Service difficulty report · Fuse · Beech C90

Difficulty date
October 10, 2008
Submitted
November 18, 2008
Operation
Air carrier
Aircraft
N767MC
Make and model
Beech C90
Aircraft serial
LJ595
Aircraft time
67,793 hours, 56,939 cycles
Engine
Pwa JT8D17A
Engine time
39,260 hours, 25,780 cycles
Part
Fuse
Condition
Failed
Location
Hyd Pump
Stage of operation
TX
How discovered
O
Nature of condition
K, J
Precautionary procedure
H

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

What was found

AFTER THE ACFT WAS PUSHED BACK FOR DEPARTURE AND FOLLOWING ENGINE START, THE RT HYDRAULIC SYSTEM LOST ALL FLUID. COM PROCEDURES WERE COMPLIED WITH AND THE ACFT RETURNED TO THE GATE. MX FOUND THE RT SIDE LOWER HYDRAULIC FUSE HAD FAILED. A HYDRAULIC SYSTEM RT SIDE RETURN LINE, THE FAILED FUSE, THE ELECTRICAL AUXILIARY HYDRAULIC PUMP, THE ENGINE DRIVEN HYDRAULIC PUMP NR 2 ENGINE AND ALL APPLICABLE HYDRAULIC SYSTEM FILTERS WERE REPLACED. NO DEBRIS WAS FOUND IN ANY FILTER OR PUMP HOUSING. LEAK CHECK AND OPS CHECK WERE GOOD AND THE ACFT WAS RETURNED TO SERVICE.

More about the Beech C90