Honeywell TFE731-3R-1H

Service difficulty reports · 38

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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 = 'TFE7313R1H'
  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.

SDR 2022F00301Hydraulic System · failedAFTER TAKEOFF, HAD #2 HYD LO PRESS ANNUNCIATOR. RETURNED TO AIRPORT . #2 HYD SYSTEM ONLY PRODUCING APPROX. 2000 PSI. PUMP TTIS AND TOTAL CYCLES ARE UNKNOWN.Jul 22, 2022 · N564BR · Braero HS125700A · Hydraulic System, MainSDR CA150109004Landing Gear · malfunctioned(CAN) LEFT MAIN LANDING GEAR EXTENSION INDICATOR DISPLAYED A GEAR NOT FULLY DEPLOYED INDICATION. CREW INITIATED EMERGENCY GEAR EXTENSION PROCEDURE, ADVISED ATC AND DID A FLY BY FOR VISUAL VERIFICATION BY THE TOWER CONTROL , CREW DID NOT DECLARE AN EMERGENCY BJan 5, 2015 · Hwksly HS125600B · Landing Gear Retraction/Extension SystemSDR CA150116011Lever · binding(CAN) REFER TO HS125-700A IPC 32-30-01-11 REVERSING VALVE MECHANISM LEVER COULD NOT TURN FREELY DUE TO CONTAMINATION, PART AND BRACKET ASSEMBLY WAS CLEANED, MANUFACTURER DOES NOT CALL FOR LUBRIFICATION. THIS LEVER ENABLES THE LOCKING OF THE SIDESTAY ASSEMBLY.Jan 5, 2015 · Braero HS125700A · Landing Gear Retraction/Extension SystemSDR CA130527008Seal · deteriorated(CAN) IT WAS DETERMINED THAT THE SEAL LOCATED AT THE HP/LP FLANGE HAD DETERIORATED AND WAS CAUSING A MINOR LEAK. BECAUSE OF IT`S CLOSE PROXIMITY TO A TEMPERATURE SENSOR: COMPARTMENT OVERTEMP WARNINGS WERE RECEIVED IN THE COCKPIT, CAUSING TO UTILIZE THE EMERGENMay 7, 2013 · Braero HS125700A · Pneumatic Distribution SystemSDR CA130325005Shaft · failed(CAN) IN CRUISE, ACFT EXPERIENCED HYD LOW NR 2 WARNING FOLLOWED BY HYDRAULIC LOW NR 1 WARNING. MAIN HYD PRESSURE DROPPED BELOW NOMINAL PRESSURE. GEAR EXTENSION WAS DONE WITH AUXILIARY HYD CIRCUIT. ACFT LANDED WITH NO FURTHER INCIDENT. INSPECTION BY MFG RMar 22, 2013 · Braero HS125700A · Hydraulic Pump (Electric/Engine), MainSDR CA130326008Indicator · burned(CAN) DURING ENGINE GROUND RUNS, ABOUT 5 MIN AFTER THE MAIN BUSES WERE BROUGHT ON LINE A ELECTRICAL BURNING ODOR WAS NOTED IN THE COCKPIT. THE AVIONICS SYS WERE SYSTEMATICLY SHUTDOWN AND THE ODOR DISAPATED. THE ENGINE RUNS WERE COMPLETED AND THE ACFT BROUGHT Mar 22, 2013 · Braero HS125700A · Rate of Climb IndicatorSDR CA130201005Drive Shaft · broken(CAN) DURING PREFLIGHT GROUND RUN, RT HYDRAULIC LOW PRESSURE WARNING LIGHT DID NOT EXTINGUISH DURING ENGINE START. TROUBLESHOOTING DETERMINED THE RT HYDRAULIC PUMP FAILED. HYDRAULIC PUMP REPLACED IAW CH 