BS G 217:1975
Current
The latest, up-to-date edition.
Specification for general requirements for cockpit lighting controllers
Hardcopy , PDF
English
31-01-1975
Foreword
Specification
Section one. General
1 Scope
2 References
3 Definitions
4 General construction
5 Nominal supply voltages
6 Preferred output ratings
7 Input supply characteristics
8 Output characteristics
9 Efficiency
10 Operation
11 Protection
12 Environmental conditions
Section two. Particular requirements
13 Arrangement and construction
14 Components
15 Electromagnetic interference
16 Magnetic influence
17 Temperature limitation
18 Bonding
19 Markings
Section three. Tests
20 General
21 Test conditions
22 Performance type tests
23 Environmental tests
24 Production acceptance tests
25 Production quality tests
Appendix
A Dust and sand test
Tables
1 Preferred voltages
2 Preferred output ratings
Figure
1 Measuring device for dust and sand test
Gives general design characteristics for lighting controllers to supply electric filament lamps used in aircraft instruments and for the illumination of panels, operating from nominal 28V d.c. and 115V a.c. 400 Hz aircraft supplies. Includes markings details, performance type tests, environmental tests, production acceptance tests, production quality tests and dust and sand test. Illustrates a measuring device for dust and sand test.
Committee |
ACE/6
|
DevelopmentNote |
Supersedes 73/35031 DC. (06/2005) Reviewed and confirmed by BSI, December 2012. (11/2012)
|
DocumentType |
Standard
|
Pages |
12
|
PublisherName |
British Standards Institution
|
Status |
Current
|
This British Standard specifies general design characteristics for lighting controllers to supply electric filament lamps used in aircraft instruments and for the illumination of panels, operating from nominal 28 V d.c. and 115 V a.c. 400 Hz aircraft supplies.
DEFSTAN 00-970(PT1)SEC6/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/14(2015) : 2015 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT7)SEC7/1(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
DEFSTAN 00-970(PT1)SEC6/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/4(2006) : 2006 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT A/C - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT7)SEC2/SUPP6/5(2015) : INTERIM | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SUPPLEMENT 6: EQUIPMENT (SUBPART F) |
DEFSTAN 00-970(PT7)SEC7/2(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
DEFSTAN 00-970(PT1)SEC6/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6 - EQUIPMENT |
DEFSTAN 00-970(PT7)SEC7/3(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 7: ROTORCRAFT - SECTION 7: INSTALLATIONS |
DEFSTAN 00-970(PT1)SEC6/6(2010) : 2010 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/5(2007) : 2007 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: COMBAT AIRCRAFT - SECTION 6: EQUIPMENT |
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT |
BS PD5686(1965) : LATEST | |
BS 3763:1964 | The International System of units (SI) |
BS 3G 100-2.2:1972 | Specification for general requirements for equipment for use in aircraft. All equipment Magnetic influence |
BS 3G 100-2.3.8:1972 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Salt mist |
BS 3G 100-2.3.2:1970 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Temperature-pressure requirements |
BS 4727(1971) : LATEST | |
BS 3G 100-2.1:1973 | Specification for general requirements for equipment for use in aircraft. All equipment Construction |
BS 350:2004 | Conversion factors for units |
BS 3G 100-2.3.1:1969 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Vibration |
BS 3G 100-2.3.7:1972 | Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Tropical exposure |
Access your standards online with a subscription
Features
-
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.