Service difficulty report · Flap System · Beech 400A

Difficulty date
January 2, 2012
Submitted
January 5, 2012
Operation
General aviation
Filed by
E81R759X
Chronos Aviation, LLC.
Aircraft
N462LX
Make and model
Beech 400A
Aircraft serial
RK423
Aircraft time
4,473 hours, 3,814 cycles
Part
Flap System
Condition
Malfunctioned
Stage of operation
NR
How discovered
9
Nature of condition
J
Precautionary procedure
O

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

What was found

INVESTIGATED FLAP SYS ASSYMETRY WARNING ANNUNCIATOR LIGHT INDICATION. FOUND RT FLAP FOLLOW-UP SWITCH ACTUATING ARM .075 IN. LONGER THAN LT FOLLOW-UP SWITCH ACTUATING ARM. ADJUSTED RT FOLLOW-UP SWITCH ACTUATING ARM TO MATCH LT FOLLOW-UP SWITCH ACTUATING SWITCH ARM LENGTH. ADJUSTED LT AND RT FLAP POSITION TRANSMITTER VOLTAGES AND LT AND RT FLAP FOLLOW-UP SWITCH VOLTAGES AS REQUIRED TO BRING WITHIN MM 27-50-00 SERVICE LIMITS. VERIFIED FLAP SYS FOLLOW-UP SWITCH CLEARANCES AND FLAP SYS RIGGING WITHIN THE MM 27-50-00 SERVICE LIMITS. FLAP SYS FUNCTIONAL CHECKS SATISFACTORY, NO FAULTS INDICATED. PAST MX HISTORY ON FLAP SYS COMPONENTS UNKNOWN.

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