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 COOSDR010095Bulkhead · crackedBS 1016, BULKHEAD WEB CRACKED.SDR COOSDR010097Skin · crackedFUSELAGE SKIN, HOLES CRACKED AND MISSING MATERIAL AT UPPER SKIN, LAP JOINT AREA.SDR COOSDR010098Doubler · crackedMAIN CARGO CABIN, FORWARD ENTRY DOOR UPPER HINGE CUTOUT INTERNAL DOUBLER WITH CRACK.SDR COOSDR010112Bulkhead · crackedFUSELAGE, PRESSURE BULKHEAD WEB WITH CRACK AT BS 178, WL 233.5 BETWEEN RBL 10 AND RBL 13.SDR COOSDR 010113Beam · crackedAFT ENTRY DOOR BEAM NR 2, INSIDE CHORD CRACKED.SDR COOSDR010114Bulkhead · crackedUPPER FUSELAGE AFT PRESSURE BULKHEAD WEB CRACKED AT BS 1016, STR 6L, AT AFT FASTENER ROWS ATTACHMENT TO THE Y CHORD.SDR COOSDR010115Floorbeam · corrodedMAIN CARGO CABIN FLOOR BEAM WITH CORROSION AT BS 312, LBL 58, WL 204.SDR COOSDR010116Frame · crackedMAIN CARGO CABIN FRAME CRACKED AT BS 277, BETWEEN S9L, AND S10L.SDR COOSDR010117Stringer · corrodedFORWARD CARGO COMPARTMENT STRINGER 19R CORRODED, AT BS 500A+14.SDR COOSDR010118Frame · corrodedLOWER NOSE COMPARTMENT, AT BS 222, WL 168, LBL 18 FRAME WITH CORROSION.SDR COOSDR010119Doubler · delaminatedLOWER NOSE COMPARTMENT, BONDED DOUBLER WITH DELAMINATION, FROM BS 211 TO BS 203, BETWEEN LBL 16 AND LBL 20.SDR COOSDR010120Doubler · delaminatedLOWER NOSE COMPARTMENT, BONDED DOUBLER WITH DELAMINATION, FROM BS 241 TO BS 247, BETWEEN RBL 17 AND RBL 20.SDR COOSDR010121Doubler · delaminatedCARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 995 TO BS 1006 AND BETWEEN STR 8R AND STR 10R.SDR COOSDR010122Doubler · delaminatedCARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 995 TO BS 1006 AND BETWEEN STR 8L AND STR 10L.SDR COOSDR010123Doubler · delaminatedCARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 927 TO BS 947 AND BETWEEN STR 14L AND STR 15L.SDR COOSDR010124Doubler · delaminatedCARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 500 TO BS 500A AND BETWEEN STR 3L AND STR 6L.SDR COOSDR010125Doubler · delaminatedCARGO CABIN BONDED DOUBLER WITH DELAMINATION, FROM BS 639 TO BS 655 AND BETWEEN STR 9L AND STR 8L.SDR COOSDR010126Doubler · delaminatedCARGO CABIN BONDED DOUBLER WITH DELAMINATION AT BS 937 AND BETWEEN STR 6R AND STR 7R.SDR 2001UALA01728Ferrule · leakingAIRCRAFT DIVERTED TO MIA DUE TO IDLE POWER CONDITION FROM NR 1 ENGINE. *S/D* THE CAUSE WAS A FUEL LEAK FROM THE FUEL LINE FROM THE FUEL/OIL COOLER TO THE P&D VALVE. THIS LINE WAS MISSING A FERRULE AT THE P&D VALVE CONNECTION. THIS ENGINE HAD ONLY 370 HRS SDR DL72E011334Control Valve · failedEXPERIENCED COMPRESSOR STALL ON NR 2 ENGINE AT 20 KTS ON TAKEOFF ROLL. ABORTED TAKE OFF. REPLACED NR 2 PRBC.SDR COOSDR010083Rib · crackedRIGHT WING, INBOARD MID FLAP RIB CRACKED AT WBL 86.74.SDR COOSDR010084Rib · crackedLEFT WING, INBOARD MID FLAP RIB CRACKED AT WBL 86.74.SDR COOSDR010086Skin · delaminatedRIGHT WING, AILERON PN 65-46454-2, SN 306 UPPER SKIN WITH DELAMINATIONS.SDR COOSDR010087Skin · delaminatedRIGHT WING, FLIGHT SPOILER NR 6, PN 65-79952-7 UPPER AND LOWER SKIN WITH DELAMINATIONS.SDR COOSDR010088Skin · delaminatedRIGHT WING, OUTBOARD FLIPPER FLAP, PN 6571950, SN BN-137 SKIN DELAMINATED.SDR 2001UALA01725Indicator · malfunctionedAIRCRAFT HAD SPLIT FLAP INDICATION ON APPROACH. OUTBOARD FLAP POSITION INDICATOR FAILED. REPLACED OUTBOARD FLAP POSITION INDICATOR. SYSTEM TESTS NORMAL.SDR 2001UALA01726Battery · failedAFT AIRSTAIRS EMERGENCY LIGHT IS INOPERABLE. SUPPLEMENTAL DATA UPDATE THE BATTERY FAILED. REPLACED BATTERY. OPERATIONS CHECK NORMAL.SDR 2001UALA01719Cover · leakingNR 3 ENGINE WAS SHUT DOWN DURING LANDING. *S/D* ENGINE WAS SHUT DOWN TO LOSS OF OIL FROM THE THE MAIN OIL SCREEN. THE OIL PRESSURE DROPPED TO 38 PSI. CAUSE WAS STUDS PULLED ON THE MAIN OIL SCREEN COVER AND WAS REPAIRED.SDR 2001UALA01609Pump · failedAIRCRAFT EXPERIENCED B-HYDRAULIC SYSTEM ZERO QUANTITY INDICATION DURING CRUISE. AIRCRAFT CONTINUED TO ORD. THE NR 1 ENGINE HYDRAULIC PUMP FAILED. REPLACED NR 1 ENGINE HYDRAULIC PUMP, SYSTEM TESTS NORMAL.SDR 2001UALA01608Tire · failedUPON LANDING THE TWO LEFT MAIN LANDING GEAR TIRES BURST. *S/D* HARD LANDING INSPECTION ACCOMPLISHED. ANTISKID FUNCTIONAL TEST ACCOMPLISHED. OPERATIONAL CHECK FOUND NO DISCREPANCIES.SDR 2001UALA01593Control Cable · obstructedCREW REPORTS STEERING TILLER BINDS, ESPECIALLY IN A LEFT TURN. *S/D* FOUND OBSTRUCTION IN NOSE METERING VALVE CABLE SYSTEM. CLEARED OBSTRUCTION AND INSPECTED CABLE SYSTEM. OPS CHECKS NORMAL.SDR DL72S011271Engine · making metalNR 1 ENG OIL FILTER BYPASS LT ILLUM. C/W POM PROCEDURE. LT DID NOT GO OUT. ENG SHUTDOWN. CA REPLACED NR 1 ENG OIL FILTER, LK CK GOOD. FOUND METAL ON MAIN OIL CHIP DET. PERFORMED ENG PENALTY RUN PER M/M. ON RE-INSP OF CHIP DET FOUND METAL AGAIN. REPLACED NR 1 ESDR 2001UALA01594Valve · failedNR 1 OIL TEMP IN YELLOW BAND FOR 15 MIN. ENGINE SHUTDOWN AND DIVERTED TO COS. THE FUEL HEAT VALVE FAILED. REPLACED FUEL HEAT VALVE AND DRAINED, REPLACED OIL AND SCREEN. THE MOTOR IN THE ACTUATOR OF THE VALVE ASSEMBLY WAS FOUND TO BE BAD.SDR FX72001F00002Hydraulic Line · leakingAFTER TAKE-OFF LOSS OF QUANTITY AND PRESSURE OF A SYSTEM (A) HYDRAULIC. DUMPED REQUIRED FUEL FOR RETURN TO AIRPORT. AIRCRAFT RETURNED WITH NO EMERGENCY DECLARED AIRCRAFT LANDED, UNEVENTFUL. T/S HYD LOSS TO RT MLG FLEX HOSE RETURN. REMOVED AND REPLACED RIGHSDR FX72001F00004Hydraulic Line · leakingAFTER TAKEOFF, LOSS OF QUANTITY AND PRESSURE OF SYSTEM (A) HYDRAULIC. DUMPED REQUIRED FUEL FOR RETURN TO AIRPORT. AIRCRAFT RETURNED WITH NO EMERGENCY DECLARED, AIRCRAFT LANDED UNEVENTFUL. T/S HYDRAULIC LOSS TO RIGHT MAIN LANDING GEAR FLEX HOSE RETURN. REMOSDR 2001UALA01513Battery · failedAFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT IS INOPERABLE. SUPPLEMENTAL DATA UPDATE BATTERY FAILED. REPLACED BATTERY. OPERATIONS CHECK NORMAL.SDR 2001UALA01511Bypass Switch · failedAIRCRAFT DIVERTED DUE TO A NR 1 OIL FILTER BYPASS LIGHT. REPLACED THE OIL FILTER BYPASS SWITCH.SDR 2001UALA01462Skin · crackedFUSELAGE SKIN CRACK LOCATED JUST AFT OF NR 2 VHF ANTENNA, LEFT OUTBOARD BETWEEN 4TH AND 5TH ROW OF RIVETS. CRACK IS APPROX. 