Accession Number:

AD0774084

Title:

Test Plan for the Hook Bounce Condition of the E-2A Airplane Arresting Gear 'A' Frame.

Descriptive Note:

Test plan rept.,

Corporate Author:

NAVAL AIR DEVELOPMENT CENTER WARMINSTER PA AIR VEHICLE TECHNOLOGY DEPT

Personal Author(s):

• Cadman,Robert B.

Report Date:

1973-11-30

Pagination or Media Count:

8.0

Abstract:

The E-2A arresting hook A-frame is currently adequate for 500 arrested landings. It is the purpose of this effort to extend the life to 3,000 arrested landings for the hook bounce condition. Author

Descriptors:

• *CARRIER LANDINGS
• *ARRESTING GEAR
• ARRESTING(PROCESS)
• HOOKS
• LOADS(FORCES)
• LIFE EXPECTANCY(SERVICE LIFE)
• AVIATION SAFETY

Subject Categories:

• Patrol and Reconnaissance Aircraft
• Terminal Flight Facilities

Distribution Statement:

APPROVED FOR PUBLIC RELEASE