Garrett TPE331-10UA

Service difficulty reports · 375

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 = 'TPE33110UA'
  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 CA041008002Regulator · leaking(CAN) UPON LANDING THE FLIGHT CREW NOTICED FUEL RUNNING OUT OF THE ENGINE COWLING AND DRIPPING FROM THE LT WHEEL WELL. MAINTENANCE WAS INFORMED AND DISCOVERED THAT THE START FUEL PRESSURE REGULATOR WAS LEAKING FUEL OUT OF THE ELECTRICAL CONNECTOR PORTION OF TOct 6, 2004 · Swrngn SA226TC · Fuel Pressure SensorSDR CA040726003Bearing Cage · worn(CAN) UPON RECEIVING A REQUEST, FROM WEAR CHECK, DUE TO A BAD ENGINE OIL SAMPLE, A TEAR DOWN OF THE SUSPECT ENGINE REVEALED THAT THE HIGH SPEED PINION BEARING AND CAGE WERE WORN AND THE SILVER COATING FLAKINGOFF OF THE COMPONENTS. THE PINION HAS BEEN REPLACED.Jul 23, 2004 · Turbine SectionSDR CA040705004Steering Sys · inoperative(CAN) UPON LANDING, WHEN SPEED LEVERS SELECTED TO LOW AT 70 KIAS, NOSE WHEEL STEERING WAS ARMED AND THE AIRCRAFT VEERED SHARPLY RT AND DEPARTED THE RUNWAY. THE ENGINES WERE SHUTDOWN AS A PRECAUTIONARY MEASURE. NO DAMAGE NOTED. THE AIRCRAFT STOPPED ON THE ADJun 30, 2004 · Swrngn SA226TC · Landing Gear Steering SystemSDR CA040629004Fcu · unserviceable(CAN) DURING THE ATTEMPTED ENGINE START, THE EGT ROSE RAPIDLY TOWARDS REDLINE AND THE ENGINE WAS SHUTDOWN. TOO MUCH FUEL WAS BEING INTRODUCED DURING THE START SEQUENCE THEREFORE CAUSING THE OVERTEMP PROBLEM. THE FUEL CONTROL WAS REPLACED. ENCOUNTER THIS PROBLJun 23, 2004 · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA040617002Bearing · making metalAN IMMEDIATE ENGINE INSPECTION WAS REQUESTED BY WEAR CHECK DUE TO MAJOR SILVER CONTENT IN THE OIL SAMPLE. UPON INSPECTION OF THE ENGINE GEAR CASE THE HIGH SPEED PINION BEARING AND CAGE WERE FOUND TO HAVE THE SILVER COATING FLAKING OFF. THIS PROBLEM IS IDENTJun 16, 2004 · Swrngn SA226TC · Turbine SectionSDR CA040617003Bearing · overheatedDURING A SCHEDULED ENGINE INSPECTION OF THE HIGH SPEED PINION ASSY A BRIGHT BLUECOLOR WAS NOTICED ON THE PINION GEAR. THE HIGH SPEED PINION SUFFERED SEVERE HEAT DAMAGE CLOSE TO THE POINT OF FAILURE. THIS PART WAS PURCHASED THROUGH AN AMERICAN PARTS DISTRIBUTJun 15, 2004 · Turbine SectionSDR CA040617004Master Cylinder · lockedDURING A MAINTENANCE RUN-UP AND SUBSEQUENT TAXI, THE BRAKES LOCKED UP AND THE AIRCRAFT COULD NOT BE MOVED. BRAKE PRESSURE WAS RELIEVED AT THE BRAKE ASSY AND WAS FOUND THE NR 1 BRAKE MASTER CYLINDER HAD MALFUNCTIONED AND CAUSED THE BRAKES TO LOCK UP. REFERENCJun 14, 2004 · Swrngn SA226TC · BrakeSDR CA040617005Pin · brokenDURING A DAILY INSPECTION, IT WAS NOTICED