N653FE

Service difficulty reports · 221

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 = 'N653FE' 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 07FDEA02882Seat Track · gougedFUSELAGE MAIN DECK SEAT TRACK 2L GOUGED ON I/B FLANGE, AROUND 7 FASTENER HOLES BETWEEN FRAMES 43-47. REF A300-600 SRM 51-10-00 TOTAL AREA GOUGED 7 INCH APPROX BY 0.010 DEEP. BLENDED GOUGES IAW A300-600 SRM 51-73-10. SEAT TRACK OUT OF LIMITS IAW A300-600 SRMAug 14, 2007 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02881Seat Track · wornFUSELAGE MAIN DECK SEAT TRACK 5L I/B FLANG PANEL LANDING HAS WEAK AROUND 7 EA FASTENER HOLES BETWEEN FRAMES 47-51 (ZONE 240) REF A300-600 SRM 51-10-00. BLENDED 7 AREAS AT LT 5L FR47-51 IAW A300-600 SRM 51-73-10. AFTER REWORK ALL 7 AREAS WERE OUT OF LIMITS IAAug 14, 2007 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02875Seat Track · corrodedSEAT TRACK 2R AT FR 78 AND FR75 HAS 1 SQ IN OF CORROSION EACH ZONE 260 REF A300-600 SRM 51-10-00. REMOVED CORRODED FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. CUT OUT SECTION OF SEAT TRACK IAW A300-600 SRM 53-10-16 FIG 201. INSTALLED NEW REPAIR SECAug 14, 2007 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02874Frame · dentedFWD CARGO DOOR CUT-OUT STRUCTURE FR 20 HAS INCOMING CONDITION IMPACT DENT ON FRAME W/APPROX SIZE 4-IN LONG BY 2-IN WIDTH BY 0.25 DEPTH. (REF A300-600 AMM 53-13-11-6) SRM 53-10-13. CUT OUT DAMAGED SECTION AND DRILLED UP, REPAIR SECTION AND INSTALLED IAW FEDEX Aug 14, 2007 · N653FE · Airbus A300F4605R · Fuselage Main, FrameSDR 07FDEA02873Seat Track · gougedMDCC AT FR22 BETWEEN STG 9R AND 8R HAS 1 EA GOUGE APPROX 1" ZONE 230 REF A300-600 SRM 51-10-00. REMOVED DAMAGE FRAME SPLICE PER A300-600 SRM 51-40-21. CUT OUT CRACKED FRAME INNER FLANGE AND INSTALLED REPAIR SPLICE PER FEDEX EA 6-5310-110521.Aug 14, 2007 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02654Angle · gougedMDCC AT FR 24 BETWEEN STG 11R AND 15R HAS 4 EA GOUGES APPROX 4 " ZONE 230 REF A300- 600 SRM 51-10-00. BLENDED GOUGES (4EA) FR 24 BETWEEN STR 11R AND 15R IAW A300 SRM 51-73-10 1 EA AREA OUT OF LIMITS IAW A300 SRM 53-10-00 PG 101 B=.63 A=0.50 L= .013. FABRICAJul 28, 2007 · N653FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 07FDEA02653Floorbeam · crackedFLOORBEAM FRAME 31 BETWEEN SEAT TRACKS NR L4 AND NR 5L HAS A .5 INCH CRACK AT STIFFENER. CUT OUT CRACKED SECTION OF FLOORBEAM IAW A300-600 FREIGHTER SRM 53-10-15. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW A 300-600 FREIGHTER SRM 53-10-15. ALODINEJul 28, 2007 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA02631Seat Track · corrodedCOURIER AREA FR 16A- FR 18 SEAT TRACK 3L 20 SQ IN CORROSION REF A300-600 AMM 53-12-00-6 ZONE 230. REMOVED CORROSION ON L3 SEAT TRACK. WENT OUT OF LIMITS IAW A300-600 SRM 53-10-16. REPAIR SEAT TRACK IAW A300-600 SRM 53-12-16. PRIMED AND TREATED PARTS IAW A3Jul 26, 2007 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02630Seat Track · gougedFUSELAGE MAIN DECK SEAT TRACK 2L GOUGED ON I/B FLANGE, AROUND 6 FASTENER HOLES BETWEEN FRAMES 47-51 (ZONE 240) REF A300-600 SRM 51-10-00 TOTAL AREA GOUGED 6 INCHES APPROX. BY .010 DEEP. BLENDED DAMAGE PER A300-600 SRM 51-73-10 AND FOUND TO BE OUT OF LIMITS PJul 26, 2007 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02629Seat Track · corrodedMDCC SEAT TRACK L5 FR 19-FR 24 18 SQ IN CORROSION INBOARD FLANGE IN AND AROUND FASTENER HOLES REF A300-600 AMM 53-13-11-6 ZONE 230. CLEAN CORROSION IAW A300-600 SRM 51-74-10. CHECK LIMITS PER A300-600 SRM 53-10-16 OUT OF LIMITS. FAB REPAIR PART PER A300-600Jul 26, 2007 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02628Floorbeam · crackedFWD CARGO COMPT CEILING, CABIN