N740FD
Registered owner: FEDERAL EXPRESS CORP, TN (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.
156 reports on file, 2007-02-02 – 2023-09-22.
Part: STRINGER SPLICE — CRACKED (ZONE 200) · airframe 53,979 hrs · 24,130 cycles
COMPLY WITH EO 6-5310-7-5023 A PT2. REPLACED THE CRACKED SPLICE AT THE JUNCTION AT STGR18RH - FR47. TITLE: FUSELAGE - CENTER SECTION - INSPECTION OF STRINGER 18 LH/RH AT FRAME47, AIRBUS SB A300-53-6157 COMPLIED WITH EO 6-5310-7-5023 A PT2. TITLE: FUSELAGE - CENTER SECTION - INSPECTION OF STRINGER 18 LH/RH AT FRAME47, AIRBUS SB A300-53-6157. REPLACED THE CRACKED SPLICE AT THE JUNCTION AT STGR18RH - FR47. THIS IS CATEGORY B REPAIR. FOLLOW-UP INSPECTION WAS TRACKED BY EO 6-5310-7-5023 A PT2. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE WRI 53107851 FOR WORK DETAILS.
Part: SKIN — DENTED (ZONE 300) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR94 AND FR96, STGR4LH AND STGR6LH REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR IN FUSELAGE SKIN BETWEEN FR94 AND FR96, STGR4LH AND STGR6LH WAS EVALUATED AND FOUND CONFORMITY WITH RAS/DATLS/0002239/2004 ISSUE:A. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.
Part: SKIN — DAMAGED (ZONE 300) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE SKIN BETWEEN FR95 AND FR97, STGR3LH AND STGR5LH REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR IN FUSELAGE SKIN BETWEEN FR95 AND FR97, STGR3LH AND STGR5LH WAS EVALUATED AND FOUND CONFORMITY WITH A300-600 SRM53-19-12 FIG.202. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE STRINGER AT STGR33 LH BETWEEN FR72 AND FR73 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR33 LH BETWEEN FR72 AND FR73 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. THE FIRST INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-010-00.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE STRINGER AT STGR32 LH BETWEEN FR72 AND FR73 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR32 LH BETWEEN FR72 AND FR73 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. THE FIRST INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-010-00.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE STRINGER AT STGR31 LH BETWEEN FR72 AND FR73 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR31 LH BETWEEN FR72 AND FR73 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. THE FIRST INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-010-00.
Part: SKIN PANEL — CRACKED (ZONE 500) · airframe 53,979 hrs · 24,130 cycles
LH WING - LEADING EDGE PANEL 523BB CUTOUT EDGE SKIN 1EA CRACK WAS FOUND COMPLIED WITH EA: 6-5710-T0375872 P1. TITLE: WINGS - BASIC WING STRUCTURE - LH WING BOTTOM SKIN PANEL NO.1 LEADING EDGE BETWEEN RIBS 8-9 - CRACK. REPAIRED THE LH WING LEADING EDGE PANEL 523BB CUTOUT EDGE SKIN CRACK. THIS IS CATEGORY B REPAIR. FOLLOW- UP INSPECTION WAS TRACKED BY EA: 6-5710-T0375872. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57108209 FOR WORK DETAILS.
Part: ANGLE — CRACKED (ZONE 600) · airframe 53,979 hrs · 24,130 cycles
RIB8 INSPECTION OF CENTER SPAR SEALING ANGLE VERTICAL WEB ADJACENT TO PYLON REAR ATTACH FITTING, FASTENER HOLE 58 FOUND CRACK COMPLIED WITH EA: 6-5710-T0375850 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK ON RH WING RIB 8 SEAL ANGLE - REPAIR. REPAIRED THE RH WING RIB8 CENTER SPAR SEALING ANGLE VERTICAL WEB ADJACENT TO PYLON REAR ATTACH FITTING FASTENER HOLE 58 CRACK. THIS IS CATEGORY B REPAIR. FOLLOW-UP INSPECTION WAS TRACKED BY EA: 6-5710-T0375850. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57108210 FOR WORK DETAILS.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE STRINGER AT STGR50 LH BETWEEN FR70 AND FR71 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR50 LH BETWEEN FR70 AND FR71 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. THE FIRST INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-010-00.
Part: SPOILER — DELAMINATED (ZONE 500) · airframe 53,979 hrs · 24,130 cycles
LH WING #4 SPOILER CENTER I/B & O/B HINGE ARM OUTSIDE SURFACE AND CENTER I/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1)44MM*25MM, DEPTH: 1.3MM (2)80MM*25MM, DEPTH: 1.14MM (3)25MM*20MM, DEPTH: 2.65MM COMPLIED WITH EA: 6-5750-T0359414 A P2. TITLE: WING - FLIGHT SURFACES - LH #4 SPOILER CENTER HINGE ARM LOWER AND OUTER SURFACE DELAMINATION. REPAIRED THE LH WING #4 SPOILER CENTER I/B & O/B HINGE ARM OUTSIDE SURFACE AND CENTER I/B HINGE ARM LWR SURFACE DELAMINATION. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW FEDEX GMM6-2-100. SEE WRI 57508179 FOR WORK DETAILS.
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR59 - FR60, Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR59 - FR60, Y1959 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND CLASSIFIED AS MAJOR PER GMM6-2-100.
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR66 - FR68, Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR66 - FR68, Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE STRINGER AT STGR41 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR41 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. THE FIRST INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-010-00.
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE STRINGER AT STGR27 LH BETWEEN FR77 AND FR78 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR27 LH BETWEEN FR77 AND FR78 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. THE FIRST INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-010-00
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR66, Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR66, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND CLASSIFIED AS MAJOR PER GMM6-2-100.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE STRINGER AT STGR28 LH BETWEEN FR77 AND FR78 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR28 LH BETWEEN FR77 AND FR78 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. THE FIRST INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-010-00
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR68, -Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR68, -Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE STRINGER AT STGR43 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR43 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. THE FIRST INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-010-00
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.
Part: STRINGER — UNKNOWN (ZONE 100) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON FUSELAGE STRINGER AT STGR42 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR42 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "B" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100. THE FIRST INSPECTION THRESHOLD WAS 51000FC/89000FH AFTER REPAIR EMBODIMENT. THE REPETITIVE INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-010-00
Part: SEAT TRACK — UNKNOWN (ZONE 200) · airframe 53,979 hrs · 24,130 cycles
EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR54.3 - FR55, Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5100-7-5000 D7 PT1 WAS COMPLETED. TITLE: STRUCTURES - REPAIR CATALOG - A300/310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707. THE REPAIR WAS CATEGORY "A" AND WAS CLASSIFIED AS MAJOR PER GMM6-2-100.
Earlier reports · 2007–2021 · 133 reports
2021
Part: NONE — DAMAGED (N/A) · airframe 52,993 hrs · 23,489 cycles
MDIS 740 25-50 5864 24AUG21 IND FACT U REF WRI 25-50/5863 SEAT TRACK DAMAGED AT LOCK POSITION M1654 SHGN 24AUG21 09:41 IND U FOUND ADAPTER SEAT TRACK LOBES MISSING OIL 24AUG21 09:56 IND U NO RESTRICTION REF : SR30-53-003 SEAT TRACK ADAPTER LOBES AT POSTION M1654 WORN/DAMAGED PLACED ON OIL C/7283384 OILS 24AUG21 09:56 IND U OIL REFERENCE: SR30-53-003 TERMINATING ACTION REQUIRED AT OR BEFORE: SPC :
Part: PUMP — FAILED (HYD SYSTEM) · airframe 51,394 hrs · 22,450 cycles
PDIS 740 29-11 5444 01MAR21 ANC OPEN U LOGPAGES:3142187 UPON TAKEOFF YELLOW HYD PRESSURE DROPPED TO 0 PSI FOR APPROX 30 SEC WITH CORRESPONDING LOW HYD PRESS ECAM, PRESSURE THEN RETURNED TO 3050 PSI. THIS HAPPENED 3 SEPERATE TIMES WITHIN A 2 MIN WINDOW. RETURNED TO PANC, NO EMERGENCY DECLARED. FACT 02MAR21 01:18 ANC U FOUND #2 ENGINE YELLOW SYSTEM HYD EDP DEPRESSURIZATION CANNON PLUG LOOSE. R&RED #2 ENGINE YELLOW HYD EDP PER MOCC REQUEST REF AMM 29-11-32-04-01. SERVICED AND BLED YELLOW SYSTEM INCLUDING CYCLING OF CARGO DOORS. REF AMM 29-00-00-04. RAN #2 ENGINE REF A300 JRH, PERFORMED OPERATIONAL TEST REF AMM 29-10-00-05. SELECTED YELLOW PUMP ON AND OFF NUMBEROUS TIMES. OPS CHECK GOOD.
Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 51,384 hrs · 22,447 cycles
LH ELEVATOR UPR SKIN PANEL RIB4-RIB5 FOUND IMPACT DAMAGE REPAIRED THE LH ELEVATOR UPR SKIN PANEL RIB4-RIB5 IMPACT DAMAGE PER A300-600 SRM55-21-12-201-2 PARA.5.J . THIS IS CAT B REPAIR. TRACKING EA: 6-5520-T0359677 P1 RAISED AND COMPLETED. TITLE: STABILIZERS - ELEVATORS - LH ELEVATOR UPPER SKIN REPAIR - RSC TRACKING. MAJOR REPAIR IAW GMM6-2-100.
Part: HINGE ARM — DELAMINATED (NR 3 SPOILER) · airframe 51,384 hrs · 22,447 cycles
RH WING #3 SPOILER CENTER I/B HINGE ARM O/B SURFACE AND CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION. SIZE: (1)20MM*10MM, DEPTH: 1.6MM (2)20MM*15MM, DEPTH: 2.1MM (3)20MM*15MM, DEPTH: 2.4MM COMPLIED WITH EA: 6-5750-T0359409 P1. TITLE: WING - FLIGHT SURFACES - RH 3# SPOILER CENTER HINGE ARMS LOWER AND OUTSIDE SURFACES DELAMINATION. REPAIRED THE RH WING #3 SPOILER CENTER I/B HINGE ARM O/B SURFACE AND CENTER I/B & O/B HINGE ARM LWR SURFACE DELAMINATION. THIS IS CAT A REPAIR. MAJOR REPAIR IAW GMM6-2-100.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 51,384 hrs · 22,447 cycles
AFT CARGO STRINGER 46RH FOUND CORROSION BETWEEN FR61 AND FR62A COMPLIED WITH EA: 6-5310-150949 A P3. TITLE: FUSELAGE - MAINFRAME - CORROSION DAMAGE ON STRINGER 46R - REPAIR. REPAIRED THE AFT CARGO STRINGER 46RH CORROSION BETWEEN FR61 AND FR62A. THIS IS CAT B REPAIR. ENMDS IS SET UP FOR FOLLOWING-UP INSPECTION AS PER EA: 6-5310-150949 A . MAJOR REPAIR IAW FEDEX GMM6-2-100.
Part: SKIN — CRACKED (RT WING) · airframe 51,384 hrs · 22,447 cycles
RH WING - RIB8~RIB9, SUSPECTED CRACK ACROSS FASTENER HOLE ON LWR SKIN FWD EDGE APPROX 1.0 INCH IN LENGTH COMPLIED WITH EA: 6-5710-T0359505 P1. TITLE: WINGS - BASIC WING STRUCTURE - RH WING BOTTOM SKIN PANEL NO.1 LEADING EDGE BETWEEN RIBS8-9 - CRACK. REPAIRED THE RH WING - RIB8~RIB9, SUSPECTED CRACK ACROSS FASTENER HOLE ON LWR SKIN FWD EDGE. THIS IS CAT B REPAIR. FOLLOW UP INSPECTION PER EA: 6-5710-T0359505. MAJOR REPAIR IAW FEDEX GMM6-2-100.
2020
Part: HYDRAULIC SYSTEM — LOW (GREEN SYSTEM) · airframe 50,840 hrs · 22,114 cycles
DURIG CRUISE OBSERVED GREE HYDRAULICS ON OVERHEAD AT RED DOT, COMFIRMED BY ECAM. SHORTY THERE AFTER RECEIVED GRN LO LEVEL WARNIING. RAN QRH INCLUDING MANUAL GEAR EXTENETION CREW REQUESTED TOW TO GATE. ONCE PARKED, INSPECTED A/C FUSEAGE AND FLIGHT SURFACES AND FOUND NO FUILD STREAKS OR EVIDENCE OF LEAKS. PLACED ALL GEAR DOWN MANUAL RELEASE LEVERS TO SAFE POSITION. PER CREW DEBRIEF, ONCE GER WAS EXTENDED, GREEN SYSTEM WENT BACK TO TOP HAT. MX VERIFIED INDICATION. CREW REQUESTED TOW TO GATE. ONCE PARKED, INSPECTED A/C FUSELAGE AND FLIGHT SURFACES AND FOUND NO FUILD STREAKS OR EVIDENCE OF LEAKS. PLACED ALL GEAR DOWN MANUAL RELEASE LEVERS TO SAFE POSITION. RESET LANDING GEAR SYSTEM TO NORMAL PER M/M 32-33-00-02. FOUND GREEN HYDRO SYSTEM INDICATON TO BE BETWEEN YELLOW BAND AND TOP HAT AFTER GEAR DOOR CLOSURE. SERVICED GREEN HYDRO SYSTEM PER M/M 12-12-29-00, PER M/M 29-21-11-04, OPERATED GREEN HYSRO SYSTEM TO REMOVE ANY AIR. RAN BOTH ENGINE PER JRH AND CYCLED ALL FLIGHT CONTROLS SEVERAL TIMES TO VERIFY NO AIR IN SYSTEM. SHUT DOWN ENGINES AND FOUND GREEN HYRO SYSTEM TO BE AT TOP OF TOP HAT. A/C OK FOR SERVICE.
Part: SELECTOR VALVE — FAILED (LANDING GEAR) · airframe 50,345 hrs · 21,806 cycles
L/G RETRACTION FAILURE SYSTEM 1, DOORS OPENED BUT GEAR DIDNT MOVE. IF WIRING CHECKS ARE OK OK FROM 2GA TO 3GA, THE WIRING SHOULD ALSO BE MEGGED. COMPLETE IF MEG CHECKS ARE OK, R/R 2GA AND 3GA. COMPLETE IF REQUIRED R/R 2GAA AND 3GAA C/P'S . COMPLETE R&R LANDING GEAR CONTROL HANDLE MODULE 2GA REF MM 32-31-11-04. STILL REQS INSTALLATION RII AND OPS CHECK REF MM 32-31-11-04 PAR 2 D&E. R&R GEAR LANDING GEAR SELECTOR VALVE REF MM 32-31-12-04 LEAK CHECKS GOOD. SWUNG GEAR SEVERAL TIMES IN EACH SYSTEM GEAR SWING AND INDICATION CHECKS GOOD. GEAR HANDLE INSTALLATION RII C/W AND GEAR HANDLE OPS CHECKS C/W GOOD.
2019
Part: LINE — LEAKING (HYD SYSTEM) · airframe 49,536 hrs · 21,299 cycles
AFTER 30 MINUTES OF FLIGHT AT FL 290 GOT ECAM WARNING FOR GREEN HYSD PRESS LOW. VERIFIED ON OVERHEAD PANEL AND RT ECAM PAGE THAT GREEN HYDRAULIC WAS AT RED DOT. ACCOMPLISHED QRH PROCEDURE AND CRANKED GEAR DOWN.ON SHORT FINAL OVERHEAD GREEN HYDRAULIC GUAGE AND RT ECAM SHOWED NORMAL HYDRAULIC QTY. RH GEAR UPLOCK HAS A TEMP LINE INSTALLED, FOR 1000FH OR 750FC. INSTALLED TEMPORARY LINE REFERENCE MM 20-23-11-00, SERVICED GREEN SYSTEM REFERENCE 12-12-29-00, PERFORMED LEAK CHECK OF RH MLG UPLOCK TEMP HYDRAULIC LINE REFERENCE MM 32-31-00-05
2018
Part: SWITCH — OUT OF ADJUST (MAIN DECK DOOR) · airframe 48,717 hrs · 20,777 cycles
AT APPROXIMATELY 10,000 FT DURING DEPARTURE, RECIEVED AN ECAM CAUTION FOR THE MAIN DECK DOOR NOT CLOSED. COMPLIED WITH RED TABS AND RETURNED FOR LANDING. NO ABNORMAL CABIN RATE OBSERVED. FOUND THE SWITCH 48WS NOT MAKING CONTACT. ADJUSTED THE SWITCH IAW AMM 52-71-00-05-09. OPS CHECKED THE DOOR SWITCH NUMEROUS TIMES AMM 52-71-00-05. ACFT OK FOR SERVICE.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 48,716 hrs · 20,775 cycles
GOUGES ON SEAT TRACK SCALLOP IN MAIN DECK CARGO AT FR60 Y1456. BLENDED AREA IAW SRM 51-73-10. CHECKED LIMITS, MINIMUM MATERIAL REMOVED IS .260 AFTER REWORK .190 FOUND OUT OF LIMITS IAW SRM 53-10-16 FIG 101. FABRICATED NEW SEAT TRACK MATERIAL P/N# A53274005-SFS-DAP IAW SRM 53-10-16 FIG 201. INSTALLED NEW SEAT TRACK Y1456 IAW SRM 51-40-21. MAJOR REPAIR.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 48,716 hrs · 20,775 cycles
SEAT TRACK SCALLOP BROKEN IN MAIN DECK CARGO BETWEEN FR66 AND FR67 Y1456 CUT OUT SEAT TRACK SECTION Y1456 FR66 TO FR67 IAW SRM 53-10-16 FIG 201. FABRICATED NEW SEAT TRACK SECTION, MATERIAL P/N A53274005-SFS-DAP. INSTALLED NEW SEAT TRACK SECTION FR66 TO FR67 IAW SRM 53-10-16 FIG 201. MAJOR REPAIR
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 48,716 hrs · 20,775 cycles
COURIER FLOOR PANEL 222QF GOUGED AND PUNCTURED. FABRICATED COURIER FLOOR PANEL 222QF ON T18/1354018 IAW SRZ-25-005 MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 48,716 hrs · 20,775 cycles
COURIER FLOOR PANEL 221LF GOUGED AND PUNCTURED. FABRICATED COURIER FLOOR PANEL 221LF ON T18/1354016 IAW SRZ-25-005 MAJOR REPAIR.
Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 48,716 hrs · 20,775 cycles
COURIER FLOOR PANEL 222F GOUGED. FABRICATED COURIER FLOOR PANEL 222F ON T18/1354014 IAW SRZ-25-005 MAJOR REPAIR.
Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 48,716 hrs · 20,775 cycles
CRACK ON FLOOR PANEL 251WH IN MDC FABRICATED 251WH FLOOR PANEL ON T18/1354253IAW DWG SRZ 25-006 REV M. CLASSIFIED AS A CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 48,716 hrs · 20,775 cycles
MAIN DECK CARGO COMPT 232HG FLOOR PANEL BROKEN. FABRICATED 232HG FLOOR PANEL ON T18/1353529 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 48,716 hrs · 20,775 cycles
MAIN DECK CARGO COMPT 231TG FLOOR PANEL BROKEN. FABRICATED 231TG FLOOR PANEL ON T18/1353527 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 48,716 hrs · 20,775 cycles
MAIN DECK CARGO COMPT 231HG FLOOR PANEL BROKEN. FABRICATE 231HG FLOOR PANEL ON T18/1353530 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 48,716 hrs · 20,775 cycles
MAIN DECK CARGO COMPT 242EK FLOOR PANEL BROKEN. FABRICATED 242EK FLOOR PANEL ON T18/1353526 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
Part: FLOOR PANEL — BROKEN (ZONE 200) · airframe 48,716 hrs · 20,775 cycles
MAIN DECK CARGO COMPT 242LK FLOOR PANEL BROKEN. FABRICATED 242LK FLOOR PANEL ON T18/1353615 IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.
Part: B-NUT — LOOSE (APU OIL SYSTEM) · airframe 48,612 hrs · 20,706 cycles
DURING CRUISE AT 310 FT, THE APU AUTO SHUTDOWN. FOLLOWED QRH, TRIED TO RESTART, AND THE APU WOULD NOT RESTART. FOUND APU OIL LOW AT BLOCK IN. APU ECB SHOWED LOW OIL PRESSURE FAULT. CLEARED FAULT, SERVICED THE APU OIL SYSTEM. FOUND SCAVANGE LINE B-NUT LOOSE ON BOTTOM OF THE APU, TORQUED IAW SPM. RAN THE APU IAW JRH FOR 1 HOUR UNDER PNUEMATIC AND ELECTRICAL LOAD. USED APU BLEED TO START THE NR 1 ENGINE TWICE. CONTINUED TO RUN APU AFTER ENGINE RUN FOR A SHORT TIME. NO APU OIL CONSUMPTION NOTED.
2016
Part: INDICATION SYS — FAULTY (COCKPIT) · airframe 46,933 hrs · 19,509 cycles
FUEL SYSTEM HAS MEL 28-42-02-02-A. AFTER T/O TRIM FUEL DASHES CAME AND WENT CAUSING FMMS ISSUES. FUEL LOW LEVEL LIGHTS THEN CAME ON AND OFF. REF MEL 28-42-02-02-A, STEP 5 DELETES FUEL QTY. INPUTS TO FMS, REF AMM 28-42-41-04, RT FUEL LOW LEVEL LIGHTS CHECK NORMAL. SWAPPED FUEL QTY INDICATOR WITH FUELING STATION. ALL INDICATIONS CHECK NORMAL.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,426 hrs · 19,175 cycles
MDCC, FRAME 15A, Y953, SEAT TRACK WITH INNER - GRANULAR CORROSION. REPLACED THE SERIOUS CORRODED SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR IAW GMM6-6-100.
Part: WEB — CRACKED (FUSELAGE) · airframe 46,426 hrs · 19,175 cycles
MDCC FRAME 47, -Y953~-Y1456, FLOOR WEB CRACKED, APPROX 0.5 INCH IN LENGTH. DRILL CRACK STOP HOLE & REMOVED CRACK BY CUT OUT OF WEB IAW SRM53-15-15 FIG 201 SHT 2. MADE REPAIR DOUBLER IAW SRM53-15-15 FIG 201 SHT 2. WET INSTALLED REPAIR DOUBLER IAW SRM53-15-15 FIG 201 SHT 2. THIS REPAIR WAS CATEGORY B & IT MUST BE INSPECTED AT DEFINED INTERVALS IAW SRM53-15-15-2-001-00. MAJOR REPAIR IAW GMM 6-2-100.
Part: WEB — CRACKED (FUSELAGE) · airframe 46,426 hrs · 19,175 cycles
MDCC FRAME 47, Y953~ 1456, FLOOR WEB, CRACKED APPROX 0.5 INCH IN LENGTH. DRILL CRACK STOP HOLE & REMOVED CRACK BY CUT OUT OF WEB IAW SRM 53-15-15 FIG 201 SHT 2. MADE REPAIR DOUBLER IAW SRM 53-15-15 FIG 201 SHT 2. WET INSTALLED REPAIR DOUBLER IAW SRM 53-15-15 FIG 201 SHT 2. THIS REPAIR IS CATEGORY B & IT MUST BE INSPECTED AT DEFINED INTERVALS IAW SRM 53-15-15-2-001-00. MAJOR REPAIR IAW GMM 6-2-100.
Part: WEB — CRACKED (FUSELAGE) · airframe 46,426 hrs · 19,175 cycles
MDCC FRAME 47, Y0~ Y450, FLOOR WEB CRACKED, APPROX 1.0 INCH IN LENGTH. FABRICATE NEW WEB IAW DWG A53832100. INSTALL NEW WEB IAW SRM 51-40-21. MAJOR REPAIR.
Part: WEB — CRACKED (FUSELAGE) · airframe 46,426 hrs · 19,175 cycles
MDCC FRAME 47, Y0~ -Y450, FLOOR WEB CRACKED, APPROX 1.0 INCH IN LENGTH. FABRICATE THE NEW WEB IAW DWG A53832100. INSTALL NEW WEB IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 46,426 hrs · 19,175 cycles
DURING PERFORM WC 6-5310-7-5017 E PT 3, AFTER REMOVED THE BOLT FOUND HOLE H DAMAGED PREVIOUSLY. COMPLIED WITH EA 6-5310-T0324002 P 1. MAJOR REPAIR IAW GMM 6-2-100.
Part: SUPPORT BEAM — CORRODED (FUSELAGE) · airframe 46,426 hrs · 19,175 cycles
AFT CARGO FRAME 65 - RT LONGITUDINAL BEAM, FLOOR STRUCTURE, CORRODED. REPLACED THE LONGITUDINAL BEAM IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,426 hrs · 19,175 cycles
MDCC FRAME 11 - 14, Y953, FLOOR SUPPORT CORRODED AROUND BOLT HOLES. REPLACED THE CORRODED FLOOR SUPPORT IAW SRM 51-40-21. THIS IS A MAJOR REPAIR.
Part: RIB — CRACKED (TE FLAP) · airframe 46,426 hrs · 19,175 cycles
RIGHT WING INBD FLAP INTERNAL RIB, FOUND CRACK AT RIB 25A, BETWEEN STRINGER 2.2 - 2.4. COMPLIED WITH EA 6-5750-T0323968 P1. REPLACED THE RT WING INBD FLAP INTERNAL RIB AT RIB 25A, BETWEEN STRINGER 2.2 - 2.4.
Part: FRAME — CRACKED (FUSELAGE) · airframe 46,426 hrs · 19,175 cycles
MAIN DECK AREA, FUSELAGE FRAME 47 WITH HOLE L CRACKED, AT STRINGER 25R - 26R.
2015
Part: FLAP — DAMAGED (LT WING) · airframe 460 hrs · 18,972 cycles
ON DIRTY UP FOR APPROACH, KRUEGER FLAP FAILED TO EXTEND. REPLACED DAMAGED LT KRUEGER FLAP INBD CARRIER & SUPPORT WITH KRUEGER FLAP POSITION SWITCHES IAW MM 27-87-14-04. AWAITING INSTALLATION OF KRUEGER FLAP FOR OPERATIONS CHECKS. INSTALLED LT KRUEGER FLAP MOVEABLE VANE & ROD SPRING IAW MM 27-87-12-04. INSTALLED LT KRUEGER FLAP IAW MM 27-87-11-04. OPERATIONS CHECKED NORMAL. RESTORED EXTERIOR SURFACE FINISH IAW AMM 51-23-99-00. `
Part: SLAT — FAULTED (WING) · airframe 459 hrs · 18,936 cycles
SLATS SYSTEM 1 & 2 FAULTED ON APPROACH AT 240 KTS. CYCLED HANDLE TO SLATS UP & SLOWED TO 220 KTS. ATTEMPTED SECOND EXTENSION WITH SAME RESULT. FOLLOWED QRH & ECAM, LANDED SLATS 0 FLAPS 40. FOUND LT TORQUE LIMITER TRIPPED, PERFORMED INSPECTION & CHECK OF LT WING. SCREW JACKS FOUND NR 3 TRIPPED, DRAINED FLUID FOUND IT TO BE MILKY & BADLY DISCOLORED. FLUSHED & REFILLED, CHECKED BALLS CREW, NO DEFECTS NOTED. RESET TORQUE LIMITERS & CYCLED SLATS SEVERAL TIMES, NO FAILURES OR LIMITER TRIPS IAW TSM 27-80-02 FIG 101 12-13-27-00, 27-84-00-02 & 27-84-00-05.
