Pratt & Whitney JT8D-9A
Service difficulty reports · 1,388
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 = 'JT8D9A' 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 = 'JT8D9A' 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 DHL2006745001Engine · malfunctionedEPR INDICATIONS ERRATIC ON NR 2 ENGINE DURING TAKEOFF. REJECTED AC WEIGHT 156.9 LBS OPT 0 DEGREES C BRAKE ENERGY CHART REFERENCED RAN ENGINE AFTER SELECTING EAI AND EPR INDICATIONS WERE NORMAL. DEPARTED NORMALLY. NOTED BY MAINTENANCE REJECTED T/O, PAPERWORKSDR 06FDEA0118Sill · misdrilledBS 480-620 MCD CUTOUT OB SILL UPPER SURFACE HAS SEVERAL OPEN HOLES. COMPLIED WITH FED EX EA 7-5310-98574.SDR 06FDEA0117Frame · mismanufacturedN01345 FASTENER HOLES IN STUB FRAME HAVE SHORT SPACING AND EDGE MARGIN BS 611.5, LBL 22.SDR 06FDEA0120Frame · misdrilledN01348, BS 620 LBL 26 BOTH FRAME HALVES HAVE DRILL STARTS COMMON TO OEM SKIN. COMPLIED WITH FED EX EA 7-5310-98573.SDR 06FDEA0121Lap Joint · misdrilledN01349, BS 620 LBL 26 STR 4L LAP HAS HOLES WITH LESS THAN 4D FASTENER SPACING.SDR 06FDEA0122Tear Strap · misdrilledFASTENER HOLES IN TEAR STRAP HAVE SHORT SPACING AND EDGE MARGIN B.S. 640, LBL 25. REPAIRED TEAR STRAP AT BS 640 LBL 25 PER FED-EX EA 7-5330-98635.SDR 06FDEA0123Skin · damagedN01351, BS 660 LBL 25 TEAR STRAP HAS OPEN HOLES. LAP HAS 2 OPEN HOLES AT LBL . COMPLIED WITH FED EX EA 7-5330-98570SDR 06FDEA0124Frame · misdrilledN01352, BS 640 LBL 25 FRAME HAS A DRILL START COMMON TO OEM SKIN. COMPLIED WITH FED EX EA 7-5310-98575.SDR 06FDEA0125Sill · misdrilledBS 568 LBL22-24 MCD CUTOUT OB SILL UPPER SURFACE HAS 2 FASTENER HOLES WITH NO EDGE MARGIN. COMPLIED WITH FED EX EA 7-5310-98587.SDR 06FDEA0126Sill · misdrilledN01355, BS 617 LBL 22-24 MCD CUTOUT OB SILL UPPER SURFACE AFT OB HOLE HAS LESS THAN 2D EDGE MARGIN. (FASTENER HOLE SIZE .375 EDGE MARGIN .485) COMPLIED WITH FED EX EA 7-5310-98586.SDR 06FDEA0127Frame · misdrilledN01356, BS 620 LBL 23 FWD FRAME SEGMENT HINGE HOLE HAS LESS THAN 2D EDGE MARGIN. (HINGE HOLE SIZE .375 EDGE MARGIN .500).SDR 06FDEA0128Angle · misdrilledN01357 BS 480 STR 2R ATTACH ANGLE HAS 2 EA DRILL STARTS. FABRICATED NEW STRINGER ATTACH ANGLE PER SRM 51-10-2, 51-10-3, 51-30-2, 51-30-5.SDR GAIA05039OPFilter · bypassingDURING CLIMB, OIL FILTER BYPASS LIGHT ILLUMINATED. RETARDING THROTTLE DID NOT EXTINGUISH. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW ABNORMAL PORCEDURES. NOTE: THE ENGINE WAS WINDMILLING FOR ABOUT 15-20 MIN AND OIL PRESSURE WAS ABOUT 20-25 PSI. FLIGHT RETSDR GAIA05040OPOil Filter · bypassingDURING CRUISE, DURING FLIGHT VIBRATION AND NOISE FOLLOWED BY OIL FILTER BYPASS LIGHT ON NR 3 ENGINE. NR 3 EINGINE SHUTDOWN AND ENGINE WINDMILLING PROCEDURE FOLLOWED (OIL FILTER BYPASS LIGHT WENT OUT BELOW 25 PERCENT, N2) NOTE: ENGINE WINDMILLED FOR 38 MIN AT SDR XN0A1286Relief Valve · out