N136UP
Registered owner: UNITED PARCEL SERVICE CO, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
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.
196 reports on file, 2003-09-15 – 2026-08-13.
Part: COVER — CRACKED (ZONE 100) · airframe 29,160 hrs · 17,946 cycles
FR 13A, STR 51 LT NLG DOOR CUTOUT COVER PANEL HAS A .467" CRACK ON I/B EDGE.
Part: WEB — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MCD FR 74 - FR 75 LH FLOOR WEB IS CORRODED REJECTED.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MCD FLOOR STRUCTURE BETWEEN FR14 AND FR17 Y1959 HAS 5 AREAS OF CORROSION ON THE O/B SIDE OF FLOOR SUPPORT AT FASTENER HOLES INSTALLED FLOOR SUPPORT ON MCD FLOOR STRUCTURE BETWEEN FR14 AND FR17 Y1959 IAW A300 SRM 51-40-21-001, PAR 6.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC FLOOR STR AT FR29, Y100 BELOW PANEL 231XG, CLS ADAPTER HAS CORROSION , DOT 78-23. REMOVED 1 EA CORRODED CLS IAW SRM 51-40-21-001. INSTALLED CLS ADAPTER ON MAIN DECK FLOOR STR AT FR29,Y100 BELOW PANEL 321XG IAW SRM 51-40-21-001
Part: ADAPTER — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC FLOOR STR AT FR34. Y1959 BELOW PANEL 241KF CLS ADAPTER HAS CORROSION , INSTALLED NEW CLS ADAPTER ON MDC FLOOR STR AT FR34. Y1959 BELOW PANEL 241KF IAW A300-600 SRM 51-40-21-001.
Part: ADAPTER — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC RH SIDE, CLS AT Y0/FR33 WITH CORROSION. INSTALLED CLS ADAPTER ON MAIN DECK R/H SIDE Y0/FR33 IAW SRM 51-40-21-001
Part: ADAPTER — DAMAGED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC FLOOR STR AT FR33, Y100, CLS ADAPTER HAS EXFOLIATED CORROSION, INSTALLED NEW CLS ADAPTER TRAVELER # T26/1871955 ON MDC FLOOR STR AT FR33, Y100 IAW SRM 51-40-21
Part: ADAPTER — DAMAGED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC RT SIDE, CLS AT Y0/FR32 WITH CORROSION 31-39. INSTALLED NEW CLS ADAPTER TRAVELER # T26/1872231 ON MDC FLOOR STR AT FR32, Y0 IAW A300-600 SRM 51-40-21.
Part: FLOOR SKIN — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC, FLOOR SKIN STR BY FR22, BTW Y1959 AND Y1456 IS CORRODED. DOT 23-094 AUDIT COMPLETE.
Part: ADAPTER — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC RH SIDE, CLS AT Y0/FR30 WITH CORROSION 31-040 INSTALLED NEW CLS ADAPTER AT MAIN CABIN YO FR30 IAW SRM 51-40-21-001.
Part: ADAPTER — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC CLS TRACK ADAPTER HAS SPOTS OF CORROSION AY LH SIDE OF Y0, FROM FR22 TO FR26. INSPECTED AND VERIFIED APPLICATION OF SURFACE PROTECTION, IAW SRM 51-23-00-001.
Part: FLOOR SKIN — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC FLOOR SKIN BETWEEN -Y2462 AND -Y1959 FR26 WITH CORROSION. INSTALLED THRUST BRACKET (1EA), SPLICE (2EA), BRACKETS (2EA) ON MDC FLOOR -Y2462 AND -Y1959 IAW SRM 51-40-21-001.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC FLOOR SUPPORT BY FR22, RH SIDE OF Y953 IS CORRODED. INSTALLED THRUST BRACKET IAW SRM 51-40-21-001 & REMOVED WIRES PROTECTION (EWIS) IAW ESPM 20-54-50-02
Part: ADAPTER — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC FLOOR STR AT FR28 Y-100, CLS HAS CORROSION , INSTALLED NEW CLS ADAPTER TRAVELER T26/1871957 ON MDC FLOOR STR AT FR28 Y-100 IAW A300-600 SRM 51-40-21-001.
Part: THRUST BRACKET — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC RT SIDE, FLOOR SKIN BETWEEN -Y2462 AND -Y1959 FR27 WITH CORROSION. INSPECTED AND VERIFIED STEP 12 THRUST BRACKET BETWEEN FR 26 AND FR 27 SURFACE PROTECTION RESTORED IAW SRM 51-21-10.
Part: DECK PLATE — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
FAULT-STR-Z200- MDC STR SKIN AROUND CLS HAS CORROSION AT FR21 BTW Y1456 AND Y953. NO ALLOWABLE LIMITS IN THE SRM 53-13-15, OUT OF LIMITS IAW SRM 53-13-15. RESTORED SURFACE PROTECTION IAW SRM 51-21-10 AND SRM 51-75-10.
Part: SUPPORT BRACKET — CRACKED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MAIN DECK FLOOR STRUCTURE, RT SIDE BTWN FR38 AND FR 38.1, BRACKET SUPPORT (DOG BONE) IS CRACKED. REMOVED CRACKED BRACKET SUPPORT (DOG BONE) AT MAIN CABIN BETWEEN FR38 AND 38.1 IAW A300-600 SRM 51-40-21-001. INSTALLED BRACKET SUPPORT AT MAIN CABIN R/H BETWEEN FR38 AND 38.1 IAW A300-600 SRM 51-40-21-001.
Part: FLOOR SKIN — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
FAULT-STR-Z200- MDC FLOOR SKIN STR BY FR24, BTW Y0 AND Y450 IS CORRODED. DOT 23-078. REMOVED FOR REPLACE FLOOR SKIN BTW FR24 TO FR25 AND BTW Y0 TO Y450. IAW A300 SRM 51-40-21-001. INSTALLED FLOOR SKIN IAW A300-600 SRM 51-40-21-001.
Part: BRACKET — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
FLOOR SKIN STR BY FR24, BTW Y1456 AND Y953 IS CORRODED. FABRICATED BRACKET TRUST IAW GMM 09-08.
Part: BRACKET — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC LT SIDE, FLOOR SKIN BETWEEN Y2462 AND Y1959 FR30 WITH CORROSION DOT 31-060. REMOVED CORRODED AREA IAW SRM A300-600-51-74-10. INSTALLED THRUST BRACKET IAW SRM 51-40-21-001.
Part: BRACKET — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC RH SIDE, BRACKET THRUST BETWEEN -Y1956 AND -Y2462 FR30 WITH CORROSION 31-045 INSTALLED BRACKET THRUST ON MDCC RH SIDE BETWEEN -Y1956 AND -Y2462 FR30 IAW A300-600 SRM 51-40-21-001.
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
FAULT-STR-Z200- MAIN DECK FLOOR STRUCTURE, L/H SIDE BTWN FR38.1 AND FR 38.2, BRACKET SUPPORT (DOG BONE) IS CRACKED. DOT 21-117 INSTALLED NEW PART P/N A5378103821400 BATCH #0004499615 ON MAIN DECK FLOOR STRUCTURE, L/H SIDE BTWN FR38.1 AND FR 38.2 IAW A300-600 SRM 51-40-21-001
Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MAIN DECK FLOOR STRUCTURE, R/H SIDE BTWN FR38.1 AND FR 38.2, BRACKET SUPPORT (DOG BONE) IS CRACKED. DOT 21-116 INSTALLED NEW PART P/N A5378103821500 BATCH #0004500927 ON MAIN DECK FLOOR STRUCTURE, R/H SIDE BTWN FR38.1 AND FR 38.2 IAW A300-600 SRM 51-40-21-001
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC SEAT TRACK TRACK ADAPTER CORRODED BTWN FR 27 & FR 28, LT SIDE OF Y953. REMOVED EWIS PROTECTION ON MDC SEAT TRACK LT SIDE OF Y953 BTWN FR 27 & FR 30 IAW ESPM 20-54-50-02.
