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 DJFA2007141Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUSDR DXTA200702670Squat Switch · erraticPRESSURIZATION INOP ON CLIMBOUT CABIN RATE HAD NO CONTROL OF RATE OF CLIMB. AT ALTITUDE CONTROLLER HAD NO EFFECT ON CABIN ALT. ON DESCENT PRESSURIZATION FAILED (CABIN ALT) LIGHT CAME ON O2 MASKS WERE DONNED EMERGENCY DECLARED UNTIL REACHING A SAFE ALT. REMOVESDR DXTA200702665Controller · obstructedON TAKE-OFF CABIN CONTROLLER FAILED TO MAINTAIN CABIN PRESSURIZATION. TROUBLESHOT TO VENT BLOCKAGE ON CONTROLLER. CLEARED BLOCKAGE AND PERFORMED OPS CHECK. OPS CHECK GOOD. IAW CE 560 MM CH 21-31-00.SDR DXTA200702666Erosion Shield · looseEROSION TAPE CAME LOOSE FROM VERTICAL STAB AND WEDGED IN RUDDER. RUDDER ONLY MOVES ONE DIRECTION. REMOVED LOOSE EROSION TAPE FOUND IN VERTICAL STAB. AND PERFORMED RUDDER SYSTEM OPS CHECK, OPS CHECK NORMAL. WORK DONE IAW CESSNA 560 M/M CH 27-30-00.SDR DXTA200702668Squat Switch · wornLANDING GEAR WILL NOT RETRACT. GEAR INDICATES DOWN AND 3 GREEN . GEAR HANDLE WILL NOT RAISE AS IF LOCKED DOWN. JACKED AIRCRAFT AND FOUND LH SQUAT SWITCH TO BE IN GROUND MODE. WITH SLIGHT SIDE LOAD TO THE SCISSOR LINK MOVES SWITCH SHAFT LATERALLY BACK INTO FLSDR DJFA2007140Inlet · crackedDURING POSTFLIGHT, CREW REPORTED CRACKS ON THE NR2 INLET RING. MAINTENANCE CONFIRMED THE DISCREPANCY AND REPLACED THE INLET RING.SDR DXTA200702657Unknown · unknownAFTER TAKEOFF, RED LANDING GEAR NOT LOCKED AND AMBER HYD SYS PRESS LIGHTS REMAINED ILLUMINATED FOR APPROXIMATELY 2 MINUTES. AT THAT TIME A THUMP WAS HEARD AND FELT COMING FROM THE AREA OF THE NOSE GEAR. LIGHTS WENT OUT. GEAR CYCLED DOWN NORMALLY FOR LANDING. SDR DXTA200702658Brake Assy · weakCOPILOT RT BRAKE IS MUSHY. BLED RT BRAKE SYSTEM IAW CE-560 M/M 32-42-00. PERFORMED TAXI CHECK. R/H BRAKE SYSTEM OPS CHECK GOOD AT THIS TIME.SDR DJFA2007139Unknown · odorON APPROACH CREW REPORTED BURNING SMELL FROM THE RT REAR FLOOR AREA. MAINTENANCE RAN THE AIRCRAFT BUT WAS UNABLE TO DETECT ANY SMELL IN ALL CABIN TEMPERATURE MODES (AUTO/MANUAL, HOT AND COLD). AIRCRAFT WAS RELEASED.SDR DXTA200702648Arm · out of rigAFTER TAKEOFF GEAR WOULDN'T RETRACT. SECURED GEAR AND FOUND BLOW DOWN BOTTLE ARM AND HANDLE/CABLE OUT OF PROPER RIG. RE-RIGGED AND SERVICED BOTTLE. COMPLETED SEVERAL GEAR OPS CHECKS AND GEAR BLOW DOWN. ALL CHECKS GOOD PER CE560 M.M. 32-31-08.SDR DXTA200702647Indicator · out of adjustDURING TAKEOFF, AIRCRAFT REQUIRED SIGNIFICANT FOWARD PRESSURE DURING CLIMBOUT. ALL OTHER INDICATIONS WERE NORMAL EXCEPT NOSE TRIM WHEEL INDICATOR WAS BEYOND THE FORWARD WHITE ARC. FOUND TRIM INDICATOR OUT OF ADJUSTMENT. RE-POSITIONED INDICATOR TO SHOW CORSDR DXTA200702644Brake Assy · unknownRT BRAKE PEDAL ON CO-PILOT SIDE IS SOFT. CAPTAIN SIDE BRAKES ARE GOOD. REMOVED LT MASTER CYLINDER, INSTALLED NEW UNIT. REMOVED RT CO-PILOTS MASTER CYLINDER & INSTALLED NEW UNIT. REMOVED PUMP RELAY AND INSTALLED NEW RELAY. BLED BRAKES IAW C560 MM 32-42-00 FOSDR JEMA010208001Window · crackedWHILE PERFORMING A SCHEDULED A-B INSPECTION FOUND NR 2 (CO-PILOT) SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD. THE (D) INSPECTION IS THE ONLY INSPECTION THAT REQUIRES THAT BOTH WINDSHIELDS BE INSPECTED BY REMOVING THE WINDSHIELD RETAINERS OR USING OSDR JEMA010208002Bulkhead · crackedWHILE PERFORMING A SCHEDULED A-B INSPECTION, FOUND RT AND LT AFT FUSELAGE BLEED AIR LINE ATTACH BRACKETS PULLED FROM AFT FUSELAGE BULKHEAD RESULTING IN CRACKS IN THE BULKHEADS AT FRAME STATION 329.92. THIS IS THE 4TH AIRCRAFT IN A ROW THAT THE BULKHEAD HAS BSDR DXTA200702638Brake · inadequateCOPILOT'S BRAKES TEND TO REQUIRE MORE THAN NORMAL PRESSURE FOR EVEN BRAKING. TROUBLESHOT BRAKE SYSTEM. FOUND CO-PILOT'S BRAKES (BOTH PEDALS) FIRM. SERVICED BRAKE RESERVOIR TO FULL AND BLED BOTH LT AND RT BRAKE SYSTEM AS REQUIRED. CO-PILOTS BRAKES OPS NML NOW.SDR DXTA200702635Brake Assy · unknownON ROLL OUT, F/O LT BRAKE PEDAL WENT TO THE FLOOR. CAPTAIN`S BRAKES WORK NORMALLLY. BLEED LEFT AND RIGHT BRAKES IAW 32-42-00. OPS CK GOOD.SDR 2007FA0001050Engine · leakingON THE DECENT, THE CREW HAD AN OIL PRESSURE LOW LIGHT AT THAT TIME THE CREW OBSERVED THE OIL PRESSURE GAUGE WAS INDICATING LOW PRESSURE. THE CREW SHUTDOWN THE NR 1 ENGINE DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. UPON INSPECTION BY MAINTENANCE IT WAS FOUNSDR 420CT010Sensor · contaminatedDURING CLIMB NOTICED COCKPIT VERY WARM TO HOT. BETWEEN 12000' AND 18000' IT APPEARED A THIN LAYER OF SMOKE WAS PRESENT IN THE COCKPIT. ABOUT 30 SECONDS LATER THE FIRST OFFICER VERIFIED THERE WAS SMOKE IN THE COCKPIT AND THICKER. EMERGENCY DESCENT AND LANDINSDR DJFA2007137Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQSDR DJFA2007136Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUSDR DJFA2007135Converter · failedAFTER LANDING CREW REPORTED BURNING ODOR COMING FROM AREA AROUND PAX TABLE. MAINTENANCE FOUND THE DC TO DC CONVERTOR FAILED. THE COMPONENT WAS REPLACED.SDR DJFA2007134Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQSDR DJFA2007131Unknown · odorTHE CREW REPORTED HOT ODOR FROM CABIN DUCTING. RT SIDE TABLE FELT HOT AFTER SHUTDOWN. MAINTENANCE REMOVED THE SIDEWALL PANEL AND INSPECTED DUCTING. THE AIRCRAFT WAS RUN IN FULL HOT. NO DEFECTS OR LEAKS WERE NOTED. NO (HOT) OR BURNING ODOR NOTED DURING GROSDR 2008FA0000090Wire · chafedPITCH TRIM INOPERATIVE REMOVED RT FWD GALLEY AND RT FWD PARTITION. FOUND WIRE BUNDLE CHAFED BEHIND PARTITION. REPAIRED (3) WIRES THAT WERE CHAFED THROUGH TO THE CONDUCTORS. PROVIDED CLEARANCE BETWEEN WIRE BUNDLE AND PARTITION. INSTALLED ANTI-CHAFE MATERIALSDR DXTA200702607Brake Assy · weakCAPTAIN'S BRAKES ON TAXI OUT WERE EXTREMELY SPONGY. BLED BOTH CO-PILOTS & PILOTS BRAKES IAW CE-560 ULTRA AMM CHAPTER 32-40-00, TAXIED AIRCRAFT AND BRAKES OPS CHECKED GOOD ON BOTH PILOTS & COPILOTS SIDE.SDR DXTA200702605Switch · malfunctionedCABIN DOOR LIGHT ILLUMINATED IN FLIGHT. REMOVED CABIN DOOR SWITCH P/N P18M30 S/N 1020. INSTALLED NEW PART P/N P18M30 S/N 4317. OPERATIONAL AND LEAK