# Service difficulty reports: N412FE, cancelled Apr 25, 2013

A list on [N412FE, cancelled Apr 25, 2013](https://openairdocs.org/deregistered/N412FE-2013-04-25.md).

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

- [SDR 07FDEA04967](https://openairdocs.org/sdr/07FDEA04967.md): Switch · failed · Nov 29, 2007 · N412FE · Airbus A310 · Landing Gear Position and Warning
  > RECEIVED AN AUDIBLE "TOO LOW-GEAR" WNG ON SHORT FINAL. ALL GEAR INDS SHOWED GREEN/DOWN, SWITCHED TO POS1, REATTEMPT LANDING ALL SYS WORK NORMAL. ACN RELEASED FOR SVC. BRIEF INCREASED ALTITUDE AND TERRAIN AWARENESS." R&R MICROSWITCH 79GB IN REF TO MM 32-
- [SDR 07FDEA00908](https://openairdocs.org/sdr/07FDEA00908.md): Skin · corroded · Mar 15, 2007 · N412FE · Airbus A310324 · Fuselage Main, Plate/Skin
  > AVIONICS BAY, CORROSION BELOW FRAME 17 AT STR 44L REPAIRED IAW EA 6-5330-107691.
- [SDR 07FDEA00905](https://openairdocs.org/sdr/07FDEA00905.md): Floorbeam · misrepaired · Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MDCC - FLOORBEAM FRAME 36 CRACKED (PREVIOUS REPAIR NOT PER SRM). REWORKED PREVIOUS REPAIR IAW EA 6-5321-29042.
- [SDR 07FDEA00902](https://openairdocs.org/sdr/07FDEA00902.md): Skin · corroded · Mar 15, 2007 · N412FE · Airbus A310324 · Fuselage Main, Plate/Skin
  > AVIONICS BAY CORROSION AROUND FASTENERS FS 16 TO 17, STR 44L TO 45L REPAIRED PER EA 6-5330-107691.
- [SDR 07FDEA00889](https://openairdocs.org/sdr/07FDEA00889.md): Skin · corroded · Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > FOUND CORROSION EXIST AT AVIONIC COMPARTMENT AT STA 1315/FR 16 AND 17 STGR 46 ON FUSELAGE SKIN TOTAL 2 BY 2 INCHES BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH FEDEX EA 6-5330-107691.
- [SDR 07FDEA00884](https://openairdocs.org/sdr/07FDEA00884.md): Unknown · corroded · Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Structure (General)
  > FOUND CORROSION EXIST AT AVIONICS COMPARTMENT STA 1315/ FR 17 STGR 45 LT 2' BY 2' INCHES BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH EA 6-5330-107691.
- [SDR 07FDEA00881](https://openairdocs.org/sdr/07FDEA00881.md): Frame · corroded · Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Main, Frame
  > FOUND CORROSION EXIST AT AVIONIC COMPARTMENT AT STA 1315/ FRAME 16 AND 17 BETWEEN S47 AND 48 BELOW ACCESS PNL 121 PF ZONE 120 COMPLIED WITH EA 6- 5330-107691.
- [SDR 07FDEA00876](https://openairdocs.org/sdr/07FDEA00876.md): Skin · cracked · Mar 15, 2007 · N412FE · Airbus A310203 · Wing, Plate/Skin
  > LT WING LOWER SKIN SURFACE HAS A CRACK OF APPROX 1 INCH LONG AT AFT END OF RIB 11, 4 INCHES AFT OF REAR SPAR, FWD INBD END OF CUTOUT FOR ACCESS PANEL 581AB. CRACK RUNS THROUGH 1 FASTENER HOLE. ACCOMPLISHED RIB 11 PERMANENT REPAIR IAW FED EX EA 6-5710-107675
- [SDR 07FDEA00873](https://openairdocs.org/sdr/07FDEA00873.md): Floorbeam · cracked · Mar 15, 2007 · N412FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FOUND CRACK FR 38 PROFILE MDCC FLOORBEAM LT FWD CARGO COMPARTMENT BETWEEN SEAT TRACKS L-4 & L-5, REF SRM 53-10-00 AND SRM 53-10-15. REPAIRED FR 38 MDCC FLOORBEAM BETWEEN SEATRACKS L-4 AND L-5 IAW A310-200 SRM 53-10-15, FIG 201, SHT 6A.
