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MODUK - DEF STAN 00-970: PT 1: SEC 6

Design and Airworthiness Requirements for Service Aircraft - Part 1 Fixed Wing - Section 6 - Equipment

inactive
Organization: MODUK
Publication Date: 1 December 2012
Status: inactive
Page Count: 44
scope:

This leaflet specifies the characteristics of electrical power supplied to the terminals of airborne equipment and defines limits for those aspects of utilisation equipment that may adversely affect the characteristics of electrical power supplied to other equipment.

The characteristics specified in this leaflet are based on the following assumptions:

(a) the system capacity is not less than 1.5 kW;

(b) the normal loading on the system is between 5% and 85% of the power supply system capacity;

(c) the load balance in A.C. systems is such that under steady state conditions the maximum difference in line current on any power source does not exceed 15% of the rated current of that power source; and

(d) the power factor in A.C. systems is between 0.8 lag and 1.0 at loads between 30% and 85% of rated load, and between 0.5 lag and 1.0 at loads between 5 % and 30% of rated load.

Document History

September 19, 2016
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 6: Equipment
INTRODUCTION This Clause specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 6: Equipment
PREFACE (a) This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military...
January 30, 2015
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 6: Equipment
PREFACE (a) This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military...
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 6: Equipment
INTRODUCTION This Clause specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
January 10, 2014
Design and Airworthiness Requirements for Service Aircraft - Part 1: Fixed Wing - Section 6: Equipment
INTRODUCTION This Clause specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 6: Equipment
A description is not available for this item.
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 6 - Equipment
PREFACE (a) This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military...
DEF STAN 00-970: PT 1: SEC 6
December 1, 2012
Design and Airworthiness Requirements for Service Aircraft - Part 1 Fixed Wing - Section 6 - Equipment
This leaflet specifies the characteristics of electrical power supplied to the terminals of airborne equipment and defines limits for those aspects of utilisation equipment that may adversely affect...
Design and Airworthiness Requirements for Service Aircraft - Part 1 Fixed Wing - Section 6 - Equipment
PREFACE (a) This Part of the Defence Standard provides requirements for Airworthiness and Design Certification for the design, development and testing of Fixed Wing Aircraft for UK Military...
October 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 6 - Equipment
PREFACE a. This Part of the Defence Standard provides requirements and guidance for the design of aircraft to meet the airworthiness requirements for UK military operation. The requirements stated...
January 31, 2011
Design and Airworthiness Requirements for Service Aircraft Part 1 Fixed Wing Section 6 - Equipment
INTRODUCTION This chapter specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
February 5, 2010
Design and Airworthiness Requirements for Service Aircraft Part 1 – Fixed Wing Section 6 - Equipment
INTRODUCTION This chapter specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
February 5, 2010
Design and Airworthiness Requirements for Service Aircraft Part 1 – Fixed Wing Section 6
INTRODUCTION This chapter specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
January 31, 2007
Design and Airworthiness Requirements for Service Aircraft Part 1 Section 6 - Equipment
INTRODUCTION This chapter specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
December 1, 1999
Design and Airworthiness Requirements for Service Aircraft Part 1: Fixed Wing Section 6: Equipment
INTRODUCTION This chapter specifies the requirements relating to equipment and systems embodied on any aircraft. These requirements are to be used where there are no aircraft specific requirements...
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