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 03FDEA00178A/C Pack · contaminated5 MIN. AFTER T/O R/PACK OVERHEAT LIGHT ILLUM'D. PACK COOLING FLAP SELECTOR IN AUTO. PACK TEMP APPROX. 180 DEG. ,SHUT DOWN PACK, TEMP DECREASED. FOLLOWED BY NR 6 MAIN SMOKE CARGO LIGHT AND FIRE WARN GLARESHIELD LIGHTS. HORN ILLUMINATED, FOLLOWED BY NR4 THENSDR CA030321011Control Unit · misoverhauled(CAN) UNSCHEDULED REMOVAL OF RUDDER PCU, OCCURRED ON FEB 25/26/2003 WAS IN RESPONSE TO A REQUEST FROM MATERIAL SERVICES BASED ON A FAA UNAPPROVED PARTS NOTIFICATION NR 2001-0089 DATED AUG 12,2002. SUSPECT PCU P/N 1U1150-3 S/N 737 WAS LISTED IN THE NOTIFICATIONSDR BJNA030216Fitting · corrodedDURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND IN THE BORES OF THE HORIZONTAL STABILIZER CENTER SECTION FORWARD TERMINAL FITTINGS UPPER AND LOWER AFT LUGS. THE BORES WERE REAMED TO THE MAXIMUM DIAMETER (1.125 INCH) SHOWN IAW SB. AFTER REAMING INSPECTION SSDR KNNA200300001Skin · crackedAIRCRAFT AT MAINT. BASE FOR "A3" CHECK COMPLIANCE. IN C/W TASK CARD A-07A A 1.8 INCH CRACK WAS FOUND IN EXTERIOR FUSELAGE SKIN AT LT BS 757 BELOW STR 17. A NON-ROUTINE T030446 AND ACO 035313R00 WAS ISSUED TO DOCUMENT SRM REPAIR CH 53-30-3 FIG 25. CRACK IN SKSDR CA030225003Oxygen Mask · misinstalled(CAN) A/C EXPERIENCED RAPID DEPRESSURIZATION. CLIMBED TO 15,000 FT IN APPROX 5-10 SECONDS. O2 SYS DEPLOYED AUTOMATIC. STANDBY MODE DID NOT OPERATE NORMALLY BUT CABIN PRESSURE WAS RECAPTURED. DURING EMER DESCENT WITH MANUAL MODE MAINT REPLACED CABIN PRESSURSDR 03FDEA00148Actuator · inoperativeA/C AIR TURNBACK DUE TO NR 6 LEADING EDGE FLAP LIGHT INDICATION, WOULD NOT GO GREEN. ON FRONT PANEL AND S/O STATION. RED TAB PROCEDURES TO NO AVAIL. REMOVED AND REPLACED NR 6 LEADING EDGE FLAP POSITION INDICATING SWITCH IAW M/M 27-82-001-4, OK FOR SERVICE.SDR 03FDEA00151Actuator · malfunctionedAMBER LEADING EDGE FLAPS LIGHT REMAINED ILLUMINATED ON CLIMBOUT AFTER SELECTED FLAPS 2. SECOND OFFICER AUX PANEL SHOWED SLAT 7 AMBER LIGHT ILLUMINATED. QRH PROCEDURES CONDUCTED UNSUCCESSFULLY. FLAPS EXTENDED NORMALLY IN ALL OTHER POSITIONS. REMOVED AND REPSDR CA030224003Fire Loop · malfunctioned(CAN) CREW REPORTED, AT CRUISING ALTITUDE, 20 MINUTES OUT OF YLW THEY EXPERIENCED A VIBRATION FOLLOWED BY AN APU FIRE WARNING. CREW SHUTDOWN APU WITH THE FIRE HANDLE AND APU FIRE BOTTLES WERE DISCHARGED. A/C COMPLETED AN (ABNORMAL LANDING CONFIGURATION) IN YLSDR CA030220009Hose · ruptured(CAN) AFTER SELECTING LANDING GEAR UP ON CLIMB, WARNING RED/GREEN NOSE GEAR LIGHTS ILLUMINATED. CONTACTED MCC AND WERE ADVISED TO LOWER GEAR AND CONTINUE TO MAINT BASE. FUEL REMAINING WAS NOT SUFFICIENT AND ELECTED TO RETURN. NOTICED SYSTEM "A" HYDRAULICSSDR FX72003F00001Indicator · failedDURING THE BEFORE TAKEOFF CHECK OF THE ELEVATORS, THE LEFT