# Service difficulty reports: N427FE, cancelled Feb 20, 2024

A list on [N427FE, cancelled Feb 20, 2024](https://openairdocs.org/deregistered/N427FE-2024-02-20.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 56 reports

- [SDR FDEA201506031688](https://openairdocs.org/sdr/FDEA201506031688.md): Unknown · malfunctioned · Jun 3, 2015 · N427FE · Airbus A310203 · Cabin Pressure Control System
  > LOST 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.
- [SDR FDEA201504141230](https://openairdocs.org/sdr/FDEA201504141230.md): Nut · lack of lube · Apr 14, 2015 · N427FE · Airbus A310203 · Trailing Edge Flap Control System
  > ON 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 WHE
- [SDR FDEA201312132980](https://openairdocs.org/sdr/FDEA201312132980.md): Valve · failed · Dec 13, 2013 · N427FE · Airbus A310203 · Pressure Regulator/Outflow Valve
  > ON 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. PER
- [SDR FDEA201308242031](https://openairdocs.org/sdr/FDEA201308242031.md): Window · cracked · Aug 24, 2013 · N427FE · Airbus A310203 · Flight Compartment Windows
  > CAPTAIN'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.
- [SDR FDEA201308201962](https://openairdocs.org/sdr/FDEA201308201962.md): Fitting · cracked · Aug 20, 2013 · N427FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826.
- [SDR FDEA201308201961](https://openairdocs.org/sdr/FDEA201308201961.md): Fitting · cracked · Aug 20, 2013 · N427FE · Airbus A310203 · Fuselage Main, Attach Fittings
  > FRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826.
- [SDR FDEA201308161913](https://openairdocs.org/sdr/FDEA201308161913.md): Frame · cracked · Aug 16, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame
  > FUSELAGE FRAME 40, UPPER CORNER FOUND CRACK IN RT NR 2 HOLE COMPLIED WITH EA 6-5710-T0301577.
- [SDR FDEA201308131861](https://openairdocs.org/sdr/FDEA201308131861.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame
  > RIGHT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.
- [SDR FDEA201308131860](https://openairdocs.org/sdr/FDEA201308131860.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame
  > RT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5330-T0301676.
- [SDR FDEA201308131859](https://openairdocs.org/sdr/FDEA201308131859.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame
  > RT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.
- [SDR FDEA201308131858](https://openairdocs.org/sdr/FDEA201308131858.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame
  > LEFT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.
- [SDR FDEA201308131857](https://openairdocs.org/sdr/FDEA201308131857.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Frame
  > LEFT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.
- [SDR FDEA201308131856](https://openairdocs.org/sdr/FDEA201308131856.md): Frame · cracked · Aug 13, 2013 · N427FE · Airbus A310203 · Fuselage Main, Structure
  > LEFT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.
- [SDR FDEA201308091817](https://openairdocs.org/sdr/FDEA201308091817.md): Skin · delaminated · Aug 9, 2013 · N427FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > LEFT FWD FUSELAGE TOILET SERVICE PANEL LOWER SKIN CUTOUT DELAMINATED. REPAIRED IAW EA 6-5330-T0301676.
- [SDR FDEA201301210152](https://openairdocs.org/sdr/FDEA201301210152.md): Controller · inoperative · Jan 21, 2013 · N427FE · Airbus A310203 · Cabin Pressure Controller
  > CLIMBING 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. W
- [SDR 08FDEA04940](https://openairdocs.org/sdr/08FDEA04940.md): Warning Light · illuminated · Nov 20, 2008 · N427FE · Airbus A310203 · Door Warning System
  > ON 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.
- [SDR 08FDEA04857](https://openairdocs.org/sdr/08FDEA04857.md): Vane · gouged · Nov 11, 2008 · N427FE · Airbus A310203 · Trailing Edge Flaps
  > LT 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.
- [SDR 08FDEA04856](https://openairdocs.org/sdr/08FDEA04856.md): Adapter · cracked · Nov 11, 2008 · N427FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > MDCC 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.
- [SDR 08FDEA04589](https://openairdocs.org/sdr/08FDEA04589.md): Seat Track · cracked · Oct 28, 2008 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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.
- [SDR 08FDEA04429](https://openairdocs.org/sdr/08FDEA04429.md): Skin · gouged · Oct 19, 2008 · N427FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > LOWER 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.
- [SDR 07FDEA05149](https://openairdocs.org/sdr/07FDEA05149.md): Controller · malfunctioned · Dec 27, 2007 · N427FE · Airbus A310203 · Cabin Pressure Controller
  > EXCESSIVE 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 I
- [SDR 07FDEA04752](https://openairdocs.org/sdr/07FDEA04752.md): Outflow Valve · malfunctioned · Nov 8, 2007 · N427FE · Airbus A310203 · Pressure Regulator/Outflow Valve
  > ON 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/
- [SDR 06FDEA03993](https://openairdocs.org/sdr/06FDEA03993.md): Arm · unknown · Nov 10, 2006 · N427FE · Airbus A310203 · Landing Gear Retraction/Extension System
  > NR 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
- [SDR 06FDEA2357](https://openairdocs.org/sdr/06FDEA2357.md): Angle · corroded · Jun 16, 2006 · N427FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR 06FDEA2356](https://openairdocs.org/sdr/06FDEA2356.md): Skin · corroded · Jun 16, 2006 · N427FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > AFT 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.
