Pratt & Whitney JT8D-17
Service difficulty reports · 1,680
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 = 'JT8D17' 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 = 'JT8D17' 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 CA060309003Turbine Blades · failed(CAN) ON START UP THE CREW WAS UNABLE TO SUCCESSFULLY START THE NR 2 ENGINE. LARGE PIECES OF TURBINE BLADES WERE DISCOVERED LAYING IN THE TAILPIPE AREA. THE ENGINE WAS REPLACED AND A/C RETURNED TO SERVICE. (TC NR 20060309003)SDR C7WA200600002Turbine Blades · failedAT FLIGHT LEVEL 260 NR 3 ENGINE EXPERIENCED SEVERAL COMPRESSOR STALLS, ENGINE RPM DECREASED AND EGT WENT HIGH. SHUTDOWN ENGINE. INSPECTION OF NR 3 ENGINE REVEALED THE 9TH STAGE TURBINE DISK BLADE ASSY FAILED. REMOVED AND REPLACED NR 3 ENGINE. (K)SDR 0600399869Actuator · leakingDURING CRUISE THE RT HYDRAULIC SYSTEM QUANTITY DROPPED TO 1 QUART. COM PROCEDURES COMPLIED WITH AND THE CREW DEACTIVATED SOME RT HYDRAULIC SYSTEM COMPONENTS WHICH INCREASED THE QUANTITY TO 6 QUARTS. ON APPROACH WHEN THE RT SYSTEM WAS REACTIVATED THE QUANTITY WSDR C8GA20060001Engine · activatedFLT 737 FROM MMMY TO TOL. WHILE CLIMBING THRU 10,000 FEET NUMBER ONE ENGINE LOW OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN, EMERGENCY WAS DECLARED, AIRCRAFT WAS DIVERTED TO LRD AND LANDED WITHOUT INCIDENT. ENGINE WAS INSPECTED AND METSDR 1HA200681002Line · crackedDURING FLIGHT THE NR2 (B) SYSTEM HYDRAULIC LOW PRESSURE LT ILLUMINATED FOLLOWED BY THE B SYSTEM NR 1 LOW PRESSURE LT ILLUMINATING AND LOSS OF B SYSTEM HYDRAULIC PRESSURE , THE B SYSTEM QUANTITY GUAGE INDICATED FULL THE ENTIRE FLIGHT. HYDAULIC BRAKE PRESSURE SDR 0601046Skin · dentedREPAIRED NONPRESSURIZED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS.SDR 0601039Window Frame · corrodedREPAIRED FUSELAGE WINDOW FRAME AT TWO LOCATIONS, FROM B/S 688 TO 703.25, AND FROM B/S 727+3 TO 727+18.25, DUE TO CORROSION.SDR 0601043Skin · damagedREPAIRED FUSELAGE SKIN DUE TO SCRIBE LINES DAMAGE.SDR 0601047Skin · dentedREPAIRED APU DOOR NONPRESSURIZED OUTER SKIN AT 2 LOCATIONS, FROM B/S 1098.5 TO 1108, AND FROM B/S 1113.5 TO B/S 1129.5 AT CENTER SECTION, DUE TO DENTS OUT OF LIMITS.SDR 0601048Skin · elongatedREPLACED RT WING TO NR 2 ENGINE AFT FAIRING IB SKIN PANEL DUE TO ELONGATED HOLES.SDR 0601032Floorbeam · corrodedREPAIRED FUSELAGE MAIN CARGO CABIN FLOORBEAM UPPER CHORD DUE TO CORROSION.SDR 0601035Skin · dentedREPAIRED FUSELAGE SKIN SECTION DUE TO DENT OUT OF LIMITS.SDR 0601033Floorbeam · corrodedREPAIRED FUSELAGE MAIN CARGO CABIN FLOOR