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 GAIA05019OPLight · illuminatedEMERGENCY EXIT DOOR LIGHT ON ALL THE TIME. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (K)SDR GAIA05018OPSmoke Detector · dirtyDURING CRUISE, MAIN CARGO SMOKE WARNING ILLUMINATED IN FLIGHT. VISUAL INSPECTION REVEALED NO SMOKE IN CARGO AREA. FLIGHT CONTINUED TO DESTINATION, WHERE A LANDING WAS MADE WITHOUT INCIDENT. CLEANED SMOKE DETECTORS FROM NR1 TO NR 6. ON NR 1 REPLACED BOTH LISDR GAIA05016OPBattery Pack · dischargedDURING PREFLIGHT, FOUND L1 DOOR AND COCKPIT ENTRY DOOR EMERGENCY BATTERY PACKS DRAINED TO DIM ILLUMINATION. REPLACED BATTERY PACKS (2 EA). OPERATED EMERGENCY LIGHTS SYSTEM AND FOUND OPERATING NORMALLY. OK FOR SUBSEQUENT FLIGHT. AC WAS RETURNED TO SERVICE. SDR FX7A200500003Shutoff Valve · defectiveDURING CLIMB ENGINE NR 1 STRUT OVER HEAT LIGHT ILLUMINATED.SDR CA050322008Wire · arced(CAN) CAPT L2 SLIDING WINDOW POWER CORD ARCING AND FILLING THE COCKPIT WITH SMOKE. WINDOW HEAT SELECTED OFF AND BREAKER PULLED. POWER CORD DISCONNECTED FROM RECEPTICLE. REMOVED AND REPLACED THE CAPT L2 SLIDING WINDOW, SYSTEM TESTED SERVICEABLE, AIRCRAFT RETURSDR 05FDEA00501Oil Filter · bypassingDESCENDING THROUGH 20,000 FEET, THE NR 1 LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED; ENGINE OIL PRESSURE READ 45 PSI (MATCHED NR 2 AND NR 3). SHUT DOWN NR 1 ENGINE IAW QRH PROCEDURES. NO OTHER PROBLEMS NOTED.SDR DHL2005746004Filter · bypassingNR 3 OIL FILTER BYPASS LIGHT ILLUMINATED. ABNORMAL PROCEDURE COMPLETE. REMOVED & REPLACED NR 3 ENG ASSY IAW B727 MTM 71.1.SDR CA050218003Tube · separated(CAN) DURING CLIMB THROUGH 18000 FT ENGINE NR 1 LOW OIL PRESSURE LIGHT ILLUMINATED ACCOMPANIED BY RAPIDLY DECREASING OIL QUANTITY AND PRESSURE INDICATIONS. CREW CARRIED OUT ENGINE SHUTDOWN CHECKLIST DECLARED AN EMERGENCY, DUMPED FUEL AND RETURNED TO DEPARTURE SDR AU510001960Nut · separated(AUS) NR 2 ENGINE POWER CONTROL LEVER CONTROL CRANK RETAINING NUT LOCATED ON THE MAIN ACCESSORY GEARBOX CROSS SHAFT ADRIFT. THE CRANK MOVED OFF THE CROSS SHAFT AND POWER LEVER CONTROL WAS LOST. THE RESULT OF THE UNCONTROLLED POWER LEVER ALLOWED AN UNCOMMANDED SDR CA050214003Switch · failed(CAN) MAIN CARGO DOOR LIGHT AND HOOKS UNLOCKED LIGHT ILLUMINATED AFTER TAKEOFF. AIRCRAFT RETURNED TO AIRPORT AND LANDED OVERWEIGHT. CARGO DOOR VERIFIED CLOSED AND LOCKED. MAIN CARGO DOOR INDICATION MEL RAISED AND OVERWEIGHT LANDING INSPECTION C/O IAW MM 5-51-SDR CA050203005Cylinder · intermittent(CAN) NLG FAILED TO EXTEND ON