N731FD

Service difficulty reports · 202

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 = 'N731FD' 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 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 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 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 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 FDEA202405190696Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, AND RIB26 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379257 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 20May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA202405190695Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 3EA CRACKS AT RIB20 BETWEEN STGR2.7 AND REAR SPAR, AND RIB21 BETWEEN STGR2.7 AND STGR2.8 COMPLIED WITH EA: 6-5750-T0379257 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 20, 2May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA202405190694Rib · crackedRH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB11 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379257 P1. TITLE: WING - FLIGHT SURFACES - RH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 20, 21, 25 AND 26 AT STR. 2.7 /2.8 - ALI 57May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA202405190693Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB25 BETWEEN STGR2.8 AND REAR SPAR, AND RIB26 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379258 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 12May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA202405190692Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 2EA CRACKS AT RIB18 BETWEEN STGR2.8 AND REAR SPAR, AND RIB19 BETWEEN STGR2.8 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379258 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP CRACKS IN UPPER FLANGES OF RIBS 11, 12May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA202405190691Rib · crackedLH WING CENTER FLAP RIB UPR FLANGE FOUND 4EA CRACKS AT RIB11 BETWEEN STGR2.8 AND REAR SPAR, RIB12 BETWEEN STGR2.8 AND REAR SPAR, AND RIB13 BETWEEN STGR2.7 AND REAR SPAR. COMPLIED WITH EA: 6-5750-T0379258 P1. TITLE: WING - FLIGHT SURFACES - LH CENTER FLAP May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge FlapsSDR FDEA202405190690Skin · delaminatedLH WING #3 SPOILER CENTER O/B HINGE ARM OUTSIDE SURFACE FOUND DELAMINATION. SIZE: 30MM*15MM, DEPTH: 1.51MM. COMPLIED WITH EA: 6-5750-T0379154 P1. TITLE: WING - FLIGHT SURFACES - LH #3 SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WIMay 19, 2024 · N731FD · Airbus A300B4605R · SpoilersSDR FDEA202401260115Apu · failedAFTER CLOSING THE DOORS FOR DEPARTURE, SMELLED ELECTRICAL SMOKE. DISCOVERED SMOKE OF UNKNOWN ORIGIN IN COURIER COMPART & CARGO AREA. APU AUTO SHUTDOWN. NOT SURE IF THE APU SHUTDOWN IS RELATED TO THE SMOKE & ELECTRICAL ODOR. R & R STARTER. OPS CHECK FAJan 26, 2024 · N731FD · Airbus A300B4605R · APU Core EngineSDR FDEA202312131936Pressure Switch · failedL1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHT INOP. BUZZER WORKS NORMALLY. ENT BY: 691135 RPT BY:691135 MEL 13DEC23 