# Service difficulty reports: N448FE, cancelled Jul 29, 2013

A list on [N448FE, cancelled Jul 29, 2013](https://openairdocs.org/deregistered/N448FE-2013-07-29.md).

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

- [SDR FDEA201007082404](https://openairdocs.org/sdr/FDEA201007082404.md): Unknown · multiple fail · Jul 8, 2010 · N448FE · Airbus A310 · Standard Practices/Structures
  > AFTER TAKEOFF GEAR WOULD NOT RETRACT USING SYS 2 OR SYS1. TRANSPONDER REPORTED INOP BY DEPARTURE. ACFT WOULD NOT PRESSURIZE. AUTO THROTTLES INOP. AUTOPILOTS WHEN SELECTED ON, REVERTED TO CONTROL WHEEL STEERING. BOTH CAPT AND F/O SPD TAPE WENT AWAY. WHE
- [SDR FDEA200804111385](https://openairdocs.org/sdr/FDEA200804111385.md): Stringer · damaged · Apr 11, 2008 · N448FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > 1 EA FASTENER HOLE AT FR 54, STRINGER 40 RT HAS DOUBLE DRILL AND DAMAGE IN COUNTERSINK REPAIRED DAMAGE HOLE IAW EA 6-5310-118123.
- [SDR 08FDEA01385](https://openairdocs.org/sdr/08FDEA01385.md): Skin · damaged · Apr 11, 2008 · N448FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > 1 FASTENER HOLE AT FR 54, STRINGER 40 RT HAS DOUBLE DRILL AND DAMAGE IN COUNTERSINK REPAIRED DAMAGE HOLE IAW FED EX EA 6-5310-118123.
- [SDR 08FDEA01379](https://openairdocs.org/sdr/08FDEA01379.md): Seat Track · damaged · Apr 10, 2008 · N448FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 2 LT Y450 BETWEEN FRAMES 51 TO 52 HAS 2 EA REPAIR SPLICES MEASURING 7 IN LONG BY 3 IN TALL AND 1 REPAIR SECTION 51.9 IN LONG FROM FR 54 TO BETWEEN FRAMES 51 AND 52 REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PR
- [SDR 08FDEA01232](https://openairdocs.org/sdr/08FDEA01232.md): Seat Track · misrepaired · Apr 1, 2008 · N448FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 4 RT - Y1456 BETWEEN FRAMES 62 TO 63, HAS 2. REPAIR ANGLES MEASURING 9.5" LONG BY 1.9" TALL AND 1. REPAIR PIECE 4 INCHES LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED REPAIR AND INSTALLED CORRECT SEAT TR
- [SDR 08FDEA01225](https://openairdocs.org/sdr/08FDEA01225.md): Seat Track · damaged · Apr 1, 2008 · N448FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC NR 3 LT SEAT TRACK BETWEEN FRAMES 54.3 TO 54.2 HAS 2 AREAS OF DAMAGED SCALLOPS REMOVED AND REPLACED DAMAGED SEAT TRACK IN MDCC NR 3 LT AT FRAMES 54.2 TO 58 IAW A310-200 SRM 53-10-16 AND SRM 51-72-10.
- [SDR 08FDEA01224](https://openairdocs.org/sdr/08FDEA01224.md): Stringer · misrepaired · Apr 1, 2008 · N448FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 56 RT BETWEEN FRAMES 67 TO 69, HAS REPAIR SECTION MEASURING 16" LONG AND 2 REPAIR SPLICES, THE FORWARD SPLICE IS 7.9 INCHES LONG AND THE AFT SPLICE IS 8.4 INCHES LONG. REPAIR NOT IAW SRM REQUIREMENTS.
