N669FE

Service difficulty reports · 320

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 = 'N669FE' 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 07FDEA01060Seat Track · corrodedMAIN CABIN SEAT TRACK CORROSION SEVERAL AREAS BETWEEN FRAME 38.2 AND 40, LBL 57. BLENDED AREAS OF CORROSION IAW A300-600 SRM 51-22-00. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. RECEIVED NEW SEAT TRACK, PO NR 566271.1. REMOVED AND REPLACED SEAT TMar 21, 2007 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00892Seat Track · corrodedMAIN CARGO DECK SEAT TRACK ADAPTER AT FR61/Y-1456 IS CRACKED REMOVED SEAT TRACK ADAPTER AT FR 61,Y-1456 REF TO A300-600 SRM 51-40-21 PARAGRAPH 7 LOCATED AND DRILLED NEW SEAT TRACK ADAPTER REF TO A300600 SRM 51-40-44 PAR 2. ALODINED, PRIMED NEW SEAT TRACK ADAPMar 15, 2007 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00886Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED IN AREAS FROM FRAME 40 TO FRAME 45 RBL 77. REMOVED CORROSION ORIGINAL THICKNESS .145 REMOVED .033 REMAINING MAT IS .112. FOUND TO BE OUT OF LIMITS IAW A300-600 53-10-16 TOOL NR TWS 58329B. REMOVED SEAT TRACK IAW FEDEX A300-600Mar 15, 2007 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00805Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED OVER FS 15A AT BL Y593 REMOVED CORROSION IAW A300-600 SRM 51-74-10, SEAT TRACK FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16 FIG 101. REMOVED AND REPLACED SEAT TRACK P/N A53612524200 IAW A300-600 SRM 51-40-21, PO 565252.1.Mar 13, 2007 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00798Seat Track · gougedCABIN SEAT TRACK GOUGED BETWEEN FR 40-50 LBL 18 REPLACED SEAT TRACK FROM FR40 TO FR54 AT LBL18 IAW AIRBUS DWG A53812912. TREATED SEAT TRACK IAW FEDEX A300-600 SRM 51-21-10, PO NR 564624.4.Mar 13, 2007 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00745Seat Track · corrodedCABIN SEAT TRACK CORRODED BETWEEN FR 54.1 AND 54.2 LBL18 REMOVED CORROSION ON SEAT TRACK FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16 FIG 102. REMOVED CORRODED (DAMAGED) SEAT TRACK, RECEIVED NEW SEAT TRACK SECTION AND INSTALLED IAW A300-600 SRM 51-40Mar 12, 2007 · N669FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA00645Floorbeam · corrodedMAIN CARGO COMPT FLOORBEAM AT FRAME 62, 32 RIGHT OF B/L SUPPORT ANGLE HAS CORROSION AROUND FASTENER HOLES. REMOVED AND REPLACED ADAPTER SEAT TRACK.Mar 4, 2007 · N669FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA00644Crossbeam · corrodedMAIN CABIN ADAPTER TRACK CORRODED FRAME 48 RBL 32 REMOVED CORROSION IAW A300-600 SRM 51-22-10. ORIGINAL SCALLOP OPENING 0.421 IAW A300-600 SRM 53-15-15 FIG 9 AND A300-600 SRM 51-31-20 FIG 36. REMAINING SCALLOP OPENING .475 FOUND TO BE OUT OF LIMITS IAW A300-Mar 4, 2007 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 07FDEA00643Adapter · corrodedFOUND MAIN CABIN ADAPTER TRACK CORRODED FRAME 36 RBL32. REMOVED AND REPLACED ADAPTER TRACK.Mar 4, 2007 · N669FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 05FDEA03268Pitot Tube · contaminatedON