17:31 MEM U RELEASED FOR SERVICE PER MEL : 52-73-01-01 CATEGORY : C EXPIRATION : 23DEC23 "MEL 52-73-01-01: L1 CREW ENTRY DOOR ESDec 13, 2023 · N731FD · Airbus A300B4605R · Escape SlideSDR FDEA202308021345Transmitter · failedAROUND 45 MIN INTO CRUISE FLIGHT WE NOTICED THE GREEN HYD REVISOR QUANTITY DECREASING. SHORTLY AFTER WE RECEIVED AN ECAM - GREEN RSVR LO LEVEL. COMPLIED WITH ECAM AND ASSOCIATED PROC S. LANDING GEAR WAS MANUALLY EXTENDED. UNEVENTFUL LANDING KMEM 36C. EMAug 2, 2023 · N731FD · Airbus A300* · Hydraulic System, MainSDR FDEA202303240498Line · leakingDURING CRUISE FLIGHT ECAM DISPLAYED HYD , HYD RSVR LO LEVEL , GREEN SYSTEM OVERHEAD GAUGE SHOWED QTY AT APPROX RED DOT , ECAM HYD PAGE DISPLAYED APPROX THE SAME . EMERGENCY DECLARED. FOUND GREEN SYS PRESS LINE ON BRAKE SYSTEM MANIFOLD (1311) LEAKING WHEN Mar 24, 2023 · N731FD · Airbus A300* · Hydraulic Indicating SystemSDR FDEA202303230497Transmitter · failedPDIS 731 29-02 6666 23MAR23 OMA FACT AFTER CLEANUP DEPARTING KMEM, RECEIVED ECAM INDICATION OF LOW LEVEL ON GREEN HYD SYSTEM. LVL INDICATED ZERO ON ECAM AND OVERHEAD GAUGE. EXECUTED QRH FOR HYD LOW LEVEL. EMERGENCY DECLARED WITH OMA APPROACHMar 23, 2023 · N731FD · Airbus A300* · Hydraulic Power SystemSDR FDEA202303010355Hose · leakingPDIS 731 29-02 6592 01MAR23 IND OPEN U UPON GEAR EXTENSION AT KIND GREEN HYDRAULIC QUANTITY WENT TO ZERO. ACCOMPLISHED ECAM/QRH AND LANDED ON 05L. TOWED INTO CHOCKS OFF RUNWAY. NO FURTHER ISSUES. ***EMERGENCY DECLARED*** HOSE OPENED AFT CMar 1, 2023 · N731FD · Airbus A300B4605R · Hydraulic Power SystemSDR FDEA202203080524None · noneREF ORIGINAL WRI ATA 22-10-XXX 08MAR22, TECH SERVICE ITEM ISSUED AND C/W. DUE TO A/P2, AND 2X'S FO'S SPEED DISPLAY DROPPING BACK TO 35 KNOTS THEN RECOVERING QUICKLY. CHECK OF THE PITOT HEAT SYSTEM, PITOT DRAIN SYSTEM FOR MOISTURE. WARM OAT STATION OR HEMar 8, 2022 · N731FD · Airbus A300* · Flight Environment DataSDR FDEA202203080523None · noneFL 350, AUTO PILOT #2, COST INDEX 200, SMOOTH AIR, IN CRUZ, IN PROFILE; TWO TIMES THE FO S SPEED ROLLED BACK TO 35 KNOTS ON THE SPEED TAPE. THE FIRST TIME FO SELECTED ALTITUDE HOLD. THE SECOND TIME THE SPEED RETURNED TO .80 MACH AFTER A FEW SECONDS. THE AMar 8, 2022 · N731FD · Airbus A300* · Autopilot SystemSDR FDEA202201160123Seat Track · damagedN00464 MAIN DECK SEAT TRACK LOBE AT LOCKS L1206 & L1199 DAMAGED. REPLACED THE DAMAGED SEAT TRACK WITH NEW ONE. I.A.W. A300-600 SRM 51-72-10-001 PAGE. 1~3. SEE ATTACHED JPF FOR DETAIL.Jan 16, 2022 · N731FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202201140065None · noneN00446 AFTER REMOVE CENTER WING JOINT FR40 LH & RH UPPER HOLE BUSHES,FOUND BUSHES ID HOLE DAMAGE. I.A.W T6-5710-T0347753 B P2 PAGE 4 OF 4 STEP 3 FABRICATE NEW BUSHES ACCOMPLISHED.Jan 14, 2022 · N731FD · Airbus A300* · Wing Main, Frame StructureSDR FDEA202201110229Doubler · unknownAT THE TIME OF RECORDS REVIEW THE FOLLOWING WAS IDENTIFIED ON MAJIOR REPAIR W/O 45404 SNRM N00072,DOCUMENTATION PROVIDED IS INCOMPLETE UNABLE TO VERIFY ALL PARTIAL WORK ACCOMPLISHED FOR THE REPAIR,JPF PAGE 1 NOT PROVIDED,PAGE 2 STARTS AT