Airbus Industrie A300 B4-605R

Service difficulty reports · 2,994

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A300B4605R'
  ORDER BY difficulty_date DESC"

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SDR FDEA202609271454Spoiler · delaminatedRIGHT WING SPOILER NR 5. CENTER OTBD HINGE ARM, OTBD SURFACE FOUND DELAMINATED. COMPLIED WITH EA: 6-5750-T0388918 P1 TO REPAIR RT WING SPOILER NR 5 CENTER OTBD HINGE ARM, OTBD SURFACE DELAMINATION. THIS IS CATEGORY A REPAIR. MAJOR REPAIR IAW GMM 6-2-100.Sep 27, 2026 · N731FD · Airbus A300B4605R · SpoilersSDR FDEA202609161354Seat Track · damagedSEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080. AMM 53-10-16-06 SEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080 MEL: 25-50-02-01-J LOCKED REMOVED AND PLACED IN CLOSET PER WRI 25-50/0129. C/7462504 . REMOVED THE DAMAGED SEAT TRACK IAW SRM 51-40-21. FASep 16, 2026 · N733FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202609091463Fitting · damagedCARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24 COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MASep 9, 2026 · N731FD · Airbus A300B4605R · Cargo/Baggage DoorsSDR FDEA202609061306Repair · noneEXISTING REPAIR ON RUDDER TRAILING EDGE RH AFT LOWER SKIN BTW RR0-BR1 REQUIRES EVALUATION FOR CONFORMITY. EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM 55-41-12-201 FIGURE 208A BUT NO RECORD FOUND.EO:6-5100-7-5000 E PART 1 WAS COMPLETED.TITLE:STRUCTSep 6, 2026 · N731FD · Airbus A300B4605R · Standard Practices/StructuresSDR FDEA202609051321Repair · noneEXISTING REPAIR ON FRAME FR12 AT 8-9 O'CLOCK REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FRAME FR12 AT 8-9 O'CLOCK WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600 SRM53-12-13-201 FIG.201.REPORTED TO FEDEX ENGINEERING.EO 6- 5100-7-500Sep 5, 2026 · N731FD · Airbus A300B4605R · Standard Practices/StructuresSDR FDEA202609041453Backboard · puncturedLH PAX DOOR SLIDE BACK-PLATE PUNCTURED. REPLACED THE LH PASSENGER/CREW DOOR SLIDE/RAFT PER AMM 25-61-22-04-01. MINOR REPAIR IAW FEDEX GMM 6-2-100.Sep 4, 2026 · N731FD · Airbus A300B4605R · Escape SlideSDR FDEA202609041305Repair · misinstalledEXISTING REPAIR ON FWD CARGO FLOOR BEAM AT FR30,Y140~Y805 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FWD CARGO FLOOR BEAM AT FR30,Y140~Y805 WAS EVALUATED AND FOUND NO APPLICABLE REPAIR IN A300-600 SRM FOR THE EXISTING REPAIR.NO RECORD FOSep 4, 2026 · N731FD · Airbus A300B4605R · Standard Practices/StructuresSDR FDEA202609041304Repair · no discrepancyEXISTING REPAIR ON FWD CARGO ROLLER TRACK AT -Y140 BETWEEN FR35 AND FR36 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON FWD CARGO ROLLER TRACK AT -Y140 BETWEEN FR35 AND FR36 WAS EVALUATED AND FOUND IN CONFORMITY WITH SRM53-10-15-201 FIG.203. NSep 4, 2026 · N731FD · Airbus A300B4605R · Standard Practices/StructuresSDR FDEA202609031303Roller Track · misrepairedEXISTING REPAIR ON AFT CARGO ROLLER TRACK AT Y805 BETWEEN FR59 AND FR60 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON AFT CARGO ROLLER TRACK AT Y805 BETWEEN FR59 AND FR60 WAS EVALUATED AND FOUND NOT IN CONFORMITY WITH A300-600 SRM53-10-15 FIGSep 3, 2026 · N731FD · Airbus A300B4605R · Fuselage Main, StructureSDR FDEA202608071099Skin · crackedMAIN DECK CARGO DOOR UPPER EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 4 EA FASTENER HOLES. REPAIRED THE FASTENER HOLES ON THE MAIN DECK CARGO DOOR UPPER EDGE AT PT1 BETWEEN FR22 & FR25 IAW EA 6-5230-T0388329, P1. MAJOR REPAIR IAW GMM 6-2-100.Aug 7, 2026 · N733FD · Airbus A300B4605R · Cargo/Baggage DoorsSDR FDEA202608051111Skin Panel · crackedFUSELAGE FRAME, FR 54 LATERAL PANEL THREE HOLES CRACKED AT STRINGER 36L, 44L - 44R. COMPLIED WITH EA 6-5330-T0388383 P1 REPAIRED THE FUSELAGE FRAME FR54 LATERAL PANEL 3EA CRACKED HOLES AT S36L S44L S44R. EA TITLE: FUSELAGE - PLATES & SKINS - CRACK HOLES OAug 5, 2026 · N733FD · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR FDEA202608021117Fitting · damagedCARGO DOOR, HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 C P5. REPLACED THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS. MAJOR REAug 2, 2026 · N733FD · Airbus A300B4605R · Cargo/Baggage DoorsSDR FDEA202608011089Skin · contaminatedLEFT ELEVATOR LOWER SURFACE HAS 1EA TRAPPED WATER AT ER5. REPAIRED LH ELEVATOR LOWER SURFACE ER5 TRAPPED WATER IAW SRM 55-21-12-201-2, PARA.5.J & SRM 51-77-12-201. THIS IS CAT B REPAIR AND THE FOLLOW UP INSPECTION IS TRACKED BY EA 6-5520-T0388407. MAJOR REAug 1, 2026 · N733FD · Airbus A300B4605R · Elevator, Plate/SkinSDR FDEA202608011088Skin · contaminatedLEFT ELEVATOR UPPER SURFACE HAS 3EA TRAPPED WATER AT ER10. REPAIRED LT ELEVATOR UPPER ER10 TRAPPED WATER IAW SRM55-21-12-201-2 PARA.5.J & SRM 51-77-12-201. THIS IS CAT B REPAIR AND THE FOLLOW UP INSPECTION IS TRACKED BY EA 6- 5520-T0388407, MAJOR REPAIR IAAug 1, 2026 · N733FD · Airbus A300B4605R · Elevator, Plate/SkinSDR FDEA202608011087Floorbeam · corrodedFUSELAGE SKIN INTERNAL BEAM CORRODED AT FR39 S50L - S54L. COMPLIED WITH EA 6-5310-T0388500 P1 REPAIRED THE FWD CARGO COMPARTMENT FR39 LOWER TEE BEAM CORROSION BETWEEN STGR51L AND STGR54L. EA TITLE: FUSELAGE - MAINFRAME - FR39 LOWER TEE BEAM CORROSION BETWEEAug 1, 2026 · N733FD · Airbus A300B4605R · Fuselage Main, Floor BeamSDR FDEA202607311110Reinforcement · corrodedAFT CARGO COMPARTMENT LOWER INTERNAL REINFORCING RING AND STRINGER FITTING CORRODED AT FR 54, STRINGERS 44R - 45R. FUSELAGE - MAINFRAME - FR54 TEE SECTION CORROSION BETWEEN STGR44RH AND 45RH. THIS REPAIR IS CONSIDERED AS CAT B REPAIR DUE TO AWAITING FURJul 31, 2026 · N733FD · Airbus A300B4605R · Fuselage Main, StructureSDR FDEA202607291098Door Frame · crackedRT PAX DOOR FRAME SEGMENT AT FR14C FOUND 2EA CRACKS. REPLACED THE CRACKED SEGMENT ON RH PAX DOOR FRAME AT FR14C IAW SRM 51-40-21 AND DWG F52181299(ISSUE: G). RSC TRACKING EA: 6-5210-T0387549 RAISED AND ACCOMPLISHED. THIS IS A CATEGORY A REPAIR. MAJOR REPAIJul 29, 2026 · N733FD · Airbus A300B4605R · Fuselage Main, StructureSDR FDEA202607291079Cargo Track · corrodedMDC LOADING SYS TRACK Y450 CORRODED AT FR18 - FR19. REPLACED THE MDC CORRODED LOADING SYS TRACK AT FR18 - FR19 Y450 PER SRM 51-40-21 & DWG A53612518 (ISSUE.A00). THIS IS CAT A REPAIR, MAJOR REPAIR IAW GMM6-2- 100.Jul 29, 2026 · N733FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607291078Cargo Track · corrodedMDC LOADING SYS TRACK Y953 CORRODED AT FR18 - FR19. REPLACED THE MDC CORRODED LOADING SYS TRACK AT FR18 - FR19 Y953 IAW SRM 51-40-21 & DWG: A53615224 (ISSUE.A00). THIS IS CAT A REPAIR MAJOR REPAIR IAW GMM6-2-100.Jul 29, 