Pratt & Whitney JT8D-15A
Service difficulty reports · 538
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 = 'JT8D15A' 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 = 'JT8D15A' 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 DHLA200700022Compressor · stalledREJECTED TAKEOFF AT APPROX 20 KNOTS DUE TO AN AUTOPACK TRIP AND AN APPARENT COMPRESSOR STALL.SDR DHLA200700023Compressor · stalledDEPARTING RNWY 22R AT ILN, NR 2 ENG COMPRESSOR STALL OCCURRED AT AN EPR OF 2.05. WIND WERE 290DEG AT 14 GUSTING TO 26 (70DEG X-WIND) IAS -0, OAT - 13DEG, PA - 1077 A/C GW 178.8. FOR INFORMATION ONLY. INSPECTED INLET AND EXHAUST OF NR 2 ENG PER AOM CHPT 1.8 PSDR KNNA200700022Floorbeam · corrodedFLOOR PANEL ATTACH POINT STA 344, LBL 12 IS CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF STA 344, LBL 12 FLOOR PANEL ATTACH POINT. REMOVED AND REPLACED FLOORBEAM SRM 53-10-9 FIG 6.SDR KNNA200700025Skin · corrodedAFT CARGO PIT INTERIOR BILGE, BS 927 BETWEEN STR-27L STR AND 27R, FRAME BOTTOM SIDE CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF CORROSION AFT CARGO PIT, INTERIOR BILGE BS 927 BETWEEN STR 27L AND STR 28 R BOEING SRM 53-10-4 FIGURE 7.SDR KNNA200700026Frame · damagedAFT CARGO PIT, INTERIOR BILGE B-STA 867 BETWEEN STR 27 R AND STR 28 L FRAME BOTTOM SIDE, CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF CORROSION AFT CARGO PIT, INTERIOR BILGE BS 867 BETWEEN STR 27R-27L BOEING SRM 53-10-4 FIGURE 7.SDR KNNA200700021Floorbeam · crackedCARGO FLOORBEAM CRACKED AT BS 460, RBBL 14.5 FWD CARGO COMPARTMENT. PROVIDE INSTRUCTIONS ON REPAIR OF CARGO FLOORBEAM BS 460 RBL 14.5. REMOVED AND REPLACED CARGO DOOR FLOORBEAM SRM 53-10-5 FIGURE 11.SDR KNNA200700024Skin · corrodedCORRODED SKIN AT BS 500A+ 10' BETWEEN STR 27L/28L. PROVIDE INSTRUCTION ON REPAIR OF CORRODED EXTERIOR SKIN STA 500A + 10' STR 27L/28L.SDR KNNA200700020Skin · damagedMAIN ENTRY DOOR L-2 EXTERIOR SURFACE, UPPER AFT CORNER, SKIN BEND. PROVIDE INSTRUCTIONS ON REPAIR OF DOOR SKIN. CUT OUT BEND CORNER AND REPAIR PER SRM 52-00-3 FIGURE 5.SDR KNNA200700023Skin · corrodedFUSELAGE, EXTERNAL SURFACE LOWER LOBE, B-STA 968, STR 27 L CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF FUSELAGE EXTERNAL SURFACE LOWER LOBE BS 968 STR 27 L. BOEING SRM 53-10-3 FIGURE 1 AND 53-30-3 FIGURE 48.SDR CA070202005Duct · missing(CAN) UPON ARRIVAL, MAINTENANCE NOTICED AN APPROXIMATELY 6 INCH HOLE IN NR 1 ENGINE COWL. FURTHER INVESTIGATION DETERMINED THE CAP ON THE 6TH STAGE SADDLE DUCT MISSING, LOCATED IN