# Service difficulty reports: N450FE, cancelled Apr 23, 2020

A list on [N450FE, cancelled Apr 23, 2020](https://openairdocs.org/deregistered/N450FE-2020-04-23.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 6 · 270 reports

- [SDR FDEA201402030253](https://openairdocs.org/sdr/FDEA201402030253.md): Pressure Switch · faulty · Feb 3, 2014 · N450FE · Airbus A310222 · Hydraulic System, Main
  > NR 2 ENG GREEN HYD PUMP LOW PRESS WHEN SETTING TAKEOFF POWER. DISCONTINUED TAKEOFF. REMOVED OLD NR 2 ENG GREEN PUMP PRESS SWITCH 112GK & REPLACED WITH NEW SWITCH IAW AMM 29-11-62-04. LEAK & OPERATIONS CHECKED GOOD. ACFT OK TO CONTINUE.
- [SDR FDEA201310252615](https://openairdocs.org/sdr/FDEA201310252615.md): Skin · dented · Oct 25, 2013 · N450FE · Airbus A310222 · Trailing Edge Flaps
  > LT INBD FLAPS T/E LOWER SURFACE HAS NUMEROUS DENTS. FOUND WITHIN LIMITS IAW SRM 57-52-12, FIG 101, DETAIL IV. TWO DENTS, PUNCTURED, REPAIRED DENTS IAW SRM 57-52-12 AND SRM 51-77-12, PARA 4B. MAJOR REPAIR.
- [SDR FDEA201310202564](https://openairdocs.org/sdr/FDEA201310202564.md): Support · corroded · Oct 20, 2013 · N450FE · Airbus A310222 · Wing, Landing Gear Attach Fittings
  > RIGHT MLG RIB 5, FWD LUG LOWER SURFACE IS CORRODED. RT MLG RIB 5 FWD LUG CORROSION. R & R IAW REPAIR DWG R57249389, REV B IAW EA 6-5710-T0302172, PART 1. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310172530](https://openairdocs.org/sdr/FDEA201310172530.md): Skin · damaged · Oct 17, 2013 · N450FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FOUND DAMAGE TO SKIN AT FRAME 87 BETWEEN STRINGERS 25-30R, REPAIRED IAW EA 6-5330-T0302997, PART 1. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201310172528](https://openairdocs.org/sdr/FDEA201310172528.md): Skin · damaged · Oct 17, 2013 · N450FE · Airbus A310222 · Trailing Edge Flaps
  > RIGHT WING INBD TE FLAPS LOWER SURFACE HAS IMPACT DAMAGE. REPAIRED IAW SRM 57-52-12, PARA 4.D, FIG 204. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310172532](https://openairdocs.org/sdr/FDEA201310172532.md): Skin · corroded · Oct 17, 2013 · N450FE · Airbus A310222 · Trailing Edge Flaps
  > LEFT OTBD FLAPS T/E LOWER SURFACE HAS CORROSION LOCATED 22 INCHES INBD OF NR 5 FLAP TRACK. PERFORMED REPAIR IAW SRM 57-53-12, FIG 209. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310172529](https://openairdocs.org/sdr/FDEA201310172529.md): Lug · corroded · Oct 17, 2013 · N450FE · Airbus A310222 · Wing, Landing Gear Attach Fittings
  > LEFT MLG RIB 5 FWD LUG LOWER SURFACE IS CORRODED. R & R IAW REPAIR DWG R57249389, REV B IAW EA 6-5710-T0302173. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310152508](https://openairdocs.org/sdr/FDEA201310152508.md): Skin · corroded · Oct 15, 2013 · N450FE · Airbus A310222 · Elevator, Plate/Skin
  > LEFT ELEVATOR LOWER SKIN HAS A SPOT OF CORROSION LOCATION 5 INCHES FROM T/E, 15 INCHES FROM TIP. PERFORMED REPAIR ON LT ELEVATOR SKIN IAW SRM 55-21-11, FIG 209. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310152509](https://openairdocs.org/sdr/FDEA201310152509.md): Skin · cracked · Oct 15, 2013 · N450FE · Airbus A310222 · Wing, Plate/Skin
  > RT WING, RIB 9 LOWER SKIN FWD EDGE CRACKED. REPAIRED SKIN IAW DWG R572-57208 & EA 6-5710-T0302280. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310132493](https://openairdocs.org/sdr/FDEA201310132493.md): Stringer · corroded · Oct 13, 2013 · N450FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > STRINGER 44R FWD OF FRAME 17 HAS CORROSION AROUND RIVET. REPAIRED STRINGER IAW SRM 53-12-14. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310132494](https://openairdocs.org/sdr/FDEA201310132494.md): Mount · corroded · Oct 13, 2013 · N450FE · Airbus A310222 · Engine Mount Section
  > TWO FWD ENGINE MOUNTS HAVE PITTING CORROSION IN BOTH FWD MOUNT HOLES AND THE AFT OTBD MOUNT HOLE. PERFORMED REPAIR IAW SRM 54-51-18 WITH FABRICATED BUSHINGS.
