UNLIMITED FREE
ACCESS TO THE WORLD'S BEST IDEAS

SUBMIT
Already a GlobalSpec user? Log in.

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

Customize Your GlobalSpec Experience

Select Your Free Newsletters

Industry Newsletters

Select Your Free Product Alerts

Finish!
Privacy Policy

This is embarrasing...

An error occurred while processing the form. Please try again in a few minutes.

NATO - STANAG 3237

Aperture of Terminal Ring or Link of Aircraft Lifting Slings

active, Most Current
Organization: NATO
Publication Date: 25 November 1982
Status: active
Page Count: 11
scope:

AIM

The aim of this agreement is to enable direct attachment of Aircraft Lifting Slings to Crane Hooks in those cases where slings designed to lift the complete aircraft are provisioned.

NOTE: Slings designed to lift complete aircraft by helicopters are excluded.

Document History

STANAG 3237
November 25, 1982
Aperture of Terminal Ring or Link of Aircraft Lifting Slings
AIM The aim of this agreement is to enable direct attachment of Aircraft Lifting Slings to Crane Hooks in those cases where slings designed to lift the complete aircraft are provisioned. NOTE: Slings...
STANAG 3237
January 1, 1982
Aperture of Terminal Ring or Link of Aircraft Lifting Slings
A description is not available for this item.
STANAG 3237
January 1, 1982
Aperture of Terminal Ring or Link of Aircraft Lifting Slings
A description is not available for this item.

References

This document references:
STANAG 3542 - TECHNICAL CRITERIA FOR THE TRANSPORT OF CARGO BY HELICOPTER - ATP-110 EDITION A
Published by NATO on October 1, 2019
A description is not available for this item.
This document is referenced by:
DEF STAN 00-970: PT1 SEC4 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 4: Design and Construction
Published by MODUK on July 13, 2015
PREFACE (a) This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military...
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: PART 9 - Design and Airworthiness Requirements for Service Aircraft Part 9: Remotely Piloted Air Systems
Published by MODUK on September 28, 2017
(a) The mandatory requirements set out in this Standard are those basic requirements needed for the design and development of airworthy RPAS for all three UK Armed Services based on the requirements...
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.
View Less
View All
Advertisement