N686FE

Service difficulty reports · 181

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 = 'N686FE' 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 FDEA201209073251Floorboard · damagedFLOORBOARD 151TF HAS TWO AREAS DAMAGED UPPER AND LOWER SKIN PLYS WITH CRUSHED CORE. THE LARGEST AREA IS 8" BY 3". FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 7, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209063247Floorbeam · crackedMAIN CARGO DECK FLOORBEAM AT FR 61 BETWEEN SEAT TRACK 4R AND 5R CRACKED ABOUT 0.125" ON THE AFT FACE EXTRUSION REF AMM 53-10-15-06-02, ZONE 250. BLENDED FLOORBEAM IAW SRM 53- 10-15- PG 14. CUT OUT CRACKED AREA OF FLOORBEAM IAW SRM 53-10-15 FIG 211 PG 386. Sep 6, 2012 · N686FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201109274153Heater · arcedL1 WINDOW HEAT ARCHING THEN CRACKED AT FLIGHT LEVEL 350. FOLLOWED QRH AND TURNED OFF WINDOW HEAT AND DESCENDED TO 250, DIVERTED. REMOVED AND REPLACED LEFT WINDSHIELD PANEL PER AMM 56-11-11-04.Sep 27, 2011 · N686FE · Airbus A300F4605R · Windshield/Door Rain/Ice RemovalSDR FDEA201010124014Carriage · misalignedRT WING T/E FLAP NR 5 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. GMM 6-2-100 REPAIR CLASSIFIED AS MINOR.Oct 12, 2010 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201010124013Carriage · misalignedRT WING T/E FLAP NR4 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 12, 2010 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201010124012Carriage · misalignedRT WING T/E FLAP NR3 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 12, 2010 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201010124010Carriage · misalignedRT WING T/E FLAP NR 6 FRONT CARRIAGE UPPER BRIDGE WAS FOUND SHIM MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 12, 2010 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201010124009Carriage · misalignedRT WING T/E FLAP NR6 REAR CARRIAGE LEVER MOUNTING YOKE INBD SHIM MIGRATED. EA 6-2750-414636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 12, 2010 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201010124008Carriage · misalignedLT WING T/E NR 3 TRACK CARRIAGE UPPER BRIDGE INBD SHIM GOT MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 12, 2010 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201010124007Shim · misalignedLT WING T/E NR 5 TRACK CARRIAGE UPPER BRIDGE INBD SHIM GOT MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 12, 2010 · N686FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201010063953Rib · crackedFASTENER HOLES WERE FOUND CRACKED AT RIB25A OF LEFT WING INBD FLAP IAW EO E6-5750-7-5003, PT1. THE REPAIR CLASSIFIED AS MINOR GMM 6-2-100.Oct 6, 2010 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201010063952Door · crackedLT MLG DOOR OTBD EDGE GOT IMPACT DAMAGED AT CTR AREA. DAMAGE EDGE AREA REPAIRED IAW EA NR 6-5280-141635 . THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Oct 6, 2010 · N686FE · Airbus A300F4605R · Landing Gear DoorsSDR FDEA201010063951Skin · crackedLT WING T/E UPPER