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 FDEA201605201687Unknown · malfunctionedLANDING GEAR WOULD NOT RETRACT. GEAR HANDLE DID MOVE PAST INTERLOCK TO UP POSITION, BUT GEAR DID NOT RETRACT. NO ABNORMAL GEAR POSITION INDICATIONS SHOWN. INSTALLED THREE EACH GEAR PINS. JACKED ACFT IAW MM 07-11-00-00 & RETRACTED GEAR SEVERAL TIMES IAW AMMay 20, 2016 · N686FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201502220576Seat Track · wornMDCC FRAMES 60 - 61, Y1456 SEAT TRACK WORN. REPAIRED THE SEAT TRACK IAW SRM 53-10-16 FIGURE 201. THIS REPAIR IS CATEGORY A. AND LOADING SYS TEST OK. MAJOR REPAIR IAW GMM 6-2-100.Feb 22, 2015 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201502130528Skin · puncturedRIGHT WING INBD FLAP LOWER SKIN BETWEEN RIB 12 - 13 FOUND ONE EACH PUNCTURE. REPAIRED IAW SRM 57-50-00 PARA. 4E. MAJOR REPAIR IAW GMM 6-2-100.Feb 13, 2015 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201502060461Splice · crackedFUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 - 26 LT, INSPECTION FOUND FASTENER HOLE L WITH CRACK SIGNAL. COMPLIED WITH EA 6-5310-T0315451 PT1. REPAIRED FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STGR24-26 LT, FASTENER HOLE "L". THIS REPAIR IS CATEGORFeb 6, 2015 · N686FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201502060460Splice · crackedFUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 - 26 LT, INSPECTION FOUND FASTENER HOLE B WITH CRACK SIGNAL. COMPLIED WITH EA 6-5310-T0315451 PT1. REPAIRED FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STGR24-26 LT, FASTENER HOLE "B". THIS REPAIR IS CATEGORFeb 6, 2015 · N686FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201502060459Splice · crackedFUSELAGE FRAME 47 SPLICE FITTING BETWEEN STRINGER 24 - 26 LT, INSPECTION FOUND FASTENER HOLE A WITH CRACK SIGNAL. REPAIRED FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24-26 LT, FASTENER HOLE "A". THIS REPAIR IS CATEGORY B. MAJOR REPAIR IAW GMM 6-2-100Feb 6, 2015 · N686FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201502040431Structure · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION INSPECTION, RT LOWER BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0315522 PT 1. REPAIR FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RT LOWER BOLT HOLE. THFeb 4, 2015 · N686FE · Airbus A300F4605R · Wing Main, Frame StructureSDR FDEA201502040430Structure · crackedFRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION INSPECTION, RT MID BOLT HOLE WITH CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0315522 PT 1. REPAIR FRAME 40 TO CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RT MID BOLT HOLE. THIS RFeb 4, 2015 · N686FE · Airbus A300F4605R · Wing Main, Frame StructureSDR FDEA201405191076Adc · faultyREPEAT, CAPTAIN`S ALTIMETER FAULTED WHEN PULLED TO STANDARD. UNABLE TO SILENCE THE CONTINUAL CHIME & WARNING SEQUENCE UNTIL RETURNED TO BARO POSITION, ECAM WARNINGS INCLUDED. AFTER LANDING IN BARO POSITION, THE WARNING REPEATED THEN CLEARED AS WE SLOWED BELOMay 19, 2014 · N686FE · Airbus A300F4605R · Air Data ComputerSDR FDEA201405191073Proximity Sensor · inoperativeCAPTAINS ALTIMETER FAULTED WHEN PULLED TO STANDARD. UNABLE TO SILENCE THE CONTINUAL CHIME & WARNING SEQUENCE UNTIL RETURNED TO BARO POSITION. INCLUDED ECAM WARNINGS. AFTER LANDING IN