# Service difficulty reports: N409FE, cancelled Dec 19, 2013

A list on [N409FE, cancelled Dec 19, 2013](https://openairdocs.org/deregistered/N409FE-2013-12-19.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 · 57 reports

- [SDR FDEA200901060047](https://openairdocs.org/sdr/FDEA200901060047.md): Reservoir · leaking · Jan 6, 2009 · N409FE · Airbus A310203 · Hydraulic Reservoir, Auxiliary
  > ON TAKEOFF PLUS 317 AT FL360 HEARD WHAT SOUNDED LIKE A TRANSIENT ELECTRICAL CHANGE OVER, HOWEVER ALL ELECTRICS APPEARED NORMAL. THEN NOTICED WHEN SCANNING OVERHEAD THAT GREEN HYDRAULIC RESEVIOR WAS IN YELLOW. WHEN POWER CAME TO IDLE FOR DECENT ECAM SHOWED L
- [SDR 07FDEA05022](https://openairdocs.org/sdr/07FDEA05022.md): Warning Light · false activation · Dec 11, 2007 · N409FE · Airbus A310203 · Central Warning
  > DURING CLIMB AT APPROX FL 260, GOT PACK 1 AND PACK 2 FAULT, WOULD NOT RESET. DESCENDED TOWARDS 10.000, PACKS RESET AT ABOUT 14,000. CLIMBED BACK TOWARDS FL 340, BUT BOTH PACKS FAULTED AGAIN AT APPROX FL260. DIVERTED INTO BOS. PERFORMED CABIN PRESS CONTRO
- [SDR 07FDEA02368](https://openairdocs.org/sdr/07FDEA02368.md): Controller · failed · Jul 3, 2007 · N409FE · Airbus A310203 · Cabin Pressure Controller
  > ATB AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. ECAM MAN PRESS VALVE INDICATED OPEN. EMERGENCY VALVE INDICATION IN COCKPIT NEAR HANDLE INDICATED CLOSED AND VALVE LOOKED CLOSED ON PREFLIGHT. PERFORMED CABIN PRESSURE CONTROL AND MONITORING TEST PER AMM 21-31
- [SDR 07FDEA01091](https://openairdocs.org/sdr/07FDEA01091.md): Skin · dented · Mar 22, 2007 · N409FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > AREA 200 FUSELAGE SKIN SURFACE FOUND DENTED, BETWEEN FR 68 AND FR 69 RT AND BETWEEN STR 2 AND STR 3 REPAIRED IAW SRM 53-10-12 FIG 225. REPAIR INSPECTED PER SRM 53-10-12-2-005-00. INITIAL INSP AT 32.800 FC, REPAIR AT 4400FC REPAIR EVALUATED PER GMM 6-2-100 A
- [SDR 07FDEA00738](https://openairdocs.org/sdr/07FDEA00738.md): Skin · misrepaired · Mar 10, 2007 · N409FE · Airbus A310203 · Passenger/Crew Doors
  > PREVIOUS REPAIR FOUND LOCATED ON LOWER SECTION OF NR 2 RT DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTEING SRM REPAIR.
- [SDR 07FDEA00737](https://openairdocs.org/sdr/07FDEA00737.md): Panel · cracked · Mar 9, 2007 · N409FE · Airbus A310203 · Nacelle/Pylon, Plate/Skin
  > NR 1 PYLON, RT SIDE PANEL AT RIB 8 FOUND CRACKED REPAIRED IAW SRM 54-51-31 FIG 201 SHT 1 AND 2.
- [SDR 07FDEA00736](https://openairdocs.org/sdr/07FDEA00736.md): Seat Track · damaged · Mar 9, 2007 · N409FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK FOUND WITH DAMAGED "TOOTH" BETWEEN FR 20 AND FR 21 AT Y 2462. REPAIRED IAW FEDEX EA 6-5310-106699.