APPROACH, THEN RE-CYCLED AND EXTENDED NORMALLY. NOSE GEAR JACKED, NOSE GEAR TRUNION GREASED AND GEAR RETRACTED AND EXTENDED 4 TIMES WITH NO FAULTS. AC WAS DISPATCHED WITH NO FURTHER FAULTS. QA GROUNDED THE AC DUE TO 2 OTHER EVENSDR CA050119003Switch · intermittent(CAN) ON APPROACH, LANDING GEAR CYCLED DOWN FOR LANDING. THE NOSE LANDING GEAR RED INDICATOR STAYED ILLUMINATED AND NO GREEN INDICATION WAS SEEN. GEAR WAS RE-CYCLED AND THE GEAR WAS EXTENDED WITH PROPER INDICATION. MAINTENANCE LUBED THE NOSE GEAR AND JACKED THSDR GAIA05002OPO-Ring · damagedDURING CRUISE THE FLIGHT CREW SHUT DOWN THE NR 2 ENGINE DUE TO LOSS OF OIL QUANTITY AND PRESSURE. THE AIRCRAFT DIVERTED, AND MADE AN UNEVENTFUL LANDING. REMOVED AND REINSTALLED NR 2 ENGINE FUEL PUMP, REPLACED FUEL PUMP GARLOC SEAL AND SHAFT O-RING PACKING. SDR 2005FA0000116Skin · misdrilledDRILL START NOTED AT L-BAND NR 1 ANTENNA FWD RT MOUNT HOLE. BS410, RBL 1. (IN SKIN) FOUND WHILE PERFORMING INSPECTION OF ANTENNA IAW WORKCARD NR 34X4505. (K)SDR C8GA20040029Engine · leakingFLT 202 FROM SVMI TO KMIA - ON CLIMB-OUT, NR 2 ENGINE OIL QUANTITY DECREASED. AT 1.8 GALLONS INDICATED, NOTICEABLE DECREASING INDICATION. RETURNED TO SVMI AND LANDED WITHOUT INCIDENT. FERRIED AIRCRAFT TO JAX AND CHANGED NR 2 ENGINE. OPS AND LEAK CHECK GOODSDR 0412001Fire Warning · activatedFLIGHT 9604 - WHILE EN ROUTE (CRUISE) FROM ATL TO ADS AN UNSCHEDULED LANDING IN SHV WAS ENCOUNTERED DUE TO NR 1 ENGINE FIRE LIGHT ILLUMINATION AND THE FIRE BELL RINGING. FOLLOWED THE AAC QRH MEMORY ITEMS AND UPON PULLING FIRE HANDLE THE LIGHT EXTINGUISHED. DSDR CA041216008Transmitter · sticking(CAN) DURING INITIAL CLIMBOUT, FLAPS CYCLED FROM 5 DEG. TO 2 DEG. CREW NOTICED THAT LT OUTBOARD FLAPS WERE INDICATING 5 DEG. & RT OUTBOARD FLAPS WERE INDICATING 3 DEG. CAUSING AN ASSYMETRY SPLIT. CREW HAD TO DUMP FUEL TO LAND WITHIN LANDING WEIGHT. CREW ACCOMPSDR FX7A2004XXXX3Packing · pinchedAFTER ENGINE START ON THE NR 3 NOTICED THE LOW OIL QUANTITY INDICATION. RETURNED TO THE GATE. REPLACED THE DEFECTIVE PACKING ON THE OIL TANK CAP AND TIGHTENED OIL PRESSURE SWITCH LINE B-NUT, IAW MM REF 79-20-11 AND 79-11-0. SERVICED THE NR 3 ENGINE FOUR QUASDR FX7A2004XXXX2Position Switch · misriggedDURING TAXI OUT NR 4 LEADING EDGE FLAPS RIGHT DOES NOT HAVE A GREEN LIGHT ON THE F/E PANEL POSITION TEST, RETURNED TO THE GATE. TROUBLESHOT AND FOUND NR 4 LEADING EDGE FLAP POSITION SWITCH LEVER ARM MISALIGNED. ADJUSTED THE POSITION SWITCH LEVER ARM IAW MM RSDR GAIA04177OPClamp · brokenDURING