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 FDEA201707101892Power Supply · inoperativeR1 DOOR ECAM INDICATES SLIDE NOT ARMED. ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT 70WN. OPS AND BITE CHECKED GOOD.SDR FDEA201707061884Power Supply · inoperativeL1 AND R1 ESCAPE SLIDE RELEASE WARNING SYS LIGHTS INOPERATIVE. TROUBLESHOT IAW WDM 52-73-00, REMOVED CONTROL PANEL, AUTONOMOUS STBY POWER SUPPLY UNIT, CHECKED FOR 28 VDC AT PIN N. 28 VDC PRESENT. CLEANED THE CONTROL PANEL , CONNECTED & DOOR ECAM SLIDSDR FDEA201707031854Power Supply · failedR1 DOOR SLIDE INDICATION ON ECAM INOPERATIVE. REMOVED AND REPLACED AUTONOMOUS STANDBY POWER SUPPLY UNIT 70WN. OPS AND BITE CHECKED GOOD IAW AMM 52-73-18-04.SDR FDEA201706241754Smoke Detector · false activationAVIONICS SMOKE WARNING DURING PREFLIGHT. INSPECTED AVIONICS COMPARTMENT WITH NO EVIDENCE OF SMOKE FOUND. PERFORMED AVIONICS COMPARTMENT SMOKE ADJUSTMENT & TEST IAW AMM 26-15-00-05. TESTED GOOD. ACFT OK FOR SERVICE.SDR FDEA201705231487Floor Panel · brokenMDCC FLOOR PANEL 242MF BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231483Floor Panel · brokenMDCC FLOOR PANEL 242GK BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231477Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 252YH BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231476Floor Panel · brokenMAIN CARGO FLOOR PANEL 242LK BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.SDR FDEA201705231486Floor Panel · brokenMDCC FLOOR PANEL 242BF BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231485Floor Panel · brokenMDCC FLOOR PANEL 242TH BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231484Floor Panel · brokenMDCC FLOOR PANEL 241RJ BROKEN. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231482Floor Panel · brokenMDCC FLOOR PANEL 242RG BROKEN. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231481Floor Panel · damagedMDCC FLOOR PANEL 241AK BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231480Floor Panel · damagedMDCC FLOOR PANEL 262VF BROKEN. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231479Floor Panel · damagedMDCC FLOOR PANEL 251ZF BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201705231478Floor Panel · brokenMDCC FLOOR PANEL 241XG BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005, REV M. MAJOR REPAIR.SDR FDEA201610193657Detector · failedSHORTLY AFTER TAKEOFF AT APPROXIMATELY 1500 FT, CAPTAIN`S PITOT OVERHEAT, STBY PITOT OVERHEAT, FIRST OFFICER PITOT OVERHEAT AND CAPTAIN`S TAT HEAT FAULT. R & R THE PROXIMITY DETECTOR PROCESSING UNIT IAW MM 32-31-71-04. ALL TESTS PERFORMED AND FOUND OK.SDR FDEA201608032784Handle · damagedDURING CLIMB OUT PASSING FL 270, RECEIVED A ECAM ALERT FOR FWD CARGO DOOR UNLOCKED, WITH CORRESPONDING INCREASING CABIN ALTITUDE. COMPLIED WITH QRH, DURING DESCENT TO MINIMUM VECTOR ALTITUDE AT 17000FT, ECAM ALERT WENT OUT FLICKERED ON AND OFF THREE OR MORSDR FDEA201511023446Diaphragm · damagedDURING L1 SLIDE INSTALLATION, ACTUATOR DIAPHRAGM DAMAGED, NO PART IN STOCK. RELEASED FOR SERVICE IAW MEL 52-11-01-02, CATEGORY C, EXPIRATION 10 NOV 15. L1 CREW ENTRY DOOR INOPERATIVE. IF SLIDE TO BE RETAINED ONBOARD THEN PRIOR TO EACH DEPARTURE, MX MUST VESDR