# Service difficulty reports: N421FE, cancelled Feb 18, 2016

A list on [N421FE, cancelled Feb 18, 2016](https://openairdocs.org/deregistered/N421FE-2016-02-18.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 · 97 reports

- [SDR FDEA200904171573](https://openairdocs.org/sdr/FDEA200904171573.md): Frame · damaged · Apr 17, 2009 · N421FE · Airbus A310222 · Fuselage Main, Frame
  > AFT CARGO COMPARTMENT, EXISTING HOLES WRONGLY DRILLED AT FR 63A, STGR 27 RT. THE FRAME WAS REPAIRED AS PER SRM 53-17-13 FIG 203.
- [SDR FDEA200904061439](https://openairdocs.org/sdr/FDEA200904061439.md): Seat Track · corroded · Apr 6, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WITH CORROSION BTW FR 72 AND FR 73 AT Y0. SEAT TRACK REPAIRED AS PER SRM 53-10-16 FIG 202.
- [SDR FDEA200904061427](https://openairdocs.org/sdr/FDEA200904061427.md): Seat Track · corroded · Apr 6, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WITH CORROSION BETWEEN FR 76 AND FR 77 AT Y1448. SEAT TRACK REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200904031552](https://openairdocs.org/sdr/FDEA200904031552.md): Seat Track · corroded · Apr 3, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WITH SPOTS OF CORROSION BETWEEN FR72-73 AT Y-1456. THE SEAT TRACK WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200904021444](https://openairdocs.org/sdr/FDEA200904021444.md): Skin · damaged · Apr 2, 2009 · N421FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > FUSELAGE, EVALUATE BLENDING AT STGR 43 LT BTW FR 20 AND FR 21. SKIN WAS REPAIRED AS PER SRM 53-10-12 FIG 216 SHEET 1.
- [SDR FDEA200904021438](https://openairdocs.org/sdr/FDEA200904021438.md): Seat Track · corroded · Apr 2, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WITH SPOTS OF CORROSION BTW FR 69-FR 70 AT Y-450. SEAT TRACK REPAIRED BTW FR 68-69 AS PER SRM SUPP 53-10-16 FIG 202.
- [SDR FDEA200904021436](https://openairdocs.org/sdr/FDEA200904021436.md): Seat Track · corroded · Apr 2, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WITH SPOTS OF CORROSION BTW FR58-69 AT Y-953. SEAT TRACK WAS REPAIRED BTW FR 62-63 AND BETWEEN FR 64-65 AS PER SRM 53-10-16 FIG 202.
- [SDR FDEA200904021435](https://openairdocs.org/sdr/FDEA200904021435.md): Seat Track · corroded · Apr 2, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WITH SPOTS OF CORROSION BTW FR 69-71, AT Y-953. THE SEAT TRACK WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200903311709](https://openairdocs.org/sdr/FDEA200903311709.md): Floorbeam · corroded · Mar 31, 2009 · N421FE · Airbus A310222 · Fuselage Main, Floor Beam
  > N1322 AFT CARGO COMPT - FLOORBEAM WITH CORROSION AT FR 63 AND BTW 44-55 LH. THE BEAM WAS REPLACED IN ACCORDANCE WITH 51-72-10.
- [SDR FDEA200903301737](https://openairdocs.org/sdr/FDEA200903301737.md): Hinge Fitting · corroded · Mar 30, 2009 · N421FE · Airbus A310222 · Fuselage, Door Hinge
  > AFT CARGO DOOR HINGE FITTING WAS FOUND WITH CORROSION AT FRAME 63. THE FITTING WAS REPAIRED AS PER EA 6-5310-129288.
- [SDR FDEA200903301736](https://openairdocs.org/sdr/FDEA200903301736.md): Hinge Fitting · corroded · Mar 30, 2009 · N421FE · Airbus A310 · Fuselage, Door Hinge
  > AFT CARGO DOOR HINGE FITTING WAS FOUND WITH CORROSION AT FRAME 62. THE FITTING WAS REPAIRED AS PER FEDEX EA 6-5310-129288.
- [SDR FDEA200903301429](https://openairdocs.org/sdr/FDEA200903301429.md): Seat Track · worn · Mar 30, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WITH WEAR BETWEEN FR62-63 AT Y0. SEAT TRACK REPAIRED BTW FR 62 AND FR 63 AND BETWEEN FR 64 AND FR 65 AS PER SRM SUPP 53-10-16 FIG 202.
- [SDR FDEA200903301426](https://openairdocs.org/sdr/FDEA200903301426.md): Seat Track · corroded · Mar 30, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK WITH CORROSION AND WEAR BETWEEN FR 54.2 AND FR 58 AT Y450. THE RELEVANT SEAT TRACK WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200903271554](https://openairdocs.org/sdr/FDEA200903271554.md): Roller Track · corroded · Mar 27, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > TRACK AT ROLLERS LT SIDE BTW FRAMES 54.2 TO 55 AT STGR 43 WITH CORROSION. ROLLER TRACK REPAIRED AS PER SRM 53-10-15 FIG 203.
- [SDR FDEA200903261407](https://openairdocs.org/sdr/FDEA200903261407.md): Fitting · corroded · Mar 26, 2009 · N421FE · Airbus A310222 · Wing, Landing Gear Attach Fittings
  > RT WING FLAP OTBD, FITTING AT BUSHINGS OF NR 4 TRUNNION WITH CORROSION. THE CORROSION WAS BLENDED AS PER EA 6-5710-127419.
- [SDR FDEA200903251742](https://openairdocs.org/sdr/FDEA200903251742.md): Skin · corroded · Mar 25, 2009 · N421FE · Airbus A310 · Wing, Plate/Skin
  > CENTER WING BOX LOWER SKIN EXTERNAL SURFACE FOUND WITH SEVERAL SPOTS OF CORROSION - REFER TO EA6-5710-129280 FOR DETAILS. REPAIR WAS ACCOMPLISHED AS PER EA 6-5710-129280.
- [SDR FDEA200903251425](https://openairdocs.org/sdr/FDEA200903251425.md): Crossbeam · cracked · Mar 25, 2009 · N421FE · Airbus A310222 · Fuselage Main, Structure
  > CROSSBEAM AT FR36 CRACKED AT Y-953. CROSSBEAM AT FR 36 WAS REPAIRED AS PER SRM SUPP 53-10-15 FIG 201 SHEET2A.
- [SDR FDEA200903251406](https://openairdocs.org/sdr/FDEA200903251406.md): Floorbeam · corroded · Mar 25, 2009 · N421FE · Airbus A310222 · Fuselage Main, Floor Beam
  > ZONE 100 - FUSELAGE - PREVIOUS REPAIR AT FLOORBEAM LOCATED AT FR 55/58 AT Y-1200. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. THE REPAIR WAS REMOVED BECAUSE THE FLOORBEAM WAS REPLACED AS PER TH
- [SDR FDEA200903241734](https://openairdocs.org/sdr/FDEA200903241734.md): Beam · corroded · Mar 24, 2009 · N421FE · Airbus A310 · Passenger/Crew Doors
  > RT FWD PAX DOOR - SPOTS OF CORROSION AT BEAM 3. BEAM 3 WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200903241668](https://openairdocs.org/sdr/FDEA200903241668.md): Beam · corroded · Mar 24, 2009 · N421FE · Airbus A310222 · Fuselage Main, Structure
  > RT FWD PAX DOOR, SPOTS OF CORROSION AT BEAM 3. BEAM 3 WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200903241442](https://openairdocs.org/sdr/FDEA200903241442.md): Track · corroded · Mar 24, 2009 · N421FE · Airbus A310222 · Nacelle/Pylon Miscellaneous Structure
  > NR 1 PYLON, RIB 18, LUG ATTACHMENT WING TO PYLON WITH CORROSION AT ATTACHMENT ROLLER TRACK OF BEARING. REPAIR ACCOMPLISHED AS PER FEDEX EA 6-5450-127411.
- [SDR FDEA200903231708](https://openairdocs.org/sdr/FDEA200903231708.md): Floorbeam · corroded · Mar 23, 2009 · N421FE · Airbus A310222 · Fuselage Main, Floor Beam
  > N938 AFT CARGO COMPT - FLOORBEAM AT FRAME 55/58 WITH SEVERAL SPOTS OF CORROSION BTW STGR 44 AND 45LH- THE FLOORBEAM WAS REPLACED IN ACORDANCE WITH SRM 51-72-10.
- [SDR FDEA200903231437](https://openairdocs.org/sdr/FDEA200903231437.md): Fitting · corroded · Mar 23, 2009 · N421FE · Airbus A310222 · Fuselage Main, Attach Fittings
  > FWD COMPT, CORROSION FOUND BETWEEN FRAMES 24 TO 25 AND STGR 55 RT TO 53 LT. THE FITTING WAS REPAIRED AS PER EA 6-5310-127421.
- [SDR FDEA200903231434](https://openairdocs.org/sdr/FDEA200903231434.md): Skin · cracked · Mar 23, 2009 · N421FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > COCKPIT PLATE FOUND CRACKED AT COCKPIT FLOOR NEXT TO Y-790 BTW FR 0 AND FR 1. THE CRACKED PANEL WAS REPAIRED AS PER FEDEX EA 6-5310-127415.
- [SDR FDEA200903231430](https://openairdocs.org/sdr/FDEA200903231430.md): Seat Track · worn · Mar 23, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK NEXT TO Y0, NEXT TO FR 33 FOUND WORN. SEAT TRACK REPAIRED AS PER FEDEX EA 6-5310-127412.
- [SDR FDEA200903231402](https://openairdocs.org/sdr/FDEA200903231402.md): Floor Support · corroded · Mar 23, 2009 · N421FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > BULK CARGO COMPT, RT FLOOR PANELS LONGITUDINAL SECTION WITH CORROSION AT FR 67 AND FR 65 UNDER STRINGER 49. SECTION LONGITUDINAL WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200903211404](https://openairdocs.org/sdr/FDEA200903211404.md): Floorbeam · corroded · Mar 21, 2009 · N421FE · Airbus A310222 · Fuselage Main, Floor Beam
  > BULK COMPT, CORROSION AT BULK CARGO COMPT FLOORBEAM AT FR 65 ABOVE STRINGER 49 RT. FLOORBEAM REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200903211403](https://openairdocs.org/sdr/FDEA200903211403.md): Floorbeam · corroded · Mar 21, 2009 · N421FE · Airbus A310222 · Fuselage Main, Floor Beam
  > BULK COMPT - CORROSION AT BULK COMPT FLOORBEAM OF FR 64 ABOVE STRINGER 49 RT. FLOORBEAM WAS REPLACED AS PER SRM 51-72-10.
- [SDR FDEA200903191551](https://openairdocs.org/sdr/FDEA200903191551.md): Skin · dented · Mar 19, 2009 · N421FE · Airbus A310222 · Ailerons
  > RT WING AILERON, LOWER SKIN FOUND DAMAGED. LOWER SKIN OF AILERON REPAIRED IN ACCORDANCE WITH SRM 57-61-12 FIG 201.
