MIL-L-6503 Revision H:1975
Current
The latest, up-to-date edition.
Lighting Equipment, Aircraft, General Specification for Installation of
02-04-1975
Outlines requirements for installation of interior and exterior aircraft lighting.
| DevelopmentNote |
INACTIVE FOR NEW DESIGN 25/3/96
|
| DocumentType |
Standard
|
| Pages |
43
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers the requirements for the installation of exterior and interior aircraft lighting, except instrument lighting and aircrew station visual signals.
| MIL-STD-203 Revision G:1991 | Aircrew Station Controls and Displays: Location, Arrangement and Actuation of, for Fixed Wing Aircraft |
| JSSG-2010-5 Base Document:1998 | Crew Systems Aircraft Lighting Handbook |
| 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)/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)/12(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)/13(2014) : 2014 | 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 |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| SAE ARP693D | Landing and Taxiing Lights - Design Criteria for Installation |
| MIL-L-85762 Revision A:1988 | LIGHTING, AIRCRAFT, INTERIOR, NIGHT VISION |
| SAE ARP5825A | Design Requirements and Test Procedures for Dual Mode Exterior Lights |
| SAE ARP6402A | LED Landing, Taxiing, Runway Turnoff, and Recognition Lights |
| SAE AIR1106B | Some Factors Affecting Visibility of Aircraft Navigation and Anticollision Lights |
| MIL R 6749 : 0 | RHEOSTATS: AIRCRAFT POWER |
| MS25338 Revision D:1986 | LAMP, INCANDESCENT-SINGLE CONTACT BAYONET CANDELABRA, GG-12A1 BULB (S/S BY MIL-L-6363/1) |
| AN3119 Revision 3:2009 | Gasket - Common, Tail Position Light |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MS25237 Revision D:1978 | Lamp, Incandescent, Single Contact Midget Flanged Base (T-1-3/4 Bulb) (S/Sby MIL-L-6363/8) |
| AN 3040 : 0005 | COVER - CIRCULAR FORMATION LIGHT |
| MS25241 Revision E:1972 | Lamp, Incandescent, Par-46 Bulb, Screw Terminal Base, Landing |
| AN887 Revision 2:2006 | Gasket-Circular Formation Light Cover |
| AN3177 Revision 7:2006 | Light Assembly, Top and Bottom Fuselage (Two Lamps) |
| MS25239 Revision A:1962 | Lamp, Incandescent - Par-36 Bulb, Screw Terminal Base, Signaling (ASG) |
| MIL L 25866 : B | LIGHT, EMERGENCY EXIT, AIRCRAFT LEU AND 1-A |
| MS35478 Revision K:1977 | LAMP, INCANDESCENT, S-8 BULB, SINGLE CONTACT, BAYONET CANDELABRA BASE (S/S BY A-A-52463 OR MIL-L-6363/12) |
| MIL-C-25050 Revision A:1963 | Colors, Aeronautical Lights and Lighting Equipment, General Specification for (S/S by SAE-AS25050) |
| MIL-E-6051 Revision D:1967 | Electromagnetic Compatibility Requirements, Systems (S/S by MIL-STD-464) |
| MS25309 Revision D:1973 | LAMP, INCANDESCENT SINGLE CONTACT BAYONET CANDELABRA, GG-10 BULB (S/S BY MIL-L-6363/2) |
| MIL P 7788 : F | PANEL, INFORMATION INTEGRALLY ILLUMINATED |
| MS15570 Revision F:1986 | LAMP, INCANDESCENT, G-6 BULB, SINGLE CONTACT, BAYONET CANDELABRA BASE (S/S BY A-A-52463) |
| MIL-STD-411 Revision F:1997 | Aircrew Station Alerting Systems |
| MIL-E-25499 Revision C:1970 | Electrical System, Aircraft, Design and Installation of, General Requirements for (No S/S Document) |
| MS25235 Revision D:1985 | LAMP, INCANDESCENT, SINGLE-CONTACT BAYONET CANDELABRA BASE, S-11 BULB (S/S BY MIL-L-6363/13) |
| MS 17245 : E | LIGHT, COCKPIT UTILITY |
| AN904 Revision 2:2008 | Gasket and Upward Recognition Light Cover |
| MS25027 Revision F:1992 | LIGHT ASSEMBLY, COCKPIT, FIXED (S/S BY SAE-AS25027) |
| MS25358 Revision C:1967 | Light, Dome, Cabin-Red and White |
| MIL-F-26301 Revision H:2014 | Flasher, Solid State, Aircraft Navigational Light, General Specification for |
| MS35480 Revision B:1972 | LAMP, INCANDESCENT, R-12 BULB, SINGLE CONTACT, BAYONET CANDELABRA BASE (S/S BY A-A-52463) |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MS25215 Base Document:1957 | Light Assembly, Upward Recognition |
| MIL-L-81174 Revision A:1993 | Lights, Landing, Aircraft, Retractable |
| MS24513 Revision F:1990 | Lamp, Incandescent, Single Contact Bayonet Indexing Candelabra, GG-12B1 Bulb (S/S by MIL-DTL-6363/3) |
| MS25331 Revision C:1985 | Light Assembly, Press to Test Indicator |
| MIL R 22 : C | RESISTOR VARIABLE (WIREWOUND POWER TYPE) GENERAL SPECIFICATION FOR |
| AN3042 Revision 7:1992 | Cover-Position Light |
| MIL S 9419 : E | SWITCH, TOGGLE, MOMENTARY, FOUR-POSITION ON, CENTER OFF, GENERAL SPECIFICATION FOR |
| MS24474 Revision C:1984 | LIGHT ASSEMBLY, TAXI (PAR 46 BULB) (NO S/S DOCUMENT) |
| MS25069 Revision C:1977 | LAMP, INCANDESCENT, SINGLE CONTACT, MINIATURE BAYONET BASE, T-4-1/2 BULB (NO S/S DOCUMENT) |
| MIL-L-21652 Revision A:1964 | Light, Beacon, Anticollision, Aircraft, General Specification for |
| MIL-STD-462 Revision D:1993 | MEASUREMENT OF ELECTROMAGNTIC INTERFERENCE CHARACTERISTICS (S/S BY MIL-STD-461) |
| MS28916 Base Document:1964 | Light, Cabin Dome, Aircraft |
| MIL L 6484 : C | LIGHT, COCKPIT UTILITY, AIRCRAFT GENERAL SPECIFICATION FOR |
| AN899 Revision 2:1955 | GASKET, FUSELAGE LIGHT - COVER SCREW (S/S BY SAE-AS8991) |
| MIL-B-5087 Revision B:1964 | Bonding, Electrical, and Lightning Protection, for Aerospace Systems (S/S by MIL-STD-464) |
| MS25010 Revision F:1974 | Light, Panel - Plastic Plate Lighting |
| MIL-W-5088 Revision L:1991 | Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881) |
| MS25216 Revision C:2011 | Cover, Top and Bottom Fuselage Lights |
| MS25231 Revision G:2004 | Lamps, Incandescent, Center Contact, Miniature Bayonet Base (T-3-1/4 Bulb) |
| MIL-E-7080 Revision B:1962 | Electric Equipment, Aircraft, Selection and Installation of (S/S by MIL-STD-7080) |
| MS24517 Revision B:1970 | LAMP-INCANDESCENT, PAR-46 BULB, SCREW TERMINAL BASE, TAXIING (NO S/S DOCUMENT) |
| MS25219 Revision H:2010 | Light - Navigational and Warning, Aircraft |
| AN 3037 : 0006 | LIGHT ASSEMBLY, CABIN DOME |
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