N162UP
Registered owner: UNITED PARCEL SERVICE CO, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED PARCEL SERVICE CO. (IPXA) | Operator | on 2024-10-29 | Operator named in NTSB report |
Accident & incident history
Operated by United Parcel Service Co (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
162 reports on file, 2007-10-19 – 2026-03-16.
Part: WARNING BUZZER — INOPERATIVE (ZONE 800) · airframe 24,889 hrs · 14,869 cycles
BUZZER AND RED LIGHT TO L1 DOOR ESCAPE SLIDE IS INOPERATIVE. PERFORMED OPS CHECK OF L1 DOOR BUZZER AND WARNING LIGHT IAW AMM 52-73-12-0401 AND 52-73-11-0401, OPS CHECKED GOOD. PERFORMED BITE CHECK OF 70WN AUTONOMOUS STANDBY POWER SUPPLY UNIT IAW 52-73-00-0501, BITE CHECK GOOD.
Part: SLIDE — INOPERATIVE (ZONE 800) · airframe 24,889 hrs · 14,869 cycles
BUZZER AND RED LIGHT TO L1 DOOR, ESCAPE SLIDE IS INOPERATIVE. PANELS 831FZ, 831DZ, 831CZ, & 831BZ REMOVED IAW AMM 52-10-13-0401.
Part: PLATE — DAMAGED · airframe 24,889 hrs · 14,869 cycles
HOLES IN REINFORCING PLATE P/N: A57244651203 UNDERLYING STRUCTURE LOOKING FWD FOUND HOLE DIAMETER TO BE AT 0.250" 35(EA) WITH SHORT EDGE DISTANCE (1.5D). IT WAS FOUND OUT OF LIMITS. INSTALLED NEW REINFORCING PLATE P/N A57244651203 IAW SRM 51-40-21-001 AND SRM 57-51-11, FIG. 4.
Part: BRACKET — CRACKED (ZONE 500 K FLAP) · airframe 24,889 hrs · 14,869 cycles
LEFT WING, KRUEGER AREA, OTBD INNER BRACKET HAS A CRACK. INSTALLED NEW ANGLE IAW SRM51-40-21-001.
Part: PRESSURE BLKHD — DENTED (ZONE 100) · airframe 24,889 hrs · 14,869 cycles
MAJOR REPAIR, THROUGH RADOME 110AL, FWD PRESSURE BULKHEAD, ABOVE LOCALIZER ANTENNA RH ATTACHMENT HAS BULGE. DOT 103-25 ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96865-REQ1 AND VT-MAE EA 300-5311-27-A4387, REV. -.
Part: WEB — CRACKED (ZONE 400) · airframe 24,889 hrs · 14,869 cycles
NR 1 ENG, AFT PYLON, INNER BOX, BTWN RIB 19 TO RIB 20, PLATE STRUCTURE AT HYD PRESSURIZATION LINE FITTING CUTOUT HAS A CRACKS (2EA). REMOVED WEB FROM #1 PYLON LOWER SPAR EXTENTION MEMBER UNDER AFT FAIRING IAW SRM 51-40-21-001. INSTALLED SPAR EXTENTION MEMBER AT NR 1 PYLON LOWER AFT, UNDER AFT. FAIRING, DRAIN LINE UNION MOUNT STRUCTURE IAW SRM 51-40-21-001.
Part: BRACKET — CRACKED (ZONE 500) · airframe 24,889 hrs · 14,869 cycles
LH WING, KRUEGER AREA, I/B INNER BRACKET HAS A CRACK. DOT 90-04 VERIFIEDÃÂ NEW BRACKET AT LH WING KRUEGER AREA INSTLLED IAW A300-600 SRM 51-40-21, JOB COMPLETED.
Part: BRACKET — CRACKED (ZONE 600) · airframe 24,889 hrs · 14,869 cycles
RIGHT WING LEADING EDGE INSIDE THE ACCES PANEL 675AB HYD LNES SUPPORT BRACKET BROKEN. INSTALLED NEW BRACKET-MOUNTING AT RT WING LEADING EDGE INSIDE THE ACCES PANEL 675AB, IAW SRM 51-40-21.
Part: BRACKET — CRACKED (ZONE 500) · airframe 24,889 hrs · 14,869 cycles
LEFT WING, ACCESS PANEL 575AB AREA, INNER TOP BRACKET HAS A CRACK. REMOVED BRACKET AT LT WING, ACCESS PANEL 575AB AREA, INNER TOP. IAW SRM-51-40-21. INSTALLED PLATE MOUNTING USING EXISTING FASTENERS, IAW SRM 51-40-21.
Part: BRACKET — CRACKED (ZONE 500) · airframe 24,889 hrs · 14,869 cycles
LH WING, KRUEGER AREA, I/B BRACKET HAS A CRACK. DOT 90-05 VERIFIED NEW BRAKET INSTALLATION IAW SRM 51-40-21 ON LH WING, KRUEGER I/B AREA.
Part: GIMBAL JOINT — CRACKED (THS ACTUATOR) · airframe 24,889 hrs · 14,869 cycles
THS ACTUATOR UPPER GIMBAL IS CRACKED. INSTALLED TAB WASHER IN HINGE ARMS SECTION B-B ITEM (27) IAW AMM 55-16-36-401.
Part: BRACKET — CRACKED (ZONE 600) · airframe 24,889 hrs · 14,869 cycles
UPPER I/B ATTACH ANGLE FITTING CRACKED FROM HOLE TO EDGE-109-028-VWV INSTALLED NEW BRACKET IAW A300-600 SRM 51-40-21-001 AT ZONE 600-632BB UPPER I/B
Part: PROFILE — CRACKED (ZONE 200) · airframe 24,889 hrs · 14,869 cycles
LEFT BTW FR73-76 Z-PROFILE HAS A CRACK. REMOVED Z-PROFILE BTW FR73- FR76 IN ZONE 200 L/H SIDE IAW SRM 53-18-18 AND SRM 51-40-21. INSTALLED L/H BTW FR73-76 Z PROFILE MDC AFT SECTION IAW SRM 51-40-21-001.
