Turbomeca ARRIEL-2B1

Service difficulty reports · 757

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 = 'ARRIEL2B1'
  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 CA190903013Mast · corroded(CAN) DURING 24 MONTH 600 HOUR INSPECTION ENGINEER WAS PLACING TAPE ON UPPER FLANGE TO KEEP DUST ETC FROM GOING INSIDE MAST UPON REMOVING TAPE SOME PRIMER PAINT FROM INSIDE THE MAST CAME OFF SHOWING CORROSION. THE MAST WAS SENT TO THE MANUFACTURER AS THERE WERApr 23, 2019 · Snias AS350B3 · Main Rotor Mast/SwashplateSDR QMLA2019042629042Unknown · odor15 MINS INTO FLIGHT, CREW NOTIFIED THEY SMELLED BURNING ELECTRICAL IN THE CABIN, LANDED WITH NO OTHER ISSUES. MECHANIC AND PILOT RAN UP AIRCRAFT CHECKED SYSTEMS AND COULD NOT DUPLICATE. AIRCRAFT WAS VISUALLY CHECKED AND NO DISCREPANCIES WE NOTED.Apr 22, 2019 · N253LF · Snias AS350B3 · Air Distribution SystemSDR QMLA201904221940Circuit Breaker · faultyDURING THE PATIENT LEG OF AN INTER-FACILITY TRANSFER, BEGAN TO NOTICE THE STRONG ODOR OF WHAT WAS SUSPECTED TO BE HOT WIRES. INVESTIGATED THE POSSIBLE CAUSES BY SHUTTING DOWN INDIVIDUAL PIECES OF EQUIPMENT ONE AT A TIME. NONE SEEMED TO MAKE A DIFFERENCE. THEApr 20, 2019 · N353AM · Urocop EC130B4 · Light System WiringSDR QMLA2019040299033Bevel Gear · corrodedWHILE PERFORMING 600HR INSPECTION THE TRANSMISSION WAS PULLED OFF THE AIRCRAFT TO PERFORM AIRBUS ASB AS350-62.00.42 REV.0 DATED 17-SEPT-2018(AIRMETHODS E) 00-6200-EO-2626)THE MAST INSPECTION WAS PERFORMED AND THE MECHANIC NOTICED CORROSION AND PITTING ON THE Mar 29, 2019 · N805LF · Snias AS350B3 · Main Rotor GearboxSDR 2019FA0000097Wire Harness · brokenAIRCRAFT STAYED AT FLIGHT IDLE EVEN AFTER THROTTLE TWIST GRIP WAS ROLLED TO THE IDLE POSITION. FOUND BROKEN WIRES FROM CONNECTIONS AT THE 53KA, 53KB AND 65K MICRO SWITCHES LOCATED UNDER CO-PILOT FLOOR.Mar 23, 2019 · N3972A · Snias AS350B3 · Engine Control System WiringSDR QMLA2019022619022Heater · odorAPPROXIMATELY 3 MINUTES AFTER TAKEOFF FROM OUR HOSPITAL FOR A NICU TEAM FLIGHT; BOTH CREW-MEMBERS SAID THEY SMELLED FUEL. THE AIRPORT WAS RIGHT IN FRONT OF ME SO I INITIATED A LANDED TO THE KSPI BRAVO RAMP IN COORDINATION WITH TOWER. DURING MY DESENT, I REMEMBFeb 26, 2019 · N245AM · Urocop EC130B4 · Heating SystemSDR CA190308012Bearing · cracked(CAN) DURING 600 HR INSP. IT WAS DISCOVERED THAT THE REAR FACING TAIL ROTOR LAMINATE HALF BEARING WERE WORN BEYOND LIMITS. (TC# 20190308012)Feb 26, 2019 · Snias AS350B3 · Tail Rotor BladesSDR CA190220027Limit Switch · leaking(CAN) REPLACEMENT SERVO FOR SDR 20190220025 LEAKED AFTER 0.2 TEST FLIGHT. LIMIT SWITCH LEAKING HYDRAULIC FLUID AND ALSO LIMIT SWITCH LIGHT ILLUMINATION DIM ON 4 ALPHA PANEL IN COCKPIT. SUSPECT COLD OUTSIDE AIR TEMPERATURES - 35 C AS CAUSE OF PROBLEM. (TC# 2019Feb 10, 2019 · Snias AS350B3 · Rotorcraft Servo SystemSDR CA190220025Limit Switch · leaking(CAN) REPLACEMENT SERVO FOR SDR REPORT 20190207017 LEAKED AFTER 1.5 HOURS OF FLIGHT. LIMIT SWITCH LEAKING HYDRAULIC FLUID. SUSPECT OPERATIONS IN COLD OUTSIDE AIR (- 35 C) TEMPERATURES CAUSING PROBLEM. (TC# 20190220025)Feb 9, 2019 · Snias AS350B3 · Rotorcraft Servo SystemSDR QMLA2019012319011Gas Generator · abnormalPILOT REPORTED LOSS OF FLI INDICATION ON APPROACH TO THE BASE. AFTER LANDING AND ROLLING THE THROTTLE TO IDLE, A FLASHING AMBER GOV LIGHT WAS ILLUMINATED. UPON INSPECTION OF THE T4 HARNESS , I FOUND THE T4 HARNESS WAS DAMAGED. AFTER GETTING A VIDEO SCOPE TOJan 23, 2019 · N137HN · Urocop EC130B4 · Turbine Engine Combustion SectionSDR QMLA2019012319012Frame · crackedFOUND CRACK IN RT CORNER OF PICK-UP WEB OF CANOPY FRAME. THE CRACK IS APPROXIMATELY 57 MM IN LENGTH. THIS WAS FOUND DURING THE A 0740.5 INSPECTION.Jan 23, 2019 · N139HN · Urocop EC130B4 · Fuselage Main, StructureSDR QMLA2019011519007Intake · crackedWHILE CLEANING THE ENGINE AREA (COWLING OFF DUE TO OTHER MAINT) I FOUND A CRACK ALONG A WELD ON THE LT SIDE OF THE ENGINE INTAKE.Jan 15, 2019 · N151AC · Urocop EC130B4 · Engine Air Intake SystemSDR QMLA2018121748135Data Card · unserviceableQVERLIMIT DETECTED MESSAGE ILLUMINATED IN VEMD MESSAGE ILLUMINATED IN THE VEMD MESSAGE WINDOW. THERE WERE NOT SECONDARY INDICATIONS ON THE GAUGES. ACFT WAS FLYING STRAIGHT AND LEVEL AT 4500 FEET AND 8.75 ON FLI. FLEW TO NEAREST AIRPORT AND LANDED WITHOUT INCIDDec 14, 2018 · N139HN · Urocop EC130B4 · Electrical Power System WiringSDR QMLA2018120768129Bladder · collapsedINITIALLY REPLACEING THE FUEL QUANTITY INDICATOR PROBE AFTER FAILING CALIBRATION CHECK. AFTER REMOVAL OF PLUMBING MODULE ASSY (WHICH CONTAINS THE FUEL PUMP, FQI PROBE, AND FLOAT SWITCH), LOOKED INSIDE TANK. FOUND BLADDER HAD COLLAPSED ABOUT MIDWAY FORWARD ON TDec 6, 2018 · N134LN · Urocop EC130B4 · Fuel StorageSDR QMLA2018101518112Floor Panel · crackedTHE MECHANIC REMOVED THE AUXILIARY SEATING FLOOR OVERLAY PANEL AS PER AMC AAIP C1040 AND DISCOVERED TWO CRACKS ON THE AFT CABIN FLOOR PANEL. THE CRACKS STARTED AT THE LEADING EDGE OF THE FLOOR PANEL AND RADIATED AFT. THE DAMAGE IS AT STA 70" AND RIGHT BL 4.5".Oct 15, 2018 · N133LN · Urocop EC130B4 · Fuselage Floor PanelSDR QMLA2018100818109Blower · odorWHILE ON APPROACH TO HOSPITAL LANDING PAD, THE GENERATOR DISENGAGED. IT WAS RESET, AND THE SUBSEQUENT APPROACH AND LANDING WERE COMPLETED NORMALLY. THE CREW REPORTED AN ELECTRICAL ODOR AFTER LANDING. UPON INSPECTION, NO PROBLEMS WERE FOUND WITH ELECTRICAL SYSOct 4, 2018 · N209LF · Urocop EC130B4 · Cabin Cooling SystemSDR 2019F00075Rail · corrodedDURING PAINT STRIPPING, MAJOR CORROSION WAS FOUND ON THE RT CABIN THRESHOLD RAIL FROM FS 1436.0 MM TO FS 2230.0 MM.Oct 3, 2018 · N382AM · Urocop EC130B4 · Fuselage Miscellaneous StructureSDR QMLA2018061318070Unknown · odorDURING FLIGHT, THE CREW REPORTED SMELLING JET FUEL COMING FROM AIR CONDITIONING VENTS. PILOT COULD NOT SMELL THE ODOR. RETURNED TO BASE. THE MECHANIC REMOVED THE LEFT SIDE INNER FUEL TANK PANELS AND AFT BELLY PANEL WAS LOWERED TO INSPECT FOR FUEL LEAKAGE, Jun 13, 2018 · N109LN · Snias AS350B3 · Air Distribution SystemSDR QMLA201806011868Unknown · odorTOOK OFF , AFTER APPROXIMATELY 5 MINUTES IN FLIGHT, THE CREW STARTED TO DETECT AN ODOR OF ELECTRICAL BURNING IN THE CABIN. THE PILOT TURNED OFF THE AIR CONDITIONER AND STARTING TO HEAD BACK TO BASE IMMEDIATELY. ALL ELECTRICAL SYSTEMS WERE WITH IN NORMAL LIJun 8, 2018 · N133HN · Urocop EC130B4 · Air Distribution SystemSDR QMLA2018052958063Switch · failedSHORTLY AFTER TAKEOFF DURING CLIMB. SCANNED THE AIRCRAFT INSTRUMENTS AND EVERYTHING WAS IN THE NORMAL OPERATING RANGE. NOTICED THE OIL TEMPERATURE HAD CLIMBED AROUND 7-8 DEGREES PAST THE INITIAL SCAN, STILL WITHIN NORMAL OPERATING LIMITATIONS. THE OIL TEMPMay 25, 2018 · N151AC · Urocop EC130B4 · Engine Oil TemperatureSDR QMLA2018051018056Blower Motor · odorTAKING OFF FROM BASE TO PR EVENT, THE MED CREW BEGAN TO SMELL ELECTRICAL TYPE BURNING SMELL WITH THE CABIN. THE SMELL WAS STRONG FROM THE PILOT SEAT SO I COULD ONLY ASSUME THAT IT WAS POSSIBLY SOMETHING FROM THE COCKPIT AREA. STARTED TO ISOLATE THE PROBLEM BY May 10, 2018 · N133HN · Urocop EC130B4 · Cabin Cooling SystemSDR QMLA2018040518041Bearing · failedDURING DESCENT, AROUND 6500 FEET MSL, RECEIVED AN ENGINE CHIP LIGHT. NOTIFIED APPROACH CONTROL. HEARD A POP FOLLOWED BY A DECREASE ENGINE SOUND, RAPID DESCENT AND LOW ROTOR HORN. LOWERED COLLECTIVE AND CAME MORE AFT CYCLIC AND ENTERED AN AUTO ASSUMING ENGINApr 5, 2018 · N3831 · Snias AS350B3 · Turbine SectionSDR QMLA2018040118037Shelf · crackedDURING INSPECTION, FOUND THE BATTERY SHELF CRACKED AFT OF TB FRAME 2285.8 STARTING AT 4 INCHES AND IS APPROXIMATELY 1.75 INCHES LONG, ANOTHER CRACK 3 INCHES AFT OF THAT, APPX 4.5 INCHES LONG WITH MULTIPLE CRACKS AND MISSING MATERIAL.Apr 1, 2018 · N358AM · Urocop EC130B4 · Rotorcraft Tail BoomSDR 2018F00142Bracket · bentAFTER LANDING, DURING NORMAL SHUTDOWN PROCEDURES, THE PILOT REPORTED A BURNED ELECTRICAL ODOR IN COCKPIT, SHORTLY FOLLOWING CREW REPORTED LIGHT SMOKE COMING FROM THE LEFT SIDE OF THE CENTER CONSOLE CIRCUIT BREAKER AREA. PILOT PROCEEDED TO SHUTDOWN. MAINTENAMar 25, 2018 · N530H · Snias AS350B3 · Fuselage Miscellaneous StructureSDR QMLA2018031718032Frame · crackedDURING A 300 HOUR INSPECTION OF THE HORIZONTAL STABILIZER, FOUND THE UPPER RT ATTACH FITTING BROKEN, AND THE FRAME IN THE TAILBOOM CRACKED.Mar 17, 2018 · N259AM · Urocop EC130B4 · Rotorcraft Tail BoomSDR QMLA2018022818025Bracket · crackedDURING REMOVAL