N251TR, cancelled Apr 1, 2013
Service difficulty reports · 92
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 = 'N251TR' AND deregistration_id = 'N251TR-2013-04-01' 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.
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 = 'N251TR' AND deregistration_id = 'N251TR-2013-04-01' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR KNNA251092010KACYWire · brokenAFTER PUSHBACK / DURING ENGING START NR 2 ENGINE STARTED / WHILE STARTING NR 1 ENGINE - NR 2 ENGINE FLAMED OUT. TROUBLESHOT TO A BROKEN WIRE (WDM: 28-21-01 WIRE NR: 388-010-20) ON THE ENGINE FUEL SHUTOFF VALVE AT CANNON PLUG (D790 - PIN: A) REPAIRED REF: (BOSDR PIDA09006Battery Pack · dischargedL-1 DOOR EMERGENCY ESCAPE SLIDE LIGHT INOP. TROUBLESHOT TO BATTERY. REMOVED AND REPLACED L-1 DOOR EMERGENCY ESCAPE SLIDE LIGHT BATTERY PACK. OPS CHECKS GOOD PER MM 33-51-02.SDR PIDA08033Battery · dischargedEMERGENCY FLASHLIGHT AT L-1 DOOR INOP. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-60-00. OPS CHECK GOOD. (K)SDR PID2008F00003Sensor · failedGEAR WOULD NOT RETRACT. OVER RIDE TRIGGER USED TO RETRACT GEAR. AC RETURNED TO FIELD. PERFORMED OVERWEIGHT LANDING INSPECTION IAW MM 05-51-291. AC IS SAFE FOR INTENDED FERRY FLIGHT.. 7/11/2008: FOUND AIR SAFETY SENSOR BAD. REPLACED AIR SAFELY SENSOR AND OSDR PID2008F00005Battery Pack · inoperativeAFT EMERGENCY EXIT LIGHTS NOT WORKING. REMOVED AND REPLACED AFT BATTERY PACK IAW MM 33-51-57. LIGHTS WORKING NORMAL. (K)SDR PIDA08008Battery Pack · inoperativeAFT EMERGENCY EXIT LIGHTS OUT. REPLACED LEFT EMERGENCY EXIT BATTERY PACK. OPS CHECK GOOD PER MM 33-51-31.SDR PIDA08007Battery Pack · dischargedEMERGENCY LIGHTS INOP AT RIGHT OVERWING AND NR 9 OVERHEAD BIN. REPLACED BATTERY PACK AT RIGHT OVERHEAD MID-CABIN. EMERGENCY LIGHTS OPS GOOD PER MM 33-51-31.SDR PIDA07059Skin · damagedDURING MAINTENANCE CHECK, DAMAGE NOTED ON THE TRAILING OF THE RUDDER APPROXIMATELY 10 INCHES BELOW THE TOP. REPAIRED DAMAGE PER SRM 51-40-14.SDR PIDA07061Door · damagedDURING MAINTENANCE CHECK, DAMAGE NOTED ON THE LEFT ENGINE THRUST REVERSER LOWER DOOR FORWARD EDGE AT APPROXIMATELY 5 O'CLOCK POSITION. REPAIRED PER PACE AIRLINES REPAIR PROCEDURE REPORT EA NR 78-348 DATED 12/14/07 WITH FAA DER APPROVED 8110-3 DATED 12/14/2007SDR PIDA07060Skin · damagedDURING MAINTENANCE CHECK, DAMAGE NOTED ON THE LOWER FORWARD LEFT CORNER OF THE RUDDER. REPAIRED PER BOEING TELEX MESSAGE NOS 1-724910440-9 AND -10 WITH FAA DOA APPROVED 8100-9 DATED DEC 20, 2007.SDR PIDA07058Skin · crackedDURING MAINTENANCE CHECK, NOTED A CRACK IN THE LEADING EDGE OF THE RUDDER AT RUDDER STATION 58.6. REPAIRED PER BOEING TELEX 1-720703898-1 AND -3 WITH FAA DOA APPROVED 8100-9 DATED DEC 15, 2007. SUSPECT DAMAGE OCCURRED DURING RUDDER REMOVAL FROM VERTICAL FIN.SDR PIDA07043Thrust Reverser · damagedDURING MAINTENANCE VISIT, NOTED DAMAGE TO LEFT ENGINE I/B THRUST REVERSER SKIN AND SUPPORT FRAME. REPAIRED PER PACE AIRLINES REPAIR PROCEDURE REPORT, EA 78-190.SDR PIDA07019Wedge · damagedDURING MAINTENANCE, DISCOVERED A NICK