N724FD
Service difficulty reports · 218
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 = 'N724FD' 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 = 'N724FD' 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 FDEA201002030319Module · inoperativeAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. HANDLE COULD NOT BE MOVED FROM THE FULL DOWN POSITION. R & R MLG CONTROL UNIT 2 GA AS PER MM 32-31-11-4. R & R PROXIMITY DETECT UNIT 54GB AS PER MM 32-31-71-4. PERFORMED NORMAL ETRACTION AND EXTENTION AS PERSDR FDEA200904271457Transmitter · crackedIN CRUISE, BLUE R SVR LO LEVEL ECAM WARNING. CONFIGURED HYD BLUE SYSTEM LOSS. C/W ECAM AND ALL CHECKLISTS. NORMAL LANDING IN LEMD. FOUND BLUE SYSTEM HYD PRESS TRANSMITTER IN LT WHEEL WELL SPLIT OPEN. REPLACED TRANSMITTER MPN 64250-005-1 CPN 2910415 SN ON SDR 08FDEA01699Frame · crackedRT WING, FAIRING 632BB WITH FRAME ATTACHMENT SIDE LOAD CRACK. FRAME REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5720-117327.SDR 08FDEA01660Arm · corrodedLT PAX DOOR SUSPENSION LOWER ARM (PN 5211134600000) WITH CORROSION ON JUMPER HOLE. THE ARM WAS REPLACED IN ACCORDANCE WITH AMM 52-10-12.SDR 08FDEA01661Angle · crackedCOCKPIT, CONNECTION ANGLE OF FR10 AT Y-953 TO INTERCOSTAL PANEL FOUND CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WITH SRM 51-40-21 AND SRM 51-72-10.SDR 08FDEA01648Plate · crackedLT WING, L/E ACCESS PANEL ATTACHMENT CHORD (LANDING PLATE) CRACKED 523BB BETWEEN RIB 8 AND 9. REPAIRED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION 6-5720-117325.SDR 08FDEA01340Door Frame · dentedFWD CARGO COMPT DOOR FRAME 20A FOUND DENTED BETWEEN STGR 31-32 RT. FRAME WAS REPAIRED IN ACCORDANCE WITH EA 6-5310-117323.SDR 08FDEA01447Stiffener · corrodedPYLON NR 1 STIFFENER AT RIB 9 WITH CORROSION. THE STIFFENER WAS REPLACED IN ACCORDANCE WITH SRM 51-72-10 AND 51-40-21.SDR 08FDEA01339Structure · damagedPYLON NR 1, PYRAMID HOLE WITH CORROSION (FWD RT).SDR 08FDEA01701Structure · damagedHORIZONTAL STAB, UPPER APRON RT SIDE DAMAGED RT UPPER RT SIDE WAS REPAIRED IAW FEDEX EA 6-5510-117324.SDR 07FDEA04336Skin · corrodedFOUND CORROSION ON TOP SKIN PANEL SECTION 19, BETWEEN FRAME 77-78, NEAR STGR 2-3 LT. REPAIR PERFORMED BY BLEND OUT CORROSION AND FLAP PEENING IAW EA 6-5319-92171 AND RAS/DATLS/0002704/2005 ISSUE A.SDR 07FDEA04335Beam · corrodedCORROSION FOUND ON LT FWD PAX DOOR, BEAM NR 1. REPAIR PERFORMED BY BLEND OUT CORROSION, NDT INSPECTION FOR CRACK FREE CONDITION IAW EA 6-5211-92172 AND RAS/AS/215/2005 ISSUE A.SDR 07FDEA04334Doubler · corrodedCORROSION ON KRUEGER FLAP DOUBLER AT FRAME 38, STGR 28-33 LT. REPAIR PERFORMED BY BLEND