FLOORBEAM C-27 HAS A CRACK ON FWD FACE VERTICAL FORMED SECTION, BETWEEN RT SEAT TRACK 2-3 WITH APPROX 0.25 IN LONG REF A300-600 SRM 51-10-10. CLEAN OUT CRACK IN FLOORBEAM IAW A300-600 SRM 53-10-15. FAB`D REPAIR ANGLE AND FILLERJul 26, 2007 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 06FDEA03823Pitot Tube · failedRTO NO F/O AIRSPEED ON PFD. A/C RETURNED TO BLOCKS DUE TO NO AIRSPEED INDICATION ON F/O'S PFD. BLEW OUT PITOT TUBE FOR F/O AIRSPEED PER MM 34-11-15-6, NO DEFECTS NOTED. USED PITOT TESTER TO VERIFIY SPEED TAPE ON FO,S PFD OPERATED NORMALLY PER MM 34-11-1Nov 2, 2006 · N653FE · Airbus A300F4605R · Pitot/Static SystemSDR 05FDEA01364Battery · failedEMERGENCY LIGHT POWER SUPPLY FAILED TEST PER 33-51-14 (NR#N0060, W/O NR 28630). REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERY IAW MM 33-51-14 TEST OF EMERGENCY LIGHTS GOOD IAW MM 33-51-14 (NR#N0060, W/O#28630)May 18, 2005 · N653FE · Airbus A300F4605R · Emergency LightingSDR 05FDEA01344Acoustic Panel · dentedCOMPLY WITH EA 6-7110-55485 POWER PLANT-INLET COWL NR 1 ENGINE ACOUSTIC PANEL DENT REPAIR. REPAIRED AREA PER EA 6-7110-55485.May 17, 2005 · N653FE · Airbus A300F4605R · Engine Air Intake SystemSDR 05FDEA01255Shroud · crackedPYLON NR 1 SHROUD/PAN, UNDER THE ENGINE BLEED AIR DUCT, IS CRACKED. VIEWED THRU ACCESS PANEL 413EL. REMOVED CRACKED SHROUD, FAB NEW SHROUD ON TR T5/517007 301-25 .025SS BATCH 0000887337, INSTALLED SHROUD IAW SRM 51-4-21.May 12, 2005 · N653FE · Airbus A300B4605R · Nacelle/Pylon Miscellaneous StructureSDR 05FDEA00628Control Panel · malfunctionedWHEN SPEED BRAKES WERE DEPLOYED, ALL SPOILERS DEPLOYED EXCEPT NR 6 AND NR 7 ON THE RIGHT WING THIS CAUSED A WING ROCK THAT IN TURNED CAUSED THE PLANE TO START A 10 DEGREE BANK. FOUND LT NR 5 SPOILER ONLY ATTACHED AT ACT CONNECTION. REPLACED SPOILER PANEL, Feb 20, 2005 · N653FE · Airbus A300* · Drag Control SystemSDR 05FDEA00052Idg · failedON INITIAL T/O ROLL NR 2 GEN FAULTED. T/O WAS REJECTED AT 70 KTS ESTIMATED. GENERATOR WAS RESET, VOLTS AND FREQS APPEARED NORMAL. SECOND T/O WAS ATTEMPTED GENERATOR FAILED AGAIN ON INITIAL T/O ROLL, IDG 2 FAULT LIGHT WAS FLUCUATING ON AND OFF. RELEASED FOJan 7, 2005 · N653FE · Airbus A300B4605R · Alternator-Generator DriveSDR 04FDEA03458Thrust Reverser · malfunctionedON TAKEOFF RWY 6 KBDL- NR 1 ENGINE REV PRESSURIZED LIGHT CAME ON AT 70 KNOTS, ENGINE N1 APPROX 75 PERCENT. REJECTED TAKEOFF AT 72 KNOTS. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 31DEC04 MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NRDec 21, 2004 · N653FE · Airbus A300F4605R · Engine Thrust ReverserSDR 98FDEA00546Detector · failedAVIONICS SMOKE ECAM AND CRG AT 1500 FT AFTER T/O. NO ODOR WITH SNIFFER OR SMOKE IN COCKPIT. WARNING CONTINUED, DECLARED EMERGENCY AND RETURNED FOR LANDING. NOT OVERWEIGHT. NOTICED SLIGHT ELECTRICAL SMELL IN CABIN AFTER SHUTDOWN. FOUND SMOKE DETECTOR FAILESep 3, 1998 · N653FE · Airbus A300* · Smoke DetectionSDR 96FDEA00717Panel · missingLT WING I/B FLAP FAIRING I/B SIDE DAMAGED. PANEL 416AR TORN LOOSE FROM NR 1 ENG PYLON. PANEL EXITED A/C AND STRUCK TO LT WING I/B FLAP FAIRING. REPLACED MISSING PYLON PANEL, RELEASED FLAP FAIRING PER CDL 27-1. REMOVED MOVEABLE FLAP TRACK FAIRINGS FROM LT NMar 29, 1996 · N653FE · Airbus A300F4605R · Nacelle/Pylon, Plate/SkinSDR 95FDEA01902Nr 1 Fire Squib · malfunctionedNR 2 ENGINE FIRE LIGHT, ECAM AND BELL ON LANDING AT EWR. AFTER PHASE I ITEMS COMPLETED, FIRE LIGHT CAME ON AGAIN IN HANDLE. DISCHARGED AGENT AND SECURED ENG. REMOVED AND REPLACED NR 2 ENGINE, NR 1 FIRE EXTINGUISHER BOTTLE PER MM 26-21-15, AFTER NR 1 FIRE BODec 20, 1995 · N653FE · Airbus A300F4605R · Fire Detection
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