- [SDR 07FDEA00713](https://openairdocs.org/sdr/07FDEA00713.md): Floorbeam · cracked · Mar 8, 2007 · N409FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FWD CARGO COMPARTMENT UPPER FLAP AT BEAM/FLOOR OF CABIN FOUND CRACK AT FR 38 AND Y1700 REPAIRED PER SFEDEX EA 6-5310-106694. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00712](https://openairdocs.org/sdr/07FDEA00712.md): Structure · damaged · Mar 8, 2007 · N409FE · Airbus A310203 · Passenger/Crew Doors
  > FOUND ON R1 PASS DOOR, AT THE LOWER LT CORNER, SEVERAL SPOTS WITH MISSING MATERIAL (SHEET METAL) REPAIRED PER SRM 52-11-00 FIG 206. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00711](https://openairdocs.org/sdr/07FDEA00711.md): Skin · cracked · Mar 8, 2007 · N409FE · Airbus A310203 · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON PRECOOLER HOUSING RT SIDE SKIN SURFACE FOUND CRACKED AT RIB 5A UPPER AREA INSTALLED NEW WALL P/N A5461139320300 PER SRM 51-72-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00710](https://openairdocs.org/sdr/07FDEA00710.md): Seat Track · corroded · Mar 8, 2007 · N409FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC- FOUND TRACK -Y1456 WITH CORROSION BETWEEN FRAMES 46 AND 54. REPAIRED PER SRM 53-10-16 FIG 205. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00709](https://openairdocs.org/sdr/07FDEA00709.md): Seat Track · corroded · Mar 8, 2007 · N409FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC- FOUND TRACK -Y953 WITH CORROSION BETWEEN FRAMES 53 AND 54. REPAIRED PER SRM 53-10-16. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00707](https://openairdocs.org/sdr/07FDEA00707.md): Ferrule · cracked · Mar 8, 2007 · N409FE · Airbus A310203 · Nacelle/Pylon, Main Frame
  > NR 2 PYLON PRECOOLER FERRULE WITH SEVERAL CRACKS. INSTALLED NEW FERRULE P/N A5461270000000 PER SRM 51-72-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00706](https://openairdocs.org/sdr/07FDEA00706.md): Floor Panel · cracked · Mar 8, 2007 · N409FE · Airbus A310203 · Fuselage Floor Panel
  > FOUND FWD CARGO COMP´T CABIN FLOOR UPPER FLAP CRACKED AT FR 25 AND AT -Y690. REPAIRED PER SRM 53-10-15 FIG 201 SHEET 4A. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00705](https://openairdocs.org/sdr/07FDEA00705.md): Fitting · cracked · Mar 8, 2007 · N409FE · Airbus A310203 · Spoilers
  > LT WING NR 3 SPOILER INB SEATING FITTING FOUND CRACKED REPAIRED PER SRM 57-51-11 FIG 204 SHEET 1. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00704](https://openairdocs.org/sdr/07FDEA00704.md): Skin · damaged · Mar 8, 2007 · N409FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SURFACE FOUND DENTED BETWEEN FS 68 AND FS 69 RT AND BETWEEN STR 2 AND STRG 3 REPAIRED PER SRM 53-10-12 FIG 225 (SHEET 1). REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00703](https://openairdocs.org/sdr/07FDEA00703.md): Bearing · damaged · Mar 8, 2007 · N409FE · Airbus A310203 · Horizontal Stabilizer Structure
  > RUDDER HINGE ARM NR 4 WITH FWD BEARING DAMAGED. BEARING REPLACED PER SB NO A310-55-2025 PG 27/28 DATE OCT 12/98 REVISION NO 3 APR 08/04 FEDEX EA 6-5510-106687. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00701](https://openairdocs.org/sdr/07FDEA00701.md): Panel · cracked · Mar 8, 2007 · N409FE · Airbus A310203 · Wing, Plate/Skin
  > RT WING, WING LWR SKIN SURFACE NEXT TO TOP INB OF PNL 681AB FOUND CRACKED REPAIRED PER FEDEX ENG AUTH 6-5710-106686. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00700](https://openairdocs.org/sdr/07FDEA00700.md): Skin · delaminated · Mar 8, 2007 · N409FE · Airbus A310203 · Trailing Edge Flaps
  > OUTB FLAP RT, DELAMINATION FOUND ON THE INBD AREA, INNER SKIN SURFACE REPAIRED PER FEDEX ENG AUTH 6-5710-106684. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".
