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NATO - STANAG 3950

Helicopter Design Criteria for Crew Crash Protection and Anthropometric Accommodation

active, Most Current
Organization: NATO
Publication Date: 14 February 2001
Status: active
Page Count: 37
scope:

AIM

The aim of this agreement is to provide helicopter design criteria for crash protection and anthropometric accommodation of the crew.

Document History

STANAG 3950
February 14, 2001
Helicopter Design Criteria for Crew Crash Protection and Anthropometric Accommodation
AIM The aim of this agreement is to provide helicopter design criteria for crash protection and anthropometric accommodation of the crew.
STANAG 3950
February 14, 2001
Helicopter Design Criteria for Crew Crash Protection and Anthropometric Accommodation
A description is not available for this item.
STANAG 3950
January 1, 1991
Helicopter Crew Seat Design
A description is not available for this item.
STANAG 3950
January 1, 1991
Helicopter Crew Seat Design
A description is not available for this item.

References

This document references:
ISO 2631-1 - Mechanical vibration and shock — Evaluation of human exposure to whole-body vibration — Part 1: General requirements AMENDMENT 1
Published by ISO on July 1, 2010
This part of ISO 2631 defines methods for the measurement of periodic, random and transient whole-body vibration. It indicates the principal factors that combine to determine the degree to which a...
This document references:
MIL-STD-1290 - LIGHT FIXED AND ROTARY-WING AIRCRAFT CRASH RESISTANCE
Published by NPFC on January 17, 2006
A description is not available for this item.
This document is referenced by:
DEF STAN 00-970: PART 5 - Certification Specifications for Airworthiness Part 5: LARGE TYPE AIR SYSTEMS
Published by MODUK on March 14, 2021
Where CS 25 makes reference to ‘the Agency’, this should be considered to mean the certifying authority.
This document is referenced by:
DEF STAN 00-970: PT7 SEC1 - Design and Airworthiness Requirements for Service Aircraft Part 7: Rotorcraft Section 1: Introduction
Published by MODUK on July 13, 2015
This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Rotorcraft Aircraft for UK Military operation.
This document is referenced by:
DEF STAN 00-970: PART 0 - Certification Specifications for Airworthiness Part 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
Published by MODUK on March 14, 2021
Part 0 provides guidance and content information, together with definitions of terms used throughout this Standard.
This document is referenced by:
DEF STAN 00-970: PART 11 - Certification Specifications for Airworthiness Part 11: ENGINES
Published by MODUK on August 28, 2020
Unless otherwise specified in this Standard, the certification requirements of EASA CS-E (amendment 6) including related AMC and Appendices shall be applied. Additionally, the requirements of CS-E...
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