Pratt & Whitney JT8D-15
Service difficulty reports · 2,710
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 = 'JT8D15' 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 = 'JT8D15' 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 06FDEA03599Skin · chafedINTERIOR CABIN, MCD CUTOUT RESTRAINT WEB SKIN IS CHAFED AT BS 639, WL 295, LBL 24. EVALUATED CHAFED AREA ON MCD CUTOUT RESTRAINT WEB SKIN BS 639, WL 295. REMOVED DAMAGED AREA AND FABRICATED REPAIR PARTS FOR WEB AND ALODINE, PRIMED AND INSTALLED AT BS 639 WLSDR 06FDEA03601Pressure Panel · corrodedLT WHEEL WELL, CEILING IS CORRODED BS 901, LBL 61. REMOVED CORROSION BS 901, LBL 61 AND REPAIRED IAW FED EX EA 7-5310-100592.SDR 06FDEA03602Keelbeam · crackedLT KEELBEAM CRACKED AT BS 872 INSIDE KEELBEAM BOX. REMOVED DAMAGE LT KEELBEAM AT BS 872 AND REPAIRED IAW FED EX EA 7-5310-100593.SDR DHL2006746003Indicator · malfunctionedAT BEGINNING OF TAKE-OFF ROLL, TAKE-OFF THRUST SET, MACH AIRSPEED WARNING SOUNDED. INDICATED AIRSPEED LESS THAN 60 KTS. REMOVED AND REPLACED FO'S MACH AIRSPEED INDICATOR IAW B727 MMS CH 34-12-21. TESTS GOOD. PITOT/STATIC TEST GOOD IAW B727 MMS 34-11-00. REMOVSDR 06FDEA03448Shim · corrodedLT NR 3 FLAP TRACK BEAM CENTER MOUNT TAPERED SHIM CORRODED REMOVED CORROSION FOUND OUT OF LIMITS, CORROSION EXFOLIATION IAW SRM 51-10-6 AND SRM57-10-1 FIG 1 DETAIL 1. FABRICATED NEW SHIM ON MAE TRAVLER T6/31804.SDR 06FDEA03449Shim · corrodedLT NR2 FLAP TRACK AFT MOUNT TAPERED SHIM CORRODED REMOVED CORROSION FOUND OUT OF LIMITS REMOVED .035 FROM ORG MAT .045 REMAINING MAT .010 IAW SRM 57-10-6 AND 57-10-1 FIG 1 FABERICATED NEW SHIM ON MAE TRAVLER T6/ 631803.SDR 06FDEA03442Proximity Sensor · malfunctionedAFTER TAKE-OFF, COULD NOT RAISE LANDING GEAR LEVER PAST (OFF) POSITION RAN QRM PROCEDURES, AND FAILED TEST NR 1 OF STRUT EXTENSION AND NOSE ALIGNMENT TEST. REMOVED AND REPLACED AIR SENSING PROX SENSOR(M831). PERFORMED OPS CKS PER M/M 32-09-221-4 AND 32-31-0SDR 06FDEA03440Flap Track · corrodedLT NR 3 FLAP TRACK BEAM FWD MOUNT SUPPORT FITTING CORRODED. REMOVED AND REPLACED BUSHNG IAW SR 27-57-020 AND SOPM 20-50-03. REMOVED CORROSION FROM FITTING ORIGINAL MATERIAL .750 AFTER REWORK .740. FOUND TO BE WITHIN LIMITS IAW SRM 51-106 AND SR 27-51-020 TRESDR CA060929002Indicator · failed(CAN) DEPARTING THE CREW OBSERVED A L/E FLAP UNRETRACTED INDICATION AT THE NR 1 POSITION.THE AIRCRAFT RETURNED TO POINT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE POSITION INDICATION SWITCH HAD FAIL AT THE NR 1 KRUEGER FLAP LOCATION. THE SWITCH WAS REPLACSDR CA060925009Connector · faulted(CAN) ON LANDING, THE