Service difficulty report · Sensor · Beech 400A

Difficulty date
September 19, 2010
Submitted
September 20, 2010
Operation
Air carrier
Aircraft
N151QS
Make and model
Beech 400A
Aircraft serial
RK422
Aircraft time
2,226 hours, 2,123 cycles
Part
Sensor
Condition
Faulted
Location
Stab Anti Ice
Stage of operation
CR
How discovered
O
Nature of condition
N
Precautionary procedure
A

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

What was found

THE "H STAB FAIL" LIGHT CAME ON WHEN THE HORIZONTAL STAB ANTI ICE WAS TURNED ON. DID THE APPROPRIATE CHECKLIST WHICH INCLUDED PULLING THE HORIZONTAL STAB PROTECT CIRCUIT BREAKER. ISOLATED FAULT AT SENSOR NR 1 AND THERMALLY MATCHED MATE AND SPLICED IV SPARE THERMALLY MATCHED SET IAW MM 30-12-00-201; 20-00-00-201, AND WDM 30-12-03-01. OPS CHECKS NORM. NO DISCREPANCY NOTED.

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