# Service difficulty reports: N449FE, cancelled May 10, 2010

A list on [N449FE, cancelled May 10, 2010](https://openairdocs.org/deregistered/N449FE-2010-05-10.md).

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

- [SDR FDEA200812095113](https://openairdocs.org/sdr/FDEA200812095113.md): Warning System · illuminated · Dec 9, 2008 · N449FE · Airbus A310222 · Engine Thrust Reverser
  > NR 2 ENGINE REVERSER UNLOCK ECAM AT ABOUT 60 KTS ON TAKEOFF. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXPIRATION: 14 DEC 08. FOUND NR 2 ENGINE LT REVERSER STOW SWITCH FALLING OFF CAM WHILE SHAKING WIRES FOR T/S. DUPLICATED UNLOCK LIGHT.
- [SDR 07FDEA02865](https://openairdocs.org/sdr/07FDEA02865.md): Shutoff Valve · inoperative · Aug 14, 2007 · N449FE · Airbus A310222 · Engine Thrust Reverser
  > AFTER LIFTOFF (KATL) ENG NR 1 THRUST REVERSER SHOWED "UNLOCKED". ON TAKEOFF ROLL LIGHT FLICKERED MOMENTARILY THEN WENT OUT. FOLLOWED QRH AND ECAM PROCEDURE AND DECLARED EMERGENCY. REPLACED NR 1 THRUST REVERSER PRESSURE REGULATOR SHUTOFF VALVE PER A310-200
- [SDR 07FDEA02872](https://openairdocs.org/sdr/07FDEA02872.md): Shutoff Valve · inoperative · Aug 14, 2007 · N449FE · Airbus A310222 · Engine Thrust Reverser
  > AFTER LIFTOFF(KATL) ENG1 THRUST REVERSER SHOWED "UNLOCKED". ON T/O ROLL, LIGHT FLICKERED MOMENTARILY THEN WENT OUT. FOLLOWED QRH AND ECAM PROC AND DECLARED EMERGENCY MEL 14AUG07. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-C CATEGORY: C EXP: 17AUG07 "M
- [SDR 07FDEA02375](https://openairdocs.org/sdr/07FDEA02375.md): Rectifier · failed · Jul 5, 2007 · N449FE · Airbus A310222 · AC Power Distribution System
  > FOUND NR 1 TRANSFORMER RECTIFIER FAULTED ON MAINT PANE (MULTIPLE FAULTS IN FLT- TRANSPONDER, AUTO-THROTTLE, PITCH TRIM). REMOVED AND REPLACED NR 1 TRANSFORMER RECTIFIER IAW AIRBUS M/M 24-32-11-4. OPS CHECKED NORMAL PER AIRBUS M/M 24-32-00-5. ALL OTHER FAULT
- [SDR 07FDEA02296](https://openairdocs.org/sdr/07FDEA02296.md): Connector · loose · Jun 27, 2007 · N449FE · Airbus A310222 · Engine Exhaust System Wiring
  > ON TAKEOFF REC'D NR 1 REVERSER UNLOCKED LIGHT AT 2 SEPARATE TIMES. ONCE DURING ENG OVERTEMP AND AFTER THROTTLE WAS REDUCED. ON TAKEOFF, ECAM NR 1 ENG OVERTEMP, FOLLOWED QRH A/C IN WORK. FOUND CONNECTOR DS307 LH REVERSER STOW CONNECTOR VERY LOOSE. CLEANED CON
- [SDR 07FDEA02033](https://openairdocs.org/sdr/07FDEA02033.md): Unknown · unknown · May 31, 2007 · N449FE · Airbus A310 · Auto Flight System
  > SHORTLY AFTER T/O A/C ACTED AS IF THERE WAS GROUND SENSING PROBLEM, MALFUNCTIONS TO INCLUDE; ATS 1, PITCH TRIM 1, ALL THREE PITOT PROBE, CAPT TAT, BOTH PRESS CONTROLERS: GEAR WOULD NOT RETRACT SYS 1, A/P 1&2 INOP. INSTALLED NEW NOSE STRUT SENSOR 55GB PR
- [SDR 07FDEA01348](https://openairdocs.org/sdr/07FDEA01348.md): Outflow Valve · malfunctioned · Apr 3, 2007 · N449FE · Airbus A310222 · Pressure Regulator/Outflow Valve