2026 · N733FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202607251077Seat Track · damagedSEAT TRACK LOBE DAMAGED UNDER MDC LOCK ML1080. REPLACED THE MDC CORRODED LOADING SYS TRACK AT FR40 - FR45 -Y450 PER A300-600 SRM51-40-21 & DWG A53832020, ISSUE: J. THIS IS CAT A REPAIR, MAJOR REPAIR IAW GMM6-2-100.Jul 25, 2026 · N733FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202605090576Pump · low pressureON TAKEOFF ROLL AT 30KTS, RECEIVED A YELLOW HYD PUMP LOW PR ECAM. TAKEOFF WAS REJECTED. ECAM CLEARED ON ITS OWN SHORTLY AFTER. 2ND ATTEMPT WAS MADE, SAME RESULT. RETURNED TO GATE.May 9, 2026 · N731FD · Airbus A300B4605R · Hydraulic Pump (Electric/Engine), MainSDR FDEA202602250278Skin · chafedRH WING INNER FLAP UPR SKIN FOUND CHAFE MARKS BETWEEN RIB16 AND RIB17. REPAIRED THE DAMAGED UPR SKIN IN RH WING INNER FLAP BETWEEN RIB16 AND RIB17 PER SRM57-50-00-201 PARA.4E. TRACKING EA 6-5750-T0386734 RAISED AND ACCOMPLISHED. REPAIR. MAJOR REPAIR IAW GMMFeb 25, 2026 · N746FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA202602130218Mount · corrodedWHILE WORKING WRI 25-60/9552 FOR R1 FEA SLIDE INSPECTION, THE AMTS FOUND CORROSION AND 2 SCREWS BROKEN. REMOVED R1 SLIDE PER REF ABOVE.Feb 13, 2026 · N733FD · Airbus A300B4605R · Escape SlideSDR FDEA202503180442Power Supply · unknownR1 DOOR SLIDE WILL NOT ARM. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE." AMM: 52-73-00-05-01 ALONG WITH NO SLIDE ARMED INDICATION, T/S'G NOTATED THAT BOTH R-1Mar 18, 2025 · N732FD · Airbus A300B4605R · Emergency ExitsSDR FDEA202502140229Pseu · failedSHORTLY AFTER TAKEOFF, THE FOLLOWING EVENTS OCCURRED: ECAM CAPT TAT HEAT FAULT, BOTH AUTOTHROTTLES CAME OFF, #1 PITCH TRIM LEVER CAME OFF, CAPTAIN SIDE FLIGHT DIRECTOR GONE, CABIN PRESSURE REGULATOR #1 FAULT. PITOT FAULT LIGHTS ON ALL THREE SYSTEMS ILLUMIFeb 14, 2025 · N732FD · Airbus A300B4605R · Autopilot SystemSDR FDEA202502140228Altimeter · failedDURING THE CLIMB, FOS ALTIMETER WAS ERRATIC, FLUCTUATING ABOUT 500FT. PERFORMED PITOT STATIC TEST AND PUMPED UP AIRSPEED AND ALTITUDE, NOTED BOTH CAPTAIN'S AND FIRST OFFICERS ALTIMETERS CLIMBED EVENLY WITH NO ERRADIC FLUCUATIONS NOTED REF A300-600 M/M. REMOVFeb 14, 2025 · N732FD · Airbus A300B4605R · Altimeter, Barometric/EncoderSDR FDEA202502140227Button · jammedUPON TROUBLESHOOTING OF WRI 33-20/8722 FOUND THAT COURIER EMERGENCY TEST BUTTON JAMMED TOO AND NOT WORKING. CLEANED SWITCH REF ESPM 20-55-50-0 , OPS CKS OK M/M 33-20-00-00-09.Feb 14, 2025 · N733FD · Airbus A300B4605R · Emergency LightingSDR FDEA202412091791Buffer · out of adjustR1 DOOR GUST LOCK (DOOR STAY) INOP. ADJUSTED DOOR BUFFER ON R1 DOOR IAW AMM 52-10-11-05-01 OPS CHECK GOOD.Dec 9, 2024 · N732FD · Airbus A300B4605R · Passenger/Crew DoorsSDR FDEA202411061637Cover · installedTHERE WAS A 40 KNOT DIFFERENCE BETWEEN CAPT S AND F/O AIRSPEED INDICATION ON TAKEOFF ROLL. CAPT REJECTED T/O AT APPROXIMATELY 80 KNOTS. ON WALK AROUND, FOUND CAPT PITOT COVER INSTALLED. REMOVED IAW AMM 10-11-00-02. NO FURTHER DEFECTS NOTED, A/C OK FOR FLIGNov 6, 2024 · N731FD · Airbus A300B4605R · Pitot/Static SystemSDR FDEA202408161130Contactor · failedRIGHT AFTER TAKING THE RUNWAY FOR TAKEOFF, PRIOR TO ENGINE RUN UP, GOT A GEN 1 FAULT. ATTEMPTED ONE RESET IAW QRH/ECAM, BUT FAULTED AGAIN. AMM: 24-22-18-04 ESPM: 20-46-50 