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 RYN2004F00000Element · overheatedAFTER DEPARTURE, AT GEAR RETRACTION, RECEIVED A LOWER AFT BODY OVERHEAT LIGHT. ACCOMPLISHED APPROPRIATE CHECKLIST. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LT AIRSTAIR AFT BODY OVERHEAT ELEMENT. RAN ENGINES AT TAKEOFF POWSDR 2004F00271Connector · dirtyENGINE NR 1 OIL FILTER LIGHT ILLUMINATED IN CLIMB, FOLLOWED PROCEDURES AND SHUTDOWN ENGINE DUMPED FUEL AND RETURNED TO TSJU WITHOUT INCIDENT. CLEANED CONNECTOR ON OIL FILTER BYPASS LIGHT SWITCH CHECKED AND CLEANED OIL FILTER RAN ENGINE IAW 79-33-0. ENGINE CHSDR 2004F00384Pump · failedDURING INITIAL CLIMB ENGINE NR 1 FAILED, FLAMED OUT, DUMPED FUEL AND RETURNED TO KMIA WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PER MM 73-11-01. OPS CHECK GOOD, A/C RETURNED TO SERVICE NO FURTHER INCIDENTS. (M)SDR CA031212004Control Cable · out of adjust(CAN) CONTROL WHEEL VERY STIFF WHEN DEFLECTED LT AND SLOW TO RETURN ON RT DEFLECTION. LOST MOTION CABLES ADJUSTED IAW MM 27-10-0 AILERON INPUT PUSHROD ADJUSTED IAW MM 27-10-0CENTERING PUSHROD ADJUSTED A PER MM 27-10-0 SPOILER MIXER CONTROL ROD ADJUSTED MM 27-6SDR COOSDR030161Floorbeam · corrodedMAIN CARGO CABIN, BS 1110, FLOORBEAM, LOWER CHORD CORRODED.SDR COOSDR030160Frame · corrodedRT MAIN GEAR WHEEL WELL, STA 940 WL 201, FORGING FRAME, VERTICAL FLANGE, NBOARD SURFACES CORRODED.SDR COOSDR030159Frame · corrodedRT MAIN GEAR WHEEL WELL, STA 950 WL 201, FORGING FRAME, HORIZONTAL FLANGE, LOWER SURFACES CORRODED.SDR COOSDR030158Skin · corrodedLT WING, LOWER SKIN, LOWER SURFACE, ACCESS DOOR CUTOUT CORRODED. (K)SDR CA031203004Engine · failed(CAN) FLIGHT ENROUTE, FLIGHT CREW REPORTED INCREASED VIBRATIONS COMING FROM NR 1 ENGINE AND SPARKS REPORTED ON VISUAL INSPECTION. CREW SHUTDOWN ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. ENGINE CHANGE BEING CONDUCSDR DHL2003752006Compressor · stalledENGINE NR 2 COMPRESSOR STALL WHEN ON POSITION RUNNING UP THE ENGINES AT 80 PERCENT, HIGH CROSSWIND COMPONENT. INSPECTED NR 2 ENGINE FAN, NO DEFECTS NOTED. ACCESS HATCH SECURED IAW M/M 71-00 PAGE 608.SDR 2004F00361Bleed Valve · inoperativeCREW REPORTED, NR 1 ENGINE BLEED AIR VALVE TRIP LIGHT ON DURING FLIGHT AND VALVE STATED CLOSED AFTER ACCOMPLISHING THE ALTERNATE PROCEDURE FROM AOM. AIRCRAFT RETURNED TO KMIA WITHOUT FURTHER INCIDENT. MAINTENACNE REMOVED AND REPLACED THE NR 1 ENGINE BLEED SHSDR DHL2003754018Compressor · stalledAFTER ADVANCING THRUST LEVERS FOR TAKEOFF HEARD A COMPRESSOR STALL AND REJECTED THE TAKEOFF AT 16,100 GTW AND ZERO INDICATED AIRSPEED. OAT WAS 9 C AND PRESS ALT +100 FT. THIS WAS FIRST ATTEMPT AT