PERSONNEL RESTRAINT SYSTEMS STUDY, CH-47 VERTOL CHINOOK. SUPPLEMENT

reportActive / Technical Report | Accession Number: AD0607659 | Open PDF

Abstract:

Contents Installation of personnel restraint system Inertia reel installation pilots and copilots seat Reinforcement of lap belt attachment Reinforcement of cockpit floor and tract modification Installation of tie-down strap alternate 1 Installation of control cable and shoulder harness Reinforcement of vertical track, seat bucket crew seat Modification of carriage assembly crew seat Reinforcement of lock-pin assembly seat base Shoulder harness troop commander Installation of attachment fitting for shoulder harness Fitting for shoulder harness attachment left-hand side Fitting for shoulder harness attachment right-hand side End fitting for lap belt Lap belt Installation of restraint system Lap belt attachments Lap belt tie-down strap and Pilots tie-down strap.

Author(s):
No Author(s) Identified
Author Organization(s):
AVIATION SAFETY ENGINEERING AND RESEARCH PHOENIX AZ
Descriptive Note:
Crash injury evaluation
Pagination:
0084

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited.

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
AVCIR-62-26
Contract/Grant Number(s):
DA-44-177-AMC-888(T)
Task Number(s):
1A024701A12101
Monitor Series:
TRECOM
 Subject Terms
Joint Capability Areas:
JCA_3.1.1_Maneuver to Engage; JCA_3.1_Maneuver; JCA_3_Force Application; JCA_5_Command and Control; JCA_6.1.1_Wired Transmission; JCA_6_Net Centric; JCA_6.1_Information Transport
Modernization Areas:
Microelectronics
Communities of Interest:
Human Systems
Descriptor(s):
*AVIATION SAFETY, *MECHANICAL DRAWING, COCKPITS, FUSELAGES, HELICOPTERS, LOADS(FORCES), MILITARY REQUIREMENTS, SEATS, TRANSPORT AIRCRAFT
Field(s)/Group(s):
Military Aircraft Operations
Report Date:
1964 Apr 01