N667FE

Service difficulty reports · 237

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 = 'N667FE' 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 08FDEA04421Seat Track · crackedTHE MAIN CABIN SEAT TRACK SUPPORT FITTING AT FRAME 48, STA 3036, RBL 48 IS CRACKED.Oct 17, 2008 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04405Floorbeam · crackedAFT PIT AT FRAME C 62, LBL 32, THE FLOOR ANGLE SUPPORT IS CRACKED.Oct 17, 2008 · N667FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA04359Channel · crackedMAIN BATTERY INBD SUPPORT CHANNEL IS CRACKED AT THE CENTER ATTACH POINT. REMOVED CRACKED SUPPORT CHANNEL IAW SRM 51-40-21. LOCATED & DRILLED NEW SUPPORT CHANNEL IAW SRM 51-40-11. INSTALLED NEW SUPPORT CHANNEL IAW SRM 51-40-21.Oct 15, 2008 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA04358Channel · crackedMAIN BATTERY OTBD SUPPORT CHANNEL IS CRACKED AT THE CENTER ATTACH POINT. REMOVED BATTERY TRAY CANOPY; CRACKED SUPPORT CHANNEL & 4 EA CLIPS IAW SRM 51-40-21. LOCATED & DRILLED NEW CHANNEL IAW SRM 51-40-44. INSTALLED NEW CHANNEL 4 CLIPS & BATTERY TRAY CANOOct 15, 2008 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA04357Angle · corrodedLEFT TRANSITION ANGLE IN THE BULK PIT IS CORRODED FROM FRAME 64 TO 67.Oct 15, 2008 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA04326Attach Fitting · crackedBULK CARGO DOOR INTERNAL LATCH ATTACHED FITTING FWD & AFT SIDE IS CRACKED. REMOVED CRACKED FITTING IAW SRM 51-40-21. LOCATED & DRILLED FITTING IAW DWG 17A52378079. INSTALLED NEW FITTING P/N A523780790200 IAW SRM 51-40-21. REMOVED & RE-INSTALLED LATCH Oct 13, 2008 · N667FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 07FDEA05021Valve · malfunctionedECAM DISPLAYED NR 2 ENG REVERSER PRESSURIZED ON TAKEOFF ROLL. WARNING WENT AWAY WHEN POWER WAS RETARDED. RTO LESS THAN 80KTS. MEL 09DEC07 15:05. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A. THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FDec 9, 2007 · N667FE · Airbus A300F4605R · Engine Thrust ReverserSDR 07FDEA02661Panel · misalignedFL 390 LEFT MAIN CABIN DOOR ALARM AND LIGHT FLASHING, ADV BY JUMPSEAT, RT INDICATOR BETWEEN LOCK AND UNLOCK. DOOR ALARM OFF IN DESCENT BELOW FL 200/PRESSURE DIF.6.7 CABIN AT 3300' NO ECAM INDICATIONS FOR THE LEFT CABIN UNLOCKED. FOUND COVER PANEL OF DOOR (IJul 29, 2007 · N667FE · Airbus A300F4605R · Passenger/Crew DoorsSDR 07FDEA01660Engine · bird ingestionHIGH SPEED REJECT CLE 24L AT 135 KTS. A SEAGULL WENT IN THE NR 2 ENG FOLLOWED BY A HEAVY VIBRATION. NR 2 ENG INDICATIONS APPEARED NORMAL AFTER STOPPING THE AIRCRAFT. [SUP 05-04-07] REPLACED 5 EA. 1ST. STG. FAN BLADES