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71-17-08: Rear Engine Stoppage On Take Off

FAA order 71-17-08 is an airworthiness directive in force since August 24, 1971. The FAA's subject line: Rear Engine Stoppage On Take Off. It names Cessna 337 Skymaster: about 370 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: engine.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Cessna Aircraft Company
Models
337, 337A, 337B, 337C, 337D, 337E, 337F, 337G, 337H
On this site
Cessna 337 Skymaster 370 registered

Dates and paperwork

In force since
August 24, 1971
Docket
Unknown
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (1,202 characters)
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.

Related safety bulletins advice on the same designs, not orders

2012-08-09CE-12-41 · Flight Controls Loose Glide Screw
2012-05-21CE-12-24R1 · Flight Controls Frayed Flap Extend Cables
2012-04-06CE-12-24 · Flight Controls Frayed Flap Extend Cables
2012-01-25CE-12-14 · Three Alternative Methods of Compliance for AD 2011-10-09
2010-07-30CE-10-40R1 · Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 27, 2026. Connections as data: /graph/directive/71-17-08.json · aircraft systems.