THAT THE RT MAIN LANDING GEAR SCISSOR LINK UPPER PIN WAS FOUND BROKEN. THE PIN BROKE AT THE RETAINING HOLE IN WHICH A ROLL PIN IS INSTALLED. IT WAS ALSO DETERMINED THAT THIS PIN WAS FOR A NOSE GEAR INSTALLATION. ALTJun 14, 2004 · Swrngn SA226TC · Main Landing Gear Strut/Axle/TruckSDR CA040611004Pinion Gear · worn(CAN) OIL SAMPLE ANALYSIS FINDING RECEIVED FROM WEAR CHECK TO INSPECT ENG DUE TO SILVER IN OIL SAMPLE. DURING TEARDOWN, FOUND PINION GEAR BEARING CAGES, WHICH HAVE SILVER COATING APPLIED DURING MFG. COATING HAD STARTED TO FLAKE OFF, CONTAMINATING OIL. MFG OFJun 11, 2004 · Swrngn SA226TC · Turbine SectionSDR CA040618006Link Assy · crackedFOUND LEFT AND RIGHT LINK ASSY ON AILERON PUSH PULL TUBES CORRODED AND CRACKED ON ALL FOUR SIDES. PARTS WERE REMOVED AND A NEW LINK ASSY WERE INSTALLED.Jun 10, 2004 · Swrngn SA226TC · Aileron Control SystemSDR CA040610005Switch · faulty(CAN) SHORTLY AFTER TAKEOFF, WHILE STILL CLIMBING, THE LT WING LOWER HEAT BEGAN TO FLASH. THE LT BLEED AIR AND THE LT GENERATOR WERE TURNED OFF FLIGHT MANUAL PROCEDURES, AND THE AIRCRAFT TURNED BACK FOR THE DEPARTURE POINT. AFTER THREE MINUTES THE LIGHT CONTINJun 7, 2004 · Swrngn SA226TC · Overheat DetectionSDR CA040611003Pin · loose(CAN) AC HAD A CHIP LIGHT ILLUMINATE DURING CRUISE. PREVIOUS DAY A CHIP LIGHT ILLUMINATED AND A SMALL SLIVER OF METAL WAS FOUND ON CHIP DETECTOR. AN OIL SAMPLE WAS TAKEN AND SENT FOR ANALYSIS. AFTER ILLUMINATION OF CHIP LIGHT, ENGINE WAS REMOVED FOR INSP. UPJun 7, 2004 · Swrngn SA226TC · Turbine SectionSDR AUS20040476Drag Brace · cracked(AUS) LT IB LOWER MAIN LANDING GEAR DRAG BRACE CRACKED IN AREA ADJACENT TO GREASE FITTING. FOUND DURING INSPECTION IAW AD/SWSA226/89 AND SB226-32-068.Jun 3, 2004 · Swrngn SA226TC · Landing Gear Retraction/Extension SystemSDR AUS20040280Panel · faulty(AUS) COPILOTS AUDIO PANEL FAULTY. SMOKE AND ODOR IN COCKPIT. SMOKE AND ODOR DISSIPATED WHEN CIRCUIT BREAKER POPPED.Apr 19, 2004 · Swrngn SA226TC · Audio Integrating SystemSDR CA040415007Pinion Gear · broken(CAN) AFTER TAKEOFF, FLIGHT CREW HAD CHIP DETECTOR LIGHT ILLUMINATE ON RT ENG. CREW REDUCED POWER AND IMMEDIATELY RETURNED TO LAND. MAINT WAS SENT TO INSPECT CHIP DETECTOR, DISCOVERED SEVERAL CHUNKS OF FERROUS METAL ON CHIP DETECTOR PLUG. OIL FILTER WAS REMOVApr 13, 2004 · Swrngn SA226TC · Turbine SectionSDR CA040405002Nut · mismanufactured(CAN) UPON ATTEMPTING TO INSTALL THE REAR TURBINE SHAFT NUT ONTO TURBINE SHAFT IT WAS FOUND THAT THE NUT WOULD ONLY THREAD HALFWAY DOWN & THEN THREADS WOULD START TO PILE UP AND BIND. WITH THE TURBINESHAFT IN AN UNSTRETCHED CONDITION, NUT WOULD WORK FINE & WOUApr 