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 CA131218003Fuel Nozzle · dirty(CAN) THE OPERATOR REPORTED A FLAME OUT DURING ROUTINE TAXI FOR TAKEOFF. THE ACFT RETURNED TO HANGAR AND THE MAINTENANCE CREW WAS ABLE TO REPLICATE THE EVENT DURING GROUND RUNS. WHEN REDUCING POWER FROM APPROXIMATELY 70 PERCENT DOWN TO IDLE. A BORESCOPE INSPSDR DJFA20131203001Seal · wornCREW REPORTED STRONG ODOR OF BURNING OIL IN FLIGHT. ODOR APPEARED TO INCREASE IN INTENSITY AT HIGHER POWER SETTINGS. DISCOVERED OIL IN THE BLEED AIR SYS & DETERMINED THAT THE OIL WAS BLOW BY FROM WORN SEALS ON THE ENG. THE BLEED AIR SYS WAS CLEANED & THE NRSDR CA131118001Engine · leaking(CAN) THE PILOT USED EMERGENCY PROCEDURE DUE OIL ODOR IN THE CABIN UNDER UNKNOWN CIRCUMSTANCES, NO DETAILS AVAILABLE. IT WAS THE FIRST FLIGHT AFTER ENGINE INSTALLATION. DURING THE ON GROUND INSPECTION, TRACES OF OIL WAS OBSERVED IN THE BY-PASS DUCT.SDR DJFA20130724001Brake Sys · malfunctionedCREW REPORTED AFTER TOUCHDOWN THE ACFT BRAKES CAME ON HARD BUT THEN RELEASED, WHILE PEDALS WERE STILL STIFF, THEY HAD NO BRAKING ACTION. AFTER THE ANTI-SKID SYS WAS TURNED OFF THE BREAKS FUNCTIONED. MX INSPECTED THE SYS, BUT COULD NOT DUPLICATE THE DISCREPANSDR LCPR20130606025Former · crackedRT THRUST REVERSER FAN DUCT UPPER FORMER RING IS CRACKED JUST ABOVE THE OTBD SPLICE TO LOWER RING. 9:00 POSITION.SDR CA131007015Blade · cracked(CAN) THE ENGINE WAS SENT FOR REPAIR AFTER AND IFSD. DA REPORT REVEALED THE IFSD WAS DUE TO AN HP BLADE FRACTURED IN FATIGUE IN THE FIRST SERRATION. THE ORIGIN OF THE FATIGUE CRACK WILL BE INVESTIGATED.SDR 5PGA2013110104003Hinge · delaminatedCABIN DOOR SEAL WOULD WHISTLE AT ALTITUDE AND SOMETIMES ON DESCENT. A THOROUGH INSPECTION OF THE DOOR SEAL, DOOR FRAME, AND SEAL PRESSURIZATION SYS FOUND NO PROBLEMS. PUMPED UP DOOR SEAL AND NOTICED IT WOULD NOT STAY INFLATED. SOAPED THE DOOR HINGE AND FOUNSDR DJFA20130223001Position Switch · out of adjustCREW REPORTED, DURING CRUISE THE SPEED BRAKES FAILED TO DEPLOY AFTER SEVERAL ATTEMPTS. MX PERFORMED AN ADJUSTMENT OF THE RT FLAP FOLLOWUP SWITCH.SDR DJFA20130220001Brake Sys · malfunctionedCREW REPORTED DURING LANDING ROLL-OUT AND TAXI THE PILOTS SIDE LT TOE BRAKE DID NOT APPLY BRAKE PRESSURE ON INTITAL APPLICATION. AFTER PUMPING THE BRAKE IT WAS NOTED THAT THE BRAKE THEN FELT CORRECT. MX FOUND AIR IN THE SYS AND BLED THE SYS AND SERVICED BRAKSDR DJFA20130219009Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB WAS FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZTONAL CANTED STATION 29.92, BETWEEN THE FWDSDR DJFA20130219008Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STATION 46.06, BETWEEN THE FWD AND SDR DJFA20130219007Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RIGHT HORIZONTAL STAB CANTED STATION 29.92, BETWEEN THE SDR DJFA20130219006Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL STAB CANTED STATION 62.20, BETWEEN THE FWDSDR DJFA20130219005Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LEFT HORIZONTAL STAB CANTED STATION 13.78, BETWEEN THE FSDR DJFA20130219004Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL STAB CANTED STATION 46.06, BETWEEN THE FWDSDR DJFA20130219003Rib · crackedREMOVED LT HORIZONTAL STAB RIB L2M, INSTALLED HORIZONTAL STAB RIB L2M.SDR DJFA20130219001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZONTAL STAB CANTED STATION 46.06, BETWEEN THE FWDSDR DJFA20130219002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, RIB FOUND CRACKED (ALONG WITH 8 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZONTAL STAB CANTED STATION 29.92, BETWEEN THE FWDSDR DXTR20130207002Attach Angle · crackedLT LOWER OTBD THRUST REVERSER CRACKED FROM RIVET. R & R THE LT