Part: PROFILE — CRACKED (ZONE 100) · airframe 24,889 hrs · 14,869 cycles
MDC AFT SECTION RH SIDE, Z PROFILE CRACKED AT FR 74. REMOVED Z-PROFILE BTW FR73- FR76 IN MDC AFT SECTION RT SIDE IAW SRM 53-18-18 AND SRM 51-40-21. INSTALLED RT Z PROFILE MDC AFT SECTION IAW SRM 51-40-21-001.
Part: PROFILE — CRACKED (ZONE 100) · airframe 24,889 hrs · 14,869 cycles
MDC AFT SECTION LT SIDE, Z PROFILE CRACKED AT FR 79. REMOVED Z-PROFILE IN MDC AFT SECTION IAW SRM 53-18-18, AND SRM 51-40-21. INSTALLED THE PROFILE MDC AFT SECTION IAW SRM 51-40-21-001.
Part: UNKNOWN — ODOR (CABIN) · airframe 24,702 hrs · 14,771 cycles
IN DESCENT, BOTH PACKS ON AND ENGINE & WING ANTI ICE ON, AIR FLOW THRU DUCTS WAS VERY LOUD. PACK FLOW INDICATION ON ECAM, BOTH AMBER AND LOW FLOW POSITION. CONDITIONED AIR SMELLED HOT. BOTH TAKEOFF AND LANDING. PERFORMED OPS TEST OF PACKS IAW AMM 21-51-00. NO NOISES OR HOT SMELL FOUND. INSPECTED DUCTS AND FOUND LARGE LEAK ABOVE APU DUCT CHECK VALVE. REPLACED SEAL ABOVE CHECK VALVE IAW AMM 36-12-12/401. OPS AND LEAK TEST GOOD.
Earlier reports · 2007–2025 · 146 reports
2025
Part: SKIN — CRACKED (ZONE 100) · airframe 24,598 hrs · 14,704 cycles
SECTION 18 LOWER SHELL REPLACEMENT AND INTERNAL STRUCTURE REPAIR. VERIFIED THAT REPAIR FOR SECTION 18 DAMAGE DUE TO TAILSTRIKE WAS REPAIRED ACCOMPLISHED ON AIRBUS WORK CARD 7086382 AND AIRBUS REPAIR DRAWING R53970080 ISSUE B. REPAIR THRESHOLD IS TO BE TRACKED ON EO-95446-REQ2.
Part: SKIN — CRACKED (ZONE 100) · airframe 24,598 hrs · 14,704 cycles
SECTION 17 LOWER SKIN SPLICE REPAIR/REPLACEMENT AND INTERNAL STRUCTURE REPAIR. VERIFIED THAT THE DAMAGE TO SECTION 17 DUE TO THE TAIL STRIKE WAS REPAIRED IN ACCORDANCE WITH AIRBUS WORK CARD 7086383 AND AIRBUS REPAIR DRAWINGS R53970076 ISSUE B AND R53970056 ISSUE B. REPAIR THRESHOLD IS TO BE TRACKED ON EO-95625-REQ2.
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 24,598 hrs · 14,704 cycles
SECTION 18 MAIN DECK FLOOR CROSSBEAM REPAIR AT FRAME 76 VERIFIED REPAIR ACCOMPLISHED ON AIRBUS WORK CARD 7086591 PER AIRBUS REPAIR DRAWING R53970070 ISSUE A. REPAIR THRESHOLD IS TO BE TRACKED ON EO-95628-REQ2.
Part: CROSSBEAM — CRACKED (ZONE 200) · airframe 24,598 hrs · 14,704 cycles
SECTION 18 MAIN DECK CROSS BEAM DAMAGED AT FRAME 77 VERIFIED THAT THE DAMAGE DUE TO THE TAIL STRIKE WAS REPAIRED IN ACCORDANCE WITH UPS EO-95641-REQ1, AIRBUS WORK CARD 7088148 AND AIRBUS REPAIR DRAWING R53970074 ISSUE B. REPAIR THRESHOLD IS TO BE TRACKED ON EO-95641-REQ2.
Part: SKIN — DAMAGED (ZONE 100) · airframe 24,598 hrs · 14,704 cycles
FUSELAGE SKIN DAMAGE AT FR80/82 BETWEEN STR44LH AND STR 44RH VERIFIED THAT THE DAMAGE DUE TO THE TAIL STRIKE WAS REPAIRED IN ACCORDANCE WITH UPS EO-95523-REQ1, AIRBUS WORK CARD 7086636 AND AIRBUS REPAIR DRAWING R53970081 ISSUE B. REPAIR THRESHOLD IS TO BE TRACKED ON EO-95523-REQ2.
Part: SKIN — PILOT ERROR (ZONE 100) · airframe 24,598 hrs · 14,704 cycles
TAIL STRIKE EVENT - FUSELAGE AFT INTERMEDIATE SECTION SKIN/STRUCTURE REPLACEMENT/REPAIRS
2024
Part: STRUT — CRACKED (ZONE 200) · airframe 24,598 hrs · 14,704 cycles
)FLOOR BEAM STRUTS BROKEN AT FR 76 THESE ITEMS WERE REPLACED UNDER AIRBUS WORKCARD 7086382-20 AND TIED TO BARCODE T3F18E007T13S WHICH IS THE REPLACEMENT OF THE SECTION 18. ALL WORK CAN BE FOUND ON THAT BARCODE.
Part: STRUT — CRACKED (ZONE 200) · airframe 24,598 hrs · 14,704 cycles
FLOOR BEAM STRUTS BROKEN AT FR 77 THESE ITEMS WERE REPLACED UNDER AIRBUS WORKCARD 7086382-020 AND TIED TO BARCODE T3F18E007T13S WHICH IS THE REPLACEMENT OF THE SECTION 18. ALL WORK CAN BE FOUND ON THAT BARCODE.
