N740FD
Service difficulty reports · 156
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 = 'N740FD' 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 = 'N740FD' 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 FDEA201603120908Web · crackedMDCC FRAME 47, Y0~ -Y450, FLOOR WEB CRACKED, APPROX 1.0 INCH IN LENGTH. FABRICATE THE NEW WEB IAW DWG A53832100. INSTALL NEW WEB IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201603100883Support Beam · corrodedAFT CARGO FRAME 65 - RT LONGITUDINAL BEAM, FLOOR STRUCTURE, CORRODED. REPLACED THE LONGITUDINAL BEAM IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201603100881Frame · damagedDURING PERFORM WC 6-5310-7-5017 E PT 3, AFTER REMOVED THE BOLT FOUND HOLE H DAMAGED PREVIOUSLY. COMPLIED WITH EA 6-5310-T0324002 P 1. MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA201603070858Floor Support · corrodedMDCC FRAME 11 - 14, Y953, FLOOR SUPPORT CORRODED AROUND BOLT HOLES. REPLACED THE CORRODED FLOOR SUPPORT IAW SRM 51-40-21. THIS IS A MAJOR REPAIR.SDR FDEA201603070856Rib · crackedRIGHT WING INBD FLAP INTERNAL RIB, FOUND CRACK AT RIB 25A, BETWEEN STRINGER 2.2 - 2.4. COMPLIED WITH EA 6-5750-T0323968 P1. REPLACED THE RT WING INBD FLAP INTERNAL RIB AT RIB 25A, BETWEEN STRINGER 2.2 - 2.4.SDR FDEA201603020759Frame · crackedMAIN DECK AREA, FUSELAGE FRAME 47 WITH HOLE L CRACKED, AT STRINGER 25R - 26R.SDR FDEA201511183729Flap · damagedON DIRTY UP FOR APPROACH, KRUEGER FLAP FAILED TO EXTEND. REPLACED DAMAGED LT KRUEGER FLAP INBD CARRIER & SUPPORT WITH KRUEGER FLAP POSITION SWITCHES IAW MM 27-87-14-04. AWAITING INSTALLATION OF KRUEGER FLAP FOR OPERATIONS CHECKS. INSTALLED LT KRUEGER FLAP SDR FDEA201510253334Slat · faultedSLATS SYSTEM 1 & 2 FAULTED ON APPROACH AT 240 KTS. CYCLED HANDLE TO SLATS UP & SLOWED TO 220 KTS. ATTEMPTED SECOND EXTENSION WITH SAME RESULT. FOLLOWED QRH & ECAM, LANDED SLATS 0 FLAPS 40. FOUND LT TORQUE LIMITER TRIPPED, PERFORMED INSPECTION & CHECK OF LTSDR FDEA201510103160Slat System · malfunctionedSLAT SYSTEMS 1 & 2 FAULTED DURING EXTENSION. SPF I SLAT LIGHT WAS NOT ILLUMINATED. CYCLING SLATS, DID NOT CORRECT THE STUCK SLATS. BITE CHECKED SFCC'S, FOUND SLAT JAM FAULT ON BOTH. RESET SFCC'S, OPERATED SLATS NO HELP FAULTS ON SFCC'S RETURNED. SWAPPED SDR FDEA201507172255Landing Gear · malfunctionedPUT GEAR HANDLE DOWN, NO RESPONSE, RED UNLOCK LIGHTS ON POS 1 & 2 BACK TO NEUTRAL, THEN UP, THEN NEUTRAL, THEN DOWN, NORMAL OPERATIONS. MTP IS FAULTING RT MAIN GEAR RELAY FAIL. R & R LANDING GEAR ELECTRO VALVE 3GA IAW AMM 32-31-12-04, OPS CHECKED GOOD IAW SDR FDEA201506091752Door · defectiveR1 DOOR WILL NOT DISARM. DISARM LEVER WILL NOT GO FULL TO DISARM SIDE. IT STOPS ABOUT 2 INCHES BEFORE FULL DISARM TRAVEL. DOOR LOCKING INDICATOR WINDOWS STILL INDICATE DOOR LOCKED. R1 