REMOVED AND REPLACED TRANSFER CONTACTOR 11XU AND LINE CONTACTOR CONTROL RELAY 13XU REF AAug 16, 2024 · N733FD · Airbus A300B4605R · AC Generator-AlternatorSDR FDEA202408021150Web · deformedAFT FUSELAGE SKIN 1EA SUPPORT WEB GOT DEFORM AT FR86-87, S-35R REPLACED THE DAMAGE SUPPORT WEB WITH NEW AT AFT FUSELAGE SKIN FR 86-87, S-35R I.A.W A300-600 SRM 51-72-10-001, PAGE 2 THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.Aug 2, 2024 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA202408021149Web · deformedAFT FUSELAGE SKIN 1EA SUPPORT WEB GOT DEFORM AT FR85-86, S-33R REPLACED THE DAMAGE SUPPORT WEB WITH NEW AT AFT FUSELAGE SKIN FR 85-86, S-33R I.A.W A300-600 SRM 51-72-10-001, PAGE 2 THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.Aug 2, 2024 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA202408011166Skin · noneAIRCRAFT REPAIR ASSESSMENT: EXISTING FLUSH DOULBER REPAIR FOUND ON LH SLAT #1 LEADING EDGE SKIN AT END RIB2A 5.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIAug 1, 2024 · N732FD · Airbus A300B4605R · Leading Edge DevicesSDR FDEA202408011155Seat Track · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING SLPIECE REPAIR FOUND ON MDCC SEAT TRACK BTW FR66 ~ 68, Y450 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 1Aug 1, 2024 · N732FD · Airbus A300B4605R · Standard Practices/StructuresSDR FDEA202408011153Seat Track · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING SLPIECE REPAIR FOUND ON MDCC SEAT TRACK BTW FR62 ~ 65, -Y450 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR Aug 1, 2024 · N732FD · Airbus A300B4605R · Standard Practices/StructuresSDR FDEA202408011141Seat Track · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON MDCC SEATTRACK BTW FR66~68, -Y450 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.Aug 1, 2024 · N732FD · Airbus A300B4605R · Standard Practices/StructuresSDR FDEA202407301192Crossbeam · gougedMAIN DECK CARGO COMPARTMENT FLOOR SEAT TRACK CROWN GOUGE AT FR52 Y80 FABRICATED THE CROSSBEAM WITH RAW MATERIAL AND REPLACED ON MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE AT FR52 BETWEEN Y0 TO Y450 I.A.W AIRBUS DRAWING Y53825515 AND FEDEX GMM 07-0-1001. AJul 30, 2024 · N732FD · Airbus A300B4605R · Fuselage Main, StructureSDR FDEA202407301165Rib · wornFOUND RH #5 SPOILER O/B SIDE JACK RIB LOWER HOLE DAMAGE ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER O/B SIDE JACK RIB LOWER HOLE I.A.W FEDEX EA NO:T6-5740-T0380260 P1, SEQ NO:761, TITLE:WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA 18Jul 30, 2024 · N732FD · Airbus A300B4605R · SpoilersSDR FDEA202407301164Rib · wornFOUND RH #5 SPOILER O/B SIDE JACK RIB UPPER HOLE DAMAGE ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER O/B SIDE JACK RIB UPPER HOLE I.A.W FEDEX EA NO:T6-5740-T0380260 P1, SEQ NO:761, TITLE:WINGS-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA 18Jul 30, 2024 · N732FD · Airbus A300B4605R · SpoilersSDR FDEA202407301152Seat Track · gougedMAIN DECK CGO COMP'T FLOOR SEAT TRACK CROWN GOUGE AT FR39 PLUS 16", Y1456 REPLACED THE DAMAGED SEAT TRACK WITH NEW PART ON MAIN DECK CARGO COMPARTMENT FLOOR AT FR39 PLUS 16", Y1456. I.A.W A300-600 SRM 51-40-21-001, PARA.7, PAGE.24~PAGE.50. THIS REPAIR IS CJul 30, 2024 · N732FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202407301151Seat