OUT CORROSION, NDT INSPECTION FOR CRACK FREE CONDITION IAW EA 6-5314-92161 AND RAS/DATLS/0002692/2005 ISSUE A.SDR 07FDEA04333Butt Joint · corrodedCORROSION ON BUTT-JOINT BETWEEN FRAME 101-102, STGR 23 RT. REPLACEMENT OF L-SEGMENT IAW SRM 51-72-10.SDR 07FDEA04332Structure · corrodedCORROSION ON L-SEGMENT AT FRAME 101, STGR 14 LT TO 14 RT. REPLACEMENT OF L-SEGMENT IAW SRM 51-72-10.SDR 07FDEA04331Angle · corrodedFOUND CORRODED ANGLES AT FRAME 92 BETWEEN STGR 9 LT TO 9 RT. REPLACEMENT OF ANGLES IAW SRM 51-72-10.SDR 07FDEA04330Angle · corrodedFOUND CORRODED ANGLE BETWEEN FRAME 92-93, STGR 14-15 LT. REPLACEMENT OF ANGLE IAW SRM 51-72-10.SDR 07FDEA04329Doubler · corrodedFOUND CORRODED DOUBLER AT FRAME 92, STGR 23 AD. REPLACEMENT OF DOUBLER IAW SRM 51-72-10.SDR 07FDEA04328Frame · corrodedCORROSION ON T-SEGMENT FRAME 92, STGR 12 LT TO RT. REPLACEMENT OF T-SEGMENT IAW SRM 51-72-10.SDR 07FDEA04327Skin · misrepairedOLD EXTERNAL DOUBLER REPAIR AT FUSELAGE SKIN BETWEEN FRAME 57.3-58, STGR 35-36 RT, NOT CONFORM TO SRM 53-10-12/FIG 225 OR 203. DOUBLER REPAIR RENEWED IAW SRM 53-10-12/FIG 225.SDR 07FDEA04326Frame · corrodedCORRODED ANGLE SEGMENTS AT FRAME 92 BETWEEN STGR 14 LT TO RT. REPAIR PERFORMED BY REPLACEMENT OF SEGMENTS IAW SRM 51-72-10.SDR 07FDEA04325Floorbeam · corrodedHEAVY CORROSION ON CROSSBEAM BETWEEN FLOORBEAM 12A-14. REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10.SDR 07FDEA04324Frame · misrepairedLESS EDGE MARGIN FOR INSTALLATION OF FASTENER HL DAN 5-6 DURING PTOF CONVERSION ON ATTACH ANGLE AT FRAME 66, STGR 35 RT. REPLACEMENT OF ATTACH ANGLE IAW SRM 51-72-10.SDR 07FDEA04323Floorbeam · corrodedFOUND CORROSION ON CROSSBEAM AT FRAME 58, AFT CARGO COMPARTMENT. CROSSBEAM SPLICE REPAIR PERFORMED IAW SRM 53-10-15/FIG 207/SEC F-F.SDR 07FDEA04322Floorbeam · corrodedCORROSION ON CROSSBEAM AT FRAME 60 LT, AFT CARGO COMPARTMENT. REPAIR PERFORMED REPLACEMENT OF LT HALF-BEAM IAW SRM 51-72-10 AND BEAM SPLICE IAW SRM 53-10-15/FIG 207/SEC "E-E".SDR 07FDEA04321Floorbeam · corrodedCORROSION ON CROSSBEAM AT FRAME 62 RT, AFT CARGO COMPARTMENT. REPLACEMENT OF THE CORRODED RT HALF-BEAM IAW SRM 51-72-10 AND SPLICE IAW SRM 53-10-15/FIG 207/SEC F-F.SDR 07FDEA04320Floorbeam · corrodedFOUND CORROSION ON CROSSBEAM FRAME 62 RT OUTSIDE, AFT CARGO COMPARTMENT. REPLACEMENT OF CROSSBEAM IAW SRM 51-72-10.SDR 07FDEA04308Skin · damagedOLD REPAIR ON RT OUTER FLAP TRAILING EDGE AT INBD SIDE, LOWER SKIN AND END RIB IN BAD CONDITION WITH SEVERAL DAMAGES. REPAIR PERFORMED BY REPLACEMENT OF UPPER SKIN PANEL, RESTORING CONDITION OF TD FOK/010/2005 ISSUE A AND REPLACEMENT OF RIVETS IN LOWER SKIN PSDR 