T/O. AFTER ADVANCING THRUST LEVERS FOR TAKEOFF HEARD A COMPRESDR CA031126011Skin · cracked(CAN) WHILE PERFORMING A (C CHECK), CORROSION WAS FOUND ON THE LT IB FLAP AT WBL 124. AFTER PAINT REMOVING IT WAS DISCOVERED THAT A CRACK OF .5000 INCH LONG WAS BENEATH THE PAINT. CRACK REPAIR IAW SRM.SDR CA031117004Skin · cracked(CAN) THE AIRCRAFT WAS ON A (C CHECK. UPON INSPECTION OF THE FUSELAGE, A QUESTIONABLE SCRATCH WAS FOUND AT STATION BS 700 STRINGER NR 1. PAINT WAS STRIPPED AND NDT INSPECTION CARRIED OUT. A CRACK OF HALF INCH LONG WAS DISCOVERED. THE FUSELAGE WAS REPAIRED IAWSDR AUS20031147Fitting · corroded(AUS) NR 1 ENGINE FORWARD SUPPORT FITTING TOP SURFACE CORRODED IN AREA BETWEEN FITTING AND UPPER STRUT SKINS. FOUND DURING INSPECTION IAW AD/B727/151.SDR CA031126012Skin · lightning strike(CAN) WHILE PERFORMING A (C CHECK) IT WAS FOUND THAT THE AIRPLANE HAD BEEN HIT BY LIGHTING. POINT OF ENTRY WAS AT NOSE DOOR AND EXIT POINT AT RT ELEVATOR TAB. REPAIR HAD TO BE CARRIED OUT BETWEEN BS 196 TO 203, BS 219 TO 235 , FORWARD OF NOSE LDG FS 188, NOSESDR 2004F00264Valve · leakingDURING CLIMB-OUT, F/E REPORTED NR 3 ENG FIRE WARNING LIGHT ILLUMINATED. CAPTAIN FOLLOWED EMERGENCY PROCEDURES. A/C DIVERTED TO KMIA & LANDED WITHOUT FURTHER INCIDENT. MX OPENED COWLING & FOUND EVIDENCE OF FLASH FIRE. FOUND STARTER WITH INTERNAL FAILURE, INSDR CA031030001Outflow Valve · failed(CAN) A/C EXPERIENCED LOSS OF PRESSURIZATION ON CLIMB OUT. CREW DISCOVERED RT PACK INOPERATIVE. A/C LANDED AT COMPANY MAINTENANCE FACILITY WHERE THE RT FWD PACK VALVE WAS REPLACED AND A/C RETURNED TO SERVICE.SDR AUS20031093Shaft · sheared(AUS) MAIN CARGO DOOR FORWARD AND AFT ACTUATOR PIVOT SHAFTS SHEARED. SECONDARY DAMAGE CAUSED TO AFT ACTUATOR MAIN SUPPORTS.SDR 2004F00243Engine · malfunctionedFLT 813 - KMIA-TBPB - AFTER DEPARTURE FORM KMIA, NR 3 OIL PRESSURE INDICATED ABOVE ARC LINE, AND THEN OIL TEMP BEGAN CLIMBING AND WENT ABOVE ARC LINE. SHUT OFF NR 3 ENGINE AS PER PROCEDURES. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT.SDR 0301959987Engine · making metalDURING CRUISE FLIGHT, NR 2 ENGINE OIL QUANTITY WENT TO ZERO, OIL TEMP CLIMBED INTO THE RED ZONE. THE NR 2 ENGINE WAS SHUT DOWN. FLIGHT CREW DIVERTED AIRCRAFT TO MBS AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND METAL IN THE OIL FILTER AND ON THE CHIP SDR AWXA200301207Wire · wornDURING INSPECTION THE OVER WING EMERGENCY EXIT AISLE SIGN WAS FOUND INOPERATIVE ON ONE SIDE. MAINTENANCE RE-PINNED THE BACK SHELL CONNECTOR ON OVER WING EMERGENCY EXIT AISLE SIGN, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301208Wire · brokenDURING INSPECTION EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 13 & 14 LT WERE FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN SPLICE ON EMERGENCY ESCAPE PATH LIGHT WIRE AT SEAT ROW 12 LT, OPERATIONAL CHECK WAS GOOD.SDR AWXA200301206Pump · inoperativeON CLIMB OUT OF PHX EN ROUTE FOR SJC LOST (A) SYS HYDS, TURNED BACK TO PHX & LANDED WITHOUT EVENT. MAINT R & R NR 2 EDP IAW T/C R5M29001. R & R (A) HYD SYS CASE DRAIN, PRESSURE, & RETURN FILTERS, FLUSHED SYSTEM IAW BMM 29-11-0, PG. 204. LEAK AND OPERATIONAL CHSDR DHL2003747011Light · inoperativeENTRY EMERGENCY EXIT LIGHT IS INOPERATIVE. REMOVED AND REPLACED FORWARD ENTRY EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-00. OPS CHECKED GOOD.SDR 0704010Door · delaminatedLT AC BAY DOOR DELAMINATED AT BS 634.SDR 0704024Attach Fitting · crackedRT IB FLAP IB TORQUE TUBE ATTACH FITTING CRACKED.SDR 0704020Gimbal Joint · crackedLT WING IB FLAP OB CARRIER GIMABL CRACKED.SDR AWXA200301086Wire · brokenDURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD.SDR DHL2003749513Floor Support · dentedDURING C CHECK, PIT FLOOR SUPPORT FROM STA. 950E TO STA. 990 RBL 14 HAS SEVERAL DENTS. CUT-OUT DAMAGED AREA AND FABBED FILLER FROM 7075 T6 .050 P.O. NR 9912793 DIM. 1.7500 INCH X 1INCH AND DOUBLER FROM 7075 T6 .063 P.O.NR 9912793 DIM. 6 INCHES X 2.500 INCHESDR DHL2003749505Skin · puncturedDURING C CHECK, RT SIDE FUSELAGE STA. 1340 AIRSTAIR CUTOUT HOLES PUNCTURED IN SKIN. CUT-OUT DAMAGED SKIN AND FABBED FILLER FROM 2024 T3 .050 14.6250 INCH AND 12.2500 INCH AND DOUBLERS FROM 2024 T3 .063. 1250 INCH X 4.5 INCH X 5.5 INCH X 4.2500 INCH IAW B-727 SDR DHL2003749503Web · crackedDURING C CHECK, AFT AIRSTAIR TORQUE BOX VERTICAL WEB HAS A CRACK COMING FROM LIGHTNING HOLE AT STA. 1323 LT SIDE. STOP DRILLED CRACK IAW B-727 SRM 51-10-1. 2) NDT STOP DRILLED HOLE IAW B-727 N.D.T. PT-6 51-00-00 FIG. 23, CRACK STOPS AT HOLE. FABRICATED REPASDR 0704015Static Wick · corrodedSTATIC WICK BASE CORRODED ON RT HORIZ STAB.SDR 0704008Angle · crackedANGLE CRACKED AT BS 251.6 LBL 29.SDR 0704001Support Angle · crackedSUPPORT ANGLE CRACKED BS 727+4 BETWEEN S23R-S24R.SDR 0704006Floor Support · corrodedFLOOR SUPPORT ANGLE CORRODED BS 947.5 LBL33.SDR 0704004Floorbeam · crackedANGLE CRACKED RBL 24 AT FLOORBEAM.SDR CA030910003Engine · failed(CAN) THE ENGINE HAS BEEN REMOVED FOR TEARDOWN TO DETERMINE THE CAUSE OF THE PROBLEM.SDR AWXA200301040Angle · crackedDURING C-16 CHECK A .1875 INCH CRACK WAS FOUND ON ATTACH ANGLE AFT OF L-1 DOOR CUTOUT BS 348.20, WL 222. MAINTENANCE REMOVED CRACKED ATTACH ANGLE BS 348.20, WL 222; FABRICATED A NEW REPLACEMENT ATTACH ANGLE IAW DWG 69-26555; INSTALLED REPAIR PART IAW B737-20SDR