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 DXTA200702568Receptacle · damagedAIRCRAFT TAXIED WITH GPU STILL ATTACHED. REMOVED AND REPLACED GPU POWER RECEPTACLE IAW 24-40-00. OPS CHECK WAS GOOD.SDR DXTA200702569Master Cylinder · intermittentCAPTAIN -SIDE BRAKES ARE EXTREMELY MUSHY AND INTERMITTENT. LT PEDAL WENT TO THE FLOOR AND BRAKING WAS LOST ON THAT SIDE. REPLACED PILOTS LT WHEEL MASTER CYLINDER WITH AN OVERHAULED UNIT IAW MM 32-42-00 SYSTEM OP CK'S GOOD. REPLACED PILOTS RT WHEEL MASTER SDR DJFA2007122Computer · out of adjustCREW REPORTED ENGINE ROLL BACK OF 5 PERCENT N1 ON THE RT ENGINE FOLLOWED BY A FLUXUATION OF 3-4 PERCENT. ENGINE STABILIZED AFTER ENGINE HEAT WAS TURNED ON. MAINTENANCE ADJUSTED THE EFC AUTHORITY.SDR DXTA200702563Transducer · inoperativeON CLIMB OUT AFTER FLAP RETRACTION, ACCELERATING THROUGH 160 KIS, (RDR BST FAIL) YELLOW CAUTION LIGHT ILLUMINATED ALONG WITH DISENGAGEMENT OF THE YAW DAMPER. REMOVED NR 1 ENGINE TRANSDUCER PN APTE233A-1750300A SN 7064-16-116, 7064-16-129 AND NR 2 ENGINE TRANSDSDR DXTA200702565Brake · weakRT BRAKE ON CAPTAIN'S SIDE DEPRESSES FURTHER THAN LT SIDE AND IS SOFT. CO-PILOTS SIDE HAS SIMILAR PROBLEM. REMOVED AND REPLACED RT MAIN BRAKE IAW CE-560 MAINTENANCE MANUAL 32-42-01.SDR DXTA200702560Reservoir · underservicedSIDE BRAKES ARE EXTREMELY MUSHY. LT PEDAL GOES ALMOST TO THE FLOOR. ACCOMPLISHED BRAKE BLEED ON LT AND RT BRAKES AND SERVICED RESERVOIR WITH HYDRAULIC FLUID. BRAKING SYSTEM FUNCTIONS NORMALLY AT THIS TIME COMPLIED. WORK IAW CITATION. 560 MM CHAPTER 32-42-SDR 2007FA0000939Lamp · inoperativePILOT HAD NO GREEN DOWN AND LOCKED INDICATION FOR THE RT GEAR WHEN LANDING. PILOT CONFIRMED WITH THE TOWER THE GEAR WAS DOWN, ALSO THE PILOT CONFIRMED THAT THE LIGHT WOULD NOT ILLUMINATE WHEN TESTED. AFTER LANDING MAINTENANCE CHECKED OUT AIRCRAFT AND REPLACED SDR DJFA2007121Coalescer Bag · dirtyCREW REPORTED ODOR OF SMOKE IN THE LAV AREA WITH WING HEAT ON IN ICING CONDITIONS. ODOR DISAPATED AFTER WING A/I WAS SHUTOFF. MAINTENANCE DISCOVERED THE COALESCER SOCK DIRTY. THE COALESCER SOCK WAS REPLACED.SDR DJFA2007120Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED SDR DXTA200702551Shuttle Valve · defectiveCAPT AND FO'S BRAKES ARE SPONGY. PEDALS REQUIRES MORE THAN USUAL PRESSURE TO ACHIEVE BRAKING ACTION. REMOVED DEFECTIVE RT BRAKE SHUTTLE VALVE , INSTALLED SHUTTLE VALVE IAW CMM 32-46-43. OPERATIONAL AND LEAK CHECKS GOOD.SDR DXTA200702550Flow Divider · out of rigLT ENGINE SHUTS DOWN ON SPEED BRAKE TEST. T/S LT ENGINE. FOUND ENG RIGGING LOOSE AND WITH EXCESS PLAY AT FLOW DIVIDER. RIGGED LT ENGINE. OPS CHECK GOOD. CHECKED RT ENG FOUND IN SAME CONDITION. RERIGGED. RT ENG OPS CHECK GOOD. ALSO CHECKED SPEED BRAKE TEST WITSDR DJFA2007118Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED SDR DXTA200702544Brake · malfunctionedWHEN TAXIING AND MAINTAINING LIGHT BRAKE PRESSURE ON BOTH BRAKE PEDALS, RT PEDAL PRESSURE DROPS AND PEDAL DEPRESSES ALL THE WAY TO STOP. BLED BOTH LT AND RT BRAKES IAW CE-560 MM, CHAPTER 