# Service difficulty reports: N455FE, cancelled Feb 3, 2024

A list on [N455FE, cancelled Feb 3, 2024](https://openairdocs.org/deregistered/N455FE-2024-02-03.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 3 · 144 reports

- [SDR FDEA201504101202](https://openairdocs.org/sdr/FDEA201504101202.md): Compensator · failed · Apr 10, 2015 · N455FE · Airbus A310222 · Landing Gear Brake System
  > DURING APPROACH, 2000 & 6 MILES, THE HOT BRAKE LIGHT IN THE CUBE ON THE LG TEST PANEL FLICKERED, FOLLOWED BY ECAM HOT BRAKE WARNINGS FOR ALL 4 WHEELS ON THE LT SIDE, 480, 505. LOWERED GEAR IMMEDIATELY & THE TEMPS KEPT 400, 505 & RISING. FIRE DEPARTMENT SAW
- [SDR FDEA201409102582](https://openairdocs.org/sdr/FDEA201409102582.md): Actuator · failed · Sep 10, 2014 · N455FE · Airbus A310222 · Landing Gear Actuator
  > UPON GEAR RETRACTION, RECEIVED A LT MAIN GEAR RED UNLOCK INDICATION WITH AN AMBER LT DOOR LIGHT. COMPLIED WITH ECAM EXTENDED GEAR & LANDED. WE DID HAVE A LOUD WIND NOISE WITH THE PROBLEM, PRETTY SURE DOOR WAS OPEN. DEBRIEFED CREW & VERIFIED THEY DID ATTEMPT
- [SDR FDEA201408212293](https://openairdocs.org/sdr/FDEA201408212293.md): Sequence Valve · faulty · Aug 21, 2014 · N455FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > DURING CLIMB OUT AT GEAR RETRACTION, LT MAIN GEAR DID NOT APPEAR TO RETRACT & DOOR SHOWED OPEN. ECAM INDICATED LG RETRACTION INOPERATIVE. FUEL CONSUMPTION INCREASED. SELECTED OPPOSITE SYS & CYCLED THE GEAR, NO HELP. COMPLIED WITH ECAM & QRH. DECLARED AN EM
- [SDR FDEA201405221136](https://openairdocs.org/sdr/FDEA201405221136.md): Valve · failed · May 22, 2014 · N455FE · Airbus A310222 · Leading Edge Slat Control System
  > NR 1 SLAT SYS FAULT LIGHT DURING FINAL. RECYCLING DID NOT CORRECT, QRH PROCEDURES ACCOMPLISHED. SLAT FAULT LIGHT REMAINED ON, BUT SPFI SHOWED SLATS & FLAPS 30 & 40 LANDING NORMAL. DECLARED LANDING EMERGENCY. LANDING NORMAL. REMOVED AND REPLACED PCU VALV
- [SDR FDEA201403050452](https://openairdocs.org/sdr/FDEA201403050452.md): Switch · failed · Mar 5, 2014 · N455FE · Airbus A310222 · Engine Thrust Reverser
  > ACCELERATING ABOVE 10,000 & 250 KTS, NR 1 ENGINE THRUST REVERSER UNLOCK ILLUMINATED STEADY. ALL OTHER INDICATIONS NORMAL. TROUBLESHOT IAW TSM 78-31-00, FOUND THE RT MASTER ACTUATOR SECONDARY LOCK SWITCH INOPERATIVE. REMOVED AND REPLACED THE NR 1 ENGINE RT
- [SDR FDEA201305090953](https://openairdocs.org/sdr/FDEA201305090953.md): Brake Sys · malfunctioned · May 9, 2013 · N455FE · Airbus A310222 · Landing Gear Brake System
  > ACFT LOST BRAKES. THEY HAD WORKED NORMALLY ON INITIAL TAXI AND HOLD SHORT CROSSING RWY 27. APPROACHING 36C ON TAXIWAY D, GOT NO BRAKING WITH NORMAL. RELEASED BRAKES, WENT TO ALT ON. AGAIN NO BRAKING. WENT TO IDLE REVERSE. RELEASED PEDALS AND TRIED ALT O