- [SDR 06FDEA2258](https://openairdocs.org/sdr/06FDEA2258.md): Floorbeam · cracked · Jun 8, 2006 · N427FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FWD 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.
- [SDR 06FDEA2245](https://openairdocs.org/sdr/06FDEA2245.md): Spar · corroded · Jun 7, 2006 · N427FE · Airbus A310203 · Horizontal Stabilizer, Spar/Rib
  > RIGHT 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.
- [SDR 06FDEA2244](https://openairdocs.org/sdr/06FDEA2244.md): Shear Tie · corroded · Jun 7, 2006 · N427FE · Airbus A310203 · Fuselage Internal Mounting Structure
  > BULK CARGO UNDER FR 68 STR 57 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED SHEAR TIE IAW A310-200 SRM 51-40-21.
- [SDR 06FDEA2243](https://openairdocs.org/sdr/06FDEA2243.md): Skin · corroded · Jun 7, 2006 · N427FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > AFT 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.
- [SDR 06FDEA2242](https://openairdocs.org/sdr/06FDEA2242.md): Skin · corroded · Jun 7, 2006 · N427FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > ATF 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.
- [SDR 06FDEA2241](https://openairdocs.org/sdr/06FDEA2241.md): Structure · corroded · Jun 7, 2006 · N427FE · Airbus A310203 · Vertical Stabilizer Miscellaneous Structure
  > VERT STAB BOX LOWER SURFACE AT FR 84 HAS CORR STR 2L REF N00680. COMPLIED WITH EA 6-5530-101044.
- [SDR 06FDEA2240](https://openairdocs.org/sdr/06FDEA2240.md): Attach Fitting · cracked · Jun 7, 2006 · N427FE · Airbus A310203 · Stabilizer Actuator
  > THS 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.
- [SDR 06FDEA2239](https://openairdocs.org/sdr/06FDEA2239.md): Doubler · corroded · Jun 7, 2006 · N427FE · Airbus A310203 · Fuselage Main, Structure
  > ACCESS 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.
- [SDR 06FDEA2142](https://openairdocs.org/sdr/06FDEA2142.md): Spar · corroded · May 31, 2006 · N427FE · Airbus A310203 · Horizontal Stabilizer, Spar/Rib
  > RT 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-
- [SDR 06FDEA2141](https://openairdocs.org/sdr/06FDEA2141.md): Floorbeam · cracked · May 31, 2006 · N427FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FOUND 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.
- [SDR 06FDEA2140](https://openairdocs.org/sdr/06FDEA2140.md): Floor Support · corroded · May 31, 2006 · N427FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > MAIN 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.
- [SDR 06FDEA2036](https://openairdocs.org/sdr/06FDEA2036.md): Stringer · corroded · May 26, 2006 · N427FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > AFT 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.
- [SDR 06FDEA2035](https://openairdocs.org/sdr/06FDEA2035.md): Skin · dented · May 26, 2006 · N427FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > RT 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 131/132
- [SDR 06FDEA2033](https://openairdocs.org/sdr/06FDEA2033.md): Seat Track · corroded · May 26, 2006 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC L2 SEAT TRACK AT FS 70 AND FS 72 HAS CORROSION REF N00587. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-40-21.
- [SDR 06FDEA2034](https://openairdocs.org/sdr/06FDEA2034.md): Seat Track · corroded · May 26, 2006 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC 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.
- [SDR 06FDEA2032](https://openairdocs.org/sdr/06FDEA2032.md): Seat Track · corroded · May 26, 2006 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND 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.
- [SDR 06FDEA2031](https://openairdocs.org/sdr/06FDEA2031.md): Spar · corroded · May 26, 2006 · N427FE · Airbus A310203 · Vertical Stabilizer, Spar/Rib
  > FOUND 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.
- [SDR 06FDEA2010](https://openairdocs.org/sdr/06FDEA2010.md): Seat Track · corroded · May 25, 2006 · N427FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > CENTER 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 53-10
- [SDR 06FDEA0925](https://openairdocs.org/sdr/06FDEA0925.md): Spacer · misinstalled · Nov 22, 2005 · N427FE · Airbus A310203 · Landing Gear Brake System
  > AFTER 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
- [SDR 05FDEA00884](https://openairdocs.org/sdr/05FDEA00884.md): Coalescer Bag · contaminated · Apr 7, 2005 · N427FE · Airbus A310203 · Humidity Control System
  > ON 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 TO
- [SDR 04FDEA02998](https://openairdocs.org/sdr/04FDEA02998.md): Duct · leaking · Oct 28, 2004 · N427FE · Airbus A310203 · Air Distribution System
  > ENGINE 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
- [SDR 04FDEA02727](https://openairdocs.org/sdr/04FDEA02727.md): Damper · failed · Sep 18, 2004 · N427FE · Airbus A310203 · Landing Gear Retraction/Extension System
  > ON 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
- [SDR 04FDEA02498](https://openairdocs.org/sdr/04FDEA02498.md): Adc · malfunctioned · Aug 18, 2004 · N427FE · Airbus A310203 · Air Data Computer
  > AT 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-
- [SDR 04FDEA02047](https://openairdocs.org/sdr/04FDEA02047.md): Computer · malfunctioned · Jul 12, 2004 · N427FE · Airbus A310203 · Leading Edge Slat Control System
  > AFTER 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 D
- [SDR 04FDEA01937](https://openairdocs.org/sdr/04FDEA01937.md): Controller · malfunctioned · Jul 5, 2004 · N427FE · Airbus A310203 · Trailing Edge Flap Control System
  > ON 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 SP

Next page: https://openairdocs.org/deregistered/N427FE-2024-02-20/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N427FE-2024-02-20/reports

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