- [SDR 08FDEA01223](https://openairdocs.org/sdr/08FDEA01223.md): Stringer · misrepaired · Apr 1, 2008 · N448FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 55 RT BETWEEN FRAMES 65 TO 69 HAS 1 REPAIR SECTION MEASURING 80" LONG AND 1 REPAIR SPLICE MEASURING 8.2 INCHES LONG, REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED CORRECT ST
- [SDR 08FDEA01222](https://openairdocs.org/sdr/08FDEA01222.md): Stringer · misrepaired · Apr 1, 2008 · N448FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > PREVIOUS STRINGER REPAIR LOCATED IN BULK CARGO ON STRINGER 54 RT BETWEEN FRAMES 65 TO 67 HAS 1 REPAIR SECTION MEASURING 40" LONG AND 1 REPAIR SPLICE MEASURING 8 INCHES LONG. REPAIR NOT IAW SRM REQUIREMENTS. REMOVED PREVIOUS REPAIR AND INSTALLED 1 CORRECT R
- [SDR 08FDEA01221](https://openairdocs.org/sdr/08FDEA01221.md): Seat Track · misrepaired · Apr 1, 2008 · N448FE · Airbus A310222 · Fuselage, Seat/Cargo Attach Fittings
  > PREVIOUS REPAIR LOCATED ON MAIN CABIN SEAT TRACK NR 3 LT Y953 BETWEEN FRAMES 61 TO 62 HAS 2. REPAIR SPLICES MEASURING 7.1" LONG BY 3" TALL AND 1. REPAIR SECTION 73" LONG FROM FRAME 55/58 TO BETWEEN FRAMES 61 AND 62 ALSO THE INBOARD AND OUTBOARD PRODUCTION SP
- [SDR 08FDEA01220](https://openairdocs.org/sdr/08FDEA01220.md): Paint · missing · Apr 1, 2008 · N448FE · Airbus A310222 · Trailing Edge Flaps
  > PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP LOWER MAIN SKIN BETWEEN RIBS 3 AND 4 MEASURES 10.4" BY 9.9". REPAIR NOT IAW SRM REQUIREMENTS DUE TO REPAIR DOUBLER MISSING FILLET SEAL AND PAINT. REPAIRED PROTECTIVE COATING AND RESEALED EDG
- [SDR 08FDEA01219](https://openairdocs.org/sdr/08FDEA01219.md): Seal · missing · Apr 1, 2008 · N448FE · Airbus A310222 · Trailing Edge Flaps
  > PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED ON LEFT WING OUTBOARD FLAP LOWER MAIN SKIN BETWEEN RIBS 4 AND 5 MEASURES 10.6 INCHES BY 9 INCHES. REPAIR NOT IAW SRM REQUIREMENTS DUE TO REPAIR MISSING FILLET SEAL AND PAINT. REPAIRED PROTECTIVE COATING AND RE-SEALED
- [SDR 08FDEA01218](https://openairdocs.org/sdr/08FDEA01218.md): Doubler · corroded · Apr 1, 2008 · N448FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > PREVIOUS EXTERNAL REPAIR DOUBLER LOCATED AT LEFT SIDE UPPER FWD FUSELAGE SKIN BETWEEN FRAMES 0 TO 1 AND JUST FORWARD OF THE CAPTAINS WINDSHIELD MEASURES 9.5 INCHES BY 11.6 INCHES WITH A SKIN CUTOUT MEASURING 6.7 INCH BY 5.6 INCH REPAIR NOT IAW SRM REQUIREMENTS
- [SDR 07FDEA05106](https://openairdocs.org/sdr/07FDEA05106.md): Anti-Ice Valve · malfunctioned · Dec 20, 2007 · N448FE · Airbus A310222 · Engine Anti-Icing System