Part: RIB — CRACKED (ZONE 400) · airframe 29,160 hrs · 17,946 cycles
NR 1 PYLON, RIB 3A WITH CRACK.
Part: SKIN — CRACKED (ZONE 400) · airframe 29,160 hrs · 17,946 cycles
NR 1 PYLON, PRECOOLER AREA, INTERNAL RT SKIN, AT RIB 4, WITH CRACK. EWIS, NR 1 PYLON PRECOOLER CAVITY IAW ESPM 20-54-50-02.
Part: ADAPTER — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC AT FR57.1, Y100 BY FLOOR PANEL 251LG, CLS HAS CORROSION, DOT 78-18. REMOVED CLS ADAPTER AT MDC AT FR58, Y100 BY FLOOR PANEL 251LG I.A.W. A300-600 SRM 51-40-20. INSTALLED NEW CLS ADAPTER P/N: A53275402202 IAW TRAVELER #: T26/1871958 ON MDC AT FR57.1, Y100 BY FLOOR PANEL 251LG IAW A300-600 SRM 51-40-21-001.
Part: ADAPTER — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC FLOOR AT FR57, Y100, BY FLOOR PANEL 251LG, CLS HAS CORROSION, INSTALLED NEW CLS ADAPTER TRAVELER T26/1872233 ON MDC FLOOR AT FR57, Y100 IAW A300-600 SRM 51-40-21-001
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MAJOR REPAIR, MAIN DECK FLOOR SUPPORT AT FR80 Y0, SEAT TRACK HAS CORROSION, INSTALLED A NEW SEAT TRACK AND 3EA REPAIR SPLICE AND 1EA ANGLE IAW SRM 53-10-16 AND SRM 51-40-21-001.
Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC RH SIDE, ANGLE SUPPORT UNDER SEAT TRACK -Y1580.5 AT FR 79 WITH CRACK. INSTALLED ANGLE ON MAIN DECK UNDER SEAT TRACK -Y1580.5 AT FR79 IAW A300-600 SRM 51-40-21-001.
Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 29,160 hrs · 17,946 cycles
MDC RT SIDE SEAT TRACK -Y1221.2 BETWEEN FR79 AND FR78 WITH CORROSION. REMOVED 3 REPAIR SPLICE, 1 ANGLE AND 1 SEAT TRACK FROM FR78 TO FR80 -Y 1221.2 IAW SRM 51-40-21. INSTALLED SEAT TRACK AT -Y1221.2 BTW FR79 AND FR78 IAW SRM 53-10-16-201.
Part: RETAINER — CRACKED (ZONE 400) · airframe 29,160 hrs · 17,946 cycles
NR 1 ENG, FWD CIRCUNFERENTIAL LATCH (ENGINE SIDE), RT ATTACHMENT BROKEN. DOT 73-022. REPLACE RETAINER ON FITTING AT NR 1 ENG, FWD CIRCUNFERENTIAL LATCH RT ENGINE SIDE IAW SRM 51-40-21. INSTALLED NR 1 ENGINE FWD CIRCUMFERENTIAL LATCH ATTACHMENT BRACKET FITTING IAW SRM 51-40-21.
Part: SUPPORT — CORRODED (ZONE 100) · airframe 29,160 hrs · 17,946 cycles
AFT CARGO CEILING SUPPORT AT FR 58 BETWEEN Y-1959 TO Y-450 WITH SERVAL SPOTS OF CORROSION. SUBTASK CARDS INCOMPLETE.
Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 29,160 hrs · 17,946 cycles
AFT CARGO SUPPORT BRACKET AT FR 54 Y1959 IS CRACKED INSTALLED NEW SUPPORT BRACKET AT FR 54 Y1959 AFT CARGO IAW A300-600 SRM 51-40-21.
Part: SUPPORT ANGLE — CRACKED (ZONE 400) · airframe 29,160 hrs · 17,946 cycles
RIGHT PYLON, SUPPORT ANGLE HAD A CRACK AT INBD SIDE, LOWER FWD CORNER OF RIB 18. INSTALLED SUPPORT ANGLE AT INBD SIDE, LOWER FWD CORNER OF RIB 18 IAW SRM 51-40-21-001.
Part: KEELBEAM — CRACKED (ZONE 100) · airframe 29,160 hrs · 17,946 cycles
CRACK FOUND ON LT KEEL BEAM ON AFT SIDE OF BREAK LINE BETWEEN FR 13A AND FR 14, LENGTH: 1 1/2
Part: STIFFENER — CRACKED (NOT REPORTED) · airframe 29,160 hrs · 17,946 cycles
FAULT-STR-Z500- KRUEGER BOX, FWD LOWER SIDE, STIFFENER HAS AN ANGLE SUPPORT CRACKED. INSTALLED ANGLE SUPPORT FROM KRUEGER BOX IAW SRM 51-40-21.
Part: SHIELD — CRACKED (ZONE 500) · airframe 29,160 hrs · 17,946 cycles
LEFT WING, KRUEGER BOX, AFT UPPER PANEL IS CRACKED IN 2EA CORNERS. REINSTALLED ALL FASTNERS ON LH WING KRUEGER BOX AFT UPPER PANEL IAW SRM 51-40-21 AND IAW DRAWING A572-42282. INSTALLED NEWLY FABRICATED PANEL TO SECOND NON DESCREPANT PANEL THAT IS PART OF THE FABRICATED PANELS ASSEMBLY.
Part: FLOORBOARD — DAMAGED (ZONE 200) · airframe 29,036 hrs · 17,846 cycles
MAJOR REPAIR, FOUND FLOORBOARD IN MCD DAMAGED IN BOTTOM CORNER UPON REMOVAL FOR ACCESS TO BLEED DUCT. MARKED WITH TAPE INSTALLATION ON PANEL COMPLETED ON BARCODE T3F18E008WF11
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 28,890 hrs · 17,755 cycles
FO WINDSHIELD FORMED SPIDER CRACK PASSING THRU 10KÃâ¬â¢/250KTS DURING ARRIVAL.W/S HEAT FAILED & SELECTED OFF. COMPLETED F/OÃâ¬â¢S WINDSHIELD R&R IAW AMM 56-11-11/401.
Part: BEAM — CRACKED (ZONE 800) · airframe 28,738 hrs · 17,666 cycles
FWD CARGO DOOR HAS CRACK IN BEAM 1 FWD OF FR22A CRACK LOCATED ON DOOR SIDE AT FR22A. CRACK LENGTH: 2.00" END OF CRACK TO EDGE OF OUTER SKIN: 2.10".
Part: BEAM — CRACKED (ZONE 800) · airframe 28,743 hrs · 17,668 cycles
MAJOR REPAIR, FWD CARGO DOOR HAS CRACK IN BEAM 1 FWD OF FR22A ITEM HAS BEEN TEMPORARY REPAIRED IAW EO-96845. NEW FAULT T3F18E008H4ZS HAS BEEN GENERATED FOR TRACKING PURPOSES OF NEW DEFERRAL. THIS ACTION CLOSES ORIGINATING DEFERRAL.
Part: PUMP — FAILED (ZONE 100) · airframe 28,574 hrs · 17,567 cycles
CLIMBING THRU FL 300 ALL 4 INNER TANK PUMPS FAILED. DIVERTED TO LOUISVILLE SDF. DEFERRED PER MEL 28-21-09-1. DMP C/W PLACARD INSTALLED.
Part: PUMP — FAILED (ZONE 100) · airframe 28,586 hrs · 17,577 cycles
DIVERSION, CLIMBING THRU FL 300 ALL 4 INNER TANK PUMPS FAILED. DIVERTED TO LOUISVILLE SDF. DMP 28-21-09-1 REVERSED. IAW TECH RECOMMENDATION. R & R RELAY 154QA, 132QA AND 41QA REF ESPM 20-46-50-01. OPPS CHECKED AUTO FUEL FEED SYSTEM IAW AMM 28-21-00-501. SYSTEM OPPS NORMALLY AT THIS TIME.
