Garrett TFE731-5BR

Service difficulty reports · 328

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 = 'TFE7315BR'
  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 2009FA0000286Brush Block · brokenDURING SCHEDULED INSP, ENGINE NR 1, NR 2 AND APU STARTER/GENERATORS, BRUSH INSPECTION SHOWED THE WIRES WERE BROKEN OFF SEVERAL BRUSH ASSEMBLIES. THE WEAR INDICATORS SHOWED APPROX. 50 PERCENT LIFE REMAINING. TBO AND LAST OVERHAUL AGENCY ARE UNKNOWN. THE RIVETS Apr 8, 2009 · N821LX · Raythn HAWKER800XP · Starter-GeneratorSDR DJFA2008088Oil Cap · missingDURING FLIGHT NR1 ENGINE LOW OIL PRESSURE WARNING ILLUMINATED. CREW SHUT DOWN THE NR 1 ENGINE AND DIVERTED. ACFT LANDED SAFELY. MX FOUND THE OIL SERVICING CAP NOT INSTALLED. THE OIL RESERVOIR WAS EMPTY AND OIL WAS FOUND COVERING THE EXTERIOR OF THE ENGINE. Dec 29, 2008 · N829LX · Raythn HAWKER800XP · Turbine Engine Oil SystemSDR 2008FA0000642Control Switch · inoperativeLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. (K)Sep 19, 2008 · N531FL · Amd FALCON20C5 · Landing Gear Retraction/Extension SystemSDR 2008FA0000683Landing Gear · failedLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. (K)Sep 19, 2008 · N531FL · Amd FALCON20C5 · Main Landing GearSDR 2008FA0000641Switch · inoperativeLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. (K)Sep 17, 2008 · N531FL · Amd FALCON20C5 · Landing Gear Retraction/Extension SystemSDR 2008FA0000541Module · failedAIRCRAFT EXPERIENCED A VIBRATION IN FLIGHT. CREW SHUTDOWN NR 1 ENGINE AND LANDED. MAINT CREWS DETERMINED THE THIRD STAGE LOW PRESSURE TURBINE (LPT) MODULE HAD EXPERIENCED A BLADE FAILURE. ONE BLADE WAS MISSING A PIECE ABOUT ONE INCH LONG. MAINT ALSO DISCOVERAug 1, 2008 · N225PB · Raythn HAWKER800XP · Turbine SectionSDR V0J2008F00000Eec · inoperativeNEW DIGITAL ELECTRONIC ENGINE COMPUTER WAS INOPERABLE UPON INSTALLATION. (S)Jun 25, 2008 · N1776A · Raythn HAWKER850XP · Fuel Control/Turbine EnginesSDR DXTA200803083Line · looseLT FOOT BRAKE ON CAPTS SIDE INOP. TIGHTENED LINE ON PILOTS BRAKE MASTER CYLINDER AND SERVICED AND BLED PILOTS BRAKE MASTER CYLINDER.May 28, 2008 · N872QS · Raythn HAWKER800XP · Master Cylinder/Brake ValveSDR DXTA200803060Brake Sys · intermittentWHEN APPLYING BRAKES, THEY TAKE A WHILE TO APPLY AND THEN GRAB ALL AT ONCE. DURING ENGINE RUNS APPLIED BRAKES AND NOTICED SMOOTH INCREASE IN PRESSURE AS SHOWN ON BRAKE PRESSURE GAUGE. DURING TAXI, APPLIED AND RELEASE BRAKES MANY TIMES WITH NO DEFECTS.May 14, 2008 · N858QS · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DXTA200802993Uplock Switch · inoperativeRT MLG INDICATOR RED LIGHT STAYED ON. TROUBLESHOT SYSTEM. REMOVED AND REPLACED RT MLG DOOR UPLOCK SWITCH WITH NEW SWITCH IAW MM 32-60-00. REMOVED