN THE FWD CABIN DURING TAKEOFF & LANDING, THAT CAUSED BURNING EYES, IRRITATED THROAT & A METALLIC TASTE IN THE FLIGHT ATTENDANTS MOUTH. ACCOMPLISHED JC 33L00021001, REPLACED 2 EACH OVENS & ALL 8 HEPA FILTERS IAW AMM 25-35-19 & 21-21-41. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK. PLEASE SEE AALA 201602229003 FOR ADDITIONAL PART.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,709 hrs · 1,824 cycles

AIRCRAFT WAS NOT GNDED. EMER CEILING LIGHT AFT RT INOPERATIVE. REPLACED EMER LIGHT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — ODOR (CABIN) · airframe 11,621 hrs · 1,809 cycles

AIRCRAFT WAS GNDED. AFTER TOP OF DESCENT AT 40 MINUTES FROM DESTINATION. FLIGHT ATTENDANTS REPORTED ELEC SMELL THROUGHOUT CABIN. ACCOMPLISHED JC 33L00021001 TROUBLESHOOT CABIN AIR QUALITY. ACFT OK FOR SERVICE.

Part: SIGN — BROKEN (CABIN) · airframe 10,803 hrs · 1,644 cycles

OVERHEAD EXIT SIGN AT ROW 23 AC RT IS BROKEN. REPLACED EXIT SIGN & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-17.

Part: SIGN — OUT OF ADJUST (CABIN) · airframe 8,925 hrs · 1,393 cycles

ROW 22 EMER EXIT SIGN NEEDS ADJUSTED. R & R EMER EXIT LIGHT IAW TASK 33-51-11.

Part: LENS — MISSING (CABIN) · airframe 6,917 hrs · 1,080 cycles

BULKHEAD WALL AT 23F WHITE COVER FOR EMER LIGHT ON WALL IS MISSING. INSTALLED LENS COVER ON EXIT SIGN AT 23F. OK FOR SERVICE.

Part: RELAY — INOPERATIVE (CABIN) · airframe 6,854 hrs · 1,072 cycles

EXIT SIGNS DID NOT ILLUMINATE ON TAXI OUT OR WHEN GEAR CAME DOWN FOR LANDING. REPLACED RELAY AT 8WL PANEL 751VU. SYS CHECKED GOOD.

Part: COVER — BROKEN (CABIN) · airframe 6,368 hrs · 981 cycles

EMERGENCY EXIT LIGHT BROKEN AT DOOR 3L. REINSTALLED LIGHT COVER AT 3L. OK FOR SERVICE.

Part: SIGN — LOOSE (CABIN) · airframe 6,358 hrs · 980 cycles

EXIT SIGN 3L IS DOWN. SECURED 3L EXIT SIGN.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 5,468 hrs · 860 cycles

AFT RT FLIGHT ATTENDANT EMER FLASHLIGHT INOPERATIVE. REPLACED EMER FLASHLIGHT BATTERY AT AFT RT FLIGHT ATTENDANT STATION. CHECKED OKAY.

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 5,193 hrs · 826 cycles

DOOR 1LT SHOWS CHECK PRESS ON FLIGHT ATTENDANT PANEL. ACCOMPLISHED TASK DISCHARGING & CHARGING OF THE DOOR DAMPER & EMER OPERATION CYLINDER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 5,163 hrs · 822 cycles

BATTERY ECPU 16WL FAILED CAPACITY CHECK. REPLACED BATTERY PACK AT 16WL EPCU. OPERATIONAL CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 4,969 hrs · 795 cycles

AFTER TAKEOFF, FLIGHT ATTENDANTS REPORTED ACRID BURNING PLASTIC ODOR IN THE CABIN. ODOR DIMINISHED DURING CLIMB OUT, BUT SOME FLIGHT ATTENDANTS REPORTED MEDICAL ISSUES, DIVERTED. MAINTENANCE ACCOMPLISHED AIR QUALITY CARD WITH NO FAULTS FOUND. ACFT OK FOR SERVICE.

Part: COVER — DETACHED (EXIT SIGN) · airframe 3,992 hrs · 658 cycles

EMERGENCY EXIT SIGN FELL OFF IN MAIN CABIN. REPLACED EMERGENCY EXIT SIGN COVER AT 3L DOOR.

Part: SIGN — DETACHED (CABIN)

EXIT SIGN OVER 3L DOOR COMES APART. MX REATTACHED EXIT SIGN FRAME AT DOOR 3L.

Part: GEARBOX — LEAKING (LE SLAT) · airframe 2,850 hrs · 443 cycles

TEST FLIGHT UNSATISFACTORY, SLIGHT OIL OR HYD SMELL FROM GASPERS DESCENDING THROUGH 18,000', AGAIN AT 10,000' AFTER SPEED BRAKES DEPLOYED. NO ODOR NOTED IN CABIN. FOUND SLAT TEE GEARBOX LEAKING GREASE. R & R SLAT TEE GEARBOX. THE AIR CYCLE MACHINE, CONDENSER & THE REHEATER WERE ALSO R & R.

Part: CONTROLLER — FAULTY (COCKPIT) · airframe 2,841 hrs · 439 cycles

LOUD BUZZING TRANSFORMER LIKE NOISE IN COCKPIT & DEFINITE SMELL OF ELEC SMOKE IN FLIGHT DECK AREA, NOISE NOT NORMAL. MX R & R LIGHT CONTROLLER 2LF.

Part: LAMP — WRONG PART (COCKPIT LIGHT) · airframe 2,242 hrs · 302 cycles

CAPTAIN'S OVERHEAD LIGHT WAS SPARKING ON INITIAL LIGHTING. MAINTENANCE INSTALLED CORRECT LAMPS.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 2,171 hrs · 292 cycles

BREAKAWAY FLASHLIGHT UNDER OTBD F/A JUMPSEAT SEAL BROKEN AND BATTERY DISCHARGED. MAINTENANCE REPLACED BATTERIES AND SEAL AS REQUIRED.

Part: WINDSHIELD — CRACKED (ZONE 100) · airframe 1,098 hrs · 141 cycles

F/O'S EXTERIOR WINDSHIELD CRACKED IN FLIGHT AT FL400 AT APPROX 30W. ALSO ACCOMPANIED BY ECAM ANTI-ICE RT WINDSHIELD HEAT. F/O WINDSHIELD BEGAN ARCHING. WHC2 RESET BREAKER PULLED. MX REPLACED F/O WINDSHIELD AND ALSO WINDOW HEAT CONTROLLER.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 919 hrs · 117 cycles

EMERGENCY EXIT LIGHT COVER MISSING. MX REPLACED COVER AS REQUIRED.

Part: COVER — DETACHED (R3 DOOR) · airframe 802 hrs · 103 cycles

R3 DOOR EMERGENCY LIGHT COVER DETACHED. MX SECURED COVER.