Earlier reports · 2003–2024 · 152 reports
2024
Part: SLIDE — UNWANTED DEPLOY (ZONE 800) · airframe 26,750 hrs · 16,586 cycles
SLIDE WAS NOT RELEASED WHEN CAPTAIN OPENED THE ARMED DOOR. SLIDE DEPLOYE, DID NOT INFLATE. R&R DIAPHRAGM FOR CREW DOOR DAMPER/EMERGENCY OPERATION CYLINDER IAW AMM 52-10-14/301. NO LEAKS NOTED. REFERENCE T3F18E005Q3Y7 FOR SAFETY PIN REMOVAL.
Part: BRACKET — CRACKED (ZONE 400) · airframe 26,569 hrs · 16,488 cycles
LH ENGINE LOWER OUTBOARD SIDE OF THE PYLON JUNCTION FOUND CRACK. NEED SM EVAL. PICTURES ATTACHED RECEIVED FINAL EO-91459-REQ2 ALL STEPS COMPLETED. REPLACED L/H LATERAL PANEL LOWER TRAILING EDGE I/A/W AIRBUS A300-600 SRM 51-40-21, AMM 51-40-00.
Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 25,885 hrs · 16,079 cycles
THE R/H CENTER FLAP ASSY HAS 1EA CRACK LOCATED ON RIB 26 AFT SIDE. ACCOMPLISH PERMANENT REPAIR PER EO-89571-REQ1 AND EA 300-5750-27-A3527 REV. -. ACCOMPLISHED PERMANENT REPAIR WITH FINAL EO-89571 REQ1 AND EA# 300-5750-27-A3527. JOB COMPLETE.
Part: SKIN — CRACKED (RT WING TE FLAP) · airframe 25,885 hrs · 16,079 cycles
THE RT CENTER FLAP ASSY HAS 1EA CRACK LOCATED ON RIB 27 AFT SIDE. ACCOMPLISH THE PERMANENT REPAIR PER EO-89571-REQ1 AND EA 300-5750-27-A3527 REV. -. ACCOMPLISHED PERMANENT REPAIR WITH FINAL EO-89571 REQ1 AND EA# 300-5750-27-A3527. JOB COMPLETE.
Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 25,885 hrs · 16,079 cycles
THE L/H CENTER FLAP ASSY HAS 1EA CRACK LOCATED ON RIB 26 AFT SIDE. AREA MARKED IN RED. ACCOMPLISH THE PERMANENT REPAIR PER EO-89591-REQ1 AND EA 300-5750-27-A3528 REV. -.
Part: FRAME — CORRODED (FRM 40) · airframe 25,885 hrs · 16,079 cycles
THE MIDDLE FASTENER HOLE FOR L/H SIDE FRAME 40 UPPER JUNCTION HAS CORROSION / DAMAGE INDICATIONS INSIDE THE HOLE. AREA MARKED IN RED. ACCOMPLISH TIME LIMITED REPAIR PER EO-89836-REQ1 AND EA 300-5710-27-A3522 REV.
Part: TEST BUTTON — OUT OF ADJUST (CARGO DOOR) · airframe 25,876 hrs · 16,071 cycles
DURING MCD OPERATION- CLOSING DOOR 140 DEGREE LIGHT ILLUMINATED WITH CARGO DOOR CLOSED- DOOR ONLY OPERATED TO 70 DEGREE POSITION PUSH TO TEST LIGHT STUCK IN TEST POSITION, ADJUSTED PUSH TO TEST BUTTON IAW AMM 33-14-00/501 OPS CHECK GOOD
2023
Part: UNKNOWN — VIBRATION (FUSELAGE) · airframe 25,394 hrs · 15,770 cycles
INSPECTION TYPE:NA*ATB* CLIMBING THRU 30,100 A/C BEGAN TO SHAKE. FELT LIKE IT WAS COMING FROM THE TAIL. SLOWED DOWN FROM 302 TO 290. THEN 280 KTS. LEVEL AT FL 320, VIBRATION LESSENED BUT DIDNT DISSIPATE COMPLETELY. DESCENDING THROUGH 14,500 VIBRATION INCREASED AND COULD BE FELT THROUGH RUDDERS AND CRTL COLUMNFOUND RUDDER WOULD MOVE AND CHATTER WITH YAW DAMP SYS 1 ENGAGE REMOVED AND REPLACED YAW DAMP ACTUATOR IAW AMM 22-23-22 OPS 2 LH CK GOOD REF LP 639185 ITEM #3
Part: UNKNOWN — DAMAGED (FUSELAGE) · airframe 25,373 hrs · 15,752 cycles
INSPECTION TYPE:NALEFT SIDE FUSELAGE DAMAGED AT STA3670 BETWEEN FR 57 AND FR 57.1REMOVED DAMAGE IAW EO A300-5310-87913A 6354368 08/14/23. ACCOMPLISHED STEPS 6-11 (A) VERIFIED DAMAGE REMOVED PER EO 87913A, 0557771 QC 08/15/23. ACCOMPLISHED STEPS 12-15 IAW EO A300-5310-87913A, 6354368 08/15/23. FOUND NO DMZ REQ THIS COMPLETS EO A300-5310-87913A MAINT C/W.
2022
Part: NONE — NONE (UPPER SURFACE IB) · airframe 23,710 hrs · 14,729 cycles
INSPECTION TYPE:N/ALEFT WING FLAP UPPER SKIN GOUGE/ PUNCTURE DAMAGEREPAIRED DAMAGE IAW E.O # A300-5750-83011-B
2021
Part: NONE — NONE (CABIN) · airframe 23,249 hrs · 14,495 cycles
INSPECTION TYPE:N/A**SUPPLEMENTAL SDR **HOT AIR SUPPLY OVHT ON DEPT. MID/AFT CABIN OPERATED IN MANUAL. DEF'D HOT AIR SUPPLY VALVE, MEL 21-11-10. DMP 21-11-10 C/W REF AMM 21-62-11 PGBLK 0901. PLACARD INSTALLED, OK TO CONT. ON DEF'L.REMOVED AND REPLACED #2 PACK OUT TEMP SENSOR 4HH PER AMM A300-21-61-12. OPS CHECK SAT IN AUTO AND MANUAL. THIS CLEARS DEF M764765 DMP REVERSED.
Part: BRACKET — CRACKED (FRM 54) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGAFT CARGO FWD SIDE FR 54 CENTER AREA UPPER CEILING SUPPORT HAS CRACKED.REMOVED AND REPLACED CEILING BRACKET SUPPORT IAW A300 SRM 51-40-21
Part: FITTING — CRACKED (LT WING) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:A300LH WING UPPER FUSELAGE FR46.5 BRACKET SUPPORT CRACKED.REMOVED AND REPLACED BRACKET FITTING IAW A300 SRM 51-40-21. A300-5310-18290.
Part: FLOOR PANEL — BROKEN (MAIN CARGO) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGMAIN CARGO DECK FLOOR PANEL 232QH 4TH HOLE BACK OUTBOARD SCREW IS STILL INSTALLED AND HONEYCOMB BROKENCOMPLIED WITH SREO A300-5320-42722-F
Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGPNL 252BN DAMAGEDFABBED IAW SREO A300-40552-B
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:CPNL 231SG BROKENFABBED IAW SREO A300-5320-40552-B
Part: ADAPTER — CORRODED (FRMS 20-22) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGCLS ADAPTER AT FR 20 - FR 22 Y2244 UNDERNEITH FLOOR PANEL 231MJ IS HEAVILY CORRODED. LENGTH OF CORROSION L=1.4" BY DEPTH= .120". FOUND CLS ADAPTOR TRACK TO BE OUT OF LIMITS IAW SRM 53-10-15-101 FIG 006.REMOVED CORRODED CLS ADAPTOR TRACK AND INSTALLED REPLACEMENT CLS ADAPTOR TRACK IAW SRM 51-74-10
Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGPNL 132QG DAMAGEDFABBED PER SREO A300-5320-16407-E
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGMAIN CABIN FLOORBOARD #262CM HAS COMPOSITE DAMAGECOMPLIED WITH SREO A300-5320-42722-F
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGMAIN CABIN FLOORBOARD #262EM HAS COMPOSITE DAMAGECOMPLIED WITH SREO A300-5320-42722-F
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGMAIN CABIN FLOORBOARD #262AH HAS COMPOSITE DAMAGECOMPLIED WITH SREO A300-5320-42722-F
Part: FLOOR PANEL — CRACKED (MAIN CARGO) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGMAIN CARGO COMPARTMENT FLOOR ACCESS PANEL 242HN INNER FACE CRACKEDCOMPLIED WITH SREO A300-5320-42722-F
Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGMAIN CABIN FLOORBOARD #262AM HAS COMPOSITE DAMAGECOMPLIED WITH SREO A300-5320-42722-F
Part: FLOOR PANEL — DAMAGED (MDC) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGPNL 262BH DAMAGEDFABBED IAW SREO A300-5320-40552-B
Part: SUPPORT BRACKET — CRACKED (FRM 46) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:A300RH WING UPPER FUSELAGE FRAME 46.5 BRACKET SUPPORT CRACKED.REMOVED AND REPLACED BRACKET P/N A5391005920303 IAW SRM 53-15-63 ITEM 15 AND SRM 51-40-44.
