N730FD

Service difficulty reports · 213

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N730FD' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA202604300529Power Supply · inoperativeDURING CRUISE, THE L1 SLIDE ARMED WARNING BUZZER STARTED GOING OFF WITH THE SLIDE LIGHT FLASHING. WE PUSHED THE INTERIOR DOOR CONTROL HANDLE AND CHECKED THE LOCKING INDICATIONS WITH NO SUCCESS IN DEACTIVATING THE BUZZER. ALL DOOR AND SLIDE INDICATORS ONApr 30, 2026 · N730FD · Airbus A300B4622R · Door Warning SystemSDR FDEA202511142180Spring · failedIN CRUISE CAPTAINS FOOTREST SPRING NOT RETRACTING FOOT REST. COMPLIED WITH E.A. 6-2510-T0385692 REV NO: PS P3.Nov 14, 2025 · N730FD · Airbus A300B4622R · Flight Compartment EquipmentSDR FDEA202509071636Support Fitting · corrodedLH MLG FWD LUG RIB 5 BORE AND FWD FACE HAS CORROSION REMOVED CORROSION FROM LH MLG FWD LUG RIB 5 BORE AND FWD FACE PER EA 6-5710-T0306007 B P3 & P4.Sep 7, 2025 · N730FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA202503240493Battery · failedAT CRUISE, L1 DOOR AUDIBLE SLIDE WARNING. CONFIRMED HANDLE IN FULLY DOWN POSITION AND ATTEMPTED TO REARM, BUT WARNING HORN PERSISTED. WHILE T/S REF TSM 52-73-00, FOUND ASPSU BATTERY #2 WITH RED FAULT LIGHT. REMOVED AND REPLACED BATTERY REF AMM 52-73-18-04Mar 24, 2025 · N730FD · Airbus A300B4622R · Door Warning SystemSDR FDEA202503180443Wire · damaged#2 HP BLEED VALVE FAULT DURING TAKEOFF. COMPLIED WITH ECAM AND QRH. COORDINATED WITH GOC. BECAUSE OF MAINTENANCE HISTORY, NOT COMFORTABLE CONTINUING. ATB. REPAIRED WIRING.Mar 18, 2025 · N730FD · Airbus A300B4622R · Pneumatic System WiringSDR FDEA202409231339Angle · crackedCOMPLY WITH EA 6-5310-T0380417 P1 JACKING AND SHORING THE AIRCRAFT AND REPAIRED THE DIAMETER DEVIATION HOLES COMPLIED WITH EA 6-5310-T0380417 P1 COMPLETED JACKING AND SHORING THE AIRCRAFT AND REPAIRED THE DIAMETER DEVIATION HOLES, TITLE: FUSELAGE - MAINFRASep 23, 2024 · N730FD · Airbus A300B4622R · Standard Practices/StructuresSDR FDEA202409141319Angle · damagedCOMPLY WITH EA 6-5710-T0380525 REPAIRED THE BASIC WING STRUCTURE RH FRONT SPAR FR40 ANGLE FITTING #H13 OVERSIZED HOLE COMPLIED WITH EA 6-5710-T0380525 REPAIRED THE BASIC WING STRUCTURE RH FRONT SPAR FR40 ANGLE FITTING #H13 OVERSIZED HOLE,TITLE: WINGS - BASSep 14, 2024 · N730FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA202408271177Floorbeam · corrodedAFT CARGO - LOWER FLOOR BEAM FR62 -Y805~Y805 FOUND CORROSION REPLACED THE AFT CARGO CORRODED LOWER FLOOR BEAM FR62 -Y805~Y805 PER A300-600 SRM51-40-21 AND EA 6-5321-T0380436 P1, TITLE: FUSELAGE - CARGO COMP FLOORS - AFT CARGO FRAME 62 LOWER FLOOR BEAM FABRAug 27, 2024 · N730FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA202408181147Skin · delaminatedLH WING #5 SPOILER CENTER O/B HINGE ARM LWR SKIN FOUND DELAMINATION. SIZE:50MM*26MM,DEPTH:2.10MM COMPLIED WITH EA 6-5750-T0380281 P1, ACCOMPLISHED THE MODIFICATION OF SB A300-57-6082 R03 ON THE LH WING #5 SPOILER AND ALLOWED TO LEAVE THE DELAMINATION AS ISAug 18, 2024 · N730FD · Airbus A300B4622R · SpoilersSDR FDEA202408181146Skin · dentedLWR FUSELAGE - EXTERNAL SKIN FR1-FR2 8-9 O'CLOCK FOUND A DENT REPAIRED THE LWR FUSELAGE EXTERNAL SKIN FR1-FR2 8-9 O'CLOCK DENT AREA PER