N683FE

Service difficulty reports · 289

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 = 'N683FE' 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.

SDR FDEA200906112030Floor Panel · crackedMAIN CABIN FLOOR PANEL CRACKED. REMOVED CRACKED FLOOR PANEL IAW AMM 53-10-25-4; PG 2. FABRICATED NEW FLOOR PANEL AND PART MARKED IAW DWG SRZ 25-0056; REV "H". INSTALLED FLOOR PANEL IAW AMM 53-10-25-4; PG 3.Jun 11, 2009 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906112029Floor Panel · crackedMAIN CABIN FLOOR PANEL CRACKED. FABRICATED AND PART MARKED NEW FLOOR PANEL 242 GF; REMOVED DAMAGED FLOOR PANEL AND REPLACED NEW IAW SRZ 25-005; REV "H" AND AMM 53-10- 25-4.Jun 11, 2009 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906112024Floor Panel · crackedMAIN CABIN FLOOR PANEL CRACKED. FABRICATED FLOOR BOARD REF DWG SRZ 25-005; REV "H". REMOVED OLD FLOORBOARD AND INSTALLED NEW FLOORBOARD REF AMM 53-10-25-4.Jun 11, 2009 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906112023Floorboard · puncturedMAIN CABIN FLOORBOARD PUNCTURED 6 INCHES FWD OF LOCK L1466 IN POSITION 11L. FLOOR PANEL WAS REPLACED ON N/R N00258.Jun 11, 2009 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906112022Floorboard · deterioratedMAIN CABIN CARGO COMPARTMENT FLOORBOARD SF Z242 DETRIORATED/ PUNCTURED. FABRICATED NEW FLOOR PANEL REF DWG SRZ 25-005; REV "H". REMOVED DAMAGED FLOOR PANEL AND INSTALLED NEW FLOOR PANEL REF AMM 53-10-25-4.Jun 11, 2009 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906112021Floor Panel · crackedMAIN CABIN FLOOR PANEL 231KG CRACKED. FABRICATED NEW FLOOR PANEL REF DWG SRZ 25-005; REV "H". REMOVED DAMAGED FLOOR PANEL AND INSTALLED NEW FLOOR PANEL REF AMM 53-10-25-4.Jun 11, 2009 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906112020Floor Panel · crackedMAIN CABIN FLOOR PANEL CRACKED. FABRICATED NEW FLOOR PANEL REF DWG SRZ 25-005; REV "H". REMOVED DAMAGED FLOOR PANEL AND INSTALLED NEW FLOOR PANEL REF AMM 53-10-25-4.Jun 11, 2009 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906092012Cover · crackedFWD AVIONICS COMPARTMENT, 20 INCHES AFT OF FWD BULKHEAD, LBL 20, WINDOW HEAT CONTROLLER BOX COVER CRACKED. MATERIAL ID FOR NEW COVER 2024-T3 .025 / PN 528930.1 AND FORMED IAW MFG DWG A25510235, ALODINED AND PRIMED IAW SRM 51-21-10 PG. 8 STEP C AND PG 11 STEPJun 9, 2009 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200906092010Retainer · crackedAFT CARGO COMP. AFT DOOR JAMB LOWER SEAL DEPRESSOR, IN LWR CORNER OF DOOR JAMB, RETAINER CRACKED. REMOVED AND REPLACED AFT DOOR JAMB LWR SEAL RETAINER IAW SRM 51-40- 21 PARA. 13.Jun 9, 2009 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200906072007Channel · crackedFWD AVIONICS COMPARTMENT, RT SIDE, FRAME 16, BATTERY RACK, FWD CHANNEL, CENTER SUPPORT, CRACKED. REMOVED HAT CHANNEL; LOCATED, DRILLED AND DEBURRED HOLES AND INSTALLED IAW SRM 51-72-10. REMOVED AND INSTALLED BATTERY AND BATTERY COVER IAW AMM 24-31-11-4 STEP 2Jun 7, 2009 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200906072008Channel · crackedE AND E COMPARTMENT BATTERY RACK CENTER HORIZONTAL