N427FE, cancelled Feb 20, 2024

Service difficulty reports · 56

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 = 'N427FE' AND deregistration_id = 'N427FE-2024-02-20'
  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 FDEA201506031688Unknown · malfunctionedLOST CABIN AT APPROX 18 - 210 FL, THE MAN PRESS VLV SHOWED OPEN & TRIED MANUAL CONTROL & IT DID NOT FIX PROBLEMS. NEITHER PRESSURIZATION SYS FAULTED. TROUBLESHOOTING ON THE PRESSURIZATION SYS IN PROGRESS.Jun 3, 2015 · N427FE · Airbus A310203 · Cabin Pressure Control SystemSDR FDEA201504141230Nut · lack of lubeON APPROACH, WHEN CONFIG FROM SLATS 15 TO FLAPS 15, RECEIVED FLAPS SYS 1 & SYS 2 FAULT. RECYCLED HANDLE TO SLATS 15 IAW PHASE ONES THEN RE-ATTEMPTED FLAPS 15, SAME RESULT FLAPS SYS 1 & SYS 2 FAULT. REVIEWED QRH, ELECTED TO DIVERT, ON APPROACH, CONFIGURED WHEApr 14, 2015 · N427FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201312132980Valve · failedON DEPARTURE, CLIMBING THROUGH 10,000' CABIN ADVISORY HIGH RATE, THEN EXCESS CABIN ALTITUDE COMPLIED WITH ECAM & QRH. ACFT WOULD NOT PRESSURIZE. RETURNED TO A/P. PRESS PAGE SHOES MAN PRESS DOOR OPEN. TRIED REG 1 & 2, MANUAL PRESSURIZATION TO NO AVAIL. PERDec 13, 2013 · N427FE · Airbus A310203 · Pressure Regulator/Outflow ValveSDR FDEA201308242031Window · crackedCAPTAIN'S FRONT FIXED WINDOW CRACKED AT FL 390. INSTALLED SERVICEABLE WINDSHIELD TO STEP 1.E.17, REF MM 56-11-11-04. WINDOW IS INSTALLED SEALED & TORQUED.Aug 24, 2013 · N427FE · Airbus A310203 · Flight Compartment WindowsSDR FDEA201308201962Fitting · crackedFRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826.Aug 20, 2013 · N427FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201308201961Fitting · crackedFRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826.Aug 20, 2013 · N427FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201308161913Frame · crackedFUSELAGE FRAME 40, UPPER CORNER FOUND CRACK IN RT NR 2 HOLE COMPLIED WITH EA 6-5710-T0301577.Aug 16, 2013 · N427FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201308131861Frame · crackedRIGHT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201308131860Frame · crackedRT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5330-T0301676.Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201308131859Frame · crackedRT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201308131858Frame · crackedLEFT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201308131857Frame · crackedLEFT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201308131856Frame · crackedLEFT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201308091817Skin · delaminatedLEFT FWD FUSELAGE TOILET SERVICE PANEL LOWER SKIN CUTOUT DELAMINATED. REPAIRED IAW EA 6-5330-T0301676.Aug 9, 2013 · N427FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201301210152Controller · inoperativeCLIMBING OUT OF 12,000 RECEIVED A "CABIN ALT EXCEEDS 10,000" RED ECAM. DONNED O2 MASK. CABIN WAS VERIFIED ABOVE 10,000. BOTH FWD & AFT FLOW VALVE ON NR 2 SYSTEM WERE FULLY OPENED AND AMBER. BOTH FWD & AFT OUTFLOW VALVE ON NR 1 SYS WERE FULLY CLOSED. WJan 21, 2013 · N427FE · Airbus A310203 · Cabin Pressure ControllerSDR 08FDEA04940Warning Light · illuminatedON TAKEOFF ROLL KBDL LOWER ACCESS DOOR LT CAME ON AT 70KTS RTO AND RETURN TO RAMP WITH LTS ON ECAM AFT LOWER ACCESS DOOR OPENED AND CLOSED LIGHTS WENT OUT. DOOR IS CLOSED AND LOCKED. NOTE: TSI OPENED TO RECHECK DOOR 136AR.Nov 20, 2008 · N427FE · Airbus A310203 · Door Warning SystemSDR 08FDEA04857Vane · gougedLT OTBD FLAP UPPER SURFACE HAS 9 INCH GOUGE APPROX .020 IN DEEP LOCATED 54 INCHES FROM OTBD END AND 21 INCHES FROM T/E. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW EA 6-5750-124167, RELEASE DATE4 NOVEMBER, 2008.Nov 11, 2008 · N427FE · Airbus A310203 · Trailing Edge FlapsSDR 08FDEA04856Adapter · crackedMDCC CLS ADAPTER AT FRAME 46 BETWEEN SEAT TRACK 2 RT AND 3 RT HAS 1 CRACK 3 INCHES LONG. REMOVED AND REPLACED 1 CLS ADAPTER AT FR 46 BETWEEN SEAT TRACK 2 RT AND 3 RT IAW A310-200 SRM 51-40-21.Nov 11, 2008 · N427FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 08FDEA04589Seat Track · crackedSEAT TRACK 5 RT CRACKED AT FR 60. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED REPAIR SPLICE AT SEAT TRACK 5 RT BETWEEN FR 58 AND FR 62 IAW A310-200 SRM 53-10-16, FIG 208A, PG 250, SHT 2.Oct 28, 2008 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04429Skin · gougedLOWER FUSELAGE EXTERNAL SKIN FR 59 TO 61, STRINGER 44L - 45L HAS GOUGE 26" BY 1/4 INCH BY .052 INCH RUNNING JUST BELOW LAP SEAM REPAIRED AREA AT LOWER FUSELAGE EXTERNAL SKIN FR 59 TO 61, STRINGER 44L - 45L IAW SRM 53-10-12 FIG 217.Oct 19, 2008 · N427FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA05149Controller · malfunctionedEXCESSIVE CABIN ALT ECAM ALERT ON DEPARTURE. SYS 2 VALVES SEEMED TO BE STUCK OPEN. ON INITIAL TROUBLESHOOTING, BOTH CAB PRESS REGULATORS SHOWED ACTIVE (GREEN TRIANGLE ON SWITCH). NR 2 REGULATOR WOULD ACTIVATE AND DEACTIVATE, BUT AS LONG AS NR 1 REG WAS ON IDec 27, 2007 · N427FE · Airbus A310203 · Cabin Pressure ControllerSDR 07FDEA04752Outflow Valve · malfunctionedON TAKEOFF, SHORTLY AFTER GEAR RETRACTION ECAM SHOWED NO PRESSURIZATION. PRESS PAGE SHOWED BOTH NR 2 FWD AND AFT OUTFLOW VALVES FULL OPEN AND CABIN V/S PEGGED IN CLIMB. TURNED OFF NR 2 REG NO EFFECT. TRIED TURNING OFF BOTH REG AND USING MANUAL PRESS WITH V/Nov 8, 2007 · N427FE · Airbus A310203 · Pressure Regulator/Outflow ValveSDR 06FDEA03993Arm · unknownNR 2 LANDING GEAR INDICATING PANEL DEFERRED PER MEL 32-61-01A SYSTEM NR 1 