# Service difficulty reports: Garrett TFE731-5R

A list on [Garrett TFE731-5R](https://openairdocs.org/engine/garrett-tfe731-5r.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 108 reports

- [SDR 2022FA0000279](https://openairdocs.org/sdr/2022FA0000279.md): None · none · Jun 2, 2022 · N850SX · Braero BAE125800A · Cabin Pressure Indicator
  > DURING CLIMB PASSING FL 355 THE "CABIN ALTITUDE" LIGHT CAME ON WITH DIFFERENTIAL PRESSURE INDICATOR SHOWING ZERO. CABIN DID NOT LOSE PRESSURIZATION; HOWEVER THE CREW FOLLOWED THE CHECKLIST DECLARED EMERGENCY, DESCENDED TO LOWER ALTITUDE AND RETURNED TO THE DEP
- [SDR 2021F00032](https://openairdocs.org/sdr/2021F00032.md): Oil System · fluctuates · Feb 13, 2021 · N664S · Raythn HAWKER800 · Turbine Engine Oil System
  > AFTER DEPARTURE FROM KJVL DURING CLIMB OUT THE CREW NOTICED THE RH ENGINE OIL PRESSURE FLUCTUATING. THE CREW FOLLOWED CHECKLIST PROCEDURES AND SHUT THE ENGINE DOWN AS A PRECAUTION.
- [SDR 2019FA0000330](https://openairdocs.org/sdr/2019FA0000330.md): Relay · malfunctioned · Oct 4, 2019 · N780DW · Raythn HAWKER800XP · Engine Oil Indicating System
  > DURING POST MAINTENANCE FUNCTIONAL CHECK, FOUND LH OIL PRESSURE INDICATOR LIGHT TO NOT ILLUMINATE DURING CHECK (PUSH TO TEST CHECK GOOD). MECHANICS FOLLOWING MAINTENANCE TECHNICAL DATA CHECKED BULBS, AND SD CARD PER INSTRUCTIONS. AFTER FURTHER TROUBLESHOOTING,
- [SDR G73R201808225587](https://openairdocs.org/sdr/G73R201808225587.md): Cabin Pressure · malfunctioned · Aug 19, 2018 · N126KC · Raythn HAWKER800 · Cabin Pressure Control System
  > DURING CRUISE AT FL360, WITH CABIN CONTROLLER SET TO FL380 AND NORMAL PRESSURIZATION. AT TOP OF DESCENT REDUCED POWER SLIGHTLY AND AT THE SAME TIME THE CABIN RATE KNOB TURNED TO MIN AND CABIN CONTROLLER MOVED SLIGHTLY TOWARD FIELD ELEVATION. WITHIN SECONDS
- [SDR ZP7A2016F00039](https://openairdocs.org/sdr/ZP7A2016F00039.md): Fuel Control · defective · Dec 1, 2015 · N798PA · Braero BAE125800A · Fuel Control/Turbine Engines
  > AT FL400, ENGINE NR 2 BEGAN LOOSING POWER, N1 REDUCED TO BELOW 60 PERCENT, DESCENDED TO 14,000 FT N1 REDUCED TO BELOW 40 PERCENT. AT BELOW 8000 FT MSL ENGINE POWER BECAME FULLY RESPONSIVE.