  > AFTER TAKEOFF RECEIVED NR 1 ENGINE ADVISORY NAC TEMP AT 200 DEGREES, AT CRUISE NR 1 ENG BLEED OFF, NO CHANGE. TEMP LOWERED TO 180 DEGREES IN CRUISE WHEN THROTTLES WERE REDUCED. REMAINED AT 180 DEGREES FOR THE DURATION OF THE FLIGHT. ALL OTHER ENGINE INDICA
- [SDR 07FDEA05109](https://openairdocs.org/sdr/07FDEA05109.md): Bleed Valve · cracked · Dec 20, 2007 · N448FE · Airbus A310222 · Compressor Bleed Valve
  > DURING CLIMB TO CRUISE ALTITUDE, ECAM PRESENTED AN ADVISORY PAGE FOR NR 1 ENG NAC TEMP AT 200. SELECTED NR 1 BLEED VALVE OFF AND REDUCED POWER ON NR 1 WITH NO CHANGE IN NR 1 NAC TEMP. AFTER THROTTLE WAS REDUCED TO ALMOST IDLE SETTING, NR 1 NAC TEMP FELL TO
- [SDR 07FDEA05115](https://openairdocs.org/sdr/07FDEA05115.md): Valve · cracked · Dec 20, 2007 · N448FE · Airbus A310222 · Bleed Air Indicating System
  > DURING CLIMB TO CRUISE ALTITUDE, ECAM PRESENTED AN ADVISORY PAGE FOR NR 1 ENG NAC TEMP AT 200. SELECTED NR 1 BLEED VALVE OFF AND REDUCED POWER ON NR 1 WITH NO CHANGE IN NR 1 NAC TEMP. AFTER THROTTLE WAS REDUCED TO ALMOST IDLE SETTING, NR 1 NAC TEMP FELL TO 1
- [SDR 05FDEA03385](https://openairdocs.org/sdr/05FDEA03385.md): Smoke Detector · malfunctioned · Oct 11, 2005 · N448FE · Airbus A310222 · Smoke Detection
  > JUST AFTER T/O HAD AVIONICS SMOKE WARNING ON ECAM AND OVERHEAD. NO ODOR OR SIGN OF SMOKE. DECLARED EMERGENCY. RETURNED TO KABQ LANDING WT APPROX 209,000 NR, BELOW MAX LANDING WEIGHT. CHECKED AVIONICS COMPT FOR EVIDENCE OF SMOKE. DUE TO NO EVIDENCE OF SMOK
- [SDR 05FDEA03141](https://openairdocs.org/sdr/05FDEA03141.md): Skin · corroded · Sep 27, 2005 · N448FE · Airbus A310222 · Fuselage Main, Plate/Skin
  > ACCOMPLISH MAINTENANCE "C" CHECK NR 004, FWD CARGO COMPARTMENT, FUSELAGE SKIN SURFACE PANEL FOUND WITH CORROSION AT INTERNAL PART OF COMPARTMENT BETWEEN FS 37 AND FS 38 BETWEEN STR 53 LT AND STR 53 RT. REPAIRED ACCOMPLISH PER FEDEX EA 6-5330-93193 (FOR DETAIL
- [SDR 05FDEA03047](https://openairdocs.org/sdr/05FDEA03047.md): Skin · corroded · Sep 22, 2005 · N448FE · Airbus A310222 · Wing, Center Box
  > CORROSION AT CENTRAL WING UPPER SKIN SURFACE FR 46 Y- 2126. REMOVED/INSTALLED ELEMENTS PER SRM 51-40-21 & 51-40-44. REMOVED CORROSION PER SRM 51-74-10 & 51-29-00 PG. 201. PERFORMED EDDY CURRENTS FOUND "OK". PAINTED PER SRM 51-75-10-08.
- [SDR 05FDEA03045](https://openairdocs.org/sdr/05FDEA03045.md): Arm · corroded · Sep 22, 2005 · N448FE · Airbus A310222 · Passenger/Crew Doors
  > RT FWD DOOR, LOWER ARM ASSY FOUND CORRODED. REPLACED BY A NEW ONE IAW AMM 52-11-21-4. FUNCTIONAL CHECK IAW AMM 52-10-11-501.