32-42-00. OPERATIONAL CHECKS GOOD. FOR DETAILS OF WORK ACCOMPLISHED, SESDR DXTA200702546Anti-Skid Sys · stickingBRAKE RELEASE, GRAB WITH THE ANTISKID ON. BLED BRAKES IAW CE560 MM 32-42-00.SDR DXTA200702547Indicator · unknownDURING APPROACH TO LANDING THERE WAS AN UNSAFE RT MLG INDICATION (GREEN LIGHT OUT) WITH NO OTHER UNSAFE INDICATIONS EMERGENCY EXTENSION WAS PERFORMED WITH BOTTLE. T/S SYS AND FOUND RT GEAR INDICATOR BULB INOP. REPLACED WITH NEW FROM A/C FLYAWAY KIT. SERVICSDR DXTA200702541Unknown · smokeON POST FLIGHT INSPECTION, FOUND "HELL HOLE" AREA FULL OF WHITE/GREY SMOKE AND STRONG BURNED RUBBER ODOR. REMOVED & REPLACED A/C MOTOR ASSY. OPS CHECK GOOD IAW 1134400-9 ASSY CMM.SDR DXTA200702542Brake Assy · weakBRAKES ARE SPONGY ON APPLICATION OF PEDAL PRESSURE WHICH DELAYED BRAKING ACTION RESULTS. BLED LT AND RT BRAKES NO AIR WAS NOTED IN SYSTEM OPS CHECK GOOD. NO DEFECTS NOTED. WORK PERFORMED IAW CE-560 MM CHAP 32-42-00. FOR DETAILS REF FAS W/O 07-2508SDR DXTA200702539Unknown · unknownAIRPLANE WILL NOT PRESSURIZE. REPLACED PNEUMATIC RELAY WITH OVERHAULED UNIT I.A.W. CESSNA 560 M.M. 21-32-02.SDR DXTA200702538Unknown · odorTHERE IS A BURNING ELECTRICAL ODOR IN COCKPIT WHEN DEFOG FAN IS SELECTED ON. REMOVED & REPLACED DEFOG BLOWER WITH OVERHAULED UNIT IAW CE-560 MM CH 21-21-01. OPS CHECK GOOD.SDR DXTA200702534Brake Assy · weakCAPT AND FO BRAKES ARE SPONGY. COMPLIED WITH TAXI AND BRAKE CHECK OF AIRCRAFT NO DEFECTS NOTED. WORK DONE IAW CE560 MM 32-42-00SDR DXTA200702535Landing Gear · malfunctionedLT MAIN GEAR DID NOT INITALLY RETRACT AFTER TAKEOFF OTHER GEAR RETRACTED NORMALLY. REMOVED LEFT MAIN GEAR UPLOCK SWITCH DUE TO HIGH RESISTANCE. INSTALLED NEW SWITCH IAW CE560 M/M CH 32-30-00, OPS CHECKED GOOD DURING GEAR SWING.SDR DJFA2007116Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE RT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED SDR DXTA200702531Brake · malfunctionedF/O'S BRAKES GO TO THE FLOOR WHEN PRESSED. 11-01-07 FOUND BRAKES TO BE SPONGY. BLEED BRAKES THREE TIMES IAW CE-560MM CH 32-42-00. OPS CHECKS GOOD.SDR DJFA2007127Skin · corrodedDURING A SCHEDULED MAINTENANCE INSPECTION, TECHNICIANS FOUND MODERATE CORROSION ON BOTH HORIZONTAL STABILIZER LEADING EDGES. CORROSION WAS BEYOND REPAIRABLE LIMITS. BOTH LEADING EDGES WERE REPLACED.SDR DXTA200702528Squat Switch · malfunctionedTHE CABIN WOULD NOT PRESSURIZE AFTER TAKEOFF. 10-29-07 TROUBLESHOT TO INTERMITTENTLY FAILED LEFT SQUAT SWITCH. REMOVED AND REPLACED LT SQUAT SWITCH. OPERATIONAL CHECKS GOOD AT THIS TIME. WORK DONE IAW. CESSNA MODEL 560 M.M. CHAPTER 21-31-04.SDR DXTA200702525Brake Assy · malfunctionedTHE BRAKE PEDALS NEED TO BE PUSHED HALF WAY DOWN TO GET BRAKES TO ACTIVATE AND DURING TAXI BRAKES PULSATE/GRAB. 10-29-07 COMPLIED WITH ON-GROUND MODE TEST & ANTI-SKID SELF TEST IAW AMM 32-42-00 & FOUND NO DEFECTS. BOTH BRAKE PRESSURES WERE AT 800 PSI WITH EISDR DJFA2007115Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RT AND LT IB ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREASDR DJFA2007114Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED SDR 2007FA0000914Fitting · looseWHILE PERFORMING AN A-D INSPECTION FOUND 8 LOOSE RIVETS IN THE FORWARD RIVET LINE OF THE ATTACHMENT PIVOT FITTING PN 45A21183-11 ON THE BOTTOM OF THE HORIZONTAL STABILIZER. IT IS SUSPECTED THAT THE LOOSE RIVETS WERE CAUSED BY FATIGUE AND AGE. RECOMMEND INSPESDR DXTA200702518Brake Assy · weakCAPTAIN SIDE LT BRAKE GOES SOFT INTERMITTENTLY. WHEN PEDAL PRESSURE RELEASED AND BRAKE REAPPLIED OPERATION IS NORMAL. PERFORMED ANTI-SKID BRAKE BLEED PROCEDURE IAW 560 MM 32-42-00. SYSTEM CHECK NORMAL AT THIS TIME.SDR DJFA2007113Unknown · odorCREW NOTED AN "ACRID ODOR" FROM THE LAV AREA. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE LAV AREA AND FOUND NO DISCREPANCIES. MAINTENANCE PERFORMED AN ENGINE RUN WITH NO DEFECTS NOTED.SDR 2007FA0000912Window · crackedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND NR 2 (COPILOT) SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD. THE D-INSPECTION REQUIRES THAT BOTH WINDSHIELD RETAINERS OR USING OPTICAL PRISM INSPECTION METHOD. THE IS NO STATEMENT IN THE AIRCRAFT MM SDR DXTA200702511Computer · inoperativeCOPILOT'S PFD SHOWED RED X'S ON ASI, ALT, AND VSI DURING TAKEOFF ROLL. REMOVED AND REPLACED THE COPILOTS IC-600 WITH EXCHANGE. PERFORMED OPERATIONAL TEST. OPERATION TESTS GOOD. WORK DONE IAW CESSNA 560 MM CH 34-23-02.SDR DXTA200702506Switch · out of adjustON TAKEOFF AT ROTATION, "CABIN DOOR" LIGHT CAME ON. ONCE ON THE GROUND WITH THE DOOR OPEN, LIGHT FLICKERED ON AND OFF SEVERAL TIMES. GAINED ACCESS TO THE CABIN DOOR SWITCH. INSPECTED CONDITION AND WIRING FOUND SATISFACTORY; ADJUSTED SWITCH AND TIGHTENED AS RSDR DXTA200702507Wheel · out of balanceDURING TAKEOFF, SEVERE NOSE WHEEL SHIMMY BEGAN AT 35 KTS. AS FORWARD NOSE PRESSURE RELEASED, SHIMMY GOT WORSE AND ABORT INITIATED AT 50 KTS. AHRS 1 AND 2 FAILED AND FORWARD EMER LIGHT ILLUMINATED. FOUND BOTH LT & RT NOSE WHEEL/TIRE UNBALANCED & TIRE WORN. RSDR DXTA200702504Display · inoperativeAT 60 KNOTS, RT PFD WENT BLANK. DURING ABORTED TAKEOFF RT PFD FLICKERED 2 TIMES WITH A RED X DISPLAYED. AFTER RED X DISPLAYED PFD WENT BLANK TO NORMAL. UNABLE TO DUPLICATE DISCREPANCY. TROUBLESHOT SYSTEM. FOUND GROUND CONNECTOR CCS20 LOOSE. TIGHTENED GROUND CSDR DJFA2007110Rib · crackedDURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, BOTH THE RIGHT AND LEFT INBOARD ROLLER BRACKETS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OSDR DXTA200702505Bulb · burned outNO GREEN LIGHT ON LT MAIN GEAR DURING GEAR EXTENTION, RAN THE EMERGENCY EXTENTION CHECKLIST. BLOWED GEAR DOWN FOR POSITIVE DOWN AND LOCKED. CREW VERIFIED GREEN VISUAL INDICATOR IS SHOWING ON THE MLG ACTUATOR. AT THIS TIME WITH ROTARY TEST, THE LT MAIN GEAR INSDR DXTA200702499Computer · malfunctionedON TAKEOFF, JUST AS WE REACHED 40 KIAS, RT PFD BLANKED OUT, AFTER 0 SECONDS A RED X APPEARED, APPX 10 SECONDS AFTER THAT ATT IND AND RMI REAPPEARED BUT NO ADC INFO. SELECTING ADC REV DID NOT RESTORE DATA. ABORTED