ELEVATOR POSITION INDICATION FAILED AIRCRAFT RETURNED TO GATE. FLIGHT MECHANIC VERIFIED CORRECT OPERATION OF ELEVATORS IAW MEL 27-10 OF THE DDPG. AIRCRAFT WAS RETURNED TO SERVICE WITH NO FURTHER INCISDR BJNA03025Floor Support · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON A FLOOR SUPPORT ANGLE LOCATED AT BS 285, BL 12L, WL 208.1. REMOVED CORRODED SECTION, FABRICATED AND INSTALLED A REPLACEMENT FLOOR SUPPORT ANGLE FROM BAC 1510-335 EXTRUSION. DIMENSION OSDR 03FDEA00109Warning Light · illuminatedNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT DURING CLIMBOUT. COMPLETED PROCEDURES IAW QRH. LIGHT EXTINGUISHED AFTER NR 3 BLEED CLOSED - R PACK OFF - NR 3 THRUST LEVER TO IDLE. NR 3 THRUST LEVER RESTORED WITH NO REOCCURANCE. ***S/D COMING ****SDR BJNA03024Support Bracket · corrodedDURING A SCHEDULED MAINTENANCE VISIT, LEVEL 2 CORROSION WAS DISCOVERED ON AN APU BLEED AIR SUPPORT BRACKET LOCATED IN THE AFT PIT ACCESSORY COMPARTMENT AT STA 1016. REMOVED AND REPLACED THE CORRODED SUPPORT BRACKET IAW SRM.SDR CA030204001Control Panel · smoke(CAN) AT 33000 FT, SMOKE WAS NOTICE COMING FROM THE OVERHEAD COCKPIT FUEL PANEL P5-2. PUMPS SELECTED OFF. DECLARED AN EMERGENCY LANDING. REPLACED PANEL.SDR C1HA200394005Compressor · stalledDURING TAXI, ENGINE NR 2 EXPERIENCED A COMPRESSOR STALL/ PERFORMED COM 2.72.13. INSPECTED NR 2 ENGINE INLET & EXHAUST PER P&W MM 72-00-00 NO DEFECTS NOTED. OPERATED ENGINE TO 1.85 EPR. ALL PARAMETERS NORMAL.SDR AUS20030041Floorbeam · corroded(AUS) FUSELAGE FLOORBEAM LOCATED AT BS 1130 LBL 71 AND RBL 71 CORRODED.SDR AUS20030042Skin · corroded(AUS) WING CENTRE SECTION LOWER SKIN CORRODED AT BS 840 LBL30, WL168.SDR AUS20030043Floorbeam · corroded(AUS) FUSELAGE FLOORBEAM CORRODED AT BS 1110 LBL 68 AND RBL 68 WL 208.SDR AUS20030044Floorbeam · corroded(AUS) FLOORBEAM CORRODED AT BS 950 AND RBL 70.SDR AUS20030045Floorbeam · corroded(AUS) FLOORBEAM CORRODED AT BS 1030 FL AND RBL 70.SDR AUS20030046Skin · corroded(AUS) WING CENTRE SECTION LOWER SKIN CORRODED AT BS 800 LBL20, WL168.1.SDR AUS20030047Floorbeam · corroded(AUS) FLOORBEAM CORRODED AT BS 72 LBL 65 AND RBL 65.SDR AUS20030048Floorbeam · corroded(AUS) FLOORBEAM CORRODED AT BS 620 LBL 62 AND RBL 62.SDR AUS20030049Floorbeam · corroded(AUS) FLOORBEAM CORRODED AT BS 870 LBL 65 AND RBL 65.SDR AUS20030050Wing · delaminated(AUS) LH WING DELAMINATED.SDR AUS20030051Skin · delaminated(AUS) INBOARD FORE FLAP LOWER SKIN DELAMINATED.SDR AUS20030052Skin · delaminated(AUS) INBOARD FORE FLAP LOWER SKIN DELAMINATED.SDR CA030205011Strut · overserviced(CAN) AFTER TAKE OFF, NOSE GEAR DID NOT STOW. OLEO DID NOT EXTEND FULLY OR MADE CONTACT WITH SNUBBERS. THRUST REVERSER ISOLATION VALVE LIGHT ILLUMINATED. GEAR WAS CYCLED WAS NORMAL. MAINT FIRST CHECKED NOSE OLEO SERVICING AND DISCOVERED OLEO TO