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 FDEA201201110080Skin · misrepairedLT WING ALL SPEED AILERON LOWER SURFACE T/E AT APPROX RIB 15 MISREPAIRED. REPAIR CARRIED OUT IAW EA 6-5750-155869. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Jan 11, 2012 · N731FD · Airbus A300B4605R · AileronsSDR FDEA201201110085Seat Track · corrodedCABIN FORWARD ENTRY AREA SEAT TRACK AT FR14, -Y=450 FOUND CORRODED. R & R SEAT TRACK IAW SRM 51-40-21, REV 76. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 11, 2012 · N731FD · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201110084Structure · crackedCRACK INDICATION FOUND ON 3RD LAYER FROM BELOW OF HOLE 'F' DURING HFEC OPEN HOLE INSPECTION ON RT SIDE CENTER WING BOX REAR SPAR BOTTOM PANEL AT FRAME 47. REPAIR CARRIED OUT AT RT SIDE CENTER WING BOX FRAME 47 HOLE 'F' IAW EA 6-5710-155862 PART 1. REPAIR CLAJan 11, 2012 · N731FD · Airbus A300B4605R · Wing Main, Frame StructureSDR FDEA201201110083Floor Panel · dentedBULK CARGO COMPARTMENT FLOOR PANEL NR 162DF FOUND WITH MULTIPLE DENTS. R & R IAW AMM 53-10-35-04 REV 52.1. NEW FLOOR PANEL 162DF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 11, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201201110082Floor Panel · dentedBULK CARGO COMPARTMENT FLOOR PANEL NR 161GF FOUND DENTED IN SEVERAL LOCATIONS. R & R IAW AMM 53-10-35-04, REV 52.1. NEW FLOOR PANEL 161GF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 11, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201201110081Floor Panel · dentedBULK CARGO COMPARTMENT FLOOR PANEL NR 162HF FOUND DENTED IN SEVERAL LOCATIONS. R & R IAW AMM 53-10-35-04, REV 52.1. NEW FLOOR PANEL 162HF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 11, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201201090057Floor Panel · delaminatedAFT CARGO COMPARTMENTS FLOOR PANEL 152DF FOUND DELAMINATION. R & R IAW AMM 53-10-33-04, REV 52.1. NEW FLOOR PANEL 152DF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 9, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201201090056Floor Panel · delaminatedAIR CONDITIONING COMPARTMENT FLOOR PANEL NR 143CF FOUND DELAMINATED. FLOOR PANEL R & R IAW AMM 20-21-12, REV 52.1. NEW FLOOR PANEL NR 143CF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.Jan 9, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201201090055Floor Panel · delaminatedAFT CARGO COMPARTMENTS FLOOR PANEL 152HF FOUND DELAMINATION. R & R IAW AMM 53-10-33-04, REV 52.1. NEW FLOOR PANEL 152HF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 9, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201201090054Floor Panel · delaminatedAFT CARGO COMPARTMENTS FLOOR PANEL NR 152GF FOUND DELAMINATION. R & R IAW AMM 53-10-33-04, REV 52.1. NEW FLOOR PANEL 152GF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 9, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201201090053Floor Panel · delaminatedAFT CARGO COMPARTMENTS FLOOR PANEL NR 151HF FOUND DELAMINATION. R & R IAW AMM 53-10-33-04, REV 52.1. NEW FLOOR PANEL 151HF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 9, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201201090052Floor Panel · delaminatedAFT CARGO COMPARTMENTS FLOOR PANEL NR 152EF, FOUND DELAMINATION. R & R IAW AMM 53-10-33-04, REV 52.1. NEW FLOOR PANEL 152EF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 9, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201201090051Floor Panel · delaminatedAFT CARGO COMPARTMENTS FLOOR PANEL, NR 151GF FOUND DELAMINATION. R & R IAW AMM 53-10-33-04, REV 52.1. NEW FLOOR PANEL 151GF FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Jan 9, 2012 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201110094390Floorboard · delaminatedFWD CARGO FLOORBOARD DELAMINATED. REPLACED FLOORBOARD IAW SRDM SR27-53-005 REV D.Oct 9, 2011 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR FDEA201012044594Line · leakingHYD YELLOW RESERVIOR LO LEVEL - ECAM QTY AND OVERHEAD GAUGE INDICATIONS SHOWED YELLOW SYS QTY. DECLARED TO RED DOT. YELLOW PUMP LO PRESS WITH SUBSEQUENT LOSS OF YELLOW SYS COMPONENTS FACT. HYD LINE FOUND LEAKING TO THE AILERON SERVO CONTROL, LINE HAS BEEN RDec 4, 2010 · N731FD · Airbus A300F4605R · Hydraulic System, MainSDR FDEA200908133006Frame · corrodedUPON REMOVAL OF LAV SERVICE BOX FOUND CORROSION ON SKIN ON INTERNAL SIDE AT TOP SIDE OF CUT OUT. REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED INTERNAL LAV SERVICE PANEL CUTOUT DOUBLER AND INSTALLED FRAME SPICE REPAIR AT FR 12 BETWEEN STR 38 AND STR 44 LT IAug 13, 2009 · N731FD · Airbus A300B4605R · Fuselage Main, FrameSDR FDEA200908112978Skin · dentedAFT FUSELAGE SKIN BEHIND L2 DOOR 12" AFT OF FRAME 76 AND 4" BELOW STRINGER 21L HAS A DENT 1" SQ WITH .250 GOUGE IN CENTER DEPTH .030" DENT AT FRAME 76 STR 21L WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-12. NDT PERFORMED WITH NO CRACKS IAW NTM 51-10-08. REPAug 11, 2009 · N731FD · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR FDEA200906051937Check Valve · leakingPDIS 731 29-10 0001926 05JUN09 MEM OPEN R LOGPAGES: 01488379 AT FL 340 ECAM GREEN SYS RSVR LO. CONFIRMED GREEN SYS LOW QUANTITY. NEEDLE WAS IN YELLOW BAND AT RED DOT. COMPLIED WITH QRH AND LANDED 36C KMEM. GEAR WAS ALTERNATELY EXTENDED. AFTER EXTENDINGJun 5, 2009 · N731FD · Airbus A300F4605R · Hydraulic System, MainSDR FDEA200903170939Pump · leakingATB - TOTAL LOSS OF GREEN HYD FLUID DURING CLIMB-OUT, MANUAL GEAR EXTRACTION GREEN SYSTEM HYD. R & R HOSE AND NR 1 AND 2 ENG DRIVEN HYD PUMPS AND FILTERS PER MM 29-11-32-4. SERVICED GREEN SYSTEM, OPERATED FLIGHT CONTROLS THROUGH SEVERAL CYCLES, LEAK CHECK Mar 17, 2009 · N731FD · Airbus A300B4605R · Hydraulic Pump (Electric/Engine), MainSDR 