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 K11A2020072800003Fuel Control · failedON TAKEOFF ROLL, NR 3 ENGINE DID NOT PRODUCE FULL THRUST, AIRCRAFT PERFORMED REJECTED TAKEOFF. TROUBLESHOOTING IN WORK AT THIS TIME.SDR YYFA20141227001Display · faultyLEFT FUEL INDICATION 9 NOT INDICATING FUEL FLOW. REPLACED DISPLAY UNIT DUE ERROR CODE 9. OPERATIONS CHECKED NORMAL AMM 77-42-00.SDR YYFA2014121100001Circuit Breaker · trippedLEFT START VALVE DID NOT OPEN UPON START. FOUND CIRCUIT BREAKER OF START VALVE TRIPPED, RESET, ALL NORMAL.SDR CA141104012Wire · failed(CAN) NR 3 ENGINE OIL TEMP INDICATION PEGGED PAST RED BAND. SUPPLEMENTAL CHECK LIST COMPLIED WITH AND ENGINE SHUTDOWN. MAINTENANCE INSPECTED ENGINE AND ISOLATED FAULT TO GROUND WIRE ON NR 3 ENGINE. GROUND WIRE INSTALLED IAW SWPM 20-10-13. ACFT RETURNED TO SSDR E4EB2014073112891Battery Pack · inoperativeFORWARD CENTER AISLE OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK.SDR 2013FA0000134Pa System · malfunctionedL1, L2 AND RC PA'S NOT WORKING IN AIR. PERFORMED PA CHECK IN ALL STATIONS L1, L2 AND RC DURING FLIGHT AND ON GROUND OPERATIONS WITH SENIOR F/A. OPS CHECKED GOOD FOR CONTINUED SERVICE AMM 23-30-00.SDR 2012F00218Compressor · damagedAFTER TAKEOFF, HEARD A LOUD POP. ON LANDING DISCOVERED NOSE OF ACFT ENCOUNTERED BIRD STRIKE. LEFT ENGINE INGESTED BIRD CAUSING DAMAGE TO 3 N1 COMPRESSOR BLADES.SDR 2012FA0000691Handset · malfunctionedFWD F/A HAND SET DOES NOT RESET WHEN RETURNED TO CRADDLE, CALL AURAL ALERT DOES NOT WORK.SDR YYFA2012F00153Pa System · intermittentF/A'S PA INTERMITTENT.SDR YYFA2012F00182Handset · intermittentF/A HANDSET WORKS INTERMITTENTLY AT L2 AND RC HANDSETS F/A TO F/A AND F/A TO PILOTS WORK.SDR YYFA20110825001Epr System · inoperativeLEFT EPR WILL NOT GO ABOVE 1.63 ON TAKEOFF.SDR YYFAN836NK1811Pa System · weakAFT F/A POSITION PA WEAK.SDR FDEA201101310431Compressor · stalledCOMPRESSOR STALL DURING TAKEOFF ROLL, UNSURE OF ENGINE, INDICATION WERE MOMENTARY ILLUMINATION OF ENG FAIL LIGHT ACCOMPANIED BY AN ENG COUGH. ENGINE RECOVERED IMMEDIATELY. TAKEOFF WAS REJECTED. PERFORMED NR 1 ENGINE BORESCOPE INSP IN REF TO MM 72-00-00. NSDR 2ARF201012002Drive Unit · damagedCAPTAIN REPORTED THAT DURING CLIMB THE RT UVC AND GENERATOR WERE DISCONNECTED BY HIGH TEMPERATURE; SO THE FLIGHT CREW PERFORMED THE DRIVE GENERATOR MALFUNCTION PROCEDURE, CONFIRMING THE FAILURE AND SHUT DOWN THE UVC AND GENERATOR, CONTINUING TO DESTINATION. DUSDR DALA1030219865Skin · misrepairedDURING M-CHECK AND REPAIR DATA COLLECTION. FUSELAGE EXTERIOR SKIN REPAIR FS 370 BETWEEN LONG 24-25 RR DOES NOT MEET STATIC STRENGTH REQUIREMENTS OF SRM. TRIMED OUT OUTER SKIN FROM STA 373 BETWEEN L25R TO L26R PERFORMED HFEC NDT SRM 06-10-01 .001 NO CRACK NOTEDSDR DALA1030229865Skin · misrepairedDURING M-CHECK AND REPAIR DATA COLLECTION, FUSELAGE EXTERIOR SKIN REPAIR AT FS 361 BETWEEN LONG 26-27R. LESS THAN 3" PROXIMITY TO INTERNAL PRODUCTION DOUBLER AT DOOR CUT OUT. REQUEST ENGINEERING DISPOSITION. REPAIR APPEARS TO BE INSTALLED IAW