07FDEA04314Stringer · corrodedCORROSION ON STRINGER 56 LT, NEAR TO FRAME 59 OUT OF LIMIT REMAINING THICKNESS IS 3,8MM (NOMINAL 4,5MM). REPAIR PERFORMED BY BLEND OUT TO DEPTH NO GREATER THAN REPORTED, ROTOTEST INSPECTION IN VOID FASTENER HOLES WITH NIL FINDINGS AND NEW FASTENER INSTALLATIOSDR 07FDEA04313Diaphragm · dentedFOUND TWO DENTS ON DIAPHRAGM BETWEEN TRACK 4-5 LT, FRAME 52-54. REPAIR PERFORMED BY SMOOTHLY REWORK AT DENT ONE, THE OTHER ONE IS REPAIRED BY DRILLING OUT THE SCRATCH (DIA 4MM) AND INSTALLING AN ALUMINUM RIVET IAW EA 6-5314-82929 AND RAS/AS/0166/2005 ISSUE SDR 07FDEA04312Frame · damagedFOUND LOCK FASTENER HOLE WITH DIAMETER 6,26MM ON FRAME 54.2, BETWEEN STGR 34-35 LTS, IT'S IN THE PTOF AREA AND IN COLLISION WITH FRAME FOOT. REPAIR PERFORMED BY INSTALLING BUSHING RE0001-202 PER DRW RE0003-004 WITH NECESSARY LOCK FASTENER IAW ENG-STATEMENT.SDR 07FDEA04311Plate · damagedDAMAGED SHEAR PLATE BETWEEN FRAME 69-70, STGR 40 RT. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.SDR 07FDEA04310Plate · crackedCRACKED SHEAR PLATE BETWEEN FRAME 79-80, STGR 26 RT. REPLACEMENT OF SHEAR PLATE IAW SRM 51-72-10.SDR 07FDEA04309Stringer · corrodedCORROSION ON STRINGER 44 LT, BETWEEN FRAME 16A-17. STRINGER SPLICE REPAIR PERFORMED IAW SRM 53-12-14/FIG 201.SDR 07FDEA04306Skin Panel · failedFOUND OLD REPAIR ON BOTTOM SKIN FLANGE SUPPORT STRAP AFT FROM REAR SPAR, INBOARD OF RIB NR 9, LT WING CRACK (20MM) IN SUPPORT FLANGE. REPAIR PERFORMED BY MOD SB A300-57-6064 (FINAL REPAIR).SDR 07FDEA04304Plate · noneFOUND OLD REPAIR AT CLOSING RIB TO TRACK NR 1 LT WING (LHT GLB S868048 AND REPORT 34624), PERMANENT REPAIR HAVE TO BE PERFORMED AT NEXT D-CHECK. REPAIR PERFORMED BY INSTALLING NEW ORIGINAL PARTS IAW DWG A572-42993, A572-42285 AND SRM 51-72-10.SDR 07FDEA04303Angle · noneFOUND OLD REPAIR AT CLOSING RIB TO TRACK NR 1 LT WING (LHT GLB S868048 AND REPORT 34624), PERMANENT REPAIR HAVE TO BE PERFORMED AT NEXT D-CHECK. REPAIR PERFORMED BY INSTALLING NEW ORIGINAL PARTS IAW DWG A572-42993, A572-42285 AND SRM 51-72-10.SDR 07FDEA04302Stringer · looseFOUND DEBONDED STRINGER 42 BETWEEN FRAME 28-30 LT. REPAIR PERFORMED BY CUTTING STRINGER BETWEEN FRAME 30-31, REMOVING AND CHECKING THEM IF DAMAGED. INSTALLING AGAIN IAW SRM 53-10-14/FIG 201, 202.SDR 07FDEA04301Stringer · delaminatedFOUND DEBONDED STRINGER 39 BETWEEN FRAME 28-30 LT AND STGR 41 BETWEEN FRAME 29-30 LT. REPAIR PERFORMED BY CUTTING BOTH STRINGER BETWEEN FRAME 30-31, REMOVING AND CHECKING THEM IF DAMAGED. INSTALLING AGAIN IAW SRM 53-10-14/FIG 201, 202.SDR 07FDEA04300Skin Panel · failedOLD EXTERNAL DOUBLER REPAIR ON FUSELAGE SKIN AT FRAME 67, STGR 