Pratt & Whitney JT8D-9A
Service difficulty reports · 1,388
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 = 'JT8D9A' 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 = 'JT8D9A' 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 F3LA00223Structure · wornDEN - DURING C-3 CHECK, FOUND NR 2 ENGINE INLET TRAILING EDGE MATING SURFACE FOR ENGINE COWL AT 6:00 POSITION WORN VERY THIN. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED TWO REPAIR ANGLES AND FILLERS PER SRM 54-10-03 AND TREATED AND PRIMED PER SRM 51-10-02. SDR CA000830036Hydraulic Line · ruptured(CAN) LOSS OF HYDRAULIC FLUID DURING DESCENT AND LANDING. NR2 ENGINE THRUST REVERSER PRESSURE LINE WAS FOUND RUPTURED IN PYLON UNDER A SUPPORT CLAMP.HYDRAULIC PUMP AND FILTER WERE CHECKED FOR CONTAMINATION AND FOUND SERVICEABLE. HYDRAULIC LINE REPLACED AS PERSDR CA000731003Splice · overheated(CAN) SEVERAL RPTS OF REJECTED TAKEOFFS, DUE TO NR 1 GEN DROPPING OFF LINE & LEADING EDGE DEVICES INTRANSIT LIGHT ILLUMINATING. INSP FOUND, NR 1 ENGINE GEN AL TO CU SPLICE OVERHEATED. SPLICE LOCATED AT WING STATION WBL 157, ABOVE ENGINE ELECT. DISCONNECTS IN DSDR CA000804015Tire · failed(CAN) CREW REPORTED LOUD BANG FROM NOSE WHEEL AREA ON TAKEOFF ROLL AND JUST BEFORE ROTATION. THEY ALSO NOTICED SOMEHTING GO PAST THE WINDSCREEN. A FLY PAST THE CONTROL TOWER AND DEBRIS FOUND ON THE RUNWAY CONFIRMED TREAD SEPARATION FROM ONE OF THE NOSE WHEEL TSDR CA000808020Radar · failed(CAN) DURING CLIMB, WEATHER RADAR FAILED. AIRCRAFT RETURNED TO STATION. WEATHER RADAR REPLACED I.A.W. M.M. 34-01-01. CHECKED SERVICEABLE.SDR CA000808019Module · failed(CAN) AT FLIGHT LEVEL 5,000 FEET, NOSE GEAR UNSAFE LIGHT ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. LANDING GEAR ACC. MODULE REPLACED AND TESTED I.A.W. M.M. 32-09-100. FUNCTION CHECKED SERVICEABLE.SDR CA000804017Track · broken(CAN) DURING THE WALK AROUND AND INSPECTION FOR AN A CHECK THE MECHANIC NOTICED EXCESSIVE MOVEMENT IN THE NR 6 SLAT. FURTHER INVESTIGATION REVEALED THAT THE CENTER AUX RACK HAD BROKEN AT THE ATTACH POINT TO THE SLAT. THE SLAT ASSEMBLE WAS REPLACED WITH A SERVISDR CA000718006Circuit Breaker · failed(CAN) NEARING TOP OF CLIMB, CIRCUIT BREAKERS BEGAN TO TRIP. FUEL PUMP CIRCUIT BREAKERS FOR LEFT SIDE, TCAS, STALL WARNING, EQUIPMENT COOLING, WINDOW ANTI-ICE, RADIO ALTIMETER. RETURNED TO YUL, NO EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. REPLACED NR 1 GENERSDR CA000808017Coupling · broken(CAN) AFTER LANDING AND TAXIING AIRCRAFT, APU WAS STARTED & FIRE HANDLE ILLUMINATED & AUDIBLE WAS HEARD. CREW PULLED APU FIRE HANDLE & EMPTY THE APU FIRE BOTTLE. ON FURTHER INVESTIGATION, THE COUPLING FOR THE COMBUSTION LINER BROKE. COUPLING WAS REPLACED. FIRESDR CA000718008Connector · loose(CAN) 85 MILES OUT OF MEM, NR 2 ENGINE OVERHEAT WARNING ILLUMINATED, THROTTLED BACK SNAG CLEARED. AIRCRAFT DIVERTED TO MEM. ON APPROACH, OVERHEAT WARNING REAPPEARED, FIRE BOTTLES DISCHARGED AND NR 2 ENGINE SHUTDOWN. DECLARED AN EMERGENCY AND LANDED WITHOUT INCSDR CA000731004Connector · loose(CAN) ENGINE OVERHEAT WARNING ILLUMINATED, THROTTLED BACK SNAG CLEARED. AIRCRAFT DIVERTED. ON APPROACH, OVERHEAT WARNING REAPPEARED, FIRE BOTTLES DISCHARGED AND NR 2 ENGINE SHUTDOWN. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND FIRE AND OVERHEAT ESDR CA000802021Control Panel · missing(CAN) DURING WALK AROUND IT WAS OBSERVED THAT THE RT INBOARD FUEL BOOST PUMP PANEL WAS MISSING. PANEL AREA TAPED. PANEL FASTENERS CAME LOOSE DUE TO VIBRATION AND AIRSPEED. PANEL WAS POSSIBLY LOST IN FLIGHT. PART REPLACED.SDR CA000718003Valve · failed(CAN) ON CLIMBOUT FROM MCO, NR 1 FUEL HEAT VALVE FAILED IN OPEN POSITIOIN, CAUSING NR 1 ENGINE HIGH OIL TEMPERATURE. RETURNED TO MCO. REPLACED NR 1 ENGINE FUEL HEAT VALVE AS PER MM, TESTED AS PER MM. CHECKED OK.SDR CA000706006Valve · failed(CAN) ON CLIMBOUT FROM MCO, NR 1 FUEL HEAT VALVE FAILED IN OPEN POSITION, CAUSING NR 1 ENGINE HIGH OIL TEMP. RETURNED TO MCO. REPLACED NR 1 ENGINE FUEL HEAT VALVE AS PER MM 73-14-11 PAGE 401, TESTED AS PER MM 73-14-11 PAGE 501. CHECKED OK.SDR CA000718002Fitting · leaking(CAN) AIRCRAFT DIVERTED TO YOW DUE LOW OIL QUANTITY IN NR 2 ENGINE. NO EMERGENCY WAS DECLARED, LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FITTING (ON GEARBOX) FOR DIFFERENTIAL PRESSURE SWITCH LEAKING.INSERT AND JAMB NUT REPLACED, LEAK CHECKED OK.SDR CA000706004Tire · missing(CAN) AIRCRAFT ON TAKEOFF, REPORTED TIRE DEBRIS ON RUNWAY. MAINTENANCE ADVISED, UNABLE TO DETERMINE FLT, LANDING, CREW REQUESTED CFR, DUE POTENTIAL TIRE PROBLEMS. FLIGHT LANDED WITHOUT INCIDENT. INSPECTION FOUND TIRE CAP MISSING FROM LEFT INBOARD WHEEL. DAMAGSDR CA000621005Oil Cooler · failed(CAN) A/C 759, , FLT 195, NR 2 CSD DISCONNECTED DUE LOW OIL PRESSURE LIGHT CAME ON. REPLACED NR 2 CSD OIL COOLER DUE COOLER BLOCKED BY PIECES OF FAN DIFUSER DUCT LINING, THAT HAD BROKEN UP. REPLACED NR 2 ENGINE AS PER WORK CARD 1125-2,SDR CA000706002Csd · failed(CAN) A/C 759, JUNE 17/2000, FLT 195, LOG SEQUENCE 0300876. NR 2 CSD DISCONNECTED DUE LOW OIL PRESSURE LIGHT CAME ON. REPLACED NR 2 CSD OIL COOLER DUE COOLER BLOCKED BY PIECES OF FAN DIFFUSER DUCT LINING, THAT HAD BROKEN UP. REPLACED NR 2 ENGINE AS PER WORK CASDR CA000614004Sensor · out of tolerance(CAN) ON TAKEOFF, LANDING GEARS WOULD NOT RETRACT WITHOUT USING GEAR OVERRIDE. AIRCRAFT RETURNED. LANDING GEAR ACCESSORY MODULE REPLACED AS PER WORK CARD 4281. OFF CANADIAN PART 7-326-9-0010 SERIAL 0054, ON SERIAL #0438. FURTHER TROUBLESHOOTING FOUND AIR SENSSDR 2000UALA00227Fire Detector · failedCREW REPORTS APU FIRE WARNING SOUNDED AFTER TAKEOFF. *S/D* FOUND APU FIRE DETECTOR M717 BAD.SDR P2EA00119Fitting · strippedPIT - FLT 732 - ON SHORT FINAL, NR 1 ENGINE OIL QUANTITY WENT TO ZERO. OIL PRESSURE FLUCTUATED 35 - 45 PSI, OIL PRESSURE LIGHT FLICKERED ON. UPON LANDING, OIL QUANTITY WAS ZERO, OIL