AD 70-15-18

Active

Automatic Pilot and Automatic Aileron Stabilizer Instruments

Key Information
70-15-18
Active
August 31, 1970
Not specified
Unknown
39-1046
Applicability
["Appliance"]
Not specified
Mitchell Industries, Inc.
Auto Pilot Systems Instruments
Regulatory Text

70-15-18 MITCHELL INDUSTRIES, INC., doing business as EDO-AIRE MITCHELL: Amendment 39-1046. Applies to the Mitchell Century II, Century III (Serial Numbers 624 and below) and Stabilizer, automatic pilot and automatic aileron stabilizer instruments, and to Piper AutoControl III, Altimatic III and AutoFlite automatic pilot and automatic aileron stabilizer instruments installed in various light aircraft in accordance with the following Supplemental Type Certificates:

AIRCRAFT MAKE
SUPPLEMENTAL TYPE CERTIFICATE NUMBERS
Aero Commander
SA680SW

Beech
SA617SW SA742SW SA755SW SA800SW

SA638SW SA745SW SA761SW SA824SW

SA651SW SA754SW SA767SW SA837SW

Cessna
SA603SW SA624SW SA668SW SA784SW
(See also Wren)
SA606SW SA637SW SA669SW SA789SW

SA607SW SA658SW SA709SW SA795SW

SA621SW SA667SW SA737SW SA829SW

deHavilland
(See Riley 400)

Helio
SA615SW

Maule
SA693SW

Piper
SA511SW SA540SW SA596SW SA757SW

SA525SW SA566SWSA662SW SA822SW

SA532SW SA576SW SA707SW SA862SW

SA533SW SA581SW SA756SW SA921SW

Riley 400 (deHavilland modified per STC's SA120SO, SE163SO and SA164SO)
SA676SW

Wren (Cessna modified per
SA791SW
STC No. SA485SW)

Compliance required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent slippage of servo bridle cable clamps and resultant binding of the control system, accomplish the following:

Remove Servo Bridle Cable Clamps, Mitchell P/N 42A173 or 42A184, as applicable, and replace with new Servo Bridle Cable Clamps, Mitchell P/N 42A173-1 or 42A184-1, as applicable, in accordance with the installation instructions in Mitchell Industries, Inc. Service Bulletin No. MB-1 dated 2-11-68, revised as Edo-Aire Mitchell Service Bulletin No. MB-1 dated 6-1-70, or later FAA approved revision, or in accordance with instructions approved by the Chief, Engineering and Manufacturing Branch, Flight Standards Division, Southwest Region, Federal Aviation Administration.

The revised bulletin may be obtained from Edo-Aire Mitchell, P.O. Box 610, Mineral Wells, Texas 76067.

This Amendment becomes effective August 31, 1970.

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References
This information is not available.
--- - Part 39
FAA Documents