Pratt & Whitney JT8D-9
Service difficulty reports · 686
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 = 'JT8D9' 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 = 'JT8D9' 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 KNNA200700015Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT WL-234, LBL-8 TO LBL-9. PROVIDE INSTRUCTION ON REPAIR OF BULKHEAD AT STA 178 LBL 8 - LBL 9 AND LBL-10-LBL 12.SDR KNNA200700017Vertical Beam · crackedFOUND LBL 5.7 VERTICAL BEAM IS CRACKED BOTH FLANGES AT STA 178 BULKHEAD. PROVIDE INSTRUCTIONS ON REPAIR OF LBL 5.7 VERTICAL CHORD AT STA 178.SDR KNNA200700018Frame · crackedFOUND STA 178, LT SIDE FRAME IS CRACKED AT W/L 195. PROVIDE INSTRUCTION ON REPAIR CRACK BY INSTALLING A SPLICE OVER THE (LEFT SIDE) SIDE CHORD AT WL 212.SDR KNNA200700013Skin · damagedE/E BAY ACCESS DOOR EXTERIOR SURFACE, RT EDGE BEND. PROVIDE INSTRUCTIONS ON REPAIR OF E/E BAY DOOR .SDR KNNA200700016Stringer Splice · activeFOUND CRACKED CHORD OF STRINGER 14L AT BS 663.75. PROVIDE INSTRUCTION ON REPAIR OF S14L AT BS 663.75.SDR KNNA200700005Attach Fitting · corrodedCORRODED REINFORCING CLIP ON STRINGER 27-L, BS 1016. COMPLIED ACO 0653125, REPLACE CORRODED PRODUCTION SPLICE.SDR KNNA200700006Frame · crackedFOUND CRACKED FRAME ON BL-0, B,STA-727. REPAIRED FRAME IAW ACO NR 0653122. INTERIM REPAIR INSP EVERY 5,000 FLIGHT HOURS.SDR KNNA200700008Frame · crackedFOUND CRACKED FRAME ON LBL-24, B-STA727. INSTALLED INTERIM REPAIR, REQ, INSP EVERY 5,000 F/HRS.SDR KNNA200700007Frame · crackedCRACKED VERTICAL FITTING ON RBL-26 AND BS 727 AT UPPER LIGHTENING HOLE. REPAIR SKIN PER ACO NR 0653124.SDR KNNA200700004Floorbeam · crackedFOUND CRACK AT FLOORBEAM INTERIOR MAIN PASS CABIN, B-STA 678, LBL25. REPAIRED FLOORBEAM IAW ACO NR 653121.SDR KNNA200700003Skin · corrodedCORROSION AT LOWER LOBE EXTERIOR SURFACE BETWEEN BS 727 AND BS 727A, STRINGER 28-L. COMPLIED ACO NUMBER 0653120. INSTALL REPAIR FUSELAGE SKIN AND DOUBLER BS- 727 KEEL BEAM.SDR KNNA200700002Frame · damagedINSTALLED INTERIM REPAIR AT L2 DOOR CUTOUT AT THE FWD LOWER CORNER. REMOVED INTERIM REPAIR AND INSTALLED PERMANENT REPAIR.SDR KNNA200700001Door Frame · damagedINSTALLED INTERIM REPAIR AT R1 DOOR CUTOUT AT THE AFT LOWER CORNER. REMOVED INTERIM REPAIR AND INSTALLED PERMANENT REPAIR.SDR 465C7Structure · crackedCOMPRESSION CHORD CRACKED ON BULKHEAD B-STA727 AT BL-0 FWD WALL OF AFT CARGO COMPARTMENT.SDR 46501Structure · crackedCOMPRESSION CHORD CRACKED ON BULKHEAD B-STA727 AT BL-0 FWD WALL OF AFT CARGO COMPARTMENT.SDR KNNA200600001Bulkhead · crackedCOMPRESSION FRAME CRACKED ON BULKHEAD BS 727 AT BL 0 FWD WALL OF AFT CARGO COMPARTMENT. CO 0653105 PROVIDE REPAIR INSTRUCTIONS ON REPAIR OF CRACKED WEB ANGLE IN WHEEL WELL AFT BULKHEAD BS 727 BL 0.SDR CA061120009Duct · ruptured(CAN) ENROUTE TO DESTINATION, #2 ENGINE FIRE WARNING. CHECKLIST ACCOMPLISHED, ENGINE SHUTDOWN. 