A300-600 SRM 53-11-12-201 FIG 201. THIS IS CAT B REPAIR. THE FIRST INSPECTION WAS 51000FC / 89000FH WHICHEVER OCCURS FIAug 18, 2024 · N730FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA202408161138Fitting · crackedMAIN DECK CARGO DOOR - ACTUATOR FR23-FR24 FWD AND AFT LUG BEARING FITTINGS FOUND CRACKS COMPLIED WITH EA 6-5230-T0380237 REPLACED THE MAIN DECK CARGO DOOR ACTUATOR FR23- FR24 CRACKED FWD AND AFT LUG BEARING FITTINGS, TITLE: DOORS - CARGO DOOR/HYD SYS - MAAug 16, 2024 · N730FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA202408161137Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB5 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0380295 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB5 BETWEEN STGR2.7 AND STGR2.8. TITLE: WING - FLIGHT SURFACES - RH Aug 16, 2024 · N730FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202408161136Rib · crackedRH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA: 6-5750-T0380295 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB17 BETWEEN REAR SPAR AND STGR2.8. TITLE: WING - FLIGHT SURFACES Aug 16, 2024 · N730FD · Airbus A300B4622 · Trailing Edge FlapsSDR FDEA202408161135Rib · crackedRRH WING CENTER FLAP RIB UPPER FLANGE FOUND 2EA CRACKS AT RIB27 BETWEEN REAR SPAR AND STGR2.7 COMPLIED WITH EA: 6-5750-T0380295 P1 REPAIRED THE RH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB27 BETWEEN REAR SPAR AND STGR2.7. TITLE: WING - FLIGHT SURFACEAug 16, 2024 · N730FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202408161134Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 3EA CRACKS AT RIB26 BETWEEN REAR SPAR AND STGR2.6 COMPLIED WITH EA: 6-5750-T0380294 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB26 BETWEEN REAR SPAR AND STGR2.6. TITLE: WING - FLIGHT SURFACESAug 16, 2024 · N730FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202408161133Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA: 6-5750-T0380294 P1 REPAIRED THE LH WING CENTER FLAP CRACKED RIB UPR FLANGE AT RIB17 BETWEEN REAR SPAR AND STGR2.8. TITLE: WING - FLIGHT SURFACES Aug 16, 2024 · N730FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202408161132Skin · delaminatedRH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE SKIN FOUND DELAMINATION. SIZE: 25MM*17MM, DEPTH: 1.60MM REPAIRED RH WING #3 SPOILER CENTER O/B HINGE ARM O/B SIDE SKIN DELAMINATION PER SB A300-57-6082 R03 FIGURE 2 SHEET 2&4 AND FIGURE 5 & EA 6-5750-T03802Aug 16, 2024 · N730FD · Airbus A300B4622R · SpoilersSDR FDEA202408111331Shear Tie · damagedCOMPLY WITH EO 6-5310-E0330747 D P12 REPAIRED THE FRAME FOOT CRACK AT FR45 RH SIDE AREA 2 COMPLIED WITH EO 6-5310-E0330747 D P12 REPAIRED THE FRAME FOOT CRACK AT FR45 RH SIDE AREA 2, TITLE: FUSELAGE - MAINFRAME - INSPECTION OF LOWER FRAME BASE FITTING BETAug 11, 2024 · N730FD · Airbus A310300 · Fuselage Internal Mounting StructureSDR FDEA202407050945Selector Valve · inoperativeON FINAL INTO KCAE, WHEN CALLED FOR GEAR DOWN, SELECTED LEVER DOWN WITH NO LOWERING OF GEAR. HAD 3 RED LIGHTS BUT NO EXTENSION. MANUALLY LOWERED GEAR IAW QRH & HAD SUCCESSFUL GEAR EXTENSION. REVERSED MEL 32-30-01-B. VERIFIED FREE FALL VALVE WAS CLOSED & ATJul 5, 2024 · N730FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA202403120279Fuel