N501TR, cancelled Dec 4, 2018
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 = 'N501TR' AND deregistration_id = 'N501TR-2018-12-04' 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 = 'N501TR' AND deregistration_id = 'N501TR-2018-12-04' 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 WRNA2009001Ground Wire · looseAFTER TAKEOFF, KRUEGER FLAP FAILED TO RETRACT. CREW REPORTED A "CONFIG" LIGHT ON MWP. ALSO, FLIGHT CHARACTERISTICS OF AIRCRAFT SEEMED DIFFERENT. DECISION MADE TO RETURN TO AIRFIELD. AIRCRAFT LANDED NORMAL, NO FUEL WAS DUMPED. MAINTENANCE UPON TROUBLESHOOTSDR WRN2008F00003Indicator · unserviceableDURING CRUISE, ENG NR1 EGT OFF SCALE HIGH INDICATION. POINTER AT 6 O`CLOCK POSITION. POINTER AND DIGITAL READOUT AGREED. AMBER EGT LIGHT ON, ENGINE EGT LIGHT ON MWP, AND SSC. AC RETURNED TO FIELD, ABNORMAL PROCEDURES WERE PERFORMED AND APPROX. 8500 LBS OF FUELSDR WRN2008F00000Gearbox · contaminatedON CLIMBOUT STJ FL230, OIL QTY DECREASING RAPIDLY. PERFORMED PRECAUTIONARY SHUTDOWN PROCEDURES, OIL PRESSURE WAS NOT LOST, OIL TEMP RISE TO 130 DEGREES. REPLACED GEARBOX IAW MM 72-60-01. OPS CHECK GOOD ON NR 2 ENGINE. (K)SDR WRNA200800014Skin · corrodedDURING M96 CHECK, FOUND OUT OF LIMIT CORROSION ON FUSELAGE AT STR 6 TO FRAME 76. CUT OUT DAMAGED AREA 2.75 INCHES BY .75 INCHES AND INSTALLED FILLER FABRICATED FROM 2024 T3 0.090 AND REPAIR DOUBLER FABRICATED FROM 2024 T3 0.100 IAW A300 SRM 53-10-10.SDR WRNA200800022Seat Track · crackedDURING M96 CHECK, MAIN CABIN SEAT TRACK AT FRAME 40 RBL 54 WAS FOUND CRACKED. REPLACED SEAT TRACK AT RBL 54 FROM FRAME 40 TO FRAME 44 +12 INCHES IAW SRM 53-10-10.SDR WRNA200800020Track · corrodedDURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAME 57. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30.SDR WRNA200800019Track · corrodedDURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD Z:-150-L403-5-01, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT BETWEEN FRAMES 58 TO 59. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30.SDR WRNA200800021Track · corrodedDURING M96 CHECK WHILE ACCOMPLISHING CPCP TASK CARD ZL-150-L403-501, CORROSION WAS FOUND ON LT INBOARD ROLLER TRACK IN AFT CARGO COMPARTMENT AT FRAMES 54 TO 57. REMOVED AND REPLACED ROLLER TRACK IAW SRM 51-30-30.SDR WRNA200800018Skin · corrodedDURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD 55-2007-0602-1-01 SEVERAL AREAS OF CORROSION WERE FOUND OUT OF LIMITS ON LT ELEVATOR SKIN FROM CENTER LINE RIVETS TO I/B END CAP. REPLACED ELEVATOR IAW A300 MM 27-31-24.SDR WRNA200800017Seat Track · corrodedDURING M96 CHECK, WHEN ACCOMPLISHING CPCP TASK CARD ZL-220-L403-9-01, CABIN SEAT TRACK WAS FOUND CORRODED AT FRAME 13B - 14C LBL 55. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN FRAME 13B - 14C LBL 55 IAW A300 SRM 51-30-30 WITH SEAT TRACK FABRICATED FROM ESDR WRNA200800016Skin · damagedDURING M96 CHECK, A 8 INCH BY 2 INCH CUT WAS FOUND IN SKIN BETWEEN FRAME 51 AND 52 AT STRINGER 36R TO 39R AFT OF RMLG DOOR CUT OUT. INSTALLED SKIN REPAIR DOUBLER AT FUSELAGE FRAME 51 TO 52 AND STRINGER 36R TO 39R IAW A300 SRM 53-10-10.SDR WRNA200800023Attach Fitting · corrodedDURING M96 CHECK, CORROSION WAS FOUND OUT OF LIMITS ON NR 3 (FROM OUTBOARD END) LEFT ELEVATOR ATTACH HINGE AT BONDING WIRE ATTACH POINT. REPLACED HINGE ATTACH IAW A300 M/M 55-51-31.SDR WRNA200800003Damper · failedAFTER TAKEOFF FROM IND, GEAR FAILED TO RETRACT ON BOTH SYSTEM A AND B, DIVERTED TO GSO, DUMPED APPROX 15,000 POUNDS OF FUEL AND MADE A SAFE LANDING. FOUND LEFT INBOARD PITCH DAMPER AT FAULT, REPLACED INBOARD PITCH DAMPER IAW A300 MM 32-11-15 PG 410, LEAK CHECSDR WRNA200700041Skin · damagedDURING WALKAROUND, FOUND FUSELAGE SKIN DAMAGED AT C-1 DOOR FRAME, RIGHT SIDE AT FRAME 24B STA 1701. INSTALLED DOUBLER REPAIR ON C-1 DOOR FRAME 24B STA 1701 IAW A300 SRM 53-13-00.SDR WRNA200700025Rudder · delaminatedDURING WALK AROUND POSSIBLE DELAMINATION NOTED ON TRAILING EDGE OF RUDDER. RUDDER REMOVED, REPAIRED IAW SRM 55-41-11 PG148-149, SRM 51-21-00 PG 15, 21, 22 SRM 51-40-00 PG 731-733 FIG 709, SRM 55-41-11 PG 148, 149 SRM 51-42-20 AND PCS PROCESS PROCEDURES PCS-PSSDR 200700025Rudder · delaminatedDURING WALK AROUND POSSIBLE DELAMINATION NOTED ON TRAILING EDGE OF RUDDER. RUDDER REMOVED, REPAIRED IAW SRM 55-41-11 PG148-149, SRM 51-21-00 PG 15, 21, 22 SRM 51-40-00 PG 731-733 FIG 709, SRM 55-41-11 PG 148, 149 SRM 51-42-20 AND PCS PROCESS PROCEDURES PCS-PSDR WRNA200700013Switch · malfunctionedAFTER TAKEOFF FROM GSO, GOT NOSE LANDING GEAR DOOR UNSAFE INDICATION, WHEN GEAR HANDLE WAS PLACED IN NEUTRAL POSITION ALL GEARS EXTENDED. RETURNED TO GSO AND MADE A SAFE LANDING. PERFORMED NORMAL SYSTEM LANDING GEAR RETRACTION IAW A300 MM 32-30-00 PAGE 501, SDR WRNA200700012Landing Gear · malfunctionedAFTER TAKEOFF FROM IND, NOSE LANDING GEAR FAILED TO RETRACT, PERFORMED ABNORMAL CHECK LIST AND DIVERTED TO GSO AND MADE A SAFE LANDING. PERFORMED NORMAL EXTENSION AND RETRACTION OF SYSTEM 1 AND 2, NO DEFECTS NOTED, AIRCRAFT RELEASED TO SERVICE.SDR WRNA200600029Connector · damagedON TAKEOFF ROLL, ENGINE NR 1 LOOP-B ON MWP AND FLIGHT ENGINEERS PANEL ILLUMINATED. ABORTED TAKEOFF, PERFORMED CHECKLIST AND RETURNED TO GATE. INSPECTED ENGINE AND FIRE LOOP, CHECKED GOOD. PLACED ON MEL 26-12-01 CAT-B, RELEASED AIRCRAFT TO SERVICE. REPAIREDSDR WRNA20060030Spar · corrodedDURING M72 CHECK, FOUND CORROSION ON RUDDER SPAR BOX ANGLE AT RIBS RR20 AND RR38. REMOVED CORROSION AND INSTALLED DOUBLERS PER EMTEQ REPAIR ORDER 2-41054-801SDR WRNA200600033Fitting · corrodedDURING M72 CHECK, FOUND CORROSION ON EMPENNAGE FORWARD RIGHT FITTING ATTACHED TO VERTICAL STABILIZER. CLEANED, PRIMED AND APPLIED TOP COAT PER A300 SRM 51-40-12 AND REPLACED EMPENNAGE FORWARD RIGHT LONGITUDINAL BRACE FITTING PER A300 DRAWING 19R53870348 SHEETSDR WRNA200600032Support · corrodedDURING M72 CHECK, FOUND CORROSION AND LOOSE FASTENERS ON HORIZONTAL SUPPORT OF VERTICAL STABILIZER TRAILING EDGE STRUCTURE ABOVE RUDDER FITTING NR 1. FABRICATED FITTING FROM EXTRUSION BAC1505100797 PER A300 ACCORDING SRM 51-41-00, TREATED, PRIMED AND APPLIED SDR WRNA200600004Jackscrew · lockedON TAXI OUT, SELECTED SLATS TO 0/16, SLATS FAILED TO EXTEND. RETURNED TO BLOCK. FOUND LT NR 3 JACKSCREW LOCKED OUT. FREED JACKSCREW IAW 27-81-00 PG 511, FUNCTIONAL CHECK ACCOMPLISHED IAW 27-81-00 PG 501. AIRCRAFT RETURNED TO SERVICE.SDR WRNA200600003Indicator · unserviceableDURING START OF TAKEOFF ROLL, PILOTS LANDING GEAR LIGHT INDICATOR RT MAIN UNLOCK LIGHT CAME ON. F/E PANEL OK. ABORTED TAKEOFF, MAX BRAKE TEMP IND 400. RETURNED TO GATE. ITEM DMI"D PER 32-31-01 CAT B EXPIRES 2-12-06 OK TO CONTINUE SERVICE. REMOVED AND REPLASDR WRNA200500006Engine · unserviceableDURING CLIMBOUT NR 2 ENGINE EXCEEDED EGT LIMITS. WHEN LIMITS WERE IN NORM OPERATING RANGE NO RESPONSE WAS SEEN WHEN THROTTLES WERE ADVANCED. FUEL DUMP PROCEDURES FOLLOWED, AIRCRAFT RETURNED TO AIRPORT, LANDING NORMAL. REMOVED AND REPLACED NR 2 ENGINE IAW A3SDR WRNA200500004Valve · malfunctionedUPON PERFORMING EMERGENCY PROCEDURES FOR A LOW SPEED AILERON FAULT, WHEN STARTING TO DUMP FUEL FOR A RETURN TO BASE LANDING, RT FUEL JETTISON VALVE MI CROSSHATCHED DURING FUEL JETTISON. DEFERRED JETTISON RT VALVE MI IAW MEL 28-31-01 CAT "C" EXPIRES 3-15-05. SDR WRNA200500003Actuator · unserviceableLT LOW SPEED AILERON FAILED TO DISCONNECT UPON SLAT RETRACTION. FUEL DUMP PROCEDURES FOLLOWED, AIRCRAFT RETURNED TO AIR FIELD, LANDING NORMAL. MANUALLY DISCONNECT LOW SPEED AILERON. LOCK OUT ACTUATOR I/A/W 27-00-00, VERIFIED ROD IS RETRACTED AND IN DISCONNECSDR WRNA200400012Dump Valve · failedWHEN ATTEMPTING TO DUMP FUEL, RT DUMP VALVE WOULD NOT OPEN WITH PRIMARY OR SECONDARY SELECTED. CLEANED C/P AT RT FUEL JETTISON VALVE ACTUATOR. SECONDARY SYS CHECK'S OK IAW 28-31-00. PRIMARY DEFERRED IAW MEL 28-31-02 CAT-C.SDR WRNA200400011Actuator · unserviceableAFTER TAKE OFF AC REQUIRED A LOT OF AILERON TO KEEP LEVEL, 35 DEGREES. RETURNED TO AIRFIELD, WHEN ATTEMPTING TO DUMP FUEL, RT DUMP VALVE WOULD NOT OPEN WITH PRIMARY OR SECONDARY. OVERWEIGHT LANDING ACCOMPLISHED. LANDING NORMAL. FOUND NR 3 LT SPOILER SERVO BSDR WRNA200400010Nut · looseCOMPLETE LOSS OF GREEN SYSTEM HYD QUANTITY. PERFORMED ABNORMAL CHECKLIST. RETURNED TO AIRPORT, PERFORMED MANUAL GEAR EXTENSION. LANDING NORMAL. MAINTENANCE FOUND JAMNUT LOOSE ON GREEN PRESSURE MANIFOLD. TORQUED NUT AND LEAK CHECK GOOD I/A/W A300 MM 20-21-SDR WRNA200300013Clamp · looseNR 1 ENG NACELLE TEMP READ 300+ ON CLIMB OUT. TEMP. REACTED TO THROTTLE MOVEMENT. DUMPED APPROX. 30K LBS. RETURNED TO FIELD, LANDING NORMAL. MAINTENANCE FOUND IP CHECK VALVE CLAMP OFF DUCT. REINSTALLED CLAMP IAW PROCESS MATERIAL SPEC. MANUAL 01-05-42. ENGINE SDR WRNA200300006Landing Light · underservicedL/H taxi/take off circuit breaker on pnl #9 trips Corrective Action: Originally MEL assigned MEL 33-46-01 3-7-03 to be cleared by 3-17-03. Closing action: R&R'd L/H taxi light assy, ops check good I/A/W 33-46-12, MEL cleared. Closing date 3-10-03.SDR WRNA200200003Stall Warning · activatedIN CLIMBOUT, CLEAN CONFIGURATION ABOVE 250 KTS VIOLENT SHUDDER WITH STALL WARNING AND STICK SHAKER. A/C WT 335 ALT FL 200, ENGINE PARAMETERS AND FLT CONTROL INDICATION NORMAL. SYS PARAMETERS NORMAL. AIRCRAFT RETURNED TO AIRPORT. PERFORM OP'S CK OF AOA SENSSDR WRNA200100017Stringer · corrodedDURING WALK AROUND FOUND CORROSION ON FUSELAGE AT BULK CARGO DOOR AREA. LOCATED AFT, L/H LOWER CORNER. STA. 365 STRINGER 47RCORRECTIVE ACTION: REPAIR CARRIED OUT I/A/W SRM 53-10-20 FIG. 701 SHEET 3 LAP JOINT REPAIR
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