Part: SKID — PILOT ERROR (ZONE 100) · airframe 24,598 hrs · 14,704 cycles
TAIL STRIKE C/W TAIL SKID INSPECTION PER AMM 05-51-21/001. FOUND EXTENSIVE DAMAGE TO LOWER FUSELAGE FROM FR70 THROUGH FR80. VERIFIED DFDR DATA WAS ROUTED TO APPROPRIATE PERSONEL. REFERENCE WORK PACKAGE NUMBER 13026706 FOR DOCUMENTED FAULT'S REQUIRING REPAIR.
Part: SKIN — PILOT ERROR (ZONE 100) · airframe 24,598 hrs · 14,704 cycles
SDR FILED OPEN, TAIL STRIKE.
Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 24,577 hrs · 14,692 cycles
**EMERGENCY DECLARED**AT FL370 GOT EMERGENCY DESCENT ECAM CAB ALT ON OVERHEAD AND ECAM INDICATED 9800, CAB RATE APPROX 1000 FPM. PACK 2 WAS THE PACK OPERATING AT THAT TIME. DESCENDED TO 10000, (CONT IN FAULT DESCRIPTION) PERFORMED CABIN PRESSURIZATION AND CONTROL TESTS IAW TSM 21-30-00/101. ALL CHECKS IN FLIGHT DECK OK, ALL 10 POSITIONS OF BOTH CONTROLLERS CHECK OK, NO DISCREPANCIES TO NOTE AT THIS TIME. PER TECH RECOMMENDATION, CHECKED FWD OUTFLOW VALVE FOR SIGNS OF DAMAGE AND OBSTRUCTION, NONE NOTED. PERFORMED DETAILED VISUAL INSPECTION OF ALL CARGO DOOR SEALS AND ENTRY DOOR, NO FINDINGS. PRESSURIZED AIRCRAFT WITH PACK 2 ONLY IAW AMM 21-31-00/501, NO MAJOR LEAKS NOTED, OPS NORMAL. ITEM HAS NO HISTORY, OK FOR CONTINUED SERVICE.
Part: TRIM PANEL — DETACHED (PAX DOOR) · airframe 23,896 hrs · 14,293 cycles
CREW ENTRY DOOR MOULDING HANDLE FELL OFF FOUND CREW ENTRY DOOR ASSIST HANDLE TOP SECTION AND SNAPPED BACK INTO PLACE IAW AMM 52-10-13.
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,477 hrs · 14,033 cycles
FUEL LEAK AT LOWER SURFACE OF L/H WING INBOARD OF ENGINE. POSSIBLE PRIOR CLICK PATCH INSTALL. ISOLATED LEAKING BOLT, INBOARD OF RIB 1 IN CENTER TANK AFT SECTION. PERFORMED REAPAIR INSIDE THE FUEL TANK. DESEALED, CLEANED AND RESEALED I.A.W SRM 51-76-20. FUELED TANK, NO LEAKS NOTED
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,477 hrs · 14,033 cycles
FUEL LEAK AT LOWER SURFACE OF L/H WING INBOARD OF ENGINE. POSSIBLE PRIOR CLICK PATCH INSTALL. FOUND CLICK PATCH CURRENTLY INSTALLED AND FUEL LEAKING PAST IT. FUEL TANK PERMANENT REPAIR REQUIRED PER AMM 28-11-00-801 PARA 2.D.(I).
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,313 hrs · 13,931 cycles
L/H NOTCH FLAP FRAME CRACKED REMOVED NOTCH FLAP UP TO AND INCLUDING AMM 27-87-13 PAGEBLOCK 0401 STEP B.(10). ROUTED TO SHEET METAL FOR DRILLING OF NEW NOTCH FLAP. QC MATCH DRILLED NEW PART IAW A300 SRM 51-00-00. FAILED NOTCH FLAP HANGER INSPECTION DURING RII FOR OK TO INSTALL NOTCH FLAP. OPEN
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 23,313 hrs · 13,931 cycles
*SUPPLEMENTAL SDR* L/H NOTCH FLAP FRAME CRACKED. REMOVED NOTCH FLAP UP TO AND INCLUDING AMM 27-87-13 PAGEBLOCK 0401 STEP B.(10). ROUTED TO SHEET METAL FOR DRILLING OF NEW NOTCH FLAP. COMPLETED REMAINING STEPS OF LEFT NOTCH FLAP REF AMM. 27-87-13-401 AND REINSTALLED NOTCH FLAP ACT. REF AMM. 27-88-15 OPS AND LEAK CKS. GOOD. WITNESSED OPS CHECKS AND VERIFIED CONTROL TRAVEL PER GMM REQUIREMENTS 04-02.
Part: WEB — DENTED (FR 87-88) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:CRH HORIZ. STAB BOX BETWEEN F87-88 STGR R33 WEB HAS A DENT.REPLACED IAW 51-31-00.
Part: WEB — DENTED (FR 85-86) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:CRH HORIZ. STAB BOX BETWEEN F85-86 STGR R33 WEB HAS A DENT.REPLACED IAW 51-31-00.
Part: WEB — DENTED (FR 86-87) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:CLH HORZ STAB BOX FRAME F86 WEB HAS A DENT.REPLACED IAW 51-31-00.
Part: FRAME — CRACKED (485AL) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:CPANEL 485AL HAS A CRACKED FRAME FLANGE.FABRICATED NEW FLANGE IAW SRM 55-55-51.
Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 132MG IS DAMAGED.FABBED PNL 132MG PER SREO A300-5320-16407.
Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131MG IS DAMAGED.FABBED PNL 131MG PER SREO A300-5320-16407.
Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131AH IS DAMAGED.FABBED PNL 131AH PER SREO A300-5320-16407.
Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131GE IS DAMAGED.FABBED PNL 131GE PER SREO A300-5320-16407.
Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131BH IS DAMAGED.FABBED PNL 131BH PER SREO A300-5320-16407.
Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:C*** MAJOR REPAIR *** PNL 131SG IS DAMAGED.FABBED PNL 131SG PER SREO A300-5320-16407.
Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:C*** MAJOR REPAIR *** PANEL 132DE IS DAMAGED.FABBED PNL 132DE PER SREO A300-5320-16407.
Part: FAIRING — CRACKED (413BL) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:CPANEL 413BL HAS A CRACK IN CORNER UNDER THE SEAL.REPAIRED CRACK IAW SRM 54-52-51.
Part: SEAT TRACK — GOUGED (MCD) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*** MAJOR REPAIR *** SEAT TRACK IS GOUGED AT FRAME 80 BL Y794.3.REPAIRED PER RCD 278424.
Part: SUPPORT — CRACKED (FRAME 80) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1CSEAT TRACK WALL SUPPORT IS CRACKED AT FR 80 BL 1173.REMOVED, FABRICATED AND REPLACED IAW SRM 51-40-21.
Part: SEAT TRACK — GOUGED (MCD) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*** MAJOR REPAIR *** SEAT TRACK IS GOUGED AT FRAME 80 BL Y450.REPAIRED PER RCD 278423.
Part: SEAT TRACK — GOUGED (MCD) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*** MAJOR REPAIR *** SEAT TRACK IS GOUGED AT FRAME 80 BL - Y450.REPAIRED PER RCD 278425.
Part: ADAPTER — CORRODED (MCD) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1CCORROSION FOUND ON MAIN DECK CARGO MID SECTION R/H ON CROSS MEMBER BETWEEN PANELS 241TK AND 241KF.REMOVE AND INSTALLED IAW SRM 51-40-21.
Part: SUPPORT — CORRODED (MCD) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C, MAJOR REPAIR CORROSION ON R/H SUPPORT FLANGE AT FR 79 - FR 80.REMOVED, FABRICATED AND INSTALLED IAW SRM 51-40-21.
Part: SEAT TRACK — CORRODED (MCD) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*** MAJOR REPAIR *** R/H SEAT TRACK 2 EA CORRODED AT FR 80.REPAIRED PER RCD 278300.
Part: UNKNOWN — BROKEN (672LB) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1CPANEL 672LB HAS 2 BROKEN CLIPS.REMOVE AND INSTALLED IAW SRM 51-40-21.
Part: FLOORBEAM — CORRODED (MCD) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*** MAJOR REPAIR *** CORROSION AROUND FASTENER HOLE ON FLOOR BEAM AT FR 79.REPAIRED PER RCD 278307.
Part: UNKNOWN — BROKEN (672GM) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1CPANEL 672GB HAS 2 BROKEN CLIPS.REMOVE AND INSTALLED IAW SRM 51-40-21.
Part: SEAT TRACK — CORRODED (MCD) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*** MAJOR REPAIR *** L/H MAIN CARGO COMP FLOOR TRACKS HAS CORROSION AT FR 79 LBL 0-60.REPAIRED PER RCD 278284.
Part: RETAINER — CRACKED (KRUGER FLAP) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1CLH WING KRUEGER FLAP AFT LIP SEAL RETAINER IS CRACKED.REMOVED, FABRICATED AND REPLACED IAW SRM 51-40-21.
Part: SEAT TRACK — CORRODED (MCD) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*** MAJOR REPAIR *** R/H MAIN CARGO COMP FLOOR TRACKS HAS CORROSION AT FR 79 RBL 0-60.REPAIRED PER RCD 278285.
Part: RIB — CRACKED (FLAP) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*MAJOR REPAIR* R/H CENTER FLAP HAS 1 EA CRACK IN RIB FLANGE #18 AFT SIDEREPAIRED PER EO A300-5750-87956-A
Part: RIB — CRACKED (FLAP) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*MAJOR REPAIR* R/H CENTER FLAP HAS 2 EA CRACKS IN RIB FLANGE #25 AFT SIDEREPAIRED PER EO A300-5750-87956-A
Part: RIB — CRACKED (FLAP) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*MAJOR REPAIR* R/H CENTER FLAP HAS 1 EA CRACK IN RIB FLANGE #13 AFT SIDE.REPAIRED PER EO A300-5750-87956-A
Part: BRACKET — BROKEN (AFT CARGO) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1CBROKEN CENTER SUPPORT BRACKET AT C54 R/H.REMOVED, FABRICATED AND REPLACED IAW SRM 51-40-21.
Part: RIB — CRACKED (FLAP) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*MAJOR REPAIR* R/H CENTER FLAP HAS 1 EA CRACK IN RIB FLANGE #12 AFT SIDEREPAIRED PER EO A300-5750-87956-A
Part: RIB — CRACKED (FLAP) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*MAJOR REPAIR* R/H CENTER FLAP HAS 2 EA CRACKS IN RIB FLANGE #27 AFT SIDEREPAIRED PER EO A300-5750-87956-A
Part: RIB — CRACKED (FLAP) · airframe 23,170 hrs · 13,852 cycles
INSPECTION TYPE:1C*MAJOR REPAIR* R/H CENTER FLAP HAS 1 EA CRACK IN RIB FLANGE #11 AFT SIDEREPAIRED PER EO A300-5750-87956-A
Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,887 hrs · 13,660 cycles
INSPECTION TYPE:NAEMERGENCY EXIT LIGHTS REMAIN 'ON' WITH SW IN DISARM POSITIONREPLACED PANEL 436VU IAW ESPM 20-44-10 AND OPS CHK'D NORMAL IAW AMM 31-10-00-0201.ÿ½Ã¿½EFF SOURCE REF: AIPC 31-41-01-19B
2022
Part: WARNING LIGHT — INOPERATIVE (L1 DOOR SLIDE) · airframe 22,370 hrs · 13,351 cycles
