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MODUK - DEF STAN 00-970: PT1 SEC7

Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 7: Operating Limitations and Information

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Organization: MODUK
Publication Date: 13 July 2015
Status: active
Page Count: 64
scope:

INTRODUCTION

This Clause specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for VSTOL aeroplanes. These requirements are to be used where there are no aircraft specific requirements that take precedence.

Requirements are provided to cover the following aspects:

Operating Limitations - covers the general criteria and requirements for aircraft operation

Climatic Conditions - covers requirements for operation in the specified climatic categories and associated weatherproofing

Aircraft Performance Limitations - covers the evaluation of aircraft performance

Operational Colouring and Markings - covers colours, markings and placards

Publication of Aircraft Performance - covers preparation and publication of data on aircraft performance

Electronic Cockpit Documentation - covers display systems for the on-aircraft provision of information

This section is intended to provide information similar to the content of CS 25 Section G.

Document History

DEF STAN 00-970: PT1 SEC7
July 13, 2015
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 7: Operating Limitations and Information
INTRODUCTION This Clause specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 7: Operating Limitations and Information
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 7: Operating Limitations and Information
INTRODUCTION  This Clause specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 7: Operating Limitations and Information
A description is not available for this item.
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 7 Operating Limitations and Information
INTRODUCTION This Clause specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
Design and Airworthiness Requirements for Service Aircraft - Part 1 Fixed Wing - Section 7 Operating Limitations and Information
INTRODUCTION  This Clause specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
October 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 7 Operating Limitations and Information
PREFACE a. This Part of the Defence Standard provides requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation. The requirements stated...
January 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 7 - Operating Limitations and Information
INTRODUCTION This chapter specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...
January 31, 2007
Design and Airworthiness Requirements for Service Aircraft Part 1 Section 7 - Operating Limitations and Information
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...
December 1, 1999
Design and Airworthiness Requirements for Service Aircraft Operating Limitations and Information
INTRODUCTION This chapter specifies the basic operational limitations for general application in the design of aircraft but are not applicable in the case of take-off and landing requirements for...

References

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