SELECTED. AFTER TAKEOFF WHEN LANDING GEAR RETRACED NOSE GEAR DOWN (GREEN ARROW) STAYED ILLUMINATED REF WRI 32-20/8357 FOR MX ACTION. REMOVED REPLACED NOSE LANDING GEAR TELESCOPIC DRAG Nov 10, 2006 · N427FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR 06FDEA2357Angle · corrodedAFT CARGO UNDER FLOOR BETWEEN FR 54.3 AND 54.2 AT STR 57 1 EA L-ANGLE HAS 3 SQ INCHES OF EXFOLIATION. REPAIRED AREA IAW EA 6-5310-100963.Jun 16, 2006 · N427FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 06FDEA2356Skin · corrodedAFT CARGO UNDERFLOOR BETWEEN FR 54.3 AND 54.2 AT STR 57 INTERIOR SKIN HAS 4 SQ INCHES OF CORROSION. REPAIRED AREA IAW EA 6-5330-100962.Jun 16, 2006 · N427FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 06FDEA2258Floorbeam · crackedFWD CARGO BAY FLOORBEAM (MAIN DECK) AT FR 34 CRACKED BETWEEN SEAT TRACK 2 & 3R (MARKED) FWD SIDE. REPAIRED FLOORBEAM IAW A310 SUPP 53-10-15 FIG 201 SH 2.Jun 8, 2006 · N427FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 06FDEA2245Spar · corrodedRIGHT HORZ STAB T/E REAR SPAR CHORD TOP SIDE BETWEEN RIB 20 AND 21 HAS CORROSION AT 3 EA NUT PLATE HOLES. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AND REPAIRED IAW A310-200 SRM 55-11-21 FIG 214 PAGE 283/284.Jun 7, 2006 · N427FE · Airbus A310203 · Horizontal Stabilizer, Spar/RibSDR 06FDEA2244Shear Tie · corrodedBULK CARGO UNDER FR 68 STR 57 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED SHEAR TIE IAW A310-200 SRM 51-40-21.Jun 7, 2006 · N427FE · Airbus A310203 · Fuselage Internal Mounting StructureSDR 06FDEA2243Skin · corrodedAFT CARGO COMP BELLY SKIN AT STR 57 FR 58 TO 59 HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-10-00.Jun 7, 2006 · N427FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 06FDEA2242Skin · corrodedATF CARGO COMP BELLY SKIN CORRODED FWD OF ANTENNA CUTOUT FR 60 TO FR 61. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AND FOUND TO BE WITHIN LIMITS OF SRM 53-10-00.Jun 7, 2006 · N427FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 06FDEA2241Structure · corrodedVERT STAB BOX LOWER SURFACE AT FR 84 HAS CORR STR 2L REF N00680. COMPLIED WITH EA 6-5530-101044.Jun 7, 2006 · N427FE · Airbus A310203 · Vertical Stabilizer Miscellaneous StructureSDR 06FDEA2240Attach Fitting · crackedTHS ACTUATOR UPPER EMPENNAGE ATTACH FITTING CRACKED IN VERT RADIUS FR 86 FR 87 REF N00371. REMOVED AND REPLACED FITTING IAW A310-200 SRM 51-72-10.Jun 7, 2006 · N427FE · Airbus A310203 · Stabilizer ActuatorSDR 06FDEA2239Doubler · corrodedACCESS DOOR CUTOUT DOUBLER DOOR 134AR BETWEEN FR 23 & 24 O/B RIGHT SIDE HAS CORROSION. REMOVED AND REPLACED DOUBLER IAW A310-200 SRM 51-74-10, 51-72-10 AND 51-40-21.Jun 7, 2006 · N427FE · Airbus A310203 · Fuselage Main, StructureSDR 06FDEA2142Spar · corrodedRT HORIZ STAB T/E REAR