LOWER OTBD THRUST REVERSER CRACKED ANGLE IAW THE A SRM 51-40-01 AND 51-41-00.SDR CA130318005Engine · flamed out(CAN) BEFORE T/O, AFTER 10 MIN AT IDLE, THE ENGINE FLAMED OUT WITHOUT ANY PILOT INPUT. EXTENSIVE TROUBLESHOOTING COULD NOT DUPLICATE THE PROBLEM. A FERRY FLIGHT WAS MADE TO BRING THE ACFT TO WHERE FURTHER TROUBLESHOOTING WAS TO BE PERFORMED.SDR 2013FA0000047Engine · flamed outON APPROACH, AT 4000 FT, THROTTLE SETTING ABOUT 55 PERCENT, NR 1 ENGINE FLAMMED OUT, APPROACH WAS CONTINUED. THERE WAS 261.5 HRS SINCE O/H ON ENGINE. UNABLE TO DUPLICATE PROBLEM. ACFT HAS MADE SEVERAL TAKEOFF AND LANDINGS SINCE THIS INCIDENT WITH NO FURTHERSDR CA130117003Engine · shutdown(CAN) DURING TAXI AFTER NORMAL ENGINE START THE NR 1 ENGINE SHUTDOWN ON ITS OWN. BEFORE SECOND ENGINE START ATTEMPT, EXECUTED A SHUTDOWN AND START CHECKLIST, BUT THE NR 1 ENGINE N2 NEVER WENT ABOVE 41 PERCENT.SDR DJFA20121222001Switch · dirtyCREW REPORTED, DURING MISSED APPROACH, WHEN GEAR WAS SELECTED TO RETRACT, GEAR REMAINED DOWN. DUE TO EXTRA DRAG FROM GEAR AND CURRENT FUEL LOAD CREW DECLARED AN EMERGENCY AND LANDED SAFELY AT DESTINATION. MX CLEANED LANDING POSITION SWITCH AND PERFORMED LANDSDR DJFA20121221001Adapter · failedCREW AND PASSENGERS REPORTED AN ELECTRICAL ODOR WHILE ENROUTE AT ALTITUDE AND DURING DESCENT/LANDING. MX FOUND BOTH IPAD ADAPTERS HAD FAILED AND REPLACED THEM.SDR DXTR20121217003Angle · crackedLEFT ENG THRUST REVERSER, LOWER DOOR, INBD & OTBD STIFFENERS CRACKED. R & R INBD STIFFENER ON THE LT ENG THRUST REVERSER LOWER DOOR, PN OFF 202-0001-29 AND PN ON 202-0001-29 IAW SRM 51-42-00. R & R OTBD STIFFENER ON THE LT ENG THRUST REVERSER LOWER DOOR, PN OSDR DXTR20121217002Angle · crackedLT T/R, OTBD STANG FAIRING, UPPER ATTACH BRACKET IS CRACKED. R & R LEFT THRUST REVERSER OTBD UPPER STANG ANGLE. WORK WAS PERFORMED IN REF TO SRM 51-40-01.SDR CA130311011Eec · malfunctioned(CAN) ABORTED TAKEOFF DUE TO ENGINE FLAMEOUT ON TOUCH AND GO FLIGHT. THE EEC WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICE. IT WAS ALSO REPORTED THAT 2 OTHER FLAME OUTS HAD OCCURRED.SDR 2013FA0000001Bearing · failedAFTER LANDING, CREW NOTICED A DRAG AND A PULL TO THE LEFT AS THE PLANE SLOWED DOWN. NOTICED IT WAS TAKING MORE POWER THAN NORMAL TO MAKE THE ACFT MOVE FORWARD. STOPPED ACFT TO INVESTIGATE THE PROBLEM. FOUND A FLAT TIRE AND WHEN MX ARRIVED AT THE ACFT THEY FSDR DJFA20120929001Brake Sys · pressure lossCREW REPORTED LEFT SIDE, RIGHT BRAKE PEDAL INTERMITTENTLY COLLAPSES TO TRAVEL LIMIT WITH LITTLE OR GRABBY BRAKING ACTION. AFTER PUMPING PEDAL NORMAL BRAKE OPS RETURN, THOUGH PEDAL STILL FEELS SOFT AND DOESN’T MATCH LT PEDAL. THE RT SIDE BRAKES OPERATES NORMALSDR CA121002006Balance Weight · missing(CAN) ACFT DEPARTED WITH 6 SOULS ON BOARD, THE CREW REPORTED A NOSE GEAR VIBRATION DURING TAKEOFF AND ADVISED ATC THAT THE NOSE GEAR MIGHT BE DAMAGED. THE ACFT WAS CARRYING 4,200 LBS FUEL AT THE TIME. THE FLIGHT RETURNED TO DEPARTURE AND AFTER A LOW AND OVERSDR DJFA20120918008Rib · crackedDURING INSPECTION, RIB WAS FOUND CRACKED ON THE LOWER FLANGE AT LT HORIZONTAL CANTED BS 13.78, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. RIB REPLACED.SDR DJFA20120918007Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZ STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZ CANTED STA 13.78, BETWEEN THSDR DJFA20120918006Rib · crackedDURING INSP FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EA RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZ CANTED STA 29.92, BETWEEN THE FSDR DJFA20120918005Rib · crackedDURING INSP FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZ CANTED STA 29.92, BETWEEN THESDR DJFA20120918004Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT LT HORIZ CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBSSDR DJFA20120918003Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZ CANTED STA 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBS WERSDR DJFA20120918002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZ STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED ON THE LOWER FLANGE AT LT HORIZ CANTED STA 62.20, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. THE RIBS WERE REPSDR DJFA20120918001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZ STABILIZER ASSY, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 7 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT RT HORIZ CANTED STA 62.20, BETWEEN THSDR E81R2012091600001Harness · mismanufacturedCOPILOT NOTED QUICK-DONNING CREW MASK HEAD HARNESS ORIENTED UPSIDE DOWN COMPARED TO PILOT'S O2 MASK WHEN TEST FITTED. MASK FUNCTIONS OK, AND HEAD HARNESS COULD BE RE-ORIENTED TO FIT, BUT CONNECTIONS WOULD FACE AWAY FROM MASK BODY INSTEAD OF TOWARDS MASK BODY.SDR DJFA20120913001Motor · overheatedWHILE ON THE GROUND, CREW REPORTED CABIN STARTED FILLING UP WITH SMOKE STARTING FROM LAVATORY AREA. SMOKE WAS ALSO NOTED TO BE COMING OUT OF THE EXTERIOR EXHAUST AND INLET PANELS FOR THE AIR CONDITIONING UNIT. MAINTENANCE FOUND THE FREON AC COMPRESSOR MOTOR SSDR DXTA2012091005119Landing Gear · malfunctionedAFTER TAKEOFF, WHEN GEAR HANDLE WAS RAISED, NOTICED RED IN TRANSIT LIGHT REMAINED ILLUMINATED AND ALL GREEN LANDING GEAR LIGHTS WERE OUT. TOWER REPORTED NOSE AND MAIN GEAR APPEARED TO BE RETRACTED BUT BOTH MAIN GEAR DOORS WERE EXTENDED. COMPLIED WITH CHECKLISSDR DXTA2012090405119Spring · failedAFTER TAKEOFF WHEN GEAR HANDLE WAS RAISED, NOTICED RED IN TRANSIT LIGHT REMAINED ILLUMINATED AND ALL GREEN LANDING GEAR LIGHTS WERE OUT. TOWER REPORTED NOSE AND MAIN GEAR APPEARED TO BE RETRACTED BUT BOTH MAIN GEAR DOORS WERE EXTENDED. COMPLIED WITH CHECKLISDR DJFA20120827001Mount · crackedDURING INSPECTION OF NR 1 ENGINE FORWARD MOUNT AFT BRACKET AS CALLED OUT BY AD 2002-01-23, THE MOUNT WAS FOUND CRACKED. MX R & R BRACKET WITH KIT 128-4035, REV B.SDR DJFA20120815001Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STABILIZER, THE RIB DESCRIBED BELOW WAS FOUND CRACKED (ALONG WITH 5 OTHER RIBS; EACH RIB FAILURE IS DOCUMENTED ON SEPARATE SDR FORMS) ON THE LOWER FLANGE AT LT HORIZTONAL CANTED STATION 13.78, BSDR DJFA20120815002Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB, RIB WAS FOUND CRACKED ON THE LOWER FLANGE AT LT HORIZONTAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATE FROM THE FASTENER HOLES. RIB REPLACED.SDR DJFA20120815003Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STATION 13.78, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED.SDR DJFA20120815004Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZONTAL CANTED STATION 29.92, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATES FROM THE FASTENER HOLES. RIB REPLACED.SDR DJFA20120815005Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZTONAL CANTED STA 46.06, BETWEEN THE FWD AND AFT SPARS. CRACKS EMANATE FROM THE FASTENER HOLES. RIB REPLACED.SDR DJFA20120815006Rib · crackedDURING INSPECTION FOR CRACKS ON THE RIB FLANGES OF THE HORIZONTAL STAB ASSY, RIB FOUND CRACKED ON THE LOWER FLANGE AT RT HORIZTONAL CANTED STATION 46.06, BETWEEN THE FWD AND AFT SPARS. CRACK EMANATE FROM THE FASTENER HOLE. RIBS REPLACED.SDR DJFA20120802001Master Cylinder · inoperativeDURING TAXI, CREW REPORTED LT BRAKE PEDAL ON BOTH SIDES TO BE INEFFECTIVE WITH ANTI-SKID ON AND OFF. MX FOUND THE LT MASTER CYLINDER FAILED. BOTH MAIN WHEEL BRAKES AND THE LT BRAKE MASTER CYLINDER WERE REPLACED.
Back to Pratt & Whitney JT15D-5