CLIMB, NR 2 ENGINE FIRE WARNING AFTER TAKEOFF. SHUT DOWN NR 2 ENGINE. RETURNED TO AIRPORT. DECLARED EMERGENCY. LANDING WAS MADE WITHOUT INCIDENT. FOUND BROKEN CLAMP ON 8TH STAGE SADDLE DUCT AT THE ANTI-ICE CONNECTION. REPLACED CLAMP. LEAK CHECKEDSDR GAIA04175OPDownlock Switch · failedDURING APPROACH, ON SHORT FINAL, NOSE GEAR LIGHT CHANGED FROM GREEN TO RED, GOT HORN. CYCLED GEAR TWICE TO NO AVAIL. VISUAL INSPECTION THROUGH PORT INDICATED DOWN AND LOCKED. DECLARED EMERGENCY. LANDING AND TAXI IN UNEVENTFUL. TROUBLESHOOT NOSE GEAR INDICSDR CA041123004Hinge · damaged(CAN) HYDRAULIC BAY DOOR SEPARATED FROM AIRCRAFT. AIRCRAFT WAS BEING POSITIONED FROM THE MAIN MAINTENANCE BASE ON THE MORNING OF NOVEMBER 22, 2004. DURING SERVICE CHECK BY MAINTENANCE, IT WAS NOTICED THAT THE HYDRAULIC BAY DOOR WAS MISSING. MAINTENANCE SUSPESDR CA041122013Skin · cracked(CAN) A 4 INCH CRACK WAS FOUND ON THE OUTER FUSELAGE SKIN JUST AFT OF THE WING TO BODY FAIRING RT SIDE. CRACK LOCATED ON STR 15R (2) TWO INCHES AFT OF STA.727A. CRACK REPAIRED IAW SRM 53-30-3 FIG48 DETAIL XI TIMES 53851.20 CYCLES 46695.SDR DHL2004782012Engine · leakingAT 10 KTS ON THE TAKEOFF ROLL RWY 35L WINDS CALM TEMP +1C A LOUD BOOM WAS HEARD THE AUTOPACK TRIP TRIPPED AND THE TAKEOFF REJECTED. THE A/C WAS TAXIED OFF THE RUNWAY AND THE NR 3 ENGINE OIL WAS DECREASING THE NR 3 ENGINE WAS SHUT DOWN RETURNED TO THE BLOCKS RSDR CA041110001Proximity Sensor · failed(CAN) UPON SELECTION OF FLAPS 15 ON LANDING CHECKLIST THE L/E FLAP TRANSIT REMAINED ILLUMINATED AND THE NR 4 SLAT INDICATOR WAS SHOWING IN TRANSIT. REPLACED AND ADJUSTED NR 4 SLAT PROX SENSOR IAW MM 27-88-11. NR 4 SLAT FOUND DENTED ON UPPER SURFACE, REPLACED SDR 04FDEA02980Frame · damagedWHILE COMPLING WITH EA 7-5310-64946 A F/U FOUND FRAME REPAIR NOT TO BE DONE IAW SRM AT BS 680 STR 24R NEED TO COMPLY WITH EA 7-5310-55392 ** SD ** COMING REPAIRED IAW EA 7-5310-55392.SDR C8GA20040024Proximity Switch · failedAFTER TAKE-OFF, TAKE-OFF WARNING SOUNDED WHEN FLAPS SELECTED FROM 5 TO 2 DEGREES. HORN SILENCED WHEN CYCLED BACK TO 5 DEGREES. CYCLED GEAR AND GEAR HANDLE STUCK IN DOWN POSITION. AIRCRAFT RETURNED TO AIRPORT. TAKE-OFF HORN SOUNDED AGAIN WHEN FLAPS SELECTED FROSDR GAIA04171OPGasket · blownDURING CLIMB, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND BLOWN GASKET AND LOOSE CLAMPS AND DUCT LEAKS. REMOVED AND REPLACED GASKET AND TIGHTENED CLASDR DL73S040969Fuse · unserviceableON PREFLIGHT CHECK FWD CABIN EMERGENCY LIGHTS FAILED TO TEST. FOUND ONE BAD FUSE IN FWD