BE OVERSERVSDR 03FDEA00042Indicator · erraticON TAKEOFF ROLL, JUST PRIOR TO V1, ALL 3 FUEL FLOW INDICATIONS BECAME ERRATIC. AFTER TAKEOFF ALL 3 FUEL FLOW INDICATORS WERE READING APPROX CORRECT BUT FLUCTUATIONS +/- 2000 LBS. AFTER 10 MINUTES ALL THREE FUEL FLOW GAUGES BECAME COMPLETELY ERRATIC AND UNUSASDR C1HA200394003Engine · stalledUPON LANDING NR 3 ENGINE COMPRESSOR STALLED AT 85 KTS 1.8 TO 1.85 EPR. RAN ENGINE PER CHECKLIST AT 70 PERCENT N1 15 SECONDS ALL INDICATIONS APPEAR NORMAL. LUBED NR 3 ENG PRESSURE BELLOWS. INSP INLET AND EXHAUST, NO DEFECTS (REF73-00-00). RAN ENGINE AT PWR SDR CA030121007Bearing(CAN) LOG SNAG - ON FLAP SELECTION TO ONE UNIT, LE FLAP TRANSIT LIGHT REMAINED ON. NO. 4 SLAT REMAINED AMBER. ALL OTHERS GREEN. ON SELECTION OF FLAP 10, NO. 4 WENT GREEN FULL EXTEND WITH OTHER LE DEVICES.THE MAINTENANCE MECHANICS DISCOVERED THE NO. 4 LE SLAT OSDR C1HA200394002Engine · stalledCOMPRESSOR STALL NR 3 - 2.0 EPR 80 KT NR 3 ENGINE ICING LIGHT ILLUMINATED BRIEFLY. CHECKED NR 1 DETENT ON REV LEVER AND ADJUSTED ACHIEVE 1.60 EPR AT DETENT, NO STALLS NOTED AT 2 DETENT, AC OK FOR CONTINUED SERVICE IAW M/M CH 76-12-0/78-30-0.SDR CA030108011Warning System · activated(CAN) DURING CRUISE, THE APU FIRE DETECT LIGHT FLICKERED 3 TIMES. MAINTENANCE GROUND TESTED, NO FAULTS FOUND AND AIRCRAFT RELEASED FOR SERVICE.THE NEXT DAY THE APU FIRE DETECT LIGHT CAME ON BEFORE LANDING. AFTER LANDINGTHE APU FIRE LIGHT AND BELL CAME ON AND TSDR CA030107016Computer · failed(CAN) MACH TRIM LIGHT CAME ON IN FLIGHT, CREW REPORTED ELEVATOR FEEL INOPERATIVE. AIRCRAFT RETURNED TO DEPARTURE STATION. ELEVATOR FEEL COMPUTER REPLACED AS PER AMM. AND OPERATION CHECKED SERVICEABLE.SDR C1HA200394001Engine · stalledUPON LANDING NR 3 ENGINE COMPRESSOR STALLED AT 2.0 EPR ANR 90 KTS. RETARDED REVERSER AND ENGINE OPERATED NORMAL. PERFORMED VISUAL INSPECTION OF 1ST STAGE COMPRESSOR & AFT TURBINE IAW P&W JT8 MM REF 72-00-00 PG 122. PERFORMED GROUND ENGINE START/RUN, ALL INDSDR CA030106004Connector · burned(CAN) ON OVERNIGHT CHECK OF AUTO PILOT STAB TRIM, C/B FOUND TRIPPED AND UNABLE TO RESET. SMOKE NOTED IN STAB COMPARTMENT AND UPON INVESTIGATION FOUND CONNECTOR AND 3 INCHES OF ASSOCIATED WIRING DAMAGED ATA/P STAB TRIM MOTOR CONNECTION. WIRING REPAIRED, CONNSDR CA030103020Connector · burned(CAN) DURING OVERNIGHT CHECK IN THE HANGER, AVIONICS FOUND THE A/P STAB TRIM MOTOR C/B WAS POPPED. TRIED A RESET BUT NO JOY AND C/B FELT ODD. TURNED A/C POWER OFF AND C/B WOULD NOT RESET. C/B REPLACED. C/B RESET BUT POPPED A FRACTION OF A SECOND LATER. AVIONSDR CA030121003Bearing · loose(CAN) ON 9 JAN 2003 IT WAS FOUND THAT THE ROLLER BEARING ON THE NR 5 SLAT OUTBOARD TRACK HAD BECOME DETACHED AND THE CONTROL ARM HAD WORN THROUGH THE TOP WING SKIN FORWARD OF THE FRONT SPAR. UPON REMOVAL OF THE