AD 82-07-04

Superseded

Fuel Shutoff Valve Modification

Key Information
82-07-04
Superseded
April 06, 1982
Not specified
Unknown
39-4355
Applicability
["Aircraft"]
["Small Airplane"]
Allied Ag Cat Productions, Inc.
G-164A G-164B G-164B-15T G-164B-20T G-164B-34T G-164B (with 73 inch wing gap) G-164C G-164D G-164D (with 73 inch wing gap)
Regulatory Text

82-07-04 SCHWEIZER: Amendment 39-4355. Applies to Model G-164A (S/Ns 1726A through 1730A); Model G-164B (S/N 335B through 659B); Model G-164C (S/N 1C through 44C); and Model G-164D (S/N 1D through 22D) airplanes certificated in any category.

COMPLIANCE: Required as indicated, unless already accomplished.

To assure a positive stop of the fuel shut-off valve at the "ON" position, within the next 100 hours time-in-service after the effective date of this AD, accomplish the following:

(a) Modify the fuel shut-off valve control by installation of a new stop-plate, P/N A1552-71, in accordance with instructions in Schweizer Ag-Cat Service Bulletin No. 78 dated January 26, 1982.

(b) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.

(c) Any equivalent method of compliance with this AD, when used, must be approved by the Chief, New York Aircraft Certification Office, FAA, Eastern Region, Federal Building, JFK International Airport, Jamaica, New York 11430; telephone (212) 995-2842.

This amendment becomes effective on April 6, 1982.

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Related ADs
2007-17-02 Replaced by the above
References
This information is not available.
--- - Part 39
FAA Documents