N448FE, cancelled Jul 29, 2013

Service difficulty reports · 34

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 = 'N448FE' AND deregistration_id = 'N448FE-2013-07-29'
  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 FDEA201007082404Unknown · multiple failAFTER 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. WHEJul 8, 2010 · N448FE · Airbus A310 · Standard Practices/StructuresSDR FDEA200804111385Stringer · damaged1 EA FASTENER HOLE AT FR 54, STRINGER 40 RT HAS DOUBLE DRILL AND DAMAGE IN COUNTERSINK REPAIRED DAMAGE HOLE IAW EA 6-5310-118123.Apr 11, 2008 · N448FE · Airbus A310222 · Fuselage Main, Plate/SkinSDR 08FDEA01385Skin · damaged1 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.Apr 11, 2008 · N448FE · Airbus A310222 · Fuselage Main, Plate/SkinSDR 08FDEA01379Seat Track · damagedPREVIOUS 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 PRApr 10, 2008 · N448FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01232Seat Track · misrepairedPREVIOUS 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 TRApr 1, 2008 · N448FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01225Seat Track · damagedMDCC 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.Apr 1, 2008 · N448FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01224Stringer · misrepairedPREVIOUS 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.Apr 1, 2008 · N448FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 08FDEA01223Stringer · misrepairedPREVIOUS 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 STApr 1, 2008 · N448FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 08FDEA01222Stringer · misrepairedPREVIOUS 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 RApr 1, 2008 · N448FE · Airbus A310222 · Fuselage Main, Longeron/StringerSDR 08FDEA01221Seat Track · misrepairedPREVIOUS 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 SPApr 1, 2008 · N448FE · Airbus A310222 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA01220Paint · missingPREVIOUS 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 EDGApr 1, 2008 · N448FE · Airbus A310222 · Trailing Edge FlapsSDR 08FDEA01219Seal · missingPREVIOUS 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 Apr 1, 2008 · N448FE · Airbus A310222 · Trailing Edge FlapsSDR 08FDEA01218Doubler · corrodedPREVIOUS 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 REQUIREMENTSApr 1, 2008 · N448FE · Airbus A310222 · Fuselage Main, Plate/SkinSDR 07FDEA05106Anti-Ice Valve · malfunctionedAFTER 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 INDICADec 20, 2007 · N448FE · Airbus A310222 · Engine Anti-Icing SystemSDR 07FDEA05109Bleed Valve · crackedDURING 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 TODec 20, 2007 · N448FE · Airbus A310222 · Compressor Bleed ValveSDR 07FDEA05115Valve · crackedDURING 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 1Dec 20, 2007 · N448FE · Airbus A310222 · Bleed Air Indicating SystemSDR 05FDEA03385Smoke Detector · malfunctionedJUST 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 SMOKOct 11, 2005 · N448FE · Airbus A310222 · Smoke DetectionSDR 05FDEA03141Skin · corrodedACCOMPLISH 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 DETAILSep 27, 2005 · N448FE · Airbus A310222 · Fuselage Main, Plate/SkinSDR 05FDEA03047Skin · corrodedCORROSION 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.Sep 22, 2005 · N448FE · Airbus A310222 · Wing, Center BoxSDR 05FDEA03045Arm · corrodedRT 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.Sep 22, 2005 · N448FE · Airbus A310222 · Passenger/Crew DoorsSDR 05FDEA00178Actuator · malfunctionedAFTER 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. PREMATJan 26, 2005 · N448FE · Airbus A310222 · Rudder Control SystemSDR 03FDEA00231Access Panel · damagedLT 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. Mar 5, 2003 · N448FE · Airbus A310 · Wing, Plate/SkinSDR 02FDEA00498ControllerCLIMBING 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.Jul 17, 2002 · N448FE · Airbus A310 · Cabin Pressure Control SystemSDR 02FDEA00143Coalescer Bag · contaminatedON 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.Feb 26, 2002 · N448FE · Airbus A310222 · Humidity Control SystemSDR 02FDEA00125Indicator · faultyAFTER 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.Feb 14, 2002 · N448FE · Airbus A310222 · Engine Oil QuantitySDR 01FDEA01070Smoke Warning · smoke1-396 RECEIVED MAIN DECK CARGO SMOKE WARNING. BITE CHECK PER MM 26-19-00-5. NO FAULT FOUND. OK FOR SERVICE.Dec 13, 2001 · N448FE · Airbus A310222 · Fire DetectionSDR 00FDEA00625Elevator · malfunctionedAFT 20 MIN OF FLT A/C HAD A AIR TURNBACK DUE TO TOO MUCH PRESS NEEDED TO OPERATE ELEVATOR. AC RETURN TO LAX.Sep 5, 2000 · N448FE · Airbus A310221 · Elevator Control SystemSDR 99FDEA00236Pitot System · dirty99-143 - 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.Jun 24, 1999 · N448FE · Airbus A310221 · Pitot/Static SystemSDR 99FDEA00233Adc · inoperativeNO 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.Jun 23, 1999 · N448FE · Airbus A310221 · Air Data ComputerSDR 99FDEA00234Airspeed Ind · inoperativeCAPT HAD NO AIRSPEED INDICATION ON PFD DURING T/O. ABORTED AT 70 KNOTS. F/O AND STBY AIRSPEED INDICATE NORMAL.Jun 22, 1999 · N448FE · Airbus A310221 · Airspeed/Mach IndicatorSDR 98FDEA00480Control Handle · failed98-0188 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 GJul 30, 1998 · N448FE · Airbus A310221 · Landing Gear SelectorSDR 97FDEA00561Pitot Line · cloggedON 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 WOULAug 16, 1997 · N448FE · Airbus A310221 · Pitot/Static SystemSDR 97FDEA00170Fuel Control · out of adjustON 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/Mar 14, 1997 · N448FE · Airbus A310221 · Fuel Control/Turbine EnginesSDR 96FDEA01684Tr Cowl · damagedUPON 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 CNov 20, 1996 · N448FE · Airbus A310221 · Engine Thrust Reverser
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