Sys · unknownINNER FUEL TANK WAS EMPTY & GREEN SCHEMATIC FOR RT INNER PUMP DID NOT TURN ORANGE & CENTER LT PUMP WOULD NOT PICK UP, IMBALANCE BETWEEN LT OUTER & RT OUTER DEVELOPED TO 1,900 LBS IN DESCENT. TRIED IN-LINE FUEL, BUT LT OUTER TANK KEPT BURNING FUEL GREATER THMar 12, 2024 · N730FD · Airbus A300B4622R · Aircraft Fuel SystemSDR FDEA202403100269Steering Sys · unknownON TAXI OUT THERE WAS A SLIGHT HESITATION IN NWS TURNING LT. STEERING & TURNING RT WITH NWS NORMAL. NWS OPERATED NORMALLY DURING TAXI IN LBB BOTH LT AND RT TURNS. PERFORMED A VISUAL INSPECTION OF ALL APPLICABLE MECHANICAL PARTS OF NWS SYSTEM COMPONENTS ON NMar 10, 2024 · N730FD · Airbus A300B4622R · Landing Gear Steering SystemSDR FDEA202401250112Battery · failedAT BLOCK-IN L1 AND R1 EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE OR TEST. R/I 25JAN24 14:48 FNT U REASON CODE : PREMATURE REMOVAL/INSTALLATION R & R EXIT DOOR LIGHT BATTERY 29WL AND ADJ/TESTS GOOD PER AMM 33-51-14-0-0.Jan 25, 2024 · N730FD · Airbus A300B4622R · Emergency LightingSDR FDEA202211052731Bracket · looseGEAR FAILED TO RETRACT ON INITIAL CLIMBOUT. CYCLED POSTION SELECTOR SWITCH, NO HELP. AIR TURN BACK OAK. ON WALK AROUND NOTICED RH GEAR BOGIE BEAM SENSOR BRACKET ASSY LOOSE AND OUT OF POSITION. REPLACED RH LANDING GEAR BOGIE BEAM SENSORS 8GA,12GA AND SNov 5, 2022 · N730FD · Airbus A300B4622R · Landing Gear Position and WarningSDR FDEA202203020387None · noneRH WING REAR SPAR HOLE 5 (E) BUSHING-REMOVE/NSTALL FOR ROTATING PROBE INSPECTION. I.A.W A300-600 SRM 51-72-20-201 REMOVE BUSHING ACCOMPLISHED. I.A.W EA NO.6-5710-161497 TITLE:WINGS-AD2005-23-08-MAIN FRAME-DAMAGE TO FR47 R/H HOLE H SB A300-57-6049 EO 6-57Mar 2, 2022 · N730FD · Airbus A300* · Wing Main, Frame StructureSDR FDEA202203020386None · noneRH WING REAR SPAR HOLE 6 (G) BUSHING-REMOVE/NSTALL FOR ROTATING PROBE INSPECTION. I.A.W A300-600 SRM 51-72-20-201 REMOVE BUSHING ACCOMPLISHED. I.A.W EA NO.6-5710-115255 PT1 TITLE:AD2005-23-08 DEVIATION TO EO 6-5710-7-3305 MAKE THE BUSHING ACCOMPLISHED. IMar 2, 2022 · N730FD · Airbus A300* · Wing Main, Frame StructureSDR FDEA202203020385None · noneRH WING REAR SPAR HOLE 5 (E) BUSHING-REMOVE/NSTALL FOR ROTATING PROBE INSPECTION. I.A.W EA NO.6-5710-115255 PT1 TITLE:AD2005-23-08 DEVIATION TO EO 6-5710-7-3305 MAKE THE BUSHING ACCOMPLISHED. I.A.W A300-600 SRM 51-72-20-201 INSTALL BUSHING ACCOMPLISHED.Mar 2, 2022 · N730FD · Airbus A300* · Wing Main, Frame StructureSDR FDEA202203020384None · noneLH WING REAR SPAR HOLE 165 (I) BUSHING-REMOVE/NSTALL FOR ROTATING PROBE INSPECTION. I.A.W A300-600 SRM 51-72-20-201 REMOVE BUSHING ACCOMPLISHED. I.A.W EA NO.6-5710-115255 PT1 TITLE:AD2005-23-08 DEVIATION TO EO 6-5710-7-3305 MAKE THE BUSHING ACCOMPLISHED. Mar 2, 2022 · N730FD · Airbus A300* · Wing Main, Frame StructureSDR FDEA202203190595Former · damagedLH WING T/E WEB AT NO.6 SPLR ACTR O/B SIDE DAMAGED AT CLAMP ATTACHED POINT. TRIMMED OUT AND INSTALLED THE DOUBLER & FILLER TO THE DAMAGE AREA I.A.W EA NO:6-5700- T0367376 P1, SEQ NO:000734, TITLE:WINGS - GENERAL - LH WING TRAILING EDGE FORMER AT SPIX 47.80Feb 26, 2022 · N730FD · Airbus A300* · Wing StructureSDR FDEA202202260533Former · damagedLH