SPAR FROM RIB 12 TO END RIB HAS 8 NUTPLATES AND/OR FASTENER HOLES WITH CORROSION REF N00300. REMOVED CORROSION IAW A310 SRM 55-10-00 PG 105. FOUND TO BE WITHIN LIMITS. REMOVED AND REPLACED NUTPLATES AND FASTENERS IAW A310 SRM 51-40-May 31, 2006 · N427FE · Airbus A310203 · Horizontal Stabilizer, Spar/RibSDR 06FDEA2141Floorbeam · crackedFOUND MAIN DECK FLOORBEAM AT FS 37 BETWEEN SEAT TRACK 2R AND 3R HAS A CRACK ON THE FWD UPPER VERTICAL RIB REF N00693. REPAIRED FLOORBEAM IAW AIRBUS SUPPLEMENT 53-10-15 PB 201 PARA 3A FIG 201 SHEET2.May 31, 2006 · N427FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 06FDEA2140Floor Support · corrodedMAIN CARGO COURIER AREA FLOOR SUPPORT "T" CAP HAS EXFOLIATION ON 3L AT FS 14 REF N00679. REMOVED AND REPLACED "T" CAP IAW A310 SRM 51-72-10.May 31, 2006 · N427FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 06FDEA2036Stringer · corrodedAFT CARGO COMPT STR 56R BETWEEN FS 61 AND FS 62 FASTENER HAVE CORROSION AROUND THEM REF N00437. REMOVED CORROSION IAW A310 SRM 51-74-10 AREA ON STR 56R. FOUND OUT OF LIMITS IAW A310 SRM 53-10-00. REPAIRED STR 56R IAW A310 SRM 53-10-14 FS 59.5-62.5.May 26, 2006 · N427FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR 06FDEA2035Skin · dentedRT SIDE FUSE EXTERNAL SKIN BETWEEN AFT CARGO AND BULK CGO 2 EA INCOMING DENTS APPROX .020 DEEP X 1.5 DIA FWD OF FS 67 AND FS 65 W/APPROX .020 DEEP BY 2.0 DIA REF N00220. DENT FOUND TO BE CRACK FREE AND WITHIN LIMITS OF A310 SRM 53-10-12 DIAGRAM 109 PG 131/132May 26, 2006 · N427FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 06FDEA2033Seat Track · corrodedMDCC L2 SEAT TRACK AT FS 70 AND FS 72 HAS CORROSION REF N00587. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-40-21.May 26, 2006 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2034Seat Track · corrodedMDCC L3 SEAT TRACK AT FR 65.5 TO 67.5 AND AT FR 71.5 HAS 5 AREAS OF CORROSION REF N00588. REMOVED CORROSION IAW A310 SRM 51-74-10 4 1 AREA OUT OF LIMITS IAW A310 SRM 53-10-16 FIG 101. REPLACED OUT OF LIMIT PRODUCTION SPLICE IAW A310 SRM 51-40-21.May 26, 2006 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2032Seat Track · corrodedFOUND SEAT TRACK FROM FS 38.2 TO FS 40 TRACK 2R HAS CORROSION REF N00505. REMOVED AND REPLACED 1 DUMMY TRACK IAW A310 SRM 51-40-21.May 26, 2006 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA2031Spar · corrodedFOUND VERT STAB SPAR BOX, LWR VERT STAB ATTACH BEAM HAS 11 AREAS OF CORROSION ON UPPER SURFACE REF N00367. REMOVED CORROSION IAW A310 SRM 51-74-10 1 EA AREA OUT OF LIMITS, REPAIRED AREA NR 11 IAW A310 SRM 55-31-19.May 26, 2006 · N427FE · Airbus A310203 · Vertical Stabilizer, Spar/RibSDR 06FDEA2010Seat Track · corrodedCENTER SEAT TRACK HAS CORROSION BETWEEN FR 73 & FR 79. SIX AREAS OF CORROSION NOTED, FIVE