Pratt & Whitney JT8D series
Service difficulty reports · 1,122
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 = 'JT8D' 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 = 'JT8D' 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 DALA1052500909Seat Track · corrodedMAIN PASSENGER CABIN LT SEAT TRACK LBL 55 HAS CORROSION FROM APPROX FS 218 TO APPROX 579. BEYOND LIMITS. SPLICED IN NEW SEAT TRACK SECTION IAW SRM 51-30-1 AND 51-30-5.SDR DALA1052610909Floorbeam · corrodedMAIN PASSENGER CABIN FLOOR SUPPORT AT FS 200 HAS CORROSION FROM RBL 9 TO RBL 47, BEYOND LIMITS. REPAIRED IAW SRM 51-30-2 AND 53-14-1, FIG 11.SDR DALA1052620909Seat Track · corrodedMAIN PASSENGER CABIN RT SEAT TRACK AT RBL44 HAS CORROSION FROM FS 200 TO APPROX FS 246. BEYOND LIMITS. REPAIRED IAW SRM 51-30-5, 51-30-4 AND 53-01, FIG 1.SDR DALA1052410909Skin · damagedFUSELAGE EXTERNAL SKIN, STA 224, LONGERON 17L, DENT IN PREVIOUS SKIN REPAIR. REMOVED DAMAGE AND REPAIRED FUSELAGE SKIN IAW SRM 53-34-0 FIG 1 AND DWG SG0953008.SDR DALA1052420909Skin · gougedFUSELAGE EXTERIOR SKIN STA 232 BETWEEN LONGERON 17L-18L, GOUGE IN PREVIOUS REPAIR.SDR DALA1052440909Skin · corrodedAFT CARGO COMP - SKIN HAS CORROSION UNDER LONGERON 29L AT STA 1201. BEYOND LIMITS. INSTALLED DOUBLER REPAIR IAW DWG SG09530001 AND SRM 51-30-2.SDR DALA1052450909Longeron Splice · corrodedMID CARGO COMPARTMENT BETWEEN STA 579 AND 598, LONGERON 30 SPLICE HAS CORROSION. BEYOND LIMITS. REPLACED SPLICE IAW SRM 51-10-4 AND SRM 51-30-5.SDR DALA1052510909Skin · crackedFUSELAGE EXTERIOR STA 731-750, LT WINDOW CUTOUT HAS STATIC DISCHARGE WITH CRACK INDICATION, NDT VERIFIED. R & R WINDOW BELT PANEL AT STA 731-750LT IAW SRM 51-30-2 AND 51-30-5.SDR DALA1052520909Skin · crackedFUS EXTERIOR LT STA 545 CRACK AT WINDOW CUTOUT. R & R WINDOW BELT PANEL STA 545 LT IAW SRM 51-30-2 AND 51-30-5.SDR DALA1026630919Light · inoperativeDURING LINE CHECK MX FOUND EMERGENCY LIGHTS AT SEAT 23D INOPERATIVE. MX REPLACED THE LIGHT ASSY AT 23D. OPERATION OF LIGHTS NOW CHECK OK.SDR DALA1026659016Slide · looseCREW WROTE UP L1 DOOR SLIDE UNPINNED. MX REPLACED L1 DOOR SLIDE IAW THE MM.SDR DALA1026060910Connector · disconnectedDURING LINE CHECK, MX FOUND PASSENGER EMERGENCY PATHLIGHT AT 11D INOPERATIVE. MX RECONNECTED EMERGENCY LIGHT HARNESS PLUG TO LIGHT. OPERATION OF LIGHT NOW CHECKS OK.SDR DALA1026070952Light · inoperativeDURING LINE CHECK MX FOUND EMERGENCY LIGHT AT SEAT 28C INOPERATIVE. MX REPLACED LIGHT ASSY AT SEAT28C. OPS CHECK OF LIGHT IS NOW OK.SDR DALA1025599886Attach Fitting · corrodedDURING M-CHECK FOUND CORROSION IN INTERCOSTAL ATTACH CLIP AT AFT CARGO COMPARTMENT DOOR CUTOUT AREA AT BS 1060, ABOVE L26R. REPAIRED IAW SRM 51-30-2, SRM 51-10-2, SRM 51-10-3, SRM 51-10-4, SRM 51-10-5, DWG 