60Duke

Parts most often named Gear (2) · Coil (1)

PILOT REPORTED ROUGH RUNNING ENGINE. REMOVED FUEL CONTROL, FLOW CHECKED. FOUND BAD RIGHT MAGNETO. TEETH STRIPPED FROM DISTRIBUTOR GEAR.

PILOT REPORTED ROUGH RUNNING ENGINE. REMOVED FUEL CONTROL FLOW, CHECKED. FOUND BAD RIGHT MAGNETO. TEETH STRIPPED FROM DISTRIBUTER GEAR.

(AUS) RH ENGINE LH MAGNETO 'CLEAR CASE' COIL DETERIORATED AND CASE SEVERLY CRACKED - FOUND DURING INSPECTION IAW AD/ELECT/66 AMDT 1 - AIRCRAFT WAS PREVIOUSLY REGISTERED AS VH-EZT

Parts most often named Transmitter (1) · Indicator (1) · O-Ring (1)

ACFT EXPERIENCED AN IN-FLIGHT FIRE IN THE LT ENG NACELLE DUE TO A LEAKING LT FUEL FLOW TRANSMITTER. THE TRANSMITTER HAD A BRITTLE/CRACKED O-RING SEAL. THE TRANSMITTER WAS LAST O/H IN 1998. THE RT ENG FUEL FLOW TRANSMITTER HAD BEEN OVERHAULED AT THE SAME TIME AND WAS FOUND TO BE LEAKING ALSO.

INSTALLED SHADIN FUEL FLOW INDICATOR SYSTEM. PROCESSOR LOCKED UP AND WOULD NOT FUNCTION ON SECOND TEST. RETURNED TO FACTORY FOR [S/N removed]. (X)

Parts most often named Fuel Cell (2)

FUEL CELL BEGAN LEAKING IN MARCH, 1994; WAS REMOVED AND SENT TO A/C FUEL CELLS WORLDWIDE, INC., FOR REPAIR. A/C CONDEMNED CELL AND REBUILT CELL WAS PURCHASED FOR REPLACEMENT (WORK ORDER NR 9938, INSPECTED 4-18-94) IN APRIL, 1994. JUNE, 1997, REPLACEMENT CELL REMOVED FOR LEAKS AND RETURNED TO A/C FUEL CELLS FOR WARRANTY REPAIR. WARRANTY REPAIR REFUSED, A/C CONDEMNED REPLACEMENT CELL. AIRCRAFT FUEL SYSTEM KEPT FULL AT ALL TIMES. REASON FOR DETERIORATION NOT KNOWN.

Parts most often named Pipe (1) · Wye Assy (1)

AN INTENSE IN-FLIGHT FIRE OCCURRED WHEN A CRACK IN THE LEFT ENGINE WYE EXHAUST ASSY DEVELOPED AND ALLOWED HOT EXHAUST GAS TO LEAK THROUGH LOOSE COUPLING INTO ACCESSORY SECTION. THE CRACK IN THE WYE ASSY COULD NOT BE DETECTED UNTIL AIR PRESSURE WAS FORCED INTO EXHAUST SYSTEM BY BLOCKING OFF PORTS. SUBMITTER SUGGESTS THIS PROCEDURE BE ACCOMPLISHED AT LEAST ON ANNUAL INSPECTIONS.

Parts most often named Hub (2)

(CAN) PROPELLER WAS RECEIVED FOR O/H DUE TO A FOREIGN OBJECT STRIKE. WHEN THE PAINT WAS REMOVED FROM THE HUB CORROSION IN THE BLADE SEAL GROOVES WAS NOTED. AFTER CONSULTING THE MFG O/H MANUAL IT WAS FOUND THAT THE HUB IS NOT REPAIRABLE AND MUST BE REMOVED FROM [S/N removed].

Parts most often named Elt (2)

(CAN) WHEN TESTING THE ELT AT ITS ANNUAL INSP THE ELT HAD NO MODULATION AND NO OUTPUT POWER. THE ELT REPLACED WITH A [S/N removed] UNIT. (TC NR 20080208002)

ALKALINE BATTERY PACK LEAKED AND CORRODED ELT MONITOR. REPLACED ELT WITH NEW ELT NOT REQUIRING A LITHIUM BATTERY PACK. (X)

Parts most often named Push-Pull Rod (1) · Motor (1)

PILOT REPORTED A FAULTY NOSE GEAR INDICATION FOR DOWN AND LOCKED. NOSE GEAR PUSH PULL ROD FAILED JUST FORWARD OF THE AFT END ATTACH POINT. STEEL DRIVE TUBE HAD INDICATIONS OF A CRACK THAT HAD PROGRESSED TO THE POINT OF FAILURE. NOSE GEAR COLLAPSED ON TOUCHDOWN.

LANDING GEAR FAILED TO EXTEND. ACFT LANDED GEAR UP. FOUND ELECTRIC MOTOR SEIZED. COULD NOT EXTEND LANDING GEAR MANUALLY.

Parts most often named Bracket (2)

DURING A 2400-HOUR INSPECTION, THE NOSE ROLLER OUTBOARD FORWARD HINGE BRACKET WAS FOUND CRACKED ON LT AND RT FLAPS. REPLACED BRACKET WITH NEW.

Parts most often named Control Unit (1) · Electrical Sys (1)

LEFT STARTER WOULD NOT ROTATE WHEN START WAS SELECTED. REPLACED GENERATOR CONTROL UNIT. SYSTEM WAS RESTORED TO NORMAL.

Parts most often named Lifter (2)

UPON REMOVAL OF PUSH RODS AND PUSH ROD TUBES FOR RESEAL, THE LIFTERS WERE REMOVED FOR BLEEDING. THE LIFTERS WERE INSPECTED AND WERE FOUND TO HAVE SEVERE SPALLING. MFG WAS NOTIFIED AND ENGINES ARE TO BE REMOVED AND SENT BACK FOR REPAIR. ENGINES HAVE 132.4 HRS TT. CAMSHAFT IS ALSO WORN.

UPON REMOVAL OF PUSH RODS AND PUSH ROD TUBES FOR RESEAL. THE LIFTERS WERE REMOVED FOR BLEEDING. THE LIFTERS WERE INSPECTED AND WERE FOUND TO HAVE SEVERE SPALLING. MFG WAS NOTIFIED AND ENGINES ARE TO BE REMOVED AND SENT BACK FOR REPAIR. ENGINES HAVE 132.4 HOURS TT. CAMSHAFT IS ALSO WORN.