of adjustNR 1 ENGINE OIL PRESSURE WENT TO REDLINE ON THROTTLE. TO TAKEOFF POWER. ADJUSTED OIL PRESSURE RELIEF VALVE TO 43 PSI AT IDLE IAW MM 72-00. OPS AND LEAK CHECKS GOOD AT IDLE. (ORIG/CLOSED)SDR 05FDEA04388Switch · malfunctionedPASSING FL250 RECEIVED INTERMITTENT LE FLAPS AMBER INDICATOR ON FORWARD PANEL WITH INTERMITTENT NR1 SLAT INDICATOR ON S/O AUX PANEL. RAN RED TABS WITH NORMAL EXTENSION TO FLAPS 30. REPLACED NR 1 SLAT RETRACT SWITCH IAW 27-82-011-4, REPLACED NR1 SLAT ACTUASDR 05FDEA04386Shear Tie · corrodedN01273 BS 950A S28-29R RBL10-15 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED IAW SRM 51-30-2.SDR 05FDEA04387Shear Tie · crackedN01277 BS 950F LBL 12 WL 140 SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-4, AND SRM 51-30-09.SDR 05FDEA04318Repair · unknownREPAIR LOCATED AT STA 303.9 STRINGER 15-L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ITEM NR 4, VISUALLY INSPECTED REPAIR AT STA 303.9 STRINGER 15-L. FOUND TO BE IAW SB 727-53A0198 AND EA 7-5SDR 05FDEA04348Frame · damagedRT FUSELAGE INTERNAL FRAME REPAIR DOUBLER 12 INCHES BY 2.5 INCHES, LOCATED AT BS 660, STRINGER 6 REQUIRES EVALUATION TO DETERMINE IF THE REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IAW APPROVED DATA. REPAIRED FRAME DOUBLER BS 660 STR 6 SRM 53-10-4.SDR 05FDEA04174Floorbeam · corrodedAFT PIT MAIN DECK FLOORBEAM HAS CORROSION AT FASTENER CLIP AT STA, BS 950F, LBL21.0. REMOVED CORROSION IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 4. REMOVED AND REPLACED FLOORBEAM UPPER TEE CAP SECTION FROM LBL8 TO LBL70 IAW STANDSDR 05FDEA04175Floorbeam · corrodedFORWARD CARGO COMPARTMENT STA BS 620 BOTTOM SURFACE OF FLOORBEAM UPPER TEE CAP HAS CORROSION AROUND SCREW HOLES LBL50 TO RBL50. REMOVED DAMAGED SECTION OF TEE CAP AT STA BS 620 BETWEEN LBL45 AND RT CUSP. FABRICATED NEW TEE CAP, SPLICES, SHIMS: ALODINED ANDSDR 05FDEA04176Floorbeam · corrodedMAIN CABIN FLOORBEAM HAS CORROSION AT FASTENER HOLES AT STA BS1130 BETWEEN RBL14 AND RBL40. REPAIRED OUT OF LIMTS SECTION OF STA BS 1130 FLOORBEAM IAW SRM 53-10-8 FIGURE 10. ALODINED AND PRIMED BARE METAL AREAS IAW SRM 51-10-2. INSTALLED REPAIR WITH WET SDR 05FDEA04177Rib · gougedWHILE WORKING CARD NR N00763 FOUND RT NR 5 ELEVATOR HINGE, SUPPORT RIB L/E GOUGED. REPAIRED RIB PER FED EX EA 7-5510-91427.SDR 05FDEA04172Skin · bulgedN00204 BS 206, STR 24-24L, 2 INCH CREASED BULGE IN THE SKIN. REPAIRED FUSELAGE SKIN AT BS 206, STR 24L-25L AS PER FED EX EA 7-5310-91431SDR 05FDEA04152Floorbeam · gougedMAIN DECK TOP SIDE OF FLOORBEAM GOUGED AT STA BS680 LBL47 TO LBL57. REMOVED DAMAGED, FABRICATED REPAIR ANGLES FROM 17-7PH CRES STEEL .063 INCH, FABRICATED FILLER AND INSTALLED REPAIR ANGLES AND FILLER IAW SRM SR27-53-034 REV E. INSTALLED SEAT TRACK AT LBL65SDR 05FDEA04153Hinge Fitting · wornRT HORIZONTAL STABILIZER IB NR1 ELEVATOR HINGE FITTING ON HORIZONTAL STABILIZER HAS IB FACE OF FITTING WORN. REMOVED BUSHING, SPOTTED FACE, HFEC INSPECTED LUG BORE FABRICATED AND INSTALLED REPAIR WASHER AND NEW BUSHING ALL IAW EA NR 7-5510-91317. THISDR 05FDEA04154Beam · corrodedSEAT TRACK ATTACH TEE CAP HAS CORROSION OUT OF LIMITS AT LBL45 FROM STA BS760 TO STA BS850. REMOVED SEAT TRACK FROM BS 740 TO BS850 AT LBL45 IAW SRM 51-30-2. REMOVED, REPLACED AND INSTALLED NEW UPPER CHORD FROM STA BS 760 TO STA BS850 AT LBL45 IAW BAC DRASDR 05FDEA04155Floorbeam · corrodedCABIN FLOORBEAM UPPER TEE CAP CORRODED AT STA BS 344 BETWEEN LBL24 AND RBL24. CUT OUT CORRODED SECTION OF TEE CAP FROM LBL45 TO RBL24 IAW SRM 53-10-8 FIGURE 9. FABRICATED NEW TEE SECTION AND SPLICE ANGLES IAW SRM 53-10-8 FIGURE 9. ALODINED AND PRIMED REPASDR 05FDEA04160Frame · corrodedN01022, CORROSION (C53-113-01(2)) ON LOWER CHORD AROUND NUTPLATE HOLE BS 1130 RBL 24 WL 201. REMOVED CORROSION ON LOWER CHORD BS 1130 RBL 24, WL 201, FOUND TO BE OUT OF LIMITS, REPAIRED LOWER CHORD IAW SRM 53-10-8 FIG 10.SDR 05FDEA04157Floor Support · corrodedN00770 CORROSION (C53-221-01) BS 304, WL 208, LBL 12 TO 50 HOZ FLOOR SUPPORT UPPER FLANGE. REPAIRED FLOOR SUPPORT IAW SRM 51-30-2.SDR 05FDEA04147Structure · damagedAFT CARGO DOOR, LOWER CHORD, UPPER TEE CAP AT STA BS 950D TO BS 950E, ABOVE STRINGER 27-R HAS SEVERAL HOLES WITH NO EDGE DISTANCE AND MINIMUM SPACING. REPAIRED DAMAGED CHORD IAW B727 SRM 51-40-4 FIGURE 1. REMOVED AND REINSTALLED 4 EACH CHORD FITTINGS, FISDR 05FDEA04144Intercostal · crackedINTERCOSTAL CRACKED BS 950B-2, STR 29R WL 155. REPAIRED IAW SRM 51-40-2.SDR 05FDEA04145Flap Track · corrodedN01126 LT WING IB FLAP OB FLAP TRACK CORRODED ON AFT ATTACH POINT. ** SD ** COMING REPLACED FLAP TRACK IAW W/C 27X5705-03SDR 05FDEA04001Frame · dentedAFT CARGO COMPARTMENT, DENT IN FRAME BS 950C RBL 36 WL 152. REMOVED DENT DAMAGE AREA, FABRICATED REPAIR PART AND INSTALLED IAW SRM 51-40-3.SDR 0501639952Pressure Valve · failedAS THE AIRCRAFT WAS TAXING OUT FOR DEPARTURE THE RT HYDRAULIC SYSTEM LOST FLUID AND PRESSURE. THE AC RETURNED TO THE GATE WITHOUT ANY FURTHER PROBLEMS. MAINTENANCE FOUND THE RT HYDRAULIC SYSTEM PRESSURE RELIEF VALVE HAD FAILED AND REPLACED IT. ALSO THE RT ELECSDR DHL2005745013Switch · malfunctionedDURING TAKEOFF ENG NR 2 WAS NOT MAKING TAKEOFF THRUST. ENG NR1, NR3 WERE NORMAL AT 80 KTS WITH THRUST LEVERS MATCH, NR2 EPR WAS AT 1.6 NOT INCREASING, N1 WAS ABOVE RED LINE. REJECTED T/O AT 80KTS,170,000 LBS 3860 PRESSURE. ENGINE RUNUP PERFORMED IAW JRH. NSDR 72300250Valve · failedNR 2 ENGINE OIL TEMPERATURE IN HIGH RANGE FOR 15 MINUTES WITH NR 2 FUEL HEAT VALVE ALREADY DEFERRED. ABNORMAL PROCEDURE GUIDELINES IN AOM REQUIRED PRECAUTIONARY ENGINE SHUT DOWN. AIRCRAFT RETURNED TO TUS.SDR GAIA05033OPSwitch · out of adjustDURING CLIMB FROM 14,000 FEET THE (MAIN CARGO DOOR NOT CLOSED) LIGHT ILLUMINATED. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. ON DECENT THE LIGHT WENT OFF AT 12,000 FEET. AN UNEVENTFUL LANDING WAS MADE AT DEPARTURE. THE MAIN CARGO DOORSDR TSAA0532055Tire · failedDURING TAXI AFTER LANDING, CREW HEARD A LOAD POP FOLLOWED BY VIBRATION FROM THE NOSEWHEEL AND STEERING DIFFICULTY. CREW STOPPED AIRCRAFT ON TAXIWAY. MAINTENANCE FOUND HOLE IN LT NOSEWHEEL AND BOTH TIRES FLAT. REMOVED AND REPLACED BOTH NOSEWHEEL TIRES, INSPESDR GAIA05027STSkin · crackedDURING B-CHECK A 1 INCH CRACK WAS FOUND ON THE FUSELAGE SKIN AT STA 530 STRINGER 26R ON THE LAP SEAM BELOW THE C-1 CARGO DOOR. THE SKIN WAS REPAIRED IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR GAIA05028STSpar · crackedDURING B-CHECK A FUEL LEAK WAS FOUND ON THE FUSELAGE AT STA 740. INSPECTION REVEALED A CRACK ON THE WING CENTER SECTION SPAR WEB. THE WING SPAR WEB WAS REPAIRED IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR 05FDEA03496Case · crackedNR 1 ENGINE IGV CASE CRACKED 3 PLACES ALONG FWD. AND AFT SIDE WELD BEAD. REMOVED NR 1 ENGINE IGV CASE ON WK CARD 7200-2002,N/R00937. REMOVED AND REINSTALLED ENGINE NOSE COWL ,NOSE DOME FOR ACCESS IAW MM 71-10-021-4, MM71-10- 041-4 LEAK AND OPS. CHECKED GOSDR CA051027004Bolt · sheared(CAN) DURING A ROUTINE WHEEL CHANGE, IT WAS FOUND THAT 2 OF THE 3 BRAKE RETAINING BOLT HEADS HAD SHEARED. THE BROKEN BOLT HEADS HAD BECOME TRAPPED BETWEEN THE BRAKE AND WHEEL INNER HALF CAUSING SCORING DAMAGE TO THE WHEEL. IT IS SUSPECTED THAT THE COUNTERSUNKSDR TSAA0532050Anti-Skid Sys · deactivatedON CLIMB OUT, PILOT OBSERVED THE LT ANTI-SKID LIGHT ON AND STAYED AND RETURNED BACK TO DEPARTURE. THE ANTI-SKID SYSTEM WAS MEL’D WAITING FOR AN ANTI-SKID CONTROL BOX. THE ANTI-SKID SYSTEM AND ANTI-SKID BRAKES WERE DEACTIVATED.SDR TSAA0527048Actuator · leakingCREW HAD INDICATION OF HYDRAULIC SYSTEM A, DROP IN PRESSURE. CREW DECLARED AN EMERGENCY AND WERE ABLE TO DEPLOY THE LANDING GEAR. LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 1 SPOILER ACTUATOR AND INSPECTED AND REPLACED BOTH ENGINE CASE DRASDR XNOA1271Outflow Valve · malfunctionedAIRCRAFT FAILED TO PRESSURIZE MORE THAN 2 PSI DIFFERENTIAL. R & R THE RT FLOW CONTROL VALVE IAW MM 36-12-61, SYSTEMS OPS CHECK GOOD. (STATUS:ORIG/CLOSED)SDR XN0A1260Door · out of adjustPILOT REPORT, COULD NOT PRESSURIZE A/C. RE-ADJUSTED EE DOOR IAW MM 52-40-11.SDR CA050810001Pitot System · fod(CAN) ON TAKEOFF ROLL, NO AIRSPEED INDICATION ON THE CAPTAINS SIDE. DEBRIS FOUND IN CAPTAINS UPPER LT PITOT TUBE. BUG REMOVED AND PITOT/STATIC SYSTEM TESTED SERVICEABLE. TIMES: 63714:40 CYCLES: 61165.SDR XN0A1253Exciter · failedON ENGINE START NR 2 ENGINE WOULD NOT START, START VALVE OPENS PRESSURE DROP NO EGT. REMOVED AND REPLACED NR 2 ENG EXCITER BOX IAW MM 74-11-1, OPS GOOD.
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