Pratt & Whitney JT15D-5
Service difficulty reports · 953
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 = 'JT15D5' 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 = 'JT15D5' 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 DXTA2010112304318Valve · malfunctionedDEPARTED & 4 MINUTES INTO CLIMBOUT, LT WING OVERPRESSURE LIGHT CAME ON. OBSERVED FUEL STREAMING OUT OF LT WING APPROX 2 FT FROM THE TIP NEAR THE OVERPRESSURE VALVE AREA. AFTER A COUPLE OF MINUTES OVERPRESSURE LIGHT WENT OUT & FUEL STOPPED FLOWING OUT OF WISDR DXTA2010112204316Brake · dirtyTHE LT BRAKE GRABBING WHEN PRESSURE IS APPLIED. BRAKE IS STILL SMOKING A LITTLE AFTER SHUTDOWN. REMOVED LEFT BRAKE ASSY, CLEANED AND REINSTALLED. PERFORMED HIGH SPEED TAXI CHECK. OPS CHECKED GOOD IAW MM 32-42-00.SDR DXTA2010112204313Strut · leakingON LANDING ROLL, BRAKES FELT "GRABBY". UPON POST FLIGHT INSP, FOUND LT MAIN GEAR STRUT WET AND FLUID DRIPPING FROM MAIN STRUT INBD SIDE OF STRUT. LT STRUT IS LESS THAN A CREDIT CARDS WIDTH. RESEALED LT STRUT AND SERVICED. R & R LT BRAKE ASSY. R & R LT MAISDR DXTA2010111704311Bulb · inoperativeLEFT MAIN GEAR INDICATOR LIGHT IS INOPERATIVE. R & R LT GEAR INDICATION LAMP IAW MM 33-10-00. OPS CHECK GOOD.SDR 2010FA0001225Motor · intermittentDURING FLIGHT, THE OVERHEAD FAN STOPPED WORKING AND WOULD COME ON INTERMITTENTLY. DURING TROUBLESHOOTING, ON GROUND POWER, TAPPING THE MOTOR STARTS THE FAN TURNING TEMPORARILY. SUSPECTED INTERNAL WIRING FAULT. RECOMMENDATIONS: DEVELOP AND APPROVE AN AFTERMSDR 2010FA0001237Motor · intermittentDURING FLIGHT, THE OVERHEAD FAN STOPPED WORKNG AND WOULD COME ON INTERMITTENTLY. DURING TROUBLESHOOTING, ON GROUND POWER, TAPPING THE MOTOR STARTS THE FAN TURNING TEMPORARILY. SUSPECTED INTERNAL WIRING FAULT. RECOMMENDATION: DEVELOP AND APPROVE AN AFTERMARKSDR DXTA2010111004303Fuel Cell · overservicedDURING CLIMBOUT THROUGH 8000 FT, NOTICED A STEADY STREAM OF FUEL COMING FROM UNDER THE LT WING. DURING RETURN TO AIRPORT, NOTICED THE STREAM STOPPED AS ACFT LEVELED OFF AT 5000 FT. FOUND FUEL CELL OVERSERVICED.SDR DXTA2010110504291Landing Gear · malfunctionedAFTER SUCCESSFUL COMPLETION OF 1ST LEG AND 1 COMPLETE CYCLE OF THE GEAR, TOOK OFF ON SECOND LEG. WHEN GEAR HANDLE WAS RAISED GEAR DID NOT COME UP. GEAR CONTROL C/B HAD POPPED WHEN GEAR WAS RAISED. MATCHED CONDITION WITH GEAR HANDLE DOWN AND TRIED TO RESET C/B.SDR DXTA2010110504292Uplock Switch · malfunctionedON TAKEOFF DURING GEAR RETRACTION THE LT MAIN GEAR DID NOT RETRACT. GEAR UNSAFE LIGHT AND LT MAIN GEAR DOWN LIGHT REMAINED ON. GEAR EXTENDED NORMALLY. JACKED ACFT, COULD NOT DUPLICATE GEAR DISCREPANCY. PERFORMED PARALLELING CIRCUIT TEST, ALL CHECKED GOOD IASDR DXTA2010110304287Push-Pull Rod · looseDURING FLT VIBRATION FELT IN ACFT AIRFRAME. VIBRATION INCREASED