1.75 INCHES LONG. FUSELAGE SKIN CRACK BETWEEN STATION 1030 AND 1070 STR 28L. DAMAGE CUTOUT, EDDY CURRENT, AND DOUBLER INSTALLED PER SSDR 2001UALA01470Pump · leakingCREW REPORTS LOSS OF B-SYSTEM BRAKE PRESSURE, ALSO REPORTS FLUID COMING FROM THE GEAR ON TAXI OUT. REPLACED NR 2 ENGINE B-SYSTEM HYDRAULIC PUMP. SYSTEM TESTS NORMAL.SDR 2001UALA01468Controller · malfunctionedAT FL240 WHEN THROTTLES PULLED BACK TO FLIGHT IDLE, CABIN PRESSURE STARTED CLIMBING AT 2000 FPM. WHEN CARGO HEAT VALVE CLOSED, CABIN PRESSURIZATION RETURNED TO NORMAL.SDR 2001UALA01469Controller · failedCABIN PRESSURE CAN NOT BE MAINTAINED (CABIN ALTITUDE RISES) IN DESCENT. BOTH AUTO & STANDBY THIS HAPPENS EVEN AT 5000 FEET. DUCT PRESSURE NORMAL. REPLACED THE NR 3 ENGINE 13TH STAGE MODULATOR VALVE, AND THE PRESSURE CONTROLLER.SDR 2001F00272Control Valve · failedON FLT 748 - FPO-CVG - TAKEOFF ROLL, NR 2 ENGINE STALLED DURING ACCELERATION THROUGH 70 KTS. PARAMETERS WERE OBSERVED TO RECOVER TO NORMAL. HOWEVER, NR 2 ENGINE ACCESS DOOR LIGHT ILLUMINATED, TAKEOFF ABORTED. REMOVED AND REPLACED NR 2 PRBC VALVE, OPERATION SDR 2001UALA01445Skin · corrodedRIGHT SIDE OF FUSELAGE 6 INCHES AFT OF FORWARD LAV SERVICE PANEL, PAINT IS BUBBLING AND SKIN IS BULGING IN A 6 INCH DIAMETER AREA.SDR 2001UALA01443Skin · delaminatedFLIGHT SPOILER LEFT WING NR 3 DELAMINATED NEAR TRAILING EDGE. FLT SPOILER LEFT WING NR 3 DELAMINATED NEAR TRAILING EDGE. SPOILER PANEL WAS CHECKED FOR CRACKS OR SCRATCHES AND NONE WERE NOTED. AN INTERIM REPAIR WAS ACCOMPLISHED WITH THE REQUIREMENT THAT THE SSDR 2001UALA01466Aileron · out of adjCREW REPORTS RIGHT HAND WING OUTBOARD AILERON, INBOARD TRAILING EDGE MAKING CONTACT. CHECKED ADJUSTMENT OF FLAP AND ADJUSTED AILERON. OPERATIONS CHECK NORMAL.SDR EISA20010108Engine · inoperative#1 ENG LOSING OIL QTY, OIL TEMP ON THE RISE, LOSING OIL PRESS. ENGINE #1 SHUT DOWN.CORRECTIVE ACTION:#1 ENGINE TO BE REMOVED.SDR 2001UALA01463Control Panel · failedCABIN PRESSURIZATION ELECTRONIC SYSTEM IN MANUAL THERE IS NO OUTFLOW VALVE INDICATOR MOVEMENT WITH FUNCTION SWITCH IN AC MANUAL. VALVE VISUALLY OBSERVED AND IS NOT MOVING. THE CONTROL PANEL FAILED. REPLACED CONTROL PANEL. OPERATIONS CHECK NORMAL.SDR 2001UALA01422Screw · missingLOSS OF HYDRAULIC FLUID IN THE 'A' SYSTEM. FOUND FLAP DRIVE MOTOR SHAFT SEAL PLATE MISSING SCREWS AND O-RING POPPED OUT. REPLACED FLAP DRIVE MOTOR AND SERVICED HYD SYS. OPERATIONS AND LEAK CHECK NORMAL.SDR 2001UALA01444Cowling · crackedNR 2 ENGINE LOWER FORWARD COWLING MATING FLANGE, FOUND 3 CRACKS, ONE 8 INCHES LONG, THE OTHERS 3.5 INCHES LONG. ALSO, THERE IS A HOLE WORN THRU COWL MATING FLANGE. REPAIRED COWL AND SPLICED IN NEW FLANGE. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01465Engine · malfunctionedNR 3 ENG EGT LIMITED T/O FROM DEN. COMMAND EPR 2.06. TARGET N1 X-CK 98.1. AT 2.06 EPR, NR 3 ENG N1 95 PERCENT AND EGT REACHED 630 DEG FOR 2 SEC. REDUCED POWER TO KEEP EGT IN LIMITS. A CHECK OF THE INLET AND EXHAUST AND PERFORM THE MAX EGT CHECK PER JRH 2-7-3
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