- [SDR FDEA200903191555](https://openairdocs.org/sdr/FDEA200903191555.md): Track · misrepaired · Mar 19, 2009 · N421FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > PREVIOUS REPAIR (DUMMY TRACK) FOUND LOCATED BETWEEN FR 38.1 AND FR 40 AT Y0. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REP
- [SDR FDEA200903191209](https://openairdocs.org/sdr/FDEA200903191209.md): Stringer · misrepaired · Mar 19, 2009 · N421FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > AREA 100, FUSELAGE, PREVIOUS STRINGER REPAIR FOUND LOCATED BTW FR 21 AND FR 22 AT STGR 51 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REP
- [SDR FDEA200903191208](https://openairdocs.org/sdr/FDEA200903191208.md): Stringer · misrepaired · Mar 19, 2009 · N421FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > AREA 100 - FUSELAGE - PREVIOUS REPAIR AT STRINGER FOUND LOCATED BTW FR21 AND FR 22 AT STGR 50 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM
- [SDR FDEA200903191207](https://openairdocs.org/sdr/FDEA200903191207.md): Stringer · misrepaired · Mar 19, 2009 · N421FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > AREA 100, FUSELAGE, PREVIOUS REPAIR (STRINGER) FOUND LOCATED BTW FR 21 AND FR 22 AT STGR 49 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXIST
- [SDR FDEA200903191206](https://openairdocs.org/sdr/FDEA200903191206.md): Stringer · misrepaired · Mar 19, 2009 · N421FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > AREA 100, FUSELAGE, PREVIOUS REPAIR FOUND LOCATED BTW FR 21 AND FR 22 AT STGR 48 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW
- [SDR FDEA200903171433](https://openairdocs.org/sdr/FDEA200903171433.md): Skin · worn · Mar 17, 2009 · N421FE · Airbus A310222 · Wing, Rib/Bulkhead
  > LT WING FIX LEADING EDGE BTW SCREWJACK 3 AND SCREWJACK 4 WITH WEAR. FIX L/E REPAIRED AS PER EA 6-5710-127425.
- [SDR FDEA200903161574](https://openairdocs.org/sdr/FDEA200903161574.md): Roller Track · misrepaired · Mar 16, 2009 · N421FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > PREVIOUS REPAIR FOUND ON ROLLER TRACK LOCATED BTW FR 22-23 AT Y-100. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WA
- [SDR FDEA200903161564](https://openairdocs.org/sdr/FDEA200903161564.md): Skin · misrepaired · Mar 16, 2009 · N421FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR FOUND LOCATED BETWEEN FR 38.1 AND 38.2, BTW STGR 54 LT AND 50 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING APPROVED
- [SDR FDEA200903161553](https://openairdocs.org/sdr/FDEA200903161553.md): Skin · misrepaired · Mar 16, 2009 · N421FE · Airbus A310222 · Spoilers
  > PREVIOUS REPAIR AT INBD FLAP LOWER SKIN LOCATED BETWEEN RIB 7 AND RIB 9. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAIR WA
- [SDR FDEA200903161443](https://openairdocs.org/sdr/FDEA200903161443.md): Structure · misrepaired · Mar 16, 2009 · N421FE · Airbus A310222 · Fuselage Main, Structure
  > FUSELAGE, PREVIOUS REPAIR FOUND LOCATED BTW FR 23 AND FR 24 BTW STGR 49 RT AND 52 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR EVALUATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO EXISTING FEDEX EA
- [SDR FDEA200903161440](https://openairdocs.org/sdr/FDEA200903161440.md): Skin · misrepaired · Mar 16, 2009 · N421FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR FOUND LOCATED BETWEEN FR 20 ANBD FR 21 STGR 47 LT AND STGR 51 RT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NE
- [SDR FDEA200903161432](https://openairdocs.org/sdr/FDEA200903161432.md): Skin · corroded · Mar 16, 2009 · N421FE · Airbus A310222 · Horizontal Stabilizer, Plate/Skin
  > THS - SUPERFICIAL CORROSION AT BASE OF HOLES NR 2 AND NR 3 OF GROUP A, RT SIDE. CORROSION BLENDED OUT AS PER EA 6-5510-127414.
