Pratt & Whitney Canada PW207D

Service difficulty reports · 133

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 = 'PW207D'
  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 AC2A119527Engine · making metalMAKING METAL, (2) CHIP LIGHTS IN 80 HOURS.Apr 15, 2008 · N427GT · Bell 427 · Engine (Turbine/Turboprop)SDR AC2A118969Skin · chafedAIRCRAFT WAS BROUGHT IN FROM OFFSHORE. DURING A DAILY INSPECTION SOME WORKING AND MISSING RIVETS WERE FOUND ON THE TAIL BOOM. A THROUGH INSPECTION WAS PERFORMED ON THE TAIL BOOM ATTACHMENT FITTING. TAIL ROTOR DRIVE TRAIN, TAIL ROTOR GEAR BOX CASTING, TAIL ROTFeb 23, 2008 · N427CU · Bell 427 · Rotorcraft Tail BoomSDR AC2A119028Support Fitting · damagedDURING A DAILY INSP SOME WORKING RIVETS WERE FOUND ALONG WITH SHEARED RIVET HEADS AT THE TAILBOOM WHERE THE TAIL ROTOR GEARBOX SUPPORT FITTING ATTACHES.Feb 23, 2008 · N427CU · Bell 427 · Rotorcraft Tail BoomSDR AC2A117357Starter Gen · failedSTARTER GENERATOR WOULD NOT ENGAGE. WENT OFFSHORE TO REPLACE STARTER. ONCE OFFSHORE, ENGAGED STARTER SWITCH 3 TIMES AND THE STARTER WORKED AS ADVERTISED. ELECTED TO REPLACE THE STARTER TO PREVENT ANY FURTHER DELAYS AND THE STARTER RAN ONLY 62.5 HOURS, REMAISep 15, 2007 · N427CK · Bell 427 · Starter-GeneratorSDR AC2A117321Transmission · making metalTRANSMISSION CHIP LIGHT ILLUMINATED. 1 VERY SMALL FLAKE AND 1 SMALL HAIR SLIVER ON LT TRANSMISSION CHIP DETECTOR. CHECKED AND CLEANED PLUG, ALSO CHECKED THE OTHER (2) CHIP DETECTORS AND FOUND TO BE CLEAN. PENALTY RAN AIRCRAFT FOR 1 HOUR WITH NO FURTHER CHIP LISep 10, 2007 · N427GT · Bell 427 · Main Rotor GearboxSDR AC2A115466Skid Shoe · severedMOUNTING EARS ARE RIPPED OUT.May 14, 2007 · N427CK · Bell 427 · Main Landing GearSDR AC2A115478Fan · damagedFAN BLADES DISENGAGED FROM THE FAN DRIVE AND DAMAGED THE HUB AND BLADES.May 14, 2007 · N427CK · Bell 427 · Air Distribution FanSDR AC2A115477Motor · damagedFAN DISENGAGED FROM FAN MOTOR AND DAMAGED THE FAN HUB.Apr 15, 2007 · N427CK · Bell 427 · Air Distribution FanSDR AC2A113940Transmission · making metalTRANSMISSION CHIP LIGHT. CALLED MECHANIC OUT TO AIRCRAFT TO CHECK AND VERIFY TRANSMISSION CHIP PLUG CONTAMINATION. MECHANIC FOUND THIN HAIRLIKE SLIVER OF METAL APPROX. .2500 INCH LONG ACROSS CONTACTS OF PLUG. CLEANED OF CHIP DETECTOR AND REINSTALLED. NO FURTHJan 27, 2007 · N427CU · Bell 427 · Main Rotor GearboxSDR AC2A113661Bolt · shearedEND OF BOLT SHEARED OFF WITH NUT.Jan 17, 2007 · N427CU · Bell 427 · Horizontal Stabilizer StructureSDR CA070209008Engine · overspeed(CAN) THE ENGINE WENT TO AN OVERSPEED CONDITION ON TAKE-OFF AND THE TAKE-OFF WAS ABORTED. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20070209008)Jan 11, 2007 · Bell 427 · Engine (Turbine/Turboprop)SDR AC2A111917Bearing · delaminatedBEARING FOUND DELAMINATED, REPLACED BEARING.Nov 5, 2006 · N427CK · Bell 427 · Main Rotor HeadSDR AC2A111918Bearing · delaminatedBEARING FOUND DELAMINATED, REPLACED BEARING.Nov 5, 2006 · N427CK · Bell 427 · Main Rotor HeadSDR AC2A111915Mast · wornDURING MAST RETORQUE, FOUND MAST SPLINES WORN, REPLACED MAST.Nov 5, 2006 · N427CK · Bell 427 · Main Rotor Mast/SwashplateSDR CA060403002Wire Strike · damagedDURING COOL DOWN AT IDLE RPM CYCLIC CONTROL STICK WAS MOVED FORWARD AND MAIN ROTOR BLADE (QTY 2) CONTACTED THE UPPER CUTTER OF THE WIRE STIKE PROTECTION SYSTEM.Mar 30, 2006 · Bell 427 · Main Rotor BladesSDR AC2A108152Relay · inoperativeBATTERY RELAY NOT WORKING / RELACED BATTERY RELAY.Feb 22, 2006 · N427CU · Bell 427 · Electrical Power System WiringSDR AC2A108368Puck · chippedDURING AN INSPECTION THEY FOUND THE ROTOR BRAKE PUCK CHIPPED/ THE CALIPER WAS REPLACED.Feb 12, 2006 · N427GT · Bell 427 · Main Rotor BrakeSDR AC2A108029Control Rod · damagedDURING A 1200HR INSPECTION IT WAS DISCOVERED THAT THE LONG TAIL ROTOR CONTROL TUBE WAS MISSING A NYLATRON SLEEVE. / BELL SENT A REPLACEMENT.Feb 10, 2006 · N427GT · Bell 427 · Tail Rotor Control SystemSDR AC2A105018Pressure Switch · malfunctionedNR 2 FUEL FILTER LIGHT CAME ON/ REPLACED THE TRIPLE SWITCH.Jul 31, 2005 · N427CK · Bell 427 · Fuel Pressure IndicatingSDR AC2A105034Pressure Switch · malfunctionedIMPENDING BYPASS LIGHT CAME ON IN FLIGHT / REPLACED SWITCH.Jul 12, 2005 · N427GT · Bell 427 · Fuel Pressure IndicatingSDR AC2A100978Intake Duct · tornNR 2 ENGINE STARTER/GENERATOR INTAKE DUCT FOUND TORN AT SCAT TUBE. DURING A 300 HR INSPECTION/REPLACED DUCT.May 20, 2005 · N427GT · Bell 427 · Starter-GeneratorSDR CA050524005Blade · damaged(CAN) 427 TAIL ROTOR BLADE SKIN SEPARATION. AFT OF LEADING EDGE NEAR THE TIP OF THE BLADE ON APPROX. 2 SQ. IN. OUTBOARD SIDE.May 20, 2005 · Bell 427 · Tail Rotor BladesSDR CA050527025Warning Light · illuminatedDURING CRUISE, THE ENGINE FUEL PRESSURE WARNING ANNUNCIATED FOLLOWED BY AN ENGINE FAIL WARNING ANNUNCIATION. THE FLIGHT CONTINUED ON OEI RATING. PWC WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE, ONCE ESTABLISHED.May 11, 2005 · Bell 427 · Engine Fuel Indicating SystemSDR CA050516004Warning Light · illuminated(CAN) AT 2500 FEET ASL DURING A 120 KNOTS CRUISE FLIGHT AT APPROXIMATELY 70 PERCENT TOTAL TORQUE, THE ENG FUEL PRESS WARNING LIGHT ILLUMINATED. APPROXIMATELY 10 SECONDS LATER THE ENG FAIL WARNING LIGHT ILLUMINATED. FLIGHT WAS CONTINUED OEI WITH A RUN ON LANDIMay 11, 2005 · Bell 427 · Engine Fuel DistributionSDR CA050401004Display · inoperative(CAN) DURING FLIGHT, TESTSCREEN NR1 (TOP SCREEN) OF IIDS DISPLAY UNIT WAS LOST. THE PILOT SELECTED BOTTOMED DISPLAY TO COMPOSITE MODE. WITHIN SECONDS , SMOKE STARTED TO APPEAR FROM UNDER BOTTOM OF IIDS DISPLAY UNIT. NO BREAKER POPOUT. PILOT