- [SDR JLTA20150824001](https://openairdocs.org/sdr/JLTA20150824001.md): Engine · malfunctioned · Aug 21, 2015 · N118GA · Braero BAE125800A · Engine (Turbine/Turboprop)
  > ON FRIDAY, AUGUST 21ST AT APPROX 1900Z, ACFT DEPARTED EMPTY & ENTERED CRUISE, EVERYTHING WAS NORMAL. ON THE INITIAL DESCENT CREW HEARD A STRANGE NOISE & OBSERVED AN ENG COMPUTER LIGHT FOR THE NR 2 ENG. ALL OF THE INSTRUMENTS FOR THE NR 2 ENG THEN FLUCTUATED
- [SDR 9JLA201506247566](https://openairdocs.org/sdr/9JLA201506247566.md): Controller · defective · May 12, 2015 · N304HE · Raythn HAWKER800 · Engine Synchronizing
  > CREW REPORTED THAT DURING FLIGHT THE RT ENG DEEC LIGHT CAME ON AT 86% N1. THE CREW INDICATED THAT THE ENG DIVERTED TO MANUAL MODE. TROUBLE SHOT THE DISCREPANCY & FOUND THAT THE ENG SYNC CONTROLLER WAS DEFECTIVE. THE UNIT WAS R & R WITH AN EXCHANGE UNIT PN 2
- [SDR CA150113022](https://openairdocs.org/sdr/CA150113022.md): Tube · leaking · Jan 2, 2015 · Braero BAE125800A · Turbine Engine Oil System
  > (CAN) POST ARRIVAL, FLIGHT CREW CONDUCTED POST FLIGHT INSPECTION OF ACFT AND NOTED SIGNIFICANT OIL LEAKAGE ON LT ENGINE COWLINGS, NO INFLIGHT INDICATIONS WERE EVIDENT TO FLIGHT CREW DURING APPROXIMATE 4.5 HR FLIGHT. OIL LEVEL COULD NOT BE SEEN THROUGH OIL TANK
- [SDR 2014FA0000506](https://openairdocs.org/sdr/2014FA0000506.md): Indication Sys · failed · Aug 26, 2014 · N82SR · Braero BAE125800A · Landing Gear Position and Warning
  > FAILURE OF RT MLG INDICATION WHEN GEAR SELECTED DOWN FOR LANDING.
- [SDR CA140407014](https://openairdocs.org/sdr/CA140407014.md): Wire Harness · chafed · Apr 2, 2014 · Braero BAE125800A · Landing Gear System Wiring
  > (CAN) FLIGHT CREW REPORTED LANDING GEAR SELECTOR WOULD NOT MOVE AFTER TAKEOFF. CHECKLIST CARRIED OUT AND FLIGHT CREW DECIDED TO RETURN TO AIRPORT AFTER CIRCLING SUFFICIENT TIME TO LOWER FUEL WEIGHT TO OBTAIN PROPER LANDING WEIGHT. ACFT LANDED WITHOUT INCIDENT
- [SDR VIBR20131202001](https://openairdocs.org/sdr/VIBR20131202001.md): Stud · unsecure · May 25, 2013 · N24JG · Braero BAE125800A · Electrical Power System Wiring
  > ENGINE STARTER GENERATOR "B" STUD NOT SECURE IN STARTER GENERATOR TERMINAL BLOCK.
- [SDR 9JLA2012073106330](https://openairdocs.org/sdr/9JLA2012073106330.md): Computer · defective · Jul 25, 2012 · N800FL · Braero BAE125800A · Fuel Controlling System
  > CREW REPORTED THE LT ENGINE DEEC LIGHT COMES ON STEADY IN FLIGHT. THE ENGINE COMPUTER WAS REMOVED. A NEW COMPUTER WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY.
- [SDR DXTA2012042004955](https://openairdocs.org/sdr/DXTA2012042004955.md): Cap · loose · Apr 19, 2012 · N894QS · Raythn HAWKER900XP · Turbine Engine Oil System
  > WHILE ENROUTE AT 39000 FT, NOTICED RT ENGINE OIL PRESSURE TURN YELLOW & BOUNCE FROM 55 TO 57 PSI FOR APPROX 5 SECONDS. DROPPED TO 53-55 PSI FOR APPROX 5 TO 10 SECONDS. PRESSURE DROPPED TO 48 PSI. SHUTDOWN RT ENGINE. SINGLE ENGINE LANDING WAS MADE. OIL WA
- [SDR 2012F00067](https://openairdocs.org/sdr/2012F00067.md): Transducer · inoperative · Mar 29, 2012 · N801RM · Braero BAE125800A · Engine RPM Indicating System
  > ON THE LAST LEG OF THE TRIP, ON START UP, THE RT ENGINE COMPUTER INOPERATIVE LIGHT ILLUMINATED. FOUND BAD N2 TRANSDUCER. REPLACED THE TRANSDUCER, OPS CHECKED GOOD.
