N682FE

Service difficulty reports · 299

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 = 'N682FE' 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 FDEA200907022454Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 132 LG HAS EDGE DAMAGE AND IS MISSING AN INSERT. FABRICATED FLOOR PANEL 132 LG IAW DWG SRZ 25-005, REV "H".Jul 2, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200907022453Floorboard · crackedFWD CARGO COMPARTMENT FLOORBOARD 132 KG CRACKED. FABRICATED FLOOR PANEL 132 KG IAW DWG SRZ 25-005, REV "H".Jul 2, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200907022452Floorboard · puncturedFWD CARGO COMPARTMENT FLOORBOARD 132 NG HAS MULTIPLE PUNCTURES ON THE BOTTOM AND EDGE DAMAGE. FABRICATED FLOOR PANEL 132 NG IAW DWG SRZ 25-005, REV "H".Jul 2, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200907012443Frame · crackedNR 1 ENGINE RT REVERSER COWL, INNER FWD UPPER U CHANNEL FRAME, HAS 2 CRACKS AT APPROX THE 11 O'CLOCK POSITION BELOW THE V-BAND ASSY; NS 59.305. DISPLACED SEAL DEPRESSOR FOR ACCESS IAW SRM 51-40-21, REPLACED CRACKED FRAME REF DWG SRZ 78-002. REINSTALLED SEALJul 1, 2009 · N682FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA200907012442Frame · crackedNR 2 ENGINE RT REVERSER COWL UPPER CORNER IS CRACKED BELOW THE V-BAND LATCH. DISPLACED SEAL DEPRESSOR FOR ACCESS IAE SRM 51-40-21. STOP DRILLED CRACK IAW DWG SRZ 78-002. INSTALLED DOUBLER IAW DWG SRZ 78-002. REINSTALLED SEAL DEPRESSOR IAW DWG SRZ 78-002.Jul 1, 2009 · N682FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA200907012441Structure · crackedNR 2 ENGINE INBD T/R FWD UPPER CORNER IS CRACKED BELOW THE V-BAND LATCH. CRACK WAS FOUND TO BE OUT OF LIMITS. T/R TO BE REPLACED ON N/R N00598.Jul 1, 2009 · N682FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA200907012440Frame · crackedNR 1 ENGINE OTBD T/R FWD FACE AT THE UPPER END NEAR THE V-BAND IS CRACKED. DISPLACED SEAL DEPRESSOR FOR ACCESS IAW SRM 51-40-21. REPAIRED CRACKED FRAME REF DWG SRZ 78-002. REINSTALLED SEAL DEPRESSOR IAW DWG 78-002.Jul 1, 2009 · N682FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA200907012438Rib · crackedRT WING INBD FLAP RIB 25-A IN CRACKED IN THE UPPER RADIUS OF THE HORIZONTAL UPPER FLANGE. REMOVED SKIN; RIB 25A IAW SRM 51-40-21, PARA 7. INSTALLED NEW RIB 25A IAW SRM 51-40-21.Jul 1, 2009 · N682FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200907012437Rib · crackedLT WING INBD FLAP RIB 25-A IN CRACKED IN THE UPPER RADIUS OF THE HORIZONTAL UPPER FLANGE. REMOVED SKIN; RIB 24; RIB 25A AND 6EA. WEBS IAW SRM 51-40-21, PARA 7. INSTALLED NEW RIB 25A ; OLD RIB 24; THE 6 EA. WEBS AND THE SKIN IAW SRM 51-40-21.Jul 1, 2009 · N682FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200906292362Seat Track · wornMAIN CABIN ARTICULATING SEAT TRACK IS WORN AT FRAME 23; LBL 26. REMOVED FLOOR PANEL IAW AMM 53-10-23-4. BLENDED WORK AREA AND REMOVED 0.001 MATERIAL. MATERIAL REMAINING WAS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-16; FIG 101. REINSTALLED FLOOR PANEL IAW AMJun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200906292382Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 VF IS CRACKED. FABRICATED FLOORBOARD 252 VF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 VF IAW AMM 53-10-25-4. INSTALLED FLOORBOARD 252 ZF IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292381Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 ZF IS CRACKED. FABRICATED FLOORBOARD 252 ZF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 ZF IAW AMM 53-10-25-4. INSTALLED FLOORBOARD 252 ZF IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292380Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 UF IS CRACKED. FABRICATED FLOORBOARD 252 UH IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 UH IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292379Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 232 YG IS DENTED/CRACKED. REPAIRED MAIN CABIN FLOORBOARD 232 YG BY FABRICATING A NEW FLOORBOARD USING THE OLD FLOORBOARD AS A TEMPLATE; POTTED EDGE; DRILLED; INSTALLED INSERTS; SANDED; CLEANED; INSTALLED ANTI-SKID TAPE Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292378Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 232 BF IS DENTED / CRACKED. FABRICATED FLOOR PANEL 242 BF IAW DWG SRZ 25-005, REV "H". REMOVED AND REPLACED 242 BF IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292377Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 GF IS DENTED/CRACKED. FABRICATED FLOOR PANEL 242 GF IAW DWG SRZ 25-005, REV "H". REMOVED AND REPLACED 242 GF IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292376Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 MF IS DENTED/CRACKED. FABRICATED FLOOR PANEL 242 MF IAW DWG SRZ 25-005, REV "H". REMOVED AND REPLACED 242 MF IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292375Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 SF IS DENTED/CRACKED. FABRICATED MAIN CABIN FLOOR BOARD 242 SF USING THE OLD BOARD AS A TEMPLATE; POTTED EDGE; DRILLED; INSTALLED INSERTS; SANDED AND CLEANED; INSTALLED ANTI-SKID TAPE AND PART MARKED IAW DWG SRZ 25Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292374Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 QJ IS DENTED/CRACKED. FABRICATED NEW FLOOR PANEL 242 QJ IAW DWG SRZ 25-005; REV "H".Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292373Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 UJ IS DENTED/CRACKED. FABRICATED NEW FLOOR PANEL 242 UJ IAW DWG SRZ 25-005; REV "H".Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292372Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 ZJ IS DENTED/CRACKED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV "H". ALL WORK WAS ACCOMPLISHED ON N/R N00168.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292371Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 EK IS DENTED/CRACKED. REPAIRED MAIN CABIN FLOORBOARD 242 EK BY FABRICATING A NEW BOARD USING THE OLD BOARD AS A TEMPLATE; POTTED EDGE; DRILLED; INSTALLED INSERTS; SANDED AND CLEANED; INSTALLED ANTI-SKID TAPE AND PAJun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292370Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 RG IS DENTED. FABRICATED FLOOR BOARD 242 RG IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 242 RG IAW AMM 53-10-25-4. ALL WORK WAS ACCOMPLISHED ON N/R N00166.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292369Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 ZJ IS CRACKED. FABRICATED NEW FLOOR PANEL IAW DWG SRZ 25-005; REV "H".Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292368Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 EK IS CRACKED. REPAIRED MAIN CABIN FLOOR BOARD 242 EK BY FABRICATING A NEW BOARD USING THE OLD BOARD AS A TEMPLATE; POTTED EDGE; DRILLED; INSTALLED INSERTS; SANDED AND CLEANED; INSTALLED ANTI-SKID TAPE AND PART MAJun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292367Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 RG IS CRACKED. FABRICATED FLOORBOARD 242 RG IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 242 RG IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292366Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 VG IS CRACKED. FABRICATED FLOOR PANEL 242 VG IAW DWG SRZ 25-005, REV "H". INSTALLED FLOOR PANEL 242 VG IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292365Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 BF IS CRACKED. FABRICATED FLOORBOARD 252 BF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 BF IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292364Floorboard · crackedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 GF IS CRACKED. FABRICATED FLOORBOARD 252 GF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 GF IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292363Floorboard · crackedMAIN CARGO COMPARTMENT FLOORBOARD 252 PH IS CRACKED. FABRICATED FLOORBOARD 252 PH IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 252 PH IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292361Floorboard · crackedMAIN CARGO COMPARTMENT FLOORBOARD 251 NG IS CRACKED. FABRICATED FLOOR PANEL 251 RT IAW DWG SRZ 25-005, REV "H". INSTALLED FLOOR PANEL 251 RT IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292360Floorboard · crackedMAIN CARGO COMPARTMENT FLOORBOARD IS DENTED/CRACKED, ZONE Z241, PANEL HK AT FRAME 53. FABRICATED FLOOR PANEL 241 HF IAW DWG SRZ 25-005, REV "H". INSTALLED FLOOR PANEL 241 HF IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292359Floorboard · damagedMAIN CARGO COMPARTMENT FLOORBOARD IS SPONGY, ZONE Z241, PANEL AJ AT FRAME 46. FABRICATED NEW FLOORBOARD 241 AJ IAW SRZ 25-005 REV "H". REMOVED AND REPLACED FLOOR PANEL 241 AJ IN REF TO AMM 53-10-23-4. PART MARKED PANEL IN REF TO GMM 7-0-1001.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292358Floorboard · crackedMAIN CARGO COMPARTMENT FLOORBOARD IS DENTED/CRACKED. ZONE Z241 PANEL WH AT FRAME 46. FABRICATED NEW FLOOR PANEL 241 WH IAW DWG SRZ 25-005; REV "H".Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292357Floorboard · puncturedMAIN CARGO COMPARTMENT FLOORBOARD IS PUNCTURED AT FRAME 31, LBL 52. FABRICATED FLOORBOARD 241 MJ IAW DWG SRZ 25-005, REV "H". INSTALLED FLOORBOARD 241 MJ IAW AMM 53-10-25-4.Jun 29, 2009 · N682FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200906292356Skin · chafedTHE R-1 DOOR AREA, FAILSAFE RING UPPER FWD CORNER EXTERNAL SKIN IS CHAFED. COMPLIED WITH E.A. 6-5330-127973.Jun 29, 2009 · N682FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA200812241227Pickup · failedON APPROACH HAD A FLAPS SYS 1 AND 2 FAULT/FLAPS STUCK. CYCLE HANDLE PER CHECK LIST COULD NOT GET FLAPS TO EXTEND. LAND 0 FLAPS SLATS EXTENDED. BELIEVE EMERGENCY DECLARED. REMOVED AND REPLACED ASYMMETRY POS P/U RT AND FEEDBACK POS P/U. REF MM 27-56-11-4 ANDec 24, 2008 · N682FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR 07FDEA05140Windshield · crackedCAPTS FWD