Part: FLOOR PANEL — DAMAGED (LWR CARGO) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGPNL 132PG DAMAGEDFABBED IAW SREO A300-5320-16407-E
Part: BRACKET — CRACKED (LT WING) · airframe 22,842 hrs · 14,270 cycles
INSPECTION TYPE:SEGLH WING RIB 16 INTERCOSTAL BRACKET BETWEEN SPOILER 4 AND 5 IS CRACKED.REMOVED CRACKED INTERCOSTAL AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-21
Part: BRACKET — DAMAGED (THRUST REVERSER) · airframe 22,823 hrs · 14,261 cycles
INSPECTION TYPE:NA**ATB-SUPPLEMENTALSDR -NO EMERG DECL'D - NO EMERG EQP USED-LAND UNEVENTFLY-AC OO ** LH ENG REV UNLK ILLUMINATED @ 11,000 FT 290 KTS NO BUFFET OR NO BANK. LT ILLUM AGAIN ON GRND W/T REV STOWED.PERF'D ADJ/TST RVDT & STOW DEPLOY SW IAW AMM 78-31-40-0501. NO HELP. R/R'D TRACK BRKT IAW AMM 20-12-12. T/S FND FAULT DS304 SW. MEL 78-30-01 DMP 78-30-1 CWREMOVED AND REPLACED PDU IAW 78-31-04-0401 STEP C STEPS 1-10. OPS CHECK GOOD IASW AMM 78-31-01-0401.
2020
Part: WARNING MESSAGE — ILLUMINATED (COCKPIT) · airframe 22,170 hrs · 13,843 cycles
INSPECTION TYPE: N/A WHEN GEAR IS EXTENDED ARM AND EMERGENCY EXIT LIGHT SWITCH IN AREA ARM "EXIT ON" MESSAGE ON MEMO PAGE IS NOT DISPLAYED, NOR IS IT DISPLAYED WITH SW IN ON POSITION. EMERGENCHY EXIT LIGHT SWITCH IS NOT SUPPOSED TO SHOW ON ECAM MESSAGE, PER AMM 33-50-00-0001. OPERATIONS CHECK GOOD.
Part: LATCH — INOPERATIVE (L1 DOOR) · airframe 21,857 hrs · 13,651 cycles
INSPECTION TYPE: N/A ON PREFLIGHT, L1 DOOR WOULD NOT LATCH IN OPEN POSITION. LUBRICATED MECHANISM NPLUNGER ROD-L-1 DOOR HOLD OPEN FUNCTION NORMAL, REF MM 52-10-00-0501.
Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 21,813 hrs · 13,618 cycles
INSPECTION TYPE: NA AFTER CHANGING EPSU BATTERY FOR CAPACITANCE DUE DATE CHECK EPSU WOULD NOT TEST. REPLACE EPSU, PER AMM 33-51-14-0401. OPERATIONS CHECKS GOOD.
Part: BLOWER — INOPERATIVE (EVAS) · airframe 21,662 hrs · 13,512 cycles
F/O'S EVAS UNIT BLOWER W/N TESTREPLACED F/O'S EVAS UNIT REF AMM 25-69-00. TESTS GOOD
2019
Part: BUTTON — STICKING (DOOR TEST) · airframe 20,436 hrs · 12,752 cycles
CREW ENTRY DOOR SLIDE RED WARNING LIGHT PUSH TO TEST BUTTON STICKING IN DOWN POSITIONTESTS GOOD PER M/M 52 70 00 0501
Part: PSU — FAULTED (COCKPIT) · airframe 20,025 hrs · 12,491 cycles
INSPECTION TYPE:SDR AUTONOMOUS STANDBY POWER SUPPLY UNIT SHOWED FAULT WHEN BITE CHECKED FOR BATT R AND R. PART ON ORDER REQ # 269335A.R AND R AUTONOMOUS STANDBY POWER SUPPLY UNIT PER AMM 52-73-18. OPS CHECK SATISFACTORY.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 19,795 hrs · 12,351 cycles
INSPECTION TYPE:N/A EMERGENCY EXIT SIGN NEAR MAIN ENTRY DOOR WILL NOT ILLUMINATE. RELAMPED EMERGENCY EXIT SIGN AT MAIN ENTRY DOOR PER AMM 33-50-00-0001, OPS GOOD, EFF REF: AIPC 33-51-04-09B ITEM # 050.
Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 19,743 hrs · 12,322 cycles
INSPECTION TYPE:4C, FOLDED ANGLE UNDER DRAIN TUBE COVER IS CRACKED. FABRICATED NEW ANGLE IAW DWG A54515063 REV K.
Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 19,743 hrs · 12,322 cycles
INSPECTION TYPE:4C, FOLDED ANGLE UNDER DRAIN TUBE COVER IS CRACKED. FABRICATED NEW ANGLE IAW DWG A54515063 REV K.
Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 19,743 hrs · 12,322 cycles
INSPECTION TYPE:4C, FOLDED ANGLE UNDER DRAIN TUBE COVER IS CRACKED. FABRICATED NEW ANGLE IAW DWG A54515063 REV K.
Part: DRAIN PAN — CRACKED (NR 2 PYLON) · airframe 19,743 hrs · 12,322 cycles
INSPECTION TYPE:4C, NR 2 ENGINE OUTBOARD FUEL SUCTION LINE DRAIN PAN CRACKED. STOP DRILLED AND WELDED IAW SRM 54-50-00-101-01 PARA 5C, FIG 105.
Part: STRUCTURE — CRACKED (NR 2 PYLON) · airframe 19,743 hrs · 12,322 cycles
INSPECTION TYPE:4C, NR 2 PYLON LOWER AFT FAIRING IB ATTACH STRUCTURE FWD EDGE CRACKED. REPAIRED ATTACH STRUCTURE IAW SRM 54-50-00 FIG 203.
Part: CAP — CRACKED (NR 2 PYLON) · airframe 19,743 hrs · 12,322 cycles
INSPECTION TYPE:4C, NR 2 PYLON LOWER AFT DRAIN TUBE END CAP CRACKED. REMOVED AND REPLACED.
Part: SKIN — WORN (NR 1 PYLON) · airframe 19,743 hrs · 12,322 cycles
INSPECTION TYPE:4C, NR 1 PYLON AFT INSIDE PANEL 473CL LOWER SKIN LARGE HOLE WORN WHERE DRAIN LINE PASSES THRU. FITTING LOOSE, REMOVED AND REPLACED.
Part: PAD — GOUGED (FUSELAGE) · airframe 19,743 hrs · 12,322 cycles
INSPECTION TYPE:4CJACK PAD IS GOUGED IN 3EA LOCATIONS.REMOVED DOUBLER AT JACK PAD AND REMOVED DOUBLER FORWARD OF JACK PAD, EXTERNAL CUTOUT AND INCORPORATED THE TWO REPAIRS,FABRICATED FILLERS, DOUBLER AND INSTALLED IAW A300-600 SRM 53-10-12, PAR.13, FIG.210.