SRM 53-04, FIG 1SDR FDEA201010274179Skin · gougedREWORK - NUMEROUS GOUGES MCD INNER SURROUND SKIN STA 620-640, S11-17L. REF: SNRM N00698 - EA 7-5330-143901 MCD SURROUND INNER SKIN REVISED. ACCOMPLISHED REPAIR ON MCD INNER AFT LOWER SKIN IAW FEDEX EA# 7-5330-143901 CUTOUT INNER SKIN SECTION DIM: 22" X SDR I5EA20101001Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.SDR I5EA20101002Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.SDR I5EA20101003Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.SDR I5EA20101004Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.SDR I5EA20101005Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.SDR I5EA20101006Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.SDR I5EA20101007Battery Pack · failedEMERGENCY LIGHT BATTERY PACK FAILED OPS TEST.SDR FDEA201010224148Floorbeam · corrodedCORROSION - STA 720 FLOORBEAM, LOWER FLANGE, LOWER SURFACE, RBL 12 TO LBL 12. CUT OUT (2) SECTIONS OF BS 720 FLOORBEAM LOWER FLANGE 5.75" AND 7.5" AT RBL 6.5 AND LBL 3.0 IAW SRM, REV 103, 53-10-8 FIG 2. FABRICATED (2) REPAIR ANGLES USING 7075-0, .063" X 35"SDR FDEA201010224149Floorbeam · corrodedCORROSION - STA 720 FLOORBEAM, LWR FLANGE LWR SURFACE RBL 24.75 - RBL 37. CUT OUT APPROX 4.0" AREA OF BS 720 FLOORBEAM LWR FLANGE AT RBL 36 IAW SRM, REV 103, 53-10-8, FIG 2. FABRICATED (2) REPAIR ANGLES USING 7075-0, .063" X 3" X 15", FILLER USING BAC1505-1SDR FDEA201010174108Rib · crackedUPON REMOVAL OF AFT ACCESS PANEL, FOUND NR 5 SLAT TO HAVE 1 CRACKED RIB ON THE OUTBD SIDE. REMOVED DAMAGED RIBS IB & OB, FABRICATED NEW IB & OB RIBS & INSTALLED NEW IB & OB RIBS AT NR 5 SLAT IAW SRM 51-30-5, SRM 51-30-2, SRM 51-10-2, & DWG NR 65-17294 & FSDR FDEA201010154079Floorbeam · corrodedCORROSION TOP TEE CAP FLOORBEAM, BL 0 TO RBL 25. CUTOUT DAMAGE AREA APPROX DIM: 2" X 6.6". FABRICATED UPPER TEE FROM BAC 1505-100617-7075T6 APPROX DIM 18" X 2", SUPPORT ANGLES AND REINFORCEMENT STRAPS. INSTALLED REPAIR PARTS IAW SRM 53-10-8 FIG 3, 51-20-0SDR FDEA201010144076Floorbeam · corrodedCORROSION TOP TEE CAP FLOORBEAM MAIN CABIN BS 720D LBL 25 - BL 0. CUTOUT DAMAGE TEE CAP FLOORBEAM DIM: 2" X 9.2" BS 720D LBL 2.8 TO LBL 12, FABRICATED TEE CAP FLOORBEAM FROM BAC 1505-100617-7075T6 DIM: 23.125" X 2" AND UPPER CHORD, SUPPORT ANGLES AND REINFORCESDR FDEA201010113991Vertical Beam · damagedMISSED DRILLED HOLES VERTICAL BEAM LBL 20 AFT CARGO PIT BS 1183. REPAIRED MISDRILLED HOLES AT VERTICAL BEAM IAW E.A. 7-5310-135599. REMOVED PREVIOUS STRAP & DOUBLER IAW SRM 51-30-2, TRIMMED OUT BEAM APT FLANGE (DIM: 33 1/4") & WEB (MISDRILLED AREAS, 8 TOTAL),SDR DALA1025819865Floorboard · puncturedDURING M-CHECK FOUND SKIN PUNCTURED IN MAIN CABIN FLOORBOARD NR 99. REPAIRED IAW SRM 53-05 FIG 1.SDR DALA1025829867Skin · dentedDURING LINE CHECK FOUND DENT IN SKIN AFT OF CARGO DOOR AT BS 1108 & BS 1121 L22R TO L26R. REPAIRED IAW ERA 486265-14.SDR DALA1025699865Floor Support · crackedDURING M-CHECK FOUND CRACK IN FWD CARGO FLOOR SUPPORT LIGHTNING HOLE AFT OF FR 389 BL 0. REPAIRED IAW SRM 