OF THE FUEL TANK SADDLES FOR THE CRASH RESISTANT FUEL TANK INSTALL, INSPECTED THE SADDLES AND FOUND A BRACKET ON THE FWD RIGHT SADDLE WITH A 25MM CRACK. THE CRACK WAS ON A 2 INCH BY 3 INCH BRACKET OF WHICH THE CRACK STARTED AT A RIVET HOLE EXTEFeb 28, 2018 · N808LF · Snias AS350B3 · Fuselage Main, Attach FittingsSDR CA180104004Bearing · cracked(CAN) DURING ROUTINE/DAILY INSPECTIONS OF THE T/R 1/2 SHELL BRGS AT 300-350 HR TSN, WEATHER CHECKING WAS OBSERVED ON THE RUBBER LAMINATE SECTION OF ALL 4 1/2 SHELL BRGS. MONITORING CONTINUED ON THE VISIBLE PORTIONS OF THE BRGS. AND AT ABOUT 400-450 HR TSN SOMDec 21, 2017 · Snias AS350B3 · Tail Rotor BladesSDR UKVR2017071900001Beam · crackedFOUND TRANSMISSION DECK BEAM CRACKED DURING 12 YEAR INSPECTION.Jul 17, 2017 · N854HW · Snias AS350B3 · Fuselage Main, StructureSDR QMLA2017042717045Terminal · brokenTHE PILOT REPORTED AN ELECTRICAL FAILURE WITH LOSS OF GPS1 , TRANSPONDER, AND HSI INDICATION. THE MECHANIC INSPECTED THE AIRCRAFT AND FOUND A BROKEN WIRE THAT FEEDS THE K5 RELAY DIRECT BATTERY CIRCUIT. REPLACED THE BROKEN TERMINAL. SYSTEM OPERATIONAL CHECK GOApr 27, 2017 · N47HN · Urocop EC130B4 · Navigation System WiringSDR 2017FA0000163Unknown · fumesFUEL FUMES IN THE COCKPIT.Apr 17, 2017 · N245AM · Urocop EC130B4 · Air Distribution SystemSDR QMLA2017033114030Switch · defectiveAPPROXIMATELY 2 MINUTES AFTER TAKEOFF FROM BASE, AND 1 MINUTE INTO FORWARD FLIGHT, THE "LOW INLET PRESSURE" LIGHT FLICKERED AT A VERY LOW LIGHT LEVEL AND CONTINUED FLICKERING THROUGH SHUTDOWN, AFTER ABORTING FLIGHT AND RETURNING TO BASEMar 31, 2017 · N341AM · Urocop EC130B4 · Engine Air Intake SystemSDR 2017FA0000317Torque Shaft · shearedTHE STARTER GENERATOR WAS RECEIVED IN AN OVERHAULED CONDITION. IT WAS PLACED INTO SERVICE ON ACFT SN 3872 ON 7/27/2016 WITH 0.0 HRS SINCE THE STARTER GENERATOR HAD BE OVERHAULED. THE ACFT FLEW FOR THE NEXT EIGHT MONTHS AND ON 3/23/2017 THE FLT CREW HAD BEEN Mar 24, 2017 · N186AE · Snias AS350B3 · Starter-GeneratorSDR 2017FA0000117Wire Harness · chafedTO IMMEDIATELY INSPECT AND PREVENT CHAFING AND ARCHING BETWEEN THE INTERCOM FUNCTION PANEL AND THE WIRE BUNDLES TO THE P132 CONSOLE IN THE COCKPIT CENTER CONSOLE. FOUND BUNDLE CHAFING TO THE INTERCOM. REPAIRED AS NECESSARY AND REPOSITION THE WIRE BUNDLES TO PRMar 21, 2017 · N3953A · Snias AS350B3 · Electrical Power System WiringSDR 2017FA0000098Wire Harness · chafedFOUND EVIDENCE OF ARCING BETWEEN THE P132 GENEVA CONSOLE WIRING BUNDLES AND THE INTERCOM FUNCTION PANEL INSTALLED IN THE CENTER CONSOLE. WIRE BUNDLES HAVE BEEN REPOSITIONED IN SUCH A MANNER THAT ARCING/CONTACT WITH THE INTERCOM FUNCTIONS PANEL WILL NO LONGER BMar 13, 2017 · N790AM · Snias AS350B3 · Communications System WiringSDR 2017FA0000100Wire · chafedFOUND EVIDENCE OF CHAFING BETWEEN THE P132 GENEVA CONSOLE WIRING BUNDLES AND THE INTERCOM FUNCTION PANEL INSTALLED IN THE CENTER CONSOLE. WIRE BUNDLES HAVE BEEN REPOSITIONED IN SUCH A MANNER THAT CHAFING/CONTACT WITH THE INTERCOM FUNCTIONS PANEL WILL NO LONGERMar 13, 2017 · N796AM · Snias AS350B3 · Communications System WiringSDR 2017FA0000145Filter · defectiveENGINE INGESTED THE INLET PLENUM AFT D-SEAL CAUSING REDUCED ENGINE POWER, THE ENGINE FAILS POWER CHECK. BORESCOPE INSPECTED REVEALING FOD DAMAGE TO MO2 1ST STAGE WHEEL, RUBBER MATERIAL FOUND IN MO2 AND MO3. INSPECTION OF THE INLET PLENUM REVEALED THE AIR FILTMar 8, 2017 · N359FB · Snias AS350B3 · Engine Air Intake SystemSDR QMLA2016111016125Sleeve · deterioratedCREW REPORTED SMOKE COMING FROM DEMISTER SYSTEM WHEN ACTIVATED. AIRCRAFT RAN UP AND VERIFIED ON GROUND. NO SMOKE COMING FROM HEATER SYSTEM WHICH IS IN PARALLEL TO DEMISTER VALVE. INSPECTED SLEEVE ASSEMBLY FOR DEMISTER AND FOUND HOSES TO BE DETERIORATED. REPLANov 10, 2016 · N358AM · Urocop EC130B4 · Air Distribution SystemSDR QMLA2016110216123Engine · making metalPERFROMED SEVERAL GROUND RUNS ON THE ENGINE WHILE DOING THE TRACK AND BALANCE FOR THE T/R BLADE, SHORT SHAFT AND M/R. AFTER THESE CHECKS WERE DONE WE HAD PROBABLY 8+ GROUND RUNS ON THIS ENGINE. WE WENT TO FLY TO FINISH OUR TRACK AND BALANCE ALONG WITH THE INov 2, 2016 · N544AM · Snias AS350B3 · Engine (Turbine/Turboprop)SDR 2017FA0000385Bushing · wornACFT LANDED ON THE SCENE AS NORMAL. THE MEDICAL CREWS BEGAN TO LOAD THE PATIENT, AS THE PILOT NOTICED ON HIS POST FLIGHT INSPECTION THERE WAS AN AMOUNT OF OIL ON THE ENG DECK. AS PRECAUTIONARY THE PILOT TOLD THE CREW MEMBERS THAT THEY COULD NOT TAKE THE ACFTOct 19, 2016 · N351HW · Snias AS350B3 · Engine (Turbine/Turboprop)SDR M7KA201610111134Pump · leakingDURING ROUTINE INSPECTION, A HYDRAULIC FLUID LEAK WAS NOTED ON THE BELT DRIVEN HYDRAULIC PUMP DRIVE AND A PREVIOUSLY REPAIRED YELLOW TAGGED PUMP ASSEMBLY INSTALLED. THE REPLACEMENT PUMP DRIVE SHAFT LIP SEAL HAD BEEN REPLACED AS PART OF THE REPAIR. A NORMAL GROOct 8, 2016 · N821MH · Urocop EC130B4 · Hydraulic Pump (Electric/Engine), MainSDR 9EKA20160920015Blade · crackedDURING AN INSPECTION, A MECHANIC NOTICED SOME PAINT FLAKING OFF THE TAIL ROTOR BLADE ABOUT MID-SPAN SO HE CLEANED IT UP AND NOTICED WHAT APPEARED TO BE A CRACK ON CLOSER INSPECTION IT WAS FOUND TO BE AN ACTUAL CRACK. CRACK LENGTH - 1.5", CRACK DISTANCE FROM Sep 20, 2016 · N359EV · Snias AS350B3 · Tail Rotor BladesSDR 2017FA0000426Blower Motor · seizedENROUTE TO SCENE FLIGHT, MED CREW BEGAN TO SMELL NOXIOUS FUMES IN CABIN. PILOT BEGAN SHEDDING ELECTRIC COMPONENTS DURING MAKING A PRECAUTIONARY LANDING. PRIOR TO LANDING PILOT MADE CONTACT WITH TOWER TO REPORT LOCATION OF LANDING. PILOT CALLED MX TO SCENE AAug 31, 2016 · N351HW · Snias AS350B3 · Cabin