N746FD
Service difficulty reports · 234
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 = 'N746FD' 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.
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 = 'N746FD' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA200906222201Panel · wornFOUND LOOSE FASTENER AND WORN HOLES ON RT WING OUTER SHROUD BOX CLOSING PANEL. REPAIR PERFORMED BY REPLACEMENT OF PART WITH THICKER MATERIAL AND INSTALLING OVERSIZE FASTENER IAW RAS/BAE/1010076/2009 ISS. A, APPROVED BU EA 6-5750-131240.SDR FDEA200906222200Panel · wornFOUND LOOSE FASTENER AND WORN HOLES ON LT WING OUTER SHROUD BOX CLOSING PANEL. REPAIR PERFORMED BY REPLACEMENT OF PART WITH THICKER MATERIAL AND INSTALLING OVERSIZE FASTENER IAW RAS/BAE/1010076/2009 ISS. A, APPROVED BU EA 6-5750-131240.SDR FDEA200906222198Panel · delaminatedFOUND DELAMINATION ON LT WING OUTER FIXED T/E TOP SKIN PANEL REPAIR PERFORMED IAW SRM 51-77-11 PARA 3.E AND 4 M, APPROVED BY RAS/BAE/1009714/2009 ISS.A AND EA 6-5750-131239.SDR FDEA200906222197Skin · chafedFOUND CHAFING MARKS ON LT SLAT NR1 LOWER SKIN BETWEEN RIB 25-26 REPAIR PERFORMED BY REMOVAL OF CHAFING MARKS IAW RAS/FOK/069/2009 ISS. B, APPROVED BY EA 6-5750-129121.SDR FDEA200906222196Splice · damagedFOUND DAMAGED AND ELONGATED HOLES AT C 40 LT IN SPLICE. REPAIR PERFORMED BY REAM UP THE HOLES UNTIL DAMAGE REMOVAL , NDT FOR CRACK FREE CONDITION AND INSTALLING NAS5350 AND NAS5356 FASTENER IAW. RAS 70519374/043/2009 ISS. A, APPROVED BY EA 6-5310-131224.SDR FDEA200906222195Splice · damagedFOUND TOOLING DAMAGE ON C 40 , HOLE 15RH. THE SB 53-6063 WAS TERMINATED BY PREVIOUS OPERATOR. REPAIR PERFORMED BY REMOVING THE DAMAGE , INSPECT THE HOLES AND INSTALLING A CONICAL WASHER IAW RAS 70519200/009/2009 ISS. APPROVED BY EA 6-5310-131222.SDR FDEA200906152104Fitting · corrodedFOUND CORROSION ON UPPER AND LOWER SPIGOT FITTING REPAIR PERFORMED BY REPLACEMENT OF PARTS IAW SB, APPROVED BY EA 6-5440-120195.SDR FDEA200906152103Fitting · corrodedFOUND CORROSION ON UPPER AND LOWER SPIGOT FITTING REPAIR PERFORMED BY REPLACEMENT OF PARTS IAW SB A300-54-6017, APPROVED BY EA 6-5440-120195.SDR FDEA200906152102Spar · corrodedFOUND CORROSION ON UPPER SPAR UNDER PYLON SPIGOT FITTING, RIB 12 REPAIR PERFORMED BY BLEND OUT THE CORROSION , NDT FOR CRACK FREE CONDITION IAW RAS 70519120/011/2009 ISS. A, APPROVED BY EA 6-5440-120195.SDR FDEA200906152101Rib · chafedFOUND CHAFING MARKS ON SLAT NR 2 RT, LWR SKIN RIB 3-4 AND 2 EXISTING FASTENER INSTALLED , RIB 11-12. REPAIR PERFORMED BY BLEND OUT THE CHAFING MARKS , NDT FORM CRACK FREE CONDITION AND REMOVAL OF THE 2 ADDITIONAL FASTENERS , CHECK FOR CRACKS AND INSTALLING NSASDR FDEA200906152100Skin · chafedFOUND CHAFING MARKS ON LT WING L/E "D" NOSE JACK RIB 1-2 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR , NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1009485/2009 ISS.A , APPROVED BY EA 6-5740-129116.SDR FDEA200906152098Shear Tie · damagedFOUND DAMAGES IN DIFFERENT HOLES AT FRAME AND FRAME BASE FITTING AT C44 RT, P35-37. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200906152096Frame · damagedFOUND DAMAGES IN DIFFERENT HOLES AT FRAME AND FRAME BASE FITTING AT C44 RT, P35-37. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200906152095Fitting · corrodedFOUND CORROSION ON PYLON NR 1 LOWER FITTING, RIB 12. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200906152094Fitting · corrodedFOUND CORROSION ON PYLON NR 2 LOWER FITTING, RIB 12. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200906102002Skin · chafedFOUND CHAFING AND IMPACT MARKS ON RT WING L/E D-NOSE SKIN OTBD OF JACK RIB 1. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE CONDITION IAW. RAS/BAE/1009632/2009 ISS A, APPROVED BY EA 6-5740-131214.SDR FDEA200906081948Web · damagedFOUND DAMAGED AREA IN WEB/SKIN C 49, P31 LT/RT. REPAIR PERFORMED BY CUT OUT, NDT FOR CRACK FREE CONDITION IAW RAS 705193288/009/2009 IS A, APPROVED BY EA 6-5310-129145.SDR FDEA200906081947Web · crackedFOUND DAMAGED AREA IN WEB/SKIN C 49, P31 LT/RT REPAIR PERFORMED BY CUT OUT, NDT FOR CRACK FREE CONDITION IAW RAS 705193288/009/2009 IS A, APPROVED BY EA 6-5310-129145.SDR FDEA200906081946Skin · corrodedFOUND CORROSION ON AFT CARGO DOOR INNER SKIN. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200906041912Hinge Bracket · wornFOUND WORN BORES IN HINGE BRACKET A576-61024-201 OF RT ASA. REPAIR PERFORMED BY OVERSIZING THE BORE AND BUSH INSTALLATION IAW RAS/FOK/132/2009 ISS B, APPROVED BY EA 6-5760-131211.SDR FDEA200906041911Hinge Bracket · wornFOUND WORN BORES IN HINGE BRACKET A576-61024-200 OF LT ASA. REPAIR PERFORMED BY OVERSIZING THE BORE AND BUSH INSTALLATION IAW RAS/FOK/134/2009 ISS B, APPROVED BY EA 6-5760-131210.SDR FDEA200906041910Skin · damagedFOUND ON TOP SKIN RT WING RIB 13-14, STRINGER 20, RIVETS NOT CORRECT INSTALLED. REPAIR PERFORMED IAW DWG R573-40251 ISS. C, BUSHING REPAIR, APPROVED BY RAS/BAE/1010098/009 ISS A AND EA 6-5710-129197.SDR FDEA200906031901Frame · corrodedFOUND CORROSION ON FRAME C 39 BETWEEN CENTER LINE STRINGER 55 AND 52 RT AND ON AFT SIDE PANEL BETWEEN P 49-48 RT. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR CRACK FREE AND CORROSION FREE CONDITION AND REPAIR OF BULKHEAD FRAME C 39 AND T-SECTION BETWSDR FDEA200905281834Spar · corrodedFOUND CORROSION IN NR 1 PYLON UPPER SPAR WEB UNDER FITTING A546-11024-204. REPAIR PERFORMED BY SMOOTH BLEND OUT AND NDT FOR CORROSION REMOVAL AND CRACK FREE CONDITION IAW RAS 70519602/018/2009 ISS. C, APPROVED BY EA 6-5410-129195.SDR FDEA200905261794Fitting · chafedFOUND CHAFING MARK ON VERTICAL STABILIZER FITTING NR 1 REPAIR PERFORMED BY NDT INSPECTION WITHOUT FINDINGS AND SURFACE REPAIR IAW RAS/DAHAM/4027020/2009 ISS A, APPROVED BY EA 6-5530-129170.SDR FDEA200905111612Beam · corrodedFOUND CORROSION ON FWD CARGO DOOR SILL BEAM C 23-25A REPAIR PERFORMED BY CUT OUT THE SILL BEAM IAW, DRAWING R537-06913 ISS A AND BUSH REPAIR IAW RAS/EFW/9000161/2009 ISS B, APPROVED BY EA 6-5310-129117.SDR FDEA200905111610Structure · damagedFOUND ON SPOILER NR 6 BEARING BORE OUT OF LIMIT. REPAIR PERFORMED BY INSTALLING COUNTERSUNK BUSHINGS IAW RAS/DABRE/7010816/2009 ISS A, APPROVED BY EA 6-5720-129171.SDR FDEA200905111609Frame · corrodedFOUND CORROSION AROUND ANCHOR NUTS HOLES OF FRAME 20A, P28-39 RT REPAIR PERFORMED BY BLEND OUT THE CORROSION AND SPLICING A NEW SECTION BETWEEN P 33-36 RT IAW RAS/EFW/9000168/2009, APPROVED BY EA 6-5310-129155.SDR FDEA200905071563Beam · corrodedFOUND CORROSION ON UPPER FLANGE OF AFT CARGO DOOR SILL BEAM C59 AND C 63 REPAIR PERFORMED BY CORROSION REMOVAL AND REPAIR THE SILL BEAM IAW DRAWING R539-70133 ISS G, APPROVED BY RAS/EFW/9000164/2009 ISS A AND EA 6-5310-129149.SDR FDEA200905071562Doubler · corrodedFOUND CORROSION ON LT AFT PAX DOOR SURROUND STRUCTURE CORNER DOUBLER C75A-76, P 26. REPAIR PERFORMED BY CORROSION BLEND OUT IAW RAS/EFW/9000173/2009 ISS A, APPROVED BY EA 6-5310-129158.SDR FDEA200905071561Beam · corrodedFOUND CORROSION ON LT AFT PAX DOOR SURROUND STRUCTURE LONGITUDINAL BEAM C73A-75A, P 26. REPAIR PERFORMED BY CORROSION BLEND OUT AND INSTALLING REPAIR BUSH IAW RAS/EFW/9000173/2009 ISS A, APPROVED BY EA 6-5310-129158.SDR FDEA200905071559Skin · corrodedFOUND CORROSION ON LT AFT PAX DOOR SURROUND STRUCTURE C73A-75A, P 26. REPAIR PERFORMED BY CORROSION BLEND OUT IAW RAS/EFW/9000172/2009 ISS A, APPROVED BY EA 6-5310-129158.SDR FDEA200905071558Frame · corrodedFOUND CORROSION ON LT AFT PAX DOOR SURROUND STRUCTURE C73A-75A, P 26 REPAIR PERFORMED BY CORROSION BLEND OUT IAW RAS/EFW/9000172/2009 ISS A, APPROVED BY EA 6-5310-129158.SDR FDEA200905041500Skin · chafedFOUND SCRATCH MARKS IN SKIN C 59-60, P 1LT-1RT. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW RAS/EFW/9000175/2009 ISS A, APPROVED BY EA 6-5330-129144.SDR FDEA200905041499Frame · crackedFOUND CRACK ON C 45 RT IN AREA 1(SEE EO 6-5310-7-5015 PT1), CENTER WING SECTION. REPAIR PERFORMED BY NDT FOR FURTHER CRACKS AND ACCOMPLISHMENT OF REPAIR IAW EO 6-5310-7-5015 PT 2, APPROVED BY RAS 70519824/005/2009 ISS A AND EA 6-5710-129119.SDR FDEA200905041498Skin · corrodedFOUND CORROSION ON LT WING TIP UNDER LOWER STATIC DISCHARGER REPAIR PERFORMED BY BLEND OUT