07FDEA04966Relay · failedAT 200' AGL RECEIVED "TOO LOW GEAR" GPWS WARNING. LOG GEAR POS DET SYS 1. EXECUTED GO AROUND, SWITCH TO SYSTEM 2 AND LANDED UNEVENTFULLY. HAD GOOD INDICATIONS ON ALL 3 GEAR INDICATORS. ACN RELEASED FOR SERVICE PER MEL/CDL: 32-61-01-B CATEGORY: B EXPIRATIONNov 30, 2007 · N731FD · Airbus A300F4605R · Landing Gear Position and WarningSDR 07FDEA02768Valve · inoperativeDURING CRUISE FLT, LT WING SPOILER NR 4 DEPLOYED INFLT. A/C ROLLED HARD LT. DISC A/P AND COUNTERED RT. SPOILERS ON BOTH WINGS DEPLOYED FOR REMAINDER OF FLT. SPOILER NR 4 PREV MEL. ON DEBRIEFING CREW, RT WING SPOILERS DEPLOYED FOR CTRL . CORRECTION ONLY.Aug 4, 2007 · N731FD · Airbus A300B4605R · Drag Control SystemSDR 07FDEA02764Unknown · unknownDURING CR FLT, LT WING SPOILER NR 4 DEPLOYED IN FLT. A/C ROLLED HARD TO LT. DISCONNECTED A/P AND COUNTERED RT SPLRS ON BOTH WINGS DEPLOYED FOR REMAINDER OF FLT. SPLR NR 4 DEFERRED. ON DEBRIEFING CREW, RT WING SPOILERS DEPLOYED FOR CONTROL CORRECTION ONLY.Aug 3, 2007 · N731FD · Airbus A300B4605R · Drag Control SystemSDR 07FDEA02361Skin · damagedRT AILERON IS AT RIB 1 UPPER SKIN TRAILING EDGE DAMAGED REPAIR PERFORMED BY INSTALLING EXTERNAL PATCH IAW SRM 517712 PB.200 PARA 4.Jul 3, 2007 · N731FD · Airbus A300B4605R · AileronsSDR 07FDEA02360Skin · wornELONGATED HOLE ON PYLON NR 1 TO BOTTOM WING SKIN REPAIR PERFORMED BY OVERSIZING THE HOLES AND INSTALLING FREEZE PLUGS IAW DRAWING R 571-50532 REV A. APPROVED BY EA 6-5720-106472 REV A AND RAS/BAE/1004873/2007 ISS A.Jul 2, 2007 · N731FD · Airbus A300B4605R · Wing, Plate/SkinSDR 07FDEA02359Skin · wornELONGATED HOLES ON PYLON NR 2 TO BOTTOM WING SKIN REPAIR PERFORMED BY OVERSIZING THE HOLES AND INSTALLING FREEZE PLUGS IAW DRAWING R571-50532, APPROVED BY EA 6-5720-106472 REV A AND RAS/BAE/1004873/2007 ISS A.Jul 2, 2007 · N731FD · Airbus A300B4605R · Wing, Plate/SkinSDR 07FDEA02358Fastener · wrong partFOUND FASTENER WRONG INSTALLED ON SPOILER NR 5 RT, P/N 577-71000-004, S/N TS0863 IAW SB A300-57-6082. REPAIR PERFORMED BY INSTALLING THE ORIGINAL FASTENER AND FILLOUT THE MISDRILLED HOLE IAW EA 6-5770-106475 AND RAS/DABRE/7007745/2007 ISS A.Jul 2, 2007 · N731FD · Airbus A300B4605R · SpoilersSDR 07FDEA02350Panel · damagedOLD REPAIR ON PYLON NR 2 INBOARD SIDE, RIB 8 NOT CONFORM TO SRM DOUBLER REPAIR RENEWED IAW SRM 54-51-31 FIG 201. APPROVED BY EA 6-5451-1067447 REV A.Jul 2, 2007 · N731FD · Airbus A300B4605R · Nacelle/Pylon, Plate/SkinSDR 07FDEA02349Panel · crackedCRACKED HOLE (ABOUT 8MM ) AT RIB 8A PYLON NR 1, INBOARD SIDE. REPAIR PERFORMED BY DOUBLER INSTALLATION IAW SRM 54-51-31 PB 200, APPROVED BY EA 6-5451-106447 A.Jul 2, 2007 · N731FD · Airbus A300B4605R · Nacelle/Pylon, Plate/SkinSDR 07FDEA02324Skin Panel · chafedSKIN LEADING EDGE LT WING NEAR WOFX-69.0 CHAFING MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5741-106450 