29, FILTERS INSPECTED IAW CH 29. FUNCTION AND LEAK CHECJan 31, 2013 · Braero HS125700A · Hydraulic Pump (Electric/Engine), MainSDR CA110514001Coupling · failed(CAN) ON CLIMB OUT HAD REAR BAY OVERHEAT COME ON INTERMITTENT THEN WENT OFF. THERE WERE NO INDICATIONS IN THE COCKPIT OTHER THAN THE NR2 ENGINE COMPUTER WENT TO MANUAL MODE. ON ARRIVAL, INSPECTION WAS CARRIED OUT AND FOUND THAT THE APU BLEED AIR DUCT FLEX COUPMay 6, 2011 · Braero HS125700A · Pneumatic Distribution SystemSDR CA110315014Hinge Fitting · cracked(CAN) DURING ACCOMPLISHMENT OF AD 80-12-10 R1/SB 57-55 THE LEFT OUTBOARD HINGE UPPER LUG WAS FOUND TO BE CRACKED.Mar 15, 2011 · Hwksly BH125400A · Wing, Control Surface Attach FittingsSDR CA100927006Transceiver · false indicationPILOTS REPORTS RADAR SHOWS FALSE RETURNS. C/O GND CHECKS/OPS CHECKS COULD NOT FAULT. JULY 09/10 PILOTS REPORTS RADAR SHOWS FALSE RETURNS LT OF CTR. REMOVE R/T AND SENT FOR BENCH CHECK/REPAIR. UNIT INSTALLED F/C OPS CHECKS SERVICEABLE. AUG 02/10 PILOTS REPOJun 22, 2010 · Braero HS125700A · Weather Radar SystemSDR CA090811002Structure · damagedAUG 09-2009 HS-125 700A INCIDENT REPORT HAIL DAMAGE. ACFT WAS RETURNING TO MAIN BASE FROM A 704 TRIP AND ATC ADVISED CREW OF THUNDER STORM ACTIVITY IN AREA. ACFT WAS HELD IN A HOLDING PATTERN AND THEN CLEARED. BETWEEN 13000FT AND 10000FT ACFT ENTERED AN AREAug 9, 2009 · Braero HS125700A · Fuselage Structure (General)SDR UG8A08P050601Skin · corrodedMISSING PAINT WITH MINOR CORROSION ON MIDDLE RT WING, UNDER THE SLAT, AT THE WING LIFTING POINT. CORROSION IS LOCATED ON WING PLANK AT LIFT POINT IN MACHINED CUTOUT. CUTOUT IS FILLED WITH SEALANT. CORROSION LOCATED UNDER SEALANT ON WING PLANK. REMOVED CORRMay 6, 2008 · N48FB · Amd FALCON2000 · Wing, Plate/SkinSDR S8A2008F00001Transducer · failedAT 15,000 ENROUTE, AIRCRAFT LOST INDICATION OF OIL PRESSURE ON THE NR ONE (LEFT) ENGINE AND THE FLIGHT CREW ACCOMPLISHED A PRECAUTIONARY SHUTDOWN OF THE NR ONE ENGINE. AFTER A REVIEW BY THE FLIGHT CREW OF ALL INDICATING ENGINE INSTRUMENTATION THE FLIGHT CREW DApr 18, 2008 · N110EJ · Braero HS125700A · Engine Oil PressureSDR CA071224002Aileron · iced(CAN) PILOT’S REPORTED ON APPROACH INTO AIRPORT, COULD NOT GET ANY ROLL ON AC CONTROLS. IT APPEARED THAT AILERONS WERE FROZEN. SHORTLY BEFORE TOUCHDOWN THEY WERE ABLE TO GAIN CONTROL OF THE AILERON MOVEMENT. THE AC LANDED WITHOUT INCIDENT. MAINT WAS CALLED ANDDec 13, 2007 · Braero HS125700A · Aileron Control SystemSDR CA071214007Pitot Tube · corroded(CAN) FOLLOWING A FAILED PITOT STATIC TEST, AN