Source: https://standards.globalspec.com/std/9954341/def-stan-00-970-pt1-sec3
Timestamp: 2020-07-13 19:18:46
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MODUK - DEF STAN 00-970: PT1 SEC3 - Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 3: Structure | Engineering360
MODUK - DEF STAN 00-970: PT1 SEC3
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 3: Structure
This section specifies the requirements for structural strength of the aircraft. Requirements are provided to cover the following aspects:
Static Strength and Deformation
Symmetric Manoeuvres
Asymmetric Manoeuvres
High Lift Devices and Airbrakes
Spinning and Spin Recovery
Strength for Ground Handling
The section is intended to provide information similar to that contained in CS 25 Section C.
DEF STAN 00-970: PT1 SEC3
DEF STAN 00-970: PT 1: SEC 3
Design and Airworthiness Requirements for Service Aircraft - Part 1: Fixed Wing - Section 3: Structure
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 3 - Structure
Design and Airworthiness Requirements for Service Aircraft Part 1 - Fixed Wing - Section 3 - Structure
Design and Airworthiness Requirements for Service Aircraft Part 1 – Fixed Wing Section 3 - Structure
INTRODUCTION This section specifies the requirements for structural strength of the aircraft. Static Strength and Deformation Fatigue Symmetric Manoeuvres Asymmetric Manoeuvres Gust Loads High...
Design and Airworthiness Requirements for Service Aircraft Part 1 Section 3 - Structure
INTRODUCTION This section specifies the requirements for structural strength of the aircraft. Requirements are provided to cover the following aspects: The section comprises the content of DEF...
Design and Airworthiness Requirements for Service Aircraft Structure