- [SDR FDEA201310132492](https://openairdocs.org/sdr/FDEA201310132492.md): Angle · bent · Oct 13, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > AFT FUSELAGE THS BAY WEB AT FRAMES 89 & 84 UPPER ANGLE BENT STRINGER 32L. REPLACED WEB UPPER ANGLE IAW SRM 51-40-21. F
- [SDR FDEA201310132491](https://openairdocs.org/sdr/FDEA201310132491.md): Angle · bent · Oct 13, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > THS BAY WEB UPPER ANGLE BENT LOCATION, STRINGER 32R, BETWEEN FRAMES 86 & 87. REPLACED WEB UPPER ANGLE IAW SRM 53-19-18.
- [SDR FDEA201310092461](https://openairdocs.org/sdr/FDEA201310092461.md): Mount · corroded · Oct 9, 2013 · N450FE · Airbus A310222 · Engine Mount Section
  > NR 2 PYLON AFT ENGINE MOUNT HAS CORROSION ON FWD & AFT SIDES OF MOUNT, ON INBD AND OTBD, HORIZONTALLY POSITIONED BOLTS, RECESSED AREAS. REPAIRED IAW EA 6-5451-T0302401 PART 1. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201310092460](https://openairdocs.org/sdr/FDEA201310092460.md): Skin · dented · Oct 9, 2013 · N450FE · Airbus A310222 · Ailerons
  > RIGHT WING ALL SPEED AILERON BOTTOM SKIN HAS DENT LOCATION 27.5 IN FROM INBD, 17IN FROM FWD END. REPAIRED IAW SRM 57-61-12, PB 201, PARAGRAPH 4.A. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310082451](https://openairdocs.org/sdr/FDEA201310082451.md): Seat Track · damaged · Oct 8, 2013 · N450FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK DAMAGED AT FRAME 40-42, -Y1959 REPAIRED IAW SRM 53-10-16, PARA 5, FIG 203, SH 5, FABRICATED & INSTALLED SEAT TRACK IAW SRM 51-27-11 & SRM 51-40-21. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201310032398](https://openairdocs.org/sdr/FDEA201310032398.md): Web · cracked · Oct 3, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > FOUND WEB BETWEEN FRAMES 86 - 87 STRINGER 35R CRACKED. R & R WEB IAW SRM 51-40-21. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA201309302352](https://openairdocs.org/sdr/FDEA201309302352.md): Skin · damaged · Sep 30, 2013 · N450FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > ACCESS DOOR 136AR EXTERNAL SKIN CUTOUT RADIUS IS OUT OF TOLERANCE. REPLACED ACCESS DOOR 136AR SKIN IAW SRM 52-41-15 & DWG 14A52475000.
- [SDR FDEA201309292337](https://openairdocs.org/sdr/FDEA201309292337.md): Profile · chafed · Sep 29, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > AFT CABIN PROFILE TEE, FRAME 80, STR 34L, WEB CHORD CHAFED. REPLACED DAMAGED PROFILE TEE IAW SRM 51-40-21.
- [SDR FDEA201309262322](https://openairdocs.org/sdr/FDEA201309262322.md): Tee Fitting · chafed · Sep 26, 2013 · N450FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > AFT CABIN FRAME 80, S34R WEB ANGLE CHAFED REPLACED DAMAGED PROFILE TEE WITH FABRICATED PROFILE TEE AT FRAME 80, STR 34R IAW SRM 51-40-21. PROFILE FABRICATED IAW SRM 53-18-18.