- [SDR 07FDEA00424](https://openairdocs.org/sdr/07FDEA00424.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Cargo/Baggage Doors
  > PREVIOUS REPAIR FOUND LOCATED ON THE AFT CARGO DOOR INSIDE STRUCTURE LOWER SECTION, FS 3355 BETWEEN FR 62-62A. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT
- [SDR 07FDEA00425](https://openairdocs.org/sdr/07FDEA00425.md): Seat Track · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > PREVIOUS REPAIR FOUND LOCATED ON THE LT SEAT TRACK, FR 20-21 AND Y246. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM
- [SDR 07FDEA00400](https://openairdocs.org/sdr/07FDEA00400.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Passenger/Crew Doors
  > PREVIOUS REPAIR FOUND LOCATED ON LOWER SECTION OF NR 2 RT DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REP
- [SDR 07FDEA00397](https://openairdocs.org/sdr/07FDEA00397.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR FOUND LOCATED RT, FS 4937-4947, FR 96 AND STR 2. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW RE
- [SDR 07FDEA00415](https://openairdocs.org/sdr/07FDEA00415.md): Crossbeam · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage Main, Structure
  > PREVIOUS REPAIR FOUND LOCATED ON THE FWD PIT CROSSBEAM, RT, FS 1976, FR 36 AND ?Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING
- [SDR 07FDEA00411](https://openairdocs.org/sdr/07FDEA00411.md): Door Frame · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage Main, Structure
  > PREVIOUS REPAIR FOUND LOCATED ON THE FWD CARGO DOOR FRAME, FS 1461, FR 20A AND STR 34. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTI
- [SDR 07FDEA00410](https://openairdocs.org/sdr/07FDEA00410.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Trailing Edge Flaps
  > PREVIOUS REPAIR FOUND LOCATED ON THE RT OUTBOARD FLAP, UPPER SURFACE BETWEEN TRACK 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXIST
- [SDR 07FDEA00409](https://openairdocs.org/sdr/07FDEA00409.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Trailing Edge Flaps
  > PREVIOUS REPAIR FOUND LOCATED ON THE RT INBOARD FLAP, LOWER SURFACE, TRAILING EDGE BETWEEN RIB 19-21. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFO
- [SDR 07FDEA00408](https://openairdocs.org/sdr/07FDEA00408.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Trailing Edge Flaps
  > PREVIOUS REPAIR FOUND LOCATED ON THE RT INBOARD FLAP, LOWER SURFACE, TRAILING EDGE, RIB 4. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EX
- [SDR 07FDEA00403](https://openairdocs.org/sdr/07FDEA00403.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Horizontal Stabilizer, Plate/Skin
  > PREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LEADING EDGE OF THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL 331CB. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND
- [SDR 07FDEA00402](https://openairdocs.org/sdr/07FDEA00402.md): Unknown · unknown · Feb 9, 2007 · N409FE · Airbus A310203 · Standard Practices/Structures
  > PREVIOUS COMPOSITE REPAIR FOUND LOCATED ON THE RT ELEVATOR LOWER SURFACE TRAILING EDGE STA 473. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER SRM 55-21-11 AND EA 6-5510-10668
- [SDR 07FDEA00394](https://openairdocs.org/sdr/07FDEA00394.md): Unknown · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage Structure (General)
  > PREVIOUS REPAIR FOUND LOCATED RT, FS 1446-1461, FR 20-20A AND STR 38-41. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR
- [SDR 07FDEA00423](https://openairdocs.org/sdr/07FDEA00423.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Trailing Edge Flaps
