# Service difficulty reports: N731FD

A list on [N731FD](https://openairdocs.org/aircraft/N731FD.md).

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

Page 1 of 5 · 202 reports

- [SDR FDEA202609271454](https://openairdocs.org/sdr/FDEA202609271454.md): Spoiler · delaminated · Sep 27, 2026 · N731FD · Airbus A300B4605R · Spoilers
  > RIGHT 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.
- [SDR FDEA202609091463](https://openairdocs.org/sdr/FDEA202609091463.md): Fitting · damaged · Sep 9, 2026 · N731FD · Airbus A300B4605R · Cargo/Baggage Doors
  > CARGO 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 MA
- [SDR FDEA202609061306](https://openairdocs.org/sdr/FDEA202609061306.md): Repair · none · Sep 6, 2026 · N731FD · Airbus A300B4605R · Standard Practices/Structures
  > EXISTING 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:STRUCT
- [SDR FDEA202609051321](https://openairdocs.org/sdr/FDEA202609051321.md): Repair · none · Sep 5, 2026 · N731FD · Airbus A300B4605R · Standard Practices/Structures
  > EXISTING 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- 5100-7-500
- [SDR FDEA202609041453](https://openairdocs.org/sdr/FDEA202609041453.md): Backboard · punctured · Sep 4, 2026 · N731FD · Airbus A300B4605R · Escape Slide
  > LH 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.
- [SDR FDEA202609041305](https://openairdocs.org/sdr/FDEA202609041305.md): Repair · misinstalled · Sep 4, 2026 · N731FD · Airbus A300B4605R · Standard Practices/Structures
  > EXISTING 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 FO
- [SDR FDEA202609041304](https://openairdocs.org/sdr/FDEA202609041304.md): Repair · no discrepancy · Sep 4, 2026 · N731FD · Airbus A300B4605R · Standard Practices/Structures
  > EXISTING 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. N
- [SDR FDEA202609031303](https://openairdocs.org/sdr/FDEA202609031303.md): Roller Track · misrepaired · Sep 3, 2026 · N731FD · Airbus A300B4605R · Fuselage Main, Structure
  > EXISTING 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 FIG
- [SDR FDEA202605090576](https://openairdocs.org/sdr/FDEA202605090576.md): Pump · low pressure · May 9, 2026 · N731FD · Airbus A300B4605R · Hydraulic Pump (Electric/Engine), Main
  > ON 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.
- [SDR FDEA202411061637](https://openairdocs.org/sdr/FDEA202411061637.md): Cover · installed · Nov 6, 2024 · N731FD · Airbus A300B4605R · Pitot/Static System
  > THERE 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 FLIG
- [SDR FDEA202405190696](https://openairdocs.org/sdr/FDEA202405190696.md): Rib · cracked · May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge Flaps
  > RH 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, 20
- [SDR FDEA202405190695](https://openairdocs.org/sdr/FDEA202405190695.md): Rib · cracked · May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge Flaps
  > RH 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, 2
- [SDR FDEA202405190694](https://openairdocs.org/sdr/FDEA202405190694.md): Rib · cracked · May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge Flaps
  > RH 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 57
- [SDR FDEA202405190693](https://openairdocs.org/sdr/FDEA202405190693.md): Rib · cracked · May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge Flaps
  > LH 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, 12
- [SDR FDEA202405190692](https://openairdocs.org/sdr/FDEA202405190692.md): Rib · cracked · May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge Flaps
  > LH 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, 12
- [SDR FDEA202405190691](https://openairdocs.org/sdr/FDEA202405190691.md): Rib · cracked · May 19, 2024 · N731FD · Airbus A300B4605R · Trailing Edge Flaps
  > LH 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
- [SDR FDEA202405190690](https://openairdocs.org/sdr/FDEA202405190690.md): Skin · delaminated · May 19, 2024 · N731FD · Airbus A300B4605R · Spoilers
