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Document ID:
MIL-STD-2066
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Overview
Title:
CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (S/S BY MIL-HDBK-2066)
Scope:
The information contained herein presents loading characteristics, associated parameters, and methods to be used in calculating the catapulting and arresting loads of MIL-A-8863 and MIL-A-8866 for the design of U.S. Navy airplanes operating from shipboard and shorebased launching and recovery gears. A listing of such gears for which data is contained herein is given in Table 1.
Status:
Canceled
Cancellation Date:
17-MAR-1999
FSC/Area:
1510
Doc Category:
Military Standard -Military Standard
Responsibilities
Lead Standardization Activity:
11
Air Force Life Cycle Management Center - Aircraft Systems
Preparing Activity:
AS
Naval Air Systems Command
Coordination:
Limited
Navy Custodian:
AS
Naval Air Systems Command
Changes to military standards or handbooks issued after August 1, 2003 are incorporated in the modified document.
Revision History
Click on column headings for a description of column content.
Media
Document Part Description
Dist Stmt
Document Date
Pages
Size
Notice 2 - Cancellation
A
17-MAR-1999
1
2.7 KB
Change Notice 1
A
08-MAR-1982
1
2.4 KB
Base Document
A
20-MAR-1981
183
21385.3 KB
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Defense Standardization Program
WARNING: UNAUTHORIZED ACCESS TO THIS UNITED STATES GOVERNMENT COMPUTER SYSTEM AND SOFTWARE IS PROHIBITED BY PUBLIC LAW 99-474 (THE COMPUTER FRAUD AND ABUSE ACT OF 1986) AND CAN RESULT IN ADMINISTRATIVE, DISCIPLINARY OR CRIMINAL PROCEEDINGS.