Part: SLAT SYSTEM — MALFUNCTIONED · airframe 459 hrs · 18,915 cycles
SLAT SYSTEMS 1 & 2 FAULTED DURING EXTENSION. SPF I SLAT LIGHT WAS NOT ILLUMINATED. CYCLING SLATS, DID NOT CORRECT THE STUCK SLATS. BITE CHECKED SFCC'S, FOUND SLAT JAM FAULT ON BOTH. RESET SFCC'S, OPERATED SLATS NO HELP FAULTS ON SFCC'S RETURNED. SWAPPED SFCC'S AND RECEIVED FAULT ON ONLY NR 2 SFCC IN NR 1 POSITION. RETURNED SFCC'S TO ORIGIONAL POSITION. DOWN POWERED A/C TO DEPART TAIL SWAP A/C. FAULTS RESET WHILE T/S IAW TSM 27-80-02. FOUND NO FAULTS AT TORQUE LIMITERS ON EITHER SIDE OF SYSTEM. OPERATED SLATS/FLAPS TO FULL TRAVEL, NO FAULTS NOTED. ORDERING BOTH SFCC'S PRECAUTIONARY. REMOVED AND REPLACED NR 1 SFCC IAW AMM 27-51-18-04. OPS CHECKED OK. ALSO, RAN BOTH ENGINES IAW JRH FOR SLAT/FLAPS OPERATION CHECK. OPERATED THE SLAT/FLAP SYSTEM SEVERAL TIMES THROUGH FULL RANGE WITHOUT ANY FAULTS. PERFORMED AMM 27-51-00-05 TEST, WITHOUT ANY NOTED.
Part: LANDING GEAR — MALFUNCTIONED · airframe 457 hrs · 18,770 cycles
PUT GEAR HANDLE DOWN, NO RESPONSE, RED UNLOCK LIGHTS ON POS 1 & 2 BACK TO NEUTRAL, THEN UP, THEN NEUTRAL, THEN DOWN, NORMAL OPERATIONS. MTP IS FAULTING RT MAIN GEAR RELAY FAIL. R & R LANDING GEAR ELECTRO VALVE 3GA IAW AMM 32-31-12-04, OPS CHECKED GOOD IAW A300 AMM 32-31-12-6. R & R LANDING GEAR NORMAL CONTROL SWITCH UNIT 2GA IAW AMM 32-31-11-04, ACCOMPLISHED LANDING GEAR GENERAL ADJUSTMENT & TEST IAW AMM 32-00-00-5. LANDING GEAR OPS CHECKED GOOD. R & R PROXIMITY DETECTOR UNIT 54GB IAW AMM 32-31-71-04, BOX BITE CHECKED GOOD.
Part: DOOR — DEFECTIVE (CABIN) · airframe 455 hrs · 18,696 cycles
R1 DOOR WILL NOT DISARM. DISARM LEVER WILL NOT GO FULL TO DISARM SIDE. IT STOPS ABOUT 2 INCHES BEFORE FULL DISARM TRAVEL. DOOR LOCKING INDICATOR WINDOWS STILL INDICATE DOOR LOCKED. R1 CREW ENTRY DOOR INOPERATIVE. IF SLIDE TO BE RETAINED ONBOARD THEN PRIOR TO EACH DEPARTURE MX MUST VERIFY SLIDE STOWED ACCORDING TO PROCEDURES. WAS ABLE TO DISARM SLIDE, BUT GIRT BAR IS CONTACTING FWD PART OF DOOR FRAME WHEN TRYING TO OPEN DOOR. CLOSED DOOR & VERIFIED LOCKED. AMM 52-11-11-04 FOUND UPPER DOOR HINGE AT FUSELAGE DOOR FRAME HAS A MIGRATING BEARING & CUP WASHER OUT OF HINGE FITTING LETTING DOOR SAG APPROX 1/2 INCH. HINGE BOLT MAY POSSIBLY BE DAMAGED. LOWER HINGE MAY HAVE A MIGRATING BEARING. FURTHER INSPECTION WILL NEED TO BE DONE ONCE DOOR IS REMOVED. REMOVED DOOR UP TO HINGE BOLTS, NEED TO BE REMOVED. WIRING WAS DISCONNECTED BY LINE AVIONICS & IS A SEPARATE WRI 52-40. SIDEWALL PANEL FWD OF R1 DOOR REMOVED TO GET TO MOD BLOCKS. FINAL ACTION WAS R & R DOOR ASSEMBLY.
Part: GIRT BAR — BENT (R1 DOOR) · airframe 455 hrs · 18,696 cycles
R1 DOOR WILL NOT DISARM. DISARM LEVER WILL NOT GO FULL TO DISARM SIDE. IT STOPS ABOUT 2 INCHES BEFORE FULL DISARM TRAVEL. DOOR LOCKING INDICATOR WINDOWS STILL INDICATE DOOR LOCKED. FOUND THE R1 DOOR SLIDE GIRT BAR BENT AT THE FWD TAB THAT HOLDS THE SLIDER NOT ALLOWING THE SLIDE TO MOVE, CAUSING GIRT BAR TO HANG ON FWD FIXTURE. FOUND UPPER DOOR HINGE AT FUSELAGE MIGRATING BEARING & CUP WASHER OUT OF HINGE FITTING LETTING DOOR SAG APPROXIMATELY .5 INCH. WIRING DISCONNECTED. R & R HINGE & BUSH, DOOR BACK TOGETHER IAW AMM. ADJUSTED SLIDER TO CORRECT POSITION IAW MM 52-10-11-05-01. OPERATED ARMING HANDLE SEVERAL TIMES, NO BINDING NOTED. DOOR ADJUSTMENT CHECKED IAW MM 52-10- 11-05-01. DOOR OPS NORMAL.
2014
Part: RIB — CORRODED (RT WING) · corrosion level 2 · airframe 44,532 hrs · 18,069 cycles
RIGHT RIB 5 MLG FWD LUG HAS CORROSION IN BORE, FWD & AFT FACE. COMPLIED WITH EA 6-5710-T0310388 P1 WING BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.
Part: RIB — CORRODED (LT WING) · corrosion level 2 · airframe 44,532 hrs · 18,069 cycles
LEFT RIB 5 MLG FWD LUG HAS CORROSION IN BORE & AFT FACE. COMPLIED WITH EA 6-5710-T0310388 P2 WINGS BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.
Part: CIRCUIT BREAKER — FAILED · airframe 44,406 hrs · 17,990 cycles
DURING CRUISE, LOST AC BUSS NR 1 ESSENTIAL BUSS & AC EMERGENCY BUSS WAS ON INVERTER. LOST CAPTAIN`S ND, AUTOPILOT 1. FOLLOWED QRH, TURNED OVERHEAD SUPPLY NR 1 ON. REMOVED AND REPLACED CIRCUIT BREAKER 10 XH IAW SMP.
Part: GENERATOR — UNKNOWN · airframe 44,407 hrs · 17,991 cycles
DURING DEPARTURE, RECEIVED ECAM ALERT, AC BUSS 1 OFF, AC EMERGENCY ON INVERTER AC ESS BUSS OFF. COMPLIED WITH QRH, PERFORMED TROUBLESHOOTING IAW TSM. CHECKED GENERATOR WIRE HARNESS FOR CHAFING & CONNECTORS FOR SECURITY. CLOSED ENG COWLS, RAN ENG IAW JRH, CYCLED GENERATOR SWITCH, OPS CHECKED NORMAL.
2011
Part: STRUCTURE — CONTAMINATED (RT ELEVATOR) · airframe 40,928 hrs · 16,080 cycles
SUSPECT WATER INDICATIONS ON RT ELEVATOR FOUND DURING THERMOGRAPHY INSPECTION. REPAIRED IAW SRM 55-21-12.
Part: RUDDER — DAMAGED · airframe 40,928 hrs · 16,080 cycles
SUSPECT WATER INDICATIONS ON RUDDER FOUND DURING THERMOGRAPHY INSP REPAIR CARRIED OUT TO T/E SCREW NR 37 RT IAW EA 6-5540-154307, PART 1, SRM 55-41-12, MAJOR REPAIR ULTRASONIC INSP OF AREAS IN FIG 2 THRU 8 TO BE CARRIED OUT AT 6 YEAR INTERVALS IAW MRBR IAW EA 6-5540-154307, PART 2.
