Pratt & Whitney JT8D-17
Service difficulty reports · 1,680
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'JT8D17' 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 engine_model_key = 'JT8D17' 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 0201159880Wire · damagedDURING TAKEOFF ROLL AT 116 KNOTS, THE RIGHT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPAIRED DAMAGED WIRES AND REPLACED THE CANNON PLUG FOR THE RIGHT ENGINE THRUST REVERSER LATCH SWITCH. ENSDR CA020502018Window · failed(CAN) ON GROUND FOUND FIRST OFFICER NR 4 WINDOW SHATTERED. RELACED NR 4 WINDOW.SDR CA020426004Latch · failed(CAN) CABIN OXYGEN PSUS NR 9 RT AND NR 14 RT, NO FLOW FOUND DURING FUNCTIONAL TEST. BOTH UNITS ARE FROM THE SAME BATCH NR. BATCH NR 99795 REPLACED LATCH ASEMBLIES.SDR CA020402005Controller · failed(CAN) FLT 146 AFTER DEPARTURE, CABIN ALTITUDE WARNING HORN SOUNDED. CREW EXECUTED CABIN ALTITUDE WARNING / RADID DEPRESSURIZATION CHECKLIST & CABIN PRESSURE STABILIZED AT 12,000 FT. AIRCRAFT DESCENDED TO 26,000 FT, FLT ATTENDENTS DONNED PORTABLE OXYGEN MASKS SDR COOSDR02054Skin · debondedLEFT WING, OUTBOARD AFT FLAP DEBONDED.SDR COOSDR02055Skin · delaminatedRIGHT WING, INBOARD FORE FLAP UPPER AND LOWER SKIN DELAMINATION.SDR CA020405001Structure · cracked(CAN) SCHEDULED MAINTENANCE;DURING REGULAR SCHEDULED MAINITENANCE INSPECTION, MAINTENANCE ENGINEER SUSPECTED A CRACK AT THE NOSE LANDING GEAR ACTUATOR ATTACH SUPPORT BRACKET (FORWARD SIDE UPPER R/H SIDE). NDT CALLED IN AND 3/8 INCH CRACK CONFIRMED BY HFEC METHSDR AUS20020395Shim · corroded(AUS) LT ELEVATOR COUNTER WEIGHT SHIM PLATE FITTING HEAVILY CORRODEDZONE 93 STA ELE 210 TO STA ELE 222. CPCP - LEVEL 2 CORROSION.SDR CA030411001Connector · shorted(CAN) AILERION, SPOILER SHUT OFF VALVE, WHEEL WELL FIRE DETECTION AND PACK COOLING FAN CIRCUIT BREAKERS TRIPPED AFTER LANDING. FOUND CONNECTOR RECEPTACLE D4658J AT BS 870 (LEFT OF KEELBEAM IN AIR CONDITIONING BAY) SHORTED. REPLACED CONNECTOR IAW STANDARD PRACTSDR AUS20020391Fitting · corroded(AUS) HORIZONTAL STABLISER BEARING ATTACHMENT FITTINGS CORRODED. CPCP - LEVEL 2 CORROSION.SDR AUS20020405Fitting · corroded(AUS) VERTICAL STABILISER BEARING ATTACHMENT FITTINGS CORRODED. CPCP -LEVEL 2 CORROSION.SDR AUS20020392Spar · corroded(AUS) HORIZONTAL STABILISER CENTRAL UPPER REAR SPAR AREA CORRODED ZONE97 STN BS1586.81. CPCP - LEVEL 2 CORROSION.SDR AUS20020390Bracket · corroded(AUS) LT WING BRACKET ATTACHED TO LOWER CHORD DELAMINATED FROM CORROSION ZONE 72, STN WS204.0. CPCP - LEVEL 2 CORROSION.SDR AUS20020396Sill · corroded(AUS) LT REAR ENTRY AND SERVICE DOOR AFT LOWER DOOR SILL CORRODED AT INNER PART OF SCUFF PLATE ZONE 24 STA 1035 TO STN 1065. CPCP -LEVEL 2 CORROSION.SDR AUS20020397Sill · corroded(AUS) RT AFT SERVICE DOOR SILL CHORD CORRODED AT INNER EDGE ATTACHMENT POINT. LEVEL 2 CORROSION.SDR AUS20020399Door Frame · corroded(AUS) CORROSION FOUND IN EMERGENCY DOOR EXIT (AFT OVERWING) AREA AT LOWER RH CORNER OF WEB ON HATCH ASSEMBLY FRAME ZONE 49 STN 825.95 TO STN 848.95. CPCP - LEVEL 2 CORROSION.SDR CA020319004Duct · missing(CAN) SHORTLY AFTER DEPARTING, FLIGHT CREW RECEIVED A NR 1 ENGINE OVERHEAT INDICATION AND