CHANNEL SUPPORT CRACKED AT ATTACH FASTENER. REMOVED DAMAGED CHANNEL, LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW CHANNEL PN A92425352020000 PN 656679.4 IAW SRM 51-72-10.Jun 7, 2009 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA200906052009Support Bracket · crackedNR 1 ENGINE INBD T/R HALF FWD LATCH PULL CABLE SUPPORT BRACKET IS CRACKED. REMOVED NR 1 ENG. INBD SUPPORT BRACKET REF CMM 78-32-00, WELDED BRACKET REF SPM 70-41-00, INSTALLED BRACKET REF CMM 78-32-00.Jun 5, 2009 · N683FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA200906031903Fitting · crackedRT FRAME 12A STIFFENER FLOORBEAM FITTING FOUND CRACKED ON UPPER SURFACE EMANATING FROM RADIUS. MARKED END OF CRACK. RT FRAME 12A FITTING REPLACED ON JOB CARD E 6-5340-7-5002 PT 8.Jun 3, 2009 · N683FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA200906031999Skin · damagedRT WING INBD FLAP UPPER SKIN DENTED AND CRACKED. FABRICATED SKIN REF. EA. 6-5750-127971, ALODINED AND PRIMED SKIN REF. AMM 51-23-10-00.Jun 3, 2009 · N683FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200906031902Floor Panel · crackedFWD CARGO FLOOR PANEL 132NG CRACKED AT PDU CUTOUT. REPAIRED FLOOR PANEL IAW SRM 51-77-12.Jun 3, 2009 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906021926Skin · damagedRIGHT FUSELAGE SKIN LIGHTENING STRIKE FR 13 - FR 13, STR 14R - STR 14R. REMOVED DAMAGE FASTENER REF SRM 53-10-12 PG 235. ACCOMPLISHED BHEC INSPECTION OF HOLE USING TESTER T8257A REF NTM PT 6 51-10-01 PROC A, NO DEFECTS NOTED. INSTALLED RIVET REF SRM 53-10-1Jun 2, 2009 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200906021925Skin · damagedRIGHT FUSELAGE SKIN LIGHTENING STRIKE FR12 - FR 12, STR 12R - STR 13R REMOVED DAMAGE FASTENER REF SRM 53-10-12 PG 235. ACCOMPLISHED BHEC INSP OF HOLE USING TESTER T8257A REF NTM PT 6 51-10-01 PROC A, NO DEFECTS NOTED. INSTALLED RIVET REF SRM 53-10-12 PG 24Jun 2, 2009 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200906021914Skin · damagedRT FUSELAGE SKIN, LIGHTENING STRIKE FR 11-FR 11, STR 12R-STR 13R. REMOVED DAMAGED FASTENER REF SRM 53-10-12 PG 235. ACCOMPLISHED BHEC INSP. OF HOLE USING TESTER T8257A REF NTM PT 6 51-10-01 PROC. A NO DEFECTS NOTED. INSTALLED NEW RIVET REF SRM 53-10-12 PG 24Jun 2, 2009 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200906021895Skin · damagedRIGHT HAND FUSELAGE SKIN HAS A LIGHTNING STRIKE FROM FRAME 11 TO FRAME 11; STRINGER 12R TO STRINGER 13R. REMOVED DAMAGE FASTENER REF SRM 53-10-12 PG 235. ACCOMPLISHED BHEC INSP. OF HOLE USING TESTER T8257A REF. A300 NTM PT 6 51-10-01 PROC. A, NO DEFECTS NJun 2, 2009 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200906021894Skin · damagedRIGHT HAND FUSELAGE SKIN HAS A LIGHTNING STRIKE FROM FRAME 12 TO FRAME 12; STRINGER 12R TO STRINGER 13R. REMOVED DAMAGE FASTENER REF SRM 53-10-12 PG 235. ACCOMPLISHED BHEC INSP OF HOLE REF NTM PT 6 51-10-01 PROC. A, NO DEFECTS NOTED. INSTALLED RIVET REFJun 2, 2009 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200906021893Skin · damagedRIGHT FUSELAGE SKIN HAS A LIGHTNING STRIKE FROM FRAME 13 TO FRAME 13; STRINGER 14R