  > NR 2 AUTO PRESSURIZATION SYSTEM FWD AND AFT VALVES WOULD NOT CLOSE. NR 1 SYSTEM COULD NOT CONTROL AIRCRAFT PRESSURE. ATTEMPTED TO CONTROL PRESSURIZATION MANUALLY. STILL COULD NOT CONTROL PRESSURIZATION WITH THE NR 2 FWD AND AFT VALVES IN THE OPEN POSITION
- [SDR 07FDEA00327](https://openairdocs.org/sdr/07FDEA00327.md): Unknown · unknown · Feb 5, 2007 · N449FE · Airbus A310222 · Standard Practices/Structures
  > IN FLIGHT AIRCRAFT WANTED TO TURN RIGHT. REQUIRED 3 UNITS AILERON DEFLECTION TO FLY STRAIGHT. REQUIRED 14 UNITS OF RIGHT RUDDER TRIM TO LEVEL OUT AILERONS. NO CHANGES FROM CLIMB POWER TO IDLE POWER. NO CHANGE YAW DAMPERS ON OR OFF. NO CHANGES AUTOPILOT O
- [SDR 06FDEA04099](https://openairdocs.org/sdr/06FDEA04099.md): Frame · unknown · Nov 23, 2006 · N449FE · Airbus A310222 · Wing, Center Box
  > UPON DETAILED SPECIAL INSP (SDET) OF CENTER WING BOX LOWER SKIN BETWEEN FRAME 40/41AND 47/48 LT SIDE AT FRAME 44.2 OB MOST FWD HOLE SHOWS POSITIVE INDICATION DUE TO A BUSHING INSTALLED IN THE HOLE COMPLIED WITH EA 6-5710-106250 PT1.
- [SDR 06FDEA04044](https://openairdocs.org/sdr/06FDEA04044.md): Stringer · damaged · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > PREVIOUS REPAIR BULK CARGO UNDER FLOOR STRINGER 55 LT HAS A STRG REPAIR BETWEEN FS 66 AND 70 WITH 4 STRINGER SECTIONS AND 4 REPAIR SPLICES REPAIRED PER FEDEX EA6-5310-105016.
- [SDR 06FDEA04043](https://openairdocs.org/sdr/06FDEA04043.md): Support · corroded · Nov 19, 2006 · N449FE · Airbus A310222 · Wing, Center Box
  > 4 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FS 40 STRG 1 C/W FEDEX EA6-5730-105024.
- [SDR 06FDEA04042](https://openairdocs.org/sdr/06FDEA04042.md): Support · corroded · Nov 19, 2006 · N449FE · Airbus A310222 · Wing, Center Box
  > 13 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FRAME 40 STRINGER 3R C/W FEDEX EA6-5730-105024.
- [SDR 06FDEA04040](https://openairdocs.org/sdr/06FDEA04040.md): Spar · corroded · Nov 19, 2006 · N449FE · Airbus A310 · Wing, Center Box
  > 33 AREAS OF CORROSION AROUND FASTENERS ALONG FS 40 AT CTR WING TANK LOWER SPAR CHORD BETWEEN STRINGER 1 AND 5R (EXTERNAL OF TANK) C/W FEDEX EA6-5730-105024.
- [SDR 06FDEA04039](https://openairdocs.org/sdr/06FDEA04039.md): Support · corroded · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > 4 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FS 40 5L. REPAIRED PER FEDEX EA6-5730-105024.
- [SDR 06FDEA04038](https://openairdocs.org/sdr/06FDEA04038.md): Support · corroded · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > SEVEN AREAS OF CORROSION AROUND FASTENERS ON HORIZONTIAL LOWER SUFACE OF STRINGER SUPPORT AT FS 40 STRINGER 2L. REPAIRED IAW FEDEX EA6-5730-105024.
- [SDR 06FDEA04037](https://openairdocs.org/sdr/06FDEA04037.md): Strap · corroded · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Miscellaneous Structure
  > 12 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FS 40 STRINGER 3L. REPAIRED IAW WITH FEDEX EA6-5730-105024.
