N656FE

Service difficulty reports · 243

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 = 'N656FE' 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 FDEA201108243451Thrust Reverser · inoperativeNR 2 ENGINE THRUST REVERSER "UNLOCKED" ECAM ILLUMINATED ON TAKEOFF AT 90 KTS, REJECTED TAKEOFF. PERFORMED CDU POSITION SWITCH MODULE FUNCTIONAL CHECK, NO DEFECTS NOTED. CHECKED LT AND RT TRANS GAPS, ALL IN LIMITS PER MM 78-31-00-05. CW CDU INSPECTION PER MMAug 24, 2011 · N656FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201006262199Proximity Sensor · malfunctionedAFTER TAKE OFF, GEAR SELECTED UP IN POSTION 2, MLG HANDLE WOULD NOT GO PAST NEUTRAL POSITION. SWITCHED TO POSITION 1 AND POSITIONED HANDLE TO UP AND LOCKED. BUT RT MAIN GEAR SHOWED DOOR LIGHT AND UNLOCK ON FWD INDICATOR. ALSO AT THAT TIME PITCH TRIM 2 TRIJun 26, 2010 · N656FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201003220958Sequence Valve · malfunctionedUNSAFE RT MAIN ON TAKEOFF GEAR RETARDATION. ON BOTH OVERHEAD AND PANEL- LOWER GEAR. GOOD INDICATIONS- LANDED NO PROBLEM. FOUND FAULT CODES 63 AND 70. R & R PROX BOX REF AMM 32-31-71-4. R & R RT GEAR SEQUENCE VALVE. REPLACED RT MAIN GEAR RESTRICTOR VALVE. REMMar 22, 2010 · N656FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201003130959Uplock · malfunctionedUNSAFE RT MAIN ON TAKEOFF GEAR RETARDATION. ON BOTH OVERHEAD AND PANEL- LOWER GEAR. GOOD INDICATIONS LANDED NO PROBLEM. FOUND FAULT CODES 63 AND 70. R & R PROX BOX REF AMM 32-31-71-4. R & R RT GEAR SEQUENCE VALVE. REPLACED RT MAIN GEAR RESTRICTOR VALVE. REMMar 13, 2010 · N656FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201003130809Sequence Valve · malfunctionedON TAKEOFF, GEAR RETARDATION ON BOTH OVERHEAD AND PANEL- LOWER GEAR. GOOD INDICATIONS EVERYWHERE- LANDED NO PROBLEM. FOUND FAULT CODES 63 AND 70. REMOVED AND REPLACED PROX BOX REF A300 AMM 32-31-71-4. REMOVED AND REPLACED RIGHT GEAR SEQUENCE VALVE. REPLACEDMar 13, 2010 · N656FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA200912084373Switch · out of positionAFTER SLAT RETRACTION, ZIPPER WENT TO 255 KTS. DURING TROUBLESHOOTING FOUND THE L/G DOWN VMO/MMO SELECT SWITCH IN THE L/G DOWN POSITION. RESET SWITCH TO NORM POSITION. ALL INDICATIONS NORMAL IAW MM 34-10-00-5. OK FOR SERVICE.Dec 8, 2009 · N656FE · Airbus A300F4605R · Landing and Taxi AidsSDR FDEA200911093910Skin · gouged2 EA GOUGES ON RT WING CTR FLAP LWR SKIN AFTER BLENDOUT ARE OUT OF LIMITS. REPAIRED RT WING CTR FLAP LWR SKIN IAW EA6-5750-135131.Nov 9, 2009 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200911033803Rib · dentedRT WING INBD FLAP AT L/E AND RIB 18 HAS A DENT 2.0L X 1.0W X .140D. REPAIRED RT INBD FLAP AT L/E AND RIB 18 IAW SRM 57-50-00, FIG 208.Nov 3, 2009 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA200906242280Idg · leakingJUST AFTER DEPARTURE NR 2 IDG FAULT. FREQ (HZ) WAS FLUCTUATING FROM 382 TO 404. COMPLIED W/ECAM AND DISCONNECTED NR 2 IDG. FOUND NR 2 IDG WITH LOW WITH OIL. SERVICED AND RECONNECTED NR 2 IDG AND RAN ENG IAW JRH. GENERATOR OPS CHECK NORMAL, OIL/HYD DRAIN PORJun 24, 2009 · N656FE · Airbus A300F4605R · Alternator-Generator