DEVELOPMENT OF MODEL 3500 ARRESTING GEAR AND CONTINUED DEVELOPMENT OF SPRING HOOK FOR COMMERCIAL AIRCRAFT
Abstract
The fuselage stresses, fuselage accelerations and engine accelerations obtained on the FAA Boeing 727-027, N-113 during arrestments into the Model 3500 Arresting Gear at speeds through 135.6 knots and gross weights through 220,000 lb were within safe working levels. A summary of stresses as obtained by strain measurement is reported. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1963
- Accession Number
- AD0408964
Entities
People
- Antonio Russo