Part: POWER SUPPLY — INOPERATIVE (L1 DOOR) · airframe 19,648 hrs · 12,262 cycles
INSPECTION TYPE:SDR EMERGENCY ESCAPE SLIDE WARNING LIGHT DOESNT WORK WHEN TESTED. PLACED WARNING LIGHT FOR EMEGENCY SLIDE ON L1 DOOR ON MEL 52-73-01-1 PLACARD INSTALLED. **SUPPLEMENTAL SDR** REPLACED ASPSU 70 WN PER AMM 52-73-18-401, OPS CK GOOD. PLACARD REMOVED AND ITEM CLEARED.
2017
Part: SKIN — GOUGED (FRAMES 84-85) · airframe 17,594 hrs · 11,050 cycles
FUSELAGE SKIN DOUBLER DAMAGED AT FRAMES 84 TO 85, STRINGER 45 - 44R AT THE TAIL STAND BALL AREA. REPAIRED IAW EO A300-5330-63531-E.
Part: WARNING LIGHT — INOPERATIVE (L1 DOOR) · airframe 17,587 hrs · 11,044 cycles
DURING A PREFLIGHT, THE SLIDE ARMED RED WARNING LIGHT ABOVE SLIDE ARMING LEVER AT THE CREW ENTRY DOOR INOPERATIVE. CHECKED GOOD
Part: FLOOR PANEL — PUNCTURED (MAIN DECK) · airframe 17,440 hrs · 10,937 cycles
MAIN DECK FLOOR PANEL AT LBL 2, FRAME 38 HAS DAMAGED EDGE 7.25 X .50 PUNCTURED. FABRICATED A NEW FLOOR PANEL IAW EO A300-5320-40552B.
Part: DAMPER — LOW PRESSURE (DOOR) · airframe 17,180 hrs · 10,778 cycles
ESCAPE SLIDE PRESSURE LOW. FOUND ESCAPE SLIDE PRESSURE OK. EMERGENCY DOOR DAMPER SERVICED PER MM 52 10 14 03.
2016
Part: STOP FITTING — WORN (DOOR FRAME) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE:12Y. LOWER AFT CARGO DOOR CUTOUT. STOP WORN FRAME 60. INSTALLED A NEW STOP IAW SRM 51-40-21.
Part: FLOOR SUPPORT — CRACKED (FRAME 79) · airframe 16,539 hrs · 10,393 cycles
MAIN CABIN AFT FLOOR SUPPORT CRACKED AT FR 79. REMOVED AND REPLACED THE FLOOR SUPPORT SECTION IAW SRM 51-40-21.
Part: ADAPTER — CRACKED (FUSELAGE) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE:1C, MAIN CABIN SEAT TRACK ADAPTER AT 4H FRAME 38 CRACKED. R & R ADAPTER IAW SRM 51-40-21.
Part: ADAPTER — CRACKED (FUSELAGE) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE:1C, MAIN CABIN SEAT TRACK ADAPTER AT 4H FRAME 38 CRACKED. R & R ADAPTER IAW SRM 51-40-21.
Part: SUPPORT — CRACKED (FRAME 54) · airframe 16,539 hrs · 10,393 cycles
RAFT ON FWD BULKHEAD SUPPORT FLANGE CRACKED AT FRAME 54 RBL 73. REMOVED AND REPLACED IAW SRM 51-40-21.
Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 16,539 hrs · 10,393 cycles
AFT CARGO FLOOR PANEL 151UF LOWER SURFACE PUNCTURED & CRACKED. REPAIRED IAW SREOA300-5320-42722-E.
Part: FLOORBEAM — WARPED (FRAME 49) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE: 1C, MAIN CABIN FLOORBEAM FRAME 49 IS WARPED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-21.
Part: FLOORBEAM — WARPED (FRAME 48) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE:1C, MAIN CABIN FLOORBEAM FRAME 48 IS WARPED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-21.
Part: SUPPORT BRACKET — CRACKED (FRM 54 BULKHEAD) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE:1C, AFT CARGO BULKHEAD SUPPORT BRACKET CRACKED AT FRAME 54, LBL 37. REMOVED AND REPLACED THE SUPPORT BRACKET IAW SRM 51-40-21.
Part: FLOORBEAM — WARPED (FRAME 50) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE:1C, MAIN CABIN FLOORBEAM AT FRAME 50 IS WARPED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-21.
Part: FLOORBEAM — WARPED (FRAME 52) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE: 1C, MAIN CABIN FLOORBEAM FRAME 52 IS WARPED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-21.
Part: SUPPORT — CRACKED (CARGO BULKHEAD) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE: 1C, AFT CARGO BAY FWD BULKHEAD SUPPORT FLANGE CRACKED AT FRAME 54, LBL73. REMOVED AND REPLACED THE SUPPORT IAW SRM 51-40-21
Part: BRACKET — CRACKED (AFT CARGO) · airframe 16,539 hrs · 10,393 cycles
AFT CARGO FWD BULKHEAD SUPPORT FLANGE CRACKED, FRAME 54, LBL 39. REMOVED AND REPLACED THE SUPPORT FLANGE IAW SRM 51-40-21, AND SRM 51-40-44.
Part: ATTACH FITTING — CRACKED (LT WING) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE:1C, LT WING INBD FIXED L/E INBD END ATTACH CLIP CRACKED. R & R CLIP IAW SRM 51-40-21.
Part: RAIL — CRACKED (E&E BAY) · airframe 16,539 hrs · 10,393 cycles
AVIONICS COMPARTMENT RIGHT SIDE, BATTERY RACK INBOARD RAIL CRACKED AT CENTER HORIZONTAL SUPPORT. REMOVED AND REPLACED THE RAIL IAW SRM 51-40-21 AND 51-40-44
Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE:1C, LT WING INBD FIXED L/E INBD END WEB ATTACH ANGLE CRACKED. R & R CRACKED IAW SRM 51-40-21 AND DWG A57241993.
Part: BRACKET — CRACKED (FRAME 54) · airframe 16,539 hrs · 10,393 cycles
AFT CARGO BRACKET AT FRAME 54, RBL 39 IS CRACKED. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21.
Part: SUPPORT FRAME — BROKEN (FRAMES 18-19) · airframe 16,539 hrs · 10,393 cycles
INSPECTION TYPE: 5Y, AVIONIC BAY UNDER FLOOR PANEL 121TF, WIRE BUNDLE SUPPORT FRAME BENT & BROKEN FRAMES 18-19, LBL 3-6. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-40-21.
Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 16,539 hrs · 10,393 cycles
MAIN CABIN FLOORBEAM AT FRAME 79 IS CRACKED. REPAIRED IAW EO A300-5310-61501-A
Part: FLOORBEAM — CRACKED (FRAME 79) · airframe 16,539 hrs · 10,393 cycles
MAIN CABIN FLOORBEAM AT FRAME 79 LT Y1580 IS CRACKED. REPAIRED IAW EO A300-5310-61501-A.
2015
Part: FORK — CRACKED (AFT CARGO DOOR) · airframe 15,461 hrs · 9,696 cycles
INSPECTION TYPE:SV, AFT CARGO DOOR FORK FITTING FRAME 61 HAS CRACK AT 3 O'CLOCK, 1.5" LONG ON FASTENERS 5 & 6. R & R FORK FRAME 61 IAW EO A300-5230-57988-B.
Part: FORK — CRACKED (AFT CARGO DOOR) · airframe 15,460 hrs · 9,695 cycles
INSPECTION TYPE:SV, AFT CARGO DOOR FORK FITTING FRAME 62 HAS CRACK AT 3 O'CLOCK ON FASTENER 6.5" LONG. R & R FORK FRAME FRAME 62 IAW EO A300-5230-27988-B.
Part: FORK — CRACKED (AFT CARGO DOOR) · airframe 15,460 hrs · 9,695 cycles
INSPECTION TYPE: SV, AFT CARGO DOOR FORK FITTING FRAME 61-A HAS CRACKS AT 3 O'CLOCK, .2500" LONG ON FASTENER 5 AND 1" LONG ON FASTENER 6. R & R FORK FRAME 61-A IAW EO A300-5230-27988-B.