SKIN SUPPORT WEB CRACKED AT NR 4 SPOILER OTBD HINGE NEARBY. FABRICATED LT SUPPORT SKIN I.AW AB6F DWG NR A57240194 (PN A57240194200). INSTALLED THE SUPPORT SKIN WITH FASTENER IAW AB6F SRM 51-40-21. THE REPAIR CLASSIFIED AS MINOR IAW GMM Oct 6, 2010 · N686FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201010053950Skin · crackedLT WING T/E UPPER SKIN SUPPORT WEB GOT CRACK AT NR 3 SPOILER INBD HINGE NEARBY. FABRICATED LT SUPPORT SKIN IAW AB6F DWG NR A57240194 (PN A57240194201). INSTALLED THE SUPPORT SKIN WITH FASTENER IAW AB6F SRM 51-41-21. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6Oct 5, 2010 · N686FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201001150151Gearbox · leakingAFTER T/O FLAPS WOULD NOT RETRACT. OVERHEAD PANEL INDICATED FLAP SYS 2 FAULT & WHEN HANDLE RAISED THE FLAPS STAYED AT 20 DEG AND FLAP SYS 1 FAULT CAME ON. THERE WAS NOT A FLAPS LIGHT ON SPFI PANEL AT ANY TIME. RECYCLED FLAP HANDLE IAW QRH & GOT SAME RESULTS Jan 15, 2010 · N686FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201001140146Pcu · failedAFTER T/O FLAPS WOULD NOT RETRACT- FOLLOWED QRH -RECYCLED NO HELP - RETURNED TO DEPARTURE. REPLACED LT FLAP PCU HIGH SPEED VALVE IAW MM 27-54-33-4. OPS CKD FLAP SEVERAL TIMES. OPS CKD GOOD. INSPECTED BOTH FSCC'S. NO FAULTS NOTED. CLOSED TDR RESULTS= CONFIJan 14, 2010 · N686FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA200812265299Unknown · unknownLEVEL CRUISE AT FL 250, ENG 2 FUEL CLOG LIGHT CAME ON WITH ASSOCIATED ECAM ALERT. REDUCED ENG 2 POWER TO IDLE IAW ECAM. STARTED RETURN TO MEM. AFTER 7-8 MINS AT IDLE, LIGHT WENT OUT AND STAYED OUT THROUGHOUT APPROACH AND LANDING USING NORMAL POWER. REPEAT Dec 26, 2008 · N686FE · Airbus A300F4605R · Engine Fuel and ControlSDR 08FDEA03174Seat Track · damagedMAIN CARGO DECK LT SIDE NR 4 SEAT TRACK BETWEEN FR 57 AND FR 57.1 HAS 2 EA ELONGATED SCALLOPS. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED SEAT TRACK SPLICE REPAIR AT TRACK NR 4 LT BETWEEN FR 57 AND FR 57.1 IAW SRM 53-10-16, FIG 201, PG 207/208.Jul 30, 2008 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03172Skin · chafedRT WING CENTER FLAP UPPER SURFACE APPROX RIB 16, 7 EA WEAR MARKS FROM BUTTON HEAD RIVETS CHAFING REMOVED DAMAGED SECTION AND INSTALLED FLAP SKIN PATCH REPAIR IAW SRM 57-50-00, FIG 205, PG 219.Jul 30, 2008 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA03045Seat Track · damagedMAIN DECK LEFT SIDE SEAT TRACK 4 AT FRAME 54 HAS 2 ELONGATED SCALLOPS. REMOVED DAMAGED TRACK FROM FRAMES 54 TO 54.2 AND INSTALLED NEW TRACK IAW A300-600 SRM 51-72-10 AND 51-40-21. RESTORED PROTECTIVE COATING IAW A300-600 SRM 51-75-10.Jul 24, 2008 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03043Seat Track · damagedMAIN DECK LT SIDE SEAT TRACK 4L AT FRAME 20 HAS 3 ELONGATED SCALLOPS. REMOVED AND REPLACED SEAT TRACK 4L FROM FRAMES 18 TO 26 IAW A300-600 SRM 51-72-10 AND 51-40-21.Jul 24, 2008 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02977Seat Track · damagedMAIN CARGO DECK LT SIDE NR 4 SEAT TRACK BETWEEN FR 60 AND FR 