ACCESS PANEL ALL THE PARTS WERE FOUND INSIDE INCLSDR BJNA021202Battery Pack · dischargedLT EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE AT OVERWING EXIT. REPLACE LT EXTERIOR EMERGENCY BATTERY PACK POWER SUPPLY IN THE AFT CARGO PIT IAW MM.SDR C1HA200285015Filter · looseSMOKE REPORTED FROM ENGINE NR 2 AFTER LANDING. INSPECTED FOUND LOOSE DRAIN FILTER AND TORN DRAIN SCUPPER. TIGHTENED FITTINGS, OPS CHECKED ENGINE AT IDLE. NO LEAKS NOTED.SDR 02FDEA00972Floorbeam · gougedLONGITUDINAL FLOORBEAM OUTBOARD, LOWER FLANGE SIDE IS GOUGED JUST BELOW FASTENER HOLES BS 760-848, LBL 51, WL 208. LONGITUDINAL FLOORBEAM, BS 760-848, FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED DAMAGED BEAM, FABRICATED, ALODINED, PRIMED AND INSTALLED REPLACESDR 0204149881Engine · malfunctionedCLIMBING THROUGH 8000 FEET, MASTER CAUTION ILLUMINATED. ENGINE NR 1 OIL QUANTITY WAS ZERO AND OIL PRESSURE LIGHT WAS ILLUMINATED. ENGINE NR 1 WAS SHUTDOWN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE REPLSDR 0204099882Indicator · malfunctionedEN ROUTE CAPTAINS HSI INOPERATIVE. ALL FOUR RED BOW TIE LIGHTS ILLUMINATED. FLIGHT DIVERTED AND LANDED WITHOUT INCIDENT. REPLACED CAPTAINS COURSE INDICATOR. REPLACED NAV/INST MONITOR UNIT AND REPLACED AMPS. SYSTEM OPERATION CHECKS GOOD.SDR 02FDEA00956Support Angle · corrodedCORROSION FLOORBEAM SUPPORT ANGLE, UPPER FLANGE, LWR SURFACE BS 825, RBL 62, 207.5. REMOVED, FABRICATED AND REPLACED FLOORBEAM SUPPORT ANGLE IAW SRM AT BS 825, RBL 62.SDR 0204089872Bungee Cylinder · failedUPON LOWERING GEAR INTO LAN NOSE GEAR WOULD NOT EXTEND. FLIGHT RETURNED TO AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR BUNGEE CYLINDER. GEAR OPS CHECK GOOD.SDR AUS20021470Fire Detector · faulty(AUS) NO2 ENGINE FIRE WARNING ALERT. ENGINE WAS SHUTDOWN AND BOTTLESFIRED. FIRE WARNING LIGHT REMAINED ON' FOR A SHORT PERIOD, THEN WENT OUT. THE DETECTOR LIGHT REMAINED ON'. INVESTIGATION FOUND THE FIRE LOOP DETECTORS LOOSE AND DIRTY.SDR C1HA200296017Oil Filter · bypassingABORTED TAKEOFF DUE TO NR 2 ENGINE OIL BYPASS LIGHT ILLUMINATED. REMOVED AND INSPECTED NR 2 ENGINE MAIN OIL FILTER IAW M/M 72-61-08, LEAK AND OPS CHECK GOOD. FOUND SOME CARBON DEPOSITS IN FILTER. (P)SDR CA021227005Cam · damaged(CAN) UPON ARRIVAL IN YEG, THE NOSE OLEO WAS FOUND LOW AND LEAKING FLUID. AIRCRAFT HAD SOME HISTORY OF HARD BOTTOMING SNAGS. AFTER INSPECTION BY MAINTENANCE IT WAS DETERMINED THE NOSE GEAR REQUIRED DIASSEMBLY FOR A SEAL CHANGE. AIRCRAFT WAS FERRIED TO YVR FOR SDR P9R2002F00019Light · looseFORWARD GALLEY EMERGENCY FLOOR DIRECTIONAL TRACK LOOSE. RESCURED EMERGENCY FLOOR DIRECTIONAL TRACK IAW MM.SDR P9R2002F00018Light · missingPHOTOLUMINESCENT STRIP MISSING IN FORWARD GALLEY. INSTALLED PHOTOLUMINESCENT STRIP IAW MM.
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