51-54 RT, DOUBLER THICKNESS NOT CONFORM TO SRM. DOUBLER REPAIR RENEWED IAW SRM 53-10-12/FIG 225/SH 2.SDR 07FDEA04296Longeron · damagedFOUND DAMAGED LONGERON BETWEEN DOOR ATTACH FITTING FRAME 22A-23, BEAM NR 1 OF FWD CARGO COMPARTMENT DOOR. REPLACEMENT OF LONGERON IAW SRM 51-72-10.SDR 07FDEA04295Failsafe · corrodedFOUND CORROSION AT RT FWD PAX DOOR FAIL/SAFE RING (AFT LOWER CORNER) BETWEEN FRAME 14C-17, STGR 26-27 RT. REPAIR PERFORMED BY BLEND OUT CORROSION AND NDT INSPECTION FOR ANY REMAINING CORROSION IAW EA 6-5312-82932 AND RAS/AS/185/2005 ISSUE A.SDR 07FDEA04294Failsafe · corrodedFOUND EXFOLIATION CORROSION AT LT FWD PAX DOOR FAIL/SAFE RING (FWD LOWER CORNER) BETWEEN FRAME 13-14, STRINGER 25-28 LT. REPAIR PERFORMED BY BLEND OUT CORROSION AND NDT INSPECTION FOR ANY REMAINING CORROSION IAW EA 6-5312-82930 AND RAS/AS/182/2005 ISSUE A.SDR 07FDEA04293Frame · gougedGOUGES ON INNER FLANGE OF FRAME 55, STGR 15 LT AND RT, AFT OF EMERGENCY EXIT DOOR TORSION BOX, CAUSED BY INCORRECT EQUIPMENT FASTENER INSTALLATION. REPAIR PERFORMED BY SMOOTH BLEND OUT, COVERED BY EA 6-5316-92163, APPROVED BY RAS/DATLS/0002690/2005 ISSUE A.SDR 07FDEA04292Panel · gougedFOUND GOUGE AS CAUSED BY INCORRECT EQUIPMENT FASTENER INSTALLATION AT TORSION BOX CROSS SHEET (PANEL) BETWEEN FRAME 56-56A, STGR 14-16 RT, EMERGENCY EXIT DOOR SURROUND PANEL. REPAIR PERFORMED BY SMOOTH BLEND OUT, HFEC INSPECTION FOR CRACK FREE CONDITION AND FSDR 07FDEA04291Skin Panel · corrodedFOUND HEAVY CORROSION ON SKIN PANEL BETWEEN FRAME 39-40, STGR 28-33 RT. REPAIR PERFORMED BY BLEND OUT CORROSION IAW TD 942.038560/011/2005 ISSUE A AND TD 942.038560/047/2005 ISSUE A. CONTAINING ALL IN EA 6-5314-82934, APPROVED BY RAS/AS/0153/2005 ISSUE A.SDR 07FDEA04290Skin Panel · corrodedFOUND HEAVY CORROSION ON SKIN PANEL BETWEEN FRAME 39-40, STGR 28-33 LT AND TWO OVALIZED HOLES ON FITTING (SEE DRW. A535-10563) AT FRAME 39, STGR 28. REPAIR PERFORMED BY BLEND OUT CORROSION IAW TD 942.038560/011/2005 ISSUE A AND TD 942.038560/047/2005 ISSUE A SDR 07FDEA04281Skin · dentedFOUND DENT ON NOSE SKIN OF RT KRUEGER FLAP (70MMX50MM, DEEPNESS 2.7MM). REPAIR PERFORMED BY DRESSING OUT THE PANEL, HFEC-ROTOTEST INSPECTION AND OVERSIZING RIVETS IN DENTED AREA IAW EA 6-5745-92141 AND RAS/AS/0160/2005 ISSUE A.SDR 07FDEA04280Retainer · corrodedHEAVY CORROSION ON SEAL RETAINER ON STR 26 BETWEEN FRAME 74-75 LT, LOWER PAX DOOR. REPLACEMENT OF SEAL RETAINER IAW SRM 51-72-10.SDR 07FDEA04279Angle · damagedDAMAGED ANGLE SHEET BETWEEN FRAME 62-63, STGR 28 RT, CARGO DOOR AREA. REPLACEMENT OF ANGLE SHEET IAW SRM 51-72-10.
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