BATTERY RACK. REPLACED SAME. CHECKS OKSDR 04FDEA02928Solenoid · failedPDIS 245 32-10 0006358 12OCT04 LAX CLOSE R LOGPAGES: 00900921 LANDING GEAR LEVER LATCH FAILED TO RAISE ON TAKEOFF PAST OFF POSITION. RAN QRH. CHECK/RESET LEVER LATCH CB (IAW QRH) AND PULLED AURAL WARNING CB (QRH) AND RETURNED.SDR 0410001Gearbox · leakingDURING CRUISE ENGINE OIL QUANTITY DROPPED TO ZERO.SDR AWXA200401089Brake · seizedABORTED TAKEOFF, FLT 0109, ON TAKEOFF, EN ROUTE WHEN APPROACHING V1 THE AIRCRAFT NOSE STARTED TO ROTATE ON ITS OWN, LOWERED NOSE AND REJECTED TAKEOFF AT 138 KTS. MAINTENANCE PERFORMED HORIZONTAL STABILIZER TRIM TEST, ALL TRIM INDICATIONS AGREE WITH (B) DIMENSSDR CA041018008Line · leaking(CAN) AFTER START-UP AT PUSH BACK THE PURSER NOTIFIED THE FLT DECK CREW OF FUMES IN THE CABIN. THE PASSENGERS WERE DEPLANED AND THE AIRCRAFT WAS RETURNED MAINTENAN CE TO IDENTIFY AND DETERMINE THE SOURCE OF THE PROBLEM. MAINTENANCE FOUND A PIN HOLE IN THE TAILSDR DHL2004754026Metering Valve · leakingNR 3 AND NR 4 MLG BRAKES DRAGGING. REMOVED AND REPLACED MLG BRAKE METERING VALVE, RT BRAKE SPRING CARTRIDGE, AND RIGGED RT AND LT BRAKE CONTROL LINKAGE IAW MM 32-41-11 AND 32-41-01. LEAK, FUNCTIONAL, AND OPS CHECKS GOOD MM 32-41.SDR C8GA20040022Duct · looseFLT 705 CLEARED FOR TAKEOFF, A LOUD BANG WAS HEARD AT 1.4 EPR CHECK. TAXI CLEAR OF RUNWAY AND PERFORMED A SECOND CHECK ON THE DE-ICE PAD WITH SAME RESULTS. AIRCRAFT RETURNED TO RAMP AND UPON INSPECTION FOUND THE PRESSURE RELIEF VALVE ON PACK DISTRIBUTION DUCT SDR DHL2004780514Skin · dentedDURING A C-CHECK, THE FOLLOWING DISCREPANCIES WERE NOTED; DENT ON LT VERTICAL STABILIZER APPROX STA FIN 177 (LT SIDE RUDDER). DENT FOUND TO BE OUT OF LIMITS IAW SRM 55-40-1 FABRICATED DOUBLER 2024T-3 .040 4.5 X 2.5 PO NR 9001359 IAW SRM 55-40-2 AND 55-20-3 TSDR DHL2004742007Controller · malfunctionedON GROUND STALL WARNING, STICK SHACKER AND AUTOPILOT DISCONNECT WARNING CAME ON AND COULD SMELL ELECTRICAL SMOKE IN COCKPIT. ADJUSTED AOA IAW 34-18-01, INSPECTED WIRING IN EE BAY NO SIGN OF SMOKE DETECTED SUSPECTED SMOKE FROM APU, INSPECTED APU IAW 21-20-01. SDR CA040923007Drag Brace · lack of lube(CAN) ON FINAL APPROACH, SELECTED GEAR DOWN. NOSE GEAR DOORS DID NOT OPEN AND THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED WITH THE NOSE GEAR GREEN LIGHT OUT. EXECUTED A MISSED APPROACH AND THE GEAR RETRACTED NORMALLY. RESELECTED GEAR DOWN AND GEAR EXTENDED NSDR 04FDEA02801Intercostal · crackedFWD CARGO, INTERCOSTAL IS CRACKED AT STRINGER 25L STA.624. REMOVED