AND RAS/BAE/1004799/2007 ISS A.Jun 29, 2007 · N731FD · Airbus A300B4605R · Wing, Plate/SkinSDR 07FDEA02325Skin Panel · chafedSKIN LEADING EDGE RT WING NEAR WOFX-69.0 CHAFING MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5741-106450 AND RAS/BAE/1004799/2007 ISS.A.Jun 29, 2007 · N731FD · Airbus A300B4605R · Wing, Plate/SkinSDR 07FDEA02323Skin · chafedCHAFING MARK ON LEADING EDGE SKIN BETWEEN RIB 28 AND WING TIP REPAIR PERFORMED BY BLEND OUT THE AREA TO SMOOTH CONTOUR IAW EA 6-5741-106450 AND RAS/BAE/1004799/2007 ISS. AJun 29, 2007 · N731FD · Airbus A300B4605R · Leading Edge DevicesSDR 07FDEA02308Skin · misrepairedOLD FLUSH REPAIR DOUBLER ON RT SLAT NR 2 RT NOT CORRECT INSTALLED REPAIR PERFORMED BY RENEW THE DOUBLER REPAIR IAW SRM 57-43-11 FIG 202, APPROVED BY EA 6-5743-106467 AND RAS/FOK/111/2007 ISS A.Jun 28, 2007 · N731FD · Airbus A300B4605R · Leading Edge DevicesSDR 07FDEA02275None · noneCONFLICT BETWEEN OLD REPAIR AT RT INBOARD FLAP LOWER SKIN AND EMBODIMENT OF SB A300-57-6100 REPAIR PERFORMED BY PATCH AND SHIM REPAIR IAW SRM 57-50-00 FIG 206, APPROVED BY EA 6-5753-106461 AND RAS/FOK/109/2007 ISS A.Jun 26, 2007 · N731FD · Airbus A300B4605R · Standard Practices/StructuresSDR 07FDEA02192Plate · noneOLD REPAIR DOUBLER AT C20, P51-54 RT, NOT COMPATIBLE WITH P TO F CONVERSION. REPAIR PERFORMED BY INSTALLATION OF NEW EXTERNAL DOUBLER IAW EA 6-5313-106478 AND RAS/DABRE/7007753/2007 ISSUE "A".Jun 19, 2007 · N731FD · Airbus A300B4605R · Standard Practices/StructuresSDR 07FDEA02191Skin · misrepairedOUTER FLAP RT, OLD STATIC DISCHARGER REPAIR FOUND NOT CONFORM TO RAS/FOK/110/2003 (DOUBLER THICKNESS). REPAIR PERFORMED BY INSTALLATION OF NEW DOUBLER IAW RAS/FOK/110/2003 ISSUE "A".Jun 19, 2007 · N731FD · Airbus A300B4605R · Aircraft StructuresSDR 07FDEA02126Fitting · corrodedPYLON NR 2 FWD ENGINE FITTING, CORROSION ON TENSILE BOLT HOLES REPAIR PERFORMED BY REMOVAL OF CORROSION THRU OVERSIZING AND BUSH INSTALLATION IAW EA 6-5442-106473 AND RAS/052121/005/2007 ISS. A.Jun 14, 2007 · N731FD · Airbus A300B4605R · Nacelle/Pylon, Attach FittingsSDR 07FDEA02105Skin Panel · damagedOLD REPAIR (BLEND OUT ) ON LT WING BOTTOM SKIN LOWER SURFACE AROUND HOLE 389 IAW DRW R571-40141 SH 17 REPAIR ACCEPTACLE BY AI RAS/BAE/1004818/2007 ISS. A, APPROVED BY EA 6-5720-106454.Jun 11, 2007 · N731FD · Airbus A300B4605R · Wing, Plate/SkinSDR 07FDEA02030Skin · corrodedCORROSION WITH CRACK FINDINGS (A= 22MM, B= 25MM) ON HOLE 699 (DRW R571-40141 SHEET 12), LT WING BOTTOM SKIN LOWER SURFACE. REPAIR PERFORMED BY REAM UP TO NEXT OVERSIZE IAW EA 6-5720-106453 AND RAS/BAE/1004815/2007 ISS. AMay 31, 2007 · N731FD · Airbus A300B4605R · Wing, Plate/SkinSDR 07FDEA02029Skin · corrodedCRACKS AND CORROSION ON RT WING BOTTOM SKIN LOWER SURFACE ON (HOLE 712 CORRODED, HOLE 311 CRACKED A=12MM, B11MM, DRW R571-40141 SHEET 14). REPAIR