CHECK GOOD. WORK DONE IAW CESSNA MAINTENANCE MANUAL 560 36-11-02.SDR DXTA200702608Wheel · out of balanceAT APPROX 50 KTS ON TAKE OFF ROLL, NOSE WHEEL SHIMMIES AND STAYS AT A STEADY STATE OF OSCILLATION UNTIL STOPPED. REMOVED NOSE SHIMMY DAMPER AND INSTALLED OVERHAULED UNIT. REMOVED NOSE WHEEL AND FOUND BALANCE TO BE OUT. REINSTALLED REPAIRED NOSE WHEEL BALANCESDR 2007FA0001068Bonding Jumper · frayedTROUBLESHOT REPORT OF HORIZONTAL STABILIZER ANTI-ICE SYSTEM FAIL INDICATION. NOTED ELEVATOR HORN HEAT SYSTEM RESISTANCE READINGS ERRATIC WHEN ELEVATORS MOVED. FOUND ELEVATOR BONDING JUMPERS FRAYED AND CORRODED. REPLACED ELEVATOR BONDING JUMPERS, ELEVATOR HOSDR 2007FA0001069Pipe · crackedPERFORMED HOT SECTION INSPECTION PRIOR TO SCHEDULED 1800 HR INTERVAL TO INVESTIGATE COMPLAINT OF SLOW STARTING. UPON DISASSEMBLY, FOUND DIFFUSER PIPES OF GAS GENERATOR CASE CRACKED AND PORTIONS MISSING AT APPROXIMATE 10:30, 11:00 POSITION. SUSPECT CAUSED BY SDR DJFA2007129Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER INBOARD RIB AND BRACKET ASSEMBLIES, THE LT AND RT IB RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINESDR DJFA2007126Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER INBOARD RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COSDR DXTA200702602Pressure Switch · inoperativeABORTED TAKE OFFDUE TO HP FAIL LT CAUTION LIGHT. INSTALLED NEW LEFT HP DIFFERENTIAL PRESSURE SWITCH (SD001). PERFORMED OPERATIONAL CHECK AND LEAK CHECK IAW CE-680 MM 36-10-00. CHECKED GOOD.SDR CA071113005Fuel Control · failed(CAN) DURING APPROACH, ENGINE SPEED DESCENDED TO SUBNORMAL VALUE. NO/SLOW RESPONSE FROM THRUST LEVER. CONDITION WAS REPEATABLE ON GROUND FOLLOWING THE INCIDENT. FUEL CONTROL CHANGED AS PART OF TROUBLESHOOTING. (TC NR 20071113005)SDR DJFA2007124Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT SIDE ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINESDR DXTA200702597Brake Assy · leakingON TAXI OUT, BRAKES PULLED HARD TO THE RT FROM BOTH CAPT AND FO POSITION. FOUND LEAK IN LT HAND BRAKE ASSY. TIGHTEN AND BLED SYSTEM, LEAK CHECKS GOOD TAXI CHECKS GOOD IAW 560MM 32-42-00.SDR DJFA2007123Hose · rupturedON APPROACH CREW EXPERIENCED COMPLETE HYDRAULIC FAILURE AT 4000' ON APPROACH INTO KDAL, LOST ALL HYDRAULIC PRESSURE WITHIN ABOUT 20 SEC. AFTER FIRST INDICATION OF A PROBLEM, DECLARED AN EMERGENCY, RAN THE EMERGENCY CK LIST FOR GEAR EXTENSION, ZERO FLAP LANDINGSDR DXTA200702590Reservoir · lowCO-PILOT'S RT BRAKE IS SPONGY, WILL PUMP UP AFTER SEVERAL APPLICATIONS. INSPECTED RESERVOIR, PUMP/MOTOR, ACCUMULATOR, ANTISKID VALVES FITTINGS, (4) MASTER CYLINDERS RT BRAKE AND ASSOCIATED PLUMBING NO LEAKS FOUND, THOROUGHLY BLED RT BRAKE MM 32-42-00. SERVICEDSDR DXTA200702592Relay · inoperativeWHEEL BRAKES FAILED DURING TAXI OUT. REPLACED POWER BRAKE RELAY VALVE ASSY IAW 32-40-00. OPS CK GOOD.SDR 2007FA0000987Bulkhead · crackedWHILE PERFORMING AN A-C INSPECTION FOUND RT AFT FUSELAGE BLEED AIR LINE ATTACH BRACKET PULLED FROM FUSELAGE BULKHEAD RESULTING