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BS 2G 100-2:1962

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

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Specification for general requirements for electrical equipment and indicating instruments for aircraft Environmental and operating conditions

Available format(s)

Hardcopy , PDF

Withdrawn date

08-02-2013

Language(s)

English

Published date

02-07-1962

US$283.91
Excluding Tax where applicable

201 Scope
202 Temperature and pressure variation
203 Equipment cooled by outside air
204 Climatic test conditions
205 Icing conditions
206 Temperature and pressure tests
207 Climatic tests
208 Tests for Climatic Class 1 equipment
     a. Combined humidity, temperature and pressure
         tests
     b. Tropical exposure tests
     c. Tests for resistance to fungus growth
209 Tests for Climatic Class 2 equipment
210 Ice formation test
211 Ice resistance tests
212 Hermetically sealed equipment
213 Leakage tests for hermetically sealed equipment
214 Waterproofness
215 Tests for waterproofness
     a. Spray test
     b. Drip test
216 Vibration conditions
217 Vibration regions
     a. Aeroplanes
     b. Rotorcraft
218 Vibration tests
     a. Characteristics of the vibration table
     b. Method of mounting for test
     c. Direction of vibration
     d. Resonance tests
     e. Endurance tests
     f. Tests for engine-mounted equipment
     g. Alternative tests for Grade A
219 Acceleration conditions
     a. Normal conditions
     b. Crash conditions
220 Acceleration tests
221 Explosion-proof equipment
222 Tests for explosion-proof equipment
223 Resistance to fire
224 Tests for fire resistance
225 Radio interference
226 Radio interference test
227 Magnetic interference
228 Measurement of compass safe distance
229 Insulation tests
Figures
1 Temperature and pressure Grade A
2 Temperature and pressure Grade B
3 Temperature and pressure Grade C
4 Ambient temperature and pressure of cooling air
5 Test cycle diagram for Climatic Class 1 equipment
6 Test cycle diagram for Climatic Class 2 equipment
7 Diagram illustrating typical test schedule for
     climatic Class 1 equipment
8 Test for ice formation
9 Test rig for drip test
10 Vibration Grade A
11 Vibration Grade B
12a Vibration Grade C.1
12b Vibration Grade C.2
13 Vibration - engine-mounted equipment
13a Diagram for apparatus for testing in explosive
     atmospheres
14 Acceptable limits of radio noise
15 Line stabilizing network for radio noise
     measurement
16 Test arrangement for radio noise measurement
17 Terminating unit for radio noise measurement
18 Limit of impedance/frequency characteristics of
     coupling capacitor used in line stabilizing network
Appendices
A Test schedule for Climatic Class 1 and Class 2
     equipment
B Apparatus and method of test for combined humidity,
     temperature and pressure tests
C Summary of characteristics of radio noise measuring
     sets for the frequency ranges 50 to 150 kc/s and
     150 to 600 Mc/s
Alphabetical index

Modifications to the section pending a major revision.

Committee
ACE/6
DevelopmentNote
Inactive for the new design. (11/2009)
DocumentType
Standard
Pages
44
PublisherName
British Standards Institution
Status
Withdrawn
SupersededBy

BS G 189:1964 Specification for Tersil type electrical cables for aircraft
BS G 209:1970 Specification for transformer rectifier units
DEFSTAN 00-970(PT1)SEC6/15(2015) : 2015 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
DEFSTAN 93-35/2(2004) : 2004 EXPANDED POLYSTYRENE MOULDINGS, TYPE GP AND QX
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(PT1)SEC6/13(2014) : 2014 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
BS 2G 147-2:1966 Specification for a.c. motors for aircraft Three-phase variable frequency squirrel-cage induction motors
BS G 246:1991 Specification for cable ties for installation under controlled tension on aircraft electric cable harnesses
BS 2G 124-1:1966 Specification for a.c. generators for aircraft Constant frequency
BS G 208:1970 Specification for general requirements for electrical relays up to 10 A rating
BS G 218-1:1975 Specification for proximity switches for aircraft General requirements
BS G 195:1966 Specification for Minyvin type electric cables for aircraft
BS 2G 132:1981 Specification for general requirements for electromagnetically operated contactors for aircraft
BS G 192:1965 Specification for Efglas type electric cables with copper conductors for aircraft
BS G 200:1967 Specification for miniature lever-operated manual switches
BS 2G 127:1967 Specification for power and current transformers for use in aircraft electrical power supply systems
DEFSTAN 00-970(PT1)SEC6/16(2016) : 2016 DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 1: FIXED WING - SECTION 6: EQUIPMENT
BS G 224:1978 Specification for lever-operated manual switches for aircraft
BS 2G 147-1:1966 Specification for a.c. motors for aircraft Three-phase constant frequency squirrel-cage induction motors
BS 2G 143:1965 Specification for a.c. and d.c. rotary and linear actuators for aircraft
BS 2G 196:1971 Specification for static invertors
BS 2G 134:1970 Specification for d.c. generators
BS 2G 146:1966 Specification for d.c. motors for aircraft
BS 3G 100-2.3.5:1972 Specification for general requirements for equipment for use in aircraft. All equipment. Environmental conditions Explosion-proofness
BS G 193:1966 Specification for aircraft lampholders
BS G 190:1964 Specification for cabin altimeters for aircraft

BS G 118:1949 Specification for aircraft magnetic compass, direct-reading
BS 727:1954 Characteristics and performance of apparatus for measurement of radio interference
BS CP1012(1961) : LATEST THE ABATEMENT AND MEASUREMENT OF RADIO INTERFERENCE FROM ELECTRICAL INSTALLATIONS IN CIVIL AIRCRAFT
BS G 177:1961 Specification for Nyvin type electrical cables for aircraft

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