INSPECTION OF THE PITOT STATIC TUBING WAS CARRIED OUT AND MAINT FOUND THAT ONE OF THE TUBES (P/N 25-7SF209-9) HAD A PIN HOLE, WHICH APPEARS TO HAVE BEEN CAUSED BY INTERGRANULAR CORROSION. THE LINE WAS REPAIRED ANDDec 10, 2007 · Braero HS125700A · Pitot/Static SystemSDR CA071106011Tube · chafed(CAN) ON A PREFLIGHT INSPECTION, MAINTENANCE DISCOVERED THE FIRE DETECTOR (P/N 3001-31-900-400-17) AGAINST THE FUEL TUBE ASSEMBLY (P/N P-84417). UPON REPOSITIONING THE FIRE DETECTOR INTO POSITION, A CHAFED MARK ON THE NR 1 ENGINE FUEL TUBE ASSEMBLY WAS DISCOVEOct 25, 2007 · Braero HS125700A · Aircraft Fuel Distribution SystemSDR CA070911010Fuel Control · faulty(CAN) - MANUAL MODE SELECTION PROVIDES IDLE ONLY FUEL. NO SPOOL UP WITH POWER LEVER INCREASE. ENGINE FUNCTIONS NORMALLY IN AUTO - COMPUTER (ON) MODE. (TC NR 20070911010)Aug 29, 2007 · Braero HS125700A · Fuel Control/Turbine EnginesSDR DTX2007F00000Manifold · leakingTHE FLIGHT CREW NOTED A STRONG FUEL ODOR IN THE AFT CABIN, UPON INVESTIGATION, FUEL WAS FOUND ON THE AFT EQUIPMENT ACCESS DOOR AND UNDER THE APU. THE APU SHROUD WAS OPENED AND THE FUEL MANIFOLD WAS REMOVED AND IT WAS DISCOVERED TO HAVE A SMALL PINHOLE IN ONE Aug 6, 2007 · N943CE · Braero HS125700A · APU Engine Fuel and ControlSDR UG82005F00009Gearshaft · worn(REF CNTRL NR: PA05005) THE S.O.A.P. LAB REPORT INDICATED HIGH LEVEL OF IRON (STEEL) IN THE ENGINE. THE SAMPLE INDICATED A SPECIFIC (BELLEVILLE) WASHER IN THE LP COMPRESSOR GEARBOX WAS FAILING DUE TO A SHIFTING OF THE LP PLANETARY GEARSHAFT ASSY. AC WAS FERAug 24, 2005 · N48FB · Braero HS125700A · Accessory GearboxesSDR UQR2005F00000Tire · crackedDURING PRELIMINARY INCOMING INSPECTION ON 7/11/05 IT WAS NOTED THAT NR3 MAIN WHEEL TIRE HAD CRACKS OR SPLITS RADIALLY IN BETWEEN TREAD. IT WAS DETERMINED THAT THIS TIRE WAS INSTALLED ON THE NR 3 WHEEL (PN AH52788, SN 675/8129 ON 6/8/05 ACTT 11,926.5, ACTL 12,Aug 1, 2005 · N700NW · Braero HS125700A · TireSDR CA050422003Wire · broken(CAN) SWITCH MONITORS FUEL TEMP AT ENGINE FUEL PUMP & IS FITTED TO TFE731-3 ENGINES INSTALLED ON HAWKER 700 ACFT. ON THIS INSTALL SWITCH WIRES CONNECT TO AIRFRAME SUPPLIED ENGINE HARNESS THROUGH IN-LINE CONNECTORS. THESE CONNECTORS ARE NORMALLY ONLY DISTURBEDApr 20, 2005 · Braero HS125700A · Fuel System WiringSDR CA050414004Fan Blade · separated(CAN) AT ROTATION, A POPPING NOISE WAS HEARD BUT NO ABNORMAL INSTRUMENT INDICATIONS WERE OBSERVED. CLIMB AND CRUISE WERE NORMAL AS WERE ALL TREND MONITOR RESULTS. ABNORMAL VIBRATION WAS APPARENT ON DESCENT WITH LOWER POWER