- [SDR FDEA201303130565](https://openairdocs.org/sdr/FDEA201303130565.md): Valve · malfunctioned · Mar 13, 2013 · N455FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > LANDING GEAR FAILED TO EXTEND IN POSITION NR 1 OR NR 2. COMPLIED W/ QRH - MANUAL EXTENSION OK. EMERGENCY DECLARED. T/S IAW TSM 32-61-00. PREFORMED BITE TEST PROX DET. BOX FOUND FAULT CODES P2, P4. (EXTERNAL PWR SUPPLY BUS). IAW MM 32-33-00-02 RESTORED
- [SDR FDEA201212044242](https://openairdocs.org/sdr/FDEA201212044242.md): Shutoff Valve · malfunctioned · Dec 4, 2012 · N455FE · Airbus A310222 · Engine Thrust Reverser
  > DURING CLIMBOUT PASSING 10000 FT, ECAM INDICATED THRUST REV NR 1 UNLOCKED. THIS INDICATION CYCLED IN AND OUT MULTIPLE TIMES. NO OTHER ENGINE INDICATIONS PRESENT. R & R NR 1 THRUST REVERSER PRSOV IAW MM 78-31-05-04. LEAK CHECKED OK. PERFORMED OPS CHECK OF
- [SDR FDEA201210133610](https://openairdocs.org/sdr/FDEA201210133610.md): Handle · sticking · Oct 13, 2012 · N455FE · Airbus A310222 · Landing Gear Brake System
  > AS POWER WAS INCREASING AFTER TOGA ON TAKE OFF, RECEIVED A CRC FOR "PARKING BRAKE SET" EVEN THOUGH PARKING BRAKE HANDLE WAS DOWN. SECOND TAKE OFF ATTEMPT OK. INSPECTED PARK BRAKE LINKAGE FOR CORRECT OPERATION NO DEFECTS NOTED, CLEANED CONNECTOR AT 7GG, FO
- [SDR FDEA201205312039](https://openairdocs.org/sdr/FDEA201205312039.md): Pressure Switch · failed · May 31, 2012 · N455FE · Airbus A310222 · Engine Oil Indicating System
  > DESCENDING OUT OF FL310 WE GOT AN OIL CLOG LIGHT ON NR 1 ENGINE. COMPLIED WITH PROCEDURES, SHUTDOWN NR 1 ENGINE. ALL OIL PRESSURES INDICATED NORMAL BEFORE AFTER SHUTDOWN. AFTER ENGINE SHUTDOWN NR 1 OIL CLOG LIGHT REMAINED ON. T/S IAW TSM 79-00-00, FIG
- [SDR FDEA201112085220](https://openairdocs.org/sdr/FDEA201112085220.md): Oil System · low pressure · Dec 8, 2011 · N455FE · Airbus A310222 · Engine Oil Pressure
  > YELLOW OIL PRESSURE LIGHT ILLUMINATED DURING TAKE OFF ROLL AT 110 KTS. ABORTED TAKE OFF, COMPLIED WITH QRH. RAN ENGINES AT POWER, OIL PRESSURE STAYED AT 52 PSI IN THE NORMAL RANGE IAW JRH. SUSPECTED COLD ENGINE OIL ON COLD SOAKED ENGINE THAT LAYED OVERNIG
- [SDR FDEA201110194576](https://openairdocs.org/sdr/FDEA201110194576.md): Transmitter · inoperative · Oct 19, 2011 · N455FE · Airbus A310222 · Engine Oil Pressure
  > DURING T/O ROLL THE HIGH OIL PRESSURE (NR 1) ENG, CAME ON AT 80 KTS. R & R THE NR 1 ENG OIL PRESS TRANSMITER IAW MM 79-33-11-04, RAN ENG IAW JRH, CHECKS GOOD. ACFT OK TO CONTINUE.
- [SDR FDEA201110064343](https://openairdocs.org/sdr/FDEA201110064343.md): Hmu · failed · Oct 6, 2011 · N455FE · Airbus A310222 · Fuel Control/Turbine Engines
  > ON TAKEOFF, NR 2 ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMENT. R & R NR 2 ENGINE HMU IAW AMM 73-21-01-04. CHECKED GOOD. PERFORMED IDLE LEAK CHECK AND POWER TRIM RUN IAW MM 71-00-00-05 LEAK CHECKS GOOD AND POWER RUNUP CHECKS GOOD.
