AD 81-24-02

Active

Hydraulic System Fluid Flow

Key Information
81-24-02
Active
November 23, 1981
Not specified
Unknown
39-4259
Applicability
["Aircraft"]
["Large Airplane"]
Gulfstream Aerospace Corporation
G-1159 G-1159A
Regulatory Text

81-24-02 GULFSTREAM AMERICAN CORPORATION (GRUMMAN AMERICAN AVIATION CORPORATION): Amendment 39-4259. Applies to Model G-1159 Serial Numbers 1 through 248, 250, 251, 253 through 258 and 775; Model G-1159A Serial Numbers 249, 252, 300 through 338 and 875.

Compliance required within the next 75 hours time in service after the effective date of this AD, unless already accomplished. To prevent the loss of fluid flow in the auxiliary hydraulic system following a complete loss of fluid in the combined hydraulic system, install a check valve in the reservoir system in accordance with Gulfstream American Aircraft Service Change (ASC) No. 295 (for the Model G-1159) and ASC No. 21 (for the Model G-1159A), both dated September 1, 1981. An equivalent method of compliance may be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region.

This amendment becomes effective November 23, 1981.

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