DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
Available format(s)
Hardcopy , PDF
Superseded date
11-07-2014
Superseded by
Language(s)
English
Published date
01-01-2014
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.
Preface
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
SUPPLEMENTS
Section 6 - Leaflets 0 to 35
Gives the requirements relating to equipment and systems embodied on any aircraft.
| DevelopmentNote |
Supersedes DEFSTAN 00-970(PT1)SEC6/11(2013). (03/2014)
|
| DocumentType |
Standard
|
| Pages |
270
|
| PublisherName |
UK Ministry of Defence Standards
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| BS 3J 12:1991 | Specification for pressure-sensitive adhesive identification tape |
| BS C 18:1976 | Specification for V-flange couplings for aircraft piping and ducting - metric series |
| BS 2M 51:1989 | Classification for pressure and temperature for fluid systems and components |
| 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 61-10(PT1)/1(1995) : 1995 | GENERATOR SETS (GROUND, ENGINE DRIVEN) POWER AND DISTRIBUTION - PART 1: BOX, DISTRIBUTION 13 A 3 WAY, 240 V FOR FIELD ELECTRICAL POWER DISTRIBUTION SYSTEMS INCORPORATING CECC 75201.007 INPUT CONNECTOR |
| BS 2G 134:1970 | Specification for d.c. generators |
| BS M 43:1973 | Methods of zoning aircraft and referencing access doors and panels |
| DEFSTAN 81-24/5(2004) : 2004 | IDENTIFICATION MARKING OF TRANSPORTABLE CONTAINERS, COMPRESSED GAS |
| BS M 55:1984 | Method for rotary flexure testing of hydraulic tubing joints and fittings for aerospace use |
| BS 2C 13:1988 | Specification for sizes of aircraft gravity filling orifices and associated replenishment nozzles (metric series) |
| BS 5M 23:1987 | Specification for an identification scheme for pipelines |
| DEFSTAN 59-97/3(1990) : AMD 1 | HEAT SHRINKABLE INSULATION MATERIALS - GENERAL REQUIREMENTS, TESTS AND TEST METHODS FOR CAPABILITY APPROVAL |
| DEFSTAN 05-42/2(1982) : 1982 | PARTICULATE CONTAMINATION CLASSES FOR FLUIDS IN HYDRAULIC SYSTEMS |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| 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 |
| MIL A 5498 : D | ACCUMULATORS, HYDRAULIC, CYLINDRICAL 3000 PSI, AIRCRAFT |
| DEFSTAN 01-5/17(2011) : 2011 | FUELS, LUBRICANTS AND ASSOCIATED PRODUCTS |
| ISO 6771:2007 | Aerospace — Fluid systems and components — Pressure and temperature classifications |
| BS 2M 53:1997 | Aircraft. Fluid systems. Thermal shock testing of piping and fittings |
| DEFSTAN 05-43/1(1977) : 1977 | STANDARD PROCEDURES FOR TAKING SAMPLES OF HYDRAULIC FLUIDS FOR EVALUATION OF PARTICULATE CONTAMINATION |
| BS 3G 231:1997 | Specification for conductors for general-purpose aircraft electrical cables and aerospace applications |
| MIL-STD-1760 Revision E:2007 | AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM |
| BS 2M 52:1989 | Method for impulse testing of hydraulic hose, tubing and fitting assemblies for aerospace fluid systems |
| 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 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 |
| STANAG 3323 : 0 | PIPE (TUBE) CONNECTIONS TO AIRCRAFT INSTRUMENTS (IMPERIAL AND METRIC) |
| 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 |
| DOD STD 1788 : LATEST | AVIONICS INTERFACE DESIGN STANDARD (METRIC) |
| 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 |
| MIL-PRF-5503 Revision G:2013 | ACTUATORS: AERONAUTICAL LINEAR UTILITY, HYDRAULIC, GENERAL SPECIFICATION FOR |
| BS M 48:1975 | Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series |
| BS M 60:1986 | Specification for separable tube fittings for fluid systems |
| BS 3G 230:2000 | Specification for general requirements for aircraft electrical cables (second series) |
| 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 199:1984 | Schedule for tables relating to altitudes, airspeed and Mach numbers for use in aeronautical instrument design and calibration |
| DEFSTAN 00-42(PT4)/3(2014) : 2014 | RELIABILITY AND MAINTAINABILITY ACTIVITY - PART 4: TESTABILITY |
| MIL-D-81641 Base Document:1972 | Display, Head-up, General Specification for |
| BS G 224:1978 | Specification for lever-operated manual switches for aircraft |
| DEFSTAN 00-41(PT1)/2(1989) : 1989 | MOD PRACTICES AND PROCEDURES FOR RELIABILITY AND MAINTAINABILITY - PART 1: RELIABILITY DESIGN PHILOSOPHY |
| MIL-H-8775 Revision D:1976 | HYDRAULIC SYSTEM COMPONENTS, AIRCRAFT AND MISSILES GENERAL SPECIFICATION FOR |
| 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 |
| MIL D 87213 : 0 | DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
| BS 2G 219:1983 | Specification for general requirements for ground support electrical supplies for aircraft |
| BS C 9:1970 | Specification for coupling dimensions for high pressure air charging valves for aircraft |
| BS 6G 205-1:1995 | Secondary batteries for aircraft Specification for lead-acid batteries |
| MIL F 8815 : D | FILTER AND FILTER ELEMENTS, FLUID PRESSURE, HYDRAULIC LINE, 15 MICRON ABSOLUTE AND 5 MICRON ABSOLUTE, TYPE 11 SYSTEMS; GENERAL SPECIFICATION FOR |
| MIL-H-5440 Revision H:1993 | HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR |
| BS G 217:1975 | Specification for general requirements for cockpit lighting controllers |
| BS 2917-1:1993 | Graphic symbols and circuit diagrams for fluid power systems and components. Specification for graphic symbols |
| ARINC 404A : 1974 | AIR TRANSPORT EQUIPMENT CASES AND RACKING |
| BS 3G 233:1990 | Specification for electric cables for general airframe or equipment interconnect use (135°C), extruded insulation |
| 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 |
| BS ISO 16889 : 2008 | HYDRAULIC FLUID POWER - FILTERS - MULTI-PASS METHOD FOR EVALUATING FILTRATION PERFORMANCE OF A FILTER ELEMENT |
| DEFSTAN 00-970/VOL2/1(1984) : 1984 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - ROTORCRAFT |
| STANAG 3212 : 2017 | DIAMETERS FOR GRAVITY FILLING ORIFICES |
| DEFSTAN 00-52/4(2014) : 2014 | THE GENERAL REQUIREMENTS FOR PRODUCT ACCEPTANCE AND MAINTENANCE TEST SPECIFICATIONS AND TEST SCHEDULES |
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