IN THE TRAILING EDGE OF THE RUDDER APPROXIMATELY 86 INCHES FROM THE LOWER END. REPAIRED DAMAGE PER SRM 51-40-15 REPAIR 11 AND BOEING MESSAGES 1-317406998-1, -7, -8, -9, -10, AND -11 WITH FAA DOA APPROVED 8100-9 DATED APR SDR PIDA06085Control Panel · inoperativeAUTOPILOT SWITCHES WILL NOT MOVE IF OPPOSING SYSTEM IS ENGAGED. REMOVED AND REPLACED MODE CONTROL PANEL IAW AMM 22-11-34 AND PERFORMED SATISFACTORY FUNCTIONAL CHECK.SDR PIDA06084Pitot Tube · obstructedRTO 90 KTS 86000 LBS, NO CAPTAIN'S AIRSPEED, NO STANDBY AIRSPEED, FIRST OFFICER AIRSPEED NORMAL. REMOVED OBSTRUCTION FROM CAPTAINS PITOT TUBE. OPS CHECK NORMAL IAW MM 34-11-0.SDR PIDA06043Sensor · out of adjustAUTO PILOT BUMPS CONTROL COLUMN UPON SELECTION OF EITHER A OR B CHANNEL. ADJUSTED ELEVATOR POSITION SENSOR PER MM 22-11-0. OPS NORMAL.SDR PIDA06037Coupler · inoperativeMACH TRIM IS INOP. REPLACED MACH TRIM COUPLER AND OPS CHECKED PER MM 22-21-0.SDR PIDA06035Transmitter · malfunctionedAUTO THROTTLE SYSTEM IS INOP. DISCONNECTED IN FLIGHT, WOULD NOT RESET. PLACED ON MEL 22-7. REPLACED NR 1 ENGINE LVDT, THRUST LEVER TRANSMITTER, RIGGED AND OPS CHECKED PER MM 22-31-81.SDR PIDA06032Computer · malfunctionedAIRCRAFT WILL NOT DESCEND IN AUTO-PILOT USING VERTICAL SPEED; REVERTS TO LEVEL CHANGE MODE. FOUND FCC B-SYSTEM AT FAULT. PLACED ON MEL 22-1. 03/20/2006: REPLACED FCC -B- AND PERFORMED SATISFACTORY OPS CHECK PER MM 22-11-331.SDR PIDA06022Computer · faultyFIRST OFFICER'S FLIGHT DIRECTOR INOP. REPLACED AFCS COMPUTER NR 2. OPS NORMAL PER MM 22-11-331.SDR PIDA20050199Control Panel · inoperativeFIRST OFFICER'S COURSE WINDOW MIDDLE DIGIT SKIPS PAST THE NR 1 ON THE MODE CONTROL PANEL. REPLACED MODE CONTROL PANEL AND OPS NORMAL IAW MM 22-11-341.SDR PIDA20050190Door Frame · crackedCRACK BEHIND R1 DOOR FRAME UPPER FORWARD STOP FITTING. REPLACED FRAME WEB PER DWG 65-45807.SDR PIDA20050178Actuator · leakingHYDRAULIC FLUID ON LINES AT AUTO PILOT ACTUATOR -B- IN LEFT WHEEL WELL. REPLACED -B- SYSTEM AUTO PILOT ACTUATOR PER MM 22-11-251.SDR PIDA20050176Floorbeam · corrodedBS 986 FLOORBEAM HAS CORROSION AT FLOORBOARD ATTACH LOCATIONS LBL 48 TO RBL 48. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-301.SDR PIDA20050166Intercostal · corrodedCORROSION AT CLIP NUT HOLES ON INTERCOSTAL AT RBL12 BETWEEN BS 344 AND BS 360. REPLACED INTERCOSTAL PER SRM 51-10-1.SDR PIDA20050165Pan · corrodedAFT LAVATORY PAN HAS CORROSION ON LOWER SURFACE FROM BS 986+8 TO BS 1016 AT LBL 38. REPLACED PAN PER DWG 65-46812 AND SRM 51-10-1.SDR PIDA20050169Floorbeam · crackedCRACK IN RADIUS OF RBL 24 FLOORBEAM AT BS 520. REPAIRED PER SB 737-53-1120.SDR PIDA20050168Floorbeam · crackedCRACK IN RADIUS OF RBL 45.50 FLOORBEAM AT BS 520. REPAIRED PER SB 737-53-1120.SDR PIDA20050167Floorbeam · crackedCRACK IN RADIUS OF LBL 45.50 FLOORBEAM AT BS 520. REPAIRED PER SB 737-53-1120.SDR PIDA20050160Intercostal · corrodedINTERCOSTAL AT BS 947 + 9 HAS CORROSION FROM LBL 18 TO LBL 42. REPLACED INTERCOSTAL SRM 51-10-1.SDR PIDA20050157Intercostal · crackedINTERCOSTAL SHIM AT BS 540 IS CRACKED AT RBL1. REPLACED