COWL. CAP INSTALLED AND SECURED IAW MM AND COWL REPAIRED. (TC NR 20070202005)SDR DHL2007743501Frame · corrodedREF ASTAR N/R'S 079970 AND 080116. AFT CARGO COMPT; CORROSION ON FLANGE ON FUSELAGE FRAME AT BS 1166 AND STR 29L. CORROSION OUT OF LIMITS. CUT OUT DAMAGE TO FRAME, 3.125 INCHES X 2.375 INCHES SRM 53-10-4 FIG 11. FABRICATED REPAIR PARTS: FILLER FROM 7075-TSDR CA070202004Wire · shorted(CAN) DURING CLIMB AT FL120, APU FIRE LIGHT AND BELL ILLUMINATED. APU FIRE DRILL CARRIED OUT, REMAINED (ON). DECLARED EMERGENCY, RETURNED TO AIRPORT WITHOUT INCIDENT. UPON INSPECTION NO FIRE DETECTED. MAINTENANCE FOUND (FIRE WARNING) WIRE NR W272-607-18 SHOSDR CA070202003Seal · failed(CAN) DURING CRUISE AT FL320, CABIN RATE STARTED TO CLIMB AT 1500 FPM. CREW (CARGO FIT) DONED O2 MASKS. PRESSURIZATION CONTROLLER SELECTED TO (MANUAL) AND (STBY), NO CHANGE. CARGO HEAT OUTFLOW VALVE CLOSED, RECOVERED PRESSURE. O2 REMOVED, FLIGHT CONTINUED WITHSDR CA061218013Switch · malfunctioned(CAN) NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE WITH LANDING GEAR SELECTED DOWN. VISUALLY INSPECTED TO ENSURE NOSE GEAR WAS DOWN AND LOCKED THROUGH VIEWPORT AND CONFORMED NOSE GEAR WAS DOWN AND LOCKED. AS A PRECAUTIONARY ACTION NOSE GEAR LOCK SWITCH REMOVED ASDR 2006FA0001126Pump · damagedUNIT RECEIVED ON 13 NOV 2006. UNIT PROCESSED ON A REPAIR WORKSHOP IAW CUSTOMER REQUIREMENTS. PUMP FAILED AS RECEIVED BENCH TEST FOR LOW FUEL FLOWS. PUMP DISASSEMBLED IAW CMM REF 73-11-1 TO INVESTIGATE INCOMING TEST FINDINGS. DISASSEMBLY OF FUEL PUMP REVEALSDR CA061219001Duct · disconnected(CAN) LOWER AFT BODY HEAT WARNING LIGHT ILLUMINATED IN FLIGHT. FLIGHT CREW FOLLOWED EMERGENCY CHECKLIST AND LIGHT EXTINGUISHED WHEN NR 3 BLEED AND THRUST LEVER CLOSED. UPON INVESTIGATION MAINTENANCE DISCOVERED SUPPLY DUCT FORWARD OF STA 1183 DISCONNECTED AND SDR 0602489993O-Ring · wornDURING DESCENT, NR 1 ENGINE THRUST WOULD NOT INCREASE ABOVE IDLE. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. ON THE GROUND, THE TOWER REPORTED A SIGNIFICANT FUEL LEAK FROM THE NR 1 ENGINE. MAINTENANCE FOUND THE INLET COUPLING ON SDR 0602499993O-Ring · leakingDURING DESCENT NR 1 ENGINE THRUST WOULD NOT INCREASE ABOVE IDLE. FLIGHT CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. ON THE GROUND THE TOWER REPORTED A SIGNIFICANT FUEL LEAK FROM THE NR 1 ENGINE. MAINTENANCE FOUND THE INLET COUPLING ON THSDR CA061219002Window · cracked(CAN) DURING SERVICING THE L4 WINDOW WAS FOUND CRACKED. WINDOW REPLACED IAW MM 56-11-31, FUNCTION