Part: ANGLE — DAMAGED (ZONE 600) · airframe 40,928 hrs · 16,080 cycles
DURING EMBODIMENT OF RT FRAME 40 PICK UP ANGLE REPLACEMENT (REF EO 6-5310-7-5001 PT2) HOLE 47 FOUND TO HAVE DISCREPANCY RT FRAME 40 PICK UP ANGLE HOLE 47. REWORKED IAW EA 6-5300-154310.
Part: ANGLE — DAMAGED (ZONE 500) · airframe 40,928 hrs · 16,080 cycles
DURING EMBODIMENT OF LT FRAME 40 PICK UP ANGLE REPLACEMENT (REF EO 6-5310-7-5001 PT2) HOLES 47,19 AND 23 TO 30 FOUND TO HAVE DISCREPANCY LT FRAME 40 PICK UP ANGLE HOLES 47, 1 AND 23 TO 30 REWORKED IAW ATTACHED EA 6-5300-154309.
Part: FITTING — CORRODED (NR 1 NACELLE) · airframe 40,928 hrs · 16,080 cycles
EVIDENCE OF LIGHT SURFACE CORROSION IN NR 1 PYLON RIB 18 BALL JOINT LUG BORE LT PYLON RIB 18 BALL JOINT LUG BORE OVERSIZED IAW SB A300-54-6018 SCHEME 1(ACCOMPLISHED ON EA 6-5451-154311).
Part: PLATE — DAMAGED (ZONE 100) · airframe 40,928 hrs · 16,080 cycles
AFT CARGO DOOR UPPER FUSELAGE CUT OUT SEALING PLATE BETWEEN FR 59A AND FR 63 FOUND BADLY DAMAGED AFT CARGO DOOR UPPER FUSE CUT OUT SEALING PLATE BETWEEN FR 59A AND FR 63. REPLACED IAW SRM 51-40-21.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,928 hrs · 16,080 cycles
AFT CARGO FLOOR STRUCTURE FOUND CORROSION AT FR 63 BETWEEN S45-46R. REPAIRED IAW SRM 53-10-14 P 202, FIG 201C DEVIATION OF FASTENER INSTALLATION ACCOMPLISHED IAW EA 6-5310-150949, MAJOR REPAIR IAW SRI 53-10-14-2-002-00, P 207, TABLE 203.
Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,928 hrs · 16,080 cycles
AFT CARGO BAY CROSSBEAM AT FR62 FOUND CORRODED AFT CARGO CROSSBEAM AT FR 62 REPLACED IAW SRM 51-40-21, MAJOR REPAIR.
Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,928 hrs · 16,080 cycles
AFT CARGO CROSSBEAM AT FR63 FOUND CORRODED AFT CARGO CROSSBEAM AT FR 63. REPLACED IAW SRM 51-40-21 & DWG A53974554.
Part: STRUCTURE — CRACKED (CENTER WING) · airframe 40,928 hrs · 16,080 cycles
DURING NDT CRACK INDICATION, FOUND IN CENTER WING BOX. REPAIR CARRIED OUT IAW EA 6-5710-154305
Part: RIB — CRACKED (ZONE 500) · airframe 40,928 hrs · 16,080 cycles
LT MLG RIB NR 5, HOLE 47 CRACK INDICATION IN SPOT FACE. REQUIREMENTS OF EA 6-5751-154313 CARRIED OUT TO LT MLG RIB 5 HOLE 47 TO REPAIR CRACK INDICATION.
Part: SKIN — CORRODED (ZONE 500) · airframe 40,928 hrs · 16,080 cycles
LEFT WING UPPER SKIN CORRODED. REPAIR CARRIED IAW EA 6-5720-154320 PART 1.
Part: SKIN — CORRODED (ZONE 600) · airframe 40,928 hrs · 16,080 cycles
RIGHT WING UPPER SURFACE SKIN CORRODED. REPAIR CARRIED OUT IAW EA 6-5720-154315,
Part: RIB — CRACKED (ZONE 600) · airframe 40,928 hrs · 16,080 cycles
RT MLG RIB NR 5, HOLE 47 CRACK INDICATION IN SPOTFACE. REQUIREMENTS OF EA 6-5751-154314 CARRIED OUT TO RT MLG RIB 5, HOLE 47 TO REPAIR CRACK INDICATION.
Part: SKIN — DENTED (ZONE 200) · airframe 40,928 hrs · 16,080 cycles
DENT AT RT FUSELAGE BETWEEN FR2-3, STR 22-25 RT. DENT TO BE REPAIRED IAW SRM 53-11-12. DENT REPAIRED IAW SRM 53-11-12, FIG 201.
Part: GUSSET — CRACKED (ZONE 100) · airframe 40,928 hrs · 16,080 cycles
LT MLG BAY GUSSET AT STR 40, FR 48 IS CRACKED GUSSET REPLACED IAW SRM 51-40-21, REF DWG A53812271.
Part: SKIN — CRACKED (ZONE 500) · airframe 40,928 hrs · 16,080 cycles
LT WING L/E PANEL 523JB LANDING ANGLE CRACKED JUST OB OF SLAT TRACK 6 FROM CAMLOCK FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 57-41-12, MINOR REPAIR.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 40,928 hrs · 16,080 cycles
RIGHT WING UPPER SURFACE SKIN AT RIB 28 ADJACENT REAR SPAR AREA CORRODED. REMOVED CORROSION FROM AREA IAW SRM 51-73-10 AND CONFIRMED USING HFEC IAW NTM 51-10-02, WITHIN LIMITS IAW SRM 57-20-12, MINOR REPAIR.
Part: SKIN — CORRODED (ZONE 500) · corrosion level 2 · airframe 40,928 hrs · 16,080 cycles
CORROSION TO LT WING LOWER SKIN PANEL NR2, LOWER SURFACE ADJACENT RIB 4. CORRODED AREA REWORKED, ASSESSED AND REPAIRED IAW EA 6-5720-154325. MAJOR REPAIR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 40,928 hrs · 16,080 cycles
SEAT TRACK AT Y450 FR 58 TO 72 FOUND DAMAGED. DAMAGED SECTION REPLACED IAW SRM 53-10-16 AND 51-40-21.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 40,928 hrs · 16,080 cycles
SEAT TRACK Y1456 FR 61TO 67 FOUND DAMAGED AT UPPER SECTION. REPLACED IAW SRM 51-40-21.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 40,928 hrs · 16,080 cycles
SEAT TRACK Y0 BETWEEN FR.58-72 FOUND DAMAGED AT ONE UPPER LOCATION BETWEEN FR 60-61. SEAT TRACK YO DAMAGED SECTION. REMOVED AND SPLICE REPAIR CARRIED OUT BETWEEN FR 58/59 AND FR 61/62 IAW SRM 53-10-16 AND SRM 51-40-21.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,928 hrs · 16,080 cycles
FLOOR SUPPORT ANGLE AT Y730 AND BETWEEN FR 11-14 FWD SECTION FOUND CORRODED FLOOR SUPPORT ANGLE AT Y730 AND BETWEEN 11 TO14 REPLACED IAW SRM51-40-20 AND DRG REF: A53612214.
Part: SKIN — CORRODED (ZONE 600) · corrosion level 2 · airframe 40,928 hrs · 16,080 cycles
CORROSION TO RT WING LOWER SKIN PANEL NR 2, LOWER SURFACE ADJACENT RIB 4. CORRODED AREA REWORKED, ASSESSED AND REPAIRED IAW EA 6-5720-154324. MAJOR REPAIR.
Part: SEAT TRACK — DAMAGED (ZONE 200) · airframe 40,928 hrs · 16,080 cycles
SEAT TRACK Y1959 BETWEEN FR 62 TO 66 FOUND DAMAGED. REPLACED IAW SRM 51-40-21
Part: SKIN — DAMAGED (ZONE 100) · airframe 40,928 hrs · 16,080 cycles
L1 DOOR SKIN CUTOUT, AFT SKIN EDGE HAS MINOR MECHNICAL DAMAGE. DAMAGE OUT OF SRM LIMITS. BLENDED DAMAGE. MAX DEPTH 0.004" X 0.5" LENGTH. INSP IAW NTM 51-10-08, NO DAMAGE. MINOR REPAIR.
Part: FAILSAFE — CHAFED (ZONE 200) · airframe 40,928 hrs · 16,080 cycles
R1 DOOR SKIN CUTOUT FAIL SAFE RING UPPER FWD CORNER REWORK IS OUT OF SRM LIMITS. BLENDED, ASSESSED AND INSP IAW SRM 53-73-10, NTM 51-10-04, 51-10-08, 51-90-00, & 51-10-01. FASTENER REMOVED , INSPECTED AND 1ST OVERSIZE FASTENER REPLACED IAW EA 6-5300-154319. MINOR REPAIR.
Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 40,928 hrs · 16,080 cycles
AFT CARGO BAY LWR DOOR SILL STRUCTURE AT FR 60 CORRODED. REPAIR CARRIED OUT IAW SRM 53-17-18 PARA7 FIG 204, MAJOR REPAIR.
Part: SKIN — GOUGED (ZONE 100) · airframe 40,928 hrs · 16,080 cycles
SKIN GOUGED BETWEEN FR 63-64 LT. BLENDED, ASSESSED AND FOUND TO BE OUT OF LIMITS. REPAIR CARRIED OUT IAW SRM 53-10-12. FIG 225. MAJOR REPAIR, SECT 17. AREA REPROTECTED AND CLOSED UP.
Part: FITTING — WORN (RUDDER ACTUATOR) · airframe 40,928 hrs · 16,080 cycles
RUDDER LOWER SERVO CONTROL ACTUATOR ATTACHMENT LUG UPPER SURFACE HAS WEAR MARKS CAUSED BY THE ANTI ROTATION WASHER. FITTING REMOVED FROM RUDDER DUE TO WEAR OUT OF LIMITS. FITTING REPLACED IAW 51-72-10/51-40-21. DUE TO MISLIGNMENT OF FITTING, ITEM REPAIRED IAW FEDEX ENG EA 6-5540-15437. REPAIRED CLASSED AS MAJOR. CAT A WITH NO REPECT INSPECTION REQUIREMENT. RDAS REF 70552790/003/2011
Part: SKIN — DAMAGED (ZONE 200) · airframe 40,928 hrs · 16,080 cycles
LEFT FUSELAGE SKIN AT FR 13, LOCATION 14TH, FASTENER UP FROM STR 25 LOCATION HAS A SKIN MARK TO THE SIDE OF THE HOLE REWORK OUT OF SRM LIMITS. BLENDED AND ASSESSED IAW SRM 53-12-12. INSPECTED IAW NTM 51-10-01/51-40-00/51-35-05 NO DEFECTS. AREA BLENDED 1" X 0.8" MAX DEPTH 0.030". FASTENER REFITTED IAW SRM. MAJOR REPAIR.
2010
Part: PROBE — DIRTY (PITOT/STATIC SYS) · airframe 39,346 hrs · 15,169 cycles
ON T/O ROLL AT 80 KNTS CALL, F/O AIRSPEED INDICATED 50 KNTS. CAPTAINS AND STBY AIRSPEED INDICATED 80 KNTS. REJECTED TAKEOFF AT 90 KNTS. R & R F/O'S PITOT PROBE IAW MM 34-11-15-4. OPS CHECKED GOOD IAW MM 34-10-00-5 (FLIGHT ENVIRONMENT DATA TEST). F/O'S LEAK TEST OK. BOTH SIDES HAD GOOD INTEGRITY CHECKS, HELD AT 6 PSI FOR 15 MINS WITH NO LEAK DOWN. A/C READY FOR SERVICE. ALSO BLEW AIR LINE FROM NR 2 ADC FWD USING NITROGEN PSI, NO DEBRIS FOUND IN LINE, BUT OLD PITOT PROBE HAD DEBRIS, VERIFIED AFTER REMOVAL FROM ACFT. (CLOSED)
2009
Part: GCU — FAILED (NR 1) · airframe 38,597 hrs · 14,765 cycles
NR1 GEN FAULTED ON TAKEOFF. TRIED ONE RESET. NO HELP. PERFORMED BITE TEST OF GROUND PWR CONTROL UNIT IAW TSM 24-00-00 PAGE 102. GOT A FAULT CODE "SHORTED PMG". IAW TSM 24-00-00 PAGE 151, REPLACE GCU. ALL OPS CKS ON THE NR1 GEN WERE NORMAL OK FOR SERVICE.
Part: AMPLIFIER — FAILED (FUEL INDICATOR) · airframe 38,447 hrs · 14,681 cycles
REPEAT OF FALSE RT OUTER FUEL QUAN LO LEVEL ECAM WARNING. ALL OTHER INDICATIONS NORMAL. LAX U FUEL LEVEL AMPLIFIER HAS HARD FAULT "R FUEL LO" WHEN INSTALLED IN RACK. WHEN SERVICEABLE FUEL LEVEL AMPLIFIER INSTALLED, FAULT DOES NOT COME BACK. TEMP INSTALLED TWICE, NO ALERTS NOTED. REMOVED AND REPLACED FUEL LEVEL AMPLIFIER IAW MM 28-46-23-4. OPS CHECK GOOD.
Part: RETAINER — GOUGED (THRUST REVERSER) · airframe 37,839 hrs · 14,353 cycles
NR 2 ENGINE OTBD T/R NR 2 BLOCKER DOOR REQUIRES REMOVAL OF NEW DOOR TO INSTALL ORIGINAL DOOR PER CUSTOMER REQUEST. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW EA 6-7830-127923. REINSTALLED DOOR IAW AMM 78-32-13-4. OPS CHECK GOOD IAW AMM 78-32-11-5.
Part: SKIN — DELAMINATED (ZONE 600) · airframe 37,839 hrs · 14,353 cycles
RIGHT WING UPPER SKIN EXTERIOR SURFACE T/E AREA HAS COMPOSITE LAYERS PEELING BETWEEN RIB 1 AND RIB 2. REPAIRED THE RIGHT WING UPPER SKIN BY REMOVING THE DAMAGE, POTTING THE PANEL AND THE HONEY COMB CORE. APPLYING FIBERGLASS OVERLAYS AND CURING IAW A300-600 SRM 51-77-11 AND EA 6-5750-127926. PRIMED AREA IAW SRM 51-35-00. INSTALLED PANEL NR 671 AT REF SRM 51-40-21, PARA 5; PG 7.
Part: SPAR — DAMAGED (RT WING FLAP) · airframe 37,839 hrs · 14,353 cycles
RIGHT INBD FLAP LEADING EDGE SPAR WEB HAS MISDRILLED HOLES ( 2 PLACES ). REMOVED & REPLACED STRUCTURE AS NECESSARY TO GAIN ACCESS TO THE DAMAGED AREA IAW SRM 51-40-21; PG 1; PG 7 AND PG 133. COMPILED WITH E.A. 6-5750-127919 PG 1 & PG 2.
Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 37,839 hrs · 14,353 cycles
INTERCOSTAL FLANGE FROM FRAME 86 - FRAME 87, STRINGER 36 IS CRACKED. REMOVED CRACKED FLANGE IAW SRM 51-40-21, PARA 7. LOCATED AND DRILLED NEW FLANGE IAW SRM 51-40-44, PG 1. ALODINED AND PRIMED IAW AMM 51-23-10-0 PARA 1. INSTALLED NEW FLANGE IAW SRM 51-40-21; PARA 7. PAINTED FLANGE IAW SRM AMM 51-23-10-0, PARA 1.
Part: PANEL — DELAMINATED (ZONE 500) · airframe 37,839 hrs · 14,353 cycles
LEFT WING TRAILING PANEL NR 572 LB HAS THE TOP SURFACE LAMINATE PEELED. REPAIRED PANEL NR 572 LB BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND REFINISHING IAW FEDEX DWG SR 27-53-011 AND FEDEX EA 6-5720-127921 "WINGS - LT WING FLAP HINGE DEFLECTOR PANELS NR 572 GB, 572 CB AND 572 LB".
Part: PANEL — WORN (ZONE 500) · airframe 37,839 hrs · 14,353 cycles
THE OTBD CORNER UPPER SURFACE IS WORN AT LEFT WING 2ND FROM INBD TRAILING EDGE DROP DOWN PANEL NR 572 CB. REPAIRED OTBD FWD UPPER CORNER OF THE PANEL BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND REFINISHING IAW DWG SR 27-53-011 AND EA 6-5720-127921.
Part: BLOCKER DOOR — GOUGED (THRUST REVERSER) · airframe 37,839 hrs · 14,353 cycles
NR 2 ENGINE OTBD T/R UPPER BLOCKER DOOR IS GOUGED IN THE AFT SIDE. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW EA 6-7830-127923. REINSTALLED DOOR IAW AMM 78-32-13-4. OPS CHECK GOOD IAW AMM 78-32-11-5.
Part: PANEL — DELAMINATED (ZONE 500) · airframe 37,839 hrs · 14,353 cycles
LEFT WING TRAILING EDGE PANEL NR 572 GB HAS THE TOP LAMINATE PEELING. REPAIRED PANEL NR 572 GB BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND REFINISHING IAW DWG SR 27-53-011 AND EA 6-5720-127921.
Part: RETAINER — GOUGED (THRUST REVERSER) · airframe 37,839 hrs · 14,353 cycles
NR 2 ENGINE OTBD T/R 5TH FROM TOP BLOCKER DOOR IS GOUGED IN THE AFT SIDE. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW EA 6-7830-127923 "EXHAUST SYSTEM - NR 2 ENGINE OTBD T/R BLOCKER DOORS SEAL RETAINER GOUGE". REINSTALLED DOOR IAW AMM 78-32-13-4. OPS CHECK GOOD IAW AMM 78-32-11-5.