61 HAS 3 EA ELONGATED SCALLOPS. REMOVED DAMAGED TRACK SECTION AND INSTALLED SEAT TRACK SPLICE. REPAIR AT LT TRACK NR 4 BETWEEN FR 60 AND FR 61 IAW A300-600 SRM 53-10-16, FIG 201, PG207/208.Jul 18, 2008 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02948Seat Track · damagedMAIN DECK LT SIDE SEAT TRACK NR 2 AT FRAME 52 HAS 1 ELONGATED SCALLOP REMOVED DAMAGED SECTION AND INSTALLED REPAIR ON NR 2 LT SEAT TRACK AT FRAMES 52-54 IAW SRM 53-10-16 FIG 203 SHEET 5.Jul 17, 2008 · N686FE · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00120Pump · leakingAPPROXIMATELY ONE HOUR IN FLIGHT, ECAM WARNING: GREEN PUMP 2 LO PR" FOLLOWED BY "GREEN PUMP 1 LO PR". OBSERVED GREEN RESERVOIR OVERHEAT LIGHT ON. COMPLIED WITH ECAM AND QRH AND TURNED OFF BOTH GREEN PUMPS. ON APPROACH AND LANDING. ON SHORT FINAL, GREEN NRJan 14, 2008 · N686FE · Airbus A300F4605R · Hydraulic Pump (Electric/Engine), MainSDR 06FDEA04247Unknown · unknownCALLED OUT A/C AFTER AN ABORTED T/O FOR A LOUD SQUEAL ON FLIGHTDECK AT 80 KTS. REQUESTED FLIGHT CREW UNPLUG PERSONAL HEADSET AND PLUG IN COMPANY HEADSET. CREW REQUESTED ANOTHER T/O ATTEMPT, A/C DEPARTED KIND.Dec 15, 2006 · N686FE · Airbus A300F4605R · Standard Practices/StructuresSDR 05FDEA01502Warning System · malfunctionedDURING APPROACH WHEN LANDING GEAR LOWERED, LANDING GEAR INDICATIONS ON FORWARD PANEL INDICATED 3 DOWN GREEN WITH 3 RED UNLOCKED INDICATION, POSITION DETECTION SYSTEM WAS SELECTED TO SYS 1. ECAM DIRECTED SWITCH TO POSITION DETECTOR SYS 2. SWITCHED TO SYSTEM 2Jun 1, 2005 · N686FE · Airbus A300B4605R · Landing Gear Position and WarningSDR 05FDEA00223Limit Switch · failedON T/O AFTER BRK REL AND STANDARD POWER SET APPROX 50 KTS HAD AMBER ECAM 1 THR REV UNLOCK WITH AMBER REV UNLOCK ON PANEL ABOVE ENG INSTRUMENTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C. ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DFeb 2, 2005 · N686FE · Airbus A300F4605R · Engine Thrust ReverserSDR 05FDEA00186Thrust Reverser · inoperativeNR 1 REVERSER PRESSURIZED ECAM ALERT ON INITIAL TAKEOFF. NR 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION.Jan 27, 2005 · N686FE · Airbus A300F4605R · Engine Thrust ReverserSDR 04FDEA02158Reservoir · lowDURING CRUISE FLIGHT AT FL 330 .80 MACH ECAM ALERTED-INDICATING LOSS OF BLUE HYD SYSTEM (HYD RSVR LO LEVEL) - ECAM SYSTEM PAGE SHOWED BLUE HYD SYSTEM RESEVIOR WAS LOW. ECAM PROCEDURE FOR HYD RSVR LO LEVEL ACCOMPLISHED. REMAINING HYD SYSTEMS NORMAL. FOUND Jul 22, 2004 · N686FE · Airbus A300F4605R · Hydraulic Reservoir, MainSDR 01FDEA00076Warning Light · illuminatedDURING T/O ROLL, RECEIVED ECAM WARNING NR 2 ENG REVERSER PRESSURIZED. AC RELEASED FOR SERVICE PER MEL 78-1.Feb 6, 2001 · N686FE · Airbus A300F4605R · Engine Thrust ReverserSDR 00FDEA00699Unknown · odorSTRONG ODOR OF NATURAL GAS OR PROPANE AT CR. ALL FREIGHT REMOVED AND INSP, NONE FOUND. AN OPS CK OF TR1, & TR2, & ESS TR WAS DONE DUE TO TR POPPING C/B.Oct 4, 2000 · N686FE · Airbus A300F4605R · Air Distribution System
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