5, 2004 · Turbine SectionSDR AUS20040234Gust Lock · cracked(AUS) RUDDER GUSTLOCK CRACKED.Mar 28, 2004 · Swrngn SA226TC · Rudder Control SystemSDR CA040227002Heat Exchanger · contaminated(CAN) ACFT LEVELED OFF IN CRUISE, FLT CREW NOTICED A FOUL ODOUR. FUMES BECAME QUITE STRONG & FLT CREW CALLED MX & RETURNED TO BASE. ENROUTE, SEVERAL PAX WERE SUPPLIED O2 DUE TO ODOUR. UPON INSP OF ACFT & MX RECORDS FROM PREVIOUS NIGHT, AIR TO AIR HEAT EXCHANGEFeb 26, 2004 · Swrngn SA226TC · Heating SystemSDR CA040226006Engine · making metal(CAN) ONCE AT LEVEL FLIGHT THE RT ENGINE OIL PRESSURE WAS NOTICE TO BE AT THE LOWER END OF THE GREEN ARC 70 PSI, THE OIL PRESSURE WAS MONITORED UNTIL IT DROPPED TO 65 PSI AND THE CREW ELECTED TO RETURN. THE PRESSURE REMAINED STABLE AT 65 PSI, UNTIL TOUCHDOWN WFeb 24, 2004 · Swrngn SA226TC · Engine (Turbine/Turboprop)SDR CA040227001Engine · making metal(CAN) ONCE AT LEVEL FLIGHT THE RT ENGINE OIL PRESSURE WAS NOTICE TO BE AT THE LOWER END OF THE GREEN ARC 70 PSI, THE OIL PRESSURE WAS MONITORED UNTIL IT DROPPED TO 65 PSI AND THE CREW ELECTED TO RETURN. THE PRESSURE REMAINED STABLE AT 65 PSI, UNTIL TOUCHDOWN WFeb 24, 2004 · Swrngn SA226TC · Engine (Turbine/Turboprop)SDR AUS20040122Bracket · cracked(AUS) HORIZONTAL STABILIZER PITCH TRIM ACTUATOR UPPER ATTACHMENT BRACKET CRACKED.Feb 24, 2004 · Swrngn SA226TC · Stabilizer Control SystemSDR AUS20040121Actuator · faulty(AUS) PITCH TRIM ACTUATOR SLIPPING.Feb 20, 2004 · Swrngn SA226TC · Elevator Tab Control SystemSDR CA040217002Hose · cracked(CAN) THE HOSE THAT SUPPLIES THE CABIN DOOR SEAL CRACKED, ALLOWING THE SEAL TO DEFLATE WHICH IN TURN ALLOWED THE CABIN OF THIS FREIGHTER TO DEPRESSURIZE AT 17000 FT. THE CREW DESCENDED TO A SAFE ALTITUDE AND COMPLETED THE FLIGHT.Feb 11, 2004 · Swrngn SA226TC · Passenger/Crew DoorsSDR CA040203003Control Chain · worn(CAN) DURING DECENT THE FLIGHT CREW NOTICED THE AILERONS BINDING AND VERY DIFFICULT TO MOVE. UPON SLOWING DOWN THE AIRCRAFT THE AILERON CONTROL RETURNED TO NORMAL. INVESTIGATION BY MAINTENANCE REVEALED THAT THE 27-71026-001 CONTROL CHAIN WAS SEIZED AND ALMOSFeb 2, 2004 · Swrngn SA226TC · Aileron Control SystemSDR AUS20040047Doubler · corroded(AUS) FUSELAGE DOUBLER LOCATED AT RT EMERGENCY EXITS, BADLY CORRODED.Jan 30, 2004 · Swrngn SA226TC · Fuselage Main, Plate/SkinSDR CA040115002Plenum · cracked(CAN) FLIGHT CREW RECEIVED SPLIT SECOND FIRE WARNING INDICATION ON LT ENG. DUE TO BRIEF NATURE OF IND FLIGHT CREW MONITORED GAUGES, DETERMINED FALSE INDICATION. SHORTLY AFTER ENG STARTED LOSING PWR UNTIL IT REACHED ABOUT 55 PERCENT TORQUE. UPON INSP, LT ENG PJan 13, 2004 · Swrngn