Part: FORK — CRACKED (AFT CARGO DOOR) · airframe 15,460 hrs · 9,695 cycles
INSPECTION TYPE:SV, AFT CARGO DOOR FORK FITTING FRAME 63 HAS CRACK AT 3 O'CLOCK ON FASTENER 5.2500" LONG. R & R FORK FRAME 63 IAW EO A300-5230-57988-B.
2014
Part: BOTTLE — LOW PRESSURE (L1 DOOR)
DURING MX INSPECTION; CREW ENTRY DOOR EMERGENCY ASSIST BOTTLE PRESSURE WAS FOUND TO REQUIRE SERVICING. EMERGENCY ASSIST BOTTLE SERVICED WITH NITROGEN IAW AMM 52-10-14-301. VERIFIED ALL TOOLING REMOVED FROM THE WORK AREA.
2013
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
LAVATORY EMERGENCY LIGHT INOPERATIVE. RELAMPED OPS TEST GOOD IAW MM 33-51-21-4.
Part: LAMP — INOPERATIVE (LAVATORY)
LAVATORY AUXILARY MIRROR LIGHT INOPERATIVE. REPLACED LAMP, CHECKED GOOD.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
INSPECTION TYPE: ASE LAV EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OPS NORMAL IAW MM 33-51-21.
Part: B-NUT — LEAKING (HYD SYSTEM)
CREW REPORTED THAT DURING TAXI OUT, AN ACRID ODOR DEVELOPED AND SMOKE OF SOME SOURCE WAS VISABLE IN THE JUMPSEAT AREA. CREW ISOLATED AIR CONDITIONING PACK AND RETURNED TO THE BLOCKS. ODOR AND SMOKE DISSIPATED ONCE PACK WAS SECURED "OFF". FOUND A PARKING BRAKE HYDRAULIC LINE LEAKING IN THE AIR CONDITIONING PACK AREA. SECURED A LOOSE B-NUT AND THEN RAN AIR CONDITIONING PACKS AND VERIFIED NO SMOKE OR VISABLE SMOKE. CREW CONTINUED ON SCHEDULED FLIGHT.
Part: LAMP — INOPERATIVE (LAVATORY)
INSPECTION TYPE :ASE, LAVATORY AUX LIGHT INOPERATIVE. REPLACED LAMP & TESTED GOOD IAW AMM 33-50-00.
Part: CONNECTOR — UNSECURE (DOOR WARNING)
CREW DOOR SLIDE WARNING LIGHT INOPERATIVE. RESEATED CONNECTOR ON ASPSU AND ACCOMPLISHED OPS TEST IAW AMM 52-73-00-0501.
2012
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 221BG HAS LOWER SKIN DELAMINATED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231LJ HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 222EG HAS LOWER SKIN CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232WG HAS LOWER SKIN CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231WG HAS LOWER SKIN TORN AND PUNCTURED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231GH HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231VG HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232UG HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-4272-B, PARA 6A.
Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232FF HAS LOWER SKIN CRACKED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231NJ HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231HG HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232SG HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR ON FLOORBOARD IAW EO A300-5320-42721-B. PARA 6A.
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232JF HAS LOWER SKIN PUNCTURED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232KG HAS LOWER SKIN CRACKED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — DELAMINATED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 232LF HAS LOWER SKIN PUNCTURED AND DELAMINATED. ACCOMPLISHED REPAIR IAW EO A300-5320-42721-B, PARA 6A.
Part: FLOORBOARD — PUNCTURED (MAIN CABIN) · airframe 12,716 hrs · 7,911 cycles
INSPECTION TYPE: SV, MAIN CABIN FLOORBOARD 231QJ HAS LOWER SKIN PUNCTURED. FABRICATED FLOORBOARD IAW EO A300-5320-40552-B, APPENDIX B.
Part: SKIN — DAMAGED (FUSELAGE)
FUSELAGE SKIN DAMAGE FROM LIGHTNING STRIKE ON STR 52L & 3.5" A FT OF FRAME 36. REPAIRED REF EO A300-5330-47332-B.
2011
Part: SWITCH — INOPERATIVE (OVERHEAD PANEL)
EMERGENCY EXIT LIGHT BULB ON OVERHEAD PANEL INOPERATIVE. (DISARM LIGHT) R & R DISARM LIGHT ILLUMINATED PUSH BUTTON SWITCH WITH A SERVICEABLE P/B SWITCH IAW ESPM 20 45 11, FIG 005 & TESTED IAW AMM 33 51 00 05, PARA 1C2 (A,B,E,G). OPS CHECKED NORMAL,
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, SEAT TRACK AT Y953 BETWEEN FR61 AND FR62 CORRODED. REMOVED EXISTING SEAT TRACK SPLICE, CUT OUT DAMAGED SEAT TRACK SECTION BETWEEN FR60 AND 62. PROCURED 1EA SEAT TRACK SECTION AND 4 EA SPLICES. LOCATED AND DRILLED REPAIR PARTS AND INSTALLED REF SRM 53-10-16, PARA 4, FIG 201.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, FLOOR PANEL 242BM CRACKED AT LOWER SURFACE CORNER. FABRICATED FLOOR PANEL 242BM REF EO A300-5320-40552-A, APPX A/B.
Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:4C, MDCC FLOOR PANEL 262JM CRACKED AT LOWER SURFACE. REPAIRED FLOOR PANEL 262JM REF A300-5320-42721-A AND SRM 53-10-20- 201, REV 20, PARA 8.B, FIG 203 (SHT 2).
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:4C, FLOOR PANEL 232TG HAS A CRACK UNDER THE BOARD. REPAIRED FLOOR PANEL 232TG REF EO A300-5320-42721-A AND SRM 53-10-20-201, REV 20, PARA 8.B, FIG 203 (SHT 2).
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 242UK HAS DELAMINATION. REPAIRED MAIN CABIN FLOOR PANEL 242UK REF EO A300-5320-42721-A AND SRM 53-10-20-201, REV 20, PARA 8.B, FIG 203 (SHT 2).
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 252FJ HAS A BROKEN CORNER. FABRICATED CABIN FLOOR PANEL 252FJ REF EO A300-5320-40552-A APPX A/B.
Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 242WK IS CRACKED ON AFT EDGE OF PANEL. REPAIRED MAIN CABIN FLOOR PANEL 242WK REF EO A300-5320-42721-A AND SRM 53-10-20-201, REV 20, PARA 8.B AND FIG 203.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR MAIN CABIN FLOOR PANEL 241EF HAS DELAMINATION. REPAIRED MAIN CABIN FLOOR PANEL 241EF REF EO A300-5320-42721-A AND SRM 53-10-20-201, REV 20, PARA 8.B, FIG 203 (SHT 2).
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 252NG IS DELAMINATED. REPAIRED FLOOR PANEL 252NG REF EO A300-5320-42721-A AND SRM 53-10-20-201 REV 20, PARA 8.B, FIG 203 (SHT.2)
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 242VK IS BROKEN ON AFT EDGE OF PANEL. FABRICATED CABIN FLOOR PANEL 242VK REF EO A300-5320-40552-A APPX A/B.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN FLOOR PANEL 241TH HAS DELAMINATION. REPAIRED MAIN CABIN FLOOR PANEL 241TH REF EO A300-5320-42721-A AND MD1 SRM 53-10-20-201, REV 20, PARA 8.B AND FIG 203 (SHT 2).
Part: FLOORBOARD — BROKEN (CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD 252CM HAS BROKEN CORNER. FABRICATED MAIN DECK FLOORBOARD 252CM REF EO A300-5320-40552-A APPX A AND B.
Part: FLOOR PANEL — BROKEN (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR MAIN CABIN FLOOR PANEL 252FM HAS A BROKEN CORNER. FABRICATED MAIN CABIN FLOOR PANEL 252FM REF EO A300-5320-40552-A.
Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN DECK FLOOR PANEL 241LJ CRACKED IN 2EA PLACES ON LOWER SURFACE. REPAIRED MAIN DECK FLOOR PANEL 241LJ REF EO A300-5320-42721-A AND SRM 53-10-20-201, REV 20, PARA 8.B, FIG 203 (SHT 2).