- [SDR FDEA201109274156](https://openairdocs.org/sdr/FDEA201109274156.md): Wire Harness · damaged · Sep 27, 2011 · N455FE · Airbus A310222 · Turbine Engine System Wiring
  > REJECTED T/O, SET BOTH ENGINES TO 40 PERCENT N1, TOGA'D AND ENGINE NR1 IMMEDIATELY POWERED UP AND ENGINE 2 STOPPED ACCELERATING AT 50 PERCENT N1. MADE 2ND ATTEMPT BUT REJECTED DUE TO ENGINE 2 WOULD NOT ACCELERATE ABOVE 50 PERCENT N1 EVEN WITH PILOT ATTEMPTED
- [SDR FDEA201107012523](https://openairdocs.org/sdr/FDEA201107012523.md): Selector Valve · malfunctioned · Jul 1, 2011 · N455FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT EXTEND NORMALLY AFTER GEAR HANDLE PLACED IN DOWN POSITION. MANUALLY EXTENDED GEAR. QRH COMPLIED WITH, UNEVENTFUL LANDING MADE. R & R LANDING GEAR SELECTOR VALVE 3GA IAW MM 32-31-12-04.
- [SDR FDEA201105111801](https://openairdocs.org/sdr/FDEA201105111801.md): Latch · malfunctioned · May 11, 2011 · N455FE · Airbus A310222 · Passenger/Crew Doors
  > CLIMBING THRU FL 310 ECAM INDICATED "R FWD CABIN DOOR NOT CLOSED". CABIN PRESSURIZATION INCREASED RATE OF CLIMB FROM 300-400 FPM TO 800 FPM AND CABIN ALTITUDE WAS 8000. SHOULD USUALLY BE AROUND 5600 FPM OR SO. CABIN DOOR SHOWED UNLOCKED ON ECAM BUT LATER SH
- [SDR FDEA201102080502](https://openairdocs.org/sdr/FDEA201102080502.md): Selector Valve · inoperative · Feb 8, 2011 · N455FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT EXTEND WHEN HANDLE WAS PLACED DOWN. PERFORMED "GRAVITY EXTENSION" IAW QRH. EMERGENCY DECLARED AND ACFT WAS STOPPED ON THE RUNWAY BECAUSE OF NWS. LOOKED AT BOTH SYS 1 & 2 BEFORE EXTENDING GEAR MANUALLY. R & R LANDING GEAR SELECTOR VALVE
- [SDR FDEA201101250353](https://openairdocs.org/sdr/FDEA201101250353.md): Flap System · malfunctioned · Jan 25, 2011 · N455FE · Airbus A310222 · Trailing Edge Flap Control System
  > GOT FLAP VANE JAM AND FLAP FAULT ECAM INDICATIONS WHILE EXTENDING FLAPS. THEY STUCK AT LESS THAN 15 DEGREE (APPROX 5 DEGREE). CYCLE TO NO AVAIL WENT AROUND AND REATTEMPTED ON DOWNWIND. SECOND ATTEMPT WAS SUCCESSFUL. FACT ADJUST/TEST FLAP VANE SYS. OP'
- [SDR FDEA201101100184](https://openairdocs.org/sdr/FDEA201101100184.md): Cable · gouged · Jan 10, 2011 · N455FE · Airbus A310222 · Engine Thrust Reverser
  > NR1 PYLON LOWER SIDE OF NACELLE LT & RT THRUST REVERSER INTERLOCK CABLES GOUGED THRU CABLE INSULATION. MARKED, R & R NR1 PYLON LT INTERLOCK CABLE IAW AMM 76-11-41-04, REMOVED NR1 PYLON RT INTERLOCK CABLE IAW AMM, REPAIRED RT INTERLOCK CABLE IAW EA 6-7611-
