Service difficulty report · Transmitter · Beech 400A

Difficulty date
October 10, 2005
Submitted
October 26, 2005
Operation
General aviation
Aircraft
N419CW
Make and model
Beech 400A
Aircraft serial
RK19
Aircraft time
8,514 hours, 8,633 cycles
Engine
Pwa JT15D1
Part
Transmitter
Condition
Out Of Adjust
Location
Te Flaps
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

FLAP ASYMMETRY ANNUNCIATOR ILLUMINATED DURING APPROACH. FOUND MIDBOARD ASYMMETRY DETECTOR READING 5.7 VOLTS. FOUND IB ASYMMETRY DETECTOR READING 7.8 VOLTS. ADJUSTED LT AND RT FLAP POSITION TRANSMITTERS AS REQUIRED IAW MM TO BRING VOLTAGES TO 5.8 VOLTS +/- 0.2 VOLTS. FLAP SYSTEM FUNCTIONAL CHECKS SATISFACTORY, NO ASYMMETRY FAULTS INDICATED AFTER 20 CYCLES. (K)

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