INTERCOSTAL PER DWG 65-46891 AND SRM 51-10-1.SDR PIDA20050159Intercostal · corrodedINTERCOSTAL AT BS 947 + 9 HAS CORROSION FROM LBL 8 TO LBL 18. REPLACED INTERCOSTAL PER DWG 65C10592.SDR PIDA20050161Intercostal · crackedINTERCOSTAL BEHIND THE UPPER AFT STOP FITTING ON THE AFT SIDE OF THE R1 DOOR FRAME IS CRACKED UNDER THE RIVET HEADS. REPLACED INTERCOSTAL PER 737 SB 53A1108.SDR PIDA20050158Intercostal · crackedINTERCOSTAL AT BS 540 IS CRACKED AT BL0. REPLACED INTERCOSTAL PER DWG 65-46891 AND SRM 51-10-1.SDR PIDA20050162Intercostal · crackedINTERCOSTAL AT BS 540 IS CRACKED AT THE AFT I/B EDGE AT RBL47. REPLACED INTERCOSTAL PER DWG 65-46891.SDR PIDA20050177Floorbeam · corrodedBS 967 FLOORBEAM HAS CORROSION FROM LBL 42 TO LBL 48. REPLACED DAMAGED SECTION OF FLOORBEAM PER EA 53-268.SDR PIDA20050156Floorbeam · crackedFLOORBEAM AT BS 520 IS CRACKED AT LBL24. REPAIRED FLOORBEAM PER 737 SB 53-1120.SDR PIDA20050154Support Channel · corrodedLOWER SUPPORT CHANNEL FOR AFT DRAIN MAST BETWEEN BS 986 AND BS 1006 BETWEEN STR 24 LT AND STR 25 LT HAS CORROSION. REPLACED HAT CHANNEL PER SRM 51-10-1 AND SRM 51-30-2.SDR PIDA20050151Intercostal · crackedTOP FLANGE OF INTERCOSTAL BETWEEN BS 500B AND BS 520 AT BL 0 IS CRACKED. REPLACED INTERCOSTAL PER DWG 69-41680 AND SRM 51-10-1 AND SRM 51-30-0.SDR PIDA20050148Stringer · corrodedFOUND STR 27 LT HAS CORROSION FROM BS 967 TO BS 1016. REPLACED DAMAGED SECTION OF STRINGER PER SRM 53-10-03 AND SRM 51-30-00.SDR PIDA20050149Stringer · corrodedSTR 25 LT HAS CORROSION UNDER FRAME AT BS 986. REPLACED DAMAGED SECTION OF STRINGER FROM BS 967 TO BS 1016 PER SRM 53-10-03 AND SRM 51-30-00.SDR PIDA20050152Strap · corrodedSTRAP IN AFT LAVATORY AREA HAS CORROSION FROM BS 1006 TO BS 1016+12. REPLACED STRAP PER DWG 65-46812 AND SRM 51-10-1.SDR PIDA20050153Panel · corrodedCLOSE-OUT PANEL AT BS 1016 HAS CORROSION ON UPPER SURFACE AT RBL4. REPAIRED CLOSE-OUT PANEL PER SRM 51-40-1.SDR PIDA20050155Angle · crackedANGLE FORWARD OF R1 DOOR JUST BELOW STR 12RT IS CRACKED. REPLACED CRACKED ANGLE PER DWG 65-45807 AND SRM 51-10-1.SDR PIDA20050150Frame · crackedCRACK AT I/B CHORD LOWER FASTENER HOLE IN BS 616 FRAME LEFT. REPAIRED FRAME PER SB 737-53-1182.SDR PIDA20050147Channel · crackedCRACK IN VHF ANTENNA MOUNT BRACKET AND HAT CHANNEL AT BS 506 AND BL 0. REPLACED MOUNT BRACKET AND HAT CHANNEL PER DWG 65-45783 AND SRM 51-10-1.SDR PIDA20050146Attach Angle · crackedCRACK IN THE WEB AND ATTACH ANGLE JUST FORWARD OF THE R1 DOOR AT BS 294 ABOVE STR 12RT. REPLACED WEB AND ANGLE PER DWG 65-45807 AND SRM 51-10-1.SDR PIDA20050145Stringer · corrodedSTR 26 RT HAS CORROSION FROM BS 1006 TO BS 1016. REPLACED STRINGER SECTION PER SRM 51-10-1.SDR PIDA20050144Frame · crackedRIGHT FORWARD DOOR FRAME (FUSELAGE FRAME) CRACKED AT FLOOR LEVEL BEHIND THE ZEE ANGLE. REPAIRED DAMAGE PER SRM 51-40-3 AND SRM 51-10-1.SDR PIDA20050143Angle · crackedATTACH ANGLE FOR THE RIGHT FORWARD ZEE ANGLE JUST FORWARD OF THE R1 DOOR CUTOUT IS CRACKED. REPLACED ANGLE PER SRM 51-10-1.
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