RT MLG DOOR FOR X-RAY. RT MLG DOOR X-RAYED BY CERTIFIED INSPECTION SERVICES CRS XI8R997N, PROJECT NR 15515 AND DEApr 13, 2008 · N873QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA20082973Brake Assy · failedBRAKES ARE VERY MUSHY AND GO TO THE FLOOR. INSPECTED SYSTEM FOR LEAKS NONE NOTED. PERFORMED OPS CHECK ALL CHECK GOOD BLEED BRAKE SYSTEM AND PERFORM TAXI CHECK ALL CHECK GOOD. ALL WORK IAW MM 32-40-00.Mar 30, 2008 · N892QS · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DXTA200802973Brake Sys · contaminatedBRAKES ARE VERY MUSHY AND GO TO THE FLOOR. INSPECTED SYS FOR LEAKS, NONE NOTED. PERFORMED OPS CHECK, ALL CHECK GOOD. BLED BRAKE SYS AND PERFORMED TAXI CHECK, ALL CHECK GOOD. ALL WORK IAW MM 32-40-00.Mar 30, 2008 · N892QS · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DJFA8032Smoke Detector · looseAFTER TAKEOFF, THE CREW REPORTED THE BAGGAGE FIRE LIGHT ILLUMINATED. A FLASHING SEQUENCE WAS NOTED AND THE BAGGAGE LIGHT WAS INTERMITENT DURING THE FLIGHT. THE AC DIVERTED AND LANDED WITHOUT INCIDENT. MAINT PERFORMED VISUAL INSPECTION OF FWD / AFT / LAV SMOKEMar 25, 2008 · N809LX · Raythn HAWKER800XP · Fire DetectionSDR DJFA2008031Duct · looseWHILE IN CRUISE, FL 390 THE PILOTS STARTED TO SENSE A CHANGE IN CABIN PRESSURE BASED ON HOW THEIR EARS FELT. THEY THEN LOOKED AT THE PRESSURIZATION INSTRUMENTATION AND CONFIRMED THERE WAS CABIN PRESSURIZATION PROBLEM. PUT ON OXYGEN MASKS AND INITIATED AN EMERMar 23, 2008 · N828CW · Raythn HAWKER800XP · Humidity Control SystemSDR UG8A08P021401Retainer · looseNR 1 ENGINE FAN WOULD NOT ROTATE FREELY ON POSTFLIGHT INSP. BINDING STILL PRESENT AFTER SEVERAL HOURS OF COOL DOWN TIME. OUTSIDE VENDOR CALLED IN TO DISASSEMBLE ENGINE ENOUGH TO DETERMINE CAUSE OF BINDING. IT WAS FOUND THAT MANY OF THE FIRST STAGE TURBINE BFeb 11, 2008 · N715PH · Raythn HAWKER800XP · Turbine SectionSDR 43385883Fmc · malfunctionedUNCOMMANDED 360 DEGREE TURN AS COMMANDED BY THE FMS. SB 0057-05 DATED DECEMBER 21, 2005 DELETING A WAYPOINT MAY CAUSE THE FMS TO INSERT AND FLY AN UNINTENDED TURN. KNOWN PROBLEM WITH OPTIONAL SOLUTION FOR FMS6000 NO SOLUTION FOR FMS5000 INSTALLED IN AC.Jan 29, 2008 · N808BL · Raythn HAWKER800XP · Flight Management Computing Hardware SystemSDR 433858831Fmc · faultedUNCOMMANDED 360 DEGREE TURN AS COMMANDED BY THE FMS. REF SB 0057-05 DATED DECEMBER 21, 2005 DELETING A WAYPOINT MAY CAUSE THE FMS TO INSERT AND FLY AN UNINTENDED TURN. KNOWN PROBLEM WITH OPTIONAL SOLUTION FOR FMS6000 INSTALLED IN AC, NO SOLUTION FOR FMS5000 Jan 29, 2008 · N808BL · Beech 400A · Flight Management Computing Software SystemSDR DXTA200802793Actuator · malfunctionedRT21, MLG RED LIGHT ILLUMINATES WHEN AC IS ACCELERATED ABOVE ABOUT 280KIAS. REMOVED