PER MM 72-21-00-4-05. SPINNER STILLApr 29, 2007 · N667FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 04FDEA03013Seat Track · corrodedAREAS OF CORROSION ON SCALLOP HOLES NR 3 LEFT SEAT TRACK AS MARKED. REMOVED AND REPLACED SEAT TRACK SECTION IAW A300-600 SRM 51-72-10 AND 51-40-21.Nov 3, 2004 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03009Seat Track · corrodedMDCC TRACK 3 R SECTION 27 INCHES TO RT OF CTR BETWEEN FR 74 AND FR 80 HAS 3 EACH AREAS OF CORROSION. (1) FR 74, (2) FR77, (3) FR 78, WHILE WORKING CORROSION FOUND 4EA ADDITIONAL AREAS OF CORROSION, REQUIRE REMOVAL AND EVACUATE. REMOVED AND REPLACED SEAT TRACNov 1, 2004 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03008Seat Track · corrodedMCD FR 15 NR 2 LT SEAT TRACK HAS 1 AREA OF CORROSION SCALLOP HOLES AND ON NR 2 RT SEAT TRACK WITH 1 AREA OF CORROSION ON SCALLOP HOLES AS MARKED. REMOVED CORROSION ON NR 2 LT SEAT TRACK AND NR 2 RT SEAT TRACK, FOUND TO BE OUT OF LIMITS ON (2EA) TRACKS. REMOVNov 1, 2004 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03007Seat Track · corrodedFROM NR N00373 MCD FR 18, NR 3 RT SEAT TRACK HAS 1 AREA OF CORROSION ON SCALLOP HOLES AS MARKED. REPAIRED SEAT TRACK AT FR 18, NR 3, RT SIDE IAW SRM 53-12-16 BY CUTTING OUT OLD SECTION AND SPLICING NEW SECTION.Nov 1, 2004 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03006Seat Track · corrodedRT FR 40 TO 54, SEAT TRACK NR 3R HAS 8 AREAS OF CORROSION. REMOVED AND REPLACED SEAT TRACK RAIL AT MDC RT FR 40 TO 44.5 NR 3 R IAW SRM 51-72-10.Nov 1, 2004 · N667FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03005Seat Track · corrodedMAIN CARGO DECK NR 2 DUMMY SEAT TRACK BETWEEN FR 54.0 TO 54.1 HAS 3 INCHES OF CORROSION .050 INCH DEEP. TRACK IS OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK IAW A300-600 SRM 51-72-10.Nov 1, 2004 · N667FE · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03003Seat Track · corrodedMDCC ZONE 260 15 INCHES TO RT OF CTR TRACK 2R BETWEEN FR 72 AND 80 HAS 2EA AREA OF CORROSION AT (1) FR 77 (2) 10 INCHES AFT OF FR76. WHILE WORKING AREA OF CORROSION FOUND 6 EACH MORE AREAS OF CORROSION. REPAIRED SEAT TRACK BY REMOVING DAMAGED SECTION AND SPLOct 30, 2004 · N667FE · Airbus A300B4605R · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02985Adapter · corrodedRT FR.41-42, BETWEEN SEAT TRACKS NR 2 AND 3, CLS ADAPTER TRACK HAS CORROSION AT BOTH ENDS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED CLS ADAPTER IAW SRM 51-72-10.Oct 23, 2004 · N667FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 03FDEA02243Actuator · failedON LANDING AT YMX COCKPIT AND COURRIER AREA FILLED WITH SMOKE AND