BEAM UPPER CHORD DUE TO CORROSION.SDR 0601034Web · corrodedREPAIRED FUSELAGE MAIN CARGO CABIN LOWER JAMB FLOOR WEB DUE TO CORROSION.SDR 0601038Fitting · damagedREPAIRED FUSELAGE MAIN CARGO CABIN FITTING UNDERNEATH LONGITUDINAL FLOOR BEAM DUE TO MISSING MATERIAL.SDR ASAA0610002Skin · cracked1.5 INCH CRACK IN FUSELAGE LT SIDE, BSTA 727B-747 JUST BELOW BLUE PAINT LINE 32 INCHES BELOW WINDOW. (S16L) REPAIRED IAW SRM. (K)SDR ASAA0610001Frame · dentedDENT IN FUSELAGE SKIN AT BSTA 927-947.5 BETWEEN STRINGERS 18 AND 19 LT. REPAIRED IAW SRM. (K)SDR SPAA0500082Battery Pack · intermittentCENTER OVERHEAD EMERGENCY EXIT LIGHT STAYS ON ONLY BRIEFLY. REPLACED CENTER OVERHEAD EMERGENCY EXIT LIGHT BATTERY CHARGER IAW MM 33-51-81. GROUND CHECK NORMAL IAW MM 33-51-11.SDR ASAA0510354Attach Fitting · crackedDURING L/E LUBE W/C 18412001, FOUND NR 5 L/E SLAT IB SLAT TRACK ATTACH FITTING CRACKED AT MOUNT EAR PN 69-40609-1. REPLACED ATTACH FITTING WITH 69-40609-3 IAW EA TO COMPLY WITH EM 5740-01458 AND AD 2005-20-16. (K)SDR SPAA0500081Structure · crackedCRACK ON BS1156 OUTER CHORD RT SIDE WL270. REPAIRED CRACK IAW SB 737-53-1086.SDR SROM200500016Skin · crackedDURING ROUTINE MAINTENANCE FOUND A 3 INCH CRACK IN THE FUSELAGE SKIN AT BS 973, STR 21L. INSTALLED TEMPORARY REPAIR DOUBLER IAW 8110-3 APPROVED REPAIR, REFERENCE DWG 33-05565-1.SDR SROM200500017Spindle · crackedDURING ROUTINE NDT INSPECTION OF OB FLAP SPINDLE IAW AD 2003-24-08 AND SB 737-57A1277 FOUND A FLAP CARRIAGE SPINDLE CRACKED 40 PERCENT AT THE RADIUS OF THE YOKE TO THE FIRST BEARING LAND. FLAP CARRIAGE ASSEMBLY REPLACED WITH A NEW UNIT. RECORDS INDICATE 5221 SDR AU510001492Skin · corrodedCABIN WING CENTER SECTION UPPER SKIN PANEL CORRODED. PANEL IS LOCATED AT FS 822 RBL12.SDR AU510001527Pressure Panel · corrodedFUSELAGE STRUCTURE PRESSURE WEB CORRODED. WEB IS LOCATED AT FS 46 IN THE MAIN LANDING GEAR WHEEL WELL.SDR AU510001528Bear Strap · corrodedNR 3 CARGO DOOR BEAR STRAP INNER SURFACE CORRODED.SDR BJNA051202Power Supply · inoperativeLT OVERWING EXTERIOR EMERGENCY EXIT LIGHT, INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY AND BATTERY. (K)SDR BJNA051201Connector · dirtyEMERGENCY EXIT LIGHT ILLUMINATED 2 TIMES ON DESCENT. CLEANED THE CONNECTORS ON THE COCKPIT REMOVABLE EMERGENCY EXIT LIGHT, SYSTEM CHECKS NORMAL. (K)SDR C1HA200594011Cap · looseDURING CLIMB-OUT DFW, NR 1 ENGINE OIL QUANTITY INDICATED CONSTANT DECREASE OIL. LANDED WITH 1.0 GALLONS OIL RETURNED DIRECT, UPON LANDING WITNESSED OIL LEAKING FROM COWLING. FOUND OIL CAP NOT ENGAGED. SERVICED