13TH STAGE SADDLE DUCT FOUND RUPTURED, REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC# 20061120009)SDR ABXA060287Linkage · lack of lubeCAPTAIN'S SLIDING WINDOW (EMERGENCY EXIT) WOULD NOT OPEN. LUBED CAPTAIN'S SLIDING WINDOW LINKAGE AS REQUIRED. OPERATIONAL CHECK GOOD IAW MM 56-10-03-5-0002.SDR 2006F00052Relay · defectiveAFTER THE FA'S REQUESTED MORE HEAT IN THE CABIN, SMOKE APPEARED IN THE CABIN AND COCKPIT. INDICATION LIGHTS WERE (1) RT PACK OVERHEAT, (2) RT AIR MIX VALVE. INITIAL INSPECTION BY THE FLIGHT MECHANIC DID NOT FIND ANYTHING WRONG; WHEN OUR ACY STATION MECHANIC SDR 2006F00053Relay · defectiveAFTER THE FA'S REQUESTED MORE HEAT IN THE CABIN, SMOKE APPEARED IN THE CABIN AND COCKPIT. INDICATION LIGHTS WERE (1) RT PACK OVERHEAT, (2) RT AIR MIX VALVE. INITIAL INSPECTION BY THE FLIGHT MECHANIC DID NOT FIND ANYTHING WRONG; WHEN OUR ACY STATION MECHANIC TSDR CA060918010Start Valve · malfunctioned(CAN) THE NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED DURING CLIMB OUT. A/C RETURNED TO BASE. A/C INSPECTED AND THE START VALVE REPLACED DUE CRACKED. A/C RETURNED TO SERVICE. FAULT REOCCURRED DURING CLIMB. A/C RETURNED TO BASE. THE FUEL HEAT DUCT WASSDR 06FDEA2721Compressor · stalledPDIS 484, 72-00 0008702 27JUL06 SDF OPEN R LOGPAGES: 01298762 REJECTED TAKEOFF AFTER ENGINE FAILURE LIGHT ILLUMINATION AND ASSOCIATED BANG NOISE AND VIBRATION. ENT BY: 188726 RPT BY: 251618 FACT 29JUL06, 14:32 SDF R IAW FLT DATA RECORDER NR 3 ENG COMPRESSORSDR 0601229603Manifold · failedDURING CLIMB, THE RIGHT ENGINE FIRE HANDLE ILLUMINATED AND THE FIRE WARNING BELL SOUNDED. THE CREW FOLLOWED THE COM AND THE WARNINGS CEASED. THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE THE RIGHT ENGINE FUEL HEAT MANIFOLDSDR TSAA0672008Engine · defectiveOGG-HNL: ON TAKEOFF NR 2 ENGINE EGT ROSE TO 650 DEGREES CELSIUS. ENGINE THROTTLED BACK UNTIL EGT WAS WITHIN LIMITS AND AIRCRAFT RETURNED TO FIELD WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE IAW FORM M-211, M-212, M-213, AND M-215. NO FAULTS NOTED. ASDR C7W2006F00000Indicator · intermittentAIR RETURN. IB FLAP STUCK AT 15 DEGREES AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD.SDR C7WA200500125Indicator · intermittentAIR RETURN. IB FLAP STUCK AT 15 DEGREES, AFTER TAKEOFF. REMOVED AND REPLACED FLAP POSITION INDICATOR IAW MM. FLAP SYS OPERATIONAL CHECKS GOOD. (K)SDR GAIA05036OPLight · inoperativeDURING MAINTENANCE THE CREW ENTRY DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT. OPS CHECK GOOD. AC WAS RETURNED TO SERVICE. (K)SDR 05FDEA04007Floorbeam · corrodedCABIN FLOORBEAM, UPPER T-CAP CORRODED AT STA BS 440 BL 0 - RBL 24. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1 FIGURE 5. REMOVED DAMAGED T-CAP FROM RBL-8 TO LBL 8 STA BS 440 IAW SRM 53-10-8 FIGURE 3. REMOVED CORROSION FROM RBL 8 TO RBL 24 IAW SRM 51-10SDR 05FDEA03986Skin · corrodedCORROSION AT LOWER FUSELAGE STA BS 480 STRINGER STR 29-L. REMOVED CORROSION IAW SRM 51-10-6. SKIN ORIGINAL THICKNESS .090 MATERIAL LOSS .022 MATERIAL REMAINING .068 FOUND OUT OF LIMITS IAW SRM 53-30-1 UT GAGE T8253C. DOUBLER AND FILLER MATERIAL ID 7075-T6 .SDR 05FDEA03988Frame · corrodedFORWARD CARGO COMPARTMENT, FRAME AT STA BS 720E BETWEEN STRINGER STR 26-R AND STR 25-R IS CORRODED. REMOVED DAMAGE AREA OF FRAME IAW SRM 53-10-4. FABRICATED INNER AND OUTER REPAIR DOUBLER AND FILLER IAW SRM 51-40-3 FIGURE 1. FABRICATED FRAME SECTION IAW MFGSDR 05FDEA04000Stringer Clip · damagedMECHANICAL DAMAGE TO STRINGER CLIP BS 950C STRINGER 5 RT. REPAIRED STRINGER CLIP PER SRM 53-10-1, 51-30-2.SDR 05FDEA03999Skin · chafedLOWER AFT CARGO DOOR OUTER SKIN IS CHAFED ALONG FAIRING RUB STRIP. REPAIRED LOWER AFT CARGO DOOR OUTER SKIN PER 52-00-3 FIG 4.SDR XN0A1274Engine · failedNR 1 ENGINE FAULT ON T/O ROLL AT STEWART, LOUD BAND HEARD FOLLOWED BY EPR REDUCTIVE TOWARDS 0. ALL OTHER ENGINE INDICATIONS NORMAL DURING T/O ROLL.SDR DHL2005742519Floorbeam · corrodedCABIN FLOORBEAM CORRODED ON FLOWER FLANGE LOWER SURFACE BS 1010 LBL 24. CUT OUT CORRODED PORTION OF LOWER LEG OF FLOORBEAM AT BS 1010 LBL 24. FABRICATED AND INSTALLED FLOOR BEAM REPAIRS 18.0 INCH X 1.95 INCH FROM BAC1505-10097, 29.50 INCH X 1.95 INCH FROM 707SDR GAIA05025Light · inoperativeDURING POST FLIGHT, FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSY, CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR DHL2005742517Floorbeam · corrodedAFT PIT CEILING, CABIN FLOORBEAM BS 1070 LOWER SURFACE HAS CORROSION AT LBL 14. REMOVED CORROSION IAW SRM 53-10-8. CORROSION REMOVAL INTO TANGENT OF RADIUS. FABRICATED AND INSTALLED REPAIR STRAP 13.3 INCHES FROM 7075-T6 .100 AND TEE FILLER FROM BAC1505-100797SDR 0501519623Duct · blownDURING CRUISE, CREW HAD TROUBLE REGULATING THE CABIN TEMPERATURE. THE CABIN STARTED TO CLIMB AT 1600 FPM AND THE RED (CABIN PRESS) WARNING LIGHT ILLUMINATED. CREW INITIATED A RAPID DESCENT AND COMPLIED WITH COM PROCEDURES BUT WAS NOT ABLE TO REGAIN CABIN PRESSSDR XN0A1267Hydraulic System · leakingLOSS (A) SYS HYD ON TAKEOFF. (ORIG/OPEN)SDR DHL2005742515Seat Track · gougedS/O 284002 N/R 037550 SEAT TRACK GOUGED AT BS 878 LBL 45. REMOVED FLOOR PANELS AT BS 870 - 950 LBL 24 - 60 IAW SRM 51-30-2. REMOVED GOUGED SEAT TRACK. FABRICATED AND INSTALLED NEW SEAT TRACK 91.00 INCHES X 1.80 INCH FROM 7178-T6511 IAW SRM 53-10-1 FIG. 3 AND 5SDR DHL2005742516Frame · corrodedBS 1070 LBL 65 WL 255 FRAME JUST AFT OF L-2 DOOR