WING T/E WEB AT NO.6 SPLR ACTR O/B SIDE DAMAGED AT CLAMP ATTACHED POINT. TRIMMED OUT AND INSTALLED THE DOUBLER & FILLER TO THE DAMAGE AREA I.A.W EA NO:6-5700- T0367376 P1, SEQ NO:000734, TITLE:WINGS - GENERAL - LH WING TRAILING EDGE FORMER AT SPIX 47.80Feb 26, 2022 · N730FD · Airbus A300* · Wing StructureSDR FDEA202202260481Floor Panel · damagedBULK CARGO COMPT FLOOR PANEL #161BF WAS FOUND DAMAGED. REPAIR THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201, P205-206, PARA9A, FIG201Feb 26, 2022 · N730FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202202260480Floor Panel · damagedBULK CARGO COMPT FLOOR PANEL #161CF WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201 P205-206 PARA9A FIG201.Feb 26, 2022 · N730FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202202250484Floor Support · corrodedMAIN DECK LONGITUDIAL FLOOR SUPPORT STRUCTURE UPR SURFACE WAS FOUND CORROSION AT FR11~FR13A, Y735MM REPLACED THE CORROSION SUPPORT STRUCTURE WITH NEW PART.I.A.W A300-600 SRM 51-72-10- 001 PAGE2Feb 25, 2022 · N730FD · Airbus A300* · Fuselage Structure (General)SDR FDEA202202250483Web · damagedWEB BENT / DAMAGED BETWEEN FRAME 86- 87 AT STRINGER 36 R. REPLACED THE PLATE AND SECTION WITH NEW ONES. I.A.W A300-600 SRM 51-72-10-001 P1-3.Feb 25, 2022 · N730FD · Airbus A300* · Fuselage Structure (General)SDR FDEA202202250446Rudder · unknownPREVIOUS COMPOSITE MAJOR REPAIR LOCATED ON RIGHT SIDE OF RUDDER APPROX. 4 FT FROM THE BOTTOM AND 3 FT FROM TRAILING EDGE. REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS IN ACCORDANCE WITH APPROVED DATA. ACCOMPLISHED THE CATE.B RUDDER SHELL CFRP AREA Feb 25, 2022 · N730FD · Airbus A300* · Rudder StructureSDR FDEA202202240482Floor Panel · damagedMAIN DECK CARGO COMPT #231RH FLOOR PANEL WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201 P205-206 PARA 9A FIG201.Feb 24, 2022 · N730FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202202240479Floor Panel · damagedMAIN DECK CARGO COMPT #232FG FLOOR PANEL WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201 P205-206 PARA9A FIG201Feb 24, 2022 · N730FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202202240476Floor Panel · damagedMAIN DECK CARGO COMPT #222RF FLOOR PANEL WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201 P205-206 PARA9A FIG201Feb 24, 2022 · N730FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202202240475Floor Panel · damagedMAIN DECK CARGO COMPT #241BK FLOOR PANEL WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201 P205-206 PARA9A FIG201Feb 24, 2022 · N730FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202202240474Floor Panel · damagedMAIN DECK CARGO COMPT #241YJ FLOOR PANEL WAS FOUND DAMAGED. REPAIRED THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201 P205-206 PARA9A FIG201Feb 24, 2022 · N730FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202202220478Skin · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR SURFACE L/E PANEL 613AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTINGFeb 22, 2022 · N730FD · Airbus A300* · Wing StructureSDR FDEA202202220477Skin · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON L/H WING LWR SURFACE L/E PANEL 513AB CUTOUT FWD O/B AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTINGFeb 22, 2022 · N730FD · Airbus A300* · Wing StructureSDR FDEA202202220374None · noneAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER FOUND ON RUDDER TRAILING EDGE APEX AREA LOCATED BTW T/E SCREW LINE NO.21 AND NO.22 FASTENER COUNTED FROM LOWER SIDE. AFTER ASSESSMENT, FOUND THE CONNECTION DOUBLER ON RUDDER T/E SCREW LINE BTW NO.20 AFeb 22, 2022 · N730FD · Airbus A300* · Rudder StructureSDR FDEA202202210473Floor Panel · damagedBULK CARGO COMPT FLOOR PANEL #161BF WAS FOUND DAMAGED. REPAIR THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201, P205-206, PARA9A, FIG201Feb 21, 2022 · N730FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202202210447Skin · noneFUSELAGE SKIN EXTERNAL SURFACE WAS FOUND DENT AT FR26 4",S-9R 1" POS ACCOMPLISHED THE CATE.B EXTERNAL PERMANENT SMALL SKIN REPAIR I.A.W A300-600 SRM 53- 13-12-201,PAGE201-202 & 53-10-12-201 ,PARA5, PAGE243-346&353/354, FIG224(SHEET4), SRI 53-10- 12-201, IIFeb 21, 2022 · N730FD · Airbus A300* · Fuselage Main, KeelSDR FDEA202202090254Warning Light · false activationDEPARTING KMEM RUNWAY 27 BETWEEN 80 AND 100 KNOTS ECAM YELLOW HYD SYS LOW PSI . REJECTED TAKEOFF. YELLOW QUANTITY OVERHEAD PANEL AT VERY BOTTOM OF TOP HAT. HYD QUANTITY ON ECAM SLIGHTLY UNDER THE MINIMUM. PERFORMED WALK AROUND OF AIRCRAFT --NO LEAKS NOFeb 9, 2022 · N730FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA202111102814None · failedPDIS 730 32-20 7278 10NOV21 MEM OPEN U NOSE GEAR DOOR LIGHT DID NOT GO OUT AFTER GEAR RETRACTED. ALL GEAR INDICATIONS AGREED BOTH ON DASH AND OVERHEAD. COMPLIED WITH QRH. MAX SPEED WAS 230 KTS, LESS THAN 0.5 MACH. LIGHTS WENT OUT UPON GEAR EXNov 10, 2021 · N730FD · Airbus A300* · Nose/Tail Landing GearSDR FDEA202012300007Ram Air Turb · unwanted deployON ARRIVAL FOUND RAT DEPLOYED. BOTH RAT HANDLES STILL SHEAR WIRED. INSPECTED RAT UPLOCK HOOK, IAW 29-25-00-06. NO DEFECTS NOTED. STOWED RAT, IAW 29-25-00-03. A/C OK FOR SERVICE.Dec 30, 2020 · N730FD · Airbus A300B4622R · Hydraulic System, AuxiliarySDR FDEA202012293219Warning Message · false activationAFTER TAKEOFF AT GEAR RETRACTION, RECEIVED ECAM L/G DOORS NOT CLOSED. BOTH FORWARD AND OVERHEAD PANEL INDICATES NOSE GEAR DOOR NOT CLOSED. WHEN GEAR EXTENDED FOR LANDING, NOSE GEAR DOOR CLOSED. OPENED AND CLOSED NLG DOORS SEVERAL TIMES, ALL INDICATIONS ANDDec 29, 2020 · N730FD · Airbus A300B4622R · Landing Gear Door Retract SectionSDR FDEA201909172264Stiffener · crackedLT PYLON - RIB9-RIB10, LWR SPAR UPR SURFACE STIFFENER CRACKED APPROX 0.75 INCH IN LENGTH REPAIRED THE LT PYLON - RIB9-RIB10, LWR SPAR UPR SURFACE STIFFENER CRACK PER EO 6-5450-7-3302 D PT5 (TITLE: NACELLES/PYLONS - PYLON LOWER SPAR - INSPECTION FOR CRACKS BETWSep 17, 2019 · N730FD · Airbus A300B4622R · Nacelle/Pylon, Frame/Spar/RibSDR FDEA2019091972261Door Sill · crackedAFT CARGO DOOR SILL BEAM BETWEEN FR60 AND FR61 FOUND 1EA CRACK REPAIRED THE AFT CARGO DOOR SILL BEAM CRACK BETWEEN FR60 AND FR61 PER EA: 6-5310-T0349431 P1. TITLE: FUSELAGE - MAINFRAME - CRACKS FOUND ON LOWER SILL OF AFT CARGO DOOR B/T FR60-FR61 - REPAIR. Sep 17, 2019 · N730FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
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