MIL-DTL-6363/14A
NOTES:
1.
Dimensions are in inches.
2.
Intended use - aircraft instrument, indicator and interior cockpit light assemblies
conforming to MS25027.
3.
For design feature purposes, this specification takes precedence over procurement
documents referenced herein.
4.
Qualification by similarity - Lamp M6363/14-1X is required to be fully qualified in
accordance with table I of MIL-DTL-6363. Refer to MIL-DTL-6363 for conditions and
data requirements for qualification.
REQUIREMENTS:
1.
Configuration and dimensions: See figure 1.
2.
Finish: Glass globe finish shall be as indicated in table I.
TABLE I. Part or identifying numbers (PIN) and operating characteristics.
Part or
Type
Bulb
Shock
Filament
MSCD
Average
±25%
Identifying
MIL-
Fin-
Test
Electrical Ratings
Style
Rated Lab
Number
DTL-
ish
Level
Volts
Amperes Watts
Life at DC
(±10%) (Max)
(PIN) 1/
6363
(G's)
(Nom)
Candelas
Hours
M6363/14-1X
I
Clear
90
28.0
0.30
9.24
C-2F
6
500
1/ Gas filled lamp.
3.
Lamp operating characteristics: When operated at rated voltage, the lamp operating
characteristics shall be as specified in table I.
4.
Coating adhesion: Not applicable.
High temperature: Applicable for qualification tests only (85°C/185F°).
5.
6.
Thermal shock: Applicable for qualification tests only. Use temperatures for Type I
lamps.
7.
Random vibration: Applicable for qualification tests only. See figure 2 for random
vibration curve.
8.
Shock: Applicable for qualification tests only. See table I for applicable "g" level.
9.
Humidity: Applicable for qualification tests only.
2
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