- [SDR L7OA2012F00066](https://openairdocs.org/sdr/L7OA2012F00066.md): Fuel Sys · leaking · Mar 21, 2012 · N359CF · Braero BAE125800A · Aircraft Fuel Distribution System
  > ON CLIMB OUT, NOTICED FUEL COMING FROM THE LT WING VENT AREA. ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT.
- [SDR DXTA2011100304738](https://openairdocs.org/sdr/DXTA2011100304738.md): Fuel Control · malfunctioned · Sep 30, 2011 · N897QS · Raythn HAWKER900XP · Fuel Control/Turbine Engines
  > AT CRUISE ALTITUDE, NR 2 ENGINE COMPUTER MM ANNUNCIATOR ILLUMINATED. ENGINE POWER CHANGED ON ITS OWN AT THAT MOMENT. CHECKLIST ITEMS COMPLIED WITH AND NR 2 ENG COMPUTER SWITCH SELECTED IN OVERSPEED PROT MODE. NORMAL LANDING MADE. PERFORMED ENGINE DEEC DOWN
- [SDR 9JLA20110801001](https://openairdocs.org/sdr/9JLA20110801001.md): Pump · defective · Aug 1, 2011 · N800FL · Raythn HAWKER800 · Engine Fuel Pump
  > THE CREW REPORTED DURING CLIMBOUT THAT THE ENG 2 FUEL ANNUNCIATOR ILLUMINATED. THE FUEL FILTER HAD BEEN REPLACED 2 DAYS PRIOR WITH SATISFACTORY OPERATIONAL CHECKS. TROUBLSHOOTING FOUND THAT THE ENGINE DRIVEN FUEL PUMP WAS DEFECTIVE. P/N 3070850-57 S/N 396995
- [SDR V0JA041176H](https://openairdocs.org/sdr/V0JA041176H.md): Oil System · low pressure · Apr 19, 2011 · N1776H · Raythn HAWKER800 · Engine Oil Indicating System
  > DURING TAXI TO RUNWAY THE CREW WAS ALERTED TO LOW OIL PRESSURE IN THE NR 1 ENGINE BY THE MWS ANNUNCIATORS. THE LOW OIL PRESSURE WAS VERIFIED BY THE NR 1 ENGINE OIL PRESSURE GAUGE AND THE ENGINE WAS SHUTDOWN FOR PRECAUTIONARY MEASURES. TECH WAS CALLED IN TO T
- [SDR CA110209019](https://openairdocs.org/sdr/CA110209019.md): Pipe · cracked · Feb 9, 2011 · Braero BAE125800A · Engine Bleed Air System
  > DURING REMOVAL OF THE ENGINE FOR INSP, IT WAS NOTED THAT THE PORTION OF PIPE EXTENDING PAST THE WELD LINE ON THE INNER SURFACE OF THE AFT COUPLING OF THIS TUBE HAD BEEN CRACKED AWAY. THERE WAS NO INDICATION OF CRACKING ON THE OUTER SURFACE OF THE PIPE, ONLY O
- [SDR CA110209021](https://openairdocs.org/sdr/CA110209021.md): Outflow Valve · cracked · Feb 9, 2011 · Braero BAE125800A · Pressure Regulator/Outflow Valve
  > DURING INSP OF THE REAR PRESSURE BULKHEAD, THE FLAPPER VALVES ON THE MAIN CABIN NON RETURN VALVE WERE FOUND TO BE STUCK IN THE OPEN POSITION. FURTHER INSP REVEALED THAT THE CTR SHAFT HAD TOOLING MARKS ON IT AND THE SHAFT WAS CRACKED. THE SPRINGS THAT FORCE THE
- [SDR CA110209022](https://openairdocs.org/sdr/CA110209022.md): Diaphragm · corroded · Feb 9, 2011 · Braero BAE125800A · Aircraft Fuel Distribution System
  > AFTER REMOVAL OF THE VENTRAL FUEL TANK FOR ROUTINE INSP, CORROSION WAS FOUND 1" BELOW FUEL FILLER AT 7 O`CLOCK POSITION. DURING CORROSION REMOVAL, IT WAS FOUND THAT IT HAD PROPAGATED ENTIRELY THROUGH THE AFFECTED AREA OF DIAPHRAGM 9.