PERFORMED BY REAM UP IAW EA 6-5720-106453 AND RAS/BAE/1004815/2007 ISS.AMay 31, 2007 · N731FD · Airbus A300B4605R · Wing, Plate/SkinSDR 07FDEA02028Skin Panel · corrodedCORROSION LT WING TOP SKIN PANEL NR 3, RIB 26-27, STRINGER 17A TO REAR SPAR REPAIR PERFORMED BY BLEND OUT AND REMOVAL OF AFFECTED FASTENER IAW EA 6-5730-106449 AND RAS/BAE/1004794/2007 ISS.AMay 31, 2007 · N731FD · Airbus A300B4605R · Wing, Plate/SkinSDR 07FDEA02008Stiffener · crackedCRACK ON LT C12A STIFFENER FITTING, CRACK LENGTH 4MM. REPAIR PERFORMED BY INCORPORATION OF SB A300-53-6137, APPROVED BY EO 6-5340-7-5003.May 29, 2007 · N731FD · Airbus A300B4605R · Fuselage Miscellaneous StructureSDR 07FDEA02004Frame · damagedGROOVE AND MISDRILLED SPOT AT C73, P 30-31 RT. REPAIR PERFORMED BY REWORK OF EXISTING GROOVE PER SRM 51-73-10 AND INSTALL RIVET LN9198-3200 IN DRILLED HOLE, APPROVED BY EA 6-5218-106451 AND RAS/DAHAM/4022141/2007 ISS. AMay 29, 2007 · N731FD · Airbus A300B4605R · Fuselage Main, FrameSDR 07FDEA02003Stringer · corrodedCORROSION ON STRINGER 56, C76-77 LHS CORROSION BLEND OUT REPAIR PERFORMED IAW EA 6-5318-106463 AND RAS/DAHAM/4022176/2007 ISS.AMay 29, 2007 · N731FD · Airbus A300B4605R · Fuselage Main, Longeron/StringerSDR 07FDEA02002Panel · damagedMARKS, DENT, CRACKS AND NICKS AT C47-53, BETWEEN TRACK 5 LT AND 5 RT. REPAIR PERFORMED BY DOUBLER REPAIR AT INTERNAL WEB C47, DRESS OUT SKIN ON DIAPHRAGM , BLEND OUT DAMAGED AREAS IAW EA 6-5315-106463 AND RAS/051804/007/2007 8ISS. AMay 29, 2007 · N731FD · Airbus A300B4605R · Fuselage Floor PanelSDR 07FDEA02000Frame · damagedFOUND 5 TOO LARGE HOLES AT JACKING POINT C 59, P26-27 RHS REPAIR PERFORMED BY HI-LOK HL110VF8 IN PLACE HL110VF6 IAW EA 6-5317-106466 AND RAS/DAHAM/4022180/2007 ISS. BMay 29, 2007 · N731FD · Airbus A300B4605R · Fuselage Main, FrameSDR 07FDEA01997Fitting · corrodedCORROSION ON AFT CARGO DOOR LOCK FITTING REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.May 29, 2007 · N731FD · Airbus A300B4605R · Fuselage Main, Attach FittingsSDR 07FDEA01996Fitting · corrodedCORROSION ON AFT CARGO DOOR LOCK FITTING REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.May 29, 2007 · N731FD · Airbus A300B4605R · Fuselage Main, Attach FittingsSDR 07FDEA01812Floorbeam · corrodedTOP CAP BEAM C38.2 CORRODED REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.May 15, 2007 · N731FD · Airbus A300B4605R · Fuselage Main, Floor BeamSDR 07FDEA01811Crossbeam · corrodedCROSSBEAM C58 CORRODED REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.May 15, 2007 · N731FD · Airbus A300B4605R · Fuselage Main, StructureSDR 07FDEA01810Stringer · corrodedSTRINGER CORROSION P53 AND P55 AT C65-66 REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.May 15, 2007 · N731FD · Airbus A300B4605R · Fuselage Main, Longeron/Stringer
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