DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT
Available format(s)
Hardcopy , PDF
Superseded date
01-31-2007
Language(s)
English
Published date
01-01-2006
Publisher
Preface
Main Text
SECTION 6 - EQUIPMENT
6.0 Introduction
6.1 General
6.2 Avionic Equipment Installations
6.3 Static Pressure Systems
6.4 Magnetic Compass Installations
6.5 Automatic Pilot Systems
6.6 Electrical Systems
6.7 Lights
6.8 Safety Equipment
6.9 Ice Protection
6.10 EMC of Safety Critical Systems
6.11 Hydraulic Systems
6.12 Pneumatic Systems
6.13 Oxygen Systems
6.14 Pressurised Gas Storage Vessels
6.15 Data Recording Systems
Tables
Diagrams
SUPPLEMENTS
Section 6 - Leaflets 0 to 34
Specifies the requirements relating to equipment and systems embodied on any aircraft. It is to be used where there are no aircraft specific requirements that take precedence.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC6/3(2003) (04/2006)
|
| DocumentType |
Standard
|
| Pages |
346
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| BS 3J 12:1991 | Specification for pressure-sensitive adhesive identification tape |
| BS 2G 124-1:1966 | Specification for a.c. generators for aircraft Constant frequency |
| BS 2G 143:1965 | Specification for a.c. and d.c. rotary and linear actuators for aircraft |
| BS 2G 180:1974 | Specification for permanent splicing of aircraft electrical cables |
| DEFSTAN 00-13/3(1994) : 1994 | REQUIREMENTS FOR THE ACHIEVEMENT OF TESTABILITY IN ELECTRONIC AND ALLIED EQUIPMENT |
| BS 2G 134:1970 | Specification for d.c. generators |
| BS 2G 231:1990 | Specification for conductors for general-purpose aircraft electrical cables and aerospace applications |
| BS 5M 23:1987 | Specification for an identification scheme for pipelines |
| DEFSTAN 00-35(PT5)/3(1999) : 1999 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 5: INDUCED MECHANICAL ENVIRONMENTS |
| DEFSTAN 59-97/3(1990) : AMD 1 | HEAT SHRINKABLE INSULATION MATERIALS - GENERAL REQUIREMENTS, TESTS AND TEST METHODS FOR CAPABILITY APPROVAL |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| BS N100(1967) : LATEST | |
| BS G 207:1969 | Specification for aircraft electrical circuit diagrams |
| BS 3G 197:1982 | Specification for stud-type terminal blocks for terminations on aircraft electric cables |
| BS 5G 178-1:1993 | Crimped joints for aircraft electrical cables and wires. Specification for design requirements (including tests) for components and tools |
| DEFSTAN 59-71/1(1988) : 1988 AMD 1 1990 | CRIMPED ELECTRICAL CONNECTIONS FOR COPPER CONDUCTORS - GENERIC SPECIFICATION |
| BS 2G 124-2:1966 | Specification for a.c. generators for aircraft Variable frequency |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| BS 2G 202:1988 | Specification for design and performance requirements for airframe-fit electrical connectors for d.c. and low frequency a.c. applications |
| DEFSTAN 59-35(PT0)/3(1990) : 1990 | CONNECTORS ELECTRICAL - PART 0: GUIDE TO CONNECTORS ELECTRICAL, DIRECT CURRENT, LOW FREQUENCY AND RADIO FREQUENCY APPLICATIONS |
| BS 2G 147-1:1966 | Specification for a.c. motors for aircraft Three-phase constant frequency squirrel-cage induction motors |
| MIL-STD-1788 Revision A:1985 | AVIONICS INTERFACE DESIGN STANDARD |
| BS G 212:1971 | Specification for general requirements for aircraft electrical cables |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| BS 2G 127:1967 | Specification for power and current transformers for use in aircraft electrical power supply systems |
| BS G 179-2:1966 | Specification for hand-operated circuit-breakers for aircraft Three-pole circuit-breakers |
| STANAG 3323 : 0 | PIPE (TUBE) CONNECTIONS TO AIRCRAFT INSTRUMENTS (IMPERIAL AND METRIC) |
