Pratt & Whitney JT8D-7A
Service difficulty reports · 262
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 = 'JT8D7A' 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 = 'JT8D7A' 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 CA971015037Rod End Bearing · loose(CAN) NOSE LANDING GEAR LOCK ACTUATOR ROD END BEARING LOOSE. ACTUATOR REPLACED.SDR CA971015038Valve · leaking(CAN) LEFT HAND WING TAI VALVE LEAKING ALLOWING HOT AIR TO BYPASS WHEN CLOSED.SDR CA971015032Selector Valve · leaking(CAN) DURING A "C" CHECK INSPECTION THE THRUST REVERSER SELECTOR VALVE OF NR1 ENGINE WAS FOUND TO HAVE A LEAKING SHAFT SEAL, THE SELECTOR WAS REMOVED AND A SERVICEABLE UNIT INSTALLED AND THE SYSTEM RETURNED TO SERVICE.SDR CA971015033Lock · leaking(CAN) AIRSTAIR LOCK ACTUATOR LEAKING. REPLACED.SDR CA971015034Seal · leaking(CAN) LEADING EDGE DEVICE SELECTOR VALVE LEAKING BEYOND LIMITS. REPLACED.SDR CA971015035Flange · cracked(CAN) BLEED AIR DUCT CRACKED AT FLANGE. REPLACED.SDR CA971015036Duct · cracked(CAN) BLEED AIR DUCT CRACKED AT FLANGE. REPLACED.SDR CA971015031Start Valve · hole(CAN) NR2 ENGINE START VALVE HAS HOLE IN BODY. REPLACED.SDR CA971015028Lockout · torn boot(CAN) DUST BOOT ON RIGHT HAND AILERON LOCKOUT MECHANISM TORN, REPLACED.SDR CA971015029Seal · leaking(CAN) AIRSTAIR ACTUATOR LEAKING. REPLACED.SDR CA971015030Seat · leaking(CAN) LEFT HAND OUTFLOW VALVE SEAT LEAKING. REPLACEDSDR CA971015026Transmitter · intermittent(CAN) DURING APPROACH 'A' SYSTEM HYDRAULIC QUANTITY WOULD FLUCTUATE IN TURBULENCE, QUANTITY TRANSMITTER REPLACED.SDR CA971016008Vertical Gyro · inoperative(CAN) ON TAKEOFF, CAPTAIN'S ATTITUDE INDICATOR GYRO AND COMPUTER FLAG CAME UP. DURING ABORT, FLAG WENT AWAY. DURING TAXIING FLAGS DISPLAY WAS INTERMITTENT. THE VERTICAL GYRO WAS REPLACED AND OPERATIONAL CHECK CARRIED OUT SERVICEABLE.SDR CA971015027Cvr Tape · broken(CAN) COCKPIT CVR FAILED TEST FUNCTION, CONTINUOUS TAPE REPLACED SERVICEABLE.SDR CA971016007Valve · failed(CAN) DURING APPROACH, CREW UNABLE TO DEPLOY LEADING EDGE SLATS. CYCLED SEVERAL TIMES. SLATS EXTEDNDED AT 25 DEGREES FLAP. MAINTENANCE ACTION INVOLVED REPLACING SLAT CONTROL VALVE. LEAK CHECK AND OPERATIONAL CHECK CARRIED OUT.SDR CA971016009Oxygen Regulator · failed(CAN) DURING NON PRESSURIZED FLIGHT WHILE AT 10,000 FEET THE PASSENGER CABIN OXYGEN MASKS DEPLOYED. MAINTENANCE ACTION FOUND OXYGEN REGULATOR HAD FAILED. OXYGEN REGULATOR REPLACED AND LEAK CHECK CARRIED OUT. TEST CHECKED SERVICEABLE AND OXYGEN MASKS RESTOWED.SDR CA971016010Ext Light Wiring · shorted(CAN) AFTER SELECTING EXTERIOR LIGHTS FOR TAKEOFF, ELECTRICAL SPARKING OCCURRED UNDER GLARE SHIELD. MAINTENANCE ACTION FOUND ELECTRICAL WIRE