Part: SKIN — CRACKED (ZONE 600) · airframe 37,839 hrs · 14,353 cycles
THE RIGHT INBD FLAP SKIN A57960007001 REMOVED ON E 6-5750-7-5003 PT 2 HAS A CRACK AT THE AFT END. COMPLIED WITH EA 6-5720-127917.
Part: DUCT — CRACKED (ZONE 100) · airframe 37,839 hrs · 14,353 cycles
LEFT PACK LOWER DUCT FROM THE HEAT EXCHANGER TO THE ACM HAS A CRACK APPROX 1.5 INCH LONG. REMOVED DUCT ASSY AS REQUIRED REF A300-600 AMM 21-51-32. PERFORMED WELD REPAIR REF DRM, PARA 4-C. ACCOMPLISHED FPI REF NTM 51-90-00 PT9 PER EA 6-2150-127942 "AIR CONDITIONING, LT PACK DUCT CRACK". NO CRACKS NOTED. REINSTALLED DUCT REF AMM 21-51-32. PERFORMED LEAK CHECK REF AMM 21-51-00. LEAK CHECK GOOD.
Part: RETAINER — GOUGED (THRUST REVERSER) · airframe 37,839 hrs · 14,353 cycles
NR 2 ENGINE OTBD T/R 4TH FROM TOP BLOCKER DOOR IS GOUGED IN THE AFT SIDE. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW EA 6-7830-127923 "EXHAUST SYSTEM - NR 2 ENGINE OTBD T/R BLOCKER DOORS SEAL RETAINER GOUGE". REINSTALLED DOOR IAW AMM 78-32-13-4. OPS CHECK GOOD IAW AMM 78-32-11-5.
Part: PANEL — DELAMINATED (ZONE 500) · airframe 37,839 hrs · 14,353 cycles
FOIL IS DISBONDED ON THE UPPER SURFACE OF THE 2ND PANEL FROM INBD, LEFT WING DROP DOWN TRAILING EDGE PANEL NR 572 CB. REPAIRED FLAP DIFFUSER PANEL INNER SKIN BY REMOVING DAMAGED ALUMINUM FOIL AND REPLACING IT WITH EXPANDED COPPER SCREEN AND BONDING IT IN PLACE AND REFINISHING IAW DWG SR 27-53-011 AND FEDEX EA 6-5720-127921.
Part: RETAINER — GOUGED (THRUST REVERSER) · airframe 37,839 hrs · 14,353 cycles
NR 2 ENGINE O/B T/R 3RD FROM TOP BLOCKER DOOR IS GOUGED IN THE AFT SIDE. REMOVED BLOCKER DOOR IAW AMM 78-32-13-4. REPAIRED DOOR IAW E.A. 6-7830-127923 " EHHAUST SYSTEM - NR 2 ENGINE OUTBD T/R BLOCKER DOORS SEAL RETAINER GOUGE". REINSTALLED DOOR IAW AMM 78-32-13-4. OPS CHECK GOOD IAW AMM 78-32-11-5.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 37,839 hrs · 14,353 cycles
MAIN CARGO DECK SEAT TRACK IS GOUGED BETWEEN FRAME 60 AND FRAME 61, LBL 37.5. REMOVED FLOORBOARD IAW SRM 51-40-20, PG 5. REMOVED SEAT TRACK SECTION IAW SRM 53-10-16, FIG 201. LOCATED AND DRILLED NEW SEAT TRACK SECTION P/N A53274005202000, PO 633379.1 AND NEW SEAT TRACK SPLICE P/N R532704902000, PO 632784.3 IAW SRM 53-10-16, FIG 201. INSTALLED SEAT TRACK AND SPLICE IAW SRM 51-40-21, PG 7. INSTALLED FLOORBOARD IAW SRM 51-40-21, PG 5.
Part: ATTACH BRACKET — BROKEN (FAIRING) · airframe 37,839 hrs · 14,353 cycles
FAIRING 636 BB LEFT AND RIGHT AFT ATTACH BRACKETS, SAFETY WIRE ATTACH POINTS ARE BROKEN. COMPLIED WITH E.A. 6-5750-127916.
Part: ATTACH BRACKET — BROKEN (FAIRING) · airframe 37,839 hrs · 14,353 cycles
FAIRING 635 BB LEFT AFT ATTACH BRACKET, SAFETY WIRE ATTACH POINT IS BROKEN. SAFETY WIRED BOLTS PER EA 6-5750-127916. NO FURTHER ACTION IS REQUIRED.
Part: ATTACH BRACKET — BROKEN (FAIRING) · airframe 37,839 hrs · 14,353 cycles
FAIRING 632 BB RIGHT AFT ATTACH BRACKET, SAFETY WIRE ATTACH POINT IS BROKEN. SAFETY WIRED BOLTS PER EA 6-5750-127916.
Part: RIB — DAMAGED (LT WING TE FLAP) · airframe 37,839 hrs · 14,353 cycles
WHILE PEFORMING EA 6-5750-5000 PT3 "WINGS - INBD FLAP NOSE RIB 7 REPLACEMENT LT"; SEVERAL HOLES WERE FOUND TO BE ELONGATED. COMPLIED WITH EA 6-5750-127920.
Part: SKIN — GOUGED (FUSELAGE) · airframe 37,839 hrs · 14,353 cycles
FUSELAGE EXTERNAL SKIN HAS A GOUGE AT FRAME 20, S39R. REMOVED GOUGE IAW SRM 51-73-10 AND IS FOUND TO BE OUT OF LIMITS IAW SRM 50-10-00. CUTOUT DAMAGE IAW SRM 53-10-12. ALODINED IAW SRM 51-21-10. PRIMED & PAINTED IAW SRM 51-23-10. INSTALLED FILLER & DOUBLER IAW SRM 51-40-21.
2007
Part: SKIN — CRACKED (ZONE 600) · airframe 34,720 hrs · 12,755 cycles
FOUND CORROSION ON BOTTOM SKIN, MLG REINFORCING PLATE RT WING. NDT DETECTED A CRACK IN HOLE NR 552. REPAIR WAS PERFORMED IAW RAS/BAE/1003853/2006 ISS.: A AND EA 6-5720-103395.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
FOUND CORROSION ON CORNER FITTING C63, P43 LT AND ON CROSSBEAM C61, P45 LT AND C58, P47 RT. REPAIR WAS PERFORMED BY REPLACE A NEW FITTING IAW SRM 51-72-10 AND SRM 53-17-15, FIG 5. CROSSBEAM REPAIR WAS PERFORMED IAW SRM 53-10-15/FIG 208 SEE ALSO SRM 53-16-15 / FIG 5 AND SRM 53-10-15 FIG 208 SEE ALSO SRM 53-17-15 FIG 10.
Part: STRUCTURE — DAMAGED (WING) · airframe 34,720 hrs · 12,755 cycles
DAMAGED HOLES FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-3305, HOLES L/U/I/K ON LT AND K ON RT. REPAIR WAS PERFORMED IAW. RAS 033237/026/2004 ISSUE: A AND EA 6-5710-106351.
Part: SKIN — MISREPAIRED (ZONE 500) · airframe 34,720 hrs · 12,755 cycles
FOUND OLD CORROSION REPAIR ON UPPER WING SKIN LT, CLOSED TO RIB 5. REPAIR WAS VERIEFIED IAW RAS/BAE/0937/2004 ISSUE B AND CAL EO AB6-57-00-0057R1. THE REPAIR DIDN'T CORRESPOND WITH THE DOCUMENTS. THE REPAIR WAS ACCOMPLISHED IN THE FOLLOW DR 456.
Part: PLATE — DAMAGED (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
FOUND OLD REPAIR ON REAR CARGO DOOR SEALING PLATE C60-C60A IN FUSELAGE ABOVE DOOR. OLD REPAIR WAS VERIFICATION THAT IT IS PERFORMED IAW RAS DA/HAM-1083/98 ISSUE B.
Part: STRUCTURE — DAMAGED (WING) · airframe 34,720 hrs · 12,755 cycles
DAMAGED HOLES FOUND DURING ACCOMPLISHMENT OF EO 6-5710-7-3305. HOLES H/I ON LT AND L/K ON RT. REPAIR WAS PERFORMED IAW RAS 033237/026/2004 ISSUE: A AND EA 6-5710-106351.
Part: SKIN — CORRODED (ZONE 500) · airframe 34,720 hrs · 12,755 cycles
OLD REPAIR ON LT SLAT NR 3 LEADING EDGE, BY AN EXTERNAL PATCH, FASTENERS WERE CORRODED AND SOME HOLE DIAMETERS ARE OVERSIZE. REPAIR WAS PERFORMED IAW TD FOK/308/2006 ISSUE A BY EA 6-5744-106357.
Part: REPAIR — UNKNOWN (WING) · airframe 34,720 hrs · 12,755 cycles
FOUND OLD REPAIR BY INSTALLATION OVERSIZE FASTENERS, HOLE 2 LT, 187 RT AND 165 RT. REPAIR VERIFICATION OF OVERSIZED FASTENERS IAW RAS 033237/017/2004 ISSUE: A AND EA 6-5710-106363.