Cooling SystemSDR QMLA2016082916100Unknown · odorFUEL FUMES IN COCKPIT NOTED ABOUT A MINUTE AFTER TAKEOFF, FOLLOWING A NORMAL START. ODOR BEGAN TO DISSIPATE ON APPROACH TO LANDING. AREA MECHANIC WAS CALLED, AND UPON ARRIVAL, LOWER BELLY PANELS WERE REMOVED, FUEL SYSTEM WAS INSPECTED, AND ENGINE WAS INSPECTAug 29, 2016 · N577LF · Urocop EC130B4 · Air Distribution SystemSDR O4VA201608250001Radio · failedDURING FLIGHT RADIO FM 1 EMITTED SMOKE. THE FRONT PASSENGER WAS TRANSMITTING ON FM 1 WHEN THE PILOT HEARD EXCESSIVE STATIC THROUGH THE RADIO. THE PILOT NOTICED THE DISPLAY SCREEN OF THE RADIO FLASHING, THEN COMPLETELY DIMMING. THE PILOT TURNED THE RADIO OFF Aug 25, 2016 · N359TA · Snias AS350B3 · VHF Communications SystemSDR QMLA2016081816094Air Duct · unsecureREPOSITIONING FLIGHT. UTILIZED AIRCRAFT DEMIST DUE TO LIGHT RAIN. SCANNED THE LANDING AREA AND NOTICED SMOKE BUILDING IN THE AFT RIGHT SECTION OF THE CABIN. PERFORMED AN EMERGENCY SHUTDOWN AFTER LANDING AND EXITED IMMEDIATELY. NO EVIDENCE OF FIRE. LEADERSAug 18, 2016 · N306LF · Urocop EC130B4 · Air Distribution SystemSDR QMLA2016080916091Exhaust Pipe · crackedENGINE EXHAUST PIPE HAS 2.5" CRACK RUNNING LATERALLY AROUND FORWARD WELD AT THE 1 TO 3 O'CLOCK POSITION.Aug 9, 2016 · N336AM · Urocop EC130B4 · Engine Collector/Tailpipe/NozzleSDR QMLA2016072016081Gearbox · damagedUPON REMOVING THE ENGINE TO MAIN GEARBOX SHAFT TO REPLACE THE MAIN GEARBOX INPUT SEAL. I FOUND THAT THE CASTLATED NUT THAT HOLDS THE ROTOR BRAKE DISK IN PLACE WAS LOOSE. REMOVED NUT, WASHER (SIGNS OF SPINNING IN PLACE) BRAKE DISK, LARGE FLAT WASHER UNDER DISK Jul 20, 2016 · N508AM · Snias AS350B3 · Main Rotor GearboxSDR QMLA2016071316078Clutch · failedSHORTLY AFTER TAKE-OFF, CREW SMELLED AN ODOR IN THE AIRCRAFT. SUSPECTED THE AIR CONDITIONING SYSTEM SINCE THE SAME HAD HAPPENED EARLIER IN THE DAY AFTER WHICH THE PROBLEM WAS CLEARED BY MAINTENANCE. TURNED OFF THE SYSTEM AND RETURNED TO BASE. DISCOVERED AIR CJul 13, 2016 · N913SM · Snias AS350B3 · Cabin Compressor SystemSDR QMLA2016071016073Bearing · corrodedWHILE TAKING OFF, THE RIGHT PEDAL BECAME INCREASINGLY HARDER TO MOVE AS POWER WAS APPLIED. AFTER LIFTING, ABORTED TAKEOFF. EXECUTED A NORMAL LEFT AND RIGHT PEDAL TURN, MEDIC STATED HE SMELLED SMOKE. RIGHT PEDAL FELT LIKE IT WAS BINDING WHEN APPLIED DURING PJul 10, 2016 · N137HN · Urocop EC130B4 · Rotorcraft Flight ControlSDR QMLA2016061316063Unknown · odorIN CRUISE FLIGHT, ABOUT A MINUTE BEFORE LANDING BACK AT AIRPORT, THE PILOT NOTED A FUEL ODOR IN THE CABIN. LANDED AT THE AIRPORT NORMALLY WITH NO ISSUES OTHER THAN THE FUEL ODOR. REMOVED THE BELLY PANEL UNDER THE FUEL TANK AND DID NOT SEE AND EVIDENSE OF FUELJun 13, 2016 · N132LN · Urocop EC130B4 · Air Distribution System
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