WITH ACFT AIRSPEED & NOT ENGINE SPEED. VIBRATION WORSE TOWARD REAR OF ACFT. VIBRATION WAS NOT FELT BELOW 190 KTS, BUT INCREASED PROGRESSIVELY AS SPEED INCREASED. CHANGING ACFT ATTITUDE DID NOT CSDR DXTA2010102804278Power Supply · inoperativeAFTER ROTATION, SEC FLT DISPLAY C/B POPPED, WITH ASSOCIATED STANDBY GYRO AMBER LIGHT ILLUMINATION. R & R STANDBY GYRO POWER SUPPLY IAW MM 34-21-14. OPS CHECKED GOOD.SDR DJFA2010034Aap · odorMX TECH NOTED A BURNING SMELL IN THE COCKPIT WHILE TROUBLESHOOTING A LIGHTING PROBLEM ON THE PILOT'S AUDIO PANEL. THE ODOR APPEARS TO HAVE COME FROM THE ALTITUDE AWARENESS PANEL (AAP). NO FIRE OR SMOKE WAS NOTED BUT THE AAP PRODUCED A STRONG ELECTRICAL BURNISDR DXTA2010101204261Brake Assy · failedDURING LANDING ROLLOUT, WHEN BRAKES APPLIED EVENLY, AIRPLANE PULLED HARD TO LEFT THEN TO RIGHT. BRAKE PEDALS FELT NORMAL. REPLACED LT BRAKE ASSY IAW MM 33-42-01. BLED BRAKE SYS IAW 33-42-00.SDR DXTA2010100404256Spacer · damagedDURING MX INSPECTION, EMERGENCY EXIT DOOR WAS NOT ABLE TO BE REMOVED USING INSIDE HANDLE. R & R 6 ANCHOR SPACERS IAW MM CH 25-53-00.SDR DXTA2010100104255Servo · failedFLASH OF RUDDER BOOST FAIL ANNUNCIATOR AND YAW DAMP KICKED OFF SHORTLY AFTER TAKEOFF. 600-800 FT. TWICE DURING DESCENT, AUTOPILOT AND YAW DAMP KICKED OFF WITH GA INDICATIONS ON PFD. 12,000-11,000FT AND 9,000-8,000FT. TWICE RUDDER BOOST FAIL AND YAW DAMP KICSDR DJFA2010027Rib · crackedDURING A SCHEDULED MX INSP, WHILE PERFORMING A BOROSCOPE INSP OF THE HORIZ STABILIZER RIBS, SEVERAL CRACKS WERE FOUND ON RIBS IN THE LT AND RT SIDES OF THE HORIZ STABILIZER. THE CRACKS WERE FOUND ON THE ATTACHMENT FLANGES FROM THE RIBS WHERE THEY ARE RIVETED TSDR DJFA2010025Fuel · odorDURING FLIGHT, PASSENGERS NOTED A STRONG FUEL ODOR IN THE CABIN. ACFT DIVERTED AND LANDED SAFELY. MX TECHS FOUND RESIDUAL FUEL IN THE ACFT BELLY AND CONFIRMED THE ODOR. FURTHER INVESTIGATION WAS UNABLE TO DETECT ANY FUEL LEAKS FROM THE FUEL TANKS. RESIDUASDR DXTA2010091004229Squat Switch · malfunctionedAFTER TAKEOFF THE GEAR WOULD NOT RETRACT. REPLACED LT MLG WOW SWITCH DUE TO UNIT BEING INTERMITTENT AND INSTALLED A NEW UNIT IAW MM 32-61-00. OPS CHECK GOOD.SDR DXTA2010090704220Brake · weakON LANDING AND TAXI IN, BRAKES ON LT AND RT SIDES APPLY WHAT FEELS LIKE MINIMAL BRAKING ON INITIAL APPLICATION. UPON INCREASE IN TOE PEDAL PRESSURE, BRAKES WILL THEN GRAB CAUSING A NOTICEABLE JERKING OF THE ACFT WHEN THEY GRAB. BLED SYS POWER BRAKE BLEED. FOSDR DXTA2010083004210Squat Switch · failedANTI SKID LIGHT ILLUM INFLT AT 35000. LIGHT WENT OUT AFTER ABOUT A MIN. CAME BACK ON 5 MIN LATER & STAYED ON UNTIL SWITCH TURNED OFF. FOUND SQUAT SWITCH DISAGREE BITE INDICATOR TRIPPED. RESET INDICATOR. JACKED ACFT & TESTED ANTI-SKID SYS, MONTIORED BITE INDISDR SFOA67Wire · chafedDURING POST ENGINE