  > LH 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 WI
- [SDR FDEA202401260115](https://openairdocs.org/sdr/FDEA202401260115.md): Apu · failed · Jan 26, 2024 · N731FD · Airbus A300B4605R · APU Core Engine
  > AFTER 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 FA
- [SDR FDEA202312131936](https://openairdocs.org/sdr/FDEA202312131936.md): Pressure Switch · failed · Dec 13, 2023 · N731FD · Airbus A300B4605R · Escape Slide
  > L1 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 ES
- [SDR FDEA202308021345](https://openairdocs.org/sdr/FDEA202308021345.md): Transmitter · failed · Aug 2, 2023 · N731FD · Airbus A300* · Hydraulic System, Main
  > AROUND 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. EM
- [SDR FDEA202303240498](https://openairdocs.org/sdr/FDEA202303240498.md): Line · leaking · Mar 24, 2023 · N731FD · Airbus A300* · Hydraulic Indicating System
  > DURING 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
- [SDR FDEA202303230497](https://openairdocs.org/sdr/FDEA202303230497.md): Transmitter · failed · Mar 23, 2023 · N731FD · Airbus A300* · Hydraulic Power System
  > PDIS 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 APPROACH
- [SDR FDEA202303010355](https://openairdocs.org/sdr/FDEA202303010355.md): Hose · leaking · Mar 1, 2023 · N731FD · Airbus A300B4605R · Hydraulic Power System
  > PDIS 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 C
- [SDR FDEA202203080524](https://openairdocs.org/sdr/FDEA202203080524.md): None · none · Mar 8, 2022 · N731FD · Airbus A300* · Flight Environment Data
  > REF 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 HE
- [SDR FDEA202203080523](https://openairdocs.org/sdr/FDEA202203080523.md): None · none · Mar 8, 2022 · N731FD · Airbus A300* · Autopilot System
  > FL 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 A
- [SDR FDEA202201160123](https://openairdocs.org/sdr/FDEA202201160123.md): Seat Track · damaged · Jan 16, 2022 · N731FD · Airbus A300* · Fuselage Main, Structure
  > N00464 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.
- [SDR FDEA202201140065](https://openairdocs.org/sdr/FDEA202201140065.md): None · none · Jan 14, 2022 · N731FD · Airbus A300* · Wing Main, Frame Structure
  > N00446 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.
- [SDR FDEA202201110229](https://openairdocs.org/sdr/FDEA202201110229.md): Doubler · unknown · Jan 11, 2022 · N731FD · Airbus A300* · Fuselage Structure (General)
  > AT 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
- [SDR FDEA202201110084](https://openairdocs.org/sdr/FDEA202201110084.md): Floor Panel · damaged · Jan 11, 2022 · N731FD · Airbus A300* · Fuselage Floor Panel
  > N00433 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.
- [SDR FDEA202201110083](https://openairdocs.org/sdr/FDEA202201110083.md): Floor Panel · damaged · Jan 11, 2022 · N731FD · Airbus A300* · Fuselage Floor Panel
  > N00432 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.
- [SDR FDEA202201080114](https://openairdocs.org/sdr/FDEA202201080114.md): Seat Track · unknown · Jan 8, 2022 · N731FD · Airbus A300* · Fuselage Main, Structure
  > N00373 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 A3
- [SDR FDEA202201080113](https://openairdocs.org/sdr/FDEA202201080113.md): Seat Track · unknown · Jan 8, 2022 · N731FD · Airbus A300* · Fuselage Main, Structure
  > N00371 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-
- [SDR FDEA202201080112](https://openairdocs.org/sdr/FDEA202201080112.md): Seat Track · unknown · Jan 8, 2022 · N731FD · Airbus A300* · Fuselage Main, Structure
  > N00370 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-
- [SDR FDEA202201080080](https://openairdocs.org/sdr/FDEA202201080080.md): Skin · unknown · Jan 8, 2022 · N731FD · Airbus A300* · Wing Structure
  > AIRCRAFT 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 D
- [SDR FDEA202201070079](https://openairdocs.org/sdr/FDEA202201070079.md): Skin · unknown · Jan 7, 2022 · N731FD · Airbus A300* · Wing Structure