- [SDR FDEA201012174712](https://openairdocs.org/sdr/FDEA201012174712.md): Door Frame · gouged · Dec 17, 2010 · N455FE · Airbus A310222 · Fuselage Main, Structure
  > LT MLG DOOR TOP AFT INNER MATING SURFACE IS GOUGED. REMOVED GOUGE AND FOUND TO BE OUT OF LIMITS. MATERIAL LOSS 0.022 FROM 0.078., 0.056 MATERIAL REMAINING. FABBED DOUBLER IAW EA 6-5280-136728, " DOORS - LT MLG MAIN DOOR UPPER FRAME". ALODINED AND PRIMED IAW
- [SDR FDEA201012154690](https://openairdocs.org/sdr/FDEA201012154690.md): Tee Fitting · cracked · Dec 15, 2010 · N455FE · Airbus A310222 · Cargo/Baggage Doors
  > BULK CARGO DOOR TEE PROFILE IS CRACKED AT FRAME 68, BEAM 3. REMOVED TEE PROFILE REF SRM 51-40-21, PARA 6. MACHINED NEW TEE PROFILE REF DWG A52378044. LOCATED HOLES ON NEW TEE PROFILE REF SRM 51-40-44. ALODINED NEW TEE PROFILE REF SRM 51-21-10, PG 6. PRIM
- [SDR FDEA201012094623](https://openairdocs.org/sdr/FDEA201012094623.md): Bracket · cracked · Dec 9, 2010 · N455FE · Airbus A310222 · Cargo/Baggage Doors
  > BULK CARGO DOOR STAY BRACKET IS CRACKED AT FRAME 68, BEAM 3. ACQUIRED MATERIAL ID FOR NEW STAY BRACKET IAW SRM 52-34-00, PO 680480.1. FORMED NEW STAY IAW SRM 51-26-00. ALODINED NEW STAY IAW SRM 51-21-10, PARA 4, PG 6. PRIMED & PAINTED NEW STAY IAW SRM 51-23
- [SDR FDEA201011304517](https://openairdocs.org/sdr/FDEA201011304517.md): Angle · cracked · Nov 30, 2010 · N455FE · Airbus A310222 · Nacelle/Pylon Miscellaneous Structure
  > NR1 PYLON ACCESS PANEL 475 AL (STRINGER), RT SIDE, CTR SECTION OF PANEL "T" ANGLE IS CRACKED. REMOVED CRACKED FRAME AND FABBED NEW FRAME FROM 0.063, 2024-0, PO NR673099.1 IAW SRM 54-55-51, FIG 3. HEAT TREATED TO 2024-T3 IAW AMS 2770, REV "H". FIT AND DRI
- [SDR FDEA201011294512](https://openairdocs.org/sdr/FDEA201011294512.md): Stop Fitting · cracked · Nov 29, 2010 · N455FE · Airbus A310222 · Fuselage Main, Structure
  > RT AFT PAX / CREW DOOR STOP FITTING IS CRACKED AT THE INBD LOWER FASTENER; LOWER AFT DOOR FRAME STOP FITTING IN THE DOOR CUTOUT. REPLACED RT AFT PAX DOOR STOP FITTING IAW SRM 51-72-10 AND SRM 51-40-21, PG 5-7.
- [SDR FDEA201011154367](https://openairdocs.org/sdr/FDEA201011154367.md): Floor Support · cracked · Nov 15, 2010 · N455FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > FWD PIT, AFT FLOOR SUPPORT, RT SIDE IS CRACKED BETWEEN FRAME 38.2 AND FRAME 39. REMOVED AND REPLACED AFT FLOOR SUPPORT, R/H SIDE AT FRAME 38.2 IAW SRM 51-40-21, PARA 5 AND 6.