BARO POSITION THE WARNING REPEATED. R & R PROXIMITY DETECTOR UNIT IAW MM May 19, 2014 · N686FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201401120085Valve · failedAFTER TAKEOFF AT APPROXIMATELY 2000 FT, RECEIVED ECAM WARNING, NR 1 ENG RUN, BLEED, TEMPERTURE KEPT RISING UNTIL NR 1 PACK TRIPPED, RECEIVED A AVIONICS SMOKE & MIN EQUIPMENT WARNINGS, ALONG WITH ASSOCIATED AURAL WARNINGS. REPEATED SEVERAL TIMES. NR 1 PNUEMATJan 12, 2014 · N686FE · Airbus A300F4605R · Pneumatic SystemSDR FDEA201401080070Windshield · arcedAT FL 350, CAPTAIN`S FRONT WINDSHIELD BEGAN TO ARC. TURN SWITCH OFF TO SECURE WINDOW. R & R WINDOW IAW AMM 56-11-11-04. OPS CHECKED TEMP CONTROL UNIT PER AMM 30-42-00,P BLOCK 501. TESTED GOOD. OPS CHECKED WINDOW HEAT PROTECTION UNIT PER AMM 30-42-00 P BLOJan 8, 2014 · N686FE · Airbus A300F4605R · Flight Compartment WindowsSDR FDEA201210053569Web · damagedMLG WHEEL WELL, LT SIDE VERTICAL KEEL BEAM WEB HAS PUNCTURE DAMAGE, APPROX 1.0 X 1.7 ADJACENT TO MLG DOOR FWD HINGE FITTING. REPAIRED DAMAGED AREA IAW EA6-5310-7-160189 FUSELAGE LT KEEL BEAM WEB AT MLG DOOR FWD HINGE REPAIR. OPS CHECK/ADJUSTMENT OF LT MLG DOct 5, 2012 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201210053558Frame · damagedDURING SB A300-57-6086 ACCOMPLISHMENT, DAMAGE FOUND IN HOLE "P" AT FRAME 47 RT SIDE. DAMAGE WAS NOTED IN THE TEE AND SPAR. REMOVED NOMINAL FASTENER FROM HOLE "P" AT FRAME 47 RT SIDE, VERIFIED DAMAGE IN UPPER 2 LAYERS (TEE AND SPAR), OVERSIZED ALL FIVE LAYERS Oct 5, 2012 · N686FE · Airbus A300F4605R · Wing SparSDR FDEA201209273482Skin · dentedRT AILERON LOWER SURFACE T/E SKIN HAS A 18.0" X 0.500" X 0.130" DEEP DENT. DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11, PB 201, PARA E. REPAIRED DENT IAW SRM 51-77-12, PARA 4 D. AND 4 A. (5). RESTORED PROTECTIVE COATING IAW SRM 51-75-10 PARA 3 A.Sep 27, 2012 · N686FE · Airbus A300F4605R · AileronsSDR FDEA201209273481Skin · dentedRT WING AILERON HAS TWO DENTS ON LOWER SURFACE. DENTS MEASURED 0.500 X 0.500 X 0.023 DEEP AND 1.00 X 1.00 X 0.019 DEEP. ONE DENT FOUND TO BE OUT OF LIMITS IAW SRM 57-61-11 PB 201, PARA E. REPAIRED BOTH DENTS IAW SRM 51-77-12 PAR 4.D. AND 4.A.(5) PAGES 292 ANSep 27, 2012 · N686FE · Airbus A300F4605R · AileronsSDR FDEA201209273474Attach Angle · crackedATTACH ANGLE FOR THE TRAILING EDGE PANEL ATTACHMENT RIB "RT" IS CRACKED .400", OFF ACFT PART. R & R UPPER ATTACH ANGLE ON RT SIDE OF HORIZONTAL STAB REAR SPAR AT RIB 5 8" IAW SRM 51-40-21. FABRICATED ATTACH ANGLE IAW SRM 55-13-11 AND DWG A55177134. LOCATED Sep 27, 2012 · N686FE · Airbus A300F4605R · Horizontal Stabilizer, Attach FittingsSDR FDEA201209263466Angle · crackedLEFT WING KREUGER FLAP WELL IN WING LE IB UPPER RIB JUST OB OF KREUGER ACTUATOR CRACKED 2.5 IN. IN THE RADIUS. REMOVED AND REPLACED REINFORCING ANGLE IAW SRM 51-40-21Sep 26, 2012 · N686FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201209203371Crossbeam · dentedUPON REMOVAL OF LT WING KRUGER FLAP 1 EA DENTED AREA APPROX 2 IN LONG WAS NOTED ON SUPPORT WEB JUST ABOVE KRUGER FLAP ACTUATOR ZONE 510. REMOVED AND REPLACED LT WING KREUGER FLAP CROSSBEAM IAW SRM 51-72-10 PG 1-3Sep 20, 2012 · N686FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA201209153331Link Assy · crackedMAIN DECK CARGO FRAME 48L BELOW SEAT TRACK 4L SUPPORT STRUCTURE ATTACHMENT LUG