MAIN DECK CARGO SMOKE DET SYSTEM ACTIVATED IN ALL ZONES. SMOKED CLEARED AFTER 5 MIN. SUSPECT EXHAUST FUMES ENTERED AIR CONDITIONING SYS, RELEASED FOR SERVICE PER MEL/CDL: 21-11-08-B MEL 21-Dec 24, 2003 · N667FE · Airbus A300F4605R · Cabin Cooling SystemSDR 02FDEA00804Skin · chafedRT I/B UPPER FLAP HAS 2 CHAFE MARKS 0.009 & 0.011 DEEP, 1.5 INCHES APART 77 INCHES FROM I/B SIDE. R/R FLAP.Nov 5, 2002 · N667FE · Airbus A300F4605R · Trailing Edge FlapsSDR 02FDEA00377Pitot Tube · obstructedPDIS- ON TAKEOFF AT 80 KNOTS CALL BY 1ST OFF, CAPT'S AIRSPEED IND STILL READ ZERO (NO TREND). REMOVED BUG FROM PITOT TUBE, OPS CHECK PITOT SYSTEM PER MM 34-10-00-5.Jun 4, 2002 · N667FE · Airbus A300F4605R · Pitot/Static SystemSDR 01FDEA00203Computer · faultyON T/O ECAM WENT CRAZY, GALLEY SHED ON, NR 1 PITCH TRIM DISCONNECTED AND WOULD NOT RESET, NR 1 PRESSURE REG FAILED, POS 1 LAND GEAR INOP, ACARS RINGER INOP, NR 1 FLT DIRECTOR INOP. APU LOOP-B FAULT.Mar 15, 2001 · N667FE · Airbus A300F4605R · Central ComputersSDR 01FDEA00202Computer · faultyON T/O ECAM WENT CRAZY, GALLEY SHED ON, NR 1 PITCH TRIM DISCONNECTED AND WOULD NOT RESET. NR 1 PRESS REG FAILED. POS 1 LAND GEAR INOP, ACARS RINGER INOP, NR 1 FLT DIR INOP, APU LOOP-B FAULT.Mar 15, 2001 · N667FE · Airbus A300F4605R · Central ComputersSDR 01FDEA00111Landing Gear · failedLANDING GEAR WOULD NOT RETRACT AFT T/O FROM MCI EITHER IN POS DET SYS 1 OR 2.Feb 10, 2001 · N667FE · Airbus A300F4605R · Main Landing GearSDR 00FDEA00215Indicator · reads lowNR 1 AIRSPEED IND IS THIRTY KNOTS LESS THAN NUMBER 2 ON T/O ROLL. FOUND BLOCKAGE IN CAPT PITOT PROBE. CLEARED BLOCKAGE MATERIAL. TESTED CAPT PITOT SYS PER AMM 34-10-00. ALL IND NORMAL.Apr 11, 2000 · N667FE · Airbus A300F4605R · Airspeed/Mach IndicatorSDR 00FDEA00207Smoke Detector · activatedUPPER DECK SMOKE IND IN COCKPIT PRIOR TO BLOCKOUT APU BLD AIR SEL.Apr 2, 2000 · N667FE · Airbus A300F4605R · Smoke DetectionSDR 00FDEA00186Smoke · detectedON FINAL AVIONICS SMOKE IN COCKPIT. SMOKE CLEAR AFT ENG SHUT DOWN.Mar 28, 2000 · N667FE · Airbus A300F4605R · Air Distribution SystemSDR 00FDEA00185Thrust Reverser · malfunctionedAT 90-100 KTS ABORTED T/O DUE TO NR 2 THRUST REVERSER PRESSURIZED (SINGLE CHIME). REVERSER DEACTIVATED PER MEL 78.1.Mar 28, 2000 · N667FE · Airbus A300F4605R · Engine Thrust ReverserSDR 00FDEA00146Warning Light · illuminatedON T/O LEFT ECAM DISPLAY NR 2 REVERSER PRESSURIZED WARNING.Mar 14, 2000 · N667FE · Airbus A300F4605R · Engine Thrust ReverserSDR 00FDEA00091Smoke · detectedDURING OFF LOADING, SMOKE COMING OUT OF CEILING PNL IN LWR AFT CARGO.Feb 20, 2000 · N667FE · Airbus A300F4605R · Air Distribution