SA226TC · Turbine Engine Compressor SectionSDR CA031224002Case · cracked(CAN) ACRFT RETURNED WITH A LOW OIL PRESS. ON RESEARCHING ENG TRENDS, OIL PRESS HAD BEEN STEADILY DECLINING FOR APPROX A MONTH AT 1-2 PSI A DAY. PROBLEM WASN`T NOTICED BY FLT CREW UNTIL A SUBSTANTIAL DROP ON DAY OF INCIDENT. OIL PRESSURE WOULD ONLY DROP ON A HDec 23, 2003 · Swrngn SA226TC · Turbine Engine Reduction GearSDR CA031209004Pressure Switch · cracked(CAN) ON TAXI IN FROM THE LAST FLIGHT OF THE DAY, THE CREW NOTICED THE OIL PRESSURE LIGHT ILLUMINATED. THE GAUGE CONFIRMED THE INDICATION. THE CREW SHUT THE ENGINE DOWN. ON ARRIVAL AT THE RAMP, A SUBSTANTIAL AMOUNT OF OIL WAS FOUND LEAKING FROM THE COWL. MAIDec 8, 2003 · Swrngn SA226AT · APU Start/Ignition SystemSDR SDR11280376Control Cable · chafedDURINE TAKE OFF PREPORATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LEFT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTIN REVEALED THE PONov 28, 2003 · N228AM · Swrngn SA226TC · Power LeverSDR 11280376Control Cable · chafedDURINE TAKE OFF PREP, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTION REVEALED THE POWER LEVENov 28, 2003 · N228AM · Swrngn SA226TC · Power LeverSDR 11290376Control Cable · chafedDURINE TAKE OFF PREPORATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LEFT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTIN REVEALED THE PONov 28, 2003 · N228AM · Swrngn SA226TC · Power LeverSDR SDR11290376Control Cable · chafedDURING TAKE OFF PREP, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LEFT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTIN REVEALED THE POWER LEVNov 28, 2003 · N228AM · Swrngn SA226TC · Power LeverSDR 22811290376Control Cable · chafedDURING TAKE OFF PREPARATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTION REVEALED THE POWNov 28, 2003 · N228AM · Swrngn SA226TC · Power LeverSDR 21200003Control Cable · chafedDURING TAKE OFF PREPORATION, PILOT ADVANCED POWER LEVERS AND NOTED THAT THE LT ENGINE POWER DID NOT RESPOND. THE TAKEOFF WAS ABORTED, BRAKES HAD NOT BEEN RELEASED, THEY RETURNED TO THE RAMP, NO EMERGENCY ACTIONS REQUIRED. SUBSEQUENT INSPECTION REVEALED THE POWNov 28, 2003 · N228AM · Swrngn SA226TC · Power LeverSDR CA031124004Pin · popped(CAN) THE OIL FILTER BYPASS PIN WAS FOUND POPPED ON THE LT ENGINE. THE OIL FILTER WAS REPLACED. DAMAGE TO THE REMOVED OIL SAMPLE WAS NOTED. THE MOUNTING FLANGE OF THE FILTER WAS MISSING FROM THE RADIUS INWARD. THE OIL FILTER P/N 3001436-1 IS INCLUDED IN THENov 21, 2003 · Swrngn SA226TC · Engine Oil Distribution (Airframe Furnished)SDR CA031113012Oil Filter · damaged(CAN) THE OIL FILTER BYPASS PIN