WINDSHIELD SHATTERED IN CRUISE. REMOVED AND REPLACED CAPT'S WINDSHIELD PANEL, WINDOW HEAT PROTECTION CONTROLLER AND WINDSHIELD TEMP REGULATOR. WINDOW INSTALLATION COMPLETED IAW MM 56-11-11-4.Dec 26, 2007 · N682FE · Airbus A300F4605R · Flight Compartment WindowsSDR 06FDEA2455Transmitter · malfunctionedEN ROUTE TO BTR BLUE SYSTEM HYDRAULIC LOSS. UNABLE LDG BTR, SHORT RUNWAY. BLUE HYD PRESS TRANSMITTER LEAKING. REMOVED AND REPLACED BLUE SYS PRESSURE XMITTER. SERVICED SYS RAN ENG OPS CHECKED GOOD AMM29-32-13-4.Jul 2, 2006 · N682FE · Airbus A300* · Hydraulic Pressure SensorSDR 06FDEA0813Gcu · faultyPDIS 682 24-30 0004948 22FEB06 MEM CLOSE R LOGPAGES: 01107636 GEN NR1 FAULT AFTER TAKEOFF WOULD NOT RESET. APU WAS INOP (ON MEL) FACT 23FEB06 07:18 MEM R VERIFIED NR 1 ENGINE IDG OIL SERVICED PROPERLY. PERFORMED BITE TEST OF THE GPCU. FAULTED LT GENFeb 23, 2006 · N682FE · Airbus A300* · DC RegulatorSDR 04FDEA00602Autothrottle Sys · failedON FINAL APPROACH, NR 1 THROTTLE STUCK AT ABOUT 15 DEGREES. DECLARED EMERGENCY AND FINISHED APPROACH. AFTER LANDING, THROTTLE MOVED FREELY. RELEASED FOR SERVICE PER MEL/CDL: 22-30-01 CATEGORY: C EXPIRATION: 16MAR04 MEL 22-30-01: AUTOTHROTTLE SYSTEM INOP. AMar 6, 2004 · N682FE · Airbus A300F4605R · Auto Throttle SystemSDR 03FDEA00680Door · gougedEXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR. COMPLIED WITH EA 8-7832-68795 EXHAUST-THRUST REV-BLOWOUT DOOR SKIN REPAIR AT MAE.May 5, 2003 · N682FE · Airbus A300F4605R · Engine Thrust ReverserSDR 03FDEA00675Angle · gougedNR 233 NR 2 ENG I/B THRUST REVERSER LOWER CORE STRUCTURE ANGLE GOUGED 4 AREAS. R/R ANGLE PER IAW SRM 51-40-21 SRM 51-40-21 AT MAE.May 3, 2003 · N682FE · Airbus A300F4605R · Engine Thrust ReverserSDR 03FDEA00669Rib · gougedCOMPLY WITH E.A. 6-5751-70370 WINGS-FIXED TRAILING EDGE- RIB 7A (LT) GOUGE REPAIR, P/N A572-46814. FACT 02MAY03 12:14 BFM U COMPLIED WITH E.A. 6-5751-70370 WINGS-FIXED TRAILING EDGE-RIB 7A (LT) GOUGE REPAIR P/N A572-46814 AT MAEMay 2, 2003 · N682FE · Airbus A300B4605R · Wing, Rib/BulkheadSDR 03FDEA00670Strip · crackedRT WING NR 3 SPOILER T/E STEEL STRIP CRACKED. R & R STRIP PER IPER IAW SRM 51-40-23 & 57-72-11.AND SRM 57-72-11 WO 22877 AT MAE.May 2, 2003 · N682FE · Airbus A300B4605R · Drag Control SystemSDR 03FDEA00671Tube · crackedNR 1 ENGINE PRECOOLER CRACKED AT COOLING TUBE INSTALLED PRECOOLER IAW W/C 64S0202 WO 22877 AT MAE.May 2, 2003 · N682FE · Airbus A300B4605R · Pneumatic Distribution SystemSDR 03FDEA00650Panel · gougedDEEP GOUGE IN RT WING L/E PNL 612B, FOUND TO BE OUT OF LIMITS PER IAW SRM 57-41-11. REPLACED PNL, TREATED, PRIMED AND PAINTED PER IAW SRM 51-40-44, SRM 51-75-10 AND SRM 51-21-10.Apr 29, 2003 · N682FE · Airbus A300B4605R · Wing, Plate/SkinSDR 02FDEA00610B-Nut · looseNR 1 GEN FAULT ILLUMINATED IN FLIGHT. FOLLOWED ECAM PROCEDURES. UNABLE TO RESET NR 1 GEN STARTED APU. ACN RELEASED PER MEL/CDL: 24-11-01GEN NR 1 - INOP. APU GEN MUST BE USED TO PWR 1 AFFECTED BUS THROUGHOUT FLIGHT. VERIFY AND RECORD IN EAML THAT OIL QTY OAug 31, 2002 · N682FE · Airbus A300F4605R · APU Oil SystemSDR 01FDEA01106Warning System · activatedDURING T/O, NR 2 REVR PRESSURIZED WARNING ON ECAM. REVR DEACTIVATED IN FWD THRUST POSITION.Dec 27, 2001 · N682FE · Airbus A300F4605R · Engine Thrust Reverser
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