CREW ENTRY DOOR INOPERATIVE. IF SLIDE TO BE RETAINED ONBOARD THEN PRIOSDR FDEA201506091751Girt Bar · bentR1 DOOR WILL NOT DISARM. DISARM LEVER WILL NOT GO FULL TO DISARM SIDE. IT STOPS ABOUT 2 INCHES BEFORE FULL DISARM TRAVEL. DOOR LOCKING INDICATOR WINDOWS STILL INDICATE DOOR LOCKED. FOUND THE R1 DOOR SLIDE GIRT BAR BENT AT THE FWD TAB THAT HOLDS THE SLIDER NSDR FDEA201408092137Rib · corrodedRIGHT RIB 5 MLG FWD LUG HAS CORROSION IN BORE, FWD & AFT FACE. COMPLIED WITH EA 6-5710-T0310388 P1 WING BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.SDR FDEA201408092136Rib · corrodedLEFT RIB 5 MLG FWD LUG HAS CORROSION IN BORE & AFT FACE. COMPLIED WITH EA 6-5710-T0310388 P2 WINGS BASIC WING STRUCTURE LT & RT RIB 5 BORE CORROSION.SDR FDEA201406201499Generator · unknownDURING DEPARTURE, RECEIVED ECAM ALERT, AC BUSS 1 OFF, AC EMERGENCY ON INVERTER AC ESS BUSS OFF. COMPLIED WITH QRH, PERFORMED TROUBLESHOOTING IAW TSM. CHECKED GENERATOR WIRE HARNESS FOR CHAFING & CONNECTORS FOR SECURITY. CLOSED ENG COWLS, RAN ENG IAW JRH, SDR FDEA201406201495Circuit Breaker · failedDURING CRUISE, LOST AC BUSS NR 1 ESSENTIAL BUSS & AC EMERGENCY BUSS WAS ON INVERTER. LOST CAPTAIN`S ND, AUTOPILOT 1. FOLLOWED QRH, TURNED OVERHEAD SUPPLY NR 1 ON. REMOVED AND REPLACED CIRCUIT BREAKER 10 XH IAW SMP.SDR FDEA201110034272Structure · contaminatedSUSPECT WATER INDICATIONS ON RT ELEVATOR FOUND DURING THERMOGRAPHY INSPECTION. REPAIRED IAW SRM 55-21-12.SDR FDEA201109304229Rudder · damagedSUSPECT WATER INDICATIONS ON RUDDER FOUND DURING THERMOGRAPHY INSP REPAIR CARRIED OUT TO T/E SCREW NR 37 RT IAW EA 6-5540-154307, PART 1, SRM 55-41-12, MAJOR REPAIR ULTRASONIC INSP OF AREAS IN FIG 2 THRU 8 TO BE CARRIED OUT AT 6 YEAR INTERVALS IAW MRBR IAW ESDR FDEA201109304227Fitting · corrodedEVIDENCE OF LIGHT SURFACE CORROSION IN NR 1 PYLON RIB 18 BALL JOINT LUG BORE LT PYLON RIB 18 BALL JOINT LUG BORE OVERSIZED IAW SB A300-54-6018 SCHEME 1(ACCOMPLISHED ON EA 6-5451-154311).SDR FDEA201109304226Angle · damagedDURING EMBODIMENT OF RT FRAME 40 PICK UP ANGLE REPLACEMENT (REF EO 6-5310-7-5001 PT2) HOLE 47 FOUND TO HAVE DISCREPANCY RT FRAME 40 PICK UP ANGLE HOLE 47. REWORKED IAW EA 6-5300-154310.SDR FDEA201109304225Angle · damagedDURING EMBODIMENT OF LT FRAME 40 PICK UP ANGLE REPLACEMENT (REF EO 6-5310-7-5001 PT2) HOLES 47,19 AND 23 TO 30 FOUND TO HAVE DISCREPANCY LT FRAME 40 PICK UP ANGLE HOLES 47, 1 AND 23 TO 30 REWORKED IAW ATTACHED EA 6-5300-154309.SDR FDEA201109294203Plate · damagedAFT CARGO DOOR UPPER FUSELAGE CUT OUT SEALING PLATE BETWEEN FR 59A AND FR 63 FOUND BADLY DAMAGED AFT CARGO DOOR UPPER FUSE CUT OUT SEALING PLATE BETWEEN FR 59A AND FR 63. REPLACED IAW SRM 51-40-21.SDR FDEA201109284185Crossbeam · corrodedAFT CARGO CROSSBEAM AT FR63 FOUND CORRODED AFT CARGO CROSSBEAM