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 02FDEA00849Floorbeam · corrodedCORROSION ON BS 1090 FLOORBEAM LOWER CHORD AT NUTPLATE HOLES, RBL 21, WL 200. REMOVED AND REPLACED FLOORBEAM IAW SRM.SDR 02FDEA00845Skin · corrodedCORROSION ON SKIN AT BS 686, WL 147, STR 28R. SKIN WAS FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED SKIN.SDR 02FDEA00846Stringer Clip · corrodedCORROSION ON STR CLIP AT BS 680, STR 26R. STR CLIP WAS FOUND TO BE OUT LIMITS IAW SRM.SDR 02FDEA00854Shear Tie · corrodedCORROSION AT BS 950E+4 BETWEEN STR 28 & 29R. REPAIRED SHEAR TIE IAW SRM.SDR 02FDEA00856Frame · corrodedCORROSION ON FRAME AFT SIDE OF SHEAR TIE AT BS 1030, WL 148, RBL 5. REPAIRED IAW SRM.SDR 02FDEA00847Doubler · corrodedCORROSION ON SKIN DOUBLER BS 680, STR 27R, WL 147. CORROSION WAS FOUND TO BE OUT OF LIMITS AT BS 680, STR 27R, WL 147. REPAIRED AREA IAW EA AND SRM.SDR 02FDEA00853Shear Tie · corrodedCORROSION ON SHEAR TIE BS 950C AFT SIDE OF FRAME JUST OUTBOARD OF STR 29L. CORROSION ON SHEAR TIE AT BS 950C O/B OF STR 29L WAS FOUND OUT OF LIMITS REPAIRED SHEAR TIE IAW FEDEX EA AND SRM.SDR 02FDEA00833Floorbeam · corrodedCORROSION ON LOWER CHORD OF BS 950D AT NUTPLATE HOLE RBL 14-40, WL 200. REPAIRED LOWER CHORD OF FLOORBEAM AT BS 950 RBL 14-40. ALL WORK DONE IAW SRM.SDR 03FDEA00020Bulkhead · crackedGENERATED DUE TO NOSE LANDING GEAR DOWNLOCK ACTUATOR FITTING CRACKED. UPON REPLACEMENT OF SUPPORT, FOUND NOSE LANDING GEAR AFT BULKHEAD WEB AND CHANNEL SUPPORT CRACKED. WEB REPAIR WAS ACCOMPLISHED IAW EA NR 7-5310-64754.SDR 02FDEA00827Floorbeam · corrodedCORROSION ON UPPER SURFACE OF FLOORBEAM AROUND FLOOR BOARD HOLES AT BS 360, LBL 6 - RBL 6, WL 208. INSTALLED REPAIR AT LBL 7 BS 360 IAW SRM.SDR 02FDEA00851Keelbeam · damagedCOMPLY WITH EO REV C1 PT5 KEELBEAM CHORD REPAIR BS 980-1007, STR 29L. REPAIRED KEELBEAM BS 980-1007, STR 29L IAW EO.SDR 02FDEA00828Floorbeam · corrodedCORROSION ON TRANSVERSE FLOORBEAM AT BS 900, LBL 65, WL 205. REMOVED AND REPLACED FLOORBEAM IAW EA AND SRM.SDR 02FDEA00829Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 680, STR 10R. REMOVED AND REPLACED STRINGER CLIP IAW SRM.SDR 02FDEA00832Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 660, STR 1. REMOVED AND REPLACED STRINGER CLIP IAW SRM.SDR 02FDEA00830Floorbeam · corrodedFLOORBEAM SURFACE CORROSION OUT OF LIMITS. REMOVED AND REPLACED FLOORBEAM IAW SRM.SDR 02FDEA00855Frame · corrodedCORROSION ON LOWER FRAME BS 700, STR 28-27R. REMOVED CORROSION, FOUND OUT OF LIMITS, REMOVED SHEAR TIE, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM AND EA.SDR AUS20021295Pump · overheated(AUS) NR 1 HYDRAULIC PUMP OVERHEATED.SDR AUS20021296Pump · overheated(AUS) NR 1 HYDRAULIC PUMP OVERHEATED.SDR CA021108022Apu · failed(CAN) ON APPROACH, APU WAS STARTED AS NORMAL. SHORTLY AFTER START UP A VIBRATION WAS FELT THROUGHOUT THE AIRFRAME. AUTO SHUTDOWN OF THE APU OCCURRED,AS WELL AS A FIRE WARNING IN THE COCKPIT. APU FIRE QRC WAS ACCOMPLISHED WITH ASSOCIATED FIRE HANDLE PULLED AND SDR F3LA200200384Stud · looseDURING CLIMBOUT, THE FLIGHT CREW REPORTED THE NUMBER ONE ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED AND OIL QUANTITY WAS SHOWN AT ZERO. THE AIRCRAFT RETURNED TO ITS DEPARTURE AIRPORT. MAINTENANCE FOUND A LOOSE STUD ON THE MAIN OIL