Service difficulty report · Steering Unit · Dhav DHC3

Difficulty date
March 21, 2014
Submitted
April 14, 2014
Operation
General aviation
Aircraft
N424K
Make and model
Dhav DHC3
Aircraft serial
338
Aircraft time
14,131 hours, 1 cycles
Part
Steering Unit
Part number
R652
Condition
Faulty
Location
Tlg
Part time
2,141 hours, 1 cycles
Stage of operation
TX
How discovered
O
Nature of condition
S
Precautionary procedure
D

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

THE ACFT IS EQUIPPED WITH AN ELEC TAIL WHEEL STEERING UNIT, THAT IS CONTROLLED BY THE PILOT BY THE USE OF A TOGGLE SWITCH. THE OFF ACTIVATION OF THE TAIL WHEEL STEERING SWITCH CAUSED THE INSTALLED AUTOPILOT YAW DAMPENER TO TURN ON UN-COMMANDED. THE ACFT WIRING SCHEMATIC SHOWS THAT THE TAIL WHEEL STEERING UNIT CONTAINS A COIL TYPE CLUTCH THAT IS ACTIVATED WHEN THE PILOT SELECTS STEER OR LOCK, THE ELEC FIELD OF THIS CLUTCH COIL COLLAPSES WHEN THE TAIL WHEEL STEERING SWITCH IS SELECTED TO THE OFF POSITION, THIS IS NORMAL, HOWEVER, THIS COIL SHOULD BE PROTECTED WITH THE USE OF A DIODE TO BLOCK THE BACK FEED THAT CAN EFFECT SENSITIVE EQUIP. MOST COILS IN THE AVIATION INDUSTRY ARE PROTECTED WITH DIODES.