• Shopping Cart
    There are no items in your cart

AFGS-87219 Revision B:2012

Current

Current

The latest, up-to-date edition.

Electrical Power Systems, Aircraft

Available format(s)

PDF

Language(s)

English

Published date

23-10-2012

€16.67
Excluding VAT

1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
APPENDIX A - ELECTRICAL POWER SYSTEMS, AEROSPACE
             VEHICLES HANDBOOK FOR

Determines the performance requirements and verifications for electric power subsystems (EPS) for aerospace vehicles, including aircraft, helicopters, and missiles.

DevelopmentNote
Supersedes MIL E 87219. (08/2003)
DocumentType
Standard
Pages
70
PublisherName
US Military Specs/Standards/Handbooks
Status
Current
Supersedes

This specification establishes the performance requirements and verifications for electric power subsystems (EPS) for aerospace vehicles, including aircraft, helicopters, and missiles.

DEFSTAN 00-970(PT0)/9(2012) : 2012 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/17(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/7(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/14(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/12(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/8(2011) : 2011 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
DEFSTAN 00-970(PT0)/16(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS
MIL-HDBK-516 Revision C:2014 Airworthiness Certification Criteria

MIL-PRF-8565 Revision K:2001 Batteries, Storage, Aircraft General Specification for
MIL-STD-704 Revision F:2004 Aircraft Electric Power Characteristics
MIL-PRF-29595 Revision A:2011 Batteries, Lithium, Rechargeable, Aircraft, General Specification for
MIL-PRF-81757 Revision D:1999 Batteries and Cells, Storage, Nickel-Cadmium, Aircraft General Specification for
MIL-HDBK-502 Revision A:2013 Product Support Analysis
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-E-85583 Revision A:1987 ELECTRIC POWER GENERATING CHANNEL, VARIABLE INPUT SPEED, ALTERNATING CURRENT, 400 HZ, AIRCRAFT, GENERAL SPECIFICATION FOR
STANAG 3109 : 2014 SYMBOL MARKING OF AIRCRAFT SERVICING AND SAFETY/HAZARDS POINTS
MIL-PRF-21480 Revision B:2010 Generator System, Electric Power, 400 Hertz, Alternating Current, Aircraft; General Specification for
JSSG-2010 Base Document:1998 Crew Systems
IEEE/ISO/IEC 12207-2008 ISO/IEC/IEEE International Standard - Systems and software engineering -- Software life cycle processes
MIL-E-7016 Revision F:1976 Electric Load and Power Source Capacity, Aircraft, Analysis of
MIL-PRF-7032 Revision H:2010 Inverters, Aircraft, General Specification for
MIL-DTL-6162 Revision C:2000 Generators and Starter-Generators, Electrical Direct Current, Nominal 30 Volts, Aircraft General Specification for
MIL-STD-464 Revision C:2010 Electromagnetic Environmental Effects Requirements for Systems
MIL-STD-1796 Revision A:2011 Avionics Integrity Program (AVIP)
MIL C 7115 : F CONVERTER, AIRCRAFT, GENERAL SPECIFICATION FOR
MIL-STD-882 Revision E:2012 System Safety
MIL-STD-461 Revision G:2015 Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment
MIL-HDBK-2165 Base Document:1995 Testability Program for Systems and Equipments
MIL-HDBK-1799 Base Document:1997 Survivability, Aeronautical Systems (For Combat Mission Effectiveness)(S/S by JSSG-2000 and JSSG-2001)
MIL-PRF-24021 Revision K:1998 Electric Power Monitors, External, Aircraft
SAE AS50881F Wiring Aerospace Vehicle
JSSG-2009 Revision A:2013 Air Vehicle Subsystems
STANAG 7073 : 2017 CONNECTORS FOR AIRCRAFT ELECTRICAL SERVICING POWER
SAE AS35061A CONNECTOR, RECEPTACLE EXTERNAL ELECTRIC POWER, AIRCRAFT, 28 VOLT DC OPERATING POWER
MIL-HDBK-470 Revision A:1997 Designing and Developing Maintainable Products and Systems, Volume I
MIL-STD-2161 Revision C:2014 Paint Schemes and Exterior Markings for U.S. Navy and Marine Corps Aircraft
MS17793 Revision B:1974 Schematic Wiring Diagram (External AC Power Connector, Aircraft) (No S/S Document)
MIL-STD-1798 Revision C:2013 Mechanical Equipment and Subsystems Integrity Program
MIL-STD-1553 Revision B:1978 Digital Time Division Command/Response Multiplex Data Bus
SAE AIR4845 THE FMECA PROCESS IN THE CONCURRENT ENGINEERING (CE) ENVIRONMENT

Access your standards online with a subscription

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.

€16.67
Excluding VAT