共找到 902 条与 航空仪表 相关的标准,共 61 页
MS33636B, dated 24 November 1970, has been reviewed and determined to be current.
MEASUREMENT, UNITS OF, FOR AIRCRAFT INSTRUMENTS
MIL-I-21735A(AS), dated 31 January 1969, hasbeenreviewed and determine dtobe current
INDICATOR, AIRSPEED AND MACH NUMBER, PITOT STATIC, 60 TO 650 KNOTS
This specification covers design and performance requirements for light we ight , small and low resolution electrochemical elapsed time indicators .
INDICATOR, ELAPSED TIME, ELECTROCHEMICAL
INDICATOR, ELECTRICAL, WHEELS& FLAPS POSITION
INDICATOR, ELECTRICAL, WHEELS& FLAPS POSITION
THE LENGTH OF THE COPPER COLUMN RELATIVE TO THE GRADUATED TIME SCALE OF THE INDICATING CELL, INDICATES TOTAL
INDICATOR, ELAPSED TIME, ELECTROCHEMICAL (COPPER) H5V 50/2400 HZ AC OR 28V DC
This specification covers one type of servo operated, sensitive Mach number indicator, designated Type ME-5.
INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.0, TYPE ME-5
THIS STANDARD ESTABLISHES THE OVER-ALL DIMENSIONS AND DETAIL ENGINEERING REQUIREMENTS FOR MINATURE SIZE ELAPSED TIME INDICATORS.
INDICATOR, ELAPSED TIME, ELECTROCHEMICAL, (MERCURY) 115 VOLT AC, 50/2400 HERTZ, 28 VOLT DC OR 5 VOLT DC
MIL-I-81683A(AS), dated 17 September 1979, has been reviewed and determined to be current
INDICATOR, ATTITUDE REFERENCE SELF-CONTAINED, 3-INCH, ID-1791/A
This specification covers the requirements for one type of precision L pressure, -1000 +80,000 feet, integrally lighted altimeter, designated.
ALTIMETER, PRESSURE AAU-7/A
MIL-I-5419B,dated 1969, has been revied and determinded to be current.
INDICATOR, INDICATED AIRSPEED, PITOT-STATIC, MAXIMUM ALLOWABLE SPEED, 50-650 KNOTS
MS28067C, dated 1 November 1971, has been reviewed and determined to be current.
INDICATOR, ANGLE OF ATTACK, 1-7/8 DIA., 28 VOLT D.C.
MIL-I-23252B(AS), dated 3 February 1981, has been reviewed and determined to be current.
INDICATOR, PRESSURE
INDICATOR, AIRSPEED AND MACH NUMBER, PITOT STATIC 60 TO 650 KNOTS
INDICATOR, AIRSPEED AND MACH NUMBER, PITOT STATIC 60 TO 650 KNOTS
This specification covers the requirements, examinations and tests for the target holding mechanism assembly of the Target Holding Mechanism/Tank Gunnery (THM/TG) unit used as a part of the Remote Target System (RETS) (see 6.1).
INDICATOR, POSITION, WING FLAP
This specification is approved for use by all Departments and Agencies of the Department of Defense.
INDICATOR, RATE OF FLOW, FUEL, TYPE A-19
This amendment Forms a part of Mlli tary Specifica€ion MIL-L-18856B dated 27 -October 1969, and is approved for use by all Departments and Agencies of the Department of Defense.
INDICATOR, ANGLE OF ATTACK, 28 VDC MS28062 AND MS28067
This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense. All products listed herein have been qualified under the requirements for the product as specified in the latest effective issue of the applicable specification. This list is subject to change without notice
INDICATOR, VERTICAL SPEED, 0-6000 FPM 2-INCH
This amendment forms a part of MIL-I-25950B (USAF), dated 29 Nov 1967, and is approved for use within the Department of the Air Force and is available for use by all Departments and Agencies of the Department of Defense.
INDICATOR, PRESSURE, OIL 0-100 PSI
This specification covers the requirements for three types of integrally lighted indicators for indicating the flow rate of engine fuel in pounds per hour (pph) for three specIfIc flow ranges. The indicator is a hermetically sealed synchro/servo receiver
INDICATOR, RATE OF FLOW, FUEL
“hie specification e s t a b l i s h e s the production and acceptance requirements for the P r o j e c t i l e , 20 mi1.1l.meter (niin) Semi-Armor P i e r c i n g , High Explosive Incendiary P r o j e c t i l e (SAPHEI), PGU-28/B, r e f e r r e d h e r e i n as the “pr oj ec t i le . ”
PROJECTILE, 20 MILLIMETER, SEMI-ARMOR PIERCING, HIGH EXPLOSIVE INCENDIARY, PGU-28/B
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