59104142, SRM 51-30-8, SRM 53-05 FIG 2.SDR DALA1025760911Wire Harness · inoperativeDURING LINE MX, FOUND EMERGENCY PATH LIGHT AT 30D INOPERATIVE. MX REPLACED LIGHT HARNESS AT 30D. OPERATION OF LIGHT NOW CHECKS OK.SDR DALA1025490921Wire · damagedINSP DURING LINE CHECK MX, FOUND EMERGENCY LIGHTS AT ROW 13 INOPERATIVE. MX REPLACED LIGHT ASSY IAW MM 33-53-01 DUE TO PULLED WIRE. OPERATION OF LIGHT NOW CHECKS OK.SDR DALA1025480994Unknown · odorFLIGHT CREW DIVERTED ACFT DUE TO AFT LAVATORY SMOKE DETECTORS SOUNDING WITH LIGHT HAZE AND ODOR IN THE CABIN. MX COMPLIED WITH OPN 5088 - AND NO TROUBLE WAS FOUND. BORESCOPED BOTH ENGINES - NO ISSUES. RAN ENGINES FOR 20 MINUTES AT POWER - NO SMOKE OR ODORSSDR DALA1025479016Power Supply · inoperativeLIGHT WAS INOPERATIVE, REPLACED LIGHT POWER SUPPLY.SDR DALA1024759009Panel · damagedVERTICAL STABILIZER/ LOWER FIXED L/E PANEL/ UPPER EDGE/ ZFS52/ HOLE DAMAGE. REPAIRED IAW ER/A 485868-14.SDR DALA1025120968Sensor · shortedDURING FLIGHT AT 26K FT AND SPEED OF 310KTS, THE AMBER "GEAR DOOR OPEN" LIGHT CAME ON. CREW SLOWED TO 280 KTS AND CONTINUED TO DESTINATION. DURING DESCENT, AT 12K FT, THE LIGHT WENT OUT. ACFT LANDED UNEVENTFULLY AND UPON ARRIVAL MX FOUND THE RT MLG DOOR OPESDR DALA1025139016Socket · failedDURING LINE CHECK, MX FOUND EMERGENCY CEILING LIGHTS AT ROW 23-25 INOPERATIVE. MX REPLACED POWER SUPPLY AND BAD LIGHT SOCKET AT ROW 23. OPS CHECK OF LIGHTS NOW CHECKS GOOD.SDR DALA1025140994Oil System · leakingDURING CLIMBOUT, BOTH OF THE AFT LAVATORIES SMOKE DETECTORS ALARMS SOUNDED WITH LIGHT HAZE AND ODOR IN THE AFTCABIN. CLEARED AND ALARMS STOPPED WHEN CLIMBING THROUGH 12K FT SO FLIGHT CONTINUED TO DESTINATION. UPON ARRIVAL, MX FOUND THE APU LEAKING OIL AND REPSDR DALA1024799012Wire · damagedDURING SERVICE CHECK MX FOUND EMERGENCY LIGHTS AT ROW 23 INOPERATIVE. MX REPLACED FIXTURE AND PIGTAIL. OPS OF LIGHTS NOW CHECKS OK.SDR 2ARF201009001Door · damagedDURING TRANSIT CHECK, TECH DETECTED THE APU DOOR OPEN AND FOLDED. MX PERFORMED THE DOOR INSP DETECTING THAT FOLD WAS NOT REPAIRABLE, SO IT WAS REPLACED IAW MM 52-45-00, ALL CORRECT.SDR 2DYA20100929001Battery Pack · dischargedDURING PREFLIGHT CHECK, NOTED OVERHEAD EMERGENCY LIGHT INOP AT L2 DOOR. REPLACED BATTERY PACK IAW MM 33-53-00.SDR DALA1024770989Deflector · damagedRETURNED TO DEPARTURE, NLG WOULD NOT RETRACT AFTER TAKEOFF. MX FOUND RT SPRAY DEFLECTOR WEARSTRIP FWD NUTPLATE PULLED AND SCREW STICKING OUT, CAUSING CONTACT WITH WHEEL WELL STRUCTURE DURING RETRACTION, R & R RT SPRAY DEFLECTOR HALF. SWUNG NLG CHECKED GOOD.SDR DALA1024780920Wire · brokenDURING LINE CHECK MX FOUND EMERGENCY LIGHTS AT ROW 2DE INOPERATIVE. MX REPAIRED BROKEN WIRE AT ROW 25DE IAW SWPM CHAP 20. OPS OF LIGHTS NOW CHECKS OK.SDR DALA1023780984Pan · crackedFWD LAV PANEL PAN CUTOUT CRACKED AT UPPER AFT EDGE. REPAIRED IAW ER/A 485789-14 REV ORIG.SDR DALA1023849001Connector · disconnectedDURING LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT SEATS 3 AND 19 TO BE INOPERATIVE. MX RECONNECTED A CONNECTOR AT SEAT 3 AND RE-LAMPED THE LIGHTS AT SEAT 19. OPS CHECK OF LIGHTS IS NOW GOOD.SDR DALA1023550947Seal · failedFLIGHT CREW DIVERTED ACFT DUE TO SMOKE IN THE CABIN. MX FOUND APU OIL CAP SEAL IN POOR CONDITION WITH OIL ON THE GROUND. MX R & R OIL CAP SEAL AND ACCOMPLISHED OPERATION 5089 DUCT BURN-OUT.SDR DALA1023149007Door Frame · corrodedDUE ERA 484488-14, REV A CODE 53-16 PERMANENT REPAIR TO C-3 CARGO DOOR SURROUND, LOWER JAMB BEAM CORROSION.SDR DALA1023779013Skin · damagedJACK PAD AND STRUCTURE AROUND IT DAMAGED.SDR C8GA201000047Skin · dentedWHILE IN HEAVY MX PERFORMING INSP, A DENT WAS NOTED AT LAP SEAM STA 520, STRINGER 26R. REMOVED DAMAGED AREA, PERFORMED HFEC INSP, NO CRACKS NOTED. FABRICATED DOUBLER 12" X 11" FROM 2024 T3 .090" AND FILLERS 4" X 3" (2) FROM 2024 T3 .080". INSTALLED REPAIR, SDR DALA1022579007Skin · damagedPITTING CORROSION ON BARREL NUT HOLES OF RT HORIZ STAB UPPER FWD AND UPPER AFT SKIN PANELS 1 EA. REPAIRED IAW AMR DOCUMENT 0955141 BARREL NUT HOLE NR3 AND NR 26 ON T0182702 AT HMV3 IN GDL.SDR DALA1021900912Battery Pack · inoperativeDURING LINE CHECK MX FOUND AFT OVERWING EXIT LIGHTS INOPERATIVE. MX REPLACED POWER PACK BATTERIES ABOVE AFT OVERWING EXIT. OPS CHECK OF EXIT SIGN NOW CHECKS OK IAW AMM 33-53-00.SDR EE4Y1009369Support Fitting · crackedMAIN CARGO CABIN SUPPORT FITTING CRACKED AT STA Y 446 BETWEEN LONGERON 18L AND 19L.SDR DALA1021910915Fuse · blownDURING LINE CHECK MX FOUND EMERGENCY LIGHTS IN SEATS 27 THRU 35 INOPERATIVE. MX REPLACED BATTERY CHARGER AT SEAT 36 NO HELP. REPLACED BLOWN FUSE. OPS CHECK OF LIGHTS NOW CHECKS OK.SDR DALA1021070908Fuse · blownMX FOUND THE EMERGENCY TRACK LIGHTING AT ROWS 24-30 TO BE INOPERATIVE. MX REPLACED THE FUSES ON THE BATTERY PACK. ALL LIGHTS WERE THEN GOOD EXCEPT 27DE WHICH WAS FORWARDED TO MCO. MX FOUND BLOWN FUSES ON THE AFT BATTERY PACK AND REPLACED THE FUSES. AN OPS CSDR Y2PA2010083000020Power Supply · inoperativeWHILE PERFORMING A SERVICE CHECK, THE OVERWING EMERGENCY EXIT LIGHTS (ON FUSELAGE) WERE FOUND INOPERATIVE DUE TO A NON FUNCTIONING RECHARGEABLE BATTERY POWER SUPPLY. BATTERY WAS FOUND TO BE CHARGED BUT UNIT NOT PROVIDING POWER TO LIGHTS. UNIT TO BE REPLACED SDR FDEA201008283173Gasper Fan · damagedCREW SMELLED SMOKE-LIKE ODOR ENTERING THE COCKPIT. ISOLATED ODOR TO GASPER FAN. ODOR WAS NOT PRESENT WITH GASPER FAN OFF. LEFT THE GASPER FAN OFF FOR REMAINDER OF THE FLIGHT. AFTER T/S FOUND THE GASPER FAN TO BE THE MAIN ISSUE. R & R GASPER FAN IAW MM 2SDR DHLA201000094Skin · misrepairedPERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG 1 D, SHEET 3 REMOVED EXISTING NON STANDARD REPAIR IAW SRM 51-1-21 FABRICATED REPAIR DOUBLER IAW SRM 53-2-0 FIG 1D SHEET 3, SRM 53-3-3 FIG 1 ITEM "A", SRM 51-9-0 FIG 68 A CLEANED, TREATED AND PRIMED AREA & REPAIR DOUBLESDR 2ARF201008002Radome · damagedCAPTAIN REPORTED A LIGHTNING STRIKE IN THE ACFT RADOME. MX PERFORMED A LIGHTNING STRIKE INSP IAW MM 05-53-00 DETECTING RADOME, TAIL CONE AND RT ELEVATOR GEAGER TAB WITH MATERIAL LOOSE OUT LIMITS OF OPERATION; 10 RIVET DAMAGED AND SMALL DAMAGES OF FUSELAGE SKINSDR C8GA2010000021Skin · corrodedWHILE IN HEAVY MX, PERFORMING INSP, IT WAS NOTED THAT THE LOWER FUSELAGE LT SIDE AT BS 950C - 1010. REMOVED DAMAGED AREA BS 950E TO 950F, STR 25L-26L 3" X 1" & 2" X 1", ALSO 950 F TO 970 BETWEEN BETWEEN STRINGER 24L-25L 7" X 2.5" AND 970 TO 990 BETWEEN 24L-25SDR C8GA2010000022Attach Fitting · corrodedWHILE IN HEAVY MX PERFORMING INSP, IT WAS NOTED THAT THE AFT CARGO, AFT BULKHEAD , RT SIDE, OTBD CEILING FLOOR TO BULKHEAD ATTACH SUPPORT HAS CORROSION. R & R SUPPORT FITTING. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000023Support · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE AFT CARGO, AFT BULKHEAD , RT SIDE, OTBD CEILING FLOOR TO BULKHEAD ATTACH SUPPORT HAS CORROSION. REMOVED AND FABRICATED NEW FLOOR TO BULKHEAD SUPPORT ANGLE FROM 2024-0 HEAT TREATED TO T3 AND INSTALLED ANGLSDR C8GA2010000024Support Angle · corrodedWHILE IN HEAVY MX PERFORMING INSP IT WAS NOTED THAT THE AFT CARGO, AFT BULKHEAD , RT SIDE, OTBD CEILING FLOOR TO BULKHEAD ATTACH SUPPORT HAS CORROSION. REMOVED AND FABRICATED NEW FLOOR TO BULKHEAD SUPPORT ANGLE FROM 2024-0 HEAT TREATED TO T3 AND INSTALLED ANGLSDR C8GA2010000025Shear Tie · corrodedWHILE IN HEAVY MX PERFORMING INSP CORROSION WAS NOTED ON THE SHEAR TIE FRAME STA 950B STRINGER 29L. REMOVED CORROSION FROM SHEAR-TIE, FABRICATED REPAIR STRAP FROM 7075 T6 .063" INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000026Stringer · corrodedWHILE IN HEAVY MX PERFORMING INSP, CORROSION WAS NOTED ON THE STRINGER 29L STATION 950B. REMOVED CORROSION FROM STRINGER, FABRICATED REPAIR STRAP FROM 7075 T6 .063" 8.5" INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.SDR C8GA2010000027Support Fitting · corrodedWHILE IN HEAVY MX PERFORMING INSP, CORROSION WAS NOTED ON THE SUPPORT FITTING ATTACHED TO THE SHEAR WEB LOWER SIDE STA 1175 LBL 30. REMOVED AND FABRICATED NEW SUPPORT FITTING FROM BAC1520-792. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SSDR C8GA2010000028Hinge · crackedWHILE IN HEAVY MX PERFORMING INSP, THE MAIN CARGO DOOR AFT HINGE LOBE IS CRACKED. NO OTHER DEFECTS NOTED. ACFT WAS RETURNED TO SERVICE.
Back to Pratt & Whitney JT8D series