LIGHT ON SLIDE WARNING, ON ENTRY DOOR INOP. PERF BITE TEST OF AUTONOMOUS STANDBY POWER UNIT PER AMM 52-73-00. OP CK GOOD EVAC SLIDE WARNING. TEST LIGHT OPS CH GOOD. ORIG SUB DATE: 11/28/2022
Part: TRANSMITTER — INOPERATIVE (ENG OIL PRESSURE) · airframe 22,176 hrs · 13,241 cycles
RIGHT ECAM LO OIL PRESSURE ON #2 ENGINE AND ANOLOG LOW PRESSURE ON GAUGE INDICATED "0", AIR TURN BACK. REPLACED RT ENG OIL PRESSURE TRANSMITTER PER AMM 79-33-11-0401
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 22,154 hrs · 13,225 cycles
DURING SECURE CHECKLIST-EMERG LIGHT SWITCH DISARMED BUT LIGHT DID NOT ILUM DISARMED" FOR APPROX 1 MIN. SEVERAL MINUTES LATER EMERG LIGHTS ACTIVATED,DISARM LIGHT OUT WITH SWITCH STILL IN DISARM POSTIION. PERFORMED OPS CHK IAW AMM 33-51-00 NO DEFECTS NOTED OK FOR SERVICE
2021
Part: NONE — INOPERATIVE (CABIN) · airframe 21,093 hrs · 12,614 cycles
INSPECTION TYPE:N/AEMERGENCY DISARM LIGHT BULB INOPFOLLOWED TROUBLESHOOTING MANUAL FOR EMERGENCY LIGHT DISARM IND LIGHT, OPERATED SWITCH OFF, ARM, ON POSITIONS PER 33-51-00, LIGHT WAS OPERATING NORMAL ON ALL THREE POSITIONS, OK TO CONTINUE
Part: BRACKET — CRACKED (FRAME 54) · airframe 20,015 hrs · 12,010 cycles
INSPECTION TYPE:SEGAFT CARGO PIT FWD BULKHEAD AT FR54 Y-1959 SUPPORT BRACKET IS CRACKEDREMOVED CRACK BRACKET AND INSTALLED REPLACEMENT BRACKET IAW A300 SRM 51-72-10
Part: BRACKET — CRACKED (RT WING TE) · airframe 20,015 hrs · 12,010 cycles
INSPECTION TYPE:CRH WING AT ABX 0 TE SUPPORT STRUCTURE IS CRACKED ON ATTACH LEGREPLACED SUPPORT STRUCTURE USING FABRICATED A57240071201 MADE FROM 2024 T3.040C IAW SRM 51-40-21
2019
Part: COALESCER BAG — ODOR (AC BAY) · airframe 17,210 hrs · 10,401 cycles
INSPECTION TYPE:N/A ACRID ODOR IN COCKPIT WHEN PACKS SELECTED ON. R AND R LT PACK COALESCER BAG AND FRAME SUPPORT PER 21-51-16-0301 OPS CKS GOOD NO ODOR NOTED.
Part: SKIN — DENTED (FUSELAGE) · airframe 17,186 hrs · 10,384 cycles
INSPECTION TYPE:A300 REPAIR FUSELAGE SKIN DENT BETWEEN Y-300 AND Y330 FR1. REPAIRED FUSELAGE SKIN BETWEEN Y-330 AND Y330 FR1, PER EA #300-5311-27-A2342, AND EO NO, A300-5330-72457-A.
Part: RELAY — FAILED (ANTI-ICE SYSTEM) · airframe 16,897 hrs · 10,226 cycles
ATB, IMMEDIATELY AFTER T/O ECAM ANTI ICE CAPT TAT HEAT FAULT. **SDR FILED OPEN** TRANSFERRED TO NRC 032603. **SUPPLEMENTAL SDR **REPLACED RELAY IAW ESPM 20-46-50. OPS OF TAT PROBE. HEATS GOOD.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:1C AFT CARGO PIT AT FRAME 45 APPROX. RBL 38.5, 4 INCHES DOWN FROM CEILING LEVEL THE FORWARD BUKLHEAD WALL SUPPORT STRUCTURE HAS A CRACK. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-21.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR54 @ RBL36 CRACKED. REMOVED CRACKED SUPPORT BRACKET AND REPLACED WITH NEW SUPPORT BRACKET P/N A5341076522100 IAW SRM 51-40-21.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR 54 RBL 40 CRACKED. REMVOED CRACKED SUPPORT BRACKET AND REPLACED WITH NEW SUPPORT BRACKET P/N A5341076521900 IAW SRM 51-40-21.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR54@ BL 0 CRACKED. REMOVED AND REPLACED BRACKET @ FR54 BL 0 IAW SRM 51-40-21.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR MAIN CABIN SEAT TRACK FR80 AT LT Y450 IS OUT OF LIMITS. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW SRM 53-10-16.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR MAIN CABIN SEAT TRACK FR80 AT -450 IS OUT OF LIMITS. REMOVED AND REPLACED DAMAGED SEAT TRACK IAW SRM 53-10-16.
Part: WEB — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR AVIONICS COMPARTMENT ACCESS DOOR 121BL RIGHT WEB/INTERCOSTAL DAMAGED INSIDE DOOR FRAME. INSTALLED WEB IAW SRM 51-40-21 & DWG A52110744.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR MAIN CABIN FLOOR BOARD 252BN IS DAMAGED. FABRICATED NEW FLOOR PANEL 252BN IAW SREO A300-5320-40552-B.
Part: RIB — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR MAIN CABIN FLOOR STRUCTURE LOWER RIB FRA 47 LBL 12 IS CRACKED LOWER CUTOUT. STOP DRILLED CRACK AND REPAIRED IAW SRM 53-15-15.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:123C AFT CARGO FLOOR PANEL 151 IS CRACKED AT AFT END. FABRICATED NEW FLOORBOARD 151 IAW SREO-A300-5320-16407.
Part: SPLICE PLATE — CRACKED (NR 2 PYLON) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR PARTS RACK : NR 2 PYLON AFT FAIRING SPLICE PLATE BTW MID AND AFT SKINS CRACKED. REMOVED AND REPLACED SPLICE PLATE PER SRM 51-40-21.