T/O. RESEATED THE CO-PILOTS FLIGHT GUIDANCE COSDR CA071016017Liner · damaged(CAN) THE ENGINE WAS REPORTED TO HAVE REPEATEDLY FLAMED OUT DURING TAXI OPERATIONS. INSPECTION REVEALED A DAMAGED/WORN COMBUSTION CHAMBER LINER. (TC NR 20071016017)SDR DXTA200702492Brake Assy · weakEXCESSIVE BRAKE PRESSURE WAS REQUIRED TO STOP AIRCRAFT UNDER NORMAL TAXI SPEED. BRAKES WERE VERY SOFT AND SPONGY. BLED BRAKES & SERVICED RESERVOIR I/A/W C560 M.M 32-42-00. OPS CHECK GOOD.SDR DXTA200702490Brake · weakCO-PILOTS RT BRAKE GOES SOFT. CAN BE PUMPED UP BUT GOES SOFT AGAIN. 09-28-07 BLED RT BRAKE. OPS CHECKS GOOD. WORK DONE IAW CITATION 560 M/M 32-42-00.SDR 2007FA0000910Door · crackedFOUND DURING INSPECTION. NOSE GEAR FOLLOW UP DOOR, P/N 45A31615-21 ON BRACKETS PN 45A31613-9, 45A31613-7 AND 45A31616-3 AT ATTACHING RIVET HAS CRACKS GOING FORWARD TO AFT THOUGH THE FIRST RIVET ALONG THE RIVET ROW. RELATIVE WIND PUSHING AFT ON THE DOOR WHILE SDR 2007FA0000911Structure · crackedFOUND DURING INSPECTION. NOSE GEAR FOLLOW UP DOOR PN 45A31615-21 ON BRACKETS PN 45A31613-9 AND 45A31613-7 AT ATTACHING RIVET HAS CRACKS GOING FORWARD TO AFT THROUGH THE FIRST RIVET ALONG THE RIVET ROW. RELATIVE WIND PUSHING AFT ON THE DOOR WHILE GEAR IS EXTESDR DXTA200702481Downlock Switch · malfunctionedDID NOT GET A RT LANDING GEAR GREEN DOWN AND LOCKED INDICATION UPON GEAR EXTENTION. 09-28-07 REMOVED FAULTY RT MAIN GEAR DOWN AND LOCKED SWITCH AND INSTALLED NEW SWITCH IAW HAWKER 400XP MM CHAP. 32-10-00. AND TEMP REV 32-1. OPS CHECK GOOD. FOR DETAILS REF SDR DXTA200702482Engine · power lossON TAKEOFF FROM SAN T/O POWER COMPUTED AS 99 PERCENT N1. WITH THRUST LEVERS FIREWALLED, LT ENGINE N1 AT 99 PERCENT, RT ENGINE N1 AT 97.8 PERCENT. CONDITIONS AT SAN: SEA LEVEL, 22DEG C WIND 250 AT 7KNTS. 29.95.SDR DXTA200702479Handle · malfunctionedRT MLG LIGHT OUT & RED GEAR HANDLE ILLUMINATED DURING APPROACH. STAYS ON WHILE ON GROUND. CHECKED RT MLG UPLOCK SWITCH, RT MLG DOWNLOCK SWITCH & RT MLG DOOR CLOSE SWITCH, NO DISCREPANCIES NOTED. VISUALLY NOTED RT MLG NOT LOCKED. JACKED RT WING. PUSHED LOCKSDR 2007FA0000830Cover · corrodedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND SPOILER MIXER ASSEMBLY BOX COVER NOT SEALED. REMOVED COVER AND FOUND CORROSION ON ACTUATOR AND MIXER ASSEMBLY. RECOMMEND THAT THE SPOILER MIXER AREA BE INSPECTED THOROUGHLY THE BOX COVER REMOVED. INSTALLED TSDR 2007FA0000831Air Duct · crackedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND THE LEFT AFT FUSELAGE BLEED AIR LINE BELLOWS BLOWN APART PN 45A63517-073 AND THE RT AFT FUSELAGE BLEED AIR LINE BELLOWS BRAIDING FRAYING PN 45A63517-075. WHEN THE LT BLEED AIR LINE BLEW APART IT CRACKED A FUSESDR 2007FA0000832Window · crackedWHILE PERFORMING A SCHEDULED A-D INSPECTION FOUND COPILOT COCKPIT SIDE WINDOW CRACKED USING THE PRISM INSPECTION METHOD. THE D-INSPECTION REQUIRES THAT BOTH WINDSHIELDS BE INSPECTED BY REMOVING THE WINDSHIELD RETAINERS OR USING OPTICAL PRISM INSPECTION METHOD
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