Service difficulty report · Case · Beech 58

Difficulty date
January 19, 1999
Submitted
March 26, 2000
Operation
General aviation
Aircraft
N7353R
Make and model
Beech 58
Aircraft serial
TH486
Engine
Cont IO520C
Part
Case
Condition
Fractured
Location
Nr 1 Engine
Stage of operation
IN
Nature of condition
O
Precautionary procedure
K

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

What was found

DURING ANNUAL INSPECTION, FOUND ABOVE MENTIONED HOSE LEAKING PROFUSELY. THE HOSE APPEARED TO BE SUPPORTED PROPERLY. WHEN FUEL PRESSURE WAS APPLIED WITH AIRCRAFT ELECTRIC BOOST PUMP, FUEL BEGAN COMING OUT OF BRAIDED, CRIMPED AREA NEAR THE END OF THE HOSE. AD 71-24-04 DOES NOT APPLY TO THIS MODEL NUMBER AND SERIAL NUMBER OF AIRCRAFT. SE 71-7, SUPPLEMENT 1, DATED 11-3-71, ENCOMPASSES ALL CESSNA SINGLE ENGINE AIRCRAFT. (X)

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