N658FE
Service difficulty reports · 352
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 = 'N658FE' 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 = 'N658FE' 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 FDEA201004061069Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 NG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 NG IAW DWG SRZ 25-005, REV "H".SDR FDEA201004061068Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 HG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 HG IAW DWG SRZ 25-005, REV "H".SDR FDEA201004061066Floor Panel · damagedMAIN CABIN FLOOR PANEL 251 VH IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 VH IAW DWG SRZ 25-005, REV "H".SDR FDEA201004061065Floor Panel · damagedMAIN CABIN FLOOR PANEL 252 PH IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 PH IAW DWG SRZ 25-005, REV "H".SDR FDEA201004061064Floor Panel · damagedMAIN CABIN FLOOR PANEL 242 RJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 242 RJ IAW DWG SRZ 25-005, REV "H".SDR FDEA201004061063Floor Panel · damagedMAIN CABIN FLOOR PANEL 251 BH IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 BH IAW DWG SRZ 25-005, REV "H".SDR FDEA201004061062Floor Panel · delaminatedAFT CARGO COMPARTMENT FLOOR PANEL RT SIDE BETWEEN FRAME 59 AMD FRAME 60 IS VERY SOFT AND DELAMINATED.SDR FDEA201004051056Seat Track · corrodedSEAT TRACK CORRODED ON THE FLANGE FROM FRAME 50 TO FRAME 51; RBL 26. REMOVED CORROSION IAW SRM 53-10-16, PG 101. MATERIAL LOSS 0.010. MATERIAL REMAINING 0.080 FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16. ALODINED AND PRIMED IAW SRM 51-21-10. CORROSION ISDR FDEA201004051055Seat Track · corrodedSEAT TRACK FLANGE HAS SOME FLAKED PAINT AND CORROSION AT FRAME 51; RBL 16. CLEANED AREA TO EVALUATE IAW AMM 51-23-10-00. NO CORROSION FOUND.SDR FDEA201004051054Seat Track · corrodedCORROSION ON SEAT TRACK FWD END AT FRAME 14; RBL 16.SDR FDEA201004051053Support Bracket · crackedAFT MAIN CABIN SUPPORT BRACKET IS CRACKED AT STRINGER 25 LT; FRAME 79 TO FRAME 80. REMOVED CRACKED SUPPORT BRACKET IAW SRM 51-72-10. LOCATED AND DRILLED HOLES IN NEW BRACKET PN A539111320051, PO 631621.2 IAW SRM 51-72-10. INSTALLED SUPPORT BRACKET IAW SRMSDR FDEA201004021048Panel · dentedAFT CARGO COMPARTMENT; RT SIDE AFT TRANSITION PANEL AT FRAME 59 IS DAMAGED AND DENTED. REMOVED TRANSITIONAL PANEL IAW A300-600 SRM 51-40-21, PARA 5. MATERIAL ID 2024-T3, 0.063, PO 674650 IAW A300-600 SRM 53-16-10, FIG 5; SRM 51-31-00, PG 23 AND AIRBUS DWG ASDR FDEA201003301029Support Bracket · crackedFWD CARGO COMPARTMENT AFT BAY HAS A CRACKED SUPPORT BRACKET AT FRAME 38.2, LT SIDE ON AFT SIDE OF THE BULKHEAD WALL UPPER MOUNT TRIM, 36 IN. TO THE LT OF THE CTR POST. REMOVED CRACKED BRACKET IAW A300-600 