STARTED EMERGENCYMar 31, 2005 · Bell 427 · Flight Management Computing Hardware SystemSDR CA050215005Blade · contaminated(CAN) AFTER AIRCRAFT RECONFIGURATION AT OUR FACILITY, NORMALLY INSTALLED THE RADS EQUIPMENT FOR VIBRATION ANALYSIS ON THE T/R SYSTEM. NOTICED A SLIGHTLY HIGH VIBRATION LEVEL WHICH WERE UNABLE TO BRING TO A STANDARD LEVEL. AFTER INVESTIGATION, FOUND OUT THAT Feb 12, 2005 · Bell 427 · Tail Rotor BladesSDR CA040128001Bearing Race · mismanufactured(CAN) IT WAS BROUGHT TO OUR ATTENTION THAT A BEARING WAS DELIVERED TO A CUSTOMER AND FOUND WITHOUT THE REQUIRED 4 (.062 DIA.) LUBE HOLES. THE 4 LUBE HOLES TO BE LOCATED IN THE LUBRICATION GROOVES.Jan 28, 2004 · Bell 427 · Tail Rotor Drive ShaftSDR CA031105005Support · cracked(CAN) FOREIGN OPERATOR NOTICED, DURING WALK AROUND, A ROUTINE MAINTENANCE CRACK ON THE TAIL ROTOR GEAR BOX/VERTICAL FIN SUPPORT ASSEMBLY. PART HAD 310 HOURS SINCE NEW. PART HAS BEEN REMOVED AND SENT FOR INVESTIGATION.Sep 22, 2003 · Bell 427 · Tail Rotor GearboxSDR VTZA02239408Connector · dirtyDURING CRUISE FROM BGR TO BOS CREW RECEIVED RT ENGINE N2 VIBRATION AND ENGINE MISCOMPARE EICAS MESSAGES. FLIGHT CREW FOLLOWED QRH PROCEDURES AND RETURNED TO POINT OF DEPARTURE. AIRCRAFT LANDED IN BGR WITHOUT ANY FURTHER INCIDENT. MAINTENANCE PERSONNEL CLEANAug 27, 2002 · N408FJ · Dorner DO328300 · Engine Vibration AnalyzerSDR CA020610008Case · damaged(CAN) DURING AN OVERHAUL ON MODEL 407 GEARBOX ASSEMBLY, WHICH AS THE SAME DETAIL CASE ASSEMBLY PART NUMBER AS THE MODEL 427,IT WAS FOUND THAT AN OIL PASSAGE WAS MISSING IN THE GEARBOX HOUSING BEARING BORE OF THE INPUT SHAFT DUPLEX BEARING. AFTER INVESTIGATION,Jun 10, 2002 · Bell 427 · Tail Rotor GearboxSDR CA020213010B-Nut · leaking(CAN) SMALL AMOUNT OF FUEL OBSERVED LEAKING FROM RT FLOOR CAVITY DRAIN. CAVITY WAS OPENED, FUEL TRANSFER LINE INSPECTED. LEAK ORIGINATED FROM AFT 'B' NUT FITTING. TORQUE WAS CHECKED ON 'B' NUT, WITHIN SPECS. AIRCRAFT DRAINED OF FUEL, LINE REMOVED AND INSPECTFeb 4, 2002 · Bell 427 · Engine Fuel DistributionSDR CA020213012Line · chafed(CAN) DURING MODIFICATION OF AIRCRAFT, NR 2 ENGINE OIL LINES WERE REMOVED. UPON REMOVAL OF LINES IT WAS OBSERVED THAT THE MAIN OIL FEED LINE (FROM OIL COOLER) WAS CHAFED TO A DEPTH OF 0.004 INCH. THE CHAFING OCCURRED IN THE AREA BELOW THE FORWARD ENGINE FIREJan 25, 2002 · Bell 427 · Engine Oil Distribution (Airframe Furnished)SDR B1H2001F00000Blade · debondedDURING A 50 HOUR INSPECTION THE CONDITION WAS FOUND. THE OUTER COMPOSITE LAYERS HAD DEBONDED FROM THE ROOT OF THE BLADE AND VOIDS WERE PRESENT. THE PROBLEM IS THE BLADE WILL HAVE TO BE SPREAD TO GET THE PITCH HORN IN AND THIS MAY BE THE CAUSE OF THE DEBONDINJun 28, 2001 · N427FW · Bell 427 · Main Rotor Blades
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