NR 1 AND NR 4 TIRES SKIDDED UNTIL THEY BLEW OUT. THE A/C HAD TO BE TOWED FROM THE RUNWAY. AVIONICS PERSONELL DISCOVERED AN INTERMITTENT FAULT IN AN ANTI-SKID CONNECTOR (D4668) ABOVE THE RT GEAR LEG. ALL 4 TIRES AND THE CONNECTOR WERE REPLSDR CA060919001Shutoff Valve · leaking(CAN) DEPARTING THE CREW OBSERVED A STRUT OVERHEAT CONDITION ON NR 3 ENGINE. THE AIRCRAFT DIVERTED WHERE MAINTENANCE DETECTED A LEAK AT THE WING ANTI ICE SHUT-OFF VALVE (SOV). GASKETS WERE REPLACED AND NO FURTHER FAULT APPEARED EVIDENT AT GROUND RUN. DURING THSDR 2006F00034A/C Pack · failedAIRCRAFT N464AT DEPARTED EWN FOR ISO WITH THE LEFT HAND AIR CONDITIONING PACK AIRFLOW SHUTOFF VALVE ON DMI (MEL 21-02) AND FLYING UNDER PACK PRESSURIZED OPERATIONS PROCEDURE. EN ROUTE TO ISO AT A FL OF 22,000 FEET THE FLIGHT CREW NOTICED THE RIGHT HAND AIR COSDR GAIA06027OPShutoff Valve · closedDURING CLIMB THE NR 2 ENGINE OIL FILTER BYPASS/LOW PRESSURE LIGHT ILLUMINATED. THE OIL PRESSURE TEMPERATURE AND QUANTITY WERE NORMAL. THE NR 2 ENGINE FLAMED OUT SHORTLY AFTERWARD. THE FLIGHT CREW PERFORMED THE ENGINE FAILURE CHECKLIST AND RETURNED. THE AIRSDR C8GA20060009Gasper Fan · smokeDURNING CRUISE OPERATION CREW EXPERIENCED SMOKE IN THE COCKPIT 139 NM FROM. DECLARED AN EMERGENCY AND PERFORMED EMERGENCY PROCEDURES, SMOKE DISAPPATED AND ORDOR FADED, AIRCRAFT CONTINUED AND LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT FOR ELECTRICAL PROBLEMS, SDR CA060724001O-Ring · swollen(CAN) ON DESCENT STABILIZER OUT OF TRIM LIGHT ILLUMINATED, STABILIZER WOULD NOT RESPOND TO COMMANDS FROM AUTOPILOT, MAIN ELECTRIC TRIM OR MANUAL TRIM. FLIGHT CREW ACCOMPLISHED THE STABILIZER JAM EMERGENCY CHECK LIST AND LANDED UNEVENTFULLY. UPON INSPECT MAINTESDR CA060714001Line · loose(CAN) CREW OBSERVED LOSS OF OIL QUANTITY NR 1 ENGINE. ENGINE SHUTDOWN PRIOR TO LOW OIL PRESSURE WARNING LIGHT ILLUMINATING. MAINTENANCE DETERMINED UPON THE JUST COMPLETED NR6 OIL BEARING REPLACEMENT THE FORWARD END OF THE PRESSURE TUBE WAS NOT SECURED AND LOCKSDR PCSA06220601Warning System · multiple failFLIGHT 611 ON TAKEOFF FROM MIA THE CREW REPORTED THE NR 1 BLEED TRIP LIGHT CAME ON. THE CREW THEN CHANGED TO THE NR 2 BLEED, ONE MINUTE LATER THE NR 1 STRUT OVERHEAT LIGHT CAME ON. THE CREW FOLLOWED THE COMPANY CHECKLIST AND SHUT DOWN THE NR 1 ENGINE; DUMPEDSDR PCSA062206SUPBlades · damagedON TAKEOFF CREW REPORTED NR 1 BLEED TRIP LIGHT CAME ON. CHANGED TO NR 2 BLEED, ONE MIN LATER NR 1 STRUT OVERHEAT LIGHT CAME ON. FOLLOWED COMPANY CHECKLIST & SHUT DOWN NR 1 ENGINE; DUMPED FUEL, & RETURNED WITHOUT INCIDENT. INSPECTION OF NR 1 ENGINE