START/PREFLIGHT CHECKS, NOTED THE "SPEED BRAKE EXTENDED" ANNUNCIATOR FAILED TO ILLUMINATE. VISUAL INSPECTION CONFIRMED THE BRAKES EXTENDED, & "HYD PRESS" LIGHT EXTINGUISHED CONFIRMING SYS HAD COMPLETED IT’S CYCLE. ANNUNCIATOR LIGHT TEST PERSDR DXTA2010082004199Engine · shutdownNR 2 ENGINE SHUTDOWN ON THE SPEED BRAKE TEST. 2 ATTEMPTS, AND BOTH TIMES THE ENGINE SHUTDOWN. THE THROTTLE WAS NOT SLAMMED TO THE STOPS.SDR DJFA2010023Rib · crackedDURING A SCHEDULED MX EVENT, WHILE PERFORMING A BOROSCOPE INSP OF THE HORIZ STABILIZER RIBS, SEVERAL CRACKS WERE FOUND ON SEVERAL RIBS IN THE LT AND RT SIDES OF THE HORIZ STABILIZER. THE CRACKS WERE FOUND ON THE ATTACHMENT FLANGES FROM THE RIBS WHERE THEY ARE SDR DJFA2010022Rib · crackedDURING A SCHEDULED MX EVENT, WHILE PERFORMING A BOROSCOPE INSP OF THE HORIZ STABILIZER RIBS, SEVERAL CRACKS WERE FOUND ON SEVERAL RIBS IN THE LT AND RT SIDES OF THE HORIZ STABILIZER. THE CRACKS WERE FOUND ON THE ATTACHMENT FLANGES FROM THE RIBS WHERE THEY ARE SDR DXTA2010071204148Trim System · looseON TAKEOFF WITH PITCH TRIM IN TAKEOFF RANGE REQUIRED EXCESSIVE AFT YOKE FORCE TO GET NOSE OFF GROUND. AFTER AIRBORNE FULL NOSE UP TRIM APPLIED & REQUIRES EXCESSIVE AFT YOKE FORCE AT 200 KTS. UPON INITIAL INSP, FOUND ELEVATOR TRIM TAB IN FULL NOSE UP POSITIONSDR DXTA2010070704144Adc · failedADC NR 1 FAILED IN FLIGHT. REVERTED TO NR 2. RED "X" ON AIRSPEED TAPE AND ALTIMETER TAPE. REVERTED BACK TO NR 1 AFTER LANDING AND RED "X" REMAINED. R & R NR 1 ADC. LEAK CHECK OK IAW MX 34-11-25 TASK 34-11-25-700. PITOT LEAK TO 249.8KTS, STATIC TO 31,350FT OSDR DJFA2010015Switch · inoperativeDURING CLIMB T THROTTLE MOVED BACK TO 86 PERCENT N1 UNCOMMANDED. RUDDER BOOST WAS INITIATED AND THE THROTTLE WOULD NOT ADVANCE FURTHER. ACFT RETURNED TO THE DEPARTURE AIRPORT SAFELY. A SIMILAR PROBLEM HAD BEEN REPORTED ON THE PREVIOUS FLIGHT WHICH RESULTED SDR EWCRN560CK20702Fuel Control · faultedACFT WAS AT 21,000 FT. AND APPROVED FOR HIGHER ALTITUDE. POWER WAS APPLIED AND RT ENGINE HAD NO RESPONSE. ACFT WAS RETURNED TO DEPARTURE POINT GSO. POWER CONTROL WAS EFFECTIVE BELOW 10,000 FT. ACFT WAS TURNED OVER TO SERVICE CENTER FOR REPAIRS NEEDED.SDR DXTA2010060704116Landing Gear · slowAFTER TAKEOFF, MLG RETRACTION TOOK LONGER THAN NORMAL TO COMPLETE. MLG NOT FULLY RETRACTED UNTIL REACHING APPROX 800 FT. MLG CAME UP ONE AT A TIME. ALL 3 GREEN LIGHTS WENT OFF, RED UNSAFE LIGHT STAYED ON APPROX 5 SECONDS. ALL OTHER HYD SYS APPEARED TO WORK NORSDR DXTA2010060404112Connector · looseDURING LANDING AND ARRIVAL AT DESTINATION, LANDING GEAR FAILED TO EXTEND. ACCOMPLISHED THE EMERGENCY CHECKLIST ITEMS AND THE GEAR EXTENDED WITHOUT ANY PROBLEMS. LANDED WITHOUT INCIDENT. TROUBLESHOT TO LOOSE ELECTRICAL CONNECTOR P160 AT LANDING GEAR CONTROL HSDR E81R_JW30284_3Mechanism · stiffINVESTIGATED REPORTED RT ENGINE THRUST REVERSER NOT FULLY DEPLOYING AFTER LANDING. FOUND REVERSER ASSY. STICKING AND UNABLE TO UNLOCK INBD ACTUATOR. UNLOCKED ACTUATOR AFTER ISOLATING AND ACTUATING WITH HAND PUMP. FOUND REVERSER ASSY. UPPER AND LOWER DOOR ACTUASDR DXTA2010051204093Throttle Cable · failedDURING AN OCF FOR THE RT ENG, THE ENG QUIT AFTER PULLING THE POWER LEVER BACK TO IDLE QUICKLY. ALSO, AFTER LANDING IT QUIT AGAIN AFTER A RAPID POWER LEVER REDUCTION. R & R RT AFT THROTTLE CABLE AND FUSELAGE CABLE IAW MM 76-12-03. OPS CHECK GOOD. AFT CABLE PSDR DJFA2010010Fitting · wornDURING CLIMB, CREW REPORTED AN UNUSUAL AIRFRAME VIBRATION. AFTER LEVELING OFF, CREW REPORTED THE VIBRATION CEASED AND A LOUD BANG; DECISION TO DIVERT WAS MADE. DURING DESCENT, VIBRATION RETURNED & SECOND BANG HEARD, IMMEDIATELY FOLLOWED BY A SUDDEN YAW MOVEMSDR DXTA2010050604086Brake Assy · malfunctionedWHEN EQUAL BRAKE PRESSURE IS APPLIED TO BOTH BRAKES, AIRCRAFT JERKS TO THE LT. LT BRAKE IS GRABBY AND SENSITIVE. RT BRAKE FEELS LESS EFFECTIVE. R & R RT MAIN BRAKE ASSY IAW MM CH 32-42-01. OPS AND LEAK CHECKS GOOD.SDR DXTA2010040504059Landing Gear · malfunctionedLT MAIN GEAR DID NOT RETRACT ON TAKEOFF (CONFIRMED BY INDICATOR LIGHTS, TOWER AND WIND NOISE). AFTER ABOUT 2 MIN RETRACTED BY ITSELF, WITHOUT US CYCLING THE GEAR. REMOVED LT MAIN GEAR UPLOCK SWITCH DUE TO HIGH RESISTANCE. INSTALLED NEW SWITCH AND ADJUSTED IAWSDR DXTA2010031504029Engine · malfunctionedRT ENGINE IDLE SPEED AT 10,000 FEET AND 150KTS WAS 52.9 PERCENT. COMPLIED WITH ADJUSTMENT OF MINIMUM FLOW OF THE RT ENGINE FCU IN REF TO THE MM CH 71-00-00. ALL FINAL OPS CHECKS SATISFACTORY.SDR DXTA2010031004023Brake Sys · weakBOTH COPILOT BRAKE PEDAL ARE SOFT, TRAVEL 75 PERCENT THEN BRAKES GRAB; ALSO PULLS LT. PILOT SIDE BRAKE PRESSURES SEEM OK BUT HAVE A SLIGHT DELAY FOR BRAKING. FOUND LT BRAKE GRABBING AND CHATTERING. REPLACED IAW AMM 32-92-01. BLED BOTH SIDES RT/LT IAW AMM 3SDR DXTA2010031004024Brake Sys · sensitivityLT BRAKE PEDAL VERY SENSITIVE. RT BRAKE PEDAL ALMOST TO FLOOR TO ACHIEVE SAME BRAKING ACTION. THIS HAPPENS FROM BOTH SIDES. BLED THE BRAKES IAW MM 32-42-00. OPS & LEAK CKS GOOD.SDR DXTA2010030804019Fuel Control · malfunctionedRT ENG EFC FAIL LIGHT ILLUMINATED SEVERAL TIMES IN FLIGHT WITH RPM ROLLBACK ON THE RT ENGINE. EFC RESET SUCCESSFULLY TWICE, THEN WOULD NOT RESET THEREAFTER. TROUBLESHOT IAW MM 76-10 & 73-20, ASSISTED BY MFG TECH SUPPORT. REMOVED THE LT & RT EEC & T/O PROBES SDR DJFA2010007Rib · crackedDURING A SCHEDULED MX VISIT WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE LT INBD RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LT AND RT RISDR DXTA2010030404012Unknown · malfunctionedDESCENDING THROUGH FL400, THE CABIN RATE OF CLIMB INDICATOR SPIKED AND REMAINED