CHECKED SERVICEABLE WITH NO FURTHER FAULTS REPORTED. (TC NR 20061219002)SDR 0602449987Pump · failedDURING TAKEOFF NR 1 ENGINE FLAMED OUT. THE FLIGHT RETURNED TO GPT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE FUEL PUMP SHAFT HAD SHEARED. REMOVED AND REPLACED THE FUEL PUMP, TESTED ENGINE AND RETURNED TO SERVICE.SDR PIDA06120Battery Pack · inoperativeMID CABIN EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK IN CEILING MID CABIN AND OPS CHECKED GOOD IAW AMM 35-51-81.SDR QPR2006F00000Sense Line · contaminatedNR 2 ENGINE REPR/N1/N2/FUEL FLOW BEGAN FLUXUATING THEN ROLLED BACK AND FAILED. PERFORMED DRIFT DOWN AND RAN ENGINE FAILURE PROCEDURES. ELECTED TO PERFORM RESTART PROCEDURE WITH OIL QTY. TEMP, PRESSURE NORMAL. ENGINE SUCCESSFULLY RESTRATED AND PERFORMED NORSDR NACA20060055Angle · corrodedFOUND LOWER FUSELAGE STA 1006 AT STRINGER 27R ANGLE HAVE CORROSION AFT SIDE OF AFT BAGGAGE BIN. REPLACED SHEAR TIE (ANGLE) AT FUSELAGE STA 1006 AT STRINGER 27R IAW B737 SRM 51-30-2.SDR NACA20060056Frame · corrodedFOUND AFT CARGO COMPARTMENT, UNDER FLOOR STRUCTURE CORRODED FRAME AT SR.27 AND STA 727A, 71-351. CUT OUT DAMAGED SECTION OF SR.27, STA 727A AND FABRICATED AND INSTALLED REPAIR PER EO 73R5311612 REV I/R DTD 26 SEPT 2006, SRM B737 51-30-2, 51-10-2.SDR PIDA06119Battery Pack · inoperativeAFT BULLNOSE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED AFT BULLNOSE ASILE LIGHT BATTERY PACK IAW AMM 33-51-81 OPPS GHECK GOOD.SDR 06FDEA03609Valve · leakingNR 1 ENG FAILED DURING FLIGHT. 1ST INDICATION WAS EXCESSIVE NR 1 FUEL FLOW AND 2 KNOB DIFF BETWEEN NR 1 THRUST LEVER AND NR 2/3. JUST PRIOR TO FAILURE, NR 1 EPR 1.6 (2/3 EPRS 1.8). NR 1 N1 80 NR 2/3 N1S 85) N2 86 (NR 2/3 N2S 88/90) NR 1 FF 4000 (2/3 3400). SDR DL76L060683Handle · jammedCAPT SIDE SLIDING WINDOW HANDLE JAMMED AND WILL NOT LOCK CLOSED. ADJUSTED CAPTS SLIDING WINDOW OPN AT WINDOW OPEN CLOSING LOCKING CKD GOOD.SDR DL76G060681Spring · brokenL1 DOOR COUNTER BALANCE SPRING BROKEN. ITEM FORWARDED TO MCO. REMOVED L1 DOOR COUNTER BAL. INSTALLED L1 DOOR COUNTER BALANCE ASSY PER MM. REPLACED L1 DOOR ROTOR ACTUATOR PER MM. MCO/PLAC REMOVED.SDR DL76L060682Odor · detectedUNKNOWN ELECTRICAL BURNING SMELL IN AFT GALLEY. UNABLE TO ISOLATE. MTC UNABLE TO FAULT.SDR DL757060684Connector · faultyON T/O WHEN FLAPS RET FROM 5 TO 1, TE FLAPS ASSYM LIGHT AND EICAS MSG DISPLAY. RTN TO LAND. FOUND CONNECTOR D1802 ON RT FLAP POS XMITTER BAD. REPLACED PLUG AND BIN. MEGGED OUT WIRING FROM XMITTER TO FSEU. ALL CKS OK. NO