TO STRINGER 14R. REMOVED DAMAGE FASTENER REF SRM 53-10-12 PG 235. ACCOMPLISHED BHEC INSP OF HOLE USING TESTER T8257A REF NTM PT 6 51-10-01 PROC. A, NO DEFECTS NOTED. INSTALJun 2, 2009 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200906021892Skin · damagedRIGHT FUSELAGE SKIN HAS A LIGHTNING STRIKE FROM FRAME 13 TO FRAME 13 STRINGER 26-27R. REMOVED DAMAGE FASTENER REF SRM 53-10-12 PG 235. ACCOMPLISHED BHEC INSP. OF HOLE USING TESTER T8257A REF NTM PT 6 51-10-01 PROC. A, NO DEFECTS NOTED. INSTALLED RIVET REF SRJun 2, 2009 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA200812115133Proximity Sensor · failedMLG FAILED TO RETRACT, TRIED BOTH SYS 1 2. RTF. FOLLOWED TSM 32-30-00, CHECKED PROX DET, RT BOGIE FAIL. INSP RT MLG BOGIE BEAM SENSOR 12GA. REMOVING DETECTOR SUPPORT BOLT, FOUND WATER IN HOUSING. REMOVED, DRIED & LUBED IAW MM 32-11-14-6. INSP PITCH DAMPER IDec 11, 2008 · N683FE · Airbus A300B4605R · Landing Gear Position and WarningSDR FDEA200812115122Pseu · failedLANDING GEAR FAILED TO RETRACT, TRIED BOTH SYS 1 & 2. RETURNED TO AIRPORT. ACFT DOWN FOR WORK. REMOVED AND REPLACED PROXIMITY DETECTOR PROCESSING UNIT PER MM REFERENCE 32-31-71-4. BDL/11, LUBRICATED PIVOT PIN AIW MM 12-22-32-0 - BDL/11, ACN RELEASED FOR SDec 11, 2008 · N683FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 07FDEA05139Valve · failedON TAKEOFF ROLL AS POWER WAS ADVANCED TO FLEX POWER LEFT ECAM SHOWED "ENG 1 REV PRESSURIZED", W/MASTER CAUTION. REJECTED TAKEOFF AT 60KTS. AS THROTTLES REDUCED TO IDLE, LEFT ECAM AND MASTER CAUTION CLEARED. RELEASED FOR SERVICE. FOUND FAULTY DPV. REMOVED ADec 26, 2007 · N683FE · Airbus A300F4605R · Engine Thrust ReverserSDR 07FDEA04704Damper · failedON TAKEOFF LANDING GEAR WOULD NOT RETRACT ON SYS2. SWITCHED TO SYS 1 AND TRIED AGAIN. GEAR STILL WOULD NOT RETRACT FAULT ON PROX BOX FOR RT GEAR, JACKED A/C. PRIOR TO RETRACTING GEAR NOTICED RT FWD TRUCK WAS NOT AS LOW AS LEFT, STOOD ON GEAR AND GOT IT TOOct 31, 2007 · N683FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 07FDEA03305Bracket · crackedA 3.5" INCH CRACK EXIST AT NR 2 ENGINE T/R I/B L/E UPPER POSITION LOCATED ON BRACKET SUPPORT FLANGE REF 78-31-00-6. REMOVED AND REPLACED NR 2 ENG I/B T/R IAW A300-600 AMM71-13-03-4-05, OPS CHECKED GOOD IAW A300-600 AMM 71-13-03-4-05.Sep 2, 2007 · N683FE · Airbus A300F4605R · Engine Thrust ReverserSDR 07FDEA03304Flange · crackedA 1.5" AND A .5 INCH CRACK EXIST AT NR 2 ENGINE O/B T/R UPPER L/E FLANGE REF 78-31-00-6 REMOVED AND REPLACED NR 2 ENG O/B T/R IAW A300-600 AMM 71-13-03-4-05 OPS CHECK GOOD IAW A300-600 AMM 71-03-4-05.Sep 2, 2007 · N683FE · Airbus A300F4605R · Engine Thrust ReverserSDR 07FDEA03303Flange · crackedA 1.5" AND A .5 INCH CRACK EXIST AT NR 2 ENGINE O/B T/R UPPER L/E FLANGE REF 78-31-00-6. REMOVED AND REPLACED NR 2 ENG O/B T/R IAW A300-600 AMM 71-13-03-4-05 OPS CHECK GOOD IAW A300-600 AMM 71-03-4-05.Sep 2, 2007 · N683FE · Airbus A300F4605R · Engine Thrust ReverserSDR 07FDEA03299Skin · chafedRT CTR FLAP UPPER SURFACE HAS 6 EA WEAR MARKS FROM CONTACT WITH NR 5 SPOILER IB SUPPORT ARM RIVETS. DEPTH RANGES FROM .005 