- [SDR 05FDEA00178](https://openairdocs.org/sdr/05FDEA00178.md): Actuator · malfunctioned · Jan 26, 2005 · N448FE · Airbus A310222 · Rudder Control System
  > AFTER TAKEOFF AND FLAPS RETRACTED, BOTH NR 1 & 2 RUDDER FAULT. WOULD NOT RESET, EXTENDED THE FLAPS & THE RUDDER FAULT WENT AWAY. REMOVED AND REPLACED RUDDER VARIABLE STOP ACTUATOR PER A310-200 MM 27-23-23-4. TEST GOOD ON SYS 1 & 2 PER MM 27-23-00-5. PREMAT
- [SDR 03FDEA00231](https://openairdocs.org/sdr/03FDEA00231.md): Access Panel · damaged · Mar 5, 2003 · N448FE · Airbus A310 · Wing, Plate/Skin
  > LT WING, LOWER ACCESS CUTOUT FOR PANEL 550GB. TWO SCREW HOLES FOR PANEL HAVE DAMAGED EDGES. REMOVED ANCHOR NUTS TO ACCESS DAMAGED HOLES. REMOVED DAMAGED AREA AND REAMED HOLES TO 0.495 AND 0.467. ENSURED CLEANED HOLES ARE CRACK FREE BY HFEC IAW NTM 51-10-01.
- [SDR 02FDEA00498](https://openairdocs.org/sdr/02FDEA00498.md): Controller · Jul 17, 2002 · N448FE · Airbus A310 · Cabin Pressure Control System
  > CLIMBING OUT OF SEA, ECAM ALERT - "EXCESS CAB ALT". DONNED O2 MASKS AND TRIED TO TROUBLESHOOT PROBLEM. SWAPPED REGULATORS FOR PRESS. TRIED MANUALLY PRESS AIRPLANE. NO SUCCESS. RETURNED TO SEA FOR LANDING. UPON BLOCK-IN, COULD NOT TEST EITHER SYS 1 OR 2.
- [SDR 02FDEA00143](https://openairdocs.org/sdr/02FDEA00143.md): Coalescer Bag · contaminated · Feb 26, 2002 · N448FE · Airbus A310222 · Humidity Control System
  > ON FINAL ECAM WARN AVIONICS SMOKE AND M/DECK M/CARGO MID SMOKE DETECT. REMOVED AND REPLACED LT & RT COALESCER BAGS PER MM 21-51-16-3. OK FOR SERVICE.
- [SDR 02FDEA00125](https://openairdocs.org/sdr/02FDEA00125.md): Indicator · faulty · Feb 14, 2002 · N448FE · Airbus A310222 · Engine Oil Quantity
  > AFTER T/O OIL QTY ON NR 1 ENG SHOW 2 QT ON BOTH ANALOG AND ECAM IND. REINSTALLED C/P AND HEAT SHIELD. REMOVED AND REPLACED OIL QTY IND. TEST NORMAL PER 79-31-00-5-A.
- [SDR 01FDEA01070](https://openairdocs.org/sdr/01FDEA01070.md): Smoke Warning · smoke · Dec 13, 2001 · N448FE · Airbus A310222 · Fire Detection
  > 1-396 RECEIVED MAIN DECK CARGO SMOKE WARNING. BITE CHECK PER MM 26-19-00-5. NO FAULT FOUND. OK FOR SERVICE.
- [SDR 00FDEA00625](https://openairdocs.org/sdr/00FDEA00625.md): Elevator · malfunctioned · Sep 5, 2000 · N448FE · Airbus A310221 · Elevator Control System
  > AFT 20 MIN OF FLT A/C HAD A AIR TURNBACK DUE TO TOO MUCH PRESS NEEDED TO OPERATE ELEVATOR. AC RETURN TO LAX.
- [SDR 99FDEA00236](https://openairdocs.org/sdr/99FDEA00236.md): Pitot System · dirty · Jun 24, 1999 · N448FE · Airbus A310221 · Pitot/Static System
  > 99-143 - NO AIRSPEED IND ON F/O SIDE PFD ON T/O. RTO AT 70 KNOTS. PERF ADC NR 2 OPS CK IAW MM 34-10-00 SYS CK GOOD. FLUSHED NR 2 PITOT SYS IAW 34-10-00, FOUND DEBRIS IN F/O PITOT TUBE, SYS OK FOR SERVICE.