SETTINGS. POST FLIGHT INSPECTION FApr 12, 2005 · Braero HS125700A · Turbine Engine Compressor SectionSDR 2005FA0000491Clamp · crackedFLUORESSCENT PENETRANT INSP OF THE TAIL PIPE CLAMP REVEALED ONE NUT TO BE CRACKED. (K)Apr 6, 2005 · N281BT · Braero HS125700A · Engine Collector/Tailpipe/NozzleSDR MJ12004F00000Carbon Seal · failedOPERATOR NOTED NR 2 ENGINE LOW OIL PRESSURE IN FLIGHT. ENGINE POWER SETTING WAS REDUCED TO IDLE AND CREW ELECTED TO RETURN TO ORIGIN. POST FLIGHT ATTEMPTS TO START NR 2 ENGINE WERE ABORTED DUE TO INABILITY TO OBTAIN PROPER ENGINE ROTATION. ENGINE SN P84313 Sep 30, 2004 · N298BP · Braero HS125700A · Turbine Engine Oil SystemSDR 2004FA0000525Bulb · failedON APPROACH CREW SELECTED THE GEAR HANDLE DOWN, THE NOSE DOWNLOCK ANNUNCIATOR DID NOT ILLUMINATE WITH GEAR HANDLE IN DOWN POSITION. CREW ATTEMPTED TO CHANGE THE NOSE DOWNLOCK ANNUNCIATOR BULBS, BUT COULD NOT REMOVE THE ANNUNCIATOR. WHEN THE AIRCRAFT ARRIVED May 17, 2004 · N41HF · Braero HS125700A · Landing Gear Position and WarningSDR YK1R062001Apu · failedDURING TAXI, SMOKE RAPIDLY FILLED THE COCKPIT AND THE CABIN. EMERGENCY SHUTDOWN OF ALL SYSTEMS WAS PERFORMED, GROUND EMERGENCY DECLARED AND AIRCRAFT EVACUATED. IT WAS FOUND DUE TO FAILURE IN THE APU, OIL ENTERED THE BLEED AIR DUCT WHICH CAUSED THE SMOKE. SYFeb 27, 2004 · N653XP · Raythn HAWKER800XP · APU Core EngineSDR 99V21902Inlet · crackedENGINE INLET INNER LINER CRACKED. FOUND DURING COMPLIANCE WITH RECOMMENDED SERVICE BULLETIN SB71-32.Mar 29, 2002 · N9999V · Hawker BAE125700B · Engine Air Intake SystemSDR G1F2001F00001Fcu · defectiveDURING NORMAL OPERATION (GROUND RUN) OF RIGHT ENGINE, THE ENGINE FLAMED OUT AFTER IDLE HAD BEEN SELECTED. THIS CONDITION COULD BE REPEATED AND WAS INTERMITTENT WHEN THE THROTTLE LEVER WAS RETARDED TO IDLE POSITION. AFTER TROUBLESHOOTING FUEL SYSTEM PER MM, TOct 17, 2001 · N101FC · Braero HS125700A · Fuel Control/Turbine EnginesSDR UO22001F00010Blade · failedFIRST STAGE LPT BLADE FAILED CAUSING MAJOR DAMAGE TO RELATED TURBINE PARTS AND RESULTING IN AN INFLIGHT SHUT DOWN.Sep 26, 2001 · N913V · Braero HS125700A · Turbine SectionSDR 257207Engine · malfunctionedDURING TAKEOFF ROLL, HEARD LOUD NOISE FROM OUTSIDE AIRCRAFT. AIRCRAFT YAWED TO RIGHT. ABORTED TAKEOFF AND APPLIED BRAKES. TAXIED BACK TO FBO WHERE NR 2 ENGINE DID NOT APPEAR NORMAL AND NR 3 MAIN TIRE WAS DEFLATED. POSSIBLE FAILURE 1 OR MORE COMPONENTS ON RSep 20, 2001 · N913V · Hawker BAE125700B · Engine (Turbine/Turboprop)SDR AJ62002F00000Tube · cracked30 MINUTES INTO A FLIGHT A