SRM 51-72-10, PARA A, PG 2. FABRICATED NEW BRACKET IASDR FDEA201003301028Support Bracket · crackedFWD CARGO COMPARTMENT AFT BAY HAS A CRACKED SUPPORT BRACKET AT FRAME 38.2, LT SIDE ON AFT SIDE OF THE BULKHEAD WALL UPPER MOUNT TRIM. REMOVED CRACKED BRACKET IAW SRM 51-72-10, PARA A, PG 2. FABRICATED NEW BRACKET IAW DWG A25370669. ALODINED BRACKET IAW SRSDR FDEA201003301027Support Bracket · crackedFWD CARGO COMPARTMENT HAS A CRACKED SUPPORT BRACKET AT FRAME 38.2, RT SIDE AND AFT SIDE OF THE BULKHEAD WALL UPPER MOUNT TRIM. REMOVED CRACKED BRACKET IAW SRM 51-72-10, PARA A, PG 2. FABRICATED NEW BRACKET IAW DWG A25370669. ALODINED BRACKET IAW SRM 51-21-1SDR FDEA201003261015Skin · crackedCRACK IN THE RT WING LOWER SKIN INBD OF RIB 9 (FASTENER THROUGH JOGGLE SECTION) SHOWN ON FIG 3. (VERIFIED WITH EDDY CURRENT) COMPLIED WITH EA 6-5710-139432 "WINGS - AD 2008-06-17- RT WING LWR SKIN PANEL INBD OF RIB 9".SDR FDEA200912104396Landing Gear · malfunctionedON INITIAL T/O LANDING GEAR WOULD NOT RETRACT. SWITCHED TO SYS 2 AND GEAR WOULD NOT RETRACT ON SYS 2 EITHER. NOTICED THAT AUTO THROTTLES WOULD NOT FLY SELECTED A/S WITH ATS LEVER AND A/THR SW ENGAGED. PROFILE WOULD NOT FLY COMMANDS ON TMA'S. ON LANDING SDR 08FDEA04428Controller · failedPASSING FL 240, BOTH PACKS FAULTED, C/W ECAM PROCEDURE. PACK WOULD NOT RESET, DESCENDED TO 10,000 FOR REMAINDER OF FLIGHT. PASSING 14,000 ON WAY BACK DOWN PACK FAULTS MAGICALLY WENT AWAY AND CABIN BEGIN TO STABILIZE PERFORMED SUCCESSFUL BITE TEST OF NR 1 ASDR 08FDEA01849Crossbeam · crackedCROSSBEAM FR 60 HAS 1 INCH CRACK ON VERTICAL FLANGE OUTBD OF SEAT TRACK 3 RT, - Y1456 REMOVED CRACK AND INSTALLED CROSSBEAM REPAIR IAW A300-600 SRM 53-10-15, FIG 211.SDR FDEA200804151418Floorbeam · crackedFLOORBEAM AT FR 60 HAS 1 IN CRACK ON VERTICLE FLANGE, OTBD OF SEAT TRACK 3 RT, - Y1456, ON AFT FACE, REMOVED CRACK AND ACCOMPLISHED FLOORBEAM REPAIR IAW SRM 53-10-15, FIG 211.SDR FDEA200804151417Crossbeam · crackedCROSSBEAM AT FR 60 HAS 1 IN CRACK ON VERTICLE FLANGE, OTBD OF SEAT TRACK 3 RT, - Y1456, ON AFT FACE REMOVED CRACK AND ACCOMPLISHED FLOORBEAM REPAIR IAW SRM 53-10-15, FIG 211.SDR 08FDEA01418Floorbeam · crackedCROSSBEAM AT FR 60 HAS 1 IN CRACK ON VERTICAL FLANGE, O/B OF SEAT TRACK 3 RT, - Y1456, ON AFT FACE REMOVED CRACK AND ACCOMPLISHED FLOORBEAM REPAIR IAW A300-600 SRM 53-10-15, FIG 211.SDR 08FDEA01417Floorbeam · crackedCROSSBEAM AT FR 60 HAS 1 IN CRACK ON VERTICAL FLANGE, O/B OF SEAT TRACK 3 RT, - Y1456. ON AFT FACE REMOVED CRACK AND ACCOMPLISHED FLOORBEAM REPAIR IAW A300-600 SRM 53-10-15, FIG 211.SDR 08FDEA01161Seat Track · corrodedMCDD FLOOR SEAT TRACK NR 3 RT INBD FLANGE HAS CORROSION 4 AREAS BETWEEN FR 40 AND FR 42 REMOVED LEVEL 1 CORROSION BY REMOVED AND REPLACED