Part: SPLICE PLATE — CRACKED (NR 2 PYLON) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR PARTS RACK: NR 2 PYLON AFT FAIRING IB SPLICE PLATE BTW MID AND AFT SKIN CRACKED. REMOVED AND REPLACED SPLICE PLATE PER SRM 51-40-21.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR FWD CARGO COMPARTMENT FLOOR PANEL 132MG HAS DAMAGE. FABRICATED NEW FLOOR PANEL 132MG IAW SREO A300-5320-16407-E.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR BULK CARGO COMPARTMENT FLOOR PANEL 161BF CRACKED. FAB NEW PANEL 161BF IAW SREO A300-5320-16407-E.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:1C AFT CARGO COMPARTMENT FWD BULKHEAD UPPER PANEL SUPPORT BRACKET FR54@RBL 77. REMOVED AND REPLACED NEW SUPPORT BRACKED IAW SRM 51-40-21.
Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR AFT CARGO COMPARTMENT FW BULKHEAD UPPER PANEL SUPPORT BRACKET FR54 @ LBL 77 CRACKED. REMOVED AND REPLACE NEW BRACKET IAW SRM 51-40-21.
Part: SEAL DEPRESSOR — GOUGED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR FWD CARGO DOOR OPENING FWD UPPER SEAL DEPRESSOR GOUGED. REMOVED AND REPLACED IAW SRM 51-40-21.
Part: SEAL — CRACKED (THRUST REVERSER) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR NR 2 ENGINE I/B T/R PYLON SPRING SEALS CRACKED. REMOVED AND REPLACED SPRING SEALS PER SRM 51-40-21.
Part: RIB — CRACKED (NR 1 PYLON) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR NR 1 PYLON FWD UPPER PRECOOLER COMPARTMENT FLAGNE ANGLE CRACK AT UPPER RADIUS. REPLACED RIB ON PANEL ASSY PN A5461146000100 IAW AB DWG A54611461.
Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR LEFT WING I/B L/E REINFORCE ANGLE UNDER KRUGER FLAP ON RIBLET IS CRACKED. REMOVED AND REPLACED RIBLET AND ATTACH ANGLE PER SRM 51-40-21 AND DWG 57241993.
Part: SUPPORT — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR FWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 @ LBL-41 CLIP CRACKED. REMOVED AND REPLACED NEW SUPPORT BRACKET IAW SRM 51-40-21.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR RT FRAME 79 HAS A CRACKED ATTACH ANGLE. REMOVED AND REPLACED ATTACH ANGLE IAW UPS EO A300-5310-71243-A.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR RT FRAME 79 HAS A CRACKED ATTACH ANGLE AFT SIDE. REMOVED AND REPLACED ANGLE PER SRM 51-40-21.
Part: SUPPORT — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YRFWD CARGO COMPARTMENT AFT BULKHEAD UPPER FRAME SUPPORT STA 38.2 @ LBL-22 CLIP CRACKED. REMOVED AND REPLACED NEW UPPER FRAME SUPPORT IAW SRM 51-40-21.
Part: PLATE — CRACKED (PYLON) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:1C1# PYLON I/B FISH PLATE CRACKED. REMOVE AND REPLACE WITH NEW IAW SRM 54-52-21.
Part: SKIN — DENTED (RT AILERON) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR RIGHT WING ALL SPEED AILERON TRACKING EDGE LOWER SKIN HAS DENT. REPAIRED AILERON WITH METAL BOND REPAIR IAW SRM 57-61-11 AND 51-77-12 4.C
Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR JUST AFT OF LT FRAME 79 HAS A CRACKED CUSP WEB. REMOVED AND REPLACED SHEAR PLATE PER SREO A300-5310-58168-A.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 16,896 hrs · 10,224 cycles
INSPECTION TYPE:12YR LT FRAME 79 HAS CRACKED ATTACH ANGLE. REMOVED CRACKED ATTACH ANGLE IAW SRM 51-40-21. REPLACED WITH NEW ATTACH ANGLE IAW SRM 51-40-21.
Part: BRACKET — CRACKED (CARGO BAY) · airframe 16,895 hrs · 10,223 cycles
INSPECTION TYPE:12YR FWD CARGO COMPARTMENT DOOR FRAME UPPER RT CORNER FR20 WIRE HARNESS BRACKET DAMAGED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.
Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 16,895 hrs · 10,223 cycles
INSPECTION TYPE:1C AVIONICS COMPARTMENT FLOOR SUPPORT ANGLE FR10 @ RBL 37 CRACKED. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW SRM 51-40-21.
2017
Part: POWER SUPPLY — INOPERATIVE (PAX DOOR SLIDE) · airframe 15,590 hrs · 9,462 cycles
DURING A POST FLIGHT INSPECTION, OBSERVED THE MAIN CABIN DOOR RED WARNING LIGHT TO BE INOPERATIVE. EVACUATION SLIDE OR SLIDE RAFT RELEASE WARNING SYSTEM LIGHT. REMOVED AND INSTALLED THE AUTONOMOUS STANDBY POWER SUPPLY UNIT IAW AMM 52-73-18. RESIDUAL PRESSURE WARNING SYSTEM OPS CHECKED GOOD IAW AMM 52-73-00.
Part: HANDLE — MISSING (COCKPIT DOOR) · airframe 14,828 hrs · 8,994 cycles
CREW ENTRY DOOR ASSIST HANDLE MISSING TOP PORTION. INSTALLED A NEW TOP HANDLE IAW AMM 52-10-13-401.
Part: SKIN — DENTED (FRAME 84) · airframe 14,817 hrs · 8,985 cycles
LOWER FUSELAGE SKIN DENTED NEAR THE TAIL. REPAIRED IAW EO A300-5330-64342-B.
2016
Part: BRACKET — CRACKED (AFT CARGO) · airframe 13,608 hrs · 8,273 cycles
INSPECTION TYPE: C-1, AFT LOWER CARGO FWD AT FRAME 54 FWD BULKHEAD SUPPORT BRACKET LEFT OF CENTER IS CRACKED. REMOVED AND REPLACED WITH NEW BRACKET IAW SRM 51-40-21
Part: PANEL — CRACKED (NR 1) · airframe 13,608 hrs · 8,273 cycles
INSPECTION TYPE: C-1, NR 1 NOSE COWL, AFT SIDE, INBD SENSE LINE PANEL CRACKED. REMOVED PANEL AND SPLICED IN A NEW SECTION IAW SRM 54-10-00 REPAIR 14.