HELP. REPLACED RT TE FLAP POS X-MSDR DL73S060680Throttle Cable · disconnectedRT ENGINE ADVANCED TO MAX FIREWALL THRUST BY ITSELF WHEN A CLIMB WAS BEGAN OUT OF FL280 TO FL 350 USING VERT SPD CLIMB MODE A/P WITH AUTOTHROTTLES ENGAGED. ENG PEGGED AT RED LINE MAX INDS THERE WAS NO ENGINE RESPONSE TO THRUST LEVER MOVEMENT BY PILOT TO CLOSESDR CA060728002Switch · out of rig(CAN) DURING CLIMB THROUGH FL210 AND 6.0 PSID CABIN DIFFERENTIAL THE CARGO DOOR UNSAFE LIGHT INDICATION ILLUMINATED. AIRCRAFT DUMPED FUEL AND RETURNED TO STATION, DURING APPROACH THE CARGO DOOR UNSAFE LIGHT EXTINGUISHED. UPON INSPECTION MAINTENANCE FOUND DOOR SDR PIDA06042Turbine Blades · missingCREW REPORTED A LOUD BANG DURING TAKEOFF ROLL AND RETURNED TO GATE FOR INVESTIGATION. FOUND TURBINE BLADES MISSING. REPLACED ENGINE PER MM 71-00-00. RIGGED AND TRIMMED PER MM 71-09-256.SDR CA060503007Switch · failedAT FL380, MAIN CARGO DOOR LIGHT ILLUMINATED ACCOMPANIED BY "LATCH LOCK PIN NOT ENGAGED" ON DOOR CONTROL PANEL. A/C TURNED BACK AND DURING DESCENT LIGHTS REMAINED ILLUMINATED UNTIL CABIN PRESSURE WAS REDUCED TO MINIMUM AT WHICH POINT BOTH LIGHTS HAVE EXTINGUISSDR XN0A1308Compressor · stalledCOMPRESSOR STALL (OFF IDLE) NR 2 ENGINE. INSPECTED NR 2 ENGINE INTAKE AND EXHAUST, NO DEFECTS NOTED. PERFORMED ENGINE POWER RUN, NR 2 ENGINE IAW B727 MM 71-00-00, NO DEFECTS NOTED. SUSPECT HIGH CROSS WIND COMPONENT, NR 2 ENGINE NO DEFECT NOTED.SDR C8GA20060004Oil Cooler · failedFLT 1707 FROM PHX TO MEM. DURING CLIMBOUT NR 2 ENGINE OIL TEMP BEGAN RISING. INITATED ENGINE SHUT DOWN AS PRECAUTIONARY. EMERGENCY WAS DECLARED, AIRCRAFT RETURNED TO PHX AND LANDED WITHOUT INCIDENT. FOUND NR 2 ENGINE OIL COOLER BAD. REMOVED AND REPLACED OSDR CA060119003Actuator · leaking(CAN) ON APPROACH, NLG FAILED TO EXTEND NORMALLY. SUSPECT POSSIBLE FREEZING IN UPLOCK MECHANISM AND/OR BUNGEE LINK. MANUAL EXTENSION USED, NLG EXTENDED AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION BY MAINTENANCE SUSPECTED ACTUATOR BYPASSING INSDR CA060119004Actuator · frozen(CAN) ON APPROACH, NLG FAILED TO EXTEND NORMALLY. SUSPECT POSSIBLE FREEZING IN UPLOCK MECHANISM AND/OR BUNGEE LINK. MANUAL EXTENSION USED. NLG EXTENDED AND LOCKED. AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION BY MAINTENANCE SUSPECTED BUNGEE ACTUATOR FROZESDR DL73S060008Window · crackedR1 WINDOW CRACKED WITH ARCING - REPLACED SAME.SDR DL73S050810Filter · bypassingNR 2 ENG FILTER BYPASS LIGHT ILLUM IN FLT. ALL ENG PARAMETERS NORMAL. PRESS STAYED GOOD WITH ENG