AREAS WITHIN LIMITS IAW A310 SRM 53-10-16 FIG 101, ONE EA AREA FOUND OUT OF LIMITS IAW A310 SRM 53-10-16 FIG 101, NOTED AREA NR 3. REPAIRED AREA NR 3 IAW A310 SRM 53-10May 25, 2006 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA0925Spacer · misinstalledAFTER LANDING NOTED NO RIGHT BRAKES AVAILABLE, BRAKE RELEASE LIGHTS IN VIEW BUT NO BRAKING PRESSURE. REMOVED 3, 4, 7 AND 8 TIRE ASSY AS PER A310 M/M 12-37-32. FOUND SPACER P/N 2606840 (4 EA) INSTALLED INCORRECTLY (SPACER WAS INSTALLED BETWEEN BRAKE AND TIRE Nov 22, 2005 · N427FE · Airbus A310203 · Landing Gear Brake SystemSDR 05FDEA00884Coalescer Bag · contaminatedON TAKEOFF ROLL JUST PRIOR TO V1, ODOR NOTED, THEN AT 300 FEET, MAIN DECK CARGO DET ILLUMINATED WITH APPROPRIATE ECAM. ATB KMEM 18R, CLEARED RWY. EMERGENCY GROUND PERSONNEL NOTED STRONG ELECTRICAL ODOR NO FUMES. DURING DEBRIEF, CREW REPORTED ECAM MESSAGE TOApr 7, 2005 · N427FE · Airbus A310203 · Humidity Control SystemSDR 04FDEA02998Duct · leakingENGINE FIRE NR 1 ENG (NAC FIRST WENT TO 120 DEG). SHUT DOWN, PULLED FIRE HANDLE AND COMPLIED WITH ECAM/QRH. ENT BY: 439732 RPT BY: 056165 SHGN 28OCT04 16:06 MEM R PER FLT CREW DEBRIEF ENGINE SHUT DOWN OIL PRESSURE NORMAL AND FIRED NR 1 BOTTLE THEN FIRE Oct 28, 2004 · N427FE · Airbus A310203 · Air Distribution SystemSDR 04FDEA02727Damper · failedON TAKEOFF FROM IAD, GEAR WOULD NOT RETRACT ON BOTH SYSTEM 2 OR SYSTEM 1. CHECK QRM, HOLD FOR FUEL BURN. APPROACH TO 19R IAD NORMAL. ENT BY: 262258 RPT BY: 053758. T/S PROBLEM, FOUND ACTUATOR LOW IN FLUID AND PRESSURE. THE ACTUATOR IS LEAKING FLUID ,THE Sep 18, 2004 · N427FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR 04FDEA02498Adc · malfunctionedAT 80 KTS THE F/O CALLED NO AIRSPEED. REJECTED T/O MAX SPEED 85 KTS. F/O HAD NO AIRSPEED INDICATIONS ON PFD, F/O PITOT PROBE BAGGED AND STATIC LINE PURGED WITH DRY N2 FROM NR 2 ADC, NO BLOCKAGE OR CONTAMINATION FOUND. CHANGED NR 2 ADC PER AMM SUPPLEMENT 34-Aug 18, 2004 · N427FE · Airbus A310203 · Air Data ComputerSDR 04FDEA02047Computer · malfunctionedAFTER TAKEOFF NR 1 SYSTEM FAULT, FLAPS RETRACTED NORMAL FROM 20/20. NEXT RETRACTION GOT BOTH SYSTEM 1 & 2 FAULT. SLATS LOCKED AT 15 DEG. FOLLOWED QRH PROCEDURES, RECYCLED AND NO HELP. SET UP FOR SLATS 15 STUCK LANDING. SFCC NR 2 WAS REMOVED AND REPLACED DJul 12, 2004 · N427FE · Airbus A310203 · Leading Edge Slat Control SystemSDR 04FDEA01937Controller · malfunctionedON TAKEOFF DURING SLAT FLAP RETRACTION SYSTEM 2 FLAP FAULT LIGHT ON OVERHEAD PANEL CAME ON WITH ACCOMPANIED ECAM WARNING. ALSO, SPEED LIMIT WARNING (LOCATED AT THE BASE OF THE FIRST OFFICERS PFD CAME ON). SELECTED ADC INST ON FO'S SIDE SWITCHING PANEL AND SPJul 5, 2004 · N427FE · Airbus A310203 · Trailing Edge Flap Control System
Back to N427FE, cancelled Feb 20, 2024