- [SDR 07FDEA00845](https://openairdocs.org/sdr/07FDEA00845.md): Floorbeam · misrepaired · Mar 14, 2007 · N412FE · Airbus A310203 · Fuselage Main, Floor Beam
  > PREVIOUS REPAIR ON CABIN FLOORBEAM FRAME 37 REPAIR ANGLES IMPROPERLY INSTALLED. CORRECTED REPAIR IAW EA 6-5310-107701.
- [SDR 07FDEA00844](https://openairdocs.org/sdr/07FDEA00844.md): Ferrule · cracked · Mar 14, 2007 · N412FE · Airbus A310203 · Nacelle/Pylon, Main Frame
  > NR 1 PYLON PRECOOLER FERRULE PAN CRACKED BETWEEN RIBS 4 AND 8. ACCOMPLISHED PERMANENT REPAIR IAW SB A310-54-2028.
- [SDR 07FDEA00843](https://openairdocs.org/sdr/07FDEA00843.md): Skin · corroded · Mar 14, 2007 · N412FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > AVIONICS BAY HAD A 2.5" BY 1.5" AREA OF CORROSION BETWEEN FRAMES 17 AND 18 AND STRINGERS 50L AND 51L. CORROSION OUT OF LIMITS. COMPLIED WITH EA 6-5330-107691.
- [SDR 07FDEA00842](https://openairdocs.org/sdr/07FDEA00842.md): Skin · corroded · Mar 14, 2007 · N412FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > AVIONICS BAY SKIN FWD OF FRAME 17 BETWEEN STRINGERS 48L AND 50L HAS 5" BY 5" AREA OF CORROSION AREA OUT OF LIMITS. COMPLIED WITH EA 6-5330-107691.
- [SDR 07FDEA00803](https://openairdocs.org/sdr/07FDEA00803.md): Seat Track · gouged · Mar 13, 2007 · N412FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK 3L GOUGED CUT OUT AND REPLACED GOUGED SECTION OF SEAT TRACK. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
- [SDR 07FDEA00802](https://openairdocs.org/sdr/07FDEA00802.md): Seat Track · gouged · Mar 13, 2007 · N412FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC SEAT TRACK 5L GOUGED BLENDED GOUGES IAW A310-200 SRM 51-74-10. FOUND TO BE IN LIMITS. MAJOR REPAIR IAW FEDEX GMM 6-2-100.
- [SDR 05FDEA03547](https://openairdocs.org/sdr/05FDEA03547.md): Warning Light · false activation · Oct 27, 2005 · N412FE · Airbus A310203 · Door Warning System
  > SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO DOOR NOT CLOSED. AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE IAW MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICA
- [SDR 05FDEA03546](https://openairdocs.org/sdr/05FDEA03546.md): Warning Light · false activation · Oct 27, 2005 · N412FE · Airbus A310203 · Door Warning System
  > SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CRAGO SW FAULT AND AN AMBER DOOR LIGHT FOR AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 "MEL 52-71-01: (IDENTIFY) AFT DOOR CLOSED AND LOCKED
- [SDR 05FDEA03505](https://openairdocs.org/sdr/05FDEA03505.md): Door · malfunctioned · Oct 26, 2005 · N412FE · Airbus A310 · Cargo/Baggage Doors
  > SOON AFTER T/O GOT ECAM ALERT FOR AFT CARGO NOT CLOSED AFT CARGO SW FAULT AND AN AMBER DOOR LIGHT FO R AFT CARGO ON RT ECAM. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-71-01 CATEGORY: C EXPIRATION: 05NOV05 MEL 52-71-01: AFT DOOR CLOSED AND LOCKED INDICATIO
- [SDR 04FDEA02835](https://openairdocs.org/sdr/04FDEA02835.md): Panel · damaged · Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/Skin
  > PANEL LAND 650KB HAS 6EA ELONGATED HOLES (RT WING). REPAIRED HOLES IAW EA 6-5710-81998 AND A310 SRM 51-40-44 FIG 1.