SHUT DOWN. REPLACED FILTER AND DIFF PRESSURE SWITCH.SDR SPAA0500077Battery · dischargedEMERGENCY FLASHLIGHT BATTERY DEAD AT AFT FLIGHT ATTENDANT STATION. REPLACED EMERGENCY FLASHLIGHT BATTERY IAW MM 25-69-0 AND 20-50-11, OPS CHECK NORMAL.SDR PIDA20050197Mount · defectiveR-2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED MOUNT PLATE DUE TO NO POWER AT LIGHT RECEPTACLE IN MOUNT PLATE. LIGHT OPS CHECKS OK.SDR DHL2005753004Compressor · stalledCREW REMARKS NOTED COMPRESSOR STALL ON T/O, ENGINE UNKNOWN. OAT +2 C, P.A. 19FT, TOGW 152,900, IAS 0 (GS EST 10 KNTS) B.E. N/A. INSPECTED INLET AND EXHAUST SECTIONS ON ENGINES 1, 2, AND 3 IAW AOPM CH 1.8 PG. 5, NO DEFECTS NOTED AT THIS TIME.SDR CA051103008Turbine Blades · missing(CAN) IN CRUISE, LOST EGT INDICATION UPON DESCENDING AND POWER REDUCTION NR1 ENGINE RESULTED IN VIBRATION REQUIRING NR1 ENGINE TO BE SHUTDOWN. INITIAL INSPECTION INDICATED SOME VISIBLE T4 BLADE DAMAGE WHEN VIEWED THROUGH TAILPIPE.SDR DL73S050589Line · leakingLOSS OF A SYSTEM HYD, ALT GEAR EXTENSION. REPLACED LEAKING PRESSURE LINE IN RIGHT PYLON.SDR DL73S050574Engine · bird ingestionON T/O AT 1000 FT, HEARD LOUD BANG AND AIRCRAFT YAWED MOMENTARLLY LT AND RT. PASSENGER REPORTED BLUE FLAME FROM FWD OF LT ENGINE. FOWL SMELL IN CABIN. ENGINE PARAMETERS NORMAL. RETURNED TO CVG. FOUND EVIDENCE OF BIRD INGESTION IN NR 1 ENGINE. INSPECTED SSDR DL73S050566Engine · malfunctionedMOMENTS AFTER ADDING T/O POWER HEARD A LOUD BOOM FROM RT SIDE OF A/C. ABORTED T/O APPROX 20 KTS. PAX REPORTED ORANGE FLAME FROM NR 2 ENG EXHAUST. SHUTDOWN NR 2 ENG AFTER CLEAR OF RUNWAY. NO ABNORMAL ENG INDICATIONS, NO FIRE INDICATION. INSP NR 2 INTAKE ANSDR CA050907001Pin · out of adjust(CAN) ON APPROACH TO YHM NLG DID NOT INDICATE DOWN AND LOCKED. CONFIRMED DOWN BY VISUAL SCOPE, AIRCRAFT LANDED WITHOUT INCIDENT. UPON INVESTIGATION IT WAS DETERMINED A PIN FOR THE LANDING GEAR ACCESSORY UNIT WAS 'PUSHED BACK'. PIN REPAIRED AND INDICATION WOSDR DL73S050399Duct · perforatedON T/O AT 3500FT, NR 2 ENG OVHT LIGHT ILLUMINATED. WHEN THRUST LEVER PULLED TO IDLE IAW QRK PROCEDURE LIGHT WENT OUTMADE RETURN LANDING AT CVG. REPLACED BLOWN ANTI-ICE DUCT.SDR CA050713005Forging · crackedDURING SCHEDULED MLG REPLACEMENT, THE RETRACTION ACTUATOR END CAP FORGING WAS FOUND CRACKED, AND BROKE APART ON REMOVAL OF THE ACTUATOR. PRIOR TO THE GEAR CHANGE THERE WAS NO INDICATIONS OF ANY RETRACTION OR EXTENSION PROBLEMS. THE NATURE OF THE INSTALLATION
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