AT MAX RATE OF CLIMB (6000 FPM); THE SAFETY VALVES LIMITED THE CABIN ALTITUDE TO 13000 FT THE CABIN ATITUDE WARNING LIGHT ILLUMINATED IN ASSOCIATION WITH THE RED MASTER WARNING LIGSDR DJFA2010005Rib · crackedDURING A MX VISIT WHILE PERFORMING A HORIZ STABILIZER ROLLER INSP OF THE HORIZ STABILIZER INBD RIB AND BRACKET ASSEMBLIES, THE RT INBD RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. THE LT AND RT RIB ASSEMBLISDR DXTA2010030104008Brake · weakBOTH CO-PILOTS SIDE BRAKES ARE SOFT. INSPECTED COPILOTS PANELS ATTACHING POINTS, MASTER CYLINDERS, LINES AND FITTINGS NO DEFECTS NOTED AT THIS TIME BLED BRAKES IAW MM CH 32-42-00 OPS CHECKS SATISFACTORY.SDR DXTA2010022504003Unknown · odorNOTED FAINT ELECT/ BURNED INSULATION TYPE ODOR IN FLIGHT. NO SMOKE. COULD NOT IDENTIFY THE SOURCE. PRECAUTIONARY LANDING MADE. INSPECTED ACFT AND PERFORMED NUMEROUS ENG RUNS LETTING THE HEAT BLOW FULL HOT EACH TIME. COULD NOT DUPLICATE ANY ODOR OR BURNED SMESDR DXTA2010022203998Brake · odorBRAKE ODOR OCURRED IN FLIGHT AND AGAIN DURING TAXI IN. REMOVED WHEEL ASSY AND INSPECTED BRAKES. NO DISCRPANCYS NOTED. REINSTALLED WHEEL ASSY IAW MM CHP 32-40-00. COMPLIED WITH A TAXI CHECK OF ACFT AND FOUND BRAKE SYS TO OPS CHECK GOOD WITH NO ABNORMAL SMELLSDR DXTA2010F00037Warning Light · illuminatedON APPROACH TO ASE, EXT FLAPS TO 15, HYD PUMP REMAINED ILLUMINATED. REPOSITIONED FLAPS AND THE LIGHT REMAINED ON. IMMEDIATELY EXT GEAR AND FULL FLAPS. THE HYD LIGHT EXTINGUISHED. FLAP POSITION APPEARED NORMAL. ON SHORT FINAL, TOO LOW FLAPS, TOO LOW TERRAINSDR 2010F00039Wire · looseRT ENG FIRE WARNING ANNUNCIATOR ILLUMINATED IN FLIGHT. CREW DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES TO THE RT ENG. THE LIGHT REMAINED ON. THE CREW SHUTDOWN THE RT ENG AND LANDED. TECHS AT THE SERVICE CENTER INSPECTED THE ACFT. THEY DETERMINED THERE WAS NSDR DXTA2009121403895Check Valve · faultyAFTER STARTING BOTH ENGINES AND CALLING FOR TAXI CLEARENCE. THE TOWER INFORMED US THAT THERE WAS GRAYISH SMOKE COMING OUT OF ONE OF THE ENGINES (THEY THOUGHT THE LT SIDE, BUT COULD NOT BE 100 PERCENT CERTAIN) ALL ENGINE PARAMETERS APPEARED NORMAL. REMOVED ANSDR DXTA2009121603898Rod · out of adjustWHEN RT THROTTLE WAS RETARDED TO IDLE AFTER SPEED BRAKE CHECK, RT ENGINE FLAMED OUT. N1, N2, AND ITT WENT SMOOTHLY TO ZERO. OPERATED RT ENG AND DUPLICATED DISCREPANCY. CHECKED RIGGING OF RT ENG. ADJUSTED FCU/FLOW DIVIDER INTERCONNECT ROD AND SET FWD CUTOFF SDR 2009F00093Igniter · crackedAIR CARRIER DISCOVERED THAT NEWLY PURCHASED IGNITERS WERE CRACKING AT HEX NUT DURING INSTALLATION. CRACKING OCCURED PRIOR TO REACHING CMM SPECIFIED TORQUE VALUE. AIR CARRIER COMMENTED THAT ON THREE SEPERATE OCCASIONS, IGNITOR ASSEMBLIES HAD CRACKED DURING INST
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