Part: WEB — CRACKED (NR 1 NACELLE) · airframe 13,608 hrs · 8,273 cycles
INSPECTION TYPE: C-1, NR 1 ENGINE AFT BULKHEAD OF NOSE COWL WEB CRACKED AT SENSE LINE FITTING. REMOVED WEB SECTION AND SPLICED IN A NEW SECTION IAW SRM 54-10-00 REPAIR 14.
Part: SUPPORT BRACKET — CRACKED (FRAME 54) · airframe 13,608 hrs · 8,273 cycles
INSPECTION TYPE: C-1, AFT LOWER CARGO FWD AT FRAME 54 FWD BULKHEAD CENTER SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED CRACKED SUPPORT BRACKET IAW SRM 51-40-21
Part: SWITCH — INOPERATIVE (PAX DOOR) · airframe 13,386 hrs · 8,114 cycles
PRESSURIZATION LOST, LOUD PAINFUL SQUEAL FROM LT FORWARD ENTRY DOOR, LT FORWARD ENTRY DOOR NOT CLOSED ON ECAM. FOUND 43 WS DOOR SWITCH INOPERATIVE. R & R DOOR SWITCH INDICATOR IAW AMM 52-71-11. OPS CKS GOOD. PRESSURIZED ACFT AFTER DOING RIG CHECK IAW AMM 52-10-20-0601. CHECKS GOOD. OK FOR SERVICE.
Part: STOWAGE BOX — NO TEST (OXYGEN) · airframe 13,386 hrs · 8,114 cycles
NR 4 SUPERNUMERARY O2 BOX WILL NOT TEST PROPERLY. R & R NR 4 SUPERNUMERARY SEAT O2 BOX IAW AMM 35-12-51-0401, CKS NORMAL.
2015
Part: OXYGEN BOX — NO TEST · airframe 12,278 hrs · 7,437 cycles
NR 1 SUPERNUMERARY SEAT OXYGEN MASK BOX WILL NOT TEST PROPERLY. REMOVED OXYGEN MASK BOX IAW AMM 35-12-51-0401. CHECKED NORMAL. LEAK CHECKED OK.
2014
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 251MG IS DELAMINATED ON LOWER SURFACE. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 231WG IS DELAMINATED ON LOWER SURFACE. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 232VG IS DELAMINATED AND HAS SCREW HEAD MARKS. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.
Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 242EF IS DAMAGED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.
Part: FITTING — CRACKED (FRAME 12A) · airframe 11,219 hrs · 6,738 cycles
RT SIDE, FRAME 12A, FITTING IS CRACKED. REPAIRED FITTING IAW EO A300-5310-23539-G.
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 232KH IS DELAMINATED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.
Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 231SG IS CRACKED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 231LG IS DELAMINATED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 231KJ IS DELAMINATED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.
Part: FLOORBOARD — BROKEN (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 251MG IS BROKEN AT OTBD SIDE. REPAIRED FLOORBOARD IAW EO 5320-42721-F.
Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 252LJ IS CRACKED AT LOWER SURFACE. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F APPENDIX B.
Part: SEAT TRACK — CORRODED (FRAME 65) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN SEAT TRACK AFT OF FRAME 65 CORRODED AT Y0. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.
Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBOARD 252WJ IS CRACKED AT UPPER SURFACE REPAIRED FLOORBOARD IAW EO A300-5320-42721-F.
Part: FLOORBOARD — DAMAGED (FWD CARGO) · airframe 11,219 hrs · 6,738 cycles
FWD CARGO FLOORBOARD 132MG IS DAMAGED IN SEVERAL PLACES FABRICATED FLOORBOARD IAW EO A300-5320-16407-E.
Part: FLOORBOARD — CRACKED (FWD CARGO) · airframe 11,219 hrs · 6,738 cycles
FWD CARGO FLOORBOARD 132AH IS CRACKED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.
Part: FLOORBOARD — CRACKED (FWD CARGO) · airframe 11,219 hrs · 6,738 cycles
FWD CARGO FLOORBOARD 132QG HAS EDGE DAMAGE AND CRACKED. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX C.
Part: FLOORBOARD — BROKEN (AFT CARGO) · airframe 11,219 hrs · 6,738 cycles
AFT CARGO FLOORBOARD 162HF AFT INBD CORNER IS BROKEN FABRICATED FLOORBOARD IAW EO A300-5320-16407-E, APPENDIX D.
Part: FLOORBOARD — DAMAGED (FWD CARGO) · airframe 11,219 hrs · 6,738 cycles
FWD CARGO FLOORBOARD 131SG FWD END AND SIDES ARE DAMAGED. FABRICATED FLOORBOARD IAW EO A300-5320-16407-E.
Part: FLOORBOARD — DAMAGED (FWD CARGO) · airframe 11,219 hrs · 6,738 cycles
FWD CARGO FLOORBOARD 131BH FWD INBD CORNER IS DAMAGED. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F.
Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 11,219 hrs · 6,738 cycles
LEFT WING OTBD FLAP UPPER SKIN IS CORRODED UNDER STATIC WICK NEAR RIB 27A. REPAIRED FLAP UPPER SKIN IAW EA 300-5750-01-A5309.
Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN SEAT TRACK CORRODED FRAMES 80-82, Y1137.1. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.
Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBEAM AT FRAME 79, -Y1137 CRACKED. REPAIRED IAW EA 300-5310-01-A5322, REV I/R AND EO A300-5310-54516-A.
Part: SEAT TRACK — CORRODED (FRAMES 80-82) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN SEAT TRACK CORRODED FRAMES 80-82, Y450. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201.
Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 11,219 hrs · 6,738 cycles
RT WING OTBD FLAP UPPER SKIN IS CORRODED UNDER STATIC WICK NEAR RIB 27A, REPAIRED FLAP UPPER SKIN IAW EA 300-5750-01-A5310, I/R AND EO A300-5750-54401-A.
Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 11,219 hrs · 6,738 cycles
MAIN CABIN FLOORBEAM AT FR79, STA Y1320 IS CRACKED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOOR CROSSBEAM AT FR 79, STA Y1320 IAW STA SA EA 300-5310-01-1-A5322 I/R AND EO A300-5310-54516-A.
Part: FLOORBOARD — DAMAGED (FWD CARGO) · airframe 11,219 hrs · 6,738 cycles
FWD CARGO FLOORBOARD 132SG HAS EDGE SIDE DAMAGE. REPAIRED FLOORBOARD IAW EO A300-5320-42721-F, APPENDIX B.
2013
Part: BULB — INOPERATIVE (EMERGENCY LIGHT)
DURING MX INSPECTION, ONE BULB FOUND TO BE INOPERATIVE DURING MX INSPECTION. REPLACED BULB IAW MM 33-51-21-04, OPS CHECKED NORMAL.
2011
Part: SKIN — DENTED (LT WING LE FLAP) · airframe 8,406 hrs · 5,001 cycles
INSPECTION TYPE:3C, LT WING OTBD FLAP L/E HAS A DENT AT NOSE SKIN BETWEEN RIBS 3 AND 4. ACCOMPLISHED REPAIR ON LT WING OTBD FLAP L/E NOSE SKIN AT RIBS 3 AND 4 IAW EO A300-5750-44826-A, PARA 6A.
2009
Part: SLIDE — INOPERATIVE (PAX DOOR)
ESCAPE SLIDE LAMP HARNESS TEST AMP READING BELOW ACCEPTABLE LEVEL. DEFERRED M406656. R&R CREW ENTRY DOOR ESCAPE SLIDE IAW AMM 25-61-21-04, REVERSED DMP 52-11-01-3. THIS CLEARS M406656. PLACARD REMOVED.
Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR AFTER REMOVAL OF FLOORBOARD PANEL 131BH FOUND 3 CRACKS AND SEVERAL PUNCTURES. FABRICATED REPLACEMENT FLOORBOARD PER EO A300-5320-16407C.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR AFTER REMOVAL FOUND FLOOR PANEL 131 DE WITH 1 CRACK. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX C.
Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR AFTER REMOVAL OF FLOORBOARD PANEL 131GE FOUND 2 CRACKS AND SEVERAL PUNCTURES. FABRICATED REPLACEMENT FLOOR PANEL PER EO A300-5320-16407C.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR AFTER REMOVAL OF FLOOR PANEL 132MG FOUND 2 CRACKS AND MULTIPLE PUNCTURES. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX C.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR AFTER REMOVAL FOUND FLOOR PANEL 131 SG WITH 3 CRACKS AND SEVERAL PUNCTURES. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX C.
Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR AFTER REMOVAL FOUND FLOORBOARD PANEL 132RG OF FWD CARGO COMP WITH A CRACK AND MULTIPLE PUNCTURES. FABRICATED FLOORBOARD PANEL 132RG PER EO A300-5320-16407C.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR AFTER REMOVAL OF FLOOR PANEL 132SG FOUND A CRACK AND SEVERAL PUNCTURES. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX C.
Part: FLOORBOARD — CRACKED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR AFTER REMOVAL OF FLOORBOARD PANEL 131MG FOUND 2 CRACKS AND SEVERAL PUNCTURES. FABRICATED FLOOR PANEL 131MG PER EO A300-5320-16407C.
Part: FLOORBOARD — CRACKED (MAIN CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR MAIN CABIN CARGO COMPARTMENT FLOORBOARD 232EF IS PUNCTURED AND CRACKED. FABRICATED FLOORBOARD 232EF PER EO A 300-5320-16407C
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR BULK CARGO COMPARTMENT FLOOR BOARD 162 HF DELAMINATED. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX D
Part: FLOORBOARD — DELAMINATED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR BULK CARGO COMPARTMENT FLOORBOARD 161KF IS DELAMINATED. FABRICATED FLOOR PANEL PER EO A300-5320-16407-C.
Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR MAIN CABIN CARGO COMPARTMENT FLOOR BOARD 241EF DAMAGED UNDER BOARD AROUND FASTENER HOLE. FABBED FLOOR PANEL 241 EF IAW UPS EO A300-5320-16407-C, APPX. B
Part: FLOOR PANEL — DAMAGED (MAIN CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR MAIN CABIN CARGO COMPARTMENT FLOOR BOARD 231 XG DAMAGED AROUND FASTENER HOLE. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX B.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR BULK CARGO FLOOR PANEL 161MF HAS A HOLE IN IT. FABRICATED FLOOR PANEL IAW IPXA EO A300-5320-16407-C, APPX D.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR BULK CARGO FLOOR PANEL 161BF HAS CRACK AND TEMP REPAIR. FABRICATED FLOOR PANEL IAW IPXA EO A300-5320-16407-C, APPX D.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR BULK CARGO AFT FLOOR PANEL 161JF HAS HOLE IN IT AND HAS TEMP REPAIRS. FABRICATED FLOOR PANEL IAW IPXA EO A300-5320-16407-C, APPX D.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 5,320 hrs · 3,194 cycles
INSPECTION TYPE:5YR BULK CARGO FLOOR PANEL 161 HF HAS SEVERAL FIELD REPAIRS. FABBED FLOOR PANEL IAW UPS EO A300-5320-16407-C, APPX D
Part: LIGHT — INOPERATIVE (LAVATORY)
INSPECTION TYPE:N/A LAVATORY AUXILIARY LIGHT OUT. RELAMPED AND OPS CHECKED GOOD PER AMM 33-51-21-04.
2007
Part: WIRE — BROKEN (EMERGENCY EXIT)
SLIDE ARM TEST BUTTON HORN INOP, FLASHING RED LIGHT DOES NOT WORK. REPAIRED BROKEN WIRES BETWEEN TB 6035VT & P/B TEST SWITCH 39WN REF WDM 52-73-01. THIS CLEARS M360929 360929