Part: FLOOR PANEL — CRACKED (MAIN DECK) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN DECK FLOOR PANEL 241LT CRACKED ON LOWER SURFACE. REPAIRED MAIN DECK FLOOR PANEL 241LT REF EO A300-5320-42721-A AND SRM 53-10-20-201, REV 20, FIG 203.
Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 113,999 hrs · 7,065 cycles
INSPECTION TYPE:10YR, 231 ZONE FLOOR PANEL 231KJ IS DELAMINATED IN 3 PLACES ON LOWER SURFACE. FABRICATED FLOOR PANEL 231KJ REF EO A300-5320-40552-A APPX A/B.
Part: FLOOR PANEL — CRACKED (CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:4C, Z31 ZONE FLOOR PANEL 231PH HAS CRACK IN LOWER SURFACE OF HONEYCOMB PANEL. FABRICATED FLOOR PANEL 231PH REF EO A300-5320-40552-A APPX A/B.
Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, FLOORBOARD 132MG IS CRACKED IN 3EA PLACES ON LOWER SIDE. FABRICATED FLOORBOARD 132MG REF EO A300-5320-16407-E, APPX A/C.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK HAS CORROSION AT STA Y1137.1 BETWEEN FR 79 AND 80. REMOVED DAMGED SEAT TRACK SECTION, 4EA SUPPORT BRACKETS AND 1EA STIFFENER. PROCURED 1EA EAT TRACK SECTION AND 2EA SEAT TRACK SPLICES. PREPPED REMOVED AND REPAIRED PARTS AND INSTALLED AT -Y1137.1 BETWEEN FR 79 AND 80 REF SRM 53-10-16 PB 201, PARA 4, FIG 201, REV 20.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK HAS CORROSION AT STA Y1137.1 BETWEEN FR 79 AND 8 0. REMOVED DAMAGED SECTION OF SEAT TRACK AT STA Y1137.1 BETWEEN FR 79 AND 80. PROCURED 1EA SEAT TRACK SECTION AND 4EA SPLICES. PREPPED REMOVED AND PROCURED PARTS AND INSTALLED REF SRM A300-600 53-10-16, PARA 4, FIG 201, REV 20.
Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK HAS CORROSION AT STA Y794.3 BETWEEN FR 79 AND 80. REMOVED DAMAGED SEAT TRACK SECTION AND 4EA SUPPORT BRACKETS. PROCURED 1EA SEAT TRACK SECTION AND 2EA SEAT TRACK SPLICES, PREPPED REMOVED AND REPAIR PARTS AND INSTALLED REF SRM 53-10-16 PB 201, PARA 4, FIG 202.
Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, FLOORBOARD 132QG IS PUNCTURED IN 4EA PLACES. REPAIRED FLOORBOARD 132QG REF EO A300-5320-42721-A AND SRM 53-10-20-201, REV 20, FIG 203.
Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK HAS CORROSION AT STA Y450 BETWEEN FR 79 AND 80. REMOVED DAMAGED SECTION OF SEAT TRACK AND 4EA SUPPORT BRACKETS. PROCURED 1EA SEAT TRACK SECTION AND 2EA SPLICES. PREPPED REMOVED AND REPAIRED PARTS AND INSTALLED AT STA Y450 BETWEEN FR79 AND 80 REF SRM 53-10-16, PB 201, PARA 4, FIG 201, REV 20.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK HAS CORROSION AT STA -Y794.3 BETWEEN FR 79 AND 8 0. REMOVED DAMAGED SEAT TRACK SECTION AND 4EA SUPPORT BRACKETS. PROCURRED 1EA SEAT TRACK SECTION AND 2EA SEAT TRACK SPLICES. PREPPED REMOVED AND REPAIR PARTS AND INSTALLED AT STA -Y794.3 BETWEEN FR79 AND 80 REF SRM 53-10-16, PB 201, PARA 4, FIG 201, REV 20.
Part: SEAT TRACK — CORRODED (CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK HAS CORROSION AT STA Y-0 BETWEEN FR 79 AND 80. REMOVED DAMAGED SEAT TRACK SECTION AND 4EA SUPPORT BRACKETS, 1EA STIFFENER. PROCURRED 2EA SEAT TRACK SPLICES, 1EA SEAT TRACK SECTION. PREPPED REMOVED AND REPAIRED PARTS AND INSTALLED AT STA Y-0 BETWEEN FR 79 AND 80 REF SRM 53-10-16, PB 201, PARA 4, FIG 201, REV 20.
Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, FLOOR PANEL 131RG IS PUNCTURED IN 2EA AREAS. REPAIRED FLOOR PANEL 131RG REF EO A300-5320-42721-A AND SRM 53-10-20-201, REV 20, PARA 8.B, FIG 203.
Part: SEAT TRACK — CORRODED (MAIN CABIN) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:10YR, MAIN CABIN SEAT TRACK HAS CORROSION AT STA-Y450 BETWEEN FR 79 AND 80. REMOVED DAMAGED SEAT TRACK,4EA SUPPORT BRACKETS. PROCURED 2 EA SEAT TRACK SPLICES AND 1EA SEAT TRACK SECTION. PREPPED R & R PARTS AND INSTALLED REPAIR AT STA Y1137.1 BETWEEN FR 79 AND 80 REF SRM 53-10-16, PB4, FIG 201, REV 20.
Part: FITTING — CRACKED (FUSELAGE) · airframe 11,399 hrs · 7,065 cycles
INSPECTION TYPE:5/10 HFEC INSPECTION OF FR12 RT FITTING AS OUTLINED IAW EO FOUND TO BE CRACKED. ACCOMPLISHED REPLACEMENT OF FR 12 FITTING ON EO A300-5310-23539-B APPX E.
2010
Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 10,344 hrs · 6,399 cycles
INSPECTION TYPE:4C, AFT PIT FLOOR PANEL NR 151QF REQUIRES REPLACEMENT IAW EO A300-5320-16407-D. FABRICATED AFT CARGO FLOOR PANEL NR 151QF IAW EO A300-5320-16407-D, APPENDIX C.
Part: FLOORBOARD — MISREPAIRED (CARGO BAY) · airframe 10,344 hrs · 6,399 cycles
INSPECTION TYPE:4C, BULK CARGO COMPARTMENT FLOOR PANEL NR161HF REQUIRES REPLACEMENT IAW EO A300-A300-5320-16407-D. FABRICATED BULK CARGO FLOORBOARD NR 161HF IAW EO A300-5320-16407-D, APPENDIX D.
Part: FLOOR PANEL — MISREPAIRED (CARGO BAY) · airframe 10,344 hrs · 6,399 cycles
INSPECTION TYPE:4C, BULK CARGO FLOOR PANEL NR 162HF REQUIRES REPLACEMENT IAW EO A300-5320-16407-D. FABRICATED BULK CARGO FLOOR PANEL NR 162HF IAW EO A300-5320-16407-D APPENDIX D.
Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 10,344 hrs · 6,399 cycles
INSPECTION TYPE:4C, REPAIR SURVEY SEQUENCE NR 136-W4-01 EXISTING REPAIR DOUBLER GOUGED ON RT WING CTR FLAP UPPER SURFACE. ACCOMPLISHED REPAIR IAW SRM 57-50-00 PARA 4E, FIG 205.
Part: FLOOR PANEL — MISMANUFACTURED (CARGO BAY) · airframe 10,344 hrs · 6,399 cycles
INSPECTION TYPE:4C, BULK CARGO COMPARTMENT FLOOR PANEL NR 161GF REQUIRES REPLACEMENT IAW EO A300-5320-16407-D. FABRICATED BULK CARGO FLOORBOARD NR 161GF IAW EO A300-5320-16407-D, APPENDIX D.
Part: SKIN — DENTED (RT AILERON LWR)
RT AILERON BOTTOM SURFACE HAS DENT 2.200 X 3.100. REPAIRED DENT IAW SRM 57-61-114D, FIG 204 AND EO A300-5750-34868-C.