- [SDR 04FDEA02834](https://openairdocs.org/sdr/04FDEA02834.md): Panel · damaged · Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/Skin
  > PANEL LAND 550JB HAS 1EA ELONGATED HOLE (LT WING). REPAIRED HOLE IAW EA 6-5710-81998.
- [SDR 04FDEA02833](https://openairdocs.org/sdr/04FDEA02833.md): Panel · damaged · Sep 28, 2004 · N412FE · Airbus A310 · Wing, Plate/Skin
  > PANEL LAND 650JB HAS 2EA ELONGATED HOLES. REPAIRED 2EA ELONGATED HOLES IAW EA 6-5710-81998
- [SDR 04FDEA02441](https://openairdocs.org/sdr/04FDEA02441.md): Seat Track · corroded · Aug 11, 2004 · N412FE · Airbus A310 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN CARGO FLOOR 3 AREAS OF CORROSION ON SEAT TRACKS AT FR66 AND FR67 ZONE 251 TRACK F. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW SRM 53-10-16
- [SDR 04FDEA02440](https://openairdocs.org/sdr/04FDEA02440.md): Pylon · cracked · Aug 11, 2004 · N412FE · Airbus A310203 · Nacelle/Pylon Structure
  > NR 1 ENGINE AFT UPPER PYLON HAS CRACKED UNDER PNL 473CL. STOP DRILLED CRACK AND INSTALLED U-CHANNEL IAW A310/200 SRM 54-50-00 AND 54-54-11 FIG 201 AND 54-54-51 FIG 206 BETWEEN PYLON STA 1059 AND STA 1115.
- [SDR 04FDEA02439](https://openairdocs.org/sdr/04FDEA02439.md): Seat Track · corroded · Aug 11, 2004 · N412FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDC ON RT SEAT TRACK NR 3 FR53 NOTED CORROSION INSIDE SCALLOP HOLES AND ON FLANGE. REMOVED DAMAGED SECTION AND INSTALLED NEW SECTION IAW A310/200 SRM 53-10-16.
- [SDR 04FDEA02438](https://openairdocs.org/sdr/04FDEA02438.md): Dummy Rail · corroded · Aug 11, 2004 · N412FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > UPPER MAIN CABIN FR48 BETWEEN TRACK D & E HAS 1EA DUMMY TRACK WITH CORROSION BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED DUMMY TRACK IAW A310 SRM 51-72-10.
- [SDR 04FDEA02437](https://openairdocs.org/sdr/04FDEA02437.md): Dummy Rail · corroded · Aug 11, 2004 · N412FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > UPPER MAIN CABIN BETWEEN D & E HAS 3EA DUMMY TRACK WITH CORROSION (LEVEL 2) AND 1EA DUMMY TRACK CRACKED (2 INCHES IN LENGTH) BETWEEN FR 52 AND 53. REMOVED AND REPLACED 4EA DUMMY TRACKS.