WAS FOUND POPPED ON THE LT ENGINE. THE OIL FILTER WAS REPLACED AND OIL SAMPLE TAKEN. DAMAGE TO THE REMOVED OIL SAMPLE WAS NOTED. THE MOUNTING FLANGE OF THE FILTER WAS MISSING FROM THE RADIUS INWARD. THE OIL FILTER IS INCLUDED Nov 9, 2003 · Swrngn SA226TC · Turbine Engine Oil SystemSDR CA031105003Engine · surges(CAN) UPON DEPARTURE/CLIMB PHASE OF FLIGHT, LT ENGINE CHIP DETECTOR LIGHT CAME ON STEADY. FLIGHT CREW MONITORED GAUGES AND NOTICED LT OIL PRESSURE GAUGE HAD EXCEEDED RED LINE LIMIT. SHORTLYAFTER ENGINE POWER BEGAN TO SURGE. LT POWER LEVER WAS REDUCED IN SMALLNov 3, 2003 · Swrngn SA226TC · Engine (Turbine/Turboprop)SDR CA031110004Hose · leaking(CAN) UPON DESCENT, CREW SELECTED GEAR DOWN. RT GEAR INDICATED ONLY (IN TRANSIT). CREW DID A FLY BY AND TOWER CONFIRMED THAT THE GEAR WAS NOT DOWN. THE CREW CLIMBED OUT, SELECTED THE EMERGENCY GEAR SYSTEM, AND THE GEAR EXTENDED NORMALLY. THEY DID ANOTHER FLOct 29, 2003 · Swrngn SA226TC · Landing Gear Retraction/Extension SystemSDR CA031024004Oil Filter · damaged(CAN) DURING A SCHEDULED OIL SAMPLE ON THE RT ENGINE THE OIL FILTER REMOVED WAS NOTEDTO BE DAMAGED AT THE RADIUS OF THE MOUNTING FLANGE. THIS IS THE OIL FILTER THAT IS INCLUDED IN THE WEAR CHECK CANADA INC. P/N GT-331 OIL SAMPLE KITS.Oct 23, 2003 · Swrngn SA226TC · Engine Oil Distribution (Airframe Furnished)SDR CA031024005Oil Filter · damaged(CAN) ON PILOT PREFLIGHT INSPECTION IT WAS DISCOVERED THE RT ENGINE OIL FILTER BYPASS WAS POPPED, THE OIL FILTER WAS REPLACED, AND OIL SAMPLE TAKEN. IT WAS NOTED THE THE REMOVED OIL FILTER WAS DAMAGED WITH MATERIAL MISSING FROM THE FLANGE. WE BELIEVE THE FILOct 23, 2003 · Swrngn SA226TC · Engine Oil Distribution (Airframe Furnished)SDR CA031024006Oil Filter · damaged(CAN) THE OIL FILTER BYPASS PIN WAS FOUND POPPED ON THE LT ENGINE.THE OIL FILTER WAS REPLACED AND OIL SAMPLE TAKEN. DAMAGE TO THE REMOVED OIL SAMPLE WAS NOTED. THE MOUNTING FLANGE OF THE FILTER WAS MISSING FROM THE RADIUS INWARD. THE OIL FILTER IS INCLUDED IN Oct 23, 2003 · Swrngn SA226TC · Engine Oil Distribution (Airframe Furnished)SDR CA031015021Receptacle · cracked(CAN) DISCOVERED CARGO DOOR (KLICK-KLACK) RECEPTACLE CRACKED WHILE COMPLYING WITH SERVICE LETTER 226-SL-027, WHICH DEALS WITH THIS PROBLEM. DISCOVERED BY REMOVING ECCENTRIC BUSHING, AND IT WAS IMMEDIATELY VISIBLE. PART WAS CRACKED THROUGH FROM THE CENTER OF TOct 15, 2003 · Swrngn SA226TC · Cargo/Baggage DoorsSDR CA031006008Wire · damaged(CAN) FLT LANDING, ONCE DECELERATED TO 60 KNOTS NOSE WHEEL STEERING WAS ARMED, RESULTING IN AN UN-COMANDED FULL AUTHORITY LT TURN CAUSING A/C TO LEAVE RUNWAY. A/C WAS TAXIED OUT