ENGINE INSTALLED NEW OIL CAP REF 12-13-01.SDR BJNA051101Landing Gear · unknownAFTER TAKEOFF, RETRACTED LANDING GEAR AND 3 RED LIGHTS REMAINED ILLUMINATED. CYCLED LANDING GEAR DOWN AND UP, 3 GREEN LIGHTS WHEN DOWN, 3 RED LIGHTS WHEN UP. LANDED WITH 3 GREEN LIGHTS. PERFORMED LANDING GEAR ACCY MODULE TEST IAW AMM, COULD NOT DUPLICATE ONSDR PCSA11030501Engine · vibrationWHILE IN CRUISE, CREW REPORTED VIBRATION ON THE CENTER CONSOLE, WHEN NR 1 ENGINE THROTTLE WAS PULLED BACK VIBRATION SEEMS TO DIMINISH. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ALL 3 ENGINES, INTAKES, AND EXHAUST, NO DAMAGE FSDR PCSA10120501Engine · overheatedAFTER DEPARTURE ENGINE NR 3 OIL TEMPERTURE INCREASED TO 160, PERFORMED ALTERNATE PROCEDURE, NO HELP. SHUT DOWN ENGINE, DUMPED FUEL TO LAND. MX INSPECTED INLET & EXHAUST OF NR 3 ENGINE; INLET OK, EXHAUST SHOWS EVIDENCE OF OIL LEAK, SUSPECT NR 6 BEARING SEAL. SDR C8GA20050022Line · leakingWHILE IN CRUISE AIRCRAFT EXPERIENCED A LOSS OF NR 2 ENGINE OIL QTY DOWN TO TWO GALLONS. ENGINE WAS SHUTDOWN AS A PRECAUTIONARY. EMERGENCY WAS DECLARED, AIRCRAFT WAS DIVERTED AND LANDED WITHOUT INCIDENT. FOUND LOOSE OIL LINE ON NR 2 ENGINE GEARBOX, SECURED LINESDR 0501529941Valve · leakingDURING FINAL APPROACH ENGINE NR 2 ROLLED BACK TO 30 PERCENT N2 AND WOULD NOT RESPOND TO THROTTLE INPUT. ENGINE NR 2 WAS SHUTDOWN AND FLIGHT CREW PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND A FUEL LEAK AT P&D VALVE COUPLING. MAINTENANCE REPLACED ENGINSDR AU510001744Bearing · collapsedGROUND SPOILER QUADRANT UPPER AND LOWER BEARINGS COLLAPSED. SPOILER DIFFERENTIAL MIXER P/N 10-60841-8 ROUGH IN OPERATION.SDR DHL2005781004Stabilizer · out of adjustAIRCRAFT ROTATES 15 KTS BEFORE VR AND THEN REQUIRES 1.0 UNIT DOWN TRIM TO MAINTAIN V2 +10 ON CLIMBOUT.SDR ASAA0510326Failsafe · corrodedCORRODED FAIL SAFE ANGLE AT BSTA 967, BETWEEN STRINGER 27 LT AND 27 RT IS CORRODED. BSTA 967 BETWEEN STRINGER 27 RT AND 27 LT FAIL SAFE ANGLE REPAIRED IAW SRM. (K)SDR ASAA0510325Seat Track · corrodedPASSENGER CABIN BSTA 570-540, NR2 FLOOR PANEL FROM LT SIDE, RT SIDE SEAT TRACK BEAM UPPER AND LOWER AREAS HAVE CORROSION. CORRODED SEAT TRACK AND SEAT TRACK BEAM REPAIRED IAW SRM. (K)SDR ABXA050235Engine · defectiveLEFT ENGINE WOULD NOT SPOOL UP DURING APPROACH. WHEN THROTTLE WAS ADVANCED, ENGINE WOULD NOT START, COMPRESSOR STALLED. EMERGENCY DECLARED. LANDED WITH ENGINE AT IDLE POWER. SERVICED FUEL CONTROL UNIT WITH 6 ML OF SILICON OIL IAW P&W JT8D-11 MM 73-21-01. SDR ASAA0510324Clevis · corrodedCORROSION ON VERTICAL STABILIZER AFT SPAR LT FAIL SAFE CLEVIS FACES NOT PARALLEL TO EACH OTHER. FACES MACHINED IAW EA. (K)SDR MYW2006F00000Wire · burnedDURING FLIGHT, ALL 8 RT READING STATION CB`S POPPED SIMULTANEOUSLY. PA INOPERATIVE ALL STATIONS. NO SMOKING CB POPPED, PASSENGER AND CREW CALL CB POPPED. ATTEMPTED TO RESET CB`S IAW AOM PROCEDURES. CB`S IMMEDIATELY POPPED. DID NOT ATTEMPT TO RESET, AGAIN.SDR ASAA0510318Floorbeam · corrodedFOUND EXFOLIATION CORROSION FOUND ON UPPER CHORD OF FLOORBEAM AT BS 328, FROM BL 0 -RBL 56. CHORD REPLACED IAW SRM 53-10-9.SDR ASAA0510300Stringer Clip · puncturedFWD TIE CLIP AT BSTA 500 STR 19 RT FOUND PUNCTURED. REPLACED TIE CLIP AT BSTA 500, STR 19 RT WITH NEW REPAIR IAW SRM. (K)SDR ASAA0510301Intercostal · crackedINTERCOSTAL WEB FOUND CRACKED AT BSTA 295, STR 8 LT. CRACKED INTERCOSTAL WEB AT BSTA 295 AND STR 8 LT REPAIRED, EO. (K)SDR 05FDEA02842Case · crackedNR 2 ENG RT FWD FAN FRAME CASE HAS SEVERAL CRACKS. DYE PENETRANT INSPECTION DONE IAW SOPM 20-20-02 FOUND 1EA CRACK AT 3 O'CLOCK POSITION. CRACK STILL WITHIN LIMITS IAW PW JT8D MM72-00-00. STOP DRILLED CRACK IAW PW JT8D MM 72-00-00. REINSPECT CASE EVERY 200SDR 05FDEA02503Drain Line · crackedNR 1 ENGINE FUEL FEED SHROUD DRAIN LINE IS CRACKED STA 870 LT MLG WW. REMOVED AND REPLACED DRAIN LINE IAW MM 20-10-005-4.SDR C7WA200500111Landing Gear · malfunctionedAIR RETURN, UNABLE TO RETRACT MAIN LANDING GEAR. PERFORMED GEAR SWING AND MANUAL EXTENSION OF LANDING GEAR IAW MM. MAIN LANDING GEAR OPERATES NORMAL, NO DEFECTS NOTED. (K)SDR CA050718008Fire Loop · failedDURING CLIMB AT FL120, NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED AND ASSOCIATED WARNING HORN SOUNDED INTERMITTENTLY. CREW FOLLOWED ENGINE FIRE EMERGENCY CHECKLIST SECURED ENGINE AND FIRE EXTINGUISHER BOTTLES WERE ACTIVATED. ENGINE FIRE INDICATION REMAINED, SDR DHL2005783002Uplock Sensor · malfunctionedFOUND RT MLG RED LIGHT ILLUMINATED. CLEANED CONTACTS ON RT MLG DOWNLOCK SWITCHS SYS OPS CHECKED BAD ON GROUND IAW B727 M/M R & R RT MAIN GEAR UPLOCK SENSOR OPS CHECK OK IAW MM 32-61-81. P/N 1-899-29.SDR PCSA6210501Oil System · leakingDURING CRUISE NR 3 ENGINE OIL TEMP WAS BETWEEN 125 & 130 DEG FOR 15 MINUTES. PERFORMED ALT PROCEDURES, RETARDED THROTTLE, DIDN'T HELP. SHUTDOWN NR 3 ENGINE, ENGINE WINDMILLED FOR 45 MIN. OIL PRESSURE STAYED ABOVE 25 PSI. DIVERTED & LANDED AT SJU. MX INSPESDR ASAA0510174Stringer Clip · corrodedAFT CRGO B-STA 747, STR 22L TIE CLIP CORRODED. REMOVED AND REPLACED TIE CLIP IAW SRM. (K)
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