INTERCOSTAL IAW SRM 51-30-2. FABRICATED,TREATED AND PRIMED NEW INTERCOSTAL IAW SRM 51-20-1 FIG.6, 51-30-5 AND 51-10-2. INSTALLED IAW SRM 51-30-2. FABRICATED INTERCOSTAL USING 2024-T3 .050,SDR 04FDEA02803Floor Support · corrodedAFT CARGO COMPT FLOOR SUPPORT BEAM CORRODED UNDER NUTPLATE STA. 1110, RBL 6. REMOVED CORROSION, MATERIAL OUT OF LIMITS IAW SRM 53-10-5 FIG.6,PG.16 AND SRM 51-10-6. REMOVED DAMAGED AREA FROM STA 1105 TO 1115 RBL, FABRICATED 4 EA ANGLES (SPLICES). REPAIR ANSDR C7WA200400047Shear Tie · corrodedSHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11. MATERIAL USED 7075-T6 X .050 INCH X 6 INCHES X 11 INCHES.SDR C7WA200400048Shear Tie · corrodedSHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 LT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11, MATERIAL USED 7075-T6 X .050 INCH X 6 INCHES X 11 INCHES.SDR C7WA20040922Shear Tie · corrodedSHEAR TIE CORRODED AT STA 950A BETWEEN STR 28 AND STR 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11 MATERIAL USED 7075-T6 X .050 INCH X 6 INCHES X 11 INCHES.SDR C7WA200400050Stringer · corrodedSTRINGER 29 RT CORRODED AT STA 950A. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED REPAIR ON RT FLANGE IAW SB 727-0170.SDR C7WA200400045Skin · corrodedFUSELAGE LOWER SKIN AT STA 720B, STR 28 RT CORRODED. INSTALLED EXTERNAL SKIN REPAIR IAW SRM 53-30-3, FIG 1 DOUBLER MATERIAL USED, 2024-T3 X.160 INCH X 27 INCHES X 28.5 INCHES.SDR C7WA200400044Stringer · corrodedSTRINGER 28 RT CORRODED AT STA 990. REPLACED DAMAGED KEELBEAM SECTION IAW EO NR 1M-727-53-0236 AND DRAWING 65-56441-8.SDR C7WA200400042Door Frame · corrodedELECTRONIC COMPARTMENT DOOR CUTOUT AFT FRAME CORRODED STA 450 BETWEEN STRINGER 27 RT AND 27 LT. REMOVED AND REPLACED FRAME SECTION. FABRICATED NEW FRAME SECTION IAW SAMPLE. MATER USED 7075-0, .050, HEAT TREATMENT TO 7075-T6 IAW BAC 5602.SDR C7WA200400043Skin · corrodedFUSELAGE LOWER SKIN AT STA 990 STR 28 RT. CORRODED AND TWO RIVETS MISSING. INSTALLED EXTERNAL SKIN REPAIR IAW SRM. 53-30-3 FIG 3. DOUBLER MATERIAL USED, 2024-T3 X .125 INCH X 17 INCHES X 11 INCHES.SDR C7WA200400046Support Angle · corrodedSUPPORT ANGLE CORRODED AT STA 1030 TO 1050 BETWEEN STR 29 AND 30 RT. REPAIR ANGLE FABRICATED IAW SAMPLE IAW SRM 51-20-1 AND 51-40-3. MATERIAL USED 7075-T6 X .050 INCH.SDR C7WA200400051Stringer · corrodedSTR 27 RT CORRODED STA 620. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED STRINGER REPAIR IAW SRM 53-10-4 FIG 1, DETAIL 2.
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