ON IT OWN POWER, AFTER INSP FERRIED ON FLIGHT PERMIT FOR MORE STRUCTURAL INSP ANDOct 2, 2003 · Swrngn SA226AT · Landing Gear Steering SystemSDR CA030722005Bushing · cracked(CAN) DURING COMPLETION OF MFG SERVICE LETTER 226-SL-027 INSPECTION OF CABIN AND CARGO DOOR CLICK CLACK BUSHING RECEPTICLES FOR CRACKS, THE NR 3 CABIN DOOR RECEPTICLE WAS FOUND CRACKED IAW THE SERVICE LETTER. THE RECEPTICLE WAS REPLACED. ALL OTHER RECEPTICLES Jul 22, 2003 · Swrngn SA226TC · Cargo/Baggage DoorsSDR CA030711001Wire · broken(CAN) ON LANDING THE RT MAIN DID NOT INDICATE GREEN SO THE PILOT DIVERTED TO A MAJOR CENTER WHERE THE TOWER CONFIRMED THE GEAR WAS DOWN AND HE LANDED WITHOUT INCIDENT. THE GROUND WIRE TO THE RT INBOARD ACTUATOR SWITCH WAS FOUND TO BE BROKEN IN THE SERVICE LOOPJul 10, 2003 · Swrngn SA226TC · Landing Gear System WiringSDR CA030714001Counterweight · torn(CAN) PILOT DISCOVERED ON HIS POST FLIGHT WALKAROUND THAT THE LT AILERON COUNTERWIEGHTWAS HANGING DOWN ON THE INBOARD END OF THE AILERON. THE AILERON WAS REMOVED AND THE BALANCE WEIGHT WAS FOUND TO HAVE TORN OUT OF THE INBOARD BOLT HOLE. THE DAMAGED PART OF THJul 8, 2003 · Swrngn SA226TC · AileronsSDR CA030709008Spline Adapter · failed(CAN) CREW STARTED ENG & NOTICED ENG WAS SLOW TO ACCELERATE TO IDLE. ONCE AT IDLE (70 PERCENT) ENGINE SLOWLY INCREASED TO APPROXIMATLY 80 PERCENT WITHOUT INPUT FROM CREW. IN AN ATTEMPT TO REDUCE ENG POWER, WAS NO RESPONSE TO ENG CONTROL INPUTS BY CREW. ENG SHUJul 7, 2003 · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA030620002Receptacle · cracked(CAN) WHILE CARRYING OUT SERVICE LETTER 226-SL-027, WHICH CALLS FOR INSPECTION OF THE ALL DOOR LATCH RECEPTICLES, WE FOUND 3 CRACKED ON PASSENGER DOOR FRAME & 2 CRACKED ON THE AFT CARGO DOOR FRAME. ONE RECEPTICAL WAS CRACKED ALMOST IN HALF WHILE OTHERS SMALL AJun 18, 2003 · Swrngn SA226TC · Fuselage Miscellaneous StructureSDR CA030610010Fuel Control · inoperative(CAN) UPON PERFORMING A GROUND RUN FOR AN ENGINE REPLACEMENT AND UPON THE APPLICATION OF FULL POWER THE ENGINE RESPONSE WAS GOOD, BUT IN ATTEMPT TO DECREASE ENGINE POWER THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUTS. IT WAS APPROXIMATELY 30 SECOND TO A MINUTJun 9, 2003 · Swrngn SA226TC · Fuel Control/Turbine EnginesSDR CA030527005Line · broken(CAN) FLIGHT CREW COMPLAINED OF PRESSURIZATION PROBLEMS. THE CABIN DIFFERENTIAL WAS LOWER THAN NORMAL. UPON INSPECTION OF THE RT WING AIR CONDITIONING SYSTEM THE FLEXABLE ACCORDION STYLE BLEED AIR LINE FROM THE HEAT EXCHANGER/COOLING TURBINE ASSY WAS FOUND BROMay 26, 2003 · Swrngn SA226TC · Cabin Compressor System
Back to Garrett TPE331-10UA