- [SDR FDEA201309252309](https://openairdocs.org/sdr/FDEA201309252309.md): Floorboard · delaminated · Sep 25, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FWD MAIN DECK CARGO UTILITY AREA LAVATORY FLOORBOARD, MULTIPLE AREAS HAS DAMAGED AND DELAMINATION. FABRICATED FLOORBOARD IAW SRZ-25-005. AND INSTALLED. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309252308](https://openairdocs.org/sdr/FDEA201309252308.md): Floorboard · damaged · Sep 25, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FWD CABIN FLOORBOARD 222DF EDGE HAS HONEYCOMB CHIPPED OFF, FABRICATED FLOORBOARD IAW SRZ-25-005 AND INSTALLED. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309232287](https://openairdocs.org/sdr/FDEA201309232287.md): Skin · dented · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > LOWER FUSELAGE SKIN, FRAME 19- 20, STR 34 -35R DENTED. REPAIRED IAW SRM 53-10-12 FIG 226 (SHEET 2). REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309232292](https://openairdocs.org/sdr/FDEA201309232292.md): Floor Panel · cracked · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN DECK CARGO FRAMES 60-62, BETWEEN Y953 AND Y1456 FLOOR PANEL 251UF CRACKED. REPLACED PANEL. PANEL FABRICATED IAW DWG SRZ-25-005.
- [SDR FDEA201309232289](https://openairdocs.org/sdr/FDEA201309232289.md): Floorboard · cracked · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOORBOARD 231BG HAS A CRACK. REPLACED FLOORBOARD. FLOORBOARD FABRICATED ON TRAVELER T13/1025840 IAW DWG SRZ-25-005 & INSTALLED ON WC 230-SWC-FIT.
- [SDR FDEA201309232288](https://openairdocs.org/sdr/FDEA201309232288.md): Floorboard · damaged · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOORBOARD 231ZF HAS DAMAGE IN SEVERAL AREAS. FABRICATED & REPLACED FLOORBOARD.
- [SDR FDEA201309232286](https://openairdocs.org/sdr/FDEA201309232286.md): Skin · damaged · Sep 23, 2013 · N450FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF STRINGER REPAIR AT FR 72 2 EA HOLES HAVE EXCESSIVE PITCH AT STRINGER 41R. ACCOMPLISHED CATEGORY B SKIN REPAIR AT FR 72 STR 41R IAW SRM 53-10-12, FIG 225SH. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309192310](https://openairdocs.org/sdr/FDEA201309192310.md): Skin · dented · Sep 19, 2013 · N450FE · Airbus A310222 · Ailerons
  > RT WING ALL SPEED AILERON BOTTOM SKIN HAS DENT LOCATION 3 INCHES FROM INBD, 24 INCHES FROM T/E. REPAIRED IAW SRM 57-61-12, FIG 201, PAGE 204. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309192262](https://openairdocs.org/sdr/FDEA201309192262.md): Floorboard · damaged · Sep 19, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FWD CABIN FLOORBOARD 221AF, EDGE HAS HONEYCOMB PIECE CHIPPED OFF/CRACKED. REPLACED FLOORBOARD. REPAIR CLASSIFIED AS A MAJOR.
- [SDR FDEA201309192259](https://openairdocs.org/sdr/FDEA201309192259.md): Floor Panel · damaged · Sep 19, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 242JK BROKEN. FLOOR PANEL FABRICATED AND INSTALLED. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309192258](https://openairdocs.org/sdr/FDEA201309192258.md): Floor Panel · cracked · Sep 19, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > CENTER MAIN DECK CARGO, RT SIDE FLOOR PANEL 242WH BOTTOM SURFACE HAS MULTIPLE PUNCTURED & CRACKED ON INBD EDGE. NEW FLOOR PANEL FABRICATED AND INSTALLED. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309192257](https://openairdocs.org/sdr/FDEA201309192257.md): Floor Panel · gouged · Sep 19, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN DECK FLOOR PANEL 222JF PUNCTURED, LOWER SIDE. FLOOR PANEL FABRICATED AND INSTALLED. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309192256](https://openairdocs.org/sdr/FDEA201309192256.md): Floor Panel · damaged · Sep 19, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL 162HF, METALLIC COVER PEELED, REPLACED FLOOR PANEL. FABRICATED NEW FLOOR PANEL. INSTALLED FLOOR PANEL ON WC 160-FL-FIT. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309192255](https://openairdocs.org/sdr/FDEA201309192255.md): Floor Panel · damaged · Sep 19, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL 147AF, UPPER SURFACE HAS COMPOSITE EXPOSED. REPLACED FLOOR PANEL. FLOOR PANEL FABRICATED. INSTALLED ON WC 130-FL-FIT. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309192254](https://openairdocs.org/sdr/FDEA201309192254.md): Floor Panel · damaged · Sep 19, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL 143CF LOWER EDGE COMPOSITE BROKEN. REPLACED FLOOR PANEL 143CF. FLOOR PANEL FABRICATED AND INSTALLED ON WC 130-FL-FIT. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201309152235](https://openairdocs.org/sdr/FDEA201309152235.md): Floor Panel · gouged · Sep 15, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CARGO, FRAME 65-69 BETWEEN SEAT TRACK Y450 AND Y953 FLOOR PANEL 251ZF, PUNCTURED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 & INSTALLED IAW SRM 51-40-21.