FDEA201510153236Radome · damagedON DEPARTURE, SUSPECT LIGHTNING STRIKE, WX RADAR INOPERATIVE, NO OTHER ISSUES. FOUND PUNCTURE ON THE NOSE OF THE RADOME & RADOME DELAMINATED FROM THE INSIDE. FOUND ANTENNA HIT BY LIGHTNING STRIKE, CREW VERBALLY REPORTS THAT BOTH WEATHER RADAR SYSTEMS ARE INSDR FDEA201502020412Pressure Switch · leakingFLIGHT ALT 330 GREEN HYD SYS DROP & INDICATED LOW PRESS BELOW RED DOT. PROCEDURES IAW ECAM, ATB & MANUALLY PUT THE GEAR DOWN. WITH GEAR DOWN & LOCKED GREEN SYS RETURNED TO NORMAL. FOUND HYD GREEN SYS LEAK AT PRESS SWITCH 30WW. R & R HYD PRESS SWITCH IAW ASDR FDEA201411203825Frame · crackedNDT FOUND LT FUSELAGE FRAME SPLICE 47 AROUND HOLE H IS CRACKED BETWEEN STRINGERS 24 & 26L. REAMED THE HOLE TO REMOVE THE CRACK AND COMPLIED WITH EA 6-5310-T0313717 PT1.SDR FDEA201411203824Frame · crackedNDT FOUND RT FUSELAGE FRAME SPLICE 47 BETWEEN STRINGER 24 & 26RT AROUND HOLE M CRACKED. REAMED THE HOLE TO REMOVE THE CRACK AND COMPLIED WITH EA:6-5310-T0313717 PT1.SDR FDEA201411183742Angle · crackedRIGHT FUSELAGE AT FRAME 40 PICKUP ANGLE INSTALLATION HOLE NR 49 NDT INSPECTION FOUND CRACK. REAMED THE HOLE TO REMOVE THE CRACK AND COMPLIED WITH EA:6-5310-T0313679 A PT1. TITLE:FUSELAGE-FRAME-AD 2000-07-22-DEVIATIONS TO MODIFICATION OF THE FWD PICK UP ANGLE SDR FDEA201411183740Skin · crackedLEFT FUSELAGE AT FRAME 40 PICKUP ANGLE INSTALLATION HOLE NR 36 NDT INSPECTION FOUND CRACK. REAMED THE HOLE TO REMOVE THE CRACK AND COMPLIED WITH FEDEX EA:6-5310-T0313679 A PT1. TITLE:FUSELAGE-FRAME-AD 2000-07-22-DEVIATIONS TO MODIFICATION OF THE FWD PICK UPSDR FDEA201411083585Frame · crackedCENTER WING JOINT AT FRAME 40 FOUND RT SIDE CRACKED. REPAIRED IAW EA:6-5710-T0313413 PT1.SDR FDEA201411083584Frame · crackedCENTER WING JOINT AT FRAME 40 FOUND LT SIDE CRACKED. REPAIRED IAW EA:6-5710-T0313413 PT1.SDR FDEA201411083583Frame · crackedCENTER WING JOINT AT FRAME 40 FOUND LT SIDE CRACKED. REPAIRED IAW EA 6-5710-T0313413 PT1.SDR FDEA201411083582Fitting · crackedCENTER WING JOINT AT FRAME 40 FOUND LT SIDE CRACKED. REPAIRED IAW EA 6-5710-T0313413 PT1.SDR FDEA201411083581Floorbeam · corrodedAFT CARGO FLOORBEAM CORRODED AT FRAME 63 BETWEEN -Y805 & Y1470. REPLACED THE FLOORBEAM IAW AMM 25-52-21-04-01. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201408082120Warning System · activatedAFTER NR 1 AUTO PRESS DISPLAYED A DELTA P PRESS OF 8.6, SWITCH TO AUTO PRESS NR 2 TO REMEDY. NR 2 AUTO PRESS LOWERED DELTA P PRESS TO 8.5 BUT REMAINED FLASHING. CRUISE ALT WAS FL 380. CABIN ALT DISPLAYED 7300. PERFORMED PRESSURIZATION PER MM 05-53-00-00. SDR FDEA201407151812Unknown · malfunctionedMAIN GEAR DOORS DID NOT RETRACT ON TAKEOFF. GEAR RETRACTED AT 230KTS. DOOR LIGHTS WENT OUT ON EXTENSION. INSPECTED MAIN GEAR & DOORS FOR EVIDENCE OF OVERSPEED RETRACTION IAW AMM 05-51-12-00 NO ANOMALIES NOTED AT THIS TIME. RELEASED FOR SERVICE IAW MEL 32SDR FDEA201311032673Connector · corrodedAFTER T/O PASSING 6000' PITOT HEAT STDBY SYSTEM FAILED. PITCH TRIM NR 2 TRIPPED OFF, ATS LEVER 1, TRIPPED OFF, NR 2 FLIGHT DIRECTOR FAILED; MAINTENANCE; CL; & CR LIGHTS ON TRIP STARTED FLASHING. MTP FAULT REPORTED NOSE GEAR RELAY - FAC NR 2, NOSE GEAR RELAY-SDR FDEA201309032110Outflow Valve · malfunctionedAFTER DEPARTURE, RECEIVED CABIN PRESSURE REGULATOR 2 FAULT ALERT. USED MANUAL PRESSURE CONTROLLER. ON THE GROUND, EXCESSIVE CABIN ALTITUDE WARNING ILLUMINATES ON ECAM. THE WARNING QUICKLY EXTINGUISHES AND CABIN PRESSURE REGULATOR 1 FAULT IS ILLUMINATED. RSDR FDEA201305241083Ram Air Turb · malfunctionedDURING FUNCTION OF RAM AIR TURBINE, ROUTINE CARD 00073 WRI 29206710, STEP 1 STATES TO LOWER THE RAT. THE RELEASE HANDLES WERE ACTIONED NUMEROUS TIMES WITH NO EFFECT, AMM REVIEWED, PROCEDURE 29-22-00-06 IS "IF RAT FAILS TO EXTEND" THIS TASK WAS CARRIED OUT ASDR FDEA201210173637Fitting · crackedWHEN PERFORM EO:6-5710-7-3305 D3 PT2, CRACK SIGNAL WAS FOUND IN HOLE "V" OF FR 47 REAR & BOTTOM PANEL AT JUNCTION WITH FUSELAGE. REPAIRED PER EA 6-5710-163141.SDR FDEA201210173636Fitting · crackedPERFORMED EO:6-5710-7-3305 D3 PT1, ELLIPSE HOLE WAS FOUND IN HOLE "X" AND CRACK SIGNAL WAS FOUND IN HOLE "V" & HOLE "Y" OF FR47 REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE REPAIR THE HOLES PER EA 6-5710-163141SDR FDEA201210163627Attach Fitting · crackedFOUND A CRACK ABOUT 20MM LENGTH IN THE AFT CARGO DOOR ACTUATOR ATTACHED FITTING. REMOVED THE AFT CARGO DOOR ACTUATOR ATTACHED FITTING IAW SRM 51-40-21. INSTALLED THE NEW PART IAW SRM 51-40-21 & RESTORE FINISH IAW SRM 51-75-10. REPLACED THE BUSHING IAW PMSDR FDEA201008132990Skin · misrepairedPREVIOUS REPAIR LOCATED AT FR63A AND STG R40 RT NOT CONFORM WITH AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IAW SRM 53-17-13, FIG 202, REV 74.SDR FDEA201008102903Rib · crackedFLAP INBD RT WING - RIB 25A FOUND CRACKED. REPLACED IAW EA 6-5750-141552.SDR FDEA201008102905Rib · crackedINBD FLAP LT WING - RIB 25A FOUND CRACKED. REPLACED AS PER EA 6-5750-141552 AND SB A300-57-6098.SDR FDEA201008062862Crossmember · corrodedFWD DOOR NR1 RT - CROSSMEMBER NR 6 WITH CORROSION. REPAIRED IN ACCORDANCE WITH EA 6-5210-141554.SDR FDEA201008062861Seat Track · wornTRACK, WEAR AT FR33 AND Y450. REPAIRED AS PER EA 6-5320-141555.SDR FDEA201008062856Sill · crackedAFT COMPARTMENT - SILL BEAM AT AFT COMPARTMENT DOOR WITH CRACK BTW FR60/61. SILL-BEAM WAS REPAIRED AS PER EA 6-5310-141556.SDR FDEA201008062860Crossbeam · corrodedFWD MDCC - CROSS BEAM AT FR16A - CORROSION SPOTS FOUND AT Y-2004. CROSSBEAM REPLACED AS PER SRM 51-72-10.SDR FDEA201008062859Floor Support · corrodedFLOOR SUPPORT - SPOTS OF CORROSION FOUND BETWEEN FR11/13 AT Y953. FLOOR SUPPORT WAS REPLACED BY A NEW ONE AS PER SRM 51-72-10.SDR FDEA201008062858Seat Track · corrodedFWD MDCC - SEAT TRACK - SPOTS OF CORROSION FOUND BTW FR17/15A AT Y450. SEAT TRACK REPLACED AS PER SRM 51-72-10.SDR FDEA201008062857Seat Track · corrodedFWD MDCC - SEAT TRACK - SPOTS OF CORROSION FOUND BTW FR14/17 AT Y-450. SEAT TRACK REPLACED AS PER SRM 51-72-10.SDR FDEA201007283145Skin · dentedFUSELAGE - DEFORMITY (DENT) BETWEEN FR14A AND 15 BTW STGR 27-30LT. DENT WAS REPAIRED AND FOUND ACCEPTABLE IAW EA 6-5330-141557.SDR FDEA201007232802Skin · damagedRT WING - AILERON T/E LOWER SURFACE BTW RIB13-RIB16 WITH EXISTING REPAIR FILLER. EXISTING REPAIR FILLER WAS REMOVED AND NEW REPAIR HAS BEEN PERFORMED IAW SRM 57-61-11, PB 201 & 51-77-12, FIG 222.
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