Part: STRINGER — CORRODED (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
CORROSION ON MILLED STRINGER P56 RT/LT BETWEEN C76/77 AND ON OUTER SKIN BETWEEN C76/77, FOUND AFTER REMOVING TAIL BUMPER. REPAIR WAS PERFORMED IAW RAS/DATLS/0003476/2006 ISSUE: B AND EA 6-5318-103383.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
AFTER REMOVAL OF AN OLD FLUSH DOUBLER BETWEEN C70/71, P45/46 RT, AN OLD CORRODED REWORKED AREA WAS FOUND AT INNER SKIN SHEET. REPAIR WAS PERFORMED IAW SRM 53-10-12, FIG 229 SHEET 1 AND SRM 53-10-14, FIG 201 SHEET 1, APPROVED BY EA 6-5317-106349.
Part: PANEL — CRACKED (NR 2 NACELLE) · airframe 34,720 hrs · 12,755 cycles
FOUND CRACK AT PYLON NR 2 RT ON AREA AT LOWER SIDE PANEL AT RIB 18 INBOARD. REPAIR WAS PERFORMED IAW RAS 048245/005/2006 ISSUE: A AND EA 6-5451-103394.
Part: SKIN — DAMAGED (LT WING) · airframe 34,720 hrs · 12,755 cycles
ON LT WING LOWER SKIN PANEL AFT FROM PYLON NR 1 ARE ELONGATED HOLES ON HYDRAULIC FITTINGS. REPAIR WAS PERFORMED IAW RAS/BAE/1003815/2006 ISSUE: A, APPROVED BY EA 6-5720-103392.
Part: DOOR — DELAMINATED (ZONE 700) · airframe 34,720 hrs · 12,755 cycles
THE FWD LOWER CORNER OF THE RT NOSE LANDING GEAR DOOR WAS DAMAGED. REPAIR WAS PERFORMED IAW RAS/CASA/5273/2007 ISSUE: A, APPROVED BY EA 6-5282-106412.
Part: DOOR — DENTED (ZONE 800) · airframe 34,720 hrs · 12,755 cycles
DENT ON RT MAIN LANDING GEAR DOOR. REPAIR WAS PERFORMED IAW RAS 048387/0082006 ISSUE: A, APPROVED BY EA 6-5281-103396.
Part: WEB — DENTED (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
WEB PLATES OF BULK CARGO DOOR TORSION BOX FWD AND AFT C68 BETWEEN P33 AND P36 RH DENTED AND SCRATCHED. REPAIR WAS PERFORMED BY DRESSED BACK DENTS AND REWORK OF AFFECTED WEB PLATES IAW RAS/DAHAM/4021476/2006 AND EA 6-5317-106348.
Part: PLATE — CHAFED (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
FOUND CHAFING MARKS ON TORSION PLATE C86 RT. REPLACEMENT WAS PERFORMED IAW SRM 51-72-10.
Part: SKIN — CORRODED (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
FOUND CORROSION ON INNER SKIN BETWEEN C55/56 BETWEEN STRINGER 55/56 RT AND 55/56 LT, AND CORROSION ON STRINGER 45 RT BETWEEN C57.3-58 AND STRINGER 51 LT BETWEEN C57.3-58. REPAIR WAS PERFORMED IAW RAS/DATLS/0003480/2006 ISS.A (CORROSION REWORK), APPROVED BY EA 6-5316-103387.
Part: CROSSBEAM — NONE (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
OLD REPAIRS ON CROSSBEAM C60 WITHOUT ANY OLD RECORDS CROSSBEAM WAS REPLACED BY NEW PART IAW SRM 51-72-10.
Part: SPAR — CORRODED (ZONE 600) · airframe 34,720 hrs · 12,755 cycles
OLD BLEND OUT REPAIR ON RT OUTER WING AT PANEL 3, BOTTOM SKIN, CLOSED TO RIB 28 ON REAR SPAR REPAIR WAS PERFORMED BY BLEND OUT THE CORROSION WITH CAL EO AB 6-57-00-0001 AND APPROVED BY RAS/BAE/0573/2002 ISS. A
Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
FOUND CORROSION SPOTS ON AFT CARGO DOOR SILL BEAM A539-73085-210 BETWEEN C 59-63 REPAIR WAS PERFORMED IAW RAS/DATLS/0003479/2006 ISS.A (FLANGE REPAIR AND CORROSION REWORK), APPROVED BY EA 6-5317-103384.
Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
FOUND CROSS BEAM ATTACHMENT PROFILE (SRM 53-17-15 FIG.10 ITEM 455) AT C61 RT CORRODED REPLACEMENT OF RELATED PART WAS PERFORMED IAW SRM 51-72-10.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
STRINGER P50 LT BETWEEN C72 AND C73 CORRODED AND CONNECTION SECTION AT C72, P50 LT CORRODED STRINGER REPAIR WAS PERFORMED IAW SRM 53-10-14 FIG 201 AND REPLACEMENT OF CORRODED CONNECTING SECTION WAS PERFORMED IAW SRM 51-72-10.
Part: CROSSBEAM — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
FOUND CROSSBEAM ATTACHMENT PROFILE IS CORRODED ON C67 RT REPLACEMENT OF CORRODED PART IAW SRM 51-72-10.
Part: ATTACH FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
FOUND CORRODED CLIP AT C35 BETWEEN P43-44 LT AND STRINGER P 44 BETWEEN C35-C36, LT CORROSION REPAIR WAS PERFORMED BY REPLACEMENT OF CLIP IAW SRM 51-72-10 AND STRINGER REPAIR IAW SRM 53-10-14 FIG 201.
Part: SKIN — CORRODED (ZONE 500) · airframe 34,720 hrs · 12,755 cycles
OLD CORROSION REPAIR ON LT OUTER WING, BOTTOM SKIN, NEAR RIB 21 REPAIR WAS PERFORMED BY BLEND OUT THE CORROSION WITH CAL EO AB 6-57-00-0023 AND APPROVED BY RAS/BAE/0701/2003 ISS.A AND EA 6-5720-106353.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
FOUND STRINGER P50 LT AT C70 CORRODED STRINGER REPAIR WAS PERFORMED IAW SRM 53-10-14 FIG 201.
Part: RIB — CRACKED (TE FLAP) · airframe 34,720 hrs · 12,755 cycles
OLD REPAIR ON RT INNER FLAP RIB 25 CRACK FINDING (3, 5 INCHES) DURING SB A300-57-6098 EMBODIMENT REPAIR WAS PERFORMED WITH CAL EO AB6-57-00-0063 AND APPROVED BY RAS/FOK/176/2004.
Part: BULKHEAD — DAMAGED (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
TOOLING MARKS FOUND ON AFT PRESSURE BULKHEAD AT ME15, C80/82. REPAIR WAS PERFORMED IAW RAS/DAHAM/4021516/2006 ISS. A (BLEND OUT, FASTENER REPLACEMENT), APPROVED BY EA 6-5319-103386.
Part: SILL — CORRODED (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
ANGLE BRACKET AT DOOR SILL C24A-25 IS DAMAGED AND CORRODED PART WAS REPLACED IAW SRM 51-72-10.
Part: BEAM — CORRODED (ZONE 600) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
DURING KRUEGER FLAP INSTALLATION, RT WING, FOUND BEAM A535-10218-201 CORRODED REPLACEMENT OF CORRODED BEAM IAW SRM 57-45-11.
Part: FLOOR SUPPORT — CRACKED (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
FLOOR STRUCTURE BETWEEN C10 AND C12A ANGLE CRACKED REPLACEMENT OF CRACKED ANGLE IAW SRM 51-72-10.
Part: SKIN — DAMAGED (ZONE 100) · airframe 34,720 hrs · 12,755 cycles
FOUND SEVERAL SCRUB MARKS ON SKIN PANEL BETWEEN C56-C57, P34-P35 LT AND RT. REPAIR WAS PERFORMED IAW RAS/DATLS/0003483/2006 ISS. A (BLEND OUT), APPROVED BY EA 6-5316-103385.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
FOUND CORRODED STRINGER P46RH, C60-C60A REPAIR WAS PERFORMED IAW RAS/DATLS/0003135/2006 ISS.A, STRINGER SPLICE REPAIR WITH DWR 17 R539 70094B), APPROVED ALSO BY EA 6-5317-106347.
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
FOUND CORROSION ON STRINGER P55 LT BETWEEN C69-C70. REPAIR WAS PERFORMED IAW SRM 53-10-14 FIG 201.
Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 34,720 hrs · 12,755 cycles
CORROSION SPOTS ON TOP CAP BEAM OF SILL BEAM C59-C64 REPAIR PERFORMED IAW, RAS/ DATLS/0003479/2006 ISS A APPROVED BY EA 6-5317-103384.
Part: DOOR — UNKNOWN · airframe 34,720 hrs · 12,755 cycles
EXTERNAL DOUBLER ON FWD PAX DOOR RT SIDE LOWER EDGE REPAIR WAS PERFORMED IAW RAS 025042/011/2003.