FOUND C-SDR C8GA20060007Oil Cooler · inoperativeFLT 1711 FROM LAX TO TOL. DURING CLIMB PASSING THROUGH 10,000FT THE NR 3 ENGINE CSD TRIPPED INDICATING 140 DEGREE'S CELSIUS IN TEMP. THE NR 2 ENGINE CSD WENT TO 140 DEGREE'S AND NR 1 CSD WAS OPERATING HOT AT 125 DEGREE'S. AIRCRAFT DIVERTED TO SAN AND LANDESDR CA060608001Switch · malfunctionedAFTER DEPARTURE ON AN ACCEPTANCE FLIGHT AFTER HEAVY MAINTENANCE, THE CREW OBSERVED A NR 1 CARGO DOOR UNSAFE INDICATION. THE WARNING LIGHT EXTINGUISHED AT 7.2 PSID AFTER REDUCING ALTITUDE TO 11K FT. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WHERE THE SWITCHSDR SROM200600010Case · crackedDURING HEAVY MAINTENANCE INSPECTION FOUND CRACKED OUT SECTION IN REAR EXHAUST CASE OF NR 2 ENGINE. REPLACED WITH OVERHAULED UNIT.SDR DHL2006748003Engine · failedNR 2 ENG FAILED AT APPROX 20000 LOUD BANG SHOOK AIRPLANE. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW B727 MTM 71.2.SDR 06FDEA1728Engine · seizedAFTER T/O AT 1,000' WITH STD POWER, NR 3 ENGINE SEIZED AT QUIET OIL QUANTITY DROPPED TO ZERO. CONDUCTED EPR REDUCTION. QRH ENGINE FIRE/SEVERE DAMAGE CHECKLIST. RETURNED TO FIELD. CRASH CREW REPORTED OIL LEAKING FROM ENGINE. PERFORMED ENGINE SEIZURE INSP PSDR 06FDEA1661Engine · failedATTEMPTED TAKEOFF ON 18L HAD SLIGHT COMPRESSOR STALL ON POWER APPLICATION. ABORTED TAKEOFF AND CHECKED ENGINE CONDITIONS ELECTED SECOND ATTEMPT DUE TO CROSSWINDS. ON SECOND ATTEMPT HAD ANOTHER COMPRESSOR STALL. 1ST STALL OCCURRED AT 1.5 EPR AND SECOND STALLSDR CA060427004Shutoff Valve · malfunctioned(CAN) CLIMBING THROUGH FL20 THE F/E ADVISED OF PRESSURIZATION PROBLEMS. AFTER REDUCING TO 10,000 FT. CABIN INDICATED 10,000 WITH 3 PSI DIFF.WHEN THRUST REDUCED THE DIFF WAS 0. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE REPLACED THE PRESSURIZATIONSDR 06FDEA1264Fuel Control · unknownON TAKEOFF ROLL, AFTER TAKEOFF POWER WAS SET, N1 AND EPR INCREASED WITHOUT ANY PILOT INPUT. THE NUMBER 3 THROTTLE WAS ADVANCED AHEAD OF OTHER THROTTLES BY 1 KNOB WIDTH. COMPLETED INSTALL OF FUEL CONTROL AND PUMP IAW 727-2 00AMM AND PWMM 73-11-01.SDR DHL2006742001Engine · failedAT 70 KIAS EXPERIENCED LOUD BANG WITH ENGINE FAILURE LIGHT. NR3 ENGINE EGT INCREASED TO 700 C. COMPLETED ENGINE FAIL CHECK LIST ACFT WEIGHT 169.500 IAS 70 KTS OAT 28 G C PA 4860. BRAKE ENERGY NORMAL WIND CALM. REMOVED AND REPLACED NR3 ENG IAW MM 71-00 PERFOSDR 06FDEA0973Compressor · stalledDEPARTING 23R IND USING STD PWER, EXPERIENCED COMPRESSOR STALLS ON NR 2 ENGINE. REJECTED TAKEOFF AT 50KTS AND EXITED RWY. ENGINE GAUGES WERE NORMAL EXCEPT NR 2 EPR, WHICH BARELY CLIMBED WHEN POWER WAS APPLIED. LEARN FROM THE MISTAKES OF OTHERS. REMOVED ANDSDR 06FDEA0858Shear Tie · corrodedFWD PIT SHEAR TIE STA 700 BETWEEN STRINGER 28L AND 27L IS CORRODED. REMOVED AND REPLACED WITH NEW SHEAR TIE AT STA 700 BETWEEN S28L AND 27L IAW SRM B727 51-30-5 AND 51-30-2. SNRM N01051.SDR 06FDEA0859Frame · corrodedFRAME STA 950F STRINGER 29L, CORROSION. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FRAME REPAIR STA 950F AT S29L ALL IA FX B727 SRM'S 53-10-4 FIG 12,53-10-1,53-10-2 AND 51-10-2 SNRM N00990.SDR 06FDEA0860Skin · lightning strikeNOSE AREA FUSELAGE EXTERNAL SKIN HAS SEVERAL LIGHTNING STRIKES BETWEEN BS178 AND 203.8 BETWEEN STRINGERS 24 TO 26 LT. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED. FUS SKIN REPAIR STA 178 TO 203 BETWEEN STRINGERS 26LAND 24L ALL IAW FX B727 SRM'SDR 06FDEA0862Skin · corrodedFUS SKIN AT FWD PIT STA 700-720A BETWEEN STRINGER 27L AND 28L IS CORRODED. REMOVED DAMAGE, FABRICATED, ALODINED , PRIMED AND INSTALLED FUS SKIN REPAIR STA 700-720A FROM STRINGER 27L TO 28L ALL IAW SRM'S 53-30-1 FIG1,53-30-3 FIG3,51-30-2 AND 51-10-2. SNRM N0SDR 06FDEA0864Stringer · corrodedFWD PIT BS 700 AT STRINGER 28L CORROSION ON STRINGER AND WEB. CORRECTIVE ACTION: REMOVED DAMAGE,LOCATED, DRILLED AND INSTALLED NEW STRINGER AT STA 700 TO 720 AND S28L ALL IAW FX B727 SRM'S 53-10-3 FIG1,51-30-2 AND 53-10-1.SDR 06FDEA0861Floorbeam · corrodedAFT PIT FLOORBEAM LOWER CHORD SEVERAL AREAS CORRODED BS 1070 AT LBL 26. REMOVED DAMAGE, FABRICATED, HEAT TREATED, ALODINED, PRIMED AND INSTALLED FLOORBEAM REPAIR TO STA BS 1070 BETWEEN RBL 54 AND LBL 26 ALL IAW FX SRZ SR27-53-034E REPAIR NR 8, B727 SRM'S 51-SDR 06FDEA0863Frame · corrodedFRAME AT STA 950C 4 INCHES RT OF CENTER LINE IS CORRODED. REMOVED DAMAGE, FABRICATED, ALODINED, PRIMED AND INSTALLED FRAME REPAIR AT STA 950C LBL 4 TO RBL 4 ALL IAW FX B727 SRM 53-10-4 FIG12,51-30-2,53-10-1, 53-10-2 AND 51-10-2.SDR 06FDEA0816Stringer Clip · corrodedN00370 STRINGER CLIP AT BS 804 AND STR 4R HAS SURFACE CORROSION. REMOVED AND REPLACED STR CLIP BS 804 STR 4R IAW SRM 51-10-1.SDR 06FDEA0815Floorbeam · corrodedCORROSION ON FLOORBEAM LWR FLANGE BS 720 LBL30-RBL37. REPLACED WITH NEW FLOOR BEAM PER SRM 51-10-2, SRM 51-30-5 & 51-30-2.SDR 06FDEA0804Stringer · corrodedN00364 STR 2R HAS SURFACE CORROSION BETWEEN BS 740- BS 826. REMOVED AND REPLACED STR 2R BS 740-870 IAW SRM 53-10-1, 51-30-2, 51-20-1 AND 51-10-2.SDR 06FDEA0800Skin · corrodedFWD PIT STA 680 FROM STRINGER 27R TO 28R SKIN IS CORRODED. FABRICATED, ALODINED, PRIMED AND INSTALLED FUS SKIN REPAIR AT STA BS 680-690 AND STRINGER 27R TO 28R ALL IAW FX SRM'S 