L329A20 SHORTED NEAR S1-9. WIRE REPAIRED. NOSE GEAR LIGHTS RH AND LH CHECKED SERVICEABLE.SDR CA970922022Receptacle · failed(CAN) DURING DEPARTURE, BURNING SMELL DETECTED IN GALLEY. THE SOURCE WAS THE GALLEY OVEN AT POSITION 16. MAINTENANCE ACTION INVOLVED CHANGING RECEPTACLE AS PER 25-32-00.SDR CA970904024Web · corrosion(CAN) CORROSION ON WEB WL 169 BS 312RLAVATORY CHEMICAL LEAK. REPAIRED.SDR CA970904025Skin · corroded(CAN) SKIN FORWARD OF FORWARD LAVATORY SERVICE PANEL HAS BULGE AT THE FASTENERS. CORROSION ON THE LOWER SKIN OF THE LAP JOINT. SKINSDR CA970812017Press Controller · inoperative(CAN) AIRCRAFT FAILED TO PRESSURIZE ON TAKEOFF AND HAD TO MOVE SWITCH MANUALLY. THEN THE TRANSFER AND LOCKOUT AND STANDBY LIGHT CAME ON. NO AUTO TRANSFER. FULL RANGE PITOT/STATIC CHECK COMPLETED. CHANGED NR1 CABIN PRESSURE CONTROLLER. SYSTEM CHECKED SERVICEABLSDR CA970812016Refrigerator · odor(CAN) DURING PUSH BACK, BURNING SMELL DETECTED COMING FROM GALLEY FRIDGE COMPRESSOR. GALLEY FRIDGE DEACTIVATED AS PER ENGINEERING INSTRUCTION 7-25-30/07-004552-03.SDR CA970807053Cable · frayed(CAN) DURING WALK AROUND INSPECTION, LEFT HAND FUEL FIRE SHUTOFF CABLE FOUND FRAYED. FUEL FIRE SHUTOFF CABLE REPLACED. TENSION ADJUSTED AND OPERATIONALLY CHECKED SERVICEABLE.SDR CA970903014Vibraton Monitor · failed(CAN) NR1 ENGINE VIBRATION AT 5.0 UNITS ON TAKEOFF. TAKEOFF WAS REJECTED AND THE ENGINE WAS SHUTDOWN. NR1 ENGINE VIBRATION PICKUP CONNECTION WAS CLEANED, NR1 ENGINE VIBRRATION MONITOR AND VIBRATION INDICATOR (P/N 24-013074-1) WERE CHANGED. NR1 ENGINE CHECKED SSDR CA970904023Valve · leaking(CAN) LH MAIN LANDING GEAR ANTI-SKID VALVE LEAKING. REPLACED.SDR CA970722008Valve · open(CAN) DURING OPERATION OF APU ON GROUND THE LH PACK SHOWED TEMPERATURE WITH THE PACK SHUT-OFF VALVE CLOSED INDICATING THAT THE VALVE BUTTERFLY WAS NOT COMPLETELY CLOSED. VALVE REPLACEDSDR CA970722009Seal · leaking(CAN) DURING ROUTINE SERVICING OF THE HYDRAULIC SYSTEM RESERVOIR HEADER PRESSURE THE REGULATOR HAD A SEAL FAILURE RESULTING IN PRESSURE LOSS. THE REGULATOR WAS CHANGED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA970722040Controller · failed(CAN) CLIMBING FROM FLIGHT LEVEL 240 THROUGH FLIGHT LEVEL 260 CABIN PRESSURE OBSERVED TO BE ERRACTIC. SLOW DESCENT INITIATED WITH NO CHANGE. CABIN EXCEEDED 10,000 FEET. RAPID DESCENT CARRIED OUT AND CABIN PRESSURE CONTROLLED AT FLIGHT LEVEL 200 FEET. MAINTENANSDR CA970722038Air Cycle Mach · failed(CAN) CABIN FILLED WITH SMOKE AFTER AUXILIARY POWER UNIT STARTED AND PACK TURNED ON. MAINTENANCE REPLACED RH AIR CONDITIONING AIR CYLING MACHINE AND COALESER BAG (P/N 180849-1).SDR CA970722036Aircycle Machine · failed(CAN) SMOKE ALARM IN