JPF ITEM13,WITH Jan 11, 2022 · N731FD · Airbus A300* · Fuselage Structure (General)SDR FDEA202201110084Floor Panel · damagedN00433 MAIN DECK CARGO COMPT #252WH FLOOR PANEL WAS FOUND EDGE DAMAGED. REPAIRED THE FLOOR PANEL I.A.W. A300-600 SRM 53-10-20-201 P.205-206 PARA.9A FIG.201.Jan 11, 2022 · N731FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202201110083Floor Panel · damagedN00432 MAIN DECK CARGO COMPT #252YH FLOOR PANEL WAS FOUND EDGE DAMAGED. REPAIRED THE FLOOR PANEL I.A.W A300-600 SRM 53-10-20-201 P.205-206 PARA.9A FIG.201.Jan 11, 2022 · N731FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202201080114Seat Track · unknownN00373 AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR55 TO FR57.3,-Y1959 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A3Jan 8, 2022 · N731FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202201080113Seat Track · unknownN00371 AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR59 TO FR60,Y1959 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-Jan 8, 2022 · N731FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202201080112Seat Track · unknownN00370 AIRCRAFT REPAIR ASSESSMENT:EXISTING REPAIR FOUND ON MAIN DECK SEAT TRACK BTW FR61 TO FR62,Y1456 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA A300-Jan 8, 2022 · N731FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202201080080Skin · 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, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DJan 8, 2022 · N731FD · Airbus A300* · Wing StructureSDR FDEA202201070079Skin · 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, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DJan 7, 2022 · N731FD · Airbus A300* · Wing StructureSDR FDEA202201070078None · unknownAIRCRAFT 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. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIJan 7, 2022 · N731FD · Airbus A300* · Rudder StructureSDR FDEA202201030026None · corrodedMAIN DECK SEAT TRACK STRUCTURE FOUND CORROSION BTWN FR11~12A , Y730 REPLACED THE CORROSION SEAT TRACK WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001, PAGE2Jan 3, 2022 · N731FD · Airbus A300* · Fuselage Structure (General)SDR FDEA202201020115Stringer · corrodedFWD CGO COMP'T BILGE STGR CORROSION BTW FR38.2 AND FR39 ,S-44R POSITION. CUT-OUT THE DAMAGED AREA AND PERFORMED STRINGER REPAIR I.A.W. A300-600 SRM 53-10- 14-201 PARA.4.A FIG.201 PAGE.203-204B, APPLIED CIC TO REPAIR AREA I.A.W. A300-600 SRM 51- 23-00-001 PAGJan 2, 2022 · N731FD · Airbus A300B4605R · Fuselage Main, Longeron/StringerSDR FDEA202108312174Brake · out of alignmentAFTER T/O HAD ECAM ALERT WITH #2 TIRE EXCEEDING 300 DEGREES. GEAR WAS ALREADY RETRACTED AT THE TIME OF ALERT. ELECTED TO PRESS ON TO CLT WITH MAX 380 DEGREES ON #2 TIRE. PUT GEAR DOWN EARLY INTO CLT WITH BRAKE FANS RUNNING AND DECLARED AN EMERGENCY. UNEVEAug 31, 2021 · N731FD · Airbus A300B4605R · Landing Gear Brake SystemSDR FDEA202101090029Pump · malfunctionedAT APPROX 60 KTS ROLL GOT NR 2 GREEN HYD PUMP LOW PSI. SAME LIGHT CAME ON AFTER START OF NR 1 ENGINE, BUT WENT OUT ON ITS