53-30-3 FIG 3, 53-30-1, 53-30-2,51-30-2 AND 51-10-2. SNRM N01070.SDR 06FDEA0798Engine · failedPRECAUTIONARY SHUTDOWN NR 2 ENGINE DUE TO VIBRATION. AIRCRAFT ON GROUND REPORTED SEEING SPARKS COMING FROM NR 1 ENGINE, HOWEVER HAD SEVERE VIBRATION ON NR 2 ENGINE. FAN HAS FOD AND BLADES BROKEN IN HALF, SECOND STAGE DAMAGED, THIRD STAGE IS ALSO DAMAGED, SDR CA060216006Pump · unknownON CLIMB, NR 2 RT AFT FUEL BOOST PUMP CB RELEASED FOLLOWED BY NR 2 LT AFT CB RELEASING APPROX 3 MIN LATER, NR 2 RT FWD CB RELEASED AND NR 2 LT FWD BOOST PUMP LOW PRESS LIGHT ILLUMINATED INTERMITTENTLY. A/C RETURNED TO DEPARTURE. MX INSPECTED ALL EFFECTED PUMSDR CA060213003Transmitter · failed(CAN) AIRCRAFT EXPERIENCED A FLAP ASYMMETRY ON APPROACH. CREW DECLARED AN EMERGENCY AND ELECTRICLY DROVE THRU FLAPS TO LANDING CONFIGURATION. AIRCRAFT LANDED SAFELY AND WAS TAXIED TO THE HANGER. HANGER MAINTENANCE CONFIRMED THE LT IB FLAP TRANSMITTER AS THE CASDR CA060208009O-Ring · swollen(CAN) SHORTLY AFTER TAKEOFF, CREW NOTICED SYS (A) HYDR INDICATED ZERO QTY. CREW DECLARED AN EMERGENCY, ASKED FOR A RETURN TO AIRPORT. CREW REQUESTED A FUEL DUMP, THIS WAS APPROVED BY ATC. AFTER FUEL DUMPING WAS COMPLETED AC RETURNED AIRPORT FOR ARRIVALS ILS 29SDR DHL2006753501Angle · crackedFOUND NR 019254; RT W/W VERTICAL ANGLE IS CRACKED AT STA 870 RBL 5. REMOVED DAMAGED PART AND INSTALLED NEW PART PN NR 65-18636-378 PO NR 550312 IAW SRM = 51-30-2 & 53-10-2 FIG 4.SDR 06FDEA0432Frame · dentedN00519 FRAME DENTED AT BS 520 BETWEEN STR 22L AND STR 24L IN THE FWD CARGO COMPARTMENT. REPAIRED FRAME AT BS 520 BETWEEN STR 22L-STR 24L IAW SRM 51-40-3.SDR PCSA01310601Nut · looseKMIA-MDSD FLIGHT 871 - CREW REPORTED APPROXIMATELY 20 MINUTES INTO CRUISE, NR 1 ENGINE EGT, N1 AND N2 RAPIDLY APPROACHED THEIR LIMITS. ENGINE NR 1 WAS SHUTDOWN PER AOM. ENGINE WINDMILLED FOR 50 MINUTES AND ENGINE OIL PRESSURE AT 25 PSI DURING WINDMILLING. A/CSDR 06FDEA0409Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT STR 5 RT BS 720C. REMOVED CORROSION FOUND OUT OF LIMITS R/R NEW STR CLIP PER SRM 51-30-2, 51-10-2.SDR 06FDEA0410Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT STR 2 RT BS 680. FOUND CORROSION OUT OF LIMITS. REMOVED AND REPLACED STR CLIP AT BS 680 STR 2 RT PER SRM 51-30-2.SDR 06FDEA0411Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT STR 3 RT BS 680. FOUND CORROSION OUT OF LIMITS R/R NEW STR CLIP PER SRM 51-30-2.SDR 06FDEA0412Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT STR 2 RT BS 720A. REMOVED CORROSION FOUND OUT OF LIMITS R/R NEW STRINGER CLIP PER SRM 51-30-2.
Back to Pratt & Whitney JT8D-15