MALFUNCTIONING RT MLG DOOR ACTUATOR AND INSTALLED OVERHAULED ACTUATOR IAW MAINT CONTROL. VERIFIED ALL RT MLG INDICATION WIRING CONDITION AND SECURITY WITH SATISFACTORY RESULTSJan 24, 2008 · N896QS · Raythn HAWKER800XP · Landing Gear ActuatorSDR DXTA200802789Solenoid Valve · inoperativeNR 2 ENGINE COMPUTER ANNUNCIATOR LIGHT ON STEADY. REPLACED LT ENGINE SURGE VALVE SOLENOID "A" IAW TFE 731-5BR LMM CH 76-10-01. OPERATIONAL CHECK SATISFACTORY IAW TFE731-5BR LMM CH 72-00-00.Jan 22, 2008 · N838QS · Raythn HAWKER800XP · Engine Fuel Indicating SystemSDR DXTA200802779Squat Switch · inoperativeAFTER LANDING GEAR RETRACTION, RT MAIN GEAR UNLOCKED ANNUNCIATOR ILLUMINATED. REPLACED RT LANDING GEAR WOW SWITCH IAW RAC DWG. 25-8 NAS-2584. OPS.CK GOOD.REF: (HBS-LIT) W/O 19-1608.Jan 20, 2008 · N845QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA200802773Warning Light · illuminatedAFTER TAKEOFF AND GEAR RETRACTION, THE RT MAIN GEAR (RED ANNUNCIATOR) REMAINED ILLUMINATED.Jan 17, 2008 · N896QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA200802770Indication Sys · malfunctionedWITH GEAR SELECTED UP AFTER T/O ALL 3 GEAR INDICATED UNSAFE WITH RED LIGHTS. JACKED AIRCRAFT CYCLED NOSE ONLY THEN UNPINNED MAINS COMPLETED 2 MORE COMPLETE CYCLES WITH NO FAULTS. WORK COMPLETED IAW MM 29-10-00.Jan 16, 2008 · N893QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DJFA2008003Brake Assy · weakCREW REPORTED THE BRAKES NEEDED EXCESSIVE FORCE TO APPLY BRAKING ACTION. PEDALS WENT NEARLY TO THE FLOOR. THE SAME PROBLEM WAS REPORTED TWO DAYS PRIOR (REF SDR DJFA2008002) AND THE AIRCRAFT FLEW 5 FLIGHTS WITHOUT DISCREPANCIES. MAINTENANCE BLED THE BRAKE COJan 13, 2008 · N815TA · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DJFA2008002Brake · inoperativeCREW REPORTED BREAKS REQUIRED EXCESSIVE PRESSURE TO ACTUATE. PEDALS NEEDED TO BE PUSHED NEARLY TO FULL TRAVEL TO OBTAIN BRAKING ACTION. MAINTENANCE BLED THE BRAKES AND CHECKED THE SYSTEM. THE SYSTEM CHECKED OK.Jan 11, 2008 · N815TA · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DXTA200802760Unknown · fumesAIRCRAFT INTERIOR HAS A TOXIC FUME ODOR TO IT, CAUSING BREATHING DISCOMFORT AND EYE IRRITATION. CLEANED AIRCRAFT CARPET. VENTILATED AIRCRAFT. NO TOXIC FUME ODOR NOTED AT THIS TIME.Jan 10, 2008 · N815QS · Raythn HAWKER800XP · Air Distribution SystemSDR DXTA200802756Spring · lack of lubeRT MAIN GEAR RED ANNUNCIATOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION AFTER TAKEOFF. REMOVED, CLEANED & LUBRICATED SPRING MECHANISM FOR RT DOOR HOOK., TESTED SPRING LOAD, INSTALLED ASSY & PERFORMED SATISFACTORY GEAR SWING, ALL TESTS GOOD. IAW HAWKER Jan 9, 2008 · N870QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA200802744Switch · malfunctionedAFTER T/O AND GEAR RETRACTION THE RT MAIN GEAR (RED) LIGHT REMAINED ILLUMINATED. REPLACED RT MLG DOOR UP SWITCH WITH NEW P/N 1EN1-14N119, PERFORMED SATISFACTORY OPS CHECK. IAW MM 32-40-00.Jan 3, 2008 · N896QS · Raythn HAWKER800XP · Landing Gear Door Retract SectionSDR DJFA2007151Valve · smokeIN CRUISE CREW REPORTED SMOKE FILLED THE COCKPIT WITH A BURNING ODOR WHEN THE HEAT VALVE WAS OPENED. SMOKE CLEARED WHEN THE VALVE WAS CLOSED AND THE DUMP PARTIALLY OPENED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY.Dec 28, 2007 · N830LX · Raythn HAWKER800XP · Heating SystemSDR DXTA200702717Uplock Switch · contaminatedRT MAIN GEAR UNSAFE LIGHT ILLUMINATED SHORTLY AFTER TAKEOFF CLIMBING THRU 17000 FT. FOUND RT GEAR DOOR UPLOCK SWITCH WATER SOAKED - CLEANED & LUBED SWTICH - COLD SOAKED SWITCH NO DEFECTS NOTED & PERFORMED GEAR SWINGS PER 800XP MM 32-30-01. OPS CHECK GOOD.Dec 27, 2007 · N870QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA200702710Engine · smokeCLIMBING THRU FL310 THE RT ENGINE PRODUCED A LOUD BANG ACCOMPANIED BY VIBRATIONS AND N1/N2 STARTED ROLLING BACK. WITH THE SMELL OF SMOKE IN COCKPIT THE CREW SHUTDOWN THE ENGINE. REMOVED & REPLACED RIGHT ENGINE WITH INSPECTED UNIT IAW H800XP AMM 71-00-01. LEAKDec 21, 2007 · N824QS · Raythn HAWKER800XP · Engine (Turbine/Turboprop)SDR DXTA200702699Roller · malfunctionedAFTER T/O AND GEAR RETRACTION THE RT MAIN GEAR RED LIGHT STAYED ON. FOUND RT IB GEAR DOOR (MAIN) UPLOCK ROLLER TO BE OUT OF RIG. RIGGED DOOR IAW HAWKER 800XP MM 32-10-41. OPS CHECK WAS GOOD.Dec 20, 2007 · N873QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DJFA2007145Brake · erraticON LANDING CREW REPORTED BRAKES DO NOT APPLY WHEN BRAKE PEDALS ARE DEPRESSED IN A NORMAL FASHION BRAKE PEDALS MUST BE DEPRESSED MUCH FURTHER DOWN THAN NORMAL BEFORE BRAKING OCCURS WHEN BRAKES DO APPLY THEY GRAB OR SUDDENLY OVER APPLY DIRECTIONAL CONTROL DIFFICDec 16, 2007 · N839LX · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DJFA2007144Acm · seizedON TAXI AFTER LANDING APU GENERATED SMOKE IN THE CABIN; SWITCHING BLEED AIR OFF REDUCED THE SMOKE. MAINTENANCE DISCOVERED THE ACM FROZEN AND A DUCT OVERHEATED TO THE POINT OF DISTORTION AND MELTING. MAINTENANCE REPLACED THE ACM.Dec 13, 2007 · N830LX · Raythn HAWKER800XP · Cabin Cooling SystemSDR DXTA200702662Metering Valve · bypassingBRAKES ARE VERY MUSHY, LT BRAKE ALMOST GOES TO THE FLOOR. REMOVED MAIN REDUCING VALVE & INSTALLED OVERHAULED MAIN REDUCING VALVE & BLED FULL BRAKE SYSTEM, OPS CHECKS GOOD. IAW 800XP MM CH 32-40-00.Dec 8, 2007 · N858QS · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DXTA200702655Landing Gear · false indicationUPON GEAR RETRACTION, (3) RED LIGHTS ALONG WITH 1 GREEN FOR THE