- [SDR FDEA200903161431](https://openairdocs.org/sdr/FDEA200903161431.md): Skin · misrepaired · Mar 16, 2009 · N421FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR FOUND LOCATED AT FR 13 STGR 28 LT. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NO TO CONFORM TO AN SRM REPAIR, NEW REPAIR WAS ACCOMPLISHED AS PER
- [SDR FDEA200903161405](https://openairdocs.org/sdr/FDEA200903161405.md): Floorbeam · corroded · Mar 16, 2009 · N421FE · Airbus A310322 · Fuselage Main, Floor Beam
  > AREA 100 - PREVIOUS REPAIR AT FLOORBEAM FOUND LOCATED AT FR 63 BTW Y420 AND Y-420. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. THE REPAIR WAS REMOVED BECAUSE THE FLOORBEAM WAS REPLACED DUE TO S
- [SDR FDEA200903161401](https://openairdocs.org/sdr/FDEA200903161401.md): Crossbeam · misrepaired · Mar 16, 2009 · N421FE · Airbus A310222 · Fuselage Main, Structure
  > N542 - FUSELAGE - PREVIOUS REPAIR IN CROSSBEAM LOCATED BETWEEN FR 36 AT Y1680. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW REPAI
- [SDR FDEA200903161400](https://openairdocs.org/sdr/FDEA200903161400.md): Crossbeam · misrepaired · Mar 16, 2009 · N421FE · Airbus A310222 · Fuselage Main, Structure
  > N544 - FUSELAGE - PREVIOUS REPAIR AT CROSSBEAM LOCATED BETWEEN FR 37 AT Y1680. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF IT WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR WAS EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR. NEW R
- [SDR FDEA200901150215](https://openairdocs.org/sdr/FDEA200901150215.md): Dampener · leaking · Jan 15, 2009 · N421FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > AIR TURN BACK DUE TO GEAR WOULD NOT RETRACT IN SYS 1 OR 2. ECAM L/G RETRACTION FAULT, LANDED AT 266.9 NOT OVERWEIGHT. ON WALK AROUND FOUND RT PITCH DAMPNER TRIPPED. ACFT BEING MOVED TO THE HANGAR FOR JACKING. REMOVED AND INSTALLED SERVICEABLE RT MLG PITCH
- [SDR FDEA200810154371](https://openairdocs.org/sdr/FDEA200810154371.md): Engine · failed · Oct 15, 2008 · N421FE · Airbus A310222 · Engine (Turbine/Turboprop)
  > NUMBER TWO ENGINE HUNG START AT 36 PERCENT N2, EGT 506'. ABORTED START FOLLOWED QRH PROCEDURES. SECOND START ATTEMPT NUMBER TWO ENGINE HUNG AT 38 PERCENT N2. START AIR PRESSURE 30 PSI. REJECTED START AT 529'. OBSERVED PEAK EGT 538'. ENGINE REMOVAL APPROV
- [SDR 08FDEA04371](https://openairdocs.org/sdr/08FDEA04371.md): Engine · hung start · Oct 15, 2008 · N421FE · Airbus A310222 · Engine (Turbine/Turboprop)
  > NUMBER TWO ENGINE HUNG START AT 36 PERCENT N2, EGT 506'. ABORTED START FOLLOWED QRH PROCEDURES. SECOND START ATTEMPT NUMBER TWO ENGINE HUNG AT 38 PERCENT N2. START AIR PRESSURE 30 PSI. REJECTED START AT 529'. OBSERVED PEAK EGT 538'. ENGINE REMOVAL APP
- [SDR 07FDEA01075](https://openairdocs.org/sdr/07FDEA01075.md): Floorbeam · corroded · Mar 21, 2007 · N421FE · Airbus A310222 · Fuselage Main, Floor Beam
  > MDCC FLOORBEAM AT FR 14 LT 64 INCHES FROM CENTER HAS 1 SPOT OF CORROSION ON FORWARD BOTTOM FACE 15" LONG BY 1" WIDE. REMOVED CORROSION IAW SRM 51-74-10 CHECKED LIMITS IAW SRM 53-12-15, OUT OF LIMITS. FABBED REPAIR IAW A310/200 SRTM 53-12-15 PB210 FIG 201. R
- [SDR 07FDEA01074](https://openairdocs.org/sdr/07FDEA01074.md): Floor Support · cracked · Mar 21, 2007 · N421FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF CEILING PANEL 131EC FOR AGING ACFT INSPECTION, FOUND MDCC FLOOR SUPPORT C36 BETWEEN L4 AND L5 SEAT TRACK TO BE CRACKED TOP OF VERTICAL STIFFENER LENGTH OF CRACK.400 INCH ROUTED OUT CRACK IAW A310/200 SRM 53-10-15. FABRICATED 2 REPAIR ANGLES

Next page: https://openairdocs.org/deregistered/N421FE-2016-02-18/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 = 'N421FE' AND deregistration_id = 'N421FE-2016-02-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N421FE-2016-02-18/reports

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