PRESSURE WAS 20 SPI, OIL LIGHT WAS ON. CREW SHUT DOWN NR 1 ENGINE. FOUND LSDR CA000519018Connector · damaged(CAN) AT CRUISE APU FIRE HANDLE ILLUMINATED AND AUDIBLE FIRE WARNING BELL. FIRE WARNING DRILL AND FIRE WARNING HANDLE WAS PULLED AND FIRE BOTTLE DISCHARGED.ATC ADVISED AND A/C LANDED SAFELY. APU AREA CLEANED AND INSPECTED. APU DMIDAND FLOWN FOR REPAIRS. APU FSDR CA000516034Wheel · cracked(CAN) WHILE TAXING MAINT NOTED NR 2 MAIN WHEEL ASSY WAS FLAT. FURTHER INVESTIGATION REVEALED 1/3 OF THE OUTBOARD WHEEL HALF HAD BROKEN OFF AND THE TIRE WAS CUT AT THE WALL EDGE. DAMAGE WAS FOUND ON THE WING BODY FAIRING, LT IB FORE FLAP AND THE LT UPPER WING TSDR SWAA000763Engine · bird strikeAIR TURNBACK, DURING TAKEOFF ROLL A LOUD BANG NOISE HEARD DUE TO BIRD STRIKE ON NR 1 ENG. C/W NR 1 ENG BIRD STRIKE INSP, CLEANED PS4 SCREEN AND CSD OIL COOLER SCREEN. ENG OPS CK GOOD PER MM.SDR CA000501018Wire · overheated(CAN) PRIOR TO PASS BOARDING WHILE FLIGHT ATTENDANTS PREPARED THE CABIN FOR FLIGHT SMOKE AND ARCING WAS NOTICED COMING FROM THE REAR OF THE AIRCRAFT GALLEY COFFEE MAKER CB PANEL. ELECTRICAL POWER WAS REMOVER FROM THE AIRCRAFT GALLEY AND THE FIRE EXTINGUISHER FSDR 20000727AP001Valve · openFLT 67 - MIA-MGA - ON CLIMB, FUEL HEAT VALVE OPENED, UNABLE TO CLOSE. AC RETURNED TO MIA 30 MIN AFTER TAKEOFF. CONFIRMED DEFECT, VALVE PLACE DON MEL 73-2, FUEL HEAT VALVE ORDERED. (M)SDR 20001011AP011Valve · failedNR 1 ENGINE FUEL HEAT VALVE REMAINS OPEN. REPLACED NR 1 ENGINE FUEL HEAT VALVE. NO FURTHER DISCREPANCIES, ITEM REMOVED FROM MEL ON LOG PAGE 00750. (M)SDR CA000501019Fire Loop · chafed(CAN) ON CLIMB CREW OBSERVED ON INTERMITTENT NR 2 ENG FIRE WARNING ILLUMINATION. A/C RETURNED. WIRE UNDER RT ENGINE ANTI SLAVE FOUND CHAFED. WIRE REPAIRED. CRUSH WASHERS UNDER FIRE LOOP CONNECTORS MISSING, REPLACED. FIRE LOOP TOUCHING LOWER COWL, REPOSITIONED.SDR CA000501020Sensor · intermittent(CAN) ON TAXI CREW OBSERVED LE SLAT IN TRANSIT LIGHT STILL ON. NR 4 LE SLAT PROXIMITY SENSOR REPLACED. SYS SERVICEABLE.SDR USAASB00108Gearbox · leakingCLT - FLT 365 - ON CLIMB-OUT FROM CLT, THE NR 1 ENGINE OIL QTY WENT TO ZERO RESULTING IN AN INFLIGHT SHUTDOWN OF THE NR 1 ENGINE. CAPTAIN DECLARED AN EMERGENCY AND THE FLIGHT RETURNED TO FIELD AT CLT. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE SDR CA000414008Tube · chafed(CAN) NO 2 SYS A LOW PRESS WARNING LIGHT ON IN FLIGHT WITH A LOSS OF SYS QTY ON APPROACH. NO 1 A SYS LOW PRESS WARNING LIGHT ON RESULTING IN LOSS OF SYS HYD. CHAFED HYD LINE ABOVE RH MLG ACTUATOR. LINE REPLACED. AC SERVICEABLE.SDR CA000419004Shutoff Valve · failed(CAN) ON TAXI AFTER LANDING A SYS HYD FAILED DUE TO LOSS OF HYD FLUID. REPLACED LANDING GEAR SHUTOFF VALVE, A/C SERVICEABLE.SDR CA000427033Bearing · failed(CAN) ON TAXI TO GATE SPRKS WERE OBSERVED COMING FROM RH BRAKE AREA. NO 4 WHEEL INNER BARING FAILURE DAMAGED WHEEL, SLEEVE AND ROLLER COLLER. PARTS REPLACED.SDR CA000410003Valve · failed(CAN) A/C RETURNED DUE TO PASS RT MIX VALVE FAILED, VALVE REPLACED.SDR CA000331006Fuel Control · out of rig(CAN) ENGINE RIGGING DIFFICULTY.SDR SWAA000550Gearbox · leakingIN FLIGHT ENGINE SHUTDOWN, NR 2 ENG OIL QTY AND PRESS INDICTING ALMOST ZERO. REMOVED AND REPLACED NR 2 ENG MAIN GEAR BOX ASSY PER MM AND AVTEAM WORK ORDER.SDR GAIA00109Warning Light · illuminatedFLT 1844 - FWA-ORF - DURING TAKEOFF, THE NR 2 ENGINE FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED. THE CREW DECLARED A EMERGENCY LANDING BACK AT FWA. THE CREW RAN EMERGENCY CHECKLIST AND DISCHARGED FIRE BOTTLE. DURING SHUT DOWN NR 2 ENGINE, THROTTLE DIFFSDR CA000313001Proximity Switch · dirty(CAN) NLG WOULD NOT RETRACT AFTER TAKEOFF. NLG RECYCLED NO FIX A/C LANDED. SLUSH IN GEAR GRAVEL DEFLECTOR, PROXIMITY SWITCH DIRTY, CLEANED AND SERVICEABLE.SDR SWAA000430Power Supply · inoperativeABORTED TAKEOFF, NR 1 ENG FUEL FLOW INDICATOR INOP AT 20-30 KNOTS INTO THE TAKEOFF. REMOVED AND REPLACED NR 1 ENG FUEL FLOW METER POWER SUPPLY PER MM.SDR SWAA000437Engine · leakingAFTER TAKEOFF, WITH RT A/C PACK SELECTED, STRONG OIL FUMES IN CABIN. REMOVED AND REPLACED NR 2 ENG AND BOTH AIR CYCLE MACHINES.SDR TWAA0003803Pump · failedTHE NUMBER 1 ENGINE SPOOLED DOWN. FLIGHT RETURNED TO STL. REPLACED THE FUEL PUMP, PN378201-7, AND FUEL CONTROL PN 743602-5. FUEL PUMP SHAFT SHEARED. CHECK-C 8-8-99 MCI.SDR CA000427009Window · cracked(CAN) DURING FLIGHT THE CREW NOTICED THE VIEWING WINDOW IN THE FWD SERVICE DOOR CRACKED. WINDOW REPLACED.SDR CA000308004Unknown · odor(CAN) BURNING SMELL IN COCKPIT ON ARRIVAL. FOUND LOOSE AND OVERHEATED ELECTRICAL TERMINAL STUD IN THE P18-3 PANEL. NEW TERMINALS INSTALLED A/C SERVICEABLE.SDR CA000224015Shaft · binding(CAN) START LEVER STIFF AND SPONGY. FOUND ENGINE CROSS SHAFT BINDING. INNER AND OUTER CROSS SHAFT REPLACED.SDR CA000224016Proximity Sensor · out of adj(CAN) AFTER TAKEOFF NLG RED POSITION WARNING LIGHT REMAINED ON WITH GEAR UP AND OFF. RECYCLED AND RED LIGHT STILL ON. SENSOR TARGET OUT OF ADJUSTMENT, ADJUSTED A/C SERVICEABLE.SDR CA000313003Sensor · out of adj(CAN) NLG RED POSITION WARNING LIGHT REMAINED ON WITH GEAR UP. RECYCLED AND NO FIX A/C LANDED. UPLOCK SENSOR OUT OF ADJUSTMENT, ADJUSTED A/C SERVICEABLE.SDR CA000301010Window · cracked(CAN) DURING CRUISE CAPTAINS SLIDING WINDOW DELAMINATED AND CRACKED. WINDOW AND HEAT CONTROLLER REPLACED.SDR USAAD00028Manifold · leakingCLT-DAY FLT 860 - AFTER TAKEOFF, THE RIGHT ENGINE FIRE INDICATION ACTIVATED. THE THROTTLE WAS REDUCED AND THE INDICATION STOPPED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACE THE RIGHT ENGINE FUEL HEAT MANIFOLD. (M)SDR CA000301009Coffeemaker · overheated(CAN) DURING CLIMB CREW REPORTED SMELL OF SMOKE IN BACK OF MAIN CABIN, A/C RETURNED. COFFEEMAKER OVERHEATED AND REPLACED.SDR CA000215031Skin · cracked(CAN) FUSELAGE SKIN CRACKED AT FS 887 STR 20R REPAIRED IAW SRM.
Back to Pratt & Whitney JT8D-9A