AT FR 63. REPLACED IAW SRM 51-40-21 & DWG A53974554.SDR FDEA201109284184Crossbeam · corrodedAFT CARGO BAY CROSSBEAM AT FR62 FOUND CORRODED AFT CARGO CROSSBEAM AT FR 62 REPLACED IAW SRM 51-40-21, MAJOR REPAIR.SDR FDEA201109284174Floor Support · corrodedAFT CARGO FLOOR STRUCTURE FOUND CORROSION AT FR 63 BETWEEN S45-46R. REPAIRED IAW SRM 53-10-14 P 202, FIG 201C DEVIATION OF FASTENER INSTALLATION ACCOMPLISHED IAW EA 6-5310-150949, MAJOR REPAIR IAW SRI 53-10-14-2-002-00, P 207, TABLE 203.SDR FDEA201109264137Skin · corrodedLEFT WING UPPER SKIN CORRODED. REPAIR CARRIED IAW EA 6-5720-154320 PART 1.SDR FDEA201109264136Skin · corrodedRIGHT WING UPPER SURFACE SKIN CORRODED. REPAIR CARRIED OUT IAW EA 6-5720-154315,SDR FDEA201109264133Structure · crackedDURING NDT CRACK INDICATION, FOUND IN CENTER WING BOX. REPAIR CARRIED OUT IAW EA 6-5710-154305SDR FDEA201109264135Rib · crackedLT MLG RIB NR 5, HOLE 47 CRACK INDICATION IN SPOT FACE. REQUIREMENTS OF EA 6-5751-154313 CARRIED OUT TO LT MLG RIB 5 HOLE 47 TO REPAIR CRACK INDICATION.SDR FDEA201109264134Rib · crackedRT MLG RIB NR 5, HOLE 47 CRACK INDICATION IN SPOTFACE. REQUIREMENTS OF EA 6-5751-154314 CARRIED OUT TO RT MLG RIB 5, HOLE 47 TO REPAIR CRACK INDICATION.SDR FDEA201109203979Skin · dentedDENT AT RT FUSELAGE BETWEEN FR2-3, STR 22-25 RT. DENT TO BE REPAIRED IAW SRM 53-11-12. DENT REPAIRED IAW SRM 53-11-12, FIG 201.SDR FDEA201109173924Gusset · crackedLT MLG BAY GUSSET AT STR 40, FR 48 IS CRACKED GUSSET REPLACED IAW SRM 51-40-21, REF DWG A53812271.SDR FDEA201109153892Skin · crackedLT WING L/E PANEL 523JB LANDING ANGLE CRACKED JUST OB OF SLAT TRACK 6 FROM CAMLOCK FASTENER HOLE. REPAIR CARRIED OUT IAW SRM 57-41-12, MINOR REPAIR.SDR FDEA201109123843Skin · corrodedRIGHT WING UPPER SURFACE SKIN AT RIB 28 ADJACENT REAR SPAR AREA CORRODED. REMOVED CORROSION FROM AREA IAW SRM 51-73-10 AND CONFIRMED USING HFEC IAW NTM 51-10-02, WITHIN LIMITS IAW SRM 57-20-12, MINOR REPAIR.SDR FDEA201109093806Skin · corrodedCORROSION TO RT WING LOWER SKIN PANEL NR 2, LOWER SURFACE ADJACENT RIB 4. CORRODED AREA REWORKED, ASSESSED AND REPAIRED IAW EA 6-5720-154324. MAJOR REPAIR.SDR FDEA201109093805Skin · corrodedCORROSION TO LT WING LOWER SKIN PANEL NR2, LOWER SURFACE ADJACENT RIB 4. CORRODED AREA REWORKED, ASSESSED AND REPAIRED IAW EA 6-5720-154325. MAJOR REPAIR.SDR FDEA201109093804Seat Track · damagedSEAT TRACK AT Y450 FR 58 TO 72 FOUND DAMAGED. DAMAGED SECTION REPLACED IAW SRM 53-10-16 AND 51-40-21.SDR FDEA201109093803Seat Track · damagedSEAT TRACK Y1456 FR 61TO 67 FOUND DAMAGED AT UPPER SECTION. REPLACED IAW SRM 51-40-21.SDR FDEA201109093802Seat Track · damagedSEAT TRACK Y1959 BETWEEN FR 62 TO 66 FOUND DAMAGED. REPLACED IAW SRM 51-40-21SDR FDEA201109093800Floor Support · corrodedFLOOR SUPPORT ANGLE AT Y730 AND BETWEEN