THE CORROSION AND APPLY FILLING COMPONENT IAW RAS/FOK/059/2009 ISS A, APPROVED BY EA 6-5720-129117.SDR FDEA200904271423Skin · dentedFOUND DENT ON CENTER FLAP RT LOWER SKIN RIB 13-15 PATCH REPAIR PERFORMED IAW SRM 57-50-00 FIG 205.SDR FDEA200904271420Fitting · crackedFOUND CRACK ON AFT CARGO DOOR LATCH FITTING C 60 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200904271419Stringer · damagedFOUND WEAR MARKS ON STRINGER P44 LT, C 39-40 REPAIR PERFORMED BY BLEND OUT OF DAMAGE TO SMOOTH CONTOUR IAW RAS 70519299/007/2009 ISS A, APPROVED BY EA 6-5310-129101.SDR FDEA200904271418Stringer · corrodedFOUND CORROSION ON STRINGER 56 LT, C76-77. REPAIR PERFORMED BY BLEND OUT THE CORROSION, NDT FOR DAMAGE REMOVAL AND FLAP PEENING IAW RAS/EFW/9000163/2009 ISS A, APPROVED BY EA 6-5310-129122.SDR FDEA200904271417Stringer · corrodedFOUND CORROSION ON STRINGER P 56 LT, C 57.3-58 REPAIR PERFORMED BY REPLACEMENT OF STRINGER IAW RAS/EFW/9000167/2009 ISS B, APPROVED BY EA 6-5310-129130.SDR FDEA200904271416Crossbeam · corrodedFOUND CORROSION ON CROSSBEAM C 61 RT REPAIR PREFORMED BY RE-PLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200904061198Failsafe · corrodedFOUND CORROSION ON FAILSAFE RING C 74-75A, P 11-12 LT. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS /EFW/9000169/2009 ISS A, APPROVED BY EA 6-5310-129147.SDR FDEA200904061197Skin · chafedFOUND CHAFING MARKS ON CROSS SHEET P15LT, C 56-56A. REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS /EFW/9000171/2009 ISS A, APPROVED BY EA 6-5310-129124.SDR FDEA200904061196Skin · chafedFOUND SCRATCHES ON SKIN PANEL C 62-63, P 2LT-2RT REPAIR PERFORMED BY BLEND OUT, NDT FOR CRACK FREE CONDITION AND FLAP PEENING IAW RAS/9000174/2009 ISS A, APPROVED BY EA 6-5330-129146.SDR FDEA200904021147Profile · corrodedFOUND CORROSION ON LONGITUDINAL PROFILE, C 63-64, Y-805 AND Y805 REPAIR PERORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200904021144Fitting · corrodedFOUND CORROSION ON CORNER FITTING C 58 RT. REPAIR PERORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200904021142Crossbeam · corrodedFOUND CORROSION ON CROSSBEAM C 58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR FDEA200904021140Frame · damagedMISDRILLED HOLE IN FRAME 50, BETWEEN P 15-16 LT REPAIR PERFORMED BY REWORK THE RIB OF FRAME AND PLUG THE HOLE IAW RAS /EFW/9000160/2009 ISS A, APPROVED BY EA 6-5310-129114.SDR FDEA200904021137Skin · damagedFOUND OVERSIZED HOLE IN SKIN ON C 54, P 35-36 LT AND NOT ENOUGH EDGE DISTANCE IN A EXTRUDED PROFILE. REPAIR PERFORMED BY COLLAR BUSH INSTALLATION IN SKIN WITH DIAMETER OF 8.0MM AND INSTALLING HL10VF6 IN AFFECTED HOLE IAW RAS 70518454/004/2009 ISS A, APPROVED
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