SDR 95ZZZX4611

Service difficulty report · Inverter Harness · Beech E90

Difficulty date
August 25, 1995
Submitted
March 26, 2000
Operation
Air carrier
Aircraft
N1UC
Make and model
Beech E90
Aircraft serial
LW140
Part
Inverter Harness
Condition
Miswired
Location
Ac Bus
Stage of operation
IN
Nature of condition
W
Precautionary procedure
K

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

What was found

DURING AN INSPECTION, A DUAL FEEDER BUS CONFORMITY TEST WAS PERFORMED. THE INVERTER POWER HARNESS WAS FOUND WIRED TO THE WRONG BUSS (LT WIRED TO RT, AND VICE VERSA). SHOULD THE 325-AMP ISOLATION LIMITER BECOME OPEN, BOTH INVERTERS WOULD FAIL. THIS IS SECOND MODEL 90 THAT HAS BEEN WIRED IMPROPERLY. A ONE-TIME INSPECTION OF THE INVERTER SYSTEM BY REMOVING ONE 325-AMP LIMITER AT A TIME AND CHECKING INVERTER OPERATION WHICH WOULD SHOW THE MISWIRING PROBLEM IF BOTH INVERTERS FAILED, NR 1 INVERTER SHOULD FAIL ONLY WHEN NR 1 LIMITER IS REMOVED. SIMILAR RESULTS FOR NR 2 LIMITER REMOVAL.

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