  > PREVIOUS REPAIR FOUND LOCATED ON THE RT INBOARD FLAP VANE, UPPER SURFACE OUTBOARD END. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO
- [SDR 07FDEA00420](https://openairdocs.org/sdr/07FDEA00420.md): Crossbeam · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage Main, Structure
  > PREVIOUS REPAIR FOUND LOCATED ON THE AFT PIT CROSSBEAM, RT, FS 3302, FR 61 AND Y160. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING
- [SDR 07FDEA00412](https://openairdocs.org/sdr/07FDEA00412.md): Crossbeam · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage Main, Structure
  > PREVIOUS REPAIR FOUND LOCATED ON FWD PIT CROSSBEAM, RT, FS 1817, FR 33 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTI
- [SDR 07FDEA00406](https://openairdocs.org/sdr/07FDEA00406.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Spoilers
  > PREVIOUS COMPOSITE REPAIR LOCATED ON THE LT WING, NR 7 SPOILER, LOWER SIDE OUTBD OF ACTUATOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO
- [SDR 07FDEA00401](https://openairdocs.org/sdr/07FDEA00401.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Horizontal Stabilizer, Plate/Skin
  > PREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LEADING EDGE OF THE RT HORIZONTAL STABILIZER LEADING EDGE PANEL 341CB. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND
- [SDR 07FDEA00398](https://openairdocs.org/sdr/07FDEA00398.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR FOUND LOCATED RT, FS 4941-4956, FR 97 AND STR 4-6. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW
- [SDR 07FDEA00395](https://openairdocs.org/sdr/07FDEA00395.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR FOUND LOCATED RT, FS 3408-3461, FS 63-64 AND STR 40-43. REPAIR AFT OF AFT CARGO DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFOR
- [SDR 07FDEA00393](https://openairdocs.org/sdr/07FDEA00393.md): Skin · misrepaired · Feb 9, 2007 · N409FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > PREVIOUS REPAIR FOUND LOCATED RT, FS 904-926, FS 7-8. REPAIR LOCATED AROUND OXYGEN DISCHARGE INDICATOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. OPEN /CLOSE ACCESS PER AMM 25-71-00
- [SDR 05FDEA02975](https://openairdocs.org/sdr/05FDEA02975.md): Control Unit · malfunctioned · Sep 16, 2005 · N409FE · Airbus A310 · Smoke Detection
  > ON CLIMB-OUT JUST ABV FL190, MAIN DECK CARGO SMOKE WARNING ANNUNCIATED FOR MID 2. PRIOR TO MAIN DECK WARNING LOOP A MID 2 FAULTED. COMMENCED AIR TURN-BACK TO KGRR, RAN MDC SMOKE PROC IAW QRH. ECAM REQUEST TO NORM ON DESCENT THROUGH APPROX 15000'MSL. NO SMO
- [SDR 05FDEA02225](https://openairdocs.org/sdr/05FDEA02225.md): Coalescer Bag · contaminated · Aug 2, 2005 · N409FE · Airbus A310 · Humidity Control System
  > ON TAXI OUT MEM, SMELLED A STRONG SMELL THEN A FULL MAIN DECK SMOKE WARNING WHICH LASTED FOR SEVERAL MINUTES. DECLARED EMERGENCY. DETECTION CLEARED ITSELF. RETURNED TO GATE. REPLACED NR 1 AND 2 PACK WATER SEPARATOR BAGS AS PRECAUTIONARY REF A310 AMM 21-51-
- [SDR 05FDEA01035](https://openairdocs.org/sdr/05FDEA01035.md): Coalescer Bag · contaminated · Apr 16, 2005 · N409FE · Airbus A310203 · Humidity Control System
  > AT 300 FT AGL BOTH CAPT AND F/O SMELLED SMOKE OR BURNING. MIN EQUIP BAY SMOKE ON ECAM ILLUMINATED FOR ONLY 10 SECONDS OR LESS THEN DISAPPEARED. THE SMOKE AND SMELL WENT AWAY. RETURNED TO MEM AND ON LANDING THE SMELL RETURNED, BUT NO SMOKE. CLEARED RUNWAY
- [SDR 05FDEA00118](https://openairdocs.org/sdr/05FDEA00118.md): Skin · dented · Jan 17, 2005 · N409FE · Airbus A310203 · Nacelle/Pylon, Plate/Skin
  > INSPECTED UPPER AND LOWER SKINS, FOUND NO DAMAGE ON UPPER SKIN, LOWER SKIN HAS MINOR DAMAGE IN SKIN SURFACE NEAR FWD LT CORNER. REPAIRED SKIN DAMAGE.