SystemSDR 99FDEA00036Connector · inopNR 1 REV NOT STOWED, ECAM WARNING WITH THROTTLE ENG ROLL BACK DURING CRUISE. DIVERT TO DEN. SLIGHT VIB ASSOCIATED WITH IND. REVERSER PREV DEACTIVATE PER MEL 36-3. FOUND CANNON PLUGS REMOVED FROM CDU. CANNON PLUGS NOT REMOVED FROM DIRECT PILOT VALVE AND PRFeb 3, 1999 · N667FE · Airbus A300F4605R · Engine Thrust ReverserSDR 98FDEA00710Module · failedNR 3 BATTERY STRONG ODOR PRESENT, BATTERY INDICATED AMBER, THEN OFF. REMOVED AND REPLACED DIODE MODULES 64VD AND 65VD.Nov 20, 1998 · N667FE · Airbus A300F4605R · DC Generating SystemSDR 98FDEA00301Pitot Tube · malfunction98-0108 - WRI 34-14-02232: CAPTAINS PFD AIRSPEED INDICATOR DOES NOT OPERATE. NO INDICATION ON T/O ROLL. TAKEOFF ABORTED. REMOVED AND REPLACED CAPTAINS PITOT TUBE, PITOT LEAK CHECK OK. NR 3 EFIS CONTROL SYS OK. CLEARED MEL 34-7.Apr 28, 1998 · N667FE · Airbus A300F4605R · Pitot/Static SystemSDR 98FDEA00300Adc · malfunction98-0107 - WRI 34-14-2231:CAPTAINS PFD DISPLAY HAS NO AIRSPEED INDICATION DURING TAKEOFF ROLL. T/O ABORTED. ALL OTHER AIRSPEED INDICATORS WERE NORMAL. REMOVED AND REPLACED THE NR 1 ADC. SWAPPED NR 1 AND NR 3 EFIS SGU'S. A/C DOWNGRADED TO CHECK CAT 2. NR 3Apr 28, 1998 · N667FE · Airbus A300F4605R · Air Data ComputerSDR 98FDEA00296Static Line · dirtyABORTED TAKEOFF FOR LOSS OF AIRSPEED INDICATION ON THE CAPTAINS SIDE. ABORTED AT 120 KNOTS. CHECKED NUMBER 1 ADC, BLEW OUT STATIC LINE WITH NITROGEN, PITOT/STATIC CK OK.Apr 25, 1998 · N667FE · Airbus A300F4605R · Pitot/Static SystemSDR 98FDEA00261Computer · failedNR 2 THROTTLE CONTINUES TO ROLL BACK ON ROTATION APPZ 1 THROTTLE WIDTH OK REST OF FLIGHT. TROUBLESHOT PER TSM 73-00-30 PG 105 FIG 103 NO THROTTLE VALID FAULT CODE CHECKED THROTTLE CONTROL EFFORT IAW M/M 76-11-00, DISPLACEMENT EFFORT NORMAL. REMOVED AND REPLAApr 9, 1998 · N667FE · Airbus A300F4605R · Engine ControlsSDR 98FDEA00256Ecu · malfunctionedAT ROTATION, NR 2 ENGINE AND THROTTLE BEGAN TO ROLL BACK. NOTICED FLUX BUT ON PUSHING NR 2 THROTTLE BACK UP, ENGINE RETURNED TO NORMAL. REMOVED AND REPLACED NR 2 ENGINE ECU PER M/M 73-21-01-4. RAN NR 2 ENGINE PER JRH AND M/M 71-00-00-5. POWER ASSURANCE CHEApr 8, 1998 · N667FE · Airbus A300F4605R · Fuel Control/Turbine EnginesSDR 97FDEA00236Buss Bar · malfunctionA/C INFLIGHT ELECTRICAL POWER FAILURE CAUSING 6,1 AND 4 SPOILER FAULT. NR 2 ENGINE OIL PRESSURE INDICATION LOSS, AND SHUTDOWN OF THE NR 2 ENGINE. REMOVED AND REPLACED 231 XD (FOUND TRIPPED AND BUSS BAR WEAK) PER M/M 24-00-00. PERFORMED ENGINE GROUND RUN PERApr 17, 1997 · N667FE · Airbus A300F4605R · AC Power Distribution System
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