AD 71-17-08

Active

Rear Engine Stoppage On Take Off

Key Information
71-17-08
Active
August 24, 1971
Not specified
Unknown
39-1273
Applicability
["Aircraft"]
["Small Airplane"]
Cessna Aircraft Company
337 337A 337B 337C 337D 337E 337F 337G 337H
Regulatory Text

71-17-08 CESSNA: Amdt. 39-1273. Applies to Model 337 Airplanes.

Compliance. To minimize the possible adverse affects of undetected rear engine stoppage during take-off, within the next 10 hours' time in service after the effective date of this AD, the following modifications must be accomplished and the following operational procedures will be applicable:

A) Readjust the rear engine idle RPM from 575-625 to 625-675 and readjust idle mixture accordingly.

B) Taxi primarily by use of the rear engine.

C) Initiate all take-offs by advancing the throttle on the rear engine to a point where the normal functioning of the rear engine has been established before advancing the throttle of the front engine.

D) Install a permanent placard to the right of the tachometer instrument to read as follows:

TAXI AND TAKE-OFF
LEAD WITH REAR ENGINE POWER
CHECK RPM AND FUEL FLOW

NOTE: The operator may make and install a temporary placard using minimum 1/8 inch highletters until the permanent placard is obtained from the manufacturer and properly installed.

Cessna Service Letter ME 71-21 refers to the subject matter of this AD.

This amendment becomes effective August 24, 1971.

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
FAA Documents