N449FE, cancelled May 10, 2010

Service difficulty reports · 40

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA200812095113Warning System · illuminatedNR 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. Dec 9, 2008 · N449FE · Airbus A310222 · Engine Thrust ReverserSDR 07FDEA02865Shutoff Valve · inoperativeAFTER 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 Aug 14, 2007 · N449FE · Airbus A310222 · Engine Thrust ReverserSDR 07FDEA02872Shutoff Valve · inoperativeAFTER 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 "MAug 14, 2007 · N449FE · Airbus A310222 · Engine Thrust ReverserSDR 07FDEA02375Rectifier · failedFOUND 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 FAULTJul 5, 2007 · N449FE · Airbus A310222 · AC Power Distribution SystemSDR 07FDEA02296Connector · looseON 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 CONJun 27, 2007 · N449FE · Airbus A310222 · Engine Exhaust System WiringSDR 07FDEA02033Unknown · unknownSHORTLY 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 PRMay 31, 2007 · N449FE · Airbus A310 · Auto Flight SystemSDR 07FDEA01348Outflow Valve · malfunctionedNR 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 POSITIONApr 3, 2007 · N449FE · Airbus A310222 · Pressure Regulator/Outflow ValveSDR 07FDEA00327Unknown · unknownIN 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 OFeb 5, 2007 · N449FE · Airbus A310222 · Standard Practices/StructuresSDR 06FDEA04099Frame · unknownUPON 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.Nov 23, 2006 · N449FE · Airbus A310222 · Wing, Center BoxSDR 06FDEA04044Stringer · damagedPREVIOUS 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.Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 06FDEA04043Support · corroded4 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FS 40 STRG 1 C/W FEDEX EA6-5730-105024.Nov 19, 2006 · N449FE · Airbus A310222 · Wing, Center BoxSDR 06FDEA04042Support · corroded13 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FRAME 40 STRINGER 3R C/W FEDEX EA6-5730-105024.Nov 19, 2006 · N449FE · Airbus A310222 · Wing, Center BoxSDR 06FDEA04040Spar · corroded33 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.Nov 19, 2006 · N449FE · Airbus A310 · Wing, Center BoxSDR 06FDEA04039Support · corroded4 AREAS OF CORROSION AROUND FASTENERS ON HORIZONTAL LOWER SURFACE OF STRINGER SUPPORT STRAP AT FS 40 5L. REPAIRED PER FEDEX EA6-5730-105024.Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 06FDEA04038Support · corrodedSEVEN AREAS OF CORROSION AROUND FASTENERS ON HORIZONTIAL LOWER SUFACE OF STRINGER SUPPORT AT FS 40 STRINGER 2L. REPAIRED IAW FEDEX EA6-5730-105024.Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 06FDEA04037Strap · corroded12 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.Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Miscellaneous StructureSDR 06FDEA04036Spar · corroded29 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.Nov 19, 2006 · N449FE · Airbus A310222 · Wing SparSDR 06FDEA04035Stringer · corroded22 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.Nov 19, 2006 · N449FE · Airbus A310222 · Wing, Longeron/StringerSDR 06FDEA04034Stringer · misrepairedPREVIOUS 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.Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 06FDEA04033Stringer · misrepairedPREVIOUS 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 EA6-5310-105015Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 06FDEA04032Stringer · misrepairedPREVIOUS 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.Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 06FDEA04031Spar · misrepairedPREVIOUS 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 BNov 19, 2006 · N449FE · Airbus A310222 · Horizontal Stabilizer, Spar/RibSDR 06FDEA04030Stringer · misrepairedPREVIOUS 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 53-10-1Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 06FDEA04029Skin · misrepairedPREVIOUS 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 MATERNov 19, 2006 · N449FE · Airbus A310222 · Cargo/Baggage DoorsSDR 06FDEA04028Frame · damagedUPON 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.Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, FrameSDR 06FDEA04027Frame · damagedUPON 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.Nov 19, 2006 · N449FE · Airbus A310222 · Fuselage Main, FrameSDR 06FDEA03902Spar · corrodedAFTER 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 RNov 6, 2006 · N449FE · Airbus A310222 · Horizontal Stabilizer, Spar/RibSDR 06FDEA02276Trunnion · crackedFOUND LT GEAR AFT TRUNNION FWD SUPPORT FITTING CRACKED WHILE PERFORMING GEAR LUBE DURING B CHECK. AIRBUS FIELD TEAM REMOVED AND REPLACED LT GEAR TRUNNION.Jun 8, 2006 · N449FE · Airbus A310222 · Wing, Landing Gear Attach FittingsSDR 06FDEA2276Support Fitting · crackedFOUND LEFT GEAR AFT TRUNNION FWD SUPPORT FITTING CRACKED WHILE PERFORMING GEAR LUBE DURING B-CHECK.Jun 8, 2006 · N449FE · Airbus A310222 · Wing, Landing Gear Attach FittingsSDR 04FDEA02081Panel · damagedPANEL 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.Jul 15, 2004 · N449FE · Airbus A310222 · Wing, Plate/SkinSDR 04FDEA02080Panel · damagedPANEL LAND 650 KB HAS 1 EA ELONGATED HOLE. COMPLIED WITH EA 6-5730-55328A PT1.Jul 15, 2004 · N449FE · Airbus A310222 · Wing, Plate/SkinSDR 01FDEA00057Idg · inoperativeDURING 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.Jan 31, 2001 · N449FE · Airbus A310222 · AC Generator-AlternatorSDR 00FDEA00794Indicator · illuminatedREJECTED T/O DUE TO AN OIL PRESSURE LIGHT ILLUMINATED ON NR 1 ENGINE.Nov 29, 2000 · N449FE · Airbus A310222 · Engine Oil QuantitySDR 00FDEA00724Controller · failedNR 1 CABIN PRESSURE FAILED AFT T/O, SEL NR 2 CABIN PRESSURE AC FAILED TO PRESSURIZE.Oct 19, 2000 · N449FE · Airbus A310222 · Cabin Pressure ControllerSDR 00FDEA00236Damper · failedAFT 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.Apr 12, 2000 · N449FE · Airbus A310222 · Landing Gear Retraction/Extension SystemSDR 00FDEA00214Landing Gear · malfunctionedLANDING GEAR WON''T RETRACT. SERVICE RT PITCH DAMPER AND REPLACED PRESSURE DROP IND PER FEDEX AC MX WORK CARD NR 47B402.Apr 9, 2000 · N449FE · Airbus A310222 · Landing Gear Retraction/Extension SystemSDR 99FDEA00514Computer · inoperative99-297 - ECAM AND MASTER SHOW CHECK FUEL MGMT. REMOVED AND REPLACED FUEL QTY COMPUTER PERFORM BITE CK.Dec 29, 1999 · N449FE · Airbus A310222 · Fuel Quantity SensorSDR 99FDEA00439Switch · out of adjustNR 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. ROct 21, 1999 · N449FE · Airbus A310222 · Engine Thrust ReverserSDR 99FDEA00367Fitting · crackedTWO 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.Sep 7, 1999 · N449FE · Airbus A310222 · Landing Gear Door ActuatorSDR 98FDEA00048Hyd Elec Pump · shortedBURNT 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.Jan 26, 1998 · N449FE · Airbus A310222 · Hydraulic Pump (Electric/Engine), Main
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