NOSEWHEEL ARE INDICATED FOR 1 MINUTE AFTER SELECTING GEAR UP. INSPECTED GEAR AND CYCLED SEVERAL TIMES IAW MM 29-10-00-501. NO DEFECTS NOTED AT THIS TIME.Dec 6, 2007 · N893QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA200702646Sequence Valve · malfunctionedRT MAIN GEAR DOOR REMAINS OPEN WITH GEAR RETRACTED-TOWER VERIFIED GEAR DOOR-RT MAIN INDICATOR HAD RED LIGHT. REMOVED AND REPLACED RT MLG DOOR SEQUENCE VALVE IAW MM 32-30-41 AND RT MLG DOOR JACK IAW MM 32-10-41 LEAK CHECKED & OPS CHECKED GOOD.Dec 3, 2007 · N873QS · Raythn HAWKER800XP · Landing Gear Door Retract SectionSDR DXTA200702643Squat Switch · malfunctionedAFTER T/O, LANDING GEAR WOULD NOT RETRACT, SQUAT AND STALL IDENT WARNING LIGHTS CAME ON. REPLACED LT & RT MLG WOW SWITCH . ROUTED WIRE TO TERMINAL BLOCKS "JK" AND "KK" AND TERMINATED. PERFORMED OPERATIONAL CHECKS AS REQUIRED WITH NO DEFECTS NOTED. ALL WORK PEDec 2, 2007 · N867QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DJFA2007138Heater · smokeAT FL 400 CREW REPORTED SMOKE AND FUMES IN THE COCKPIT APPROX 3 MINS AFTER ACTIVATING/OPENING FLIGHT DECK HEAT VALVE. SMOKE WENT AWAY AFTER HEAT VALVE WAS CLOSED. MAINTENANCE COULD NOT DUPLICATE THE DISCREPANCY. DUCTS WERE CHECKED FOR EVIDENCE OF CONTAMINATDec 2, 2007 · N733TA · Raythn HAWKER800XP · Heating SystemSDR DXTA200702640Indication Sys · malfunctionedAFTER TAKEOFF DURING GEAR RETRACTION, GEAR INDICATORS SHOWED 3 GREEN AND 3 RED . SELECTED GEAR BACK DOWN AND GOT 3 GREEN. FOUND AUXILLIARY PUMP HANDLE IN UP POSITION AND AUX HANDLE PULLED. JACKED ACFT, CYCLED GEAR SEVERAL TIMES WITH SATISFACTORY RESULTS. GEADec 1, 2007 · N871QS · Raythn HAWKER800XP · Landing Gear Retraction/Extension SystemSDR DXTA200702628Switch · out of rigRT MAIN GEAR RED INDICATION REMAINED ILLUMINATED AFTER GEAR RETRACTION AND ALL GREEN INDICATORS WERE EXTINGUISHED. PERFORMED NUMEROUS OPS CHECKS OF GEAR WITHOUT ANY DISCREPANCIES, CHECK RIGGING OF GEAR UPLOCK DOOR SWITCH IAW AMM 32-60-00 & RAC DWGS. 25-8NA5-Nov 25, 2007 · N873QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA200702618Warning Light · malfunctionedRT MAIN GEAR RED INDICATION STAYED ILLUMINATED AFTER GEAR RETRACTION. ALL GREEN INDICATION WERE EXTINGUSHED. CHECKED RESISTANCE AND VOLTAGE ON MAIN GEAR DOWN LOCK AND DOOR UPLOCK SWITCHES. CHECKED GOOD. CHECKED RIGGING ON REVERSING VALVE AND SEQUENCE VALVE CHNov 19, 2007 · N873QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA200702619Connector · damagedDURING CRUISE AT F300, AIRCRAFT PITCHED UP ABOUT 15 DEGREES AND AUTOPILOT KICKED OFF. RESEATED PIN (C) OF CONNECTOR GND 28 SYSTEM GROUND CHECKS GOOD IAW DWG NR A8-43-100 REV. F AND AMM 34-22-05. REF 19-1415 SQK 1.5Nov 19, 2007 · N836QS · Raythn HAWKER800XP · Auto Flight