- [SDR 99FDEA00233](https://openairdocs.org/sdr/99FDEA00233.md): Adc · inoperative · Jun 23, 1999 · N448FE · Airbus A310221 · Air Data Computer
  > NO AIRSPEED IND ON TAKEOFF ROLL. ALL PFD SYMBOLS WERE PRESENT BUT CAPT AIRSPEED TRIANGLE NEVER INCREASED FROM 0. REMOVED AND REPLACED NR 1 ADC IAW M/M 34-11-34, SYSTEM OK FOR SERVICE.
- [SDR 99FDEA00234](https://openairdocs.org/sdr/99FDEA00234.md): Airspeed Ind · inoperative · Jun 22, 1999 · N448FE · Airbus A310221 · Airspeed/Mach Indicator
  > CAPT HAD NO AIRSPEED INDICATION ON PFD DURING T/O. ABORTED AT 70 KNOTS. F/O AND STBY AIRSPEED INDICATE NORMAL.
- [SDR 98FDEA00480](https://openairdocs.org/sdr/98FDEA00480.md): Control Handle · failed · Jul 30, 1998 · N448FE · Airbus A310221 · Landing Gear Selector
  > 98-0188 STA-IND - AFTER T/O LANDING GEAR WOULD NOT RETRACT UNLOCK AND GREEN DIAMONDS ON ALL 6 INDICATORS. BOTH SYS 1 AND SYS 2 ON POSITION DETECTOR SWITCH TRIED MULTIPLE TIMES. REMOVED AND REPLACED LAND GEAR CONTROL HANDLE MODULE PER M/M 32-30. PERFORMED G
- [SDR 97FDEA00561](https://openairdocs.org/sdr/97FDEA00561.md): Pitot Line · clogged · Aug 16, 1997 · N448FE · Airbus A310221 · Pitot/Static System
  > ON DEPARTURE CAPTS AIRSPEED TAPE WAS SHOWING ERRONEOUS SPD IND. SWIT TO ALT SPD TAPE RETURNED TO OPERATION BUT SPD WAS 300 KTS WHEN F/O WAS 160 KTS. SWITCHED TO ALT EFIS NO CHANGE. AFTER FLAP/SLAT RETRACT NR 1 YAW DAMPER FAILED AUTO THROTTLE SYS FAILED WOUL
- [SDR 97FDEA00170](https://openairdocs.org/sdr/97FDEA00170.md): Fuel Control · out of adjust · Mar 14, 1997 · N448FE · Airbus A310221 · Fuel Control/Turbine Engines
  > ON TAXI IN AT IDLE POWER, NR 1 ENG FLAMED OUT WITH CORRESPONDING ENG FAIL ECAM WARNINGS. FOR INFORMATION, 25-30 KT TAILWIND WAS PRESENT WHEN ENG FAILED. ENGINE RUN PERFORMED AND GROUND IDLE SPEED FOUND TO BE LOW. TEST NR 9 FUEL CONTROL TRIM PERFORMED IAW M/
- [SDR 96FDEA01684](https://openairdocs.org/sdr/96FDEA01684.md): Tr Cowl · damaged · Nov 20, 1996 · N448FE · Airbus A310221 · Engine Thrust Reverser
  > UPON ARRIVAL, DURING WALKAROUND FOUND APPROX 18 DIA HOLE ON AFT INBD EDGE OF NR 2 ENGINE FAN COWL. ALSO, NOTED SEVERE DISCOLORATION ON INBD REVERSER HALF WITH BURN STREAKS AND STRUCTURAL DAMAGE TO THE REVERSER. *S/D* REMOVED AND REPLACED GROUND THRUST REV C

## 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 = 'N448FE' AND deregistration_id = 'N448FE-2013-07-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N448FE-2013-07-29/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.