TO .009" DEEP. AREA FOUND TO BE OUT OF LIMITS IAW A300 SRM 57-50-00 FIG 101, SH 5. REPAIRED AREA IAW A300 SRM 57-50-00 PARA E, FIG 205Sep 1, 2007 · N683FE · Airbus A300F4605R · Trailing Edge FlapsSDR 07FDEA03298Skin · dentedRT INBD FLAP TOP SURFACE 2 IN OTBD OF RIB 6 10 IN AFT OF FRONT SPAR IS A DENT 1.4 BY .020 INCH WITH A GOUGE .6 IN BY .1 IN BY .002 IN REF A300/600 SRM 57-50-00 AREA FOUND TO BE OUT OF LIMITS IAW A300 SRM 57-50-00 FIG 101, SH5. REPAIRED AREA IAW A300 FREIGHSep 1, 2007 · N683FE · Airbus A300F4605R · Trailing Edge FlapsSDR 07FDEA03233Seat Track · corrodedMDCC SEAT TRACK 3 RT FR15B-FR19 5 SQ IN CORROSION REF A300-600 AMM 53-10-16-6-02 ZONE 220. REMOVED CORROSION ON SEAT TRACK IAW A300 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300 SRM 53-10-16 FIG 102. REMOVED AND REPLACED SEAT TRACK IAW A300 SRM 53-40-21.Aug 29, 2007 · N683FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00352Unknown · unknownON PUSHING POWER UP FOR TAKEOFF, AFTER SELECTING TOGA, GOT NR 1 ENGINE REVERSER PRESSURIZED AT 50 KIAS. TAXIED BACK TO RAMP. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 16FEB07 "MEL 78-30-01-A: ENGINE NR 1 THRUST REVERSER INOPFeb 6, 2007 · N683FE · Airbus A300F4605R · Engine Thrust ReverserSDR 06FDEA04159Windshield · crackedF/O WINDSHIELD CRACKED AND ARCING. REMOVED AND REPLACED S/O WINDSHIELD PER AMM 56-11-11-4. REMOVED AND REPLACED WINDOW HEAT CONTROLLER PER AMM 30-42-11-4, AND WINDOW HEAT PROTECTION UNIT PER AMM 30-42-51-4, WINDOW HEAT TEST GOOD PER AMM 30-42-0.Dec 2, 2006 · N683FE · Airbus A300F4605R · Flight Compartment WindowsSDR 06FDEA0179Connector · unsecureAFTER T/O RECEIVED ECAM: NR 2 REVERSER PRESSURIZED. FOUND T/R PRESSURE SWITCH CONNECTOR CONNECTED TO PRESSURE SWITCH. REMOVED AND STOWED CONNECTOR. OPS CHECKS GOOD.Jan 13, 2006 · N683FE · Airbus A300F4605R · Engine Exhaust System WiringSDR 05FDEA01043Floorbeam · crackedFLOORBEAM CRACKED FRAME 58 / -Y953. REMOVED ALL NECESSARY CARGO LOADING SYSTEM AND FLOOR PANELS TO FOM. REMOVED DAMAGED ADAPTER.Apr 18, 2005 · N683FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 03FDEA01178Doubler · wornRT CREW ENTRY DOOR CUTOUT FAILSAFE DOUBLER GOUGED/WORN FROM FORWARD TO AFT CUTOUT BLENDED AREA AND PERFORMED HFEC (NO CRACKS INDICATED). CHECK PRELOAD ON COVER PLATE IAW DRW A007 10134. REPROTECTED AREA AND REFINISHED. ALL WORK DONE IAW EA 6-5312-71388 AND RJul 30, 2003 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 03FDEA00016Thrust Reverser · inoperativeON TAKEOFF ROLL, CYMX, RWY27, ECAM MEMO PAGE DISPLAYED WARNING THAT NR 1 REVERSER SYSTEM WAS PRESSURIZED. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A ENGINE NR 1 THRUST REVERSER INOP, THRUST (1 OR 2). REVERSER DEACTIVATED IN FORWARD THRUST POSITION. NRJan 11, 2003 · N683FE · Airbus A300B4605R · Engine Thrust ReverserSDR 01FDEA00521Pitot Line · obstructedNO AIRSPEED ON T/O ON NR 1 STBY, PFD AND NR 2 STBY PD. FLUSHED CAPT, F/O'S AND STBY PITOT LINES. OPS CK PER MM 34-10-00-5, TEST OK.Jul 7, 2001 · N683FE · Airbus A300F4605R · Pitot/Static System
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