LAVATORY SOUNDED ALONG WITH SMELL OF SMOKE AFTER PUSH BACK. AIRCRAFT RETURNED TO GATE. INSPECTED LAVATORY, WASTE CONTAINER, LIGHTING, LAVATORY PUMP, BEHIND CEILING AND UNDER SINK, NO FAULT FOUND. LAVATORY DEACTIVATED PER MINIMUM EQUIPMENT SDR CA970722032Fan · inoperative(CAN) DURING CABIN CHECK BY INFLIGHT SERVICES BOTH LAVATORY SMOKE DETECTORS WERE FOUND ACTIVATED AND SMOKE IN CABIN. LEFT HAND HEAT EXCHANGER FAN FOUND INOPERATIVE. EXCHANGER FAN REPLACED AND EXCHANGER RAM AIR EXHAUST CONTROL VALVE (P/N 20211362) REPLACEDSDR CA970710013Pneumatic Valve · malfunction(CAN) UNABLE TO CONTROL CABIN PRESSURIZATION, CABIN CLIMBING. UNABLE TO CONTROL IN MANUAL MODE. ALL OXYGEN MASKS DEPLOYED AIRCRAFT RETURNED TO DEPARTURE AIRPORT. AIRCRAFT PRESSURIZED ON GROUND WITH APU AND ENGINE BLEED AIR, ALL SEALS ON DOORS AND CABLES CHECKESDR CA970710010Galley Assy · elect short(CAN) ON APPROACH AUTO PILOT DISCONNECTED AND SMOKE BEGAN TO DEVELOP IN FLIGHT DECK. THE "C" PHASE GALLEY POWER CIRCUIT BREAKER HAD OPENED. GALLEY ELECTRICAL POWER SWITCH SELECTED OFF, SMOKE DISSIPATED.FORWARD GALLEY ASSEMBLY REPLACED AS PER JOB TICKET 25-80-0SDR CA970710009Longeron · cracked(CAN) DURING ENGINEERING ORDER EDDY CURRENT INSPECTION E.O. NO.07-238D AILERON LONGERON 6L AT FUSELAGE STN 688 FOUND CRACKED. CONFIRMED BY VISUAL INSPECTION. NEW SECTION OF LONGERON REPLACED AS PER STRUCTURAL REPAIR MANUAL 53-02 PAGE 2A.SDR CA970624016Apu System · cabin smoke(CAN) AUXILIARY POWER UNIT SHUT DOWN PRIOR TO TAXIING. THROUGH 700 FEET STRONG SMOKE SMELL WITH HAZE PRESENT IN FLT DECK & CABIN. SMOKE ALARMS ACTIVATED IN BOTH LAVATORIES & APU POWER AVAILABLE LIGHT ON APU & GEN OFF LIGHT ON. APU FIRE DRILL CARRIED OUT, FIRESDR CA970624014Micro Switch · inoperative(CAN) DURING FLIGHT, LOST BOTH VERY HIGH FREQUENCY SYSTEMS. SYSTEM TRANSMITTING BUT NOT RECEIVING. APPROXIMATELY SEVEN MINUTES LATER VHF #2 WAS WORKING AND ABLE TO RECEIVE MESSAGES FROM AIR TRAFFIC CONTROL (ATC). INVESTIGATION REVEALED CAPTAIN'S GROUND SERVICESDR CA970528010Generator · ground fault(CAN) DURING CRUISE FLIGHT THE #3 ENGINE DRIVEN GENERATOR TRIPPED OFF LINE DUE TO A DIFFERENTIAL FAULT INDICATION. CSD DISCONNECTED AND FLIGHT CONTINUED WITHOUT INCIDENT. UNABLE TO DUPLICATE, GENERATOR REPLACED.SDR CA970603023Panel · missing(CAN) ON MAINTENANCE WALK AROUND, FOUND RIGHT HAND WING TIP NAVIGATION LIGHT QUICK ACCESS PANEL MISSING. NEW PANEL INSTALLED.SDR CA970603021Extinguisher · failed(CAN) PASSENGER DEPOSITED LIT CIGARETTE INTO WASHROOM WASTE BIN CAUSING A MINI FIRE. FIRE EXTINGUISHED AND BIN EMPTIED. CONTINENTAL MAINTENANCE PERSONNEL CALLED TO INSPECT WASHROOM WASTE BIN CONTAINER. BIN EMPTIED AND EXTINGUISHED WITH