AWXA200301039Angle · crackedDURING C-16 CHECK A .5 INCH CRACK WAS FOUND ON WEB ANGLE JUST AFT OF BS 348.20, LT SIDE OF FUSELAGE, WL 216. MAINTENANCE REMOVED CRACKED WEB ANGLE BS 348.20; FABRICATED A NEW REPLACEMENT WEB ANGLE IAW DWG 69-16509; INSTALLED REPAIR PART IAW B737-200 SRM 51-30-SDR HOC2003F00020Skin · corrodedDURING A (C) CHECK, CORROSION WAS NOTED ON FUSELAGE SKIN INTERIOR AT STA 600-680, LBL85.SDR HOC2003F00024Frame · corrodedDURING A C-CHECK CORROSION WAS NOTED ON SUPPORT FRAME STA 920-920A AT BLO-LBL-1.SDR 2003F00555Fuel Control · contaminatedAFTER DEPARTURE FROM KMIA, NR 1 ENGINE RPM BEGAN TO INCREASE AND DECREASE DURING CLIMB OUT. AIRCRAFT DIVERTED BACK TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAITNENANCE INSPECTED NR 1 ENGINE INLET AND EXHAUST IAW CHAPTER 71-00. NO DAMAGE FOUND, INSPECTEDSDR AUS20030855Switch · faulty(AUS) TRAILING EDGE FLAP 27.5 SWITCH (S294) FAULTY. FOUND DURING INSPECTION IAW AD/B727/105.SDR AWXA200301041Skin · crackedDURING C-16 CHECK A .1250 INCH CRACK WAS FOUND ON NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR AT WBL 230 LT. MAINTENANCE REMOVED AND REPLACED NR 3 SLAT INBOARD MAIN TRACK CLOSE OUT DOOR ASSEMBLY AT WBL 230 LT IAW B737-200 SRM 51-30-02, PARA B & E.SDR AWXA200301042Floorbeam · crackedDURING C-16 CHECK A .5625 INCH CRACK WAS FOUND ON FLOORBEAM REPAIR BS 677, RBL 24. MAINTENANCE REMOVED REPAIR ANGLE AND 2 EACH DOUBLERS; FABRICATED A NEW REPLACEMENT REPAIR CHANNEL AND 3 EACH DOUBLERS; INSTALLED REPAIR PARTS IAW AWA E.R. 15-5715-03240-ES2.SDR 2003F00606Fuel Control · failedLEVELING OFF AT 330 WHEN NR 2 ENGINE WAS THROTTLED BACK TO CRUISE POWER, THE FUEL FLOW WENT TO ZERO, AND THE EPR WENT TO 2.24 ENGINE FLAMED OUT. FUEL WAS DUMPED AND EMERGENCY DECLARED A/C LANDED WITHOUT INCIDENT. THE FUEL CONTROL WAS CHANGED PER MM 73-21 ANDSDR CA030731017Pcu · leaking(CAN) IN CRUISE, FLT CREW REPORTED AN APU FIRE INDICATION. CREW FOLLOWED CHECKLISTS, DISCHARGED APU FIRE BOTTLE, DECLARED AN EMERGENCY & REQUESTED CLEARANCE DIRECTLY TO YWG. APU FIRE WARNING LIGHT REMAINED ON AND CREW ADVISED OF ABNORMAL LANDING CONFIGURATION.SDR SWAA031642Blade · bentON POST FLT WALK AROUND NOTICED DEVIATION IN NR 2 ENGINE FAN BLADE. DEVIATION IS 1.25 LONG AND .375 OFF OF STRAIGHT AND LEVEL. REMOVED AND REPLACED C1 FAN ASSY PER MM.SDR AWXA200300812Bleed Valve · malfunctionedDEN - ABORTED TAKEOFF - FLT 0640 - DURING TAKEOFF ROLL AT DEN EN ROUTE FOR PHX, A LOUD "BANG" CAME FROM THE NR 1 ENGINE, REJECTED TAKEOFF, SUSPECT COMPRESSOR STALL. MAINTENANCE PERFORMED A BORESCOPE INSPECTION IAW T/C I5M72008, NO DAMAGE NOTED. REMOVED AND REP
Back to Pratt & Whitney JT8D-15