51-30-2 & SRM 51-30-5.SDR DALA1025709865Floorbeam · crackedDURING M-CHECK FOUND CRACK IN MAIN CABIN FLOOR SUPPORT FASTENER HOLE AT BS 712 RBL 22- RBL 44. REPAIRED IAW SRM 51-30-2, SRM 53-13-3 FIG 1, SRM 51-10-3.SDR DALA1025309865Floor Support · crackedDURING M-CHECK, FOUND CRACK IN CABIN FLOOR SUPPORT AT BS 775 RBL 18. REPAIRED IAW SRM 51-30-2, SRM 53-13-3, FIG 11, SRM 51-10-2, SRM 51-10-3 AND DWG 5914617.SDR DALA1025329865Floor Panel · corrodedDURING M-CHECK FOUND CORROSION ON MAIN CABIN FLOOR PANEL NR 20. REPAIRED IAW SRM 51-10-4, SRM 53-01, FIG 1.SDR DALA1025339865Support Fitting · crackedDURING M-CHECK FOUND CRACK IN LT KEEL FORMER SIDE SUPPORT FITTING AT BS 734 LBL 5. REPAIRED IAW SRM 51-30-5, PAGE 205.SDR DALA1025349865Cusp Web · crackedDURING M-CHECK FOUND CRACK IN CUSP WEB AT BS 252 RBL 46. REPAIRED IAW SRM 53-13-2, SRM 51-10-3, SRM 51-30-2.SDR DALA1025359868Frame · crackedDURING M-CHECK FOUND CRACK IN FRAME AT BS 674 LONGERON 30. REPAIRED IAW SRM 51-30-1, SRM 51-30-2, SRM 51-30-5, SRM 51-10-2, SRM 51-10-4.SDR DALA1026259865Splice · chafedDURING M-CHECK FOUND CHAFING AND CRACK ON MAIN CABIN INTERCOSTAL SPLICE AT BS 813 LBL 15. REPAIRED IAW DWG PL4915719, SRM 51-10-2, SRM 51-10-4 & SRM 51-30-2.SDR EE4Y100355Exhaust Duct · corrodedDURING INSP ENGINE NR2 EXHAUST DUCT WITH SPOT CORROSION AT L/E SKIN.SDR EE4Y100356Floor Support · corrodedDURING INSP UPPER FUSELAGE PAX CABIN AT STA Y503 AND STA Y525, +X33 FLOOR CHANNEL WITH CORROSION.SDR YYFA201000021Unknown · smokeAFTER TAKEOFF, F/A REPORTED SMOKE IN THE AFT CABIN. RETURNING TO DEPARTURE UPON LANDING THE ACFT WEIGHTED 150,000 LBS MAKING IT AN OVERWEIGHT LANDING.SDR DALA1013579917Fuse · inoperativeDURING LINE CHECK MX FOUND EMERGENCY LIGHTS AT ROWS 8-10 AND LT OVER WING EXIT SIGN INOP. MX REPLACED FUSE AT LT FORWARD EXIT SIGN LIGHT. OPS CHECK OF LIGHTS NOW CHECK GOOD.SDR YYFA201000012Pa System · inoperativeP.A. INOPERATIVE ALL STATIONS.SDR YYFA201000010APa System · inoperativePA WAS INOP IN ALL STATIONS.SDR DALA109699865Battery Pack · inoperativeON FLIGHT CHECK, MX FOUND EMERGENCY PATH LIGHTS INOP IN ROWS 14-18. MX REPLACED LT EMERGENCY LIGHT BATTERY. OPS CHECK OF LIGHTS NOW CHECK GOOD.SDR FDEA201004281375Module · inoperativeDURING CLIMBOUT, CABIN FAILED TO STABILIZE AT 5200FT. CABIN ALTITUDE FOR CRUISE FLT 340 AT CRUISE FLT (340), CABIN ALT EXCEEDED 10000FT. DESCENT INITIATED AND MANUAL PRESSURIZATION WAS SELECTED AND OUTFLOW VLV WAS FULL CLOSED, CARGO HEAT VLV WAS CLOSED, 2 SDR DALA108749995Fuse · failedDURING MX CHECK FOUND LAST 4 SEAT EMERGENCY TRACK LIGHTS INOP. MX FOUND FUSE BLOWN IN BATTERY PACK. REPLACED FUSE AND OPS CHECK OF LIGHTS IS NOW GOOD IAW AMM 33-51-04.SDR TRBA2010035O-Ring · leakingDURING CLIMB OUT WHEN SELECTING BLEED VALVES ON , IN THE COCKPIT WE GET A NOXIOUS DIRTY SOCK EXHAUST SMELL, SMELL GOES AWAY WHEN DESELECTING NR 1 BLEED VALVE. R& R LT ENG NR 5, 6 AND 7 SCAVENGE TUBE O-RINGS IAW MM 72-01-50, NO SMELL NOTED AT THIS TIME, NO LEA
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