LOW OIL PRESSURE WARNING CAME ON. THE PILOT PERFORMED A PRECAUTIONARY IN FLIGHT SHUTDOWN AND RETURNED TO HOME BASE, LANDING WITHOUT INCIDENT. THE AFT BEARING SCAVENGE TUBE WAS FOUND TO HAVE CRACKED AND DEPLETED THE OIL TO AN UNACCEAug 20, 2001 · N900JT · Hawker BAE125700B · Turbine Engine Oil SystemSDR 20010409CW009Tube · crackedRIGHT ENGINE ROLLED BACK TO IDLE ON ITS OWN AFTER TAKEOFF. MAINTENANCE FOUND THE P3 TUBE ASSEMBLY BETWEEN THE FUEL CONTROL UNIT AND THE ENGINE PLENNUM CRACKED IN HALF. FATIGUE FAILURE IS SUSPECTED.Apr 9, 2001 · N700XJ · Hwksly HS125600A · Fuel Controlling SystemSDR CA001031004Cowling · failed(CAN) UPON INSPECTION FOUND AN BOLTS IN AFT ENG COWLINGS FLANGE. REPLACED WITH NAS I.A.W. HAWKER RAYTHEON I.P.C.Oct 17, 2000 · Braero HS125700A · Engine Cowling SystemSDR 20001012SH024Control Valve · failedVALVE FAILED IN THE OPEN POSITION ALLOWING UNCOOLED RIGHT ENGINE BLEED AIR INTO CABIN AND COCKPIT. CABIN AND COCKPIT BECAME UNBEARABLY HOT. SMOKE IN CABIN AND COCKPIT VALVE WAS FOUND DEFECTIVE. (X)Sep 1, 2000 · N161WC · Braero HS125700A · Cabin Temperature Control SystemSDR 2000ZZZX582Disk · failedENGINE RECEIVED WITH TURBINE DAMAGE. FIELD REPORT REVEALED THIS ENGINE EXPERIENCED AN IN-FLIGHT SHUT DOWN AT FL 350. DURING TEAR DOWN, THE LPT1 ROTOR ASSY HAD ALL BLADES BROKEN OFF JUST ABOVE THE FIR TREE AREA. ONE LPT1 BLADE COULD NOT BE FOUND. DISK GROWTJan 3, 2000 · Turbine SectionSDR 99ZZZX3374Rotor Assy · wornDURING DISASSEMBLY OF ENGINE TURBINE SECTION FOR AN OVERTEMP INSPECTION/MPI, THIRD LPT ROTOR DISK, PN 3074096-2, SN 965332200320, WAS FOUND TO HAVE BEEN RUB DAMAGED AT THE FORWARD SIDE OF THE DISK IN FIR TREE AREAS. CONDITION APPEARS TO HAVE BEEN CAUSED BY DIJul 27, 1999 · Turbine Engine Compressor SectionSDR 99ZZZX3199Check Valve · failedOXC/BDL - EN ROUTE ON A PRE-POSITIONING FLIGHT, THE CREW REPORTED THE OIL PRESSURE STARTED TO DECLINE ON THE LEFT ENGINE. AT 15 PSI, THE LEFT ENGINE WAS SHUT DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT AT BDL. AN INVESTIGATION REVEALED THAT OIL WAS LEAKING FJun 13, 1999 · N511KA · Braero HS125700A · Turbine Engine Oil SystemSDR CA980302009Engine · failed(CAN) DURING CLIMB THROUGH 4000 FT, A LOUD BANG WAS HEARD FOLLOWED BY A VIBRATION. CREW OBSERVED NR 1 ENGINE SPOOLING DOWN. #1 ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO AIRPORT. NR 1 ENGINE WAS EXAMINED BY MANTENANCE AND FOUND TO HAVE SUFFERED MASSIVE FAILMar 2, 1998 · Braero HS125700A · Engine (Turbine/Turboprop)
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