CRACKED ONE INCH LONG, STR 27-28. R & R DAMAGED LINK ASSY IAW SRM 51-40-21, PG 7, PARA 5.Sep 15, 2012 · N686FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201209143324Angle · crackedRIGHT WING LOWER L/E RIB 1 VERTICAL WEB STIFFENER ANGLE HAS 3 INCH CRACK. R & R RT WING L/E RIB 1 VERTICAL WEB STIFFENER IAW FSRM 51-72-10, PG 2-3.Sep 14, 2012 · N686FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201209143321Floorboard · damagedFLOORBOARD 232HG OUTER PLY CRUSHED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 14, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209143320Floorboard · damagedMAIN DECK CARGO FLOORBOARD 232YG HAS IMPACT DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 14, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209143319Floorboard · gougedMAIN DECK CARGO FLOORBOARD 242VG UPPER SURFACE GOUGED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 14, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209133308Attach Fitting · crackedMAIN DECK CARGO FR 48 BELOW SEAT TRACK 4R SUPPORT STRUCTURE ATTACHMENT LUG CRACKED 1.5" LONG. REMOVED AND REPLACED ATTACHMENT LUG PER SRM 51-72-10.Sep 13, 2012 · N686FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201209133316Floorboard · damagedMAIN DECK CARGO FLOORBOARD 231EF BETWEEN FR 18 AND FR21 SEAT TRACK , 4L & 5L HAS 6"X 1" AREA OF DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 13, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209133314Floor Panel · delaminatedAFT ACCESSORY BAY FLOOR PANEL 312BF IS DELAMINATED ON UPPER SURFACE, AFT INBD CORNER. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 13, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209123307Seat Track · damagedMAIN DECK CARGO SEAT TRACK 4R AT FRAME 37 HAS 1 EA ELONGATED SCALLOP. REMOVED DAMAGE SEAT TRACK 4R FR 36 TO 39 IAW SRM 53-10-16 PG 207 AND 208. LOCATED TRIMMED AND DRILLED SEAT TRACK SECTION AND 2 EA REPAIR SPLICES IAW SRM 53-10-16 PG 207 AND 208. INSTALLED Sep 12, 2012 · N686FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209123299Adapter · crackedCLEVIS ADAPTER AT FR21 BETWEEN SEAT TRACKS 3L AND 4L HAS .25 IN CRACK ON FWD FLANGE AND 1". CRACK ON AFT FLANGE. REMOVED CLEVIS ADAPTER IAW FSRM 51-72-10, PARA 5. LOCATED, DRILLED, AND INSTALLED NEW CLEVIS ADAPTER AT FR21 BETWEEN SEAT TRACKS 3L AND 4L IAWSep 12, 2012 · N686FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201209113293Floorboard · damagedMAIN DECK CARGO FLOORBOARD 241TH IS DEFORMED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209113292Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242ZJ DEFORMED & CRACKED 5 INCHES LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209113291Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242EK DEFORMED & CRACKED, 4 INCHES LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209113290Floorboard · damagedFLOORBOARD 242GF HAS THREE AREAS OF CRUSHED AND COMPRESSION DAMAGE AROUND CLEVIS ADAPTER CUT-OUTS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209113288Floorboard · damagedFLOORBOARD 132QG CRACKED ON LOWER SURFACE AND SIDES. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209113287Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242UJ CRACKED. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209113283Web · crackedMAIN DECK CARGO FLOOR WEB AT FR 79 RT OTBD OF FLOOR RAIL HAS .25" CRACK EXTENDING FROM LIGHTENING HOLE. R & R WEB IAW SRM 51-72-10, P1.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209113282Web · crackedMAIN DECK CARGO FLOOR WEB AT FR 79, OTBD OF FLOOR RAIL HAS 1.5 IN. CRACK FROM EDGE TO LIGHTENING HOLE. R & R FLOOR WEB AFT OF FR 79 STR 26 LT IAW SRM 51-40-21, PARA 7 AND SRM 51-72-10, PG 2.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209103277Floorboard · damagedFLOORBOARD 232NG TOP SKIN HAS IMPACT DAMAGE. FABRICATED FLOORBOARD IAW SRZ 25-005, REV J.Sep 10, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209103276Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242RH IS CRACKED. FABRICATED FLOORBOARD IAW 25-005, REV J.Sep 10, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209103275Floorboard · damagedFLOORBOARD 131NG CRACKED ON LOWER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 10, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209103274Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 252 BF UPPER SURFACE GOUGED AT 3 EA AFT CLEVIS ADAPTER CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 10, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209093266Web · bentTHS COMPARTMENT BETWEEN FR 86 AND FR 87 S33R WEB UPPER STIFFNER IS DEFORMED /BENT. REMOVED AND INSTALLED NEW WEB AND STIFFNER IN THS COMPARTMENT BETWEEN FR 86 AND FR 87 AT STGR 33R IAW SRM 51-40-21 PAR 6 AND 7.Sep 9, 2012 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209093265Floorboard · damagedMAIN DECK CARGO FLOORBOARD 242RG IS CRUSHED AT CLEVIS CUTOUT BETWEEN FR 54 AND FR 54.2 AND SEAT TRACKS 2R AND 3R. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 9, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209093264Floorboard · crackedFLOORBOARD 131SG CRACKED ON LOWER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 9, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209093263Floor Panel · gougedMAIN DECK CARGO FLOOR PANEL 252GF UPPER SURFACE GOUGED AT 3EA AFT CLEVIS ADAPTER CUTOUTS. MEASURED 10 SQ IN, 10 SQ IN, AND 5 SQ IN, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV. J.Sep 9, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209093262Floorboard · damagedMAIN DECK CARGO FLOORBOARD 251PH IS DEFORMED AND HAS PUNCTURES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 9, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209093261Floorboard · damagedMAIN DECK CARGO FLOORBOARD 251RG IS DEFORMED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 9, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209073255Skin · chafedLEFT WING OUTER FLAP INBD SIDE L/E CHAFED MARK APPROX LENGTH IS 1 INCH AND WIDTH IS 0.50 REF AMM 27-00-00-06, ZONE 580. REPAIRED WING OUTER FLAP IAW A300-600 FSRM 57-50-00 PARA 4.H. PG 231 THRU 233 AND FIG 208 AND EA 6-5750-160186 PT. 1.Sep 7, 2012 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201209073254Floorboard · crackedMAIN DECK CARGO FLOORBOARD 251DF CRACKED, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 7, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209073253Floorboard · gougedFLOORBOARD 252UH UPPER SURFACE GOUGED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 7, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor Panel
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