Pratt & Whitney JT8D-1
Service difficulty reports · 195
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 = 'JT8D1' 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 = 'JT8D1' 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 GTIA040418Stop Fitting · corrodedFWD CARGO DOOR FUSELAGE SIDE, DOOR STOP CORRODED/ FROZEN. REMOVE DOOR STOP. INSTALLED NEW DOOR STOP.SDR GTIA040454Cable · disengagedEVACUATION SLIDE COVER AT TAILCONE SECURITY CABLE LT SIDE DISENGAUGED. RESECURED LT SECURITY CABLE.SDR GTIA040455Panel · corrodedLT L/E WING PANEL NR 1165C EXFOLIATED CORROSION AROUND FASTENER HOLES. FABRICATED NEW PANEL.SDR GTIA040458Longeron · corrodedAFT PIT 1099 STR 29R CORRODED. REMOVED LONGERON 29R FROM STA 1136 TO 1003. FABRICATED NEW LONGERON SECTIONS FROM STA 1003 TO 1068.875 AND FROM STA 1068 TO STA 1136. FABRICATED LONGERON SPLICE. INSTALLED LONG 29R AND SPLICE FROM STA 1003-1136.SDR GTIA040290Doubler · crackedAFT CARGO DOOR LATCH CUT OUT HOLE IS DEFORMED AND REPAIR DOUBLER IS CRACKED. REMOVED DAMAGED DOUBLER. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER.SDR GTIA040460Skin · damaged12 INCH X 10 INCH CLASS II EXTERNAL REPAIR AT FS 249 BETWEEN LONGERON 17C AND 18L. REMOVED EXISTING EXTERNAL REPAIR. CUT OUT DAMAGED AREA 13.5 INCHES X 14 INCHES. FABRICATED NEW REPAIR PARTS EXTERNAL SKIN, FINGER DOUBLER, 03 EA DOUBLERS. INSTALLED NEW REPASDR GTIA040461Skin · dentedDENT AT FS 58.75 BELOW RT CUSP LINE. REMOVED DAMAGED AREA 10.2500 X 16.5000. FABRICATED FILLER, DOUBLER, AND PLATE EA 5330-0410. INSTALLED REPAIR PARTS.SDR MEX203546Tire · debondedAFTER LANDING WAS LISTED AN STRONG NOISE IN THE MAIN LANDING GEAR. DURING REVISION OF THE MENTIONED AREA WERE FOUND SEVERAL DAMAGES IN THE NEARBY AREA OF THE LEFT MLG CAUSED BY A TREAD SEPARATION. AC WAS CARRIED TO THE HANGAR TO REPAIR THE FOLLOWING AFFECTEDSDR 03FDEA01670Floor Support · corrodedCORROSION ON LONGITUDINAL BEAM AT STA 760 TO 850 LBL 29 WL 208. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208, AND INSTALLED NEW LONGITUDINAL BEAM AT BS 740-850, LBL 29, WL 208. ALL WORK DONE PER SRM 5SDR 03FDEA01674Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C STRINGER 7 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, 7RH IAW SRM 51-30-2 & 51-30-5SDR 03FDEA01675Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C, STRINGER 5 RT. REPLACED CLIP. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 5RH IAW SRM 51-30-2 & 51-30-5SDR 03FDEA01676Stringer Clip · crackedSTRINGER CLIP CRACKED AT BS 950C, STRINGER 9 LT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 9 LT IAW SRM 51-30-2SDR 03FDEA01677Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950D, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950D, STRINGER 6 RT IAW SRM 51-30-2.SDR 03FDEA01678Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950B, STRINGER 6 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950B, STRINGER 6 RT IAW SRM 51-30-2 & 51-30-5.SDR 03FDEA01679Stringer Clip · crackedCRACK IN STRINGER CLIP AT BS 950C, STRINGER 4 RT. REMOVED CRACKED STRINGER CLIP & INSTALLED NEW CLIP AT BS 950C, STRINGER 4 RT IAW SRM 51-30-2 & 51-30-5SDR 