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72-02-06: Automatic Pilot Instruments

FAA order 72-02-06 is an airworthiness directive in force since January 31, 1972. The FAA's subject line: Automatic Pilot Instruments. It names Cessna 182 Skylane, Cessna 206 Stationair, Cessna 210 Centurion, Cessna 337 Skymaster, Cessna P206 Super Skylane, Cessna U206 Stationair: about 14,900 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Appliance
Makes
Cessna Aircraft Company; Mitchell Industries, Inc.
Models
182E, 182F, 182G, 182H, 206, 210-5 (205), 210-5A (205A), 210B, 210C, 210D, 210E, 337, P206, U206, Automatic Pilot Instruments
On this site
Cessna 182 Skylane 11,828 registered
Cessna 206 Stationair 213 registered
Cessna 210 Centurion 1,527 registered
Cessna 337 Skymaster 371 registered
Cessna P206 Super Skylane 163 registered
Cessna U206 Stationair 798 registered

Dates and paperwork

In force since
January 31, 1972
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 (2,228 characters)
72-02-06 MITCHELL INDUSTRIES, INC., doing business as EDO-AIRE MITCHELL: Amdt. 39-1383. Applies to Mitchell automatic pilot instruments installed in various Cessna aircraft in accordance with the following Supplemental Type Certificates: AUTOPILOT MODEL STC NUMBER AIRCRAFT MAKE AND MODE AK086 SA20SW Cessna 210B and C AK086R SA20SW Cessna 210B and C AK086E SA20SW Cessna 210B and C AK088 SA27SW Cessna 182E and F AK088R SA27SW Cessna 182E and F AK088E SA27SW Cessna 182E and F AK110 SA101SW Cessna 182E, F and G AK110E SA101SW Cessna 182E, F and G AK110E-3 SA101SW Cessna 182E, F and G AK112 SA89SW Cessna 210B and C AK120 SA149SW (Cessna 210-5, 210-5A,) AK120E SA149SW ( 206, P206, ) AK120E-3 SA149SW ( and U206, ) AK126 SA330SW Cessna 210D and E AK126E SA330SW Cessna 210D and E AK126E-3 SA330SW Cessna 210D and E AK154 SA489SW Cessna 182H AK154E SA489SW Cessna 182H AK154E-3 SA489SW Cessna 182HAK155 SA491SW Cessna 337 AK155E SA491SW Cessna 337 AK155E-3 SA491SW Cessna 337 Compliance required within the next ten (10) hours' time in service after the effective date of this AD, unless already accomplished. To prevent fatigue failure of the control wheel shaft with possible resultant loss of aileron and elevator control, accomplish the following: Remove the Mitchell automatic pilot instrument servo, inspect the control wheel shaft, take corrective action as necessary, and reassemble in accordance with Edo-Aire Mitchell Service Bulletin No. MB-6 dated October 29, 1971, or later FAA approved revision, or any other method approved by the Chief, Engineering and Manufacturing Branch, Southwest Region, Federal Aviation Administration, Fort Worth, Texas. NOTE: The Mitchell automatic pilot instrument servo may be reinstalled in accordance with Edo-Aire Mitchell Service Letter ML-32 dated December 22, 1971, or later FAA approved revision, or any other methodapproved by the Chief, Engineering and Manufacturing Branch, Southwest Region, Federal Aviation Administration, Fort Worth, Texas. The bulletin and letter mentioned herein may be obtained from Edo-Aire Mitchell, P. O. Box 610, Mineral Wells, Texas 76067. This amendment becomes effective January 31, 1972.

Related safety bulletins advice on the same designs, not orders

2026-03-242026-08 · Floats
2025-07-282025-07 · Reciprocating Engine Supercharger
2021-08-26AIR-21-16 · FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt Inspection
2019-02-12CE-19-01 · Engine Oil and Airplane Hour Meter; Pressure Switch Failure
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM

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 8, 2026. Connections as data: /graph/directive/72-02-06.json · aircraft systems.