| DEFSTAN 00-41/3(1993) : 1993 | RELIABILITY AND MAINTAINABILITY MOD GUIDE TO PRACTICES AND PROCEDURES |
| DEFSTAN 00-31/1(1987) : 1987 | THE DEVELOPMENT OF SAFETY CRITICAL SOFTWARE FOR AIRBORNE SYSTEMS |
| BS M 44:1974 | Specification for identification of aircraft servicing, maintenance, ground handling and safety/hazard points |
| DEFSTAN 00-971/1(1987) : 1987 | GENERAL SPECIFICATION FOR AIRCRAFT GAS TURBINE ENGINES |
| BS G 209:1970 | Specification for transformer rectifier units |
| BS 2G 232:1987 | Specification for electric cables for general airframe or equipment interconnect use (135°C), wrapped insulation |
| BS 2G 233:1987 | Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation |
| BS 5G 205-1:1990 | Secondary batteries for aircraft Specification for lead-acid batteries |
| BS 3G 229:1993 | Schedule for environmental conditions and test procedures for airborne equipment |
| BS 2G 146:1966 | Specification for d.c. motors for aircraft |
| BS G 203:1967 | Specification for Unified screws with captive facing and locking washers |
| BS 2G 223:1989 | Specification for screen terminating devices for aircraft electric cables |
| MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
| BS 2G 230:1991 | Specification for general requirements for aircraft electrical cables (second series) |
| BS 2G 199:1984 | Schedule for tables relating to altitudes, airspeed and Mach numbers for use in aeronautical instrument design and calibration |
| DEFSTAN 59-36/5(1995) : 1995 | SELECTION OF ELECTRONIC AND ELECTRICAL COMPONENTS FOR USE IN DEFENCE EQUIPMENT |
| BS 3G 210:1996 | Specification for PTFE insulated equipment wires and cables, single- and multi-core, with silver plated copper conductors (190°C) or nickel plated copper conductors (260°C) |
| BS 2G 196:1971 | Specification for static invertors |
| BS 4G 173-1:1985 | Connectors for ground electrical supplies for aircraft Specification for design, performance and test requirements |
| DEFSTAN 59-31/2 : LATEST | LIGHTING PROTECTION |
| BS 2G 219:1983 | Specification for general requirements for ground support electrical supplies for aircraft |
| DEFSTAN 61-3/5(1992) : INTERIM | GENERIC SPECIFICATION FOR BATTERIES, NON RECHARGEABLE, PRIMARY |
| DEFSTAN 00-35(PT3)/3(1999) : 1999 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 3: ENVIRONMENTAL TEST METHODS |
| BS G 217:1975 | Specification for general requirements for cockpit lighting controllers |
| DEFSTAN 00-35(PT4)/3(1999) : 1999 AMD 1 2000 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 4: NATURAL ENVIRONMENTS |
| BS G 194:1965 | Specification for lever-operated manual switches for aircraft |
| BS 2G 147-2:1966 | Specification for a.c. motors for aircraft Three-phase variable frequency squirrel-cage induction motors |
| BS G 102:1971 | Specification for general requirements for rotating electrical machinery |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| BS 4G 229:1996 | Schedule for environmental conditions and test procedures for airborne equipment |
| MIL-I-8700 Revision A:1970 | INSTALLATION AND TEST OF ELECTRONIC EQUIPMENT IN AIRCRAFT, GENERAL SPECIFICATION FOR |
| BS G 222:1976 | Specification for Efglas type electric cables (metric units) |
| DEFSTAN 00-970/VOL1/1(1983) : AMD 14 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - AEROPLANES |
| DEFSTAN 00-970/VOL2/1(1984) : 1984 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - ROTORCRAFT |
| DEFSTAN 00-35(PT1)/3(1999) : 1999 | ENVIRONMENTAL HANDBOOK FOR DEFENCE MATERIEL - PART 1: CONTROL AND MANAGEMENT |
| DEFSTAN 00-52/3(1991) : 1991 | THE GENERAL REQUIREMENTS FOR PRODUCT ACCEPTANCE AND MAINTENANCE TEST SPECIFICATIONS AND TEST SCHEDULES |
Hardcopy - English
PDF - English
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