- [SDR FDEA201011124324](https://openairdocs.org/sdr/FDEA201011124324.md): Pressure Panel · corroded · Nov 12, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT HORIZ PRESSURE DECK UPPER SURFACE AT FRAME 40/41 IS CORRODED AT THE SPLICE. REPAIRED PER FEDEX EA 6-5310-136722, TITLE " FUSELAGE - PRESSURIZED FLOOR BETWEEN FR 39 AND FR 40 AT Y-95.3". REMOVED AND RE-INSTALLED 1 EA. SUPPORT BRACKET
- [SDR FDEA201011104306](https://openairdocs.org/sdr/FDEA201011104306.md): Fitting · corroded · Nov 10, 2010 · N455FE · Airbus A310222 · Nacelle/Pylon Miscellaneous Structure
  > NR1 ENGINE PYLON SPIGOT RECEPTICAL FITTING BALL JOINT FLANGE IS PITTED AT THE UPPER AND LOWER PLATES INCLUDING THE BEARING BORE. COMPLIED WITH EA 6-5450-136723; " NACELLES / PYLON - SB A310-54-2020 - NR 1 AND NR2 PYLON SPIGOT FITTING BORE CORROSION".
- [SDR FDEA201011104305](https://openairdocs.org/sdr/FDEA201011104305.md): Fitting · corroded · Nov 10, 2010 · N455FE · Airbus A310222 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 ENG PYLON SPIGOT RECEPTICAL FITTING BALL JOINT FLANGE IS PITTED AT THE UPPER AND LOWER FLANGE PLATES INCLUDING THE BEARING BORE. COMPLIED WITH EA 6-5450-136723; " NACELLES / PYLON - SB A310-54-2020 - NR1 AND NR2 PYLON SPIGOT FITTING BORE CORROSION".
- [SDR FDEA201011084276](https://openairdocs.org/sdr/FDEA201011084276.md): Sidewall Panel · dented · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > BULK CARGP COMPARTMENT SIDEWALL PANEL 161 AW HAS MULTIPLE DENTS AND IS PUNCTURED ON THE FRONT. FABRICATED NEW SIDEWALL PANEL 161 AWIAW FEDEX DWG 25-005, REV "H" AND FEDEX DWG 25-011, REV "C".
- [SDR FDEA201011084281](https://openairdocs.org/sdr/FDEA201011084281.md): Floorboard · damaged · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOORBOARD UPPER SKIN IS CRUSHED AND BROKEN FROM FRAME 60 TO FRAME 62, RBL 57 TO RBL 77. FABRICATED NEW FLOORBOARD 252 UF IAW DWG 25-005, REV "H".
- [SDR FDEA201011084280](https://openairdocs.org/sdr/FDEA201011084280.md): Floorboard · damaged · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN DECK FLOORBOARD BETWEEN FRAME 53 AND FRAME 54, LBL 78 AND LBL 98 IS BROKEN OFF AT THE AFT END. FABRICATED NEW FLOOR PANEL IAW DWG 25-005, REV "H".
- [SDR FDEA201011084279](https://openairdocs.org/sdr/FDEA201011084279.md): Floorboard · damaged · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > AFT CARGO FLOORBOARD 151 FF HAS A BROKEN CORNER. FABRICATED NEW FLOORBOARD 151 FF IAW DWG 25-005, REV "H".
- [SDR FDEA201011084278](https://openairdocs.org/sdr/FDEA201011084278.md): Floorboard · torn · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > FWD CARGO COMPARTMENT FLOORBOARD 132 QF IS TORN AND PUNCTURED. FABRICATED NEW FLOORBOARD 132 QF IAW DWG 25-005, REV "H".
- [SDR FDEA201011084277](https://openairdocs.org/sdr/FDEA201011084277.md): Floor Panel · dented · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > BULK CARGO COMPARTMENT FLOOR PANEL 162 HF TOP SURFACE IS DENTED AND CRUSHED. FABRICATED NEW FLOOR PANEL 162 HF IAW DWG 25-005, REV "H" AND DWG 25-011, REV "C".
- [SDR FDEA201011084275](https://openairdocs.org/sdr/FDEA201011084275.md): Panel · corroded · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT SIDEWALL PANEL 162 AW BOTTOM SKIN IS CORRODED AND BOTH SKINS ARE DISBONDED. FABRICATED NEW SIDEWALL PANEL 162 AW IAW DWG 25-005, REV "H" AND DWG 25-011, REV "C".