- [SDR CA110209024](https://openairdocs.org/sdr/CA110209024.md): Wire · burned · Feb 9, 2011 · Braero BAE125800A · Electrical Power System Wiring
  > DURING INSP, IN THE AFT EQUIPMENT BAY, THE ENTIRE LENGTH OF THE ABOVE MENTIONED WIRE WAS FOUND BADLY BURNED. 50 PERCENT OF THE WIRE INSULATION HAD BEEN MELTED OFF AND THE SURROUNDING WIRING HAD VISIBLE SCORCH MARKS THIS WIRE WAS USED AS THE GROUND FOR A NR OF
- [SDR CA110209026](https://openairdocs.org/sdr/CA110209026.md): B-Nut · cracked · Feb 9, 2011 · Braero BAE125800A · Hydraulic System, Main
  > DURING INSP, A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNINQ PERPENDICULAR TO THE THREADS OF THE NUT. THERE WERE NO PREVIOUS REPORTS OF HYD FLUID LEAKAGE.
- [SDR CA110209028](https://openairdocs.org/sdr/CA110209028.md): Nut · cracked · Feb 9, 2011 · Braero BAE125800A · Aircraft Fuel Distribution System
  > DURING REMOVAL OF THE VENTRAL FUEL TANK, THE ABOVE MENTIONED NUT WAS FOUND TO BE SEIZED IN PLACE. 2 CRACKS WERE NOTED ON THE OUTER SURFACE OF THE NUT: 1 PERPENDICULAR TO THE DIRECTION OF THE THREADS. AFTER DISASSEMBLY, SEVERE CORROSION OF THE THREADED PORTION
- [SDR CA110209031](https://openairdocs.org/sdr/CA110209031.md): Frame · cracked · Feb 9, 2011 · Braero BAE125800A · Fuselage Main, Frame
  > (CAN) DURING 24 YEAR INSP, A CRACK IN THE TOP CTR MEMBER OF THE LOWER PRESSING WAS FOUND.
- [SDR CA110209027](https://openairdocs.org/sdr/CA110209027.md): B-Nut · cracked · Feb 9, 2011 · Braero BAE125800A · Hydraulic System, Main
  > (CAN) DURING INSPECTION A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNING PERPENDICULAR TO THE THREADS OF THE NUT. THERE WERE NO PREVIOUS REPORTS OF HYDRAULIC FLUID LEAKAGE.
- [SDR CA101116017](https://openairdocs.org/sdr/CA101116017.md): Power Supply · overheated · Nov 9, 2010 · Braero BAE125800A · Exterior Lighting
  > (CAN) STROBE POWER SUPPLY CAPACITOR OVERHEATED AND MELTED INSULATION RESIN CAUSING ODOR AND EYE IRRITATION TO PASSENGERS. OPEN CIRCUIT TO ONE OF THE THREE STROBE OUTPUT CIRCUITS CAUSED AFFECTED CAPACITOR TO OVERHEAT BECAUSE OF INABILITY TO DISCHARGE. THE CON
- [SDR 2010F00225](https://openairdocs.org/sdr/2010F00225.md): Annunciator · activated · Oct 20, 2010 · N17DD · Braero BAE125800A · Engine Fuel Indicating System
  > CREW REPORTED THE "ENG 1 FUEL" ANNUNCIATOR ILLUMINATED DURNING FLIGHT.
- [SDR 2010F00226](https://openairdocs.org/sdr/2010F00226.md): Annunciator · activated · Aug 7, 2010 · N527M · Raythn HAWKER800 · Engine Fuel Indicating System
  > CREW REPORTED THE "ENG 2 FUEL" ANNUNCIATOR ILLUMINATED DURING FLIGHT.
- [SDR CA100106005](https://openairdocs.org/sdr/CA100106005.md): Steering Sys · failed · Jan 3, 2010 · Raythn HAWKER900XP · Landing Gear Steering System
  > (CAN) NOSE WHEEL STEERING UNSERVICEABLE AFTER LANDING NOSE WHEEL STEERING SYS INSPECTED AND LUBRICATED AND FUNCTION TESTED IAW MM 32-50-00. SYS OPS CHECK OK. FAULT DID NOT DUPLICATE.