HAS A CORROSION BULGE. CUT OUT CORROSION ON FORMED WEB ANGLE ATTACHED TO FRAME AT BS 1070 LBL 65 AFT DOOR CUT OUT AT L-2 DOOR IAW SRM 51-40-3 FIG. 1. REMOVED (T) ANGLE, FABRICATED AND INSTALLED NEW ANGLE 2.75 ISDR DHL2005742513Shear Tie · corrodedS/O 284002 N/R 037490 FWD PIT FUSELAGE FRAME AT BS 720 BETWEEN STR 28L AND STR 28R HAS AN (L) ANGLE WHICH ATTACHES TO THE FUSELAGE SKIN CORRODED IN MULTIPLE AREAS. REMOVED CORROSION BETWEEN STR 28L AND 28R BS 720. FOUND SHEAR TIE TO BE OUT OF LIMITS IAW SRM 5SDR DHL2005742514Skin · gougedRT OB FORE FLAP LEADING EDGE HAS 2 EACH GOUGES ABOUT 12 INCHES OB OF IB EDGE. FABRICATED AND INSTALLED REPAIR DOUBLER 8 INCHES X 3 INCHES FROM 024-T3 .050 FOR RT OB FORE FLAP LEADING EDGE IAW 57-50-4, 51-30-2 AND 51-10-2.SDR DHL2005742512Nut Plate · misinstalledNUT PLATES IMPROPERLY INSTALLED ON FLOOR SUPPORT BETWEEN BS 1070 - BS 1130 STR. 30 (ABOVE) REMOVED DAMAGED FLOOR SUPPORT BETWEEN BS 1070 - 1130. CUT AND FABRICATED NEW SUPPORT 13INCHES FROM BAC1490-2583 AND SPLICES 12 INCHES X 1INCH X 1INCH FROM AND10133-0702SDR DHL2005742520Window Frame · crackedPILOT'S NR 2 WINDOW AFT LOWER INTERNAL CORNER ANGLE CRACKED AND CORRODED. REMOVED FITTING P/N 69-367305, FABRICATED SHIMS IAW EA NR AA15-53-1 REV. IR, DRILLED UP FITTING IAW SRM 51-30-2. INSTALLED FITTING IAW SRM 51-30-2, HEAT CHECK IAW MM 56-12-11 STEP.SDR GAIA05023Engine · failedDURING CRUISE, NR 2 ENGINE LOW OIL PRESSURE LIGHT CAME ON BRIGHT, NOTICED NR 2 OIL PRESSURE DROPPED RAPIDLY TO ZERO. OIL TEMPS AND QUANTITY REMAINED NORMAL. ENGINE FAILURE CHECKLIST WAS PERFORMED. N1S WIND MILLED FOR APPROXIMATELY 25 MINUTES. EMERGENCY WAS SDR RYNA200500022Oil System · overtempDURING CLIMB-OUT, NR 2 ENGINE OIL TEMP INCREASED TO 122 DEG C. DURING DESCENT, OIL TEMP INCREASED TO 140 DEG C. OIL TEMP IN YELLOW BAND FOR 5 MINUTES. OIL PRESSURE WAS NORMAL IN CLIMB AND CRUISE. NR 2 ENGINE SHUTDOWN AS A PRECAUTION BECAUSE OIL TEMP COULD NOTSDR RYAN200500018Bulb · faultyDURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN.SDR 05FDEA00618Shear Tie · corrodedN01607, WHILE WORKING N00929, CORROSION ON SKIN BS 698, FOUND CRACK AND OVERSIZED FASTENER HOLE WITH LIMITED EDGE MARGIN ON SHEAR TIE BS 700 BETWEEN STR 28L AND STR 28R, WL 148. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-4.SDR 05FDEA00619Shear Tie · corrodedN01608 WHILE WORKING N00929, CORROSION ON SKIN BS 698, FOUND CORROSION ON FRAME FORMED SHEAR TIE BS 700 BETWEEN STR 28L TO STR 28R, WL 148. REPAIRED SHEAR TIE PER SRM 53-10-4.SDR 05FDEA00621Skin · crackedN00261, MAIN ENTRY DOOR EXTERIOR SKIN SHOWS EVIDENCE OF A CRACK AT PREVIOUS REPAIR, 9 INCHES BELOW AFT SIDE OF DOOR HANDLE. INSTALLED REPAIR DOUBLER IAW SRM 52-00-3.
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