IMMEDIATELY RETURNED TO BASE - AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED THE CLAMP FOR THE 8TH STAGE ANTI ICE VALVE WAS MISSING AND THE BLEED DUCTSDR AUS20020393Skin · corroded(AUS) RT STABILISER SKIN CORRODED AT ATTACHMENT POINT TO REAR UPPER AUXILIARY SPAR CHORD ZONE 92, ELE 118.0 TO ELE 120.0. CPCP -LEVEL 2 CORROSION.SDR AUS20020394Shim · corroded(AUS) RT STABILISER ELEVATOR SHIM PLATE FITTINGS CORRODED AT COUNTERWEIGHT ATTACHMENT POINT. CPCP - LEVEL 2 CORROSION.SDR AUS20020398Seat Track · corroded(AUS) SEAT TRACK CORRODED AT ZONE 24 STA 1130 TO STA 1110 LBL 2475 LT.CPCP - LEVEL 2 CORROSION.SDR SQ7A172002Fan Blade · crackedIND - DURING SCHEDULED MAINTENANCE CRACKS WERE FOUND IN THE C-1 FAN BLADES NR 13 & NR 16. REMOVED AND REPLACED THE C-1 FAN ASSY.SDR COOSDR02017Fitting · corrodedFITTING, RIGHT WING, INBOARD MID-FLAP, OUTBOARD FITTING FLAP CARRIAGE WITH CORROSION.SDR 2002F00801Smoke · detectedAFTER LANDING AT GRR, THE CABIN FILLED WITH SMOKE AFTER ALL THREE ENGINES WERE IN REVERSE THRUST. NO EMERGENCY WAS DECLARED. SMOKE CLEARED AFTER ENGINES WERE SHUT DOWN. (M)SDR COOSDR02014Fitting · corrodedFITTING, LEFT WING, INBOARD MID-FLAP INBOARD FITTING FLAP CARRIAGE WITH CORROSION.SDR COOSDR02015Fitting · corrodedRIGHT WING, OUTBOARD MID-FLAP, INBOARD/OUTBOARD FITTINGS FLAP CARRIAGE WITH CORROSION.SDR COOSDR02019Clip · crackedFRAME STA 480 STR 7 LT 8 LT, CLIP CRACKED DUE TO INADEQUATE STRINGER RIVETING.SDR COOSDR02021Clip · crackedFRAME STA 480 STR 3 LT CLIP CRACKED DUE TO INADEQUATE STRINGER RIVETING.SDR COOSDR02022Skin · crackedSKIN LAP SPLICE-LOWER SKIN. LOWER FASTENER ROW WITH CRACK INDICATION AT S-4L, BS 446.750.SDR COOSDR02025Fitting · corrodedRT WING, TRAINLING EDGE AT WS383.5, FITTING CORRODED.SDR COOSDR020026Shear Tie · corrodedLOWER FUSELAGE, STA 1050 BETWEEN STR 26L AND STR 27L SHEAR TIE CORRODED.SDR COOSDR020027Support · corrodedFWD C/C, STA 623, BETWEEN STR 25L AND STR 26L AND STA 560 BETWEEN STR 25R AND STR 26R NET TUBE SUPPORT.SDR COOSDR020028Structure · corrodedFORWARD C/C, STA 620, BETWEEN STR 23R AND STR 24R SUPPORT TEE CORRODED.SDR COOSDR02029Skin · crackedFUSELAGE SKIN LAP SPLICE-LOWER SKIN, LOWER FASTENER ROW WITH CRACK INDICATION AT S-4L, BS 390.0.SDR COOSDR02030Skin · crackedSKIN LAP SPLICE-LOWER SKIN, LOWER FASTENER ROW WITH CRACK INDICATION AT S-4L, BS 412.0.SDR CA020306003Acm · failed(CAN) FLIGHT 183 AIRCRAFT ON FLIGHT TO YWG FROM YHM AND AT CRUISING ALTITUDE, THE FORWARD LAV SMOKE DETECTOR ACTIVATED. THE FLIGHT ATTENDENTS ADVISED THE CAPTAIN OF SMOKE IN THE CABIN AND THE REAR SMOKE DETECTOR GOING OFF. FLIGHT CREW REQUESTED PRIORITY LANDINSDR CA020227010Latch · failed(CAN) DURING GEAR RETRACTION LEVER LATCH FAILED TO RELEASE ALL OTHER INDICATIONS NORMAL.REPAIRED WIRING AT LEVER LOCK SOLENOID BY REPLACING TERMINAL CONNECTOR LEVER LOCK SYSTEMM OPS TESTED AS PER MM 32-31-11. NO FURTHER DISCREPANCY.SDR C1HA200296010Compressor · stalledAFTER STARTING TO APPLY T/O POWER WITH A CROSSWIND NR 2 ENGINE COMPRESSOR STALLED. INSPECTED NR 2 ENG INLET AND EXHAUST FOUND NO DAMAGE AS PER MM 71-00, OK FOR CONTINUED SERVICE.SDR CA020228001Adc · failed(CAN) JUST AFTER TAKEOFF CAPTAINS AIRSPEED, STANDBY