OWN AFTER A MINUTE. REJECTED TAKE OFF. CONFERED WITH MAINT, DID A HIGH POWER ENGINE RUN WITH NO PROBLEM NOTED. TAXI BACK FOR TAKEOFFJan 9, 2021 · N731FD · Airbus A300B4605R · Hydraulic System, MainSDR FDEA2020090832113Fmc · abnormalPDIS 731, 34-63, 3866, 03SEP20, MEM FACT U. AT FL340 ADC 1 FAILED. AP 1 DISENGAGED, LOST PFD INSTRUMENTATION, ND UNAVAILABLE, FMC 1 FAILURE, ATS 2 TRIPPED OFF. RESET ATS 2 PER ECAM. COMPLIED WITH QRH FOR FMC UNAVAILABLE AND ADC INSTRUMENTATION FAILURE. ASep 3, 2020 · N731FD · Airbus A300B4605R · Flight Management Computing Hardware SystemSDR FDEA2019082191952Landing · damagedRIGHT HAND WING ON PANEL LANDS ON 650LB, 650MB AND 660BB HAVE BUSHINGS INSTALLED IN INSPECTION AREA WITH TWO EACH CRACKS AT PANEL LAND 660BB HOLES 1 AND 2. COMPLIED WITH EA 6-5730-T0348135-P1.Aug 19, 2019 · N731FD · Airbus A300B4605R · Wing, Plate/SkinSDR FDEA2019082171924Fitting · corrodedR/H CTR WING FR47 BOTTOM PANEL AT REAR SPAR JUNCTION, HOLE "F" HAS INDICATIONS FOUND DUE TO CORROSION PITS IN HOLE FROM 2ND TO END OF 3RD LAYER FROM LOWER SKIN. COMPLIED WITH EA 6-5710-T0328474-P1Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, StructureSDR FDEA2019082171923Fitting · crackedINDICATIONS DURING ROTOPROBE INSPECTION OF HOLE "186" DUE TO VISUAL DAMAGE INSIDE HOLE RH WING COMPLIED WITH EA 6-5710-TO348474-P1Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, StructureSDR FDEA2019082171922Fitting · crackedR/H CTR WING FR47 BOTTOM PANEL AT REAR JUNCTION , HOLE "S" HAS A CRACK INDICATIONS FOUND 3 & 9 O'CLOCK POSITION AT 3RD LAYER TO 5TH LAYER IN HOLE. COMPLIED WITH EA 6-5710-T0348474-P1Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, StructureSDR FDEA2019082171919Fitting · crackedCTR WING FR47 BOTTOM PANEL AT REAR JUNCTION, HOLE "G" HAS A CRACK INDICATION FOUND 10 O'CLOCK POSITION AT 3RD LAYER TO END OF HOLE. COMPLIED WITH EA 6-5710-T0348474-P1Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, StructureSDR FDEA2019082171918Fitting · crackedR/H FR47 FASTENER 11RH AND BUSHINGS REQUIRE REMOVAL FOR NDT ROTOTEST INSP. COMPLIED WITH EA 6-5710-T0348474-P1Aug 17, 2019 · N731FD · Airbus A300B4605R · Wing Main, Frame StructureSDR FDEA2019082171917Fitting · crackedINDICATIONS DURING ROTOPROBE INSPECTION OF HOLE "166" DUE TO VISIBLE DAMAGE INSIDE OF HOLE. RH WING COMPLIED WITH EA 6-5710-T0348474-P1Aug 17, 2019 · N731FD · Airbus A300B4605R · Wing Main, Frame StructureSDR FDEA2019082171916Fitting · crackedR/H WING INSPECTION OF FASTENER HOLE (C)FAILED ROTO PROBE INSPECTION DUE TO MULTIPLE CRACK INDICATIONS AT APOX. DEPTH OF .9" TO 1.4" INSPECTION FROM THE BOTTOM SKIN UPWARDS. POSSIBLE SHIM LOCATED IN AREA OF INDICATIONS. COMPLIED WITH EA 6-5710-TO348474-P1Aug 17, 2019 · N731FD · Airbus A300B4605R · Wing Main, Frame StructureSDR FDEA2019082171915Fitting · crackedHOLE "I" RH SIDE HAS VISIBLE GOUGES ON TANK SIDE LAYER AT THE 9 AND 6 O'CLOCK POSITIONS GIVING INDICATIONS FROM ROTOPROBE INSPECTION COMPLIED WITH EA 6-5710-TO348474-P1Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, Structure
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