SEAT TRACK SECTION FROM FR 40 TO FRAME 46, NR 3 RT.SDR 08FDEA01160Floorbeam · crackedFWD CARGO COMPT LEFT SIDE MAIN DECK FLOORBEAM FR 31 HAS 1 INCH CRACK, BETWEEN TRACKS NR 4 AND NR 5. REPAIRED MAIN DECK CRACKED FLOORBEAM AT FRAME 31 BETWEEN TRACK NR 4 AND TRACK NR 5 IAW A300-600 SRM 53-10-15, FIG 212.SDR 08FDEA01159Seat Track · gougedMDCC SEAT TRACK NR 1 HAS 1 EA GOUGED SCALLOP BETWEEN FRAMES 48 AND 49 ACCOMPLISHED SEAT TRACK REPAIR IAW A300-600 SRM 53-10-16,FIG 201SDR 05FDEA04220Line · chafedABOUT 5 MIN PRIOR TO DESCENT FOR KMEM ARRIVAL HAD ECAM GREEN HYD SYSTEM LOW LEVEL LGT WITH QTY ON OVERHEAD AND ECAM SHOWING AT RED DOT/LOW. RAN ALL CHECKLISTS, DECLARED EMERGENCY, CRANKED GEAR & STOPPED ON CENTER OF RWY AT END OF RWY 36C TOW-IN NO FURTHER PSDR 04FDEA00095Proximity Sensor · malfunctionedAFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT PAST INTERLOCK; SWITCHED TO SYSTEM NR 2, SAME PROBLEM. ENT BY: 502223 RPT BY: 123564 FACT 11JAN04 PERFORMED LANDING GEAR SAFETY RELAY CONTROL SIMULATOR TEST SET ON LANDING GEAR SWITCH UNIT (2GA) PER M/M 32-00-00SDR 03FDEA00998Fitting · damagedMDIS 658 53-10 0006643 25JUN03 BFM CLOSE R FABRICATE NEW FITTING PER EA NR 6-5310-70963 AND INSTALL AFTER FABRICATION. 29JUN03 01:33 BFM R COMPLIED WITH FUSELAGE-MAINFRAME-MATERIAL SUB FOR FITTING P/N A538-12906-200 EA NR 6-5310-70963 AND FED-EX SDR 03FDEA00994Crossbeam · damagedMDIS 658 53-10 0006641 24JUN03 BFM CLOSE R COMPLY WITH E.A. 6-5310-70959 FUSELAGE-MAINFRAME-REWORK OF MAIN DECK CROSSBEAM DAMAGE. FACT 28JUN03 14:23 BFM U COMPLIED WITH EA6-5310-70959 FUSELAGE-MAINFRAME- REWORK OF MAIN DECK CROSSBEAM DAMAGE.SDR 03FDEA00987Angle · damagedCOMPLY WITH E.A NR 6-7832-70958 EXHAUST-TR ASSY-REPAIR OF FORMED ZEE ON CORE COWL, INNER SURFACE. FACT 27JUN03 12:16 BFM R WORK COMPLIED ON EA 6-7832-70958 EXHAUST-TR ASSY REPAIR OF FORMED ZEE ON CORE COWL INNER SURFACE.SDR 03FDEA00988Thrust Reverser · damagedTHRUST REVERSER ASSY-REPAIR OF FORMED ZEE ON CORE NACELLE INNER SURFACE. FACT 27JUN03 12:16 BFM R WORK COMPLIED ON EA NR 6-7832-70958_EXHAUST-TR ASSY-REPAIR OF FORMED ZEE ON CORE, COWL INNER SURFACE.SDR 03FDEA00989Flange · gougedREPAIR OF SLIGHT GOUGES ON FR 28, INNER FLANGE. FACT 27JUN03 06:44 BFMR WORK COMPLIED WITH ON E.A. 6-5310-70955 FUSELAGE-MAINFRAME REPAIR OF SLIGHT GOUGES ON FR 28, INNER FLANGE.SDR 03FDEA00991Panel · crackedNR 1 ENGINE PYLON PRE-COOLER PANEL, CRACK REPAIR. FACT 27JUN03 03:15 BFM R COMPLIED WITH E.A. 6-5452-70948 NACELLES/PYLONS. NR 1 ENGINE PYLON PRE-COOLER PANEL PANEL CRACK REPAIR.SDR 03FDEA00956Channel · gougedMDIS 658 57-10 0006637 21JUN03 BFM CLOSE R COMPLY WITH E.A. 6-5752-70956 WINGS-BASIC-REPAIR OF FLAP TRAILING EDGE (Z CHANNEL) FACT 23JUN03 17:40 BFM R COMPLIED WITH EA NR 