- [SDR FDEA201309152234](https://openairdocs.org/sdr/FDEA201309152234.md): Floor Panel · delaminated · Sep 15, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL BETWEEN FR 32-FR 33, Y450 AROUND HOLE DELAMINATED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005 AND INSTALLED IAW SRM 51-40-21.
- [SDR FDEA201309142229](https://openairdocs.org/sdr/FDEA201309142229.md): Floorboard · damaged · Sep 14, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOORBOARD 251MK DAMAGED. FABRICATED NEW FLOORBOARD.
- [SDR FDEA201309142224](https://openairdocs.org/sdr/FDEA201309142224.md): Floor Panel · damaged · Sep 14, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > AFT MAIN CARGO FLOOR PANEL FR 77-80/82 -Y1959 IS BROKEN ON AFT END. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201309142222](https://openairdocs.org/sdr/FDEA201309142222.md): Floor Panel · damaged · Sep 14, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL 242TF PUNCTURED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201309142221](https://openairdocs.org/sdr/FDEA201309142221.md): Floor Panel · punctured · Sep 14, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FRAME 36-38.2, FLOOR PANEL 231 VF HAS MULTIPLE DENT AND PUNCTURED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201309142220](https://openairdocs.org/sdr/FDEA201309142220.md): Floor Panel · damaged · Sep 14, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL 232YF DAMAGED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201309142219](https://openairdocs.org/sdr/FDEA201309142219.md): Floorboard · damaged · Sep 14, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN CARGO DECK FLOORBOARD 231TF DAMAGED. FABRICATED NEW FLOORBOARD IAW SRZ-25-005.
- [SDR FDEA201309142218](https://openairdocs.org/sdr/FDEA201309142218.md): Floor Panel · damaged · Sep 14, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > MAIN DECK CARGO FLOOR PANEL 232TF DAMAGED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201309132210](https://openairdocs.org/sdr/FDEA201309132210.md): Floor Panel · cracked · Sep 13, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FRAMES 60-62 BETWEEN SEAT TRACKS Y450 AND Y953, FLOOR PANEL 252SF CRACKED. FABRICATED FLOOR PANEL IAW SRZ 25-005.
- [SDR FDEA201309132216](https://openairdocs.org/sdr/FDEA201309132216.md): Floorboard · cracked · Sep 13, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOORBOARD 252UF CRACKED, FRAMES 60-62 BETWEEN SEAT TRACK -Y953 AND -Y1456. FABRICATED NEW FLOORBOARD IAW SRZ-25-005.
- [SDR FDEA201309132215](https://openairdocs.org/sdr/FDEA201309132215.md): Floor Panel · cracked · Sep 13, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FLOOR PANEL CRACKED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201309132214](https://openairdocs.org/sdr/FDEA201309132214.md): Floor Panel · damaged · Sep 13, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FRAMES 54.2 - 54.3 BETWEEN SEAT TRACKS Y450 AND Y953 FLOOR PANEL 251GF DAMAGED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201309132213](https://openairdocs.org/sdr/FDEA201309132213.md): Floor Panel · damaged · Sep 13, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FRAMES 60-62 BETWEEN SEAT TRACK Y450 AND Y953 FLOOR PANEL 251SF DAMAGED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201309132212](https://openairdocs.org/sdr/FDEA201309132212.md): Floor Panel · damaged · Sep 13, 2013 · N450FE · Airbus A310222 · Fuselage Floor Panel
  > FRAMES 60-62, BETWEEN SEAT TRACK Y953 AND Y1456 FLOOR PANEL 251RG PUNCTURED AND DAMAGED. FABRICATED NEW FLOOR PANEL IAW SRZ-25-005.

Next page: https://openairdocs.org/deregistered/N450FE-2020-04-23/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 = 'N450FE' AND deregistration_id = 'N450FE-2020-04-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N450FE-2020-04-23/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.