• Shopping Cart
    There are no items in your cart

MIL-E-7016 Revision F:1976

Current

Current

The latest, up-to-date edition.

Electric Load and Power Source Capacity, Aircraft, Analysis of

Available format(s)

PDF

Published date

20-07-1976

€16.67
Excluding VAT

Prepares (ac) and (dc) electric load power source capacity analyses for aircraft.

DevelopmentNote
F NOTICE 1 - Notice of Validation. (12/2009) F NOTICE 2 - Notice of Validation. (09/2014)
DocumentType
Standard
Pages
52
ProductNote
NEW CHILD NOT 3 2019 IS NOW ADDED
PublisherName
US Military Specs/Standards/Handbooks
Status
Current

This specification covers the methods and requirements for preparing alternating current (ac) and direct current (dc) electric load and power source analyses for aircraft.

MIL-D-8684 Revision B:1959 Data and Tests, Engineering, Contact Requirements for Air Launched Guided Missile Systems (No S/S Document)
PREN 3830 : 200P1 AEROSPACE SERIES - ELECTRICAL SYSTEM - LOAD ANALYSIS
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)/11(2013) : 2013 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)/10(2013) : 2013 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
AFGS-87219 Revision B:2012 Electrical Power Systems, Aircraft
SAE ARP4404C Aircraft Electrical Installations
MIL-D-8685 Revision B:1967 Data and Tests, Engineering, Contract Requirements for Guided Missile Target Systems (No S/S Document)
MIL-HDBK-516 Revision C:2014 Airworthiness Certification Criteria
MIL-STD-1822 Revision A:2013 Nuclear Compatibility Certification of Nuclear Weapon Systems, Subsystems and Support Equipment
MIL-D-23222 Revision A:1971 Demonstration Requirements for Helicopters
DIN EN 3830:1995-08 (Draft) AEROSPACE SERIES - ELECTRICAL SYSTEM - LOAD ANALYSIS
JSSG-2009 Revision A:2013 Air Vehicle Subsystems
DIN 29571-3:1990-10 AEROSPACE - ELECTRICAL EQUIPMENT - ANALYSIS OF LOAD AND POWER SOURCE CAPACITY
ADS-63-SP : 2001 AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS
MIL-E-25499 Revision C:1970 Electrical System, Aircraft, Design and Installation of, General Requirements for (No S/S Document)
MIL-T-18232 Revision B:1968 Targets, Aerial, Powered, Design and Construction of General Specification for (No S/S Document)
SAE ARP4729A Document for 270 Voltage Direct Current (270 V DC) System
MIL-D-8708 Revision C:1991 Demonstration: Aircraft Weapon Systems, General Specification for
MIL-STD-1606 Revision A:1983 TECHNICAL INFORMATION REQUIREMENTS FOR AIR LAUNCHED GUIDED MISSILE PROPOSALS (NO S/S DOCUMENT)
ADS-65-HDBK : 2004 AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIRWORTHINESS QUALIFICATION AND VERIFICATION GUIDANCE FOR ELECTRO-OPTICAL AND SENSOR SYSTEMS

MIL-STD-704 Revision F:2004 Aircraft Electric Power Characteristics
MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)

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