- [SDR 04FDEA03085](https://openairdocs.org/sdr/04FDEA03085.md): Switch · out of rig · Nov 11, 2004 · N409FE · Airbus A310203 · Door Warning System
  > RIGHT CABIN DOOR INDICATED UNLOCKED AS SOON AS PRESSURIZED. AIR TURN BACK, REMOVED AND REPLACED R-1 DOOR SWITCH RIG AND OPS CHECK GOOD IAW A310 AMM 52-71-11.
- [SDR 04FDEA02931](https://openairdocs.org/sdr/04FDEA02931.md): Outflow Valve · inoperative · Oct 14, 2004 · N409FE · Airbus A310203 · Pressure Regulator/Outflow Valve
  > NR 2 SYSTEM FWD AND AFT OUTFLOW VALVES REMAINED FULLY OPEN. ENT BY: 105221 RPT BY: 011927 MEL 14 OCT 04 04:44, LAX R ACN RELEASED FOR SERVICE PER MEL/CDL: 21-31-04-02-A CATEGORY: C EXPIRATION: 24OCT04 "MEL 21-31-04-02-A: OUTFLOW VALVE(S) (IDENTIFY) INOP. V
- [SDR 04FDEA02393](https://openairdocs.org/sdr/04FDEA02393.md): Floor Support · corroded · Aug 6, 2004 · N409FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CORRODED FWD PIT LEFT OF CTR AND AFT OF FR 38.2 (LEVEL 2). REMOVED AND REPLACED FLOOR SUPPORT (ANGLE) IAW A310/200 SRM 51-40-21.
- [SDR 04FDEA02392](https://openairdocs.org/sdr/04FDEA02392.md): Roller Tray · corroded · Aug 6, 2004 · N409FE · Airbus A310203 · Cargo Compartments
  > FWD PIT CTR ROLLER TRAY AT JUST FWD OF FR 38.1 BOTTOM SIDE IS CORRODED (LEVEL 2). REMOVED DAMAGED SECTION AND INSTALLED SPLICE SECTION IAW A310/200 SRM 53-10-15.
- [SDR 04FDEA02391](https://openairdocs.org/sdr/04FDEA02391.md): Floorbeam · corroded · Aug 6, 2004 · N409FE · Airbus A310203 · Fuselage Main, Floor Beam
  > LOWER FUSELAGE BULK CARGO PIT LATERAL FLOORBEAM AT FR66 LT OF CENTERLINE HAS EXFOLIATED CORROSION AROUND FASTENER HOLE (LEVEL 2). REMOVED DAMAGED AREA, FABRICATED FILLER, ANGLE AND INSTALLED IAW A310/200 SRM 53-10-15 AND 51-25-00.
- [SDR 04FDEA02335](https://openairdocs.org/sdr/04FDEA02335.md): Tee Fitting · corroded · Aug 1, 2004 · N409FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > MDC FR 10 TO FR 14A, 20 INCHES OUTBOARD FROM LEFT OF CTR T-CAP HAS CORROSION (LEVEL 2) INCLUDING IN AND AROUND ALL FASTENER HOLES. REMOVED AND REPLACED T-CAP IAW A310/200 SRM 51-40-21.
- [SDR 04FDEA02337](https://openairdocs.org/sdr/04FDEA02337.md): Seat Track · corroded · Aug 1, 2004 · N409FE · Airbus A310 · Fuselage, Seat/Cargo Attach Fittings
  > REF. SNRM N00381, MDC BETWEEN FR15A AND FR19 SEAT TRACK 4L HAS (LEVEL 2) CORROSION 12 INCHES FWD OF FR17. REMOVED AND REPLACED SEAT TRACK IAW A310/200 SRM 53-12-16 AND DWG A53610798

Next page: https://openairdocs.org/deregistered/N409FE-2013-12-19/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 = 'N409FE' AND deregistration_id = 'N409FE-2013-12-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N409FE-2013-12-19/reports

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