Pratt & Whitney JT8D-15
Service difficulty reports · 2,710
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 = 'JT8D15' 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 = 'JT8D15' 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 C7WA200400038Transducer · inoperativeAIR RETURN: DURING CLIMBOUT UPPER RUDDER DEFLECTED TO FULL RT YAW DAMPER POSITION THEN BEGAN OSCILLATING LT TO RT CONTINUOUSLY. REMOVED AND REPLACED UPPER YAW DAMPER TRANSDUCER. SYSTEM OPERATIONAL CHECKS NORMAL.SDR AWXA200401011Packing · tornEN ROUTE, NR 1 ENG SHUTDOWN AT 27,000 FT, ATTEMPTED RESTART WITHOUT SUCCESS, DECLARED EMERGENCY & LANDED WITHOUT FURTHER EVENT. MX FOUND SEALS ON PRESS DUMP VALVE INPUT FUEL LINE TORN & LEAKING. REPLACED SEALS, ENGINE RUN OPERATIONAL CHECK WAS GOOD. MX R/R LSDR DHL2004752009Indicator · failedF/O'S A/S INDICATOR FAILED ON T/O ROLE AT 80KIAS INDICATED 60 KIAS AT 165,000, LBS 18 DEGREES C, PA 830 IN NORMAL BRAKE ENERGY ZONE NOTE: 0 KIAS INDICATION IS THE SAME AS 60 KIAS THERE WAS NO A/S INDICATION IE NEEDLE MOVEMENT ON THE CO-PILOTS SIDE A/S FAILED FSDR DHL2004780503Rib · crackedDURING A C-CHECK THE FOLLOWING DISCREPANCIES WERE NOTED; NR 3 SLAT IB AND OB ACT. ATTACH FRAMES WS 515 ARE CRACKED IN RADIUS. STOP DRILLED CRACKS IAW SRM 57-50-3 FIG 9 ON NR 3 SLAT IB AND OB ACT. ATTACH FRAMES AT WS 515, FABRICATED REPAIR DOUBLERS FROM .032 CSDR DHL2004748006Light · inoperativeDURING PRE-DEPARTURE CHECK FOUND L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE.REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT ASSY IAW MM 33-50-71/SYST, OPS CHECKED GOOD.SDR CA040831013Line · leaking(CAN) LOST (A) SYSTEM HYDRAULICS. FOUND RT MLG UPLOCK HYDRAULIC LINE LEAKING AT ACTUATOR. LINE REPLACED IAW AMM 32-32-11 P/N BACH8A0LEE0260T. RT MLG UPLOCK LINE PRESSURIZED AND LEAK CHECKED SERVICEABLE. NR 1,2 ENG PRESS FILTERS CHECK OK IAW MM 29-11-71 NR 1SDR DHL2004746006Battery · inoperativeENTRY WAY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED ENTRY EMERGENCY EXIT LIGHT BATTERIES. OPS TEST NORMAL IAW M/M 33-50-71.SDR CA040827001Door · out of adjust(CAN) IN CRUISE, CREW NOTICED THE MAIN CARGO DOOR UNSAFE LIGHT ILLUMINATED. IAW CHECKLIST, CREW DEPRESSURIZED AND DESCENDED INTO NEAREST AVAILABLE MAINTENANCE BASE. DOOR WAS VISUALLY INSPECTED AND A/C RETURNED TO SERVICE. UPON COMPLETION OF FINAL LEG, MAINTENASDR CA040825011Skin · delaminated(CAN) DURING A B-CHECK, WALKAROUND FOUND LT SIDE OF THE RUDDER DELAMINATED. FURTHER INSPECTION FOUND DELAMINATION TO BE BEYOND LIMITS OF SRM 55-40-1 FIG 1,K. THE DELAMINATION IS CENTERED AT THE BAYAPPROX. RUDDER STATION 121. FERRY FLIGHT AUTHORIZED FROM XXX TOSDR COOSDR040031Floorbeam · corrodedMAIN CARGO CABIN, BODY STA 1110, UPPER CAP CORRODED IN SEVERAL PLACES, WL 208.1.SDR 04FDEA02529Doubler · damagedNR 1400, RT STA 600-620 STR 9, SKIN REPAIR DOUBLER REQUIRES FURTHER EVALUATION. REMOVED SKIN DOUBLER AT STA 600 STR 9 RH AND REPAIRED PER SRM 53-30-3 FIG 3, REPAIRED DAMAGED STRINGER AT STA 600 9 RH PER SRM 53-10-3 AND REPAIRED DAMAGED TEAR STRAP AT STA 600 SDR 04FDEA02530Skin · bentAFT CARGO DOOR CUTOUT LOWER EDGE SKIN /DOUBLERS ARE BENT. REPAIRED DAMAGED AFT CARGO DOOR CUT-OUT SKIN/DOUBLERS PER EA 7-5330-55360SDR CA040825009Cap · leaking(CAN) AIRCRAFT TURN BACK DUE