WATER. WASTE BIN FIRE EXSDR CA970603014Controller · inoperative(CAN) AT FLIGHT LEVEL 350 EXPERIENCED RAPID DECOMPRESSION, FLIGHT DESCENDED UNDER MANUAL AND REGAINED CONTROL AT FL260. MANUALLY DEPLOYED OXYGEN MASKS. TRIED AUTO PRESSURIZATION AGAIN, NO LUCK. MAINTENANCE CHANGED #2 PRESSURIZATION CONTROLLER AND SYSTEM CHECKESDR CA970508008Pump · failed(CAN) DURING DESCENT THE LOW PRESSURE LIGHT FOR THE #2 TANK R/H AFT BOOST PUMP CAME ON. THE PUMP WAS SELECTED OFF AND THE FLIGHT COMPLETED WITHOUT INCIDENT. PUMP REPLACED.SDR CA970508009Boost Pack · leaking(CAN) DURING PREFLIGHT THE L/H ELEVATOR BOOST PACK WAS FOUND LEAKING WHEN HYDRAULIC SYSTEM NOT POWERED, REPLACED.SDR CA970529009Ac Genertor · failed(CAN) AIRCRAFT HAD AC CROSS-TIE, RIGHT HAND AC BUS, RIGHT HAND GENERATOR AND RIGHT HAND DC BUS OFF LIGHTS ANNUNCIATED. MAINTENANCE REPLACED RH CONSTANT SPEED DRIVE AND GENERATOR. GROUND RUN CARRIED OUT SYSTEM CHECKED SERVICEABLE.SDR CA970529010Oven Receptacle · elect shorted(CAN) FIRE FLAMES AND SPARKS IN THE GALLEY OVEN AREA. AIRCRAFT RETURNED TO BASE. MAINTENANCE TROUBLE SHOOTING REVEALED OVEN SOCKETS IN POSITION 16 & 17 BURNT. OVEN RECEPTACLES POSITION 16 & 17 CHANGED. OVENS SENT BACK TO COMMISSIONARY FOR REPAIRS. SYSTEM CHECKSDR CA970505032Actuator · inoperative(CAN) PRIOR TO ARRIVAL, UNABLE TO ARM SPOILER IN THE AIR. MAINTENANCE REPLACED AUTOSPOILER ACTUATOR. TEST AND CONTROL STAMP CARRIED OUT. SYSTEM CHECKED SERVICEABLE.SDR CA970505028Engine · high vibration(CAN) #2 ENGINE WAS SHUTDOWN IN FLIGHT DUE TO HIGH VIBRATIONS AND LOW OIL PRESSURE, #2 ENGINE OIL LIGHT ILLUMINATED. VIBRATION WAS EVIDENT AFTER ENGINE WAS THROTTLED BACK. POST FLIGHT INSPECTION FOUND METAL IN THE TAIL PIPE. #2 ENGINE REPLACED, FURTHER REPORT SDR CA970505024Controller · inoperative(CAN) CABIN AUTO CONTROLLER FAILED AT TOP OF DESCENT. SWITCHED SYSTEM AND AUTO CONTROL WAS RECOVERED. OXYGEN MASK DEPLOYED IN CABIN. #1 AND #2 PRESSURE CONTROLLER REPLACED AND CHECKED SERVICEABLE.SDR CA970505020Controller · inoperative(CAN) CABIN PRESSURIZATION FLOW LIGHT CAME ON AT FL310. CABIN CLIMBING AT 100 FEET PER MINUTE BEGAN DESCENT TO 8,000 FEET. CABIN FLOW LIGHT OFF AND ON INTERMITTENTLY. EXECUTED RAPID DESCENT TO 8,000 FEET. DURING THIS EVENT LEFT DUCT PRESSURE WAS AT 20 P.S.I. ASDR CA970505019Engine · loss of oil(CAN) #2 ENGINE SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL QUANTITY AND PRESSURE. AIRCRAFT RETURNED TO BASE. #2 ENGINE REPLACED. FINAL REPORT TO FOLLOW.SDR CA970505018Eanco Cable · failed(CAN) UNABLE TO SHUTDOWN RIGHT ENGINE. TROUBLE SHOOTING REVEALED RH EANCO CABLE AT FAULT. DEFECTIVE CABLE REPLACED.
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