DriveSDR FDEA200902200611Hydraulic System · lowON TAKEOFF ROLL DURING ENGINE THRUST APPLICATION RECEIVED ECAM "BLUE HYD PUMP LO PR" REJECTED TAKEOFF LESS THAN 10 KTS. FOUND BLUE SYSTEM HYD QTY BELOW TOP HAT. SERVICED HYD SYS TO MIDDLE OF TOP HAT REF AMM 12-12-29-0. SUSPECT BLUE HYD SYS QTY INDICATION MAFeb 20, 2009 · N656FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA200810094285Gcu · failedREJECTED TAKEOFF AT 30 KTS DUE TO LOSS OF ALL ELECT POWER EXCEPT EMERGENCY POWER. MULTIPLE PROBLEMS RELATED TO RAIN DRIPPING INTO AVIONICS BAY. SEE ALSO WRI 25-70-1318, AFTER REJECTED TAKEOFF TAXIED BACK TO BLOCKS AND INSPECTED AVIONICS BAY. FOUND SIGNIFICOct 9, 2008 · N656FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA200810094290Gcu · failedREJECTED TAKEOFF AT 30 KTS DUE TO LOSS OF ALL ELECTRICAL POWER EXCEPT EMERGENCY POWER. MULTIPLE PROBLEMS RELATED TO RAIN DRIPPING INTO AVIONICS BAY. REMOVED AND REPLACED NR 2 GCU AND ALL ASSOCIATED SYSTEMS OPERATE NORMAL ON ACFT, MM 24-41-11-4 AND 24-41-00Oct 9, 2008 · N656FE · Airbus A300F4605R · AC Generation SystemSDR 08FDEA04290Gcu · failedREJECTED TAKEOFF AT 30 KTS DUE TO LOSS OF ALL ELECTRICAL POWER EXCEPT EMERGENCY POWER. MULTIPLE PROBLEMS RELATED TO RAIN DRIPPING INTO AVIONICS BAY. R&R NR 2 GCU AND ALL ASSOCIATED SYSTEMS OPERATE NORMAL ON ACFT. MM 24-41-11-4 AND 24-41-00-0.Oct 9, 2008 · N656FE · Airbus A300F4605R · AC Generator-AlternatorSDR 08FDEA04285Gcu · failedREJECTED TAKEOFF AT 30 KTS DUE TO LOSS OF ALL ELECT POWER EXCEPT EMERGENCY POWER. MULTIPLE PROBLEMS RELATED TO RAIN DRIPPING INTO AVIONICS BAY. SEE ALSO WRI 25-70-1318 - AFTER REJECTED TO. TAXIED BACK TO BLOCKS & INSPECTED AVIONICS BAY. FOUND SIGNIFICANT AOct 9, 2008 · N656FE · Airbus A300F4605R · AC Generator-AlternatorSDR 08FDEA03702Actuator · malfunctionedLT MLG WOULD NOT RETRACT. "UNLK" AND "DOOR" LIGHTS ON BOTH DETECTION SYSTEMS. ACFT YAW ALSO CONFIRMED GEAR NOT UP. WHEN GEAR HANDLE PLACED IN NEUTRAL, GREEN DOWN LOCKED INDICATOR CAME BACK ON. RE-EXTENDED GEAR FOR LANDING, NO PROBLEMS WITH EXTENTION. SAFTIESep 1, 2008 · N656FE · Airbus A300B4605R · Landing Gear ActuatorSDR 08FDEA00487Switch · failedMAIN DECK CARGO DOOR OPEN (ECAM) IN FLT PASSING FL230 IN CLIMB. WARNING WENT OUT PASSING 10,000 MSL IN DESENT. RETURNED TO KMEM "MEL 52-71-01: (IDENTIFY) MCD DOOR CLOSED AND LOCKED INDICATION ON ECAM DOOR PAGE INOP. MTSI OPENED DUE TO PREV HISTORY. REPLACEFeb 15, 2008 · N656FE · Airbus A300F4605R · Door Warning SystemSDR 07FDEA05020Web · crackedNR 2 FWD PYLON INSIDE ACCESS HOLE JUST FWD OF BLOW-OUT DOORS 2.5 IN CRACK EXIST IN OVAL CUT OUT AT DECK LEVEL REPAIRED CRACKED WEB IAW A300-600 SRM 54-52-12. CUT OUT DAMAGED PORTION OF WEB AND INSTALLED FILLER AND REPAIR DOUBLER IAW A300-600 SRM 54-52-21 WITHDec 8, 2007 · N656FE · Airbus A300F4605R · Nacelle/Pylon, Main FrameSDR 05FDEA02324Fitting · crackedMDIS 656 52-30 0008568 03AUG05 BFM CLOSE R C/W EA 6-5230-82117 DOORS - MAIN CARGO DOOR BEARING FITTING CRACKED ENT BY: 575463 RPT BY: 575463 FACT 04AUG05 23:50 BFM R COMPLIED WITH EA 6-5230-82117 DOORS MAIN CARGO DOOR BEARING FITTING CRACKED. RII:49723Aug 8, 2005 · N656FE · Airbus A300* · Cargo/Baggage DoorsSDR 05FDEA02234Spar · crackedNR 1 PYLON INSIDE PNL 411CL UPPER SPAR WEB HAS CRACK.Aug 3, 2005 · N656FE · Airbus A300F4605R · Nacelle/Pylon, Frame/Spar/RibSDR 05FDEA02119Flap Track · dentedLT WING OB TE FLAP LE HAS DENT BET TRACKS NR 5.Jul 27, 2005 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR 05FDEA02109Spar · crackedPYLON STRUCTURE CANTILEVER BEAM LWR SPAR WEB CRACK. COMPLIED WITH EA 6-5450-82109, PYLON STRUCTURE CANTILEVER BEAM LWR SPAR WEB CRACK.Jul 26, 2005 · N656FE · Airbus A300F4605R · Nacelle/Pylon, Main FrameSDR 05FDEA02108Floorbeam · crackedCOMPLIED WITH EA 6-5310-82098 FUSELAGE MAIN FRAME 31 FLOORBEAM CRACK REPAIR, Y=1707.5.Jul 26, 2005 · N656FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 05FDEA02002Web · crackedNR AFT CARGO DOOR FWD UPPER CORNER OPENING WEB CRACKED AND BENT. REMOVED WEB IAW SRM 51-40-21. LOCATED AND DRILLED NEW WEB AND ANGLE IAW SRM 51- 40-40 INSTALLED NEW WEB & ANGLE IAW SRM 51-40-21Jul 20, 2005 · N656FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 05FDEA01999Angle · chafedNR 1 ENG TRUST REVERSER ASSY INNER BODY LWR ANGLE CHAFED.Jul 19, 2005 · N656FE · Airbus A300F4605R · Engine Thrust ReverserSDR 05FDEA01991Angle · chafedNR 2 ENGINE THRUST REVERSER CHAFED AREA ON INNER BODY LOWER ANGLE.Jul 18, 2005 · N656FE · Airbus A300F4605R · Engine Thrust ReverserSDR 05FDEA01990Fairing · delaminatedRH WING NR 4 FLAP TRACK FAIRING AT FWD O/B LWR SURFACE HAS DELAM.Jul 18, 2005 · N656FE · Airbus A300F4605R · Trailing Edge FlapsSDR 05FDEA01951Seat Track · corrodedMCD SEAT TRACK CORRODED BETWEEN FR71 - FR73 BL O.Jul 14, 2005 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01950Seat Track · corrodedSEAT TRACK CORROSION ON SEVERAL LOCATIONS BETWEEN FR 63-FR-71 BLO.Jul 14, 2005 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01851Seat Track · corrodedMCD - SEAT TRACK HAS CORROSION FR 38 PLUS 11.0, RBL 37.5. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND 53-10-16 FIG 201. SEAT TRACK SPLICE ASSY FABRICATED ON TRAVELER T5/529101 W/O 29203.Jul 7, 2005 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 05FDEA01853Seat Track · corrodedSEAT TRACK HAS CORROSION FS 40 3, RBL 37.5 SEAT TRACK. FABRICATED ON TRAVELER NR T5/529929 W/O 29203 NR N00439. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-16 FIG 201.Jul 7, 2005 · N656FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 03FDEA00782Frame · dentedDENT IN EXT. FUSELAGE AFT OF BULK CARGO DOOR, AT FRAME 72 AND APPROX. STRINGER 38R. DENT HAS CREASE IN CENTER. DENT MEASURES 1.53 IN LONG, 1.125 IN WIDE AND .093 IN DEEP AT CREASE. CUTOUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER IAW A300-600 SRM 53-10May 20, 2003 · N656FE · Airbus A300B4605R · Fuselage Main, FrameSDR 03FDEA00759Door · damagedNR 1 ENGINE RT T/R COWL BLOW OUT DOOR INTERIOR HAS TWO EACH CHAFED AREAS WHERE RETAINING CABLE HAS MADE CONTACT. REPAIRED DAMAGED AREAS BY BLENDING, ALODINING, AND FILLING AREA WITH HIGH TEMP SEALANT, AND APPLYING A COAT OF TEFLON PAINT IN THE REWORKED May 19, 2003 · N656FE · Airbus A300F4605R · Nacelle/Pylon, Main FrameSDR 01FDEA00535Lock · malfunctionedHEARD NOISE IN FLT - DISCOVERED ULD IN 2R FWD BELLY NOT LOCKED DOWN. NO APPARENT DAMAGE. AC OK FOR SERVICE.Jul 12, 2001 · N656FE · Airbus A300F4605R · Cargo CompartmentsSDR 01FDEA00290Warning System · activatedON T/O CRC SOUNDED WITH RED ECAM DISPLAYED. MIN EQUP BAY SMOKE WARN ON ECAM.Apr 20, 2001 · N656FE · Airbus A300F4605R · Smoke DetectionSDR 01FDEA00281Selector Valve · malfunctionedLANDING GEAR WOULLD NOT EXTEND NORM ON APPR TO EWR. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE 3GA PRE AMM 32-31-12. JACKED AC AND CYCLED LANDING GEAR SEVERAL TIMES. CK BOTH SYS 1 & 2 WITH NO DISCREP NOTED.Apr 15, 2001 · N656FE · Airbus A300F4605R · Landing Gear SelectorSDR 01FDEA00219Fire Warning · activatedAT CR FOR APPROX 20 MIN FMS IND A FIRE. PROC IN QRH FOLLOWED FIRE HANDLE PULL AGENT DISCHARGED. IMMEDIATE LAND AT IND. FIRE LIGHT IN APU HANDLE EXT ON TOUCHDOWN.Mar 21, 2001 · N656FE · Airbus A300F4605R · Fire DetectionSDR 00FDEA00682Controller · odorESS TR ADVISORY AND SMELL OF ELECTRICAL INSULATION. REMOVED AND REPLACED NR 1 & NR 2 T/R PER MM 24-32-00-5.Sep 26, 2000 · N656FE · Airbus A300F4605R · Engine Thrust ReverserSDR 00FDEA00028Fwc · inoperative00-15 - WHEN TOGA EVERS DEPRESS FOR MAX TOGA PWR TO, THE CRC SOUND AND THE LT ECAM DISPLAYED RED AFS/AP OFF. THIS WILL ALSO OCCUR W/ENG S/D AND EXT/APU PWR CONNNECT. REMOVED AND REPLACED NR 2 FWC IAW MM 31-53-34. OPS CK NORMAL. PER AFS/LAND TEST, OPS NORM.Jan 19, 2000 · N656FE · Airbus A300F4605R · Flight Management Computing Hardware SystemSDR 98FDEA00718Wire · cutLANDING GEAR WOULD NOT RETRACT ON T/O. TRIED SYS 2 WITH NO EFFECT. SEV COCKPIT ITEM NOT WORK, SUSP RELAY SWITCH. REMOVED 400VU PNL ON CTR INSTRUMENT PNL AND FOUND NUM CUT WIRES ON CONN 1486VC. REPAIRED WIRES 3231-0118, 3248-0107, 3231-0026, 3314-2264, 3314Nov 28, 1998 · N656FE · Airbus A300F4605R · Landing Gear System WiringSDR 97FDEA00588Pitot Tube · obstructed97-160 - CAPT'S AIRSPEED TAPE ON PFD FROZEN AT 30KTS ON T/O ROLL-TREND ARROW NOT VISIBLE-REJECTED T/O AT 110KTS, F/O'S OK. PURGED CAPT PITOT LINE OF OBSTRUCTION, PERFORMED PITOT SYSTEM LEAK TEST, FOUND SYSTEM OK.Aug 28, 1997 · N656FE · Airbus A300* · Pitot/Static SystemSDR 97FDEA00530Pitot Tube · obstructedDUAL STBY AIRSPEED INDICATOR FAILED AFTER TAKEOFF. CAPTAINS PFD AIRSPEED INDICATOR FAILED AFTER TAKEOFF, BLANK/RED SPD. CLEANED OBSTRUCTION FROM STBY PITOT TUBE. REMOVED AND REPLACED NR 1 ADC. PERFORMED LEAK AND OPS CHECK PER M/M 34-11-34.Aug 12, 1997 · N656FE · Airbus A300* · Pitot/Static SystemSDR 96FDEA01192Indication · malfunctionedON APPOACH AFTER LG EXTENDED NR 1 SYS IND 3 GREEN SYS 1 SELECTED ON SHORT FINAL TOO LOW GEAR WARNING INITIATED, SYS 2 OVERHEAD SHOWED NOSE GEAR NOT DOWN. LANDING GEAR CHECKED VISUALLY DOWN AND LOCKED ON SYS DETECTION 2. ALSO, SELECTED GAVE THE SAME WARNING.Jul 4, 1996 · N656FE · Airbus A300F4605R · Landing Gear Position and WarningSDR 96FDEA00799Door Warning · activatedAVIONICS DOOR UNSAFE AT 12,000 FT. AVIONICS DOOR FOUND CLOSED. DOOR CYCLED OPEN AND CLOSED, COCKPIT INDICATION SHOWS LOCKED AND GREEN ON ECAM.Apr 20, 1996 · N656FE · Airbus A300F4605R · Door Warning System
Back to N656FE