Part: SWITCH — OUT OF POSITION
DIVERSION - ANNUNCIATOR LIGHT TEST ACTIVATED IN FLIGHT. CREW DECLARED EMERGENCY AND DIVERTED TO MIA. ON APPROACH CREW FOUND THE TEST SWITCH IN THE ON POSITION. C/W ANNUNCIATOR LIGHT DIMMING ADJ AND TEST AND ANNUNCIATOR LIGHT TEST IAW 33-161-00-5, 33-14-00-5. OPS CHECK GOOD.
Part: SKIN — DENTED (FUSELAGE)
DENT 2 FT FWD AND LT OF TAIL STAND BALL. APPLIED SKIN DOUBLER IAW EO A300-5330-36482-A.
2009
Part: LIGHT — INOPERATIVE (CABIN)
INSPECTION TYPE:N/A EMERGENCY LIGHTS / EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHTING PSU PER MM 33-51-14-04. OPS CHECK GOOD.
Part: LIGHT — MALFUNCTIONED (COCKPIT)
INSPECTION TYPE:N/A EXIT LIGHT DID NOT ILLUMINATE WHEN GEAR EXTENDED. DEFERRED. TESTED EMERGENCY LIGHTING SYSTEM. OPS CHECK GOOD REF AMM 33-51-00-5. CLEARS DEFERRAL M397423.
2008
Part: FLOORBOARD — PUNCTURED (MAIN CARGO DECK)
INSPECTION TYPE:N/A FLOORBOARD DAMAGED MAIN CARGO DECK POS 1 RT SIDE. FABRICATED NEW PANEL IAW EO A300-5320-16409-C.
Part: CONNECTOR — DIRTY (EVAC SLIDE) · airframe 7,454 hrs · 4,728 cycles
INSPECTION TYPE:1C ESCAPE SLIDE RELEASE WARNING FAILED OP CHECK, EMERGENCY EXIT LIGHT INTERMITTENT. TROUBLESHOT TO PINS "C" AND "F", CLEANED CONNECTOR, PINS, OP CHECKED ESCAPE SLIDE RELEASE WARNING, OP CHECKED GOOD, EMERGENCY EXIT LIGHT ALSO CHECKS GOOD PER A300 MM 52-73-00.
Part: SKIN — DENTED (FUSELAGE) · airframe 7,454 hrs · 4,728 cycles
INSPECTION TYPE:3C TRANSFERRED FROM LOG PAGE 954176 ITEM 2. REF DMI D370413. SKIN DENTS FWD AND RIGHT OF TAIL STAND FITTING. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER & FILLER IAW A300-600 SRM 53-10-12 FIG 210.
2006
Part: LIGHT — NO TEST (CABIN)
SUPERNUMERARY EMERGENCY LIGHTS WON'T TEST PROPERLY. RELAMPED 3 LAMPS IN EXIT SIGN. SYSTEM OPS CKS GOOD.
Part: SKIN — DENTED (FUSELAGE) · airframe 5,632 hrs · 3,514 cycles
INSPECTION TYPE:5YR REF DMI D314583 FOUND DENT 5 INCHES LONG X .25 INCHES WIDE X .063 INCH DEEP AT SECTION 11/12, FRAME 18, STRINGER 32 AND FWD OF THE LWR AOA VANE RIGHT. CUT OUT DAMAGED SKIN AT FR 17/18 STR 30/32, FABRICATED REPAIR DOUBLER, FILLER AND INSTALLED IAW SAA EA 300-5310-01-A0309.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
CREW DOOR EMERG EXIT SIGN LOWER LAMP INOP. RELAMPED, CKS OK AMM 33-50-00.
Part: LIGHT — MALFUNCTIONED (COCKPIT)
INSPECTION TYPE:N/A EMERGENCY LIGHT ON FOR EXTENDED TIME. PERFORMED OPERATION TEST PER MM 33-51-14. OPS CHECK NORMAL.
Part: COALESCER BAG — DIRTY (A/C BAY)
INSPECTION TYPE:N/A AFTER BLOCK OUT C/P FILLED WITH GREY SMOKE. CREW DONNED OXYGEN MASKS AVIONICS SMOKE AND MAIN CARGO DECK SMOKE WARNING RECEIVED. *S/D* PERFORMED MM 21-51-00-3 USED APU AIR FIRST AND HAD SMELL OF SKYDROL CYCLE THROUGH CHECK UNTIL SMELL WAS GONE. REMOVED AND REPLACED WATER SEPARATOR COALESER PER MM 21-51-16-3 THEN USED ENG BLEED AIR TO COMPLETE MM 27-51-00-3.
Part: SKIN — GROUND DAMAGE (FUSELAGE) · airframe 5,453 hrs · 3,399 cycles
INSPECTION TYPE:CK COMPLY WITH MAG EA 300-5318-27-A1438 AFT LOWER FUSELAGE SKIN REPAIR. DUE TO CONTACT WITH GROUND EQUIPMENT. COMPLY WITH EA VERIFIED EXISTING AND REINSPECTED FOR FURTHER DAMAGE PER EA300-5318-27-1438
Part: SKIN — GROUND DAMAGE (FUSELAGE) · airframe 5,456 hrs · 3,399 cycles
INSPECTION TYPE:CK COMPLY WITH MAG GA 300-5318-27-A1438 AFT LOWER FUSELAGE SKIN REPAIR DU E TO CONTACT WITH GROUND EQUIPMENT COMPLY WITH EA VERIFIED EXISTING AND REINSPECTED FOR FURTHER DAMAGE PER EA 300-5318-24-1438.
Part: SKIN — GROUND DAMAGE (FUSELAGE) · airframe 3,399 hrs · 5,456 cycles
INSPECTION TYPE:N/A REPAIR SKIN DAMAGE CAUSED BY GROUND EQUIPMENT REF EO A300-5310-24267-A. REPLACED SKIN AND REPAIRED DAMAGED FRAMES AND STRINGERS.
2005
Part: ANGLE — CRACKED (RT WING RIB) · airframe 4,852 hrs · 3,052 cycles
INSPECTION TYPE:1C RT WING KRUEGER BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE HAS A CRACK. REMOVED & REPLACED DOUBLER ON 2ND RIB FROM FUSELAGE PER SRM 51-40-21 & 51-40-00.
Part: RIB — CRACKED (LT WING) · airframe 4,852 hrs · 3,052 cycles
FOUND LEFT WING KRUGER FLAP BOX AREA CURVED DOUBLER ON 2ND RIB FROM FUSELAGE CRACKED. REMOVED AND REPLACED DOUBLER PER SRM 51-40-00.
Part: CROSSBEAM — CRACKED (FR 50, RBL 20) · airframe 4,852 hrs · 3,052 cycles
FOUND MAIN CARGO FS 50 RBL 20 FLOORBOARD BRACE CRACKED. REMOVED, FABRICATED AND REPLACED FLOORBOARD BRACE CROSSBEAM AT FS 50 RBL 20 PER DWG A53813379, SRM 51-40-00, SRM 53-15-15, SRM 51-20-10 AND SRM 51-23-10.
Part: SMOKE BARRIER — TORN (CARGO BAY)
INSPECTION TYPE:N/A CURTAIN BETWEEN AFT LOWER CARGO AND BULK CARGO IS TORN UPPER CENTER. REMOVED AND REPLACED CURTAIN WITH REF TO MM 25-56-11-2.
2004
Part: LIGHT — INOPERATIVE (DOOR SLIDE)
CREW ENTRY DOOR EVAC SLIDE RELEASE WARNING SYSTEM LIGHTS WILL NOT TEST. BUZZERS OK. CLEANED DEBRIS FROM SWITCH NOW OPS GOOD PER MM 52-73-00. THIS CLEARS M280249. LP 234452
2003
Part: LIGHT — INOPERATIVE (EVAC SLIDE)
CREW DISCOVERED EVAC SLIDE LIGHT (WARNING LIGHT) INOPERATIVE. DEFERRED UNDER MEL 52-73-01 01 W/CONTROL NR M266526 PLACARD INSTALLED.