System WiringSDR DXTA200702613Uplock Switch · malfunctionedRT MAIN GEAR (RED INDICATION) STAYED ILLUMINATED AFTER GEAR RETRACTION. ALL GREEN INDICATORS WERE EXTINGUISHED. GEAR DEPLOYED NORMALLY WITH ALL INDICATIONS IN THE GREEN. REPLACED RIGHT HAND DOOR UP LOCK SWITCH "KN" PER WIRING DIA. 32-60-10-05, 34-13-01-10 ANDNov 16, 2007 · N873QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA200702594Brake Assy · weakBOTH PILOT AND COPILOT BRAKES ARE SPONGY. PEDALS TRAVEL HALF WAY BEFORE ANY BRAKING ACTION. PERFORMED OPS CHECK OF BRAKE SYSTEM. NO DISCREPANCIES NOTED IAW 32-40-00.Nov 4, 2007 · N838QS · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DXTA200702559Fuse · openELECTRIC ELEVATOR TRIM FAILED IN FLIGHT. REMOVED AND REPLACED ELEVATOR E-TRIM SERVO FUSE ZL-F24 PN:622-3260 SN:1CKYC AND PN: 5920-99-012-0075. PERFORMED SYSTEM FUNCTIONAL CHECK IAW AMM 27-30-00.Oct 22, 2007 · N895QS · Raythn HAWKER800XP · Elevator Control SystemSDR DXTA200702510Computer · malfunctionedDURING TAKEOFF ROLL AT APPROXIMATELY V1 OF 111KIAS, THE NR2 COMPUTER FAILED (STEADY LIGHT) IT WAS ACCOMPANIED BY A ROLL BACK OF THE NR2 ENGINE AND A SUBSEQUENT APR TRIGGER (EVENT) DURING INITIAL CLIMBOUT. THE NR2 ITT READ 996 DEG FOR APPROXIMATELY 1 MINUTE UNTSep 29, 2007 · N815QS · Raythn HAWKER800XP · Engine Fuel Indicating SystemSDR DXT2007F00001Engine · power lossDURING TAKEOFF ROLL AT APPROXIMATELY V1 OF 111KIAS, THE NR 2 COMPUTER FAILED (STEADY LIGHT) IT WAS ACCOMPANIED BY A ROLL BACK OF THE NR 2 ENGINE AND A SUBSEQUENT APR TRIGGER (EVENT) DURING INITIAL CLIMBOUT. THE NR 2 ITT READ 996 DEG FOR APPROXIMATELY 1 MINUTE Sep 29, 2007 · N815QS · Raythn HAWKER800XP · Engine (Turbine/Turboprop)SDR CA070927004Line · chafed(CAN) DURING SCHEDULE INSPECTION FOUND 2 OIL LINES CHAFING. THE SAME PROBLEM WAS ON BOTH ENGINES.THE PROBLEM COMES FROM THE FACTORY SINCE THE AIRCRAFT IS NEW AND LOW TIME. THE AIRCRAFT HISTORY DOES NOT SHOW ANY MAINTENANCE ACTION BEING PERFORMED IN THAT AREA SSep 26, 2007 · Raythn HAWKER850XP · Turbine Engine Oil SystemSDR DXTA200702483Duct · looseBAG FIRE LIGHT CAME ON IN FLIGHT DURING T/O. 09-28-07 FOUND BLEED AIR DUCT LEAKING TIGHTENED DUCT CLAMP OPS CHECKED GOOD IAW HAWKER 800XP AMM 21-10-15.Sep 16, 2007 · N821QS · Raythn HAWKER800XP · Pneumatic Distribution SystemSDR 2007FA0000893Turbine Wheel · failedCLIMBING THROUGH FL270, A LOUD BANG IN REAR OF ACFT. LT ENGINE COMPUTER LIGHT ILLUMINATED. PF BROUGHT LT ENGINE TO IDLE, PNF PULLED CHECKLIST. AFTER SURVEY OF ENGINE PARAMETERS, PF TURNED LT ENGINE COMPUTER BACK ON TO CONTROL PARAMETERS. ENGINE COMPUTER DIDSep 14, 2007 · N800WY · Raythn HAWKER800XP · Turbine Engine Compressor Section
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