MIL-C-14806 Revision A:1969
Current
Current
The latest, up-to-date edition.
COATING, REFLECTION REDUCING, FOR INSTRUMENT COVER GLASSES AND LIGHTING WEDGES
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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
|
| Pages |
17
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| PublisherName |
US Military Specs/Standards/Handbooks
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| Status |
Current
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| MIL-I-18856 Revision B:1969 | INDICATOR, ANGLE OF ATTACK, 28V DC MS28062 AND MS28067 |
| MIL-T-38034 Revision E:1970 | TIMER, FIRE CONTROL, BOMBING, DUAL |
| MIL-C-87979 Base Document:1987 | CLOCK, AIRCRAFT, ELECTRONIC |
| MIL-L-25467 Revision D:1977 | LIGHTING, INTEGRAL, RED, AIRCRAFT INSTRUMENT, GENERAL SPECIFICATION FOR |
| MIL-I-83152 Revision B:1974 | INDICATOR, INDICATED-AIRSPEED AVU-22/A (INDICATOR-TRANSDUCER) |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-T-38473 Revision A:1972 | TIMER, PRECISION, BOMBING, 0 - 30 MINUTES |
| MIL-A-38140 Revision B:1977 | ALTIMETER, PRESSURE AAU-16/A |
| MIL-PRF-83419 Revision F:2016 | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-I-38338 Revision D:1991 | INDICATOR, OIL QUANTITY, CONTINUOUS TRANSMISSION, NUCLEONIC |
| MIL-I-27196 Revision C:1988 | INDICATOR, VERTICAL VELOCITY AAU-9/A, INTEGRALLY LIGHTED |
| MIL-DTL-25949 Revision F:1995 | ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, INTEGRALLY LIGHTED |
| MIL-PRF-27197 Revision F:2017 | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL-PRF-38135 Revision D:2014 | INDICATOR, INDICATED AIRSPEED AVU-19A, STANDBY |
| 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 |
| MIL-I-22075 Revision C:1984 | Indicator, Bearing-Distance-Heading ID-663D/U |
| MIL-A-81851 Revision B:1986 | ALTIMETER AAU-31/A |
| SAE ARP 798 : 2017 | DESIGN CRITERIA FOR WHITE INCANDESCENT LIGHTED AEROSPACE INSTRUMENTS |
| MIL-DTL-83361 Revision B:2007 | INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A |
| 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 |
| MIL-I-58067 Revision A:1977 | INDICATOR, VERTICAL VELOCITY, RAPID RESPONSE ACCELERATION SENSITIVE, GENERAL SPECIFICATION FOR |
| MIL-I-22126 Revision B:1972 | INDICATOR, TORQUEMETER, ENGINE, TURBOPROP |
| 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 |
| MIL-C-81774 Revision A:1973 | CONTROL PANEL, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| MIL-G-23081 Revision C:1972 | Gyroscope Indicator System, Vertical |
| MIL A 87211 : NOTICE 1 | AIR DATA SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD ENES, WRIGHT PATTERSON, AFB OH 45433 6503 |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-A-83212 Revision A:1976 | ALTIMETER, PRESSURE AAU-27/A |
| MIL-G-26988 Revision C:1971 | GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR |
| 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 |
| MIL A 25949 : E (2) | ACCELEROMETER, AIRCRAFT RANGE -5 TO PLUS 1OG UNITS, INTEGRALLY LIGHTED |
| 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 |
| MIL I 83361 : (4) | INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI |
| MIL-STD-1293 Base Document:1979 | ELECTRO-MECHANICAL COMMAND INSTRUMENT SYSTEM FOR ROTARY WING AIRCRAFT |
| RE.AERO 79030 : 1991 | GUIDE FOR RECONFIGURATING KEYBOARD DESIGN |
| MIL O 13830 : A | OPTICAL COMPONENT FOR FIRE CONTROL INSTRUMENTS, GENERAL SPECIFICATION GOVERNING THE MANUFACTURE, ASSEMBLY AND INSPECTION OF |
| MIL-STD-1241 Revision A:1967 | Optical Terms and Definitions |
| 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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