IN A CRACK IN THE BULKHEAD AT FRAME STATION 329.92. RECOMMEND CONTACTING MFG FOR REPAIR OPTIONS CRACK HAS BEEN FOUND ON BOTH SIDES SDR DXTA200702587Master Cylinder · bypassingCO-PILOTS RT BRAKE PEDAL NEEDS TO BE DEFLECTED OR PUSHED APPROXIMATELY 30 PERCENT MORE TRAVEL THAN LT PEDAL. REMOVED AND REPLACED CO-PILOT'S MASTER CYLINDERS AND SOFT LINES IAW CE560 M/M 32-42-02, OPS CHECK GOOD AT THIS TIME.SDR 2007FA0000988Pivot · looseWHILE PERFORMING AN A-C INSPECTION FOUND 8 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A2118311 ON THE BOTTOM OF THE HORIZONTAL STABILIZER. IT IS SUSPECTED THAT THE LOOSE RIVETS WERE CAUSED BY FATIGUE AND AGE.SDR N425CT0003Hydromech Unit · restrictedPARTIAL POWER LOSS FROM RT ENGINE AT FL 390 POWER SURGED DURING APPROACH AND LANDING.SDR CA071128011Fuel Control · inoperative(CAN) DURING CRUISE, ENGINE POWER GRADUALLY REDUCED FROM 102 PERCENT N1 INDICATION TO 74 PERCENT. NO RESPONSE TO THROTTLE LEVER MOVEMENT. FLIGHT WAS DIVERTED AND AIRCRAFT LANDED WITH BOTH ENGINES RUNNING. THE ENGINE FUEL CONTROL WAS REPLACED AND AIRCRAFT RETUSDR DXTA200702583Fitting · loose1ST OFFICERS BRAKES ARE MUSHY AND REQUIRE A COUPLE OF PUMPS AFTER INTITAL PRESSURE TO FIRM UP. INSPECTED BRAKE SYSTEM, FOUND PILOTS LT MASTER CYLINDER FITTINGS LOOSE. TIGHTENED FITTINGS. BLEED BRAKE SYS MULTIPLE TIMES. OPS LEAK CHECK GOOD IAW CESSNA 560 MM 32SDR DXTA200702585Master Cylinder · bypassingPILOTS RT BRAKE PEDAL GOES SOFT AFTER 15-20 SEC OF INITIAL BRAKE APPLICATION. (LOSSED APPX 2-3 INCHES OF PEDAL TRAVEL). INSTALLED 1EA NEW PILOTS RH BRAKE MASTER CYLINDER AND BLED SYSTEM. OPERATED ENGINES AND TAXI CHECKED NORM, WORK DONE IAW C560 M/M 32-42-02SDR DXTA200702581Squat Switch · reads highLOST CABIN PRESSURIZATION AT FL290. CABIN PRESSURE ROSE TO 13500 PA AND STABILIZED. ON DESCENT, CABIIN PRESSURE DESCENDED WITH THE AIRCRAFT ALTITUDE. FOUND LT SQUAT SWITCH TO HAVE HIGH RESISTANCE AND CHANGING WITH PRESSURE ON ARM. REPLACED SWITCH WITH NEW IASDR DXTA200702578Master Cylinder · leakingDURING TAXI OUT, CO-PILOTS RT BRAKE IS SPONGY CAUSING A/C TO VEER LT. FOUND CO-PILOTS RT MASTER CYLINDER LEAKING. REMOVED AND REPLACED MASTER CYLINDER WITH NEW UNIT. OPS AND LEAK CHECK GOOD AT THIS TIME. IAW CE 560 M/M 32-42-01SDR DXTA200702580Flow Divider · malfunctionedDURING SPEED BRAKE CHECK THE LT ENGINE SHUTDOWN. REMOVED AND REPLACED FLOW DIVIDER PERFORMED OPS CK AND LEAK CHECK NO DEFECTS FOUND OPS CHECK SPEED BRAKE SYSTEM OPS CHECK GOOD IAW MM CH 73-10.SDR K452007F00001Support Bracket · missingDURING ROUTINE INSPECTION, THE LT OB THRUST REVERSER STANG FOUND DISPLACED .2500 INCH OB FROM NORMAL POSITION. REMOVAL OF STANG REVEALED THE LOWER FWD SUPPORT WAS MISSING THE UPPER FWD SUPPORT SHEARED OFF. THE ATTACHING RIVETS HAD FAILED. FURTHER INSPECTIONSDR DXTA200702573Brake Assy · weakPILOTS RT BRAKE PEDAL GOES SOFT AFTER INITIAL APPLICATION. THE RT PEDAL TRAVELS SIGNIFICANTLY FURTHER THAN THE LT BRAKE PEDAL. BLED LT AND RT BRAKES IAW MM 32-42-00.
Back to Pratt & Whitney JT15D-5