6-5752-70956 WINGS-BASIC-REPAIR OF FLAP TRAILING EDGE (Z-CHANNEL) IAW/SRM 51SDR 03FDEA00957Retainer · crackedNR 768 APU COMPT DOOR SILL SEAL RETAINERS ARE CRACKED. REMOVED AND REPLACED 4 EA RETAINERS IAW A300-600 SRM 51-40-00.SDR 03FDEA00958Floor Support · crackedNR 378 MCD FLOORBOARD SUPPORT FRAME 46 CRACKED RBL 35. REMOVED AND REPLACED SUPPORT FRAME IAW SRM 51-40-21.SDR 03FDEA00959Panel · crackedNR 593 NE 2 PYLON PRECOOLER PANEL 423 BL CRACKED LT AND RT FWD CORNERS OF SEAL BACKUP PLATE. REMOVED AND REPLACED CRACKED WEB IAW SRM 51-40-21.SDR 03FDEA00911Door Frame · damagedMAINFRAME- FUSELAGE FRAME DENT REPAIR AT FR20A. FACT 19JUN03 11:40 BFM R WORK COMPLIED WITH EA 6-5310-70932 A/C ARRIVED AT MAE WITH AN INCOMING TRACKING ACTION (REF FEDEX EA 6-5310-50593). THE AFFECTED MEMBER IS SHOWN AS ITEM 10 OF AIRBUS A300-600 SRM REFSDR 03FDEA00890Clip · brokenLEFT WING PANEL 572CB END CLIP IS BROKEN. REMOVED AND REPLACED CLIPS IAW SRM 51-40-21 ON N00596.SDR 09FDEA00895Bracket · brokenNR 2 PYLON PANEL 425 AL TETHER ANCHOR BROKEN. REMOVED AND REPLACED ANCHOR IAW SRM 51-40-21.SDR 03FDEA00894Bracket · chafedN 120 NR 1 ENG THRUST REVERSER LOWER AFT CLOSE OUT PANNEL LEADING EDGE, CHAFED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-21 PG 7 @ MAE.SDR 03FDEA00889Clip · brokenLT WING PANEL 572LB END CLIP IS BROKEN. REMOVED AND REPLACED CLIP IAW SRM 51-40-21 ON N00595 AT MAE.SDR 03FDEA00888Attach Angle · crackedFWD AVIONICS FLIGHT COMPT RT INBOARD OVERHEAD FLOOR SPT ATTACH ANGLE CRACKED AT STA 972. FR10 AS SEEN FROM ACCESS DOOR. REMOVED AND REPLACED ANGLE IAW SRM 51-40-21 ON N00283.SDR 03FDEA00891Blowout Door · damagedEXHAUST- THRUST REV - BLOWOUT DOOR SKIN REPAIR. FACT 16JUN03 05:39 BFM R COMPLIED WITH EA 6-7832-70933 PT1 EXHAUST- THRUST REV - BLOWOUT DOOR SKIN REPAIR AT BFM/MAE.SDR 03FDEA00892Bracket · brokenFWD CARGO ANT CABLE ATTACH BRACKET IS BROKEN AT FR 22 LBL 24 STR 45L. REMOVED AND REPLACED BRACKET IAW SRM 51-40-21 401.SDR 03FDEA00893Support · bentFWD CARGO ANT CABLE SUPPORTS ARE BENT AT FR 25 STR 45L. REMOVED AND REPLACED CABLE SUPPORTS IAW SRM 51-40-21.SDR 03FDEA00896Angle · chafedNR 1 ENG OUTBOARD T/R LWR FWD CLOSE OUT PANEL AFT ANGLE CHAFED. REMOVED AND REPLACED ANGLE IAW SRM 51-40-21 PG 7.SDR 98FDEA00489Module · inoperative98-193 - GEAR WOULD NOT RETRACT. STOPPED MID POSITION. TRIED BOTH SYSTEMS. REMOVED AND REPLACED LANDING GEAR HANDLE CONTROL MODULE PER M/M 32-31-11-4 RETRACTION CHECK OK. R11 012823SDR 98FDEA00403Gcu · inoperativeNR 2 GENERATOR INOPERATIVE AFTER ENGINE START, ONE RESET. REMOVED AND REPLACED NR 2 GENERATOR CONTROL UNIT. APU GENERATOR REQUIRED FOR T/O. LOST APU GENERATOR AFTER TAKEOFF. DEFERRED APU GENERATOR PER MEL 24-8.
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