- [SDR 06FDEA04036](https://openairdocs.org/sdr/06FDEA04036.md): Spar · corroded · Nov 19, 2006 · N449FE · Airbus A310222 · Wing Spar
  > 29 AREAS OF CORROSION AROUND FASTENERS ALONG FRAME 40 AT CTR WING TANK LOWER SPAR CHORD BETWEEN STGR 3L AND 5L (EXTERNAL OF TANK) REPAIRED PER FEDEX EA6-5730-105024.
- [SDR 06FDEA04035](https://openairdocs.org/sdr/06FDEA04035.md): Stringer · corroded · Nov 19, 2006 · N449FE · Airbus A310222 · Wing, Longeron/Stringer
  > 22 AREAS OF CORROSION AROUND FASTENERS ALONG STIFFENER 3 AFR43 BETWEEN CENTER WING TANK LOWER SKIN STRINGERS 2L AND 5L (EXTERNAL OF TANK). REPAIRED IAW FEDEX EA6-5730-105024.
- [SDR 06FDEA04034](https://openairdocs.org/sdr/06FDEA04034.md): Stringer · misrepaired · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > PREVIOUS REPAIR BULK CARGO UNDER FLOOR STRG 53 LT HAS A STGR REPAIR BETWEEN FS 66/70 WITH 4 STGR SECTIONS AND 4 REPAIR SPLICES PREVIOUSLY INSTALLED REPAIR FOUND NOT TO BE IAW A310SRM 53-10-14 FIG 201. REPAIRED STRG PER FEDEX EA6-5310-105016.
- [SDR 06FDEA04033](https://openairdocs.org/sdr/06FDEA04033.md): Stringer · misrepaired · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > PREVIOUS REPAIR BULK CARGO UNDER FLOOR STGR 50 LT HAS A STGR REPAIR BETWEEN FS 65 AND 66 WITH 1EA STGR SECTION AND 1EA REPAIR SPLICE. PREVIOUSLY INSTALLED REPAIR FOUND NOT TO BE IAW A310SRM 53-10-14. REPAIRED STRINGER PER FEDEX EA6-5310-105015
- [SDR 06FDEA04032](https://openairdocs.org/sdr/06FDEA04032.md): Stringer · misrepaired · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > PREVIOUS REPAIR AFT CARGO UNDER FLOOR STRINGER 49 LT HAS A STRINGER REPAIR BETWEEN FS 59/60 WITH 1 EA STRINGER SECTION AND 1 EA REPAIR SPLICE PREVIOUSLY INSTALLED REPAIR NOT TO BE IAW A310 SRM 53-10-14 FIG 201. REPAIRED PER FEDEX EA6-5310-105014.
- [SDR 06FDEA04031](https://openairdocs.org/sdr/06FDEA04031.md): Spar · misrepaired · Nov 19, 2006 · N449FE · Airbus A310222 · Horizontal Stabilizer, Spar/Rib
  > PREVIOUS REPAIR, RT REAR UPPER SPAR CHORD HAS A STRAP REPAIR 13.5" LONG BETWEEN RIB 21 TO THE END OF THE SPAR CHORD. PREVIOUSLY INSTALLED REPAIR LOCATED AT RT THS REAR THS REAR UPPER SPAR CHORD BETWEEN RIB 21 TO O/B END OF SPAR CHORD WAS DETERMINED NOT TO B
- [SDR 06FDEA04030](https://openairdocs.org/sdr/06FDEA04030.md): Stringer · misrepaired · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/Stringer
  > PREVIOUS REPAIR BULK CARGO UNDER FLOOR STRINGER 49 LT HAS A STRINGER REPAIR BETWEEN FRAMES 65 AND 66 WITH 1 STRINGER SECTION AND 1 REPAIR SPLICE PREVIOUSLY INSTALLED REPAIR LOCATED AT FRAME 65-66 ON STRINGER 49 LT WAS DETERMINED NOT TO BE IAW A310SRM 53-10-1
- [SDR 06FDEA04029](https://openairdocs.org/sdr/06FDEA04029.md): Skin · misrepaired · Nov 19, 2006 · N449FE · Airbus A310222 · Cargo/Baggage Doors
  > PREVIOUS REPAIR BULK CARGO DOOR EXTERIOR SKIN HAS AN EXTERNAL REPAIR DOUBLER MEASURING 6.25" BY 15.1" AT THE LOWER AFT CORNER PREVIOUSLY INSTALLED REPAIR LOCATED AT BULK CARGO DOOR WAS DETERMINED NOT TO BE IAW A310 SRM 52-30-00 FIG 207 DUE TO INCORRECT MATER
- [SDR 06FDEA04028](https://openairdocs.org/sdr/06FDEA04028.md): Frame · damaged · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Frame
  > UPON REMOVAL OF WEB RT BETWEEN FS 12 AND FS 13 3 HOLES ARE ELONGATED DOUBLE DRILLED FLOOR LEVEL AT FS 13 REPAIRED FRAME AT FS 13 RT IAW A310SRM 53-12-13 FIG 201 SEE JPF FOR JOB TASK STEP.