- [SDR FDEA201011084274](https://openairdocs.org/sdr/FDEA201011084274.md): Panel · damaged · Nov 8, 2010 · N455FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT SIDE WALL PANEL 162 CW HAS MULTIPLE DENTS ON THE TOP SURFACE. FABRICATED NEW SIDEWALL PANEL 162 CW IAW DWG 25-005, REV "H" AND DWG 25-011, REV "C".
- [SDR FDEA201011054263](https://openairdocs.org/sdr/FDEA201011054263.md): Attach Fitting · corroded · Nov 5, 2010 · N455FE · Airbus A310222 · Fuselage Main, Attach Fittings
  > LT MLG DOOR ACTUATOR ATTACH FITTING IS CORRODED. REMOVED WORN JACK FITTING REF SRM 51-40-21, PAPR 7. INSTALLED NEW JACK FITTING REF SRM 51-40-21, PAPR 7. ALODINED AND PRIMED TOP SKIN REF SRM 51-21-10. APPLIED TOP COAT REF SRM 51-21-11.
- [SDR FDEA201011044252](https://openairdocs.org/sdr/FDEA201011044252.md): Skin · corroded · Nov 4, 2010 · N455FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FUSELAGE INTERNAL STRUCTURE FWD CARGO COMPARTMENT AFT DOOR CUTOUT AT THE LOWER CORNER, THE SKIN IS CORRODED FROM FRAME 26 TO FRAME 27, STR 25R TO STR 26R.
- [SDR FDEA201011024207](https://openairdocs.org/sdr/FDEA201011024207.md): Floor Panel · delaminated · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MLG BAY CTR OTBD FLOOR PANEL IS DELAMINATED AT THE EDGE. REMOVED OLD PANEL 148 BF REF SRM 51-40-21, PARA 5. FABBED NEW MLG OTBD FLOOR PANEL 148 BF IAW DWG SRZ 25-005, REV. INSTALLED NEW FLOOR PANEL 148 BF REF SRM 51-40-21, PARA 5.
- [SDR FDEA201011024221](https://openairdocs.org/sdr/FDEA201011024221.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252 PH IS CRACKED. FABRICATED NEW FLOOR PANEL 252 PH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024220](https://openairdocs.org/sdr/FDEA201011024220.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 232 YH IS CRACKED. FABRICATED NEW FLOOR PANEL 232 YH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024219](https://openairdocs.org/sdr/FDEA201011024219.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252 BF IS CRACKED. FABRICATED NEW FLOOR PANEL 252 BF IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024218](https://openairdocs.org/sdr/FDEA201011024218.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252 UH IS CRACKED. FABRICATED NEW FLOOR PANEL 252 UH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024217](https://openairdocs.org/sdr/FDEA201011024217.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 252 GF IS CRACKED. FABRICATED NEW FLOOR PANEL 252 GF IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024216](https://openairdocs.org/sdr/FDEA201011024216.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242 EK IS CRACKED. FABRICATED NEW FLOOR PANEL 242 EK IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024215](https://openairdocs.org/sdr/FDEA201011024215.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242 ZJ IS CRACKED.
- [SDR FDEA201011024214](https://openairdocs.org/sdr/FDEA201011024214.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242 UJ IS CRACKED. FABRICATED NEW FLOOR PANEL 242 UJ IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024213](https://openairdocs.org/sdr/FDEA201011024213.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 242 QJ IS CRACKED. FABRICATED NEW FLOOR PANEL 242 QJ IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024212](https://openairdocs.org/sdr/FDEA201011024212.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231 BH IS CRACKED. FABRICATED NEW FLOOR PANEL 231 BH IAW DWG SRZ 25-005, REV "H".
- [SDR FDEA201011024211](https://openairdocs.org/sdr/FDEA201011024211.md): Floor Panel · cracked · Nov 2, 2010 · N455FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CABIN FLOOR PANEL 231 AH IS CRACKED. FABRICATED NEW FLOOR PANEL 231 AH IAW DWG SRZ 25-005, REV "H".

Next page: https://openairdocs.org/deregistered/N455FE-2024-02-03/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 = 'N455FE' AND deregistration_id = 'N455FE-2024-02-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N455FE-2024-02-03/reports

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