FILTER. THE STUD HOLE WAS HSDR 02FDEA00850Skin · corrodedCORROSION ON SKIN BS 720C+1 BETWEEN STR 28L-28R. REPAIRED SKIN BS 720C+1, STR 28L-28R IAW EA.SDR DHL2002746008Bleed Valve · malfunctionedNR 3 ENGINE COMPRESSOR. REJECTED TAKEOFF. WOULD NOT MAKE T/O THRUST AND WAS COMPRESSOR STALLING. REPLACED NR 3 ENGINE PRBC VALVE PER M/M 75 -30-1. GROUND RAN PER DHL JRH SATISFACTORY. WT. 127.7, IAS 60 KTS, 15 DEGREES OAT, 1150 PRESS ALT.SDR C7WA200200034Oil Cooler · faultyAFTER TAEKOFF, NR 1 ENGINE OIL TEMPERATURE WENT INTO YELLOW ARC (APPROX 126) AND STAYED THERE. HIGH OIL TEMP ABNORMAL CHECKLIST ACCOMPLISHED. AFTER 15 MINUTES OF OIL TEMPERATURE IN YELLOW BAND PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED AS PER CHECKLIST. HIGSDR AUS20021195Bearing · disintegrated(AUS) NO2 MAIN WHEEL OUTER BEARING COLLAPSED. WHEEL SEPARATED FROMAIRCRAFT LEAVING THE WHEEL NUT STILL SECURE ON THE AXLE. DAMAGE TO AXLE SLEEVE.SDR ASAA0280370Connector · looseDURING PREFLIGHT CHECK, FOUND EMERGENCY TRACK LIGHTS IN 1ST CLASS CABIN, INOPERATIVE. REATTACHED LOOSE CONNECTORS. LIGHTS THEN OPERATED PROPERLY.SDR AW32002F00000Bulb · burned outDURING POST FLIGHT, FOUND LT WING CENTER EMERGENCY LIGHT INOPERATIVE. RELAMPED LT OVERWING EMERGENCY LIGHT. SYSTEM OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0253201Structure · gougedCUTOUT DAMAGE, PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER, TRIPLER STRUCTURAL FILLER. AIRCRAFT RETURNED TO SERVICE.SDR AUS20021207Floorbeam · corroded(AUS) FLOORBEAM UPPER T CHORD LOCATED AT STA 460 CORRODED. FOUND DURING CPCP INSPECTION.SDR DL72S021146Warning System · malfunctionedON T/O ROLL, SPEED LESS THAN 60KTS, T/O POWER ESTABLISHED 1.94 EPR. THE NR 3 THRUST REV OPERATING LIGHT ILLUMINATED. T/O DISCONTINUED. AFTER CLEARING RUNWAY WITH ENGINE AT IDLE POWER THRUST REV OPERATING LIGHT WENT OUT. T/S THRUST REV OPERATING LIGHT SWITCSDR TSAA0253202Flap Track · damagedFLAP TRACK ATTACHMENT FITTING HOLE ELONGATED. REPAIRED AND AIRCRAFT RETURNED TO SERVICE.SDR 02FDEA00624Warning Light · illuminatedLOUD BOOM & AIRFRAME SHUDDER EXPERIENCED ON CLIMBOUT, AUTOPACK TRIP ACTIVATED. ENGINE FAIL LIGHT BLINKED MOMENTARILY, BUT STAYED OUT. SUSPECT COMPRESSOR STALL BUT UNABLE TO IDENTIFY ENG. ALL ENG INSTRUMENTS NORM. BORESCOPED ENGINES 1, 2, 3 PER MM 72-00-00-SDR GAIA02080STSkin · dentedDURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD LOWER CARGO DOOR CUTOUT FRAME AND SKIN WAS DENTED NEAR STRINGER S23R AT THE FORWARD PORTION OF THE DOOR CUTOUT FRAME (FUSELAGE SKIN). C/A: ACCOMPLISHED REPAIR IAW REPAIR ORDER. AIRCRAFT WAS RETSDR CA020904009Indicator · failed(CAN) DURING APPROACH, PILOT OBSERVED A SPLIT FLAP INDICATION. AIRCRAFT LANDED WITHOUT INCIDENT. FLAP POSITIONING INDICATOR REPLACED AND CHECKED SERVICEABLE IAW MM 27-50-00. 4. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT.SDR MEX2002268Controller · failedAIRCRAFT MADE A TECHNICAL STOP IN TRC DUE TO PRESSURIZATION TROUBLES. CABIN PRESSURE CONTROLLER WAS RESEATED, TESTS OK.SDR CA020814002Accessory Unit · failed(CAN) AFTER TAKE-OFF, CREW SELECTED GEAR HANDLE TO THE RETRACT POSITION. NO JOY UNTIL OVERRIDE TRIGGER INITIATED. AIRCRAFT RETURNED TO BASE & LANDED WITHOUT INCIDENT. LANDING GEAR ACCESSORY UNIT REPLACED & CHECKED SERVICEABLE IAW MM 32-10.4. NO FURTHER SDR TSAA0251186Skin · crackedRT BS 1129 AND BS 1138 FUSELAGE SKIN CRACKS LOCATED AT S5R AND S12R. TRIMMED OUT CRACKS MAINTAINING A MINIMUM TRIM OUT CORNER RADIUS .050 INCHES AT A SURFACE FINISH OF 63 RMS OR SMOOTHER. PERFORMED HFEC INSPECTION AROUND TRIMOUT AREA, NO DEFECTS NOTED. FABRSDR FX72002F00003Engine · flamed outAFTER CRUISING AT FLIGHT LEVEL 33. IN ICE CONDITIONS, WITH ENGINE ANTI-ICE ON. NR 2 ENGINE EPR AND AND FUEL FLOW OSCILLATED (EPR BETWEEN 1.7 AND 1.4), (FUEL FLOW 2500-1200). AFTER 20 MINUTES OUT OF ICE CONDITIONS AND COMMENCING DESCENT AFTER POWER REDUCTION, SDR MYW2002F00002Battery Pack · inoperativeDURING PREFLIGHT TRANSIT FOUND CEILING EMERGENCY EXIT LIGHTS AT ROW 19, INOPERATIVE. TROUBLE SHOT SYSTEM, REMOVED AND REPLACED BATTERY PACK IN CEILING, OPS CHECKED SATISFACTORY IAW MM. RETURNED AIRCRAFT TO SERVICE.SDR ABXA020059Fuel Control · malfunctionedNR 1 ENGINE WOULD NOT DECELERATE FROM FULL POWER TO IDLE, WOULD NOT RESPOND AFTER THE THROTTLE WAS RETARDED. IN-FLIGHT SHUTDOWN AND DID AN AIR TURN BACK. REPLACED THE FUEL CONTROL AND MAIN FUEL PUMP IAW DC-9 MM 73-20-01-2.SDR 0202302702Pump · damagedDURING APPROACH FOR LANDING, THE NR 2 ENGINE FLAMED OUT. AIRCRAFT COMPLETED LANDING WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE FUEL PUMP. OPERATIONAL CHECK OK. AIRCRAFT RETURNED TO SERVICE.SDR 02FDEA00474Relief Valve · out of adjustNR 2 OIL PRESSURE READ 60 PSI DURING INITIAL CLIMBOUT. AFTER REACHING 5K NR 2 THROTTLE PULLED TO IDLE IAW RED TAB PROCEDURE. OIL PRESSURE DROPPED TO 58 PSI INITIALLY THEN SLOWLY DROPPED INTO GREEN BAND APPROX 52 PSI AT IDLE AND REMAINED THERE DURING APPROACHSDR 2002UALA01143Skin · damagedFORWARD LOWER FUSELAGE SKIN, BODY STATION 312-328, DRAIN HOLE AFT OF NOSE LANDING GEAR WHEEL WELL IS PUNCTURED AND BROKEN OUT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR AUS20021035Rib · corroded(AUS) WING RIB CONTAINED GALVANIC CORROSION IN AREA OF LE WS 277.5. FOUND DURING CPCP INSPECTION.SDR 2002UALA01117Stringer · corrodedFORWARD CARGO PIT AT BODY STATION 480, STRINGER 27L IS CORRODED BEYOND LIMITS. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICE REPAIR.SDR 2002UALA01118Stringer · corrodedFORWARD PIT STRINGER 27R CORRODED BEYOND LIMITS BODY STATION 630. MAJOR REPAIR ACCOMPLISHED. HAT SECTION REPAIR.SDR 2002UALA01099Stringer · corrodedFORWARD PIT STRINGER 28R CORRODED ON LOWER SIDE AT BODY STATION 494. MAJOR REPAIR ACCOMPLISHED. SPLICE REPAIR.SDR 2002UALA01100Skin · corrodedFORWARD PIT INTERNAL SKIN STATION 500 AT STRINGER 28R IS BLENDED BEYOND LIMITS DUE TO CORROSION REMOVAL. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL DOUBLER REPAIR.SDR 2002UALA01101Shear Tie · corrodedFORWARD CARGO PIT AT BODY STATION 480-500, STRINGER 28R, INTERCOSTAL LOWER FLANGE IS CORRODED AND SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED INTERCOSTAL LOWER FLANGE & SHEAR TIE.SDR 2002UALA01082Doubler · damagedSLIGHT EDGE DAMAGE TO REPAIR DOUBLER FOUND UNDER AFT PIT BELOW LOADING THRESHOLD. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND QUADRUPLER.SDR 2002UALA01083Frame · corrodedAFT PIT FRAME AT BODY STATION 950F BETWEEN STRINGER 27L AND 28L, FRAME AND SHEAR TIE CORRODED. MAJOR REPAIR ACCOMPLISHED. REPAIRED SHEAR TIE.
Back to Pratt & Whitney JT8D-15