MIL-C-14806 Revision A:1969
Current
The latest, up-to-date edition.
COATING, REFLECTION REDUCING, FOR INSTRUMENT COVER GLASSES AND LIGHTING WEDGES
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. QUALITY ASSURANCE PROVISIONS
5. PREPARATION FOR DELIVERY
6. NOTES
Defines reflection reducing coatings applied to substrate material used as instrument cover for optical elements.
Committee |
FSC 6650
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DevelopmentNote |
A NOTICE 1 - Notice of Validation. A NOTICE 2 - Notice of Inactivation for New Design. A NOTICE 3 - Notice of Validation but remains Inactive for New Design. (11/2013)
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DocumentType |
Standard
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Pages |
17
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PublisherName |
US Military Specs/Standards/Handbooks
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Status |
Current
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SAE ARP 6161 : 2011 | FLIGHT COMPARTMENT GLARE |
MIL-I-27304 Revision E:1977 | INDICATOR, RATE OF FLOW |
MIL-D-81641 Base Document:1972 | Display, Head-up, General Specification for |
MIL-A-81852 Revision A:1986 | ALTIMETER-ENCODER AAU-32/A |
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MIL-A-81851 Revision B:1986 | ALTIMETER AAU-31/A |
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MIL-I-21735 Revision A:1969 | Indicator, Airspeed and Mach Number, Pitot Static, 60 to 650 Knots |
MIL I 38135 : B (3) | INDICATOR, INDICATED AIRSPEED AVU 19/A STANDBY |
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MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
MIL O 38338 : C (1) | OIL QUANTITY GAGING SYSTEM, CONTINUOUS TRANSISTORIZED NUCLEONIC, GENERAL SPECIFICATION FOR |
MIL-L-27160 Revision C:1972 | LIGHTING, INSTRUMENT, INTEGRAL, WHITE GENERAL SPECIFICATION FOR |
MIL A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
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MIL-A-81605 Revision D:1984 | ALTIMETER SET, ELECTRONIC AN/APN-194(V) |
MIL-I-83245 Revision A:1994 | INDICATOR SET, OIL PRESSURE A/A24J-17 |
MIL-I-83262 Revision B:1977 | INDICATOR, TEMPERATURE, THERMOCOUPLE HERMETICALLY SEALED, GENERAL SPECIFICATION FOR |
MIL-I-27673 Revision C:1993 | INDICATOR, TRUE AIRSPEED AVU-15/A |
MIL-I-27623 Revision C:1972 | INDICATOR, ATTITUDE, REMOTE STANDBY, 2 INCH |
MIL-I-83117 Revision B:1975 | INDICATOR, ANGLE OF ATTACK |
MIL-I-5415 Revision C:1987 | INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR |
MIL-I-27619 Revision G:1974 | INDICATORS, ATTITUDE DIRECTOR |
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MIL-I-27667 Revision C:1990 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, EHU-16/A MULTIFUNCTION -70 DEGREES TO +150 DEGREES C |
MIL-I-23832 Revision A:1980 | Indicator, Tachometer, Triple Pointer, Helicopter |
MIL-I-81049 Revision A:1972 | INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, VOLTAGE COMPENSATED, MULTIFUNCTION |
MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
MIL-V-85603 Base Document:1989 | VOLTMETER, DC, AIRCRAFT, DIGITAL DISPLAY GENERAL SPECIFICATION FOR |
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MIL-STD-1293 Base Document:1979 | ELECTRO-MECHANICAL COMMAND INSTRUMENT SYSTEM FOR ROTARY WING AIRCRAFT |
RE.AERO 79030 : 1991 | GUIDE FOR RECONFIGURATING KEYBOARD DESIGN |
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MIL-E-12397 Revision B:1954 | ERASER, RUBBER-PUMICE (FOR TESTING COATED OPTICAL ELEMENTS) |
MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
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