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Document ID:   MIL-STD-2066       Scroll down to access document images

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      
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.
MediaDocument Part DescriptionDist StmtDocument DatePagesSize
Document ImageNotice 2 - CancellationA17-MAR-199912.7 KB
Document ImageChange Notice 1 A08-MAR-198212.4 KB
Document ImageBase Document A20-MAR-198118321385.3 KB

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