TAKEOFF ROLL FROM KMSP F/O`S PFD AIRSPEED FROZEN. REJECTED TAKEOFF, RETURNED TO RAMP. FOUND A BUGS NEST OF DIRT AND DEBRIS IN THE PITOT TUBE, CLEANED OUT PITOT TUBE AND PERFORMED AIRSPEED TEST WITH PITOT STATIC TEST BOX PER M/M 34-10-00-5, ALL SYSTEMS COct 7, 2005 · N669FE · Airbus A300F4605R · Pitot/Static SystemSDR 04FDEA02984Warning Light · illuminatedPDIS 669 78-30 0007382 23OCT04 MEM CLOSE U LOGPAGES: 00926331 CLEARED FOR TAKE-OFF , STABILIZED ENGINES AT 40 PERE NT N1, THEN APPLIED TAKEOFF POWER. ALMOST IMMDEIATLY RECIEVED AMBER ECAM NR1 ENG REV PRESSURIZED REJECTED TAKEOFF AND RETURNED TO GATE. Oct 23, 2004 · N669FE · Airbus A300* · Engine Thrust ReverserSDR 04FDEA02193Smoke Detector · inoperativeAFTER T/O AFT AND BULK SMOKE ECAM ALERT, AIRBORNE ABORT BACK TO MEM, FOLLOWED ECAM PROCEDURES. ENT BY: 029496 RPT BY: 118583 MEL 26-16-01: FWD, AFT AND BULK) ALL SMOKE DETECTION SYSTEMS INOP. NO CARGO IS TO BE CARRIED WITH AFFECTED LOWER DECK COMPARTMENTS. Jul 26, 2004 · N669FE · Airbus A300F4605R · Fire DetectionSDR 04FDEA01254Actuator · failedDURING FLAP/SLAT RETRACTION AFTER TAKEOFF, SYSTEM 1 & 2 RUDDER TRAVEL FAULT LIGHTS ILLUMINATED. SELECTED BOTH OFF, WAITED ONE MINUTE AND TRIED RE-SET. LIGHTS RE-ILLUMINATED SELECTED BOTH SWITCHES OFF. FAULT LIGHTS STAYED OUT. FOLLOWED QRH AND RETURNED TO May 13, 2004 · N669FE · Airbus A300F4605R · Rudder Control SystemSDR 02FDEA00985Rib · gougedLEFT WING MAIN LANDING GEAR, RIB 5 HOLE NR 52 IS GOUGED. REMOVED AND REPLACED.Dec 18, 2002 · N669FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR 02FDEA00984Rib · gougedRIGHT WING MAIN LANDING GEAR RIB 5 HOLE NR 47 GOUGED. REMOVED AND REPLACED IAW SRM.Dec 18, 2002 · N669FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR 02FDEA00983Rib · gougedLEFT WING, MAIN LANDING GEAR RIB 5 HOLE NR 52, GOUGED.Dec 18, 2002 · N669FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR 01FDEA00760Generator · failedCLIMBING OVER ATLANTIC OCEAN INTO LINE OF THUNDERSTORMS WITH NR 2 GEN ALREADY INOP. AT ABOUT FL 200 APU GEN FAULTED & W/N RESET, ELECTED TO RETURN TO FLL.Aug 22, 2001 · N669FE · Airbus A300F4605R · AC Generator-AlternatorSDR 99FDEA00513Thrust Reverser · inoperativeON T/O, ECAM SOUNDED AND DISPLAY NR 2 REV PRESSURIZED. THROTTLE PLACED AT IDLE, RETURN TO DEPART. T/REV DEFERRED PER MEL 78-1 NR 2 REVERSER LOCKED OUT.Dec 28, 1999 · N669FE · Airbus A300F4605R · Engine Thrust ReverserSDR 98FDEA00751Tr Unit · inop98-304 DURING T/O ROLL, RECEIVED ECAM WARN NR 1 ENG REVERSER PRESS. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POS PER M PROC 78.1.Dec 21, 1998 · N669FE · Airbus A300F4605R · Engine Thrust ReverserSDR 96FDEA01389Tcc · malfunctionedAFTER TAKEOFF AT CLIMBOUT OF 9000 MSL, FUEL FLOW FLUX BOTH ENGINES, RETURN TO SALT LAKE. REMOVED AND REPLACED TRP PER M/M 22-35-12. ALSO, REMOVED AND REPLACED TCC PER M/M 22-36-34 ALL AFS/LANDS TEST GOOD. A/C REMAINS CAT II THIS ITEM CLOSES 22-30/1131 AND 7Aug 21, 1996 · N669FE · Airbus A300F4605R · Auto Throttle System
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