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AD 81-26-04 ACTIVE

Cable Guard & Retainer Installation
Key Information
AD Number 81-26-04 Status Active
Effective Date December 31, 1981 Issue Date Not specified
Docket Number Unknown Amendment 39-4284
Product Type ["Aircraft"] Product Subtype ["Small/Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) M7 Aerospace LLC
Model(s) SA226-AT SA226-T SA226-TC
Regulatory Text

81-26-04 SWEARINGEN: Amendment 39-4284. Applies to Swearingen Model SA226-T, S/N T201 through T290; SA226-AT, S/N AT001 through AT066; SA226-TC, S/N TC201 through TC255 airplanes certified in all categories. Compliance required within the next 50 hours' time in service after the effective date of this AD but not later than January 15, 1982. Accomplishment of Fairchild Swearingen Service Bulletin SB27-022 issued January 5, 1979, satisfies the requirements of this AD (Airworthiness Docket No. 81-ASW-65).

To prevent disengagement of the control cables from the control pulleys, install cable guards and retainers in each control column in accordance with Fairchild Swearingen Service Bulletin SB27-022 issued January 5, 1979, or an equivalent means approved by the Chief, Aircraft Certification Division, FAA, Southwest Region.

A special flight permit may be issued in accordance with FAR 21.197 to allow flight of the aircraft to a location where this AD can be accomplished.This amendment becomes effective December 31, 1981.