  > AIRCRAFT 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 D
- [SDR FDEA202201070078](https://openairdocs.org/sdr/FDEA202201070078.md): None · unknown · Jan 7, 2022 · N731FD · Airbus A300* · Rudder Structure
  > AIRCRAFT 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 REPAI
- [SDR FDEA202201030026](https://openairdocs.org/sdr/FDEA202201030026.md): None · corroded · Jan 3, 2022 · N731FD · Airbus A300* · Fuselage Structure (General)
  > MAIN 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, PAGE2
- [SDR FDEA202201020115](https://openairdocs.org/sdr/FDEA202201020115.md): Stringer · corroded · Jan 2, 2022 · N731FD · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
  > FWD 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 PAG
- [SDR FDEA202108312174](https://openairdocs.org/sdr/FDEA202108312174.md): Brake · out of alignment · Aug 31, 2021 · N731FD · Airbus A300B4605R · Landing Gear Brake System
  > AFTER 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. UNEVE
- [SDR FDEA202101090029](https://openairdocs.org/sdr/FDEA202101090029.md): Pump · malfunctioned · Jan 9, 2021 · N731FD · Airbus A300B4605R · Hydraulic System, Main
  > AT 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 TAKEOFF
- [SDR FDEA2020090832113](https://openairdocs.org/sdr/FDEA2020090832113.md): Fmc · abnormal · Sep 3, 2020 · N731FD · Airbus A300B4605R · Flight Management Computing Hardware System
  > PDIS 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. A
- [SDR FDEA2019082191952](https://openairdocs.org/sdr/FDEA2019082191952.md): Landing · damaged · Aug 19, 2019 · N731FD · Airbus A300B4605R · Wing, Plate/Skin
  > RIGHT 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.
- [SDR FDEA2019082171924](https://openairdocs.org/sdr/FDEA2019082171924.md): Fitting · corroded · Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, Structure
  > R/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-P1
- [SDR FDEA2019082171923](https://openairdocs.org/sdr/FDEA2019082171923.md): Fitting · cracked · Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, Structure
  > INDICATIONS DURING ROTOPROBE INSPECTION OF HOLE "186" DUE TO VISUAL DAMAGE INSIDE HOLE RH WING COMPLIED WITH EA 6-5710-TO348474-P1
- [SDR FDEA2019082171922](https://openairdocs.org/sdr/FDEA2019082171922.md): Fitting · cracked · Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, Structure
  > R/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-P1
- [SDR FDEA2019082171919](https://openairdocs.org/sdr/FDEA2019082171919.md): Fitting · cracked · Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, Structure
  > CTR 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-P1
- [SDR FDEA2019082171918](https://openairdocs.org/sdr/FDEA2019082171918.md): Fitting · cracked · Aug 17, 2019 · N731FD · Airbus A300B4605R · Wing Main, Frame Structure
  > R/H FR47 FASTENER 11RH AND BUSHINGS REQUIRE REMOVAL FOR NDT ROTOTEST INSP. COMPLIED WITH EA 6-5710-T0348474-P1
- [SDR FDEA2019082171917](https://openairdocs.org/sdr/FDEA2019082171917.md): Fitting · cracked · Aug 17, 2019 · N731FD · Airbus A300B4605R · Wing Main, Frame Structure
  > INDICATIONS DURING ROTOPROBE INSPECTION OF HOLE "166" DUE TO VISIBLE DAMAGE INSIDE OF HOLE. RH WING COMPLIED WITH EA 6-5710-T0348474-P1
- [SDR FDEA2019082171916](https://openairdocs.org/sdr/FDEA2019082171916.md): Fitting · cracked · Aug 17, 2019 · N731FD · Airbus A300B4605R · Wing Main, Frame Structure
  > R/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-P1
- [SDR FDEA2019082171915](https://openairdocs.org/sdr/FDEA2019082171915.md): Fitting · cracked · Aug 17, 2019 · N731FD · Airbus A300B4605R · Fuselage Main, Structure
  > HOLE "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-P1

Next page: https://openairdocs.org/aircraft/N731FD/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N731FD/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.