- [SDR 04FDEA02338](https://openairdocs.org/sdr/04FDEA02338.md): Tee Fitting · corroded · Aug 1, 2004 · N412FE · Airbus A310 · Fixed Inner Doors
  > REF. SNRM N00243 MDCC T-CAP JUST AFT OF COCKPIT DOOR HAS LEVEL 2 CORROSION REMOVED CORROED T-CAP SECTION INSTALLED A SPLICE IN SECTION IAW A310/200 SRM 53- 12-15, 51-40-20, AND 51-75-10
- [SDR 04FDEA00389](https://openairdocs.org/sdr/04FDEA00389.md): Coalescer Bag · dirty · Feb 10, 2004 · N412FE · Airbus A310 · Humidity Control System
  > ON TAKEOFF ROLL STRONG ODOR OF OIL OR AIR CONDITIONING SMOKE IN COCKPIT, REJECTED TAKEOFF. NO SIGN OF SMOKE COMING FROM VENTS, NO SMOKE WARNINGS, ALL INDICATIONS APPEAR NORMAL, RETURNED TO RAMP. FOUND NR 1 AND NR 2 PACK WATER SEPARATOR BAGS VERY DIRTY. REMO
- [SDR 03FDEA02008](https://openairdocs.org/sdr/03FDEA02008.md): Thrust Reverser · malfunctioned · Dec 2, 2003 · N412FE · Airbus A310 · Engine Thrust Reverser
  > 1 ENG ON T/O, N1 DID NOT REACH T/O PWR. ENG N1 90 PRCT. ENG 2 N1 100 PRCT. TRIED TO MATCH N1 BY PUSHING UP 1 THROTTLE WHICH CAUSED 1 EGT TO RISE TO CAUTION RANGE ABOUT 890, RETARDED THROTTLES AT THAT TIME ECAM WARNING HP VALVE FAULT -OFF, 1 HP VALVE SELECT
- [SDR 02FDEA00384](https://openairdocs.org/sdr/02FDEA00384.md): Controller · failed · Jun 8, 2002 · N412FE · Airbus A310 · Cabin Pressure Controller
  > AIRCRAFT WOULD NOT PRESSURIZE. NR 1 FWD AND AFT OUTFLOW VALVE INDICATED FULL OPEN. PERFORMED FUNCTIONAL CHECK OF NR 1 AND NR 2 PRESSURIZATION CONTROLLERS. NR 1 SYSTEM CONTROLLER CONTINUOUSLY SHOWS THE AIRCRAFT AT AN ELEVATION OF 400 FT WHEN IT SHOULD READ A
- [SDR 02FDEA00051](https://openairdocs.org/sdr/02FDEA00051.md): Light · illuminated · Jan 15, 2002 · N412FE · Airbus A310203 · Door Warning System
  > 02-51 AFTER T/O MAIN DECK DOOR LIGHT CAME ON. A/C RELEASED PER MEL 52-9.
- [SDR 02FDEA00009](https://openairdocs.org/sdr/02FDEA00009.md): Symbol Generator · inoperative · Jan 3, 2002 · N412FE · Airbus A310203 · Integrated Flight System
  > LOST F/O'S PRIMARY FLT AND NAV DISPLAY. EFIS SGU NR 2 INOP. RELEASED PER MEL 34-7.
- [SDR 00FDEA00002](https://openairdocs.org/sdr/00FDEA00002.md): Switch · failed · Jan 4, 2000 · N412FE · Airbus A310203 · Landing Gear Retraction/Extension System
  > ON T/O, L/G WOULD NOT RETRACT DESPITE SEVERAL RECYCLES ON SYS 1 AND 2 C/B'S. RESET BOX AND FAULTED SAME UNITS. REMOVED AND REPLACED PROXIMITY DETECTOR UNIT PER MM. OPS CK GOOD.
- [SDR 99FDEA00510](https://openairdocs.org/sdr/99FDEA00510.md): Relay · failed · Dec 22, 1999 · N412FE · Airbus A310203 · Pitot/Static Anti-Ice System
  > 99-293 - ON DEPT GDL, F/O PITOT HEAT FAILED, THEN NR 1 ATS TRIPPED. WOULD NOT RESET. REMOVED AND REPLACED NOSE GEAR RELAY 153GB IAW MM. ALL CK GOOD, OK FOR SERVICE.

## 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 = 'N412FE' AND deregistration_id = 'N412FE-2013-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N412FE-2013-04-25/reports

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