Track · crackedMAIN DECK CGO COMP'T FLOOR SEAT TRACK CRACK ABOUT 1-1/2" AT FR42 PLUS 6" -Y450 REPLACED THE SEAT TRACK WITH NEW PART AT FR40~FR45, Y-450. I.A.W A300-600 SRM 51-72-10- 001, P2. THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.Jul 30, 2024 · N732FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202407291163Seat Track · corrodedMAIN DECK COURIER AREA FLOOR SEAT TRACK THROAT CORROSION AT FR17 PLUS 22", -Y450 REPLACED THE SEAT TRACK WITH NEW PART IAW SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.Jul 29, 2024 · N732FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202407291162Seat Track · corrodedMAIN DECK COURIER AREA FLOOR SEAT TRACK THROAT CORROSION AT FR17 PLUS 22", Y450 REPLACED THE SEAT TRACK WITH NEW PART I.A.W A300-600 SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.Jul 29, 2024 · N732FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202407291139Seat Track · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON MDCC SEATTRACK BTW FR37~38, Y0 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707Jul 29, 2024 · N732FD · Airbus A300B4605R · Standard Practices/StructuresSDR FDEA202407281156Stiffener · crackedCENTER WING BOX MID SPAR VERTICAL STIFFENER GOT CRACK AT FR44,Y1456~Y1959 POSITION. FABRICATED AND INSTALLED NEW STIFFENER AT CENTER WING BOX FR44, Y1456~Y1959 I.A.W AIRBUS DRAWING A57110436 & GMM 7-0-1001 & EA NO:T6-5710-T0380275 P1, SEQ NO:760, TITLE:WIJul 28, 2024 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA202407281121Shear Web · crackedMAIN DECK FLOOR SHEAR WEB BROKEN AT FR77 -Y1910 FABRICATED THE SHEAR WEB AND INSTALLED WITH FASTENERS I.A.W AIRBUS DRAWING A53980389 & I.A.W A300-600 GMM 7-0-1001 SRM 51-40-21-001 PARA 7 P.24-P.50. LOCATED AT MAIN DECK FLOOR FR77 -Y1910. THIS REPAIR CLASSIJul 28, 2024 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA202407281114Shear Web · crackedMAIN DECK FLOOR SHEAR WEB CRACK AT FR79 PLUS 5", Y1630 REPLACED THE SHEAR PLATE WITH NEW PART AT FR79,STGR26. I.A.W A300-600 SRM 51-72-10- 001,P2. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 06-2-100.Jul 28, 2024 · N732FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR FDEA202407271161Skin · cracked1EA CRACK (6 MM) WAS FOUND AT RH WING CENTER FLAP RIB 27 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB27, S-2.7~2.8 AND EXTERNAL DOUBLER REPAIR AT RIB26~27, S-2.2~2.1 I.A.W FEDEX EA NO:T6-5750-T0380123 P1, SEQ NO:762, TITLE:WINGJul 27, 2024 · N732FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA202407271160Skin · cracked1EA CRACK (30 MM) WAS FOUND AT RH WING CENTER FLAP RIB 12 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT RIB12, S-2.8~REAR SPAR AND EXTERNAL DOUBLER REPAIR AT RIB11~12, S-2.1~REAR SPAR I.A.W FEDEX EA NO:T6-5750-T0380123 P1, SEQ NO:76Jul 27, 2024 · N732FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA202407261158Skin · cracked1EA CRACK (4MM) WAS FOUND AT L/H WING CENTER FLAP RIB27 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED RIB FLANGE REPAIR AT RIB27, S-2.7~S-2.8 AND EXTERNAL DOUBLER REPAIR AT RIB25~27, S-2.2~REAR SPAR. I.A.W FEDEX EA NO: T6-5750-T0330963 B P2, SEQ NO:755,Jul 26, 2024 · N732FD · Airbus A300B4605R · Trailing Edge Flaps
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