• Shopping Cart
    There are no items in your cart

DEFSTAN 00-970(PT1)SEC3/15(2015) : 2015

Withdrawn

Withdrawn

View Superseded by

DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 3: STRUCTURE

Available format(s)

PDF

Language(s)

English

Published date

01-01-2015

Withdrawn date

09-27-2015

US$20.00
Excluding Tax where applicable

Preface
SECTION 3 - STRUCTURE
SUPPLEMENTS

Covers the requirements for structural strength of the aircraft.

DevelopmentNote
Supersedes DEFSTAN 00-970(PT1)SEC3/14(2015). (09/2015)
DocumentType
Standard
Pages
323
PublisherName
UK Ministry of Defence Standards
Status
Withdrawn
SupersededBy
Supersedes

DEFSTAN 00-003/5(2016) : 2016 DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT
DEFSTAN 00-003/6(2017) : 2017 DESIGN GUIDANCE FOR THE TRANSPORTABILITY OF EQUIPMENT

MIL-HDBK-173 Revision A:1973 Audio Equipment
DEFSTAN 00-31/1(1987) : 1987 THE DEVELOPMENT OF SAFETY CRITICAL SOFTWARE FOR AIRBORNE SYSTEMS
FAA AC 20-107 : 2009 COMPOSITE AIRCRAFT STRUCTURE
BS C 11:1958 Coupling dimensions for aircraft pressure cabin ground test connections
DEFSTAN 16-17/2(1983) : 1983 AIR SUPPLY AND TEST CONNECTIONS FOR AIRCRAFT
MIL-DTL-9490 Revision E:2008 Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification for
MIL-HDBK-17-1 Revision F:2002 Composite Materials Handbook Volume 1 - Polymer Matrix Composites Guidelines or Characterization of Structural Materials (S/S by SAE-R422)
BS C 10:1958 Coupling dimensions for aircraft ground air-conditioning connections
DEFSTAN 53-68/2(1977) : 1977 AMD 2 1984 V-FLANGE COUPLINGS FOR AIRCRAFT PIPING AND DUCTING (METRIC)

US$20.00
Excluding Tax where applicable