TO LOSS OF HYDRAULIC FLUID SYSTEN B IN FLIGHT. ON INSPECTION FOUND PLUG ON NR2 SPOILER ACTUATOR LEAKING. REPLACED PLUG P/N 66-22774-1 IAW CMM OVH 27-60-41. B SYSTEM CASE DRAIN FILTER TO B SYSTEM PRESS FILTERS CHECKED FOR CONTAMINSDR ABXA040296Control Box · malfunctionedAFTER SELECTING GEAR DOWN, NOTED A RT GEAR UNSAFE LIGHT. THE LIGHT CHANGED FROM GREEN TO RED 3 TIMES. MISSED APPROACH AND CYCLED GEAR, UNLOCK REMAINED GREEN. (NOTE: INBOUND PROBLEM ON FLIGHT 194 8/16 OPS) PERFORMED SEVERAL GEAR SWINGS IAW AMM 32-60-00-2 WITH NSDR EE4Y040009Floorbeam · corrodedMAIN CARGO CABIN, AT B STA 1050 FROM LBL 63 INCHES TO RBL 56 INCHES FLOORBEAM UPPER CHORD WITH HEAVY CORROSION IN SEVERAL PLACES.SDR COOSDR040012Skin · corrodedWING CENTER SECTION FROM STA 740 TO STA 745 BETWEEN LBL 67.000 INCHES AND LBL 61.000 INCHES, UPPER SKIN PANEL WITH CORROSION ON OUTER SURFACE.SDR COOSDR040013Floorbeam · corrodedMAIN CARGO CABIN AT B STA 480 FROM RBL 62 INCHES TO LBL 65 INCHES FLOORBEAM UPPER CHORD WITH CORROSION IN SEVERAL PLACES.SDR COOSDR040018Plate · corrodedLT WING, FRONT SPAR LOWER CHORD PLATE FROM FSS 731 TO FSS 759, WITH CORROSION.SDR COOSDR040023Skin · corrodedWING CENTER SECTION LOWER SKIN AFT SECTION BETWEEN LBL 30 AND RBL 30 SKIN OUTER FACE CORRODED.SDR COOSDR040024Floorbeam · corrodedMAIN CARGO CABIN BS 720A FLOORBEAM UPPER CHORD CORRODED.SDR COOSDR040025Floorbeam · corrodedMAIN CARGO CABIN, BS 950F, WL 208 FLOORBEAM UPPER CHORD CORRODED.SDR COOSDR040026Skin · corrodedAFT CARGO COMPARTMENT, NR 3 CARGO DOOR CUTOUT SKIN CORRODED AT THE INTERNAL SURFACE.SDR COOSDR040027Floorbeam · corrodedMAIN CARGO CABIN, BS 1130 FLOORBEAM UPPER AND LOWER CHORD, CORRODED.SDR COOSDR040028Beam · damagedLT HORIZONTAL STABILIZER, T/E UPPER BEAM REPAIR.SDR COOSDR040029Floorbeam · damagedMAIN CARGO CABIN, BS 1070, FLOORBEAM DAMAGED. REPAIRED.SDR 04FDEA02470Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 22L AND 23L. REPAIRED FRAME AT BS 520 BETWEEN STR 22L AND 23L IAW SRM 51-40-3 AND EA 7-5310- 70673.SDR 04FDEA02471Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 520 BETWEEN STR 24L AND 25L. REPAIRED FRAME AT BS 520 BETWEEN STR 29L AND 25L IAW SRM 51-40-3 AND EA 7-5310- 70673.SDR 04FDEA02472Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 660 ABOVE STR 24L. REPAIRED BS 660 FRAME ST STR 24L IAW SRM 51-40-3 FIG 1.SDR 04FDEA02473Frame · dentedFWD CARGO COMPARTMENT FRAME DENTED STA 680 ABOVE STR 24L. REPAIRED BS 680. FRAME AT STR 24L IAW SRM 51-40-3 FIG 1.SDR 04FDEA02474Floorbeam · corrodedCORROSION IN COCKPIT AT 25G BEAM UPPER FLANGE BS 267 WL 208. REMOVED AND REPLACED G-BEAM CHORD IAW SRM 51-30-5, 51-30-2, 51-30-8.SDR 04FDEA02456Keelbeam · corrodedCORROSION ON RT KEELBEAM, STR 29 RT, BS 950D PLUS 8. CORROSION ON RT KEELBEAM BS 950D PLUS 8. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REPAIRED IAW FED-EX 27-53-023A.SDR 04FDEA02457Keelbeam · corrodedCORROSION ON RT KEELBEAM, STR 29 RT, BS 950D+15. CORROSION ON RT KEEL BEAM BS 950D15, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1.SDR 04FDEA02459Keelbeam · corrodedCORROSION ON KEELBEAM STR 29L, 950F+9 ON FLANGE AROUND HILOCK. CORROSION ON LT KEELBEAM BS 950F+9, FOUND TO BE OUT OF LIMITS. IAW SRM 53-10-1. REPAIRED IAW MM 27-53-013.SDR 04FDEA02461Stringer · corrodedCORROSION FOUND WHILE WORKING NRC NR00286 FOUND CORRODED STR 30 AT BS 1084 BL 0. REPAIRED STR 30 AT BS 1084 IAW SRM 53-10-3SDR 04FDEA02462Hose · leakingON GEAR RETRACTION, HYD SYSTEM A QUANTITY WENT TO ZERO. NUMEROUS SAFETY WIRES BROKEN IAW EMERG PROC. BOTH A PUMPS OFF IMMEDIATELY, HYD FLUID SHUTOFFS CLOSED 5 MINUTES LATER, NR 1 AND NR 2 ENGINES SHUT DOWN APPROX 45 MINUTES AFTER THAT. FOUND LEAKING RT GESDR 04FDEA02458Keelbeam · corrodedN00636 CORROSION, ON KEELBEAM STR 29L .950F 3 ON FLANGE AROUND FASTENER. ** SD COMING **SDR 04FDEA02460Angle · corrodedN00734 CORROSION ON FWD CARGO COMPARTMENT FLOOR SUPPORT WEB LOWER ANGLE STA 490 TO 500 LBL 9. REMOVED ANGLE AND FABRICATED, ALODINED AND PRIMED AND INSTALLED ANGLE IAW SRM 51-20-1, SRM 51-30-2, FED-EX MM 51-20-151-7SDR 04FDEA02445Stringer · dentedDENTED STRINGER 7R BS618. TRIMMED OUT DAMAGE IAW SRM 53-10-1SDR 04FDEA02442Stringer · dentedDENTED STRINGER 7L BS 720E PLUS 18 INCHES. REPAIRED STR 7L, BS 720E PLUS 18 PER SRM 53-10-3 FIG 2. DETAIL I & FED EX EA 7-5310-55358SDR 04FDEA02443Stringer · dentedDENTED STRINGER 7R BS 720C PLUS 18 INCHES. REPAIRED STR 7R, BS 720C PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL I & FED EX EA 7-5310-55358SDR 04FDEA02444Stringer · dentedDENTED STRINGER 7R BS678. REPAIRED STR. 7R AT BS 678 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358SDR 04FDEA02446Stringer · dentedDENTED STRINGER 7R, BS 558. REPAIRED STR 7R BS 558 PER SRM 53-10-3 FIG 2 & FED EX EA 7-5310-55358SDR 04FDEA02447Stringer · dentedSTRINGER DENTED AT BS 950C PLUS 18, STRINGER 7 RT. REPAIRED STR 7R. BS 950C PLUS 18 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358SDR 04FDEA02448Stringer · dentedSTRINGER DENTED AT BS 950F+18, STRINGER 7 RT ** SD COMING **.SDR 04FDEA02449Stringer · dentedSTRINGER DENTED AT BS 1088, STRINGER 7 RT. REPAIRED STR 7R BS 1088 PER SRM 53-10-3 FIG 2 DETAIL 1 & FED EX EA 7-5310-55358SDR 04FDEA02450Stringer · dentedSTRINGER DENTED AT BS 950F 18, STRINGER 7 LT. REPAIRED STR 7L BS 950F PLUS 18 PER SRM 53-10-3 FIG 3 DETAIL 1 & FED EX EA 7-5310-55358SDR 0401319919Line · rupturedFLIGHT CREW NOTICED THE LOSS OF HYDRAULIC FLUID FROM THE RT SYSTEM WHEN THE (RUDDER CONTROL MANUAL) LIGHT ILLUMINATED. COM PROCEDURES WERE COMPLIED WITH AND THE FLIGHT CONTINUED TO SCHEDULED DESTINATION. LANDING AT MSP WAS UNEVENTFUL. MAINTENANCE FOUND A RUPTUSDR C8GA20040016Engine · leakingDURING CLIMB, NR 1 ENGINE LOST 1.5 GALLONS OF OIL IN THE FIRST 10 MINUTES. AIRCRAFT RETURNED TO TOL AND LANDED WITHOUT FURTHER INCIDENT. FOUND EXCESSIVE AMOUNT OF OIL LEAKING FROM THE NR 4.5 TO NR 6 BEARING DRAIN. REPLACED THE NR 1 ENGINE. OPS AND LEAK CHESDR DHL2004752005Accessory Unit · malfunctionedAFTER T/O, LANDING GEAR LEVER WOULD NOT MOVE PAST (OFF) POSITION. CONDUCTED ABNORMAL PROCEDURE T/O CONFIG WARNING HORN SOUNDED AT FLAPS 2 DEG. DIVERTED BACK TO KDAL IAW RE-RELEASE AT 0359Z (SR). REMOVED AND REPLACED LGAU IAW MM 32-09-121. OPS CK GOOD. LG HANSDR DHL2004747005Control Unit · inoperativeMAIN GEAR ANTI- SKID OB INOPERATIVE, (LIGHT REMAINED ILLUMINATED AND IB INOPERATIVE LIGHT WOULD NOT TEST. TO ADD , OB ANTI SKID ILLUMINATED WHILE ON APPROACH. REMOVED AND REPLACED ANTI-SKID CONTROLLER IAW MM 32-42-0. NO DEFECTS NOTED.
Back to Pratt & Whitney JT8D-15