03FDEA01615Floorbeam · corrodedCORROSION ON BS 1070 FLOORBEAM LBL 45 - RBL 50.SDR 03FDEA01617Skin · corrodedCORROSION ON INTERNAL STRAP BS 683 BELOW STR 26 LT . REMOVED CORROSION ON INTERNAL STRAP BS 683 BELOW STR 26 LT OF A AREA 2 X 2 X .005 OF ORIGINAL .063 MATERIAL. FOUND IN LIMITS I.A.W. BOEING SRM 53-30-1. WORK DONE IAW BOEING 727 SRM 53-10-1, BOEINGSDR 03FDEA01616Floorbeam · corrodedCORROSION BS 950F FLOORBEAM LWR CHORD NUTPLATE HOLES LBL 45 - RBL 45 WL 200. REPAIRED IAW SRM 53-10-8SDR RYN2004F00022Line · chafedON CLIMB OUT, LOST HYDRAULIC A-SYSTEM. ACCOMPLISHED APPROPRIATE CHECK LIST AND MANUALLY EXTENDED THE LANDING GEAR. EMERGENCY DECLARED AND AIRCRAFT RETURNED. AIRCRAFT LANDED MDT WITHOUT INCIDENT. REPLACED NR 2 ENGINE HYDRAULIC PUMP FLEX PRESSURE LINE. LEAKSDR DL73S030630Insulation · out of positionSMOKE SMELL IN AFT CABIN. FOUND INSULATION TOUCHING APU BLEED DUCT CAUSING SMELL. REPOSITIONED INSUL. FWD APU AIR TO MCO AND PLAC AS PRECAUTION.SDR MEX2003271Suppressor · damagedAIRCRAFT AIR TURN BACK DUE TO ENGINE 2 FAILURE DURING INITIAL CLIMB, REACHING 660 DEGREE C OF EGT EMERGENCY PROCEDURE WAS PERFORMED. DURING REVISION THE EXHAUST CONE, SUPPRESSOR AND TURBINE FAN WITH DAMAGE. ENGINE NR 2 WAS REPLACED IAW MM, OPERATIONAL TEST SDR GTIA030221Light · inoperativeEMERGENCY OVERHEAD LIGHTS INOPERATIVE IN PAX CABIN AISLE NR 3,7,10,12,14,18,22,25,29. TROUBLESHOT AND REPAIRED EMERGENCY OVERHEAD LIGHTS.SDR GTIA030142Floor Panel · crackedAFT PIT CRACKED FLOOR WEB AT FS1289-1309 LONG 18R. FAB DOUBLER. INSTALLED DOUBLER.SDR GTIA030180Floor Support · damagedFORWARD CABIN STA 160 TO STA 200 LBL 44 FLOOR SUPPORT HAS GOUGED/ DAMAGED CORRODED. FABRICATED NEW FLOOR SUPPORT.SDR GTIA030145Floorboard · corrodedFORWARD CABIN STA 200 TO 160 LBL 44 TO 53 INCHES (9 X 40) FLOOR PNL SOFT/ MUSHY CORRODED INSERTS. FABBED NEW CABIN FLOORBOARD, STA 200-160 LBL 53.SDR GTIA030146Floor Panel · damagedFWD CABIN STA 180 TO 160 LBR 8 INCHES TO 44 INCHES (20X36) FLOOR PANEL SOFT/ MUCHEY DAMAGED DETERIORATED CORR. INSERTS. FABRICATED NEW PANEL.SDR GTIA030147Panel · deterioratedFORWARD CABIN STA 200 TO ST 256 LBL 44 INCHES (21X56) FLOOR PANEL SOFT/ MUSHEY, DETERIORATED CORR. INSERTS.SDR GTIA030148Floor Panel · deterioratedFORWARD CABIN STA 200 TO 256 FLOOR PANEL SOFT/ MUSHEY DETERIORATED, CORR. INSERTS, LBR 22 TO LBR 44 (21X56). FABRICATED NEW PANEL.SDR GTIA030144Shear Tie · crackedAFT CARGO FS 1250 SHEAR TIE CRACKED STR 28R. REMOVED CRACKED SHEAR TIE, FABRICATED NEW SHEAR TIE AND INSTALLED REPAIR PARTS.SDR GTIA030143Fitting · corrodedAFT CARGO FS 1336 STR 28R END FITTING CORRODED. REMOVED STR 28R END FITTING. LOCATED AND DRILLED NEW FITTING. INSTALLED STRINGER 28R END FITTING.SDR 03FDEA00074Position Switch · faultyINFLIGHT, NO NOSE GEAR DOWN INDICATION. (GREEN LIGHTS). REPLACED BOTH BULBS NO EFFECT. CYCLED GEAR, TESTED BULBS, DID NOT WORK, REPLACED BOTH BULBS, AGAIN A VERY WEAK LIGHT, GOOD INDICATION, WENT TO BRIGHT, WORKED. BACK TO DIM AND WAS INTERMITTENT, LANDISDR 03FDEA00008Skin · corrodedCORROSION UNDER EDGE OF RIGHT RAM AIR DOOR ACTUATOR PANEL. CORROSION OUT OF LIMITS, REPAIRED IAW EA 7-5330-68147.SDR 03FDEA00007Frame · dentedDENT IN FRAME, BS 950C STR 26L. REPAIR FRAME IAW SRM.SDR 03FDEA00010Skin · dentedOIL CAN DENT IN SKIN AT BS 211, RBL 23, WL 182. REMOVED DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR IAW SRM 53-30-3.SDR 03FDEA00009Skin · dentedOIL CAN DENT IN SKIN AT BS 190, RBL 22, WL 182. REMOVED DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR IAW SRM 53-30-3.SDR RYN2003F00002Splice · crackedAT B CHECK, CRACK FOUND AT FUSELAGE INTERIOR FLOOR SPLICE PLATE TO LOWER SILL BEAM, BS 640.SDR RYN2003F00001Frame · crackedAT B CHECK, CRACK FOUND ON FORWARD AND AFT SIDES OF FUSELAGE INTERIOR, LT FRAME AT BS 680 ATTACHMENT TO SKIN LOWER SILL BEAM.SDR RYN2003F00003Floorbeam · crackedAT B CHECK, CRACK FOUND IN FUSELAGE INTERIOR AT FLOORBEAM LOWER CHORD ANGLE BS295, LBBL30.SDR RYN2003F00004Skin · crackedDURING B CHECK, FOUND SKIN CRACKED AT FUSELAGE INTERIOR, LT SIDE, BS 480, FRAME TO LOWER SILL BEAM FROM TIE TO FUSELAGE.SDR 02FDEA00971Stringer · crackedLOWER FUSELAGE, STRINGER 21R, IS CRACKED AT STA 400. REMOVED DAMAGED SECTION OF STRINGER FROM STATION 390-410 AND REPLACED IAW SRM.SDR 02FDEA00974Skin · dentedDENTS IN SKIN, BS 660 - 670, S22R. REPAIRED DENTS IN SKIN IAW SRM.SDR 02FDEA00975Skin · damagedFUSELAGE SKIN DAMAGED AT BS 1050, STR 19R, JUST BELOW THE LAP. REPAIRED SKIN IAW SRM.SDR ABXA030012Frame · crackedLEFT MAIN FRAME, STA 699, HAD CRACK IN FORWARD FLANGE FROM POINT J TO POINT G. REPAIRED LEFT MAIN FRAME IAW EA 53400100-001-1.SDR ABXA030009Skin · delaminatedRIGHT CONTROL TAB DELAMINATED IN NUMEROUS PLACES UPPER SKIN. REPLACED RIGHT ELEVATOR CONTROL TAB IAW DC-9 MM 27-30-03-2-0000.SDR ABXA030010Skin · delaminatedRIGHT GEAR TAB DELAMINATED IN NUMEROUS PLACES UPPER SURFACE. REPLACED RIGHT GEARED TAB IAW DC-9 MM 27-30-04-2-0001.SDR ABXA030011Skin · delaminatedLEFT CONTROL TAB DELAMINATED UPPER SURFACE IN NUMEROUS PLACES. REPLACED LEFT ELEVATOR CONTROL TAB IAW DC-9 MM 27-30-03-2-0001.SDR 0204119995Strut · flatAFTER TAKEOFF WHEN GEAR WAS RETRACTED LOUD VIBRATION IN NOSE GEAR AREA. NO UNSAFE INDICATIONS ON GEAR. EXTENDED GEAR AND VIBRATION STOPPED. FLIGHT RETURNED AND LANDED WITHOUT INCIDENT. UPON RETURN TO GATE FOUND RIGHT NOSE GEAR DOOR OPEN. NOSE GEAR STRUT FSDR 0204139931Switch · inoperativeON CLIMBOUT ALL THREE (GEAR UNSAFE) LIGHTS ILLUMINATED. ALL OTHER INDICATIONS NORMAL. ON GEAR EXTENSION GOT ALL GREEN LIGHTS ILLUMINATED AND (GEAR UNSAFE) LIGHT EXTINGUISHED. ALL OTHER INDICATIONS NORMAL. FLIGHT LANDED WITHOUT INCIDENT. REPLACED SWITCH ASSEMBLSDR 02FDEA00944Downlock Switch · inoperativeDURING LANDING GEAR EXTENSION, NOSE GEAR UNSAFE LIGHT ILLUMINATED. NO DOWN, GREEN LIGHT. NOTE: MANUAL GEAR EXTENSION PROCEDURE COMPLETED EMERGENCY, DECLARED WITH ATC. TROUBLESHOT LANDING GEAR POSITION INDICATING SYSTEM IAW M.M. FOUND FAULTY NOSE LANDING SDR 02FDEA00942Duct · blownAFTER TAKEOFF NR 3 ENGINE HAD FIRE INDICATOR, IAW FLIGHT MANUAL QRM SHUTDOWN ENGINE, FIRELIGHT EXTINGUISHED BY ITSELF AND TESTED GOOD. NO ABNORMAL ENGINE INDICATIONS WERE NOTED. AFTER ENGINE SHUTDOWN WINDMILLED FOR APPROXIMATELY 10 MIN. NR 3 OIL PRESS APPR
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