FR 11-14 FWD SECTION FOUND CORRODED FLOOR SUPPORT ANGLE AT Y730 AND BETWEEN 11 TO14 REPLACED IAW SRM51-40-20 AND DRG REF: A53612214.SDR FDEA201109093798Seat Track · damagedSEAT TRACK Y0 BETWEEN FR.58-72 FOUND DAMAGED AT ONE UPPER LOCATION BETWEEN FR 60-61. SEAT TRACK YO DAMAGED SECTION. REMOVED AND SPLICE REPAIR CARRIED OUT BETWEEN FR 58/59 AND FR 61/62 IAW SRM 53-10-16 AND SRM 51-40-21.SDR FDEA201109053706Sill · corrodedAFT CARGO BAY LWR DOOR SILL STRUCTURE AT FR 60 CORRODED. REPAIR CARRIED OUT IAW SRM 53-17-18 PARA7 FIG 204, MAJOR REPAIR.SDR FDEA201109053705Skin · damagedL1 DOOR SKIN CUTOUT, AFT SKIN EDGE HAS MINOR MECHNICAL DAMAGE. DAMAGE OUT OF SRM LIMITS. BLENDED DAMAGE. MAX DEPTH 0.004" X 0.5" LENGTH. INSP IAW NTM 51-10-08, NO DAMAGE. MINOR REPAIR.SDR FDEA201109053704Failsafe · chafedR1 DOOR SKIN CUTOUT FAIL SAFE RING UPPER FWD CORNER REWORK IS OUT OF SRM LIMITS. BLENDED, ASSESSED AND INSP IAW SRM 53-73-10, NTM 51-10-04, 51-10-08, 51-90-00, & 51-10-01. FASTENER REMOVED , INSPECTED AND 1ST OVERSIZE FASTENER REPLACED IAW EA 6-5300-15431SDR FDEA201109053703Skin · gougedSKIN GOUGED BETWEEN FR 63-64 LT. BLENDED, ASSESSED AND FOUND TO BE OUT OF LIMITS. REPAIR CARRIED OUT IAW SRM 53-10-12. FIG 225. MAJOR REPAIR, SECT 17. AREA REPROTECTED AND CLOSED UP.SDR FDEA201109013622Fitting · wornRUDDER LOWER SERVO CONTROL ACTUATOR ATTACHMENT LUG UPPER SURFACE HAS WEAR MARKS CAUSED BY THE ANTI ROTATION WASHER. FITTING REMOVED FROM RUDDER DUE TO WEAR OUT OF LIMITS. FITTING REPLACED IAW 51-72-10/51-40-21. DUE TO MISLIGNMENT OF FITTING, ITEM REPAIRED ISDR FDEA201109013612Skin · damagedLEFT FUSELAGE SKIN AT FR 13, LOCATION 14TH, FASTENER UP FROM STR 25 LOCATION HAS A SKIN MARK TO THE SIDE OF THE HOLE REWORK OUT OF SRM LIMITS. BLENDED AND ASSESSED IAW SRM 53-12-12. INSPECTED IAW NTM 51-10-01/51-40-00/51-35-05 NO DEFECTS. AREA BLENDED 1" SDR FDEA201005271687Probe · dirtyON T/O ROLL AT 80 KNTS CALL, F/O AIRSPEED INDICATED 50 KNTS. CAPTAINS AND STBY AIRSPEED INDICATED 80 KNTS. REJECTED TAKEOFF AT 90 KNTS. R & R F/O'S PITOT PROBE IAW MM 34-11-15-4. OPS CHECKED GOOD IAW MM 34-10-00-5 (FLIGHT ENVIRONMENT DATA TEST). F/O'S LEAK TESSDR FDEA200910303743Gcu · failedNR1 GEN FAULTED ON TAKEOFF. TRIED ONE RESET. NO HELP. PERFORMED BITE TEST OF GROUND PWR CONTROL UNIT IAW TSM 24-00-00 PAGE 102. GOT A FAULT CODE "SHORTED PMG". IAW TSM 24-00-00 PAGE 151, REPLACE GCU. ALL OPS CKS ON THE NR1 GEN WERE NORMAL OK FOR SERVICESDR FDEA200909093279Amplifier · failedREPEAT OF FALSE RT OUTER FUEL QUAN LO LEVEL ECAM WARNING. ALL OTHER INDICATIONS NORMAL. LAX U FUEL LEVEL AMPLIFIER HAS HARD FAULT "R FUEL LO" WHEN INSTALLED IN RACK. WHEN SERVICEABLE FUEL LEVEL AMPLIFIER INSTALLED, FAULT DOES NOT COME BACK. TEMP INSTALLED
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