MODUK - DEF STAN 00-970: PT 1: SEC 1
General Requirements Effects of Angular Acceleration on Instruments & Equipment; Leaflet 2
inactive
| Organization: | MODUK |
| Publication Date: | 1 December 1999 |
| Status: | inactive |
| Page Count: | 3 |
scope:
INTRODUCTION
This leaflet amplifies the requirements and gives acceptable means of compliance. It was previously issued as Leaflet 100/3 of DEF STAN 00-970 Issue 1. The main objective is to draw attention to the need for some equipment to function correctly not only in normal conditions but also in conditions which occur in the period leading up to an accident or incident.
Document History
July 13, 2015
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 1: General requirements
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...
January 10, 2014
Design and Airworthiness Requirements for Service Aircraft - Part 1: Fixed Wing - Section 1: General requirements
PREFACE
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 operation....
July 5, 2013
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 1: General
PREFACE
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 operation....
January 7, 2013
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 1 – General Requirements
PREFACE
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 operation....
July 20, 2012
Design and Airworthiness Requirements for Service Aircraft - Part 1 Fixed Wing - Section 1 – General Requirements
INTRODUCTION
This section specifies general requirements for application in the design of aircraft. They cover a number of disparate subject areas which are relevant to the detailed system level...
October 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 1 - General Requirements
INTRODUCTION
This section specifies general requirements for application in the design of aircraft. They cover a number of disparate subject areas which are relevant to the detailed system level...
January 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 1 - General
INTRODUCTION
This section specifies general requirements for application in the design of aircraft. They cover a number of disparate subject areas which are relevant to the detailed system level...
February 5, 2010
Design and Airworthiness Requirements for Service Aircraft Part 1 - Fixed Wing Section 1 - General
INTRODUCTION
This section specifies general requirements for application in the design of aircraft. They cover a number of disparate subject areas which are relevant to the detailed system level...
January 31, 2007
Design and Airworthiness Requirements for Service Aircraft Part 1 Section 1 - General
PREFACE
This Standard provides requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation. The requirements stated herein shall be applied...
DEF STAN 00-970: PT 1: SEC 1
December 1, 1999
General Requirements Effects of Angular Acceleration on Instruments & Equipment; Leaflet 2
INTRODUCTION
This leaflet amplifies the requirements and gives acceptable means of compliance. It was previously issued as Leaflet 100/3 of DEF STAN 00-970 Issue 1. The main objective is to draw...
December 1, 1999
Design and Airworthiness Requirements for Service Aircraft General
PREFACE
This document provides requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation. The requirements stated herein shall be applied...