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Flight Instruments Mil-Specs - FSC 661

A-A-56024 - Foil, Titanium

The commercial item description covers one kind of titanium foil. The foil is intended for use in fabrication of electrical equipment for one submunition system.

A-A-58055 - Indicator, Attitude, Three Inch, Solid State Self-Contained

This commercial item description covers a 3-inch, solid state, self-contained attitude indicator intended to provide a standby attitude display for transport aircraft.

AFGS-87211 - Air Data Systems

AFGS-87213 - Displays, Airborne, Electronically/Optically Generated (Refer To Mil-Hdbk-87213)

This specification establishes the development requirements for electronically generated displays for airborne use, including head-up displays (HUD's), helmet-mounted displays (HMD's) and multi-function displays (MFD's) including displays for TV, FLIR, and radar video, and the associated electronci display generation equipment.

AFGS-87242 - Flight Control System General Specification For (S/S By Jssg-2008)

This specification delineates the operational needs and general parameters for a physical product family identified as Flight Control Systems (FCS) for piloted aerospace vehicles.

AN5530 - Indicator, Electric Tachometer, Aircraft

AN5735 - Indicator & Directional Gyro

AN5736 - Indicator & Gyro Horizon

AN5744 - Inclinator & Aircraft, Ball Style

AN5745 - Accelerometer & Aircraft

AN5760 - Altimeter & Pressure (Use Ms28044)

AN5780 - Indicator - Electrical, Wheels And Flap Position

AN5785 - Transmitter-Electrical, Wheels And Flap Position

AN5786 - Transmitter - Position, 28 Volts Dc

AN5787 - Transmitter - Position, Gearless

AN5805 - Tube & Single Throat Power Venturi

AN5806 - Tube & Double Throat Power Venturi For Turn And Bank Indicator

AN5807 - Tube & Double Throat Power Venturi For Directional Gyro And Gyro Horizon Indicators

AN5810 - Tube, Pitot&Static, Unheated, Monoplane Type

AN5811 - Tube, Pitot, Electrically Heated, "L" Shaped, Inverted

AN5812 - Tube, Pitot, Electrically Heated, "L" Shaped

AN5813 - Tube - Pitot, Electrically Heated (S/S By Sae-As5813)

AN5814 - Tube, Pitot Static, L Shaped, Electrically Heated

AN5815 - Tube & Pitot&Static, Unheated Biplane Type

AN5816 - Tube Pitot Static, Straight, Electrically Heated

AN5819 - Indicator - Electric Turn And Bank (S/S By Ms28069)

AN5820 - Indicator, Bank And Turn

AN5821 - Filter & Turn And Bank Indicator Air

AN5823 - Card - