N657FE

Service difficulty reports · 180

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 = 'N657FE' 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 07FDEA02649Beam · corrodedLT WING TIP INBD T/E UPPER SURFACE STATIC WICK BASE HAS 2 SQ IN AREA OF CORROSION EXTENDING UNDER BASE BETWEEN BASE AND UPPER SKIN SURFACE. REF A300 AMM 57-00-00. REMOVED AND REPLACED UPPER BEAM ON WING TIP IAW A300-600 SRM 57-30-11-4 AND SRM 51-40-21. REMOJul 28, 2007 · N657FE · Airbus A300F4605R · Wing Main, Frame StructureSDR 07FDEA02648Beam · corrodedRT WING TIP INBD T/E UPPER SURFACE STATIC BASE HAS 1.5 SQ IN AREA OF CORROSION EXTENDING UNDER BASE BETWEEN BASE AND SKIN SURFACE REF A300 AMM 57-00-00. REMOVED AND REINSTALLED WING TIP IAW A300-600 AMM 57-30-11-4. REMOVED AND REPLACED UPPER BEAM ON WING TIPJul 28, 2007 · N657FE · Airbus A300F4605R · Wing Main, Frame StructureSDR 07FDEA02645Skin · gougedMDCC FR 22 5 IN UP FROM STR 13 R IS A GOUGE .5 IN BY .5 IN BY .020 IN IN THE FRAME - ZONE 230 REF A300 AMM 53-13-11. FABRICATED NEW COUPLING IAW EA6-5310-113301. CUT OUT DAMAGE AREA IAW EA6-5310-113301. INSTALLED NEW COUPLING IAW EA6-5310-11330. REPROTECTJul 28, 2007 · N657FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 07FDEA02644Skin · dentedMDCC FR 24 HAS A DENT 3 IN BY 1 IN BY .032 IN BETWEEN STR 12R AND 13R - ZONE 230 - REF A300 AMM 53-13-11. COMPLIED IAW EA 6-5310-110523.Jul 28, 2007 · N657FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 07FDEA02602Seat Track · corrodedMDCC SEAT TRACK 3RH FR 45 - FR 54 20 SQ INCH CORROSION REF A300-600 AMM 53-10-16-6-02 ZONE 200. REMOVED CORROSION IAW A300-600 SRM 51-74-10. CHECKED LIMIT FOUND TO BE OUT OF LIMIT IAW A300-600 SRM 53-10-16 FIG 101. FAB`D SEAT TRACK IAW A300-600 DWG NR A5327Jul 24, 2007 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02600Seat Track · corrodedMDCC SEAT TRACK 2RT FR45-FR54 8 SQ INCH CORROSION REF A300-600 AMM 53-10-16-6. REMOVED OLD SEAT PER A300-600 SRM 51-40-21. FABRICATED NEW SEAT TRACK PER AIRBUS DRAWING 532-74005. REPROTECTED SURFACE USING ALODINE, PRIMER, TOPCOAT PER A300-600 SRM 51-75-10. Jul 24, 2007 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02569Angle · crackedFWD CARGO COMPARTMENT FWD SIDE OF FLOORBEAM C27 VERTICAL STIFFENER OUTBD SEATRACK 2R HAS .25" LONG CRACK IAW A300-600 AMM 53-13-11-6. REPAIRED FLOORBEAM IN FWD CARGO COMPARTMENT C27 OUTBD SEATRACK 2R IAW A300-600 SRM 53-10-15 FIG 207.Jul 23, 2007 · N657FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 07FDEA02574Seat Track · corrodedTHREE 4.5 SQ INCH AREAS OF CORROSION EXIST AT MDCC SEAT TRACK R-3 BETWEEN FRAMES 40 THRU 45 REF 53-10-16-06 ZONE 200 IAW A300-600 AMM. BLENDED CORROSION IAW A300-600 SRM 51-74-10. CHECKED LIMIT IAW A300-600 SRM 53-10-16, FOUND TO BE OUT OF LIMIT. FAB`D SEATJul 23, 2007 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02573Seat Track · corrodedA 5 SQ INCH AREA OF CORROSION EXIST AT MDCC SEAT TRACK L-2 FRAME 42 REF. 53-10-16-06 IAW A300-600 AMM. REMOVED CORROSION IAW A300-600 SRM 51-74-10. MAT LOSS IS FOUND TO BE OUT LIMITS. REMOVED SEAT TRACK L-2 FR 40 THRU FR 45 IAW A300-600 SRM 51-40-21. FABRIJul 23, 2007 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02572Seat Track · corrodedMDCC SEAT TRACK 3L FR15 HAS 1 SQ IN AREA OF CORROSION EXTENDING ON AND UNDER SCALLOPS ZONE 220 REF A300-600 AMM 53-10-16. REMOVED CORROSION AT 3L FR15 SEAT TRACK. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. REMOVED AND REPLACED SEAT TRACK IAW A300-Jul 23, 2007 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA02571Stiffener · crackedFWD CARGO COMPARTMENT FWD SIDE OF FLOORBEAM C23 VERTICAL STIFFENER OUTBD SEAT TRACK 2R HAS .25" LONG CRACK IAW A300-600 AMM 53-13-11-6. CUT OUT DAMAGED AREA PER A300-600 SRM 53-10-15 PG 254. NDT SHOWS NO CRACK REMAINS PER NTM 51-10-08. FABRICATED REPAIR PARJul 23, 2007 · N657FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 07FDEA02570Stiffener · crackedFWD CARGO COMPARTMENT FWD SIDE OF FLOORBEAM C32 VERTICAL STIFFENER OUTBD SEAT TRACK 4L HAS .25" LONG CRACK IAW A300-600 AMM 53-13-11-6. CUT OUT DAMAGED AREA IAW A300-600 SRM 53-10-15 PG 254. NDT SHOWS NO CRACK REMAINS PER NTM 51-10-02. FABRICATED REPAIR PAJul 23, 2007 · N657FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 06FDEA03589Floorbeam · damagedFLOOR DAMAGE AT POSITION 9L/13L DUE TO LOCK BEING PULLED FROM FLOOR. LOCK ID D1696 AT FRAME 66. UPON FURTHER INVESTIGATION FOUND FLOORBEAM ROLLED WITH A 1.25" CRACK AT LIGHTNING HOLE. REF WRI 5310-9370 FOR EA APPLYING TO THE FLOORBEAM DAMAGE EA #6-5310-1052Oct 4, 2006 · N657FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 06FDEA0401Solenoid · unknownAFTER T/O GOT YELLOW HYD SYSTEM LO PRESS ECAM, QUANTITY WAS FINE, PRESSURE READ 50 PSI. REMOVED AND REPLACED YELLOW HYD SYSTEM SOLENOID, OPERATED DEPRESSURIZING VALVE. REF: 29-11-32-4. RAN ENGINE, SYSTEM OPS CHECKS GOOD. RUN PERFORMED.Jan 27, 2006 · N657FE · Airbus A300B4622 · Hydraulic System, MainSDR 05FDEA01716Skin · damagedFWD CARGO DOOR AT FUSELAGE CUT-OUT FWD LOWER SKIN EDGE AND WEB SKIN HAS CHAFED MARK. ITEM WAS BLENDED AND RESULTING CONDITION WAS OUT OF LIMITS. REPAIR PARTS FABRICATED, REF. TRAVELER T5/527985. REPAIRS AFFECTED USING STANDARD WORK DRAWING SR30-53-001. MAJOJun 28, 2005 · N657FE · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR 05FDEA00162Warning Light · illuminatedON THROTTLE ADVANCEMENT FOR T/O RECEIVED ENG 1 REVERSER PRESSURIZED. REJECT NORMAL. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01- CATEGORY: C EXPIRATION: 04FEB05 MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATEJan 25, 2005 · N657FE · Airbus A300F4605R · Engine Thrust ReverserSDR 04FDEA01500Valve · faultyNR 2 ENGINE FAILURE WARNINGS APPEARED ON ECAM ON TAKEOFF AT 70 KTS. REJECTED TAKEOFF. TRIED ANOTHER TAKEOFF, SAME PROBLEM, REJECTED TAKEOFF AGAIN. NR 2 ENGINE WOULD NOT SHUT DOWN IN BLOCKS WITH FUEL LEVER. PULLED NR 2 FIRE HANDLE AND ENGINE WOULD NOT SHUT May 27, 2004 · N657FE · Airbus A300F4605R · Compressor Bleed ValveSDR 03FDEA00798Skin · damagedFUSELAGE EXTERIOR SKIN AT FR 43-44 STR 53L-55L HAS BLEND OUT AREA OUT OF LIMITS BY 0.006. PERFORMED HFEC OF AREA, DVI, AND REMOVED 4 FASTENERS. ROTOTESTED 4 HOLES, O/S TO 6.31MM AND INSTALLED HL11VF8/HL70-8 HILOC FASTENERS. PRIMED AND PAINTED. ALL WORKMay 24, 2003 · N657FE · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR 03FDEA00799Skin · dentedRT CENTER FLAP BOTTOM SKIN HAS 3 CREASED DENTS RANGING FROM 1/4"W TO 1/2"W, 1/2" L TO 6"L ON T/E JUST I/B OF #4 FLAP TRACK. REPAIRED BOTTOM SKIN BY INSTALLING DOUBLER I/A/W FEDEX EA 6-5750-2003May 24, 2003 · N657FE · Airbus A300B4605R · Trailing Edge FlapsSDR 03FDEA00779Slide · failedWHILE PERFORMING W/C E65210-7-5000 PT 1 OPERATIONAL CHECK OF DOOR L1- DOOR SLIDE LACES FAILED. REMOVED AND REPLACED LT CREW/PAX ENTRY DOOR EMERGENCY EVACUATION SLIDE IAW A300600.May 20, 2003 · N657FE · Airbus A300B4605R · Escape SlideSDR 03FDEA00778Ram Air Turb · inoperativeWHILE PERFORMING RAT EXTENSION, COULD NOT DEPLOY RAT WITH CONTROL HANDLES, BOTH CONTROL HANDLES IN FLIGHT COMPARTMENT. TROUBLESHOT PER A300-600 AMM 29-25-00-5, NO DEFECTS NOTED. OPS CK GOOD.May 20, 2003 · N657FE · Airbus A300B4605R · Hydraulic System, AuxiliarySDR 02FDEA00794Module · malfunctionedON TAKEOFF, LDG GEAR WOULD NOT RETRACT ON NR 2 SYSTEM. SWITCHED TO NR 1 SYSTEM AND GEAR WOULD STILL NOT RETRACT. REMOVED LANDING GEAR CONTROL HANDLE 2GA IAW TSM, CONTINUITY CHECKS GOOD BUT MODULE HAS A VERY SUSPICIOUS RATTLE. REMOVED AND REPLACED 2GA MODULENov 2, 2002 · N657FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 01FDEA00452Window · cracked01-193 IN CRUISE WINDOW L3 CRACKED. R&R LH FIXED SIDE WINDOW PER MM 56-11-12-4. R&R WINDOW HEAT CONTROLLER & WINDOW HEAT PROTECTION PER MM 30-42-11-4 & 30-42-51-4, MM 30-42-00-5.Jun 15, 2001 · N657FE · Airbus A300F4605R · Flight Compartment WindowsSDR 00FDEA00747Warning System · stuckCAPT/FO VMO/MMO STUCK AT 255 KTS ON CLIMBOUT. REF WRI 32-30/466, FOUND L/G VMO MMO SELECT SWITCH IN LG DOWN POSTION. SWITCHED TO NORMAL.Oct 26, 2000 · N657FE · Airbus A300F4605R · Airspeed/Mach IndicatorSDR 00FDEA00732Sensor · inoperativeON T/O ROLL PHL, NO FUEL FLOW NR 1. RETURNED TO GATE. REJECT 100 KTS.Oct 24, 2000 · N657FE · Airbus A300F4605R · Fuel Flow SensorSDR 00FDEA00439Wire · burnedIN ACCOMPLISHING FCD 6-24-008A FOUND DAMAGE MOCC, NOTIFIED OF BURNED T2 AND T3 WIRES & HOLES IN RACK. THIS GENERATED EA 6-2570-51827. REPLACED DAMAGED WIRES REF WDM 24-32-01. R&R VERTICAL STIFFENER PER SRM 51-71-30. REQURES AVIONICS REINSTALLATION.Jul 6, 2000 · N657FE · Airbus A300F4605R · Electrical Power System WiringSDR 00FDEA00296Indicator · malfunctionedON T/O ROLL, NR 1 ENGINE N2 GAUGE APPEAR TO STICK ABOUT 80 PERCENT ON SUB ENGINE RUN-UP. REMOVED AND REPLACED NR 1 ENGINE N2 IND PER A MM 77-12-21-4. OK TO CONTINUE.Apr 25, 2000 · N657FE · Airbus A300F4605R · Engine RPM Indicating SystemSDR 98FDEA00721Control · malfunctionedDURING CRUISE, ECAM 'RIGHT MAIN CABIN DOOR UNLOCKED'. DESCEND TO MEA OF 11,000 DIVERT TO ABQ. CABIN DOOR RT VISUALLY CKD CLOSED AND LOCKED. CATC CONTROL NR 44470, EXP 29NOV98, ASSIGN NEW CONTROL NR 44474, EXP 29NOV98.Nov 19, 1998 · N657FE · Airbus A300F4605R · Door Warning SystemSDR 98FDEA00267Door · not sealedPASSING FL 330 IN THE CLIMB MAIN DECK DOOR LIGHT ILLUMINATED. CABIN BEGAN TO DEPRESSURIZE. PASSING FL 190 IN THE DESCENT DOOR INDICATED NORMAL. ALL CABIN DOORS, OPENED AND INSPECTED MAIN CARGO DOOR SEALS, FOUND OK. CLOSED INDICATOR LIGHTS OK. NO DAMAGE FOApr 14, 1998 · N657FE · Airbus A300F4605R · Passenger/Crew DoorsSDR 98FDEA00108Expansion Vlv · leaking98-0041, SHORTLY AFTER T/O NOTICED THAT RT OUTER TANK WAS 1000 LBS LESS THAN LEFT OUTER TANK, CONT TO BURN OUT OF RT OUTER TANK INSTEAD OF RT INNER. SECURED RT OUTER PUMPS, RT OUTER TANK CONTINUED TO DROP TO 5000 LBS WITH PUMPS OFF, RETURNED TO MEM. C/W TSM Feb 15, 1998 · N657FE · Airbus A300F4605R · Aircraft Fuel Distribution System
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