AIRSPEED, GROUND PROX WARNING, AND MACH TRIM INDICATORS FAILED. AIRCRAFT RETURNED TO AIRPORT. NR 1 CENTRAL AIR DATA COMPUTER REPLACED AND OPERATION CHECKED SERVICEABLE.SDR C1HA200297005GearboxAt 33,000 feet with cruise power set, engine #2 oil temp rose from 110 to 120 C, 2 seconds later oil quantity dropped from 4 gallons to .2 gallons. Oil pressure dropped from 50 PSI to 42 PSI. We brought the engine to idle, engine gauges stabilized at .2 gallSDR CA020205007Hinge Pin · corroded(CAN) DURING INSPECTION OF HORIZONTAL STABILIZER HINGE PINS, FOUND THE RT SIDE OUTER PIN THREADS AND THREAD RELIEF AREA CORRODED. THE OUTER AND INNER PINS WILL BE REPLACED PRIOR TO NEXT FLIGHT.SDR CA020204002Bullet · separated(CAN) FLT CREW RPTED DURING CLIMB AFTER TAKEOFF THEY EXPERIENCED SERIES OF LOUD BANGS FROM NR 2 ENGINE ACCOMPANIED BY ABNORMAL HIGH EGT & LOW N 2 RPM. ALL IND.S WERE NORMAL PRIOR TO NOICE. PROBLEM OCCURRED AFTER CLIMB THRUST SET. THE CREW REDUCED NR 2 THRUST SDR CA020215007Arm · dislodged(CAN) MAINTENANCE FOUND NR 2 SLAT FOUND PROTRUDING 4 INCHES ON ONE SIDE ON WALKAROUND CHECK. SLAT MECHANISM FOUND OFF GUIDE TRACK. FLIGHT PERMIT (SPECIFIC PURPOSE, FERRY FLIGHT) ISSUED AND AIRCRAFT FLOWN TO BASE FOR REPAIRS. NR 2 LEADING EDGE SLAT DETENT ARM SDR CA020205006Tie Bolt · sheared(CAN) DURING AIRCRAFT WALK AROUND INSPECTION, FOUND NR 3 MAIN WHEEL ASSEMBLY WITH TWO SHEARED TIE BOLTS. NR 3 MAIN WHEEL ASSEMBLY REPLACED PER MAINTENANCE MANUAL 32-45-1. MAIN WHEEL ASSEMBLY TO BE SENT TO OVERHAUL FACILITY FOR INVESTIGATION AND TEAR DOWN REPOSDR AUS20020336Bulkhead · corroded(AUS) FUSELAGE BULKHEAD LOCATED AT BS 950 CONTAINED LEVEL 2 CORROSION IN LOWER CHORD.SDR AUS20020337Keelbeam · corroded(AUS) KEELBEAM EXTENSION CONTAINED LEVEL 2 CORROSION IN THE AREA LOCATED BETWEEN STN BS 950.12 AND BS 957.12 BL6L.SDR C1HA200296001Engine · malfunctionedON RUNWAY ADVANCED THROTTLE TO 1.4 CHECK PARAMETERS GOOD, CONTINUED THROTTLE ADVANCE FORFLEX POWER, LOUD BANG FROM NR 2 ENGINE, ENGINE FAIL LIGHT ILLUMINATED AND PACKS TRIPPED. ACCOMPLISHED THOROUGH EXAMINATION OF ENGINE NR 2 INTAKE AND EXHAUST WITH NO DAMAGESDR C1HA200296002Bleed Valve · malfunctionedPOWER UP FOR TAKEOFF NR 2 ENGINE COMPRESSOR STALLED POWER WAS AT 1.6 EPR AND SPEED WAS BELOW 40 KTS. NR 2 PRBC WAS CHANGED AND OPS CHECK GOOD AND NR 2 GENERATOR PUT ON MEL. NR 2 COMP BLEED SYS OPS NORMAL REF: 75-31.SDR CA020103007Engine · failed(CAN) NR 3 ENGINE SHUT DOWN IN FLIGHT DUE VIBRATION. REPAIR FACILITY EVALUATION: EXTENSIVE IMPACT DAMAGE WAS NOTED ON THE 7-12 STAGE STATOR VANES AND THE 7-13 STAGE BLADES. THIS DAMAGE APPEARS TO HAVE ORIGINATED FROM A FRACTURED 7 STAGE COMPRESSOR BLADE. THSDR CA020110002Transmitter · failed(CAN) ENGINE NR 1 OIL PRESSURE DROPPED TO 20 PSI AFTER TAKEOFF. ENGINE FAILURE AND SHUT DOWN COMPLETED. AIRCRAFT RETURNED TO VANCOUVER. OIL PRESSURE TRANSMITTER REPLACED.SDR CA020104010Gasper Fan · seized(CAN) AIRCRAFT ENROUTE FROM SAN FRANSISCO TO VANCOUVER, DIVERTED TO KLAMATH FALLS OREGON, DUE SMOKE IN THE CABIN. SMOKE DISIPATED WHEN GASPER FAN SELECTED OFF. GASPER FAN FOUND SEIZED. GASPER FAN REPLACED.
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