- [SDR 06FDEA04027](https://openairdocs.org/sdr/06FDEA04027.md): Frame · damaged · Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Frame
  > UPON REMOVAL OF WEB BETWEEN FS 12 - FS 13 FOUND 3 HOLES ELONGATED DOUBLE DRILLED FLOOR LEVEL LT SIDE AT FS 13 REPAIRED FRAME AT FS-13, IAW A310 SRM 53-12-31 FIG 201 SEE JPF FOR JOB TASK STEPS.
- [SDR 06FDEA03902](https://openairdocs.org/sdr/06FDEA03902.md): Spar · corroded · Nov 6, 2006 · N449FE · Airbus A310222 · Horizontal Stabilizer, Spar/Rib
  > AFTER REMOVAL OF LEADING EDGE OF LT HORIZONTAL STAB, FOUND CORROSION ON UPPER CHORD OF FORWARD SPAR NEAR RIB 10 REMOVED CORROSION IAW A310 SRM 51-74-10, CHECKED MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW A310 SRM 55-10-00 FIG 101 TABLE 101. INSTALLED STRAP R
- [SDR 06FDEA02276](https://openairdocs.org/sdr/06FDEA02276.md): Trunnion · cracked · Jun 8, 2006 · N449FE · Airbus A310222 · Wing, Landing Gear Attach Fittings
  > FOUND LT GEAR AFT TRUNNION FWD SUPPORT FITTING CRACKED WHILE PERFORMING GEAR LUBE DURING B CHECK. AIRBUS FIELD TEAM REMOVED AND REPLACED LT GEAR TRUNNION.
- [SDR 06FDEA2276](https://openairdocs.org/sdr/06FDEA2276.md): Support Fitting · cracked · Jun 8, 2006 · N449FE · Airbus A310222 · Wing, Landing Gear Attach Fittings
  > FOUND LEFT GEAR AFT TRUNNION FWD SUPPORT FITTING CRACKED WHILE PERFORMING GEAR LUBE DURING B-CHECK.
- [SDR 04FDEA02081](https://openairdocs.org/sdr/04FDEA02081.md): Panel · damaged · Jul 15, 2004 · N449FE · Airbus A310222 · Wing, Plate/Skin
  > PANEL 550HB HAS 2 EA ELONGATED HOLES. REPAIRED 1 EA HOLE IAW A310/200 SRM 51-40-44 FIG 1 CHAMBER CODE-J, COMPLIED WITH EA 6-5730-55328A PT 1 ON 1EA HOLE.
- [SDR 04FDEA02080](https://openairdocs.org/sdr/04FDEA02080.md): Panel · damaged · Jul 15, 2004 · N449FE · Airbus A310222 · Wing, Plate/Skin
  > PANEL LAND 650 KB HAS 1 EA ELONGATED HOLE. COMPLIED WITH EA 6-5730-55328A PT1.
- [SDR 01FDEA00057](https://openairdocs.org/sdr/01FDEA00057.md): Idg · inoperative · Jan 31, 2001 · N449FE · Airbus A310222 · AC Generator-Alternator
  > DURING CLIMBOUT, NR 2 IDG TEMP CONT TO CLIMB. VERIFIED NR 2 IDG DEFERRED CORRECTLY. VERIFIED PROPER SERVICE ACCOMPLISH. NO FAULTS NOTED. IDG TEMP WITHIN LIMITS REF MM 24-11-00-001. AC OK FOR SERVICE. NR 2 IDG REMAINS DEFERRED.
- [SDR 00FDEA00794](https://openairdocs.org/sdr/00FDEA00794.md): Indicator · illuminated · Nov 29, 2000 · N449FE · Airbus A310222 · Engine Oil Quantity
  > REJECTED T/O DUE TO AN OIL PRESSURE LIGHT ILLUMINATED ON NR 1 ENGINE.
- [SDR 00FDEA00724](https://openairdocs.org/sdr/00FDEA00724.md): Controller · failed · Oct 19, 2000 · N449FE · Airbus A310222 · Cabin Pressure Controller
  > NR 1 CABIN PRESSURE FAILED AFT T/O, SEL NR 2 CABIN PRESSURE AC FAILED TO PRESSURIZE.
- [SDR 00FDEA00236](https://openairdocs.org/sdr/00FDEA00236.md): Damper · failed · Apr 12, 2000 · N449FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > AFT TO LANDING GEAR WOULD NOT RETRACT IN SYS 1 OR 2. RECYCLED TWICE EACH SYS. REMOVED AND REPLACED RT MLG PITCH DAMPER IAW AMM 32-11-15. OPS CK PER IAW AMM 32-31-00-5.
- [SDR 00FDEA00214](https://openairdocs.org/sdr/00FDEA00214.md): Landing Gear · malfunctioned · Apr 9, 2000 · N449FE · Airbus A310222 · Landing Gear Retraction/Extension System
  > LANDING GEAR WON''T RETRACT. SERVICE RT PITCH DAMPER AND REPLACED PRESSURE DROP IND PER FEDEX AC MX WORK CARD NR 47B402.
- [SDR 99FDEA00514](https://openairdocs.org/sdr/99FDEA00514.md): Computer · inoperative · Dec 29, 1999 · N449FE · Airbus A310222 · Fuel Quantity Sensor
  > 99-297 - ECAM AND MASTER SHOW CHECK FUEL MGMT. REMOVED AND REPLACED FUEL QTY COMPUTER PERFORM BITE CK.
- [SDR 99FDEA00439](https://openairdocs.org/sdr/99FDEA00439.md): Switch · out of adjust · Oct 21, 1999 · N449FE · Airbus A310222 · Engine Thrust Reverser
  > NR 1 ENG REV UNLOCK LIGHT CAME ON AT APPROX 55 KTS ON T/O ROLL. ABORTED T/O. NR 1 THRUST REVERSER WAS DEFERRED MEL 78-1 CTRL NR 61783. ADJUSTED STOW SWITCHES PER A310 MM 78-31-00 PG 513. REACTIVATED T/R'S AND CLOSED FOA COWL DOORS PER A 310 MM 71-13-00. R
- [SDR 99FDEA00367](https://openairdocs.org/sdr/99FDEA00367.md): Fitting · cracked · Sep 7, 1999 · N449FE · Airbus A310222 · Landing Gear Door Actuator
  > TWO MAIN CROSSBEAMS THAT RUN ACROSS THE LANDING GEAR BAY AND HOLD BOTH MLG DOOR ACTUATORS UPPER ATTACH ARE BROKEN. RT MLG DOOR ACTUATOR ATTACH FITTING WAS PULLED AWAY FROM MAIN CROSSBEAM. *S/D* REPAIRED PER EA 6-5310-42321.
- [SDR 98FDEA00048](https://openairdocs.org/sdr/98FDEA00048.md): Hyd Elec Pump · shorted · Jan 26, 1998 · N449FE · Airbus A310222 · Hydraulic Pump (Electric/Engine), Main
  > BURNT 101 VU WIRING CAUSED BY GREEN HYDRAULIC PUMP INTERNALLY SHORTED. C/B DID NOT POP. THIS CAUSED WIRING BEHIND 101 VU PANEL TO SMOKE AND BURN UP. REPLACED GREEN ELECTRIC HYDRAULIC PUMP. REPLACED 50 AMP CIRCUIT BREAKER, REPAIRED BURNT WIRING.

## 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 = 'N449FE' AND deregistration_id = 'N449FE-2010-05-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N449FE-2010-05-10/reports

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