- [SDR CA100104004](https://openairdocs.org/sdr/CA100104004.md): Terminal · burned · Dec 7, 2009 · Braero BAE125800A · Window System Wiring
  > (CAN) PILOTS REPORTED SMOKE IN THE COCKPIT. FIRST REPORTS THAT SMOKE CAME FROM THE INSTRUMENT PANEL. UPON INSP, FOUND LT WINDSHEILD C/B PN 6TC14-10. TERMNIAL A1 WAS BURNED AND DAMAGE TO THE WIRE.
- [SDR CA090909002](https://openairdocs.org/sdr/CA090909002.md): Seal · leaking · Jul 31, 2009 · Braero BAE125800A · Nose/Tail Landing Gear
  > NLG ACTUATOR SEAL FAILED OVER NIGHT WHILE ACFT WAS SITTING IN HANGAR. A LARGE AMOUNT OF HYD FLUID LEAKED, REQUIRING REPLACEMENT OF NOSE GEAR TIRES.
- [SDR CA090506009](https://openairdocs.org/sdr/CA090506009.md): Bearing · binding · Apr 29, 2009 · Raythn HAWKER900XP · Turbine Engine Accessory Drive
  > (CAN) FOUND 2 BEARINGS IN ENGINE ACCY GEARBOX INTERMITTENTLY BINDING, STARTER GENERATOR DRIVESHAFT OFF BEARING (PN 3072885-1) AND OIL PUMP DRIVESHAFT FWD BEARING (PN 3072885-1). REPLACED STARTER GEN DRIVESHAFT FWD BEARING (PN 3072883-1) AS A PERCAUTIONARY ME
- [SDR 2009FA0000257](https://openairdocs.org/sdr/2009FA0000257.md): Engine · damaged · Mar 25, 2009 · N423SJ · Piper PA34220T · Engine (Turbine/Turboprop)
  > PILOT REPORTED THAT THE RT ENGINE LOST OIL PRESSURE AND RPMS. NO N1 INDICATION. ENGINE WAS SHUT DOWN AND ACFT RETURNED TO DEPARTURE.
- [SDR CA090225011](https://openairdocs.org/sdr/CA090225011.md): Diode · shorted · Feb 23, 2009 · Raythn HAWKER900XP · Electrical Power System Wiring
  > (CAN) PILOT REPORTED SMOKE COMING FROM UNDER COPILOTS SEAT, WITH BATTERY SWITCHED OFF AND MASTER REFUEL PANEL POWERED ON. MASTER REFUEL VALVE WAS OPEN, MAIN FUEL VALVES WERE OPEN. OCCURENCE OCCURED WHILE ACFT WAS PARKED ON GROUND. MX ACTION REMOVED SHORTED D
- [SDR CA081104001](https://openairdocs.org/sdr/CA081104001.md): Hose · leaking · Oct 28, 2008 · Braero BAE125800A · Landing Gear Door Retract Section
  > (CAN) PILOTS REPORTED LOSS OF HYD PRESSURE AFTER LANDING WHILE TAXING BACK TO AMO. ON INSP, FOUND IN THE RT GEAR WELL A FLEX HYD LINE INSTALLED WITH A SLIGHT TWIST ON IT. THE LOCKWIRE ON THE B-NUT WAS LOOSE, AND THE TWIST ON THE HYD LINE AIDED IN ALLOWING THE
- [SDR CA081021006](https://openairdocs.org/sdr/CA081021006.md): Jackscrew · frozen · Oct 20, 2008 · Braero BAE125800A · Elevator Control System
  > (CAN) CREW REPORT THE ELEVATOR TRIM WAS DIFFICULT TO MOVE IN FLIGHT. UPON INSPECTION BY MX IT WAS FOUND THE ACTUATOR WAS CORRODED INTERNALLY AND THE GREASE WAS CONTAMINATED AND HARDENED. HAWKER BEECHCRAFT ALREADY HAS SB 27-3840 R1 TO CHECK FOR THIS SAME ISSUE
- [SDR DGC2008F00002](https://openairdocs.org/sdr/DGC2008F00002.md): Line · cracked · Sep 12, 2008 · N5119 · Braero BAE125800A · Engine Oil Distribution (Airframe Furnished)
  > AT CRUISE FLIGHT, AFTER 1 HR 27 MIN INTO FLIGHT, THE LT OIL PRESSURE INDICATOR FLUCTUATED FROM APPROXIMATELY 42-45 PSI DOWN TO 30-35 PSI TWICE PER SECOND CONTINUOUSLY. OIL TEMP REMAINED NORMAL, ALL OTHER ENGINE INDICATIONS NORMAL, (N1, ITT, N2). APPROXIMATELY
- [SDR 2008FA0000382](https://openairdocs.org/sdr/2008FA0000382.md): Regulator · damaged · Apr 24, 2008 · N626CG · Braero BAE125800A · Engine Oil Temperature Regulator
  > RECEIVED O/H OIL TEMP REGULATOR FROM MFG UNDER THEIR WO 815978-001, DATED 04/22/2008. WHILE PERFORMING INCOMING PARTS INSPECTION ON 04/24/2008, FOUND FUEL INLET PORT SMASHED. THERE WAS NO DAMAGE TO THE SHIPPING CONTAINER. PROBABLE CAUSE OF DAMAGE WAS MOST L
- [SDR DXTA200802843](https://openairdocs.org/sdr/DXTA200802843.md): Unknown · odor · Feb 6, 2008 · N848QS · Raythn HAWKER900XP · Air Distribution System
  > ELECTRICAL BURNING ODOR FROM BEHIND OR UNDER COPILOTS SEAT. POWERED UP AC SYS USING THE APU AND BOTH ENGS, SELECTED FULL HOT ON TEMP SELECTOR, RADIO MASTER ON, ENG ALTERNATOR'S ON WINDSCREEN HEAT ON AND COCKPIT AND CABIN LIGHTS ON OPERATED ALL SYS FOR 1 HR WIT
- [SDR DXTA200802839](https://openairdocs.org/sdr/DXTA200802839.md): Unknown · odor · Feb 5, 2008 · N848QS · Raythn HAWKER900XP · Air Distribution System
  > BURNING ELECTRICAL AND RUBBER ODOR FROM BEHIND CO-PILOTS SEAT. ON ENTERING CABIN THE ONLY ODOR NOTED WAS THAT OF NEW INTERIOR. ACCESSED THE DA PANEL AND OPENED SUB PANELS DA/A (CB PANEL BEHIND CO-PILOT) DA/B (RELAY PANEL BEHIND CO-PILOT), DA/J (A/C ELECTRICAL
- [SDR DXTA200802834](https://openairdocs.org/sdr/DXTA200802834.md): Outflow Valve · inoperative · Feb 1, 2008 · N848QS · Raythn HAWKER900XP · Pressure Regulator/Outflow Valve
  > AFTER T/O LT MAIN AIR VALVE LIGHT CAME ON AND CHECKLIST CALLS TO RECYCLE CLOSED/OPEN. LIGHT CAME BACK ON. REPLACED LT MAIN AIR VALVE WITH O/H UNIT. OPS AND LEAK CHECKED GOOD IAW MM 21-16-25.
- [SDR DELA200700009](https://openairdocs.org/sdr/DELA200700009.md): Fuel Filter · unknown · Nov 25, 2007 · N904JR · Braero BAE125800A · Engine Fuel Indicating System
  > ENG 2 FUEL LIGHT. ABORTED TAKEOFF DUE TO ENGINE 2 FUEL LIGHT ON. REPLACED FILTER WITH NEW, PERFORMED GROUND ENGINE RUN, NO LEAKS NOTED, (ENG 2 FUEL) ENUNCIATOR DID NOT ILLUMINATE.
- [SDR CA071126007](https://openairdocs.org/sdr/CA071126007.md): Computer · inoperative · Nov 8, 2007 · Braero BAE125800A · Engine (Turbine/Turboprop)
  > (CAN) ENGINES FRESH, NEW INSTALLATION OF DEECS ON AC. DEEC PROBLEMS OCCURRED. THE PROBLEM ENCOUNTERED WITH DIGITAL ENGINE COMPUTERS (DEEC). (TC NR 20071126007)
- [SDR CA071016021](https://openairdocs.org/sdr/CA071016021.md): Float Valve · stuck · Oct 16, 2007 · Braero BAE125800A · Fuel Storage
  > (CAN) DURING REFUELLING USING SINGLE-POINT SYS & FILLING BOTH MAIN (WINGS) & VENTRAL TANK. AS VENTRAL TANK REACHED 1.5 TO 3 QUARTERS CAPACITY FUEL WOULD FLOW THROUGH VENT SYS INTO LT SURGE TANK & SHUTDOWN BY CLOSING MAIN VALVE. COMPLETION OF REFUELLING COULD O
- [SDR CA070827003](https://openairdocs.org/sdr/CA070827003.md): Seal · deteriorated · Aug 8, 2007 · Braero BAE125800A · Doors
  > (CAN) UPON CLIMB OUT WITH CABIN DIFFERENTIAL PRESSURE APPROACHING APPROXIMATELY 6 PSI, A DISTINCT AUDIABLE DISCERNING NOISE WAS HEARD FROM THE CENTER AREA OF THE CABIN. DURING DESCENT WHERE CABIN DIFFERENTIAL PRESSURIZATION FELL BELOW 6 PSI, NOISE WOULD SUBSID
- [SDR DJFA2006337](https://openairdocs.org/sdr/DJFA2006337.md): Hsi · burned · Oct 25, 2006 · N810LX · Raythn HAWKER800 · Attitude and Direction Data System
  > DURING PREFLIGHT, RT HSI WAS FLICKERING ON AND OFF THEN SMOKE STARTED BELLOWING OUT FROM UNDER THE WHOLE INSTRUMENT PANEL. COCKPIT FILLED WITH SMOKE IN SECONDS. FOUND THE RT EHSI TO BE THE CAUSE OF THE SMOKE. INSTALLED A KNOWN GOOD UNIT AND FUNCTIONALLY CHE
- [SDR AOQ2006F00003](https://openairdocs.org/sdr/AOQ2006F00003.md): Switch · intermittent · Oct 17, 2006 · N800FH · Braero BAE125800A · Landing Gear Position and Warning
  > (REF NR: ON 800FH101706JC) AFTER TAKEOFF, COULD NOT RAISE LANDING GEAR. INSPECTED LANDING GEAR. FOUND LEFT WEIGHT ON WHEELS SWITCH TO BE INTERMITTENT. REPLACED LEFT MAIN GEAR WEIGHT ON WHEEL MICROSWITCH. ACCOMPLISHED SEVERAL GEAR SWINGS WITH SATISFACTORY
- [SDR COZ2006F00000](https://openairdocs.org/sdr/COZ2006F00000.md): Display · unreliable · Oct 5, 2006 · N118K · Braero BAE125800A · Indicating/Recording System
  > AT FLIGHT LEVEL 34 K, FLIGHT CREW ENCOUNTERED STATIC BUILD UP IN THE COMM SYSTEM. IT WENT AWAY SHORTLY FOLLOWED BY AUTOPILOT DISCONNECTING AND PRIMARY DISPLAYS BECAME UNRELIABLE. THE AIRCRAFT LANDED SAFELY. ON THE GROUND, FLIGHT CREW POWERED DOWN THE AIRCR
- [SDR RU32006F00002](https://openairdocs.org/sdr/RU32006F00002.md): Landing Gear · malfunctioned · Mar 8, 2006 · N98 · Braero BAE125800A · Landing Gear Retraction/Extension System
  > GEAR HANDLE WOULD NOT MOVE TO UP POSITION. AC LANDED WITH GEAR LEFT IN DOWN POSITION. OVERWEIGHT LANDING INSPECTION REQUIRED. VISIBLE PRECIP. ICING PREVAILED ON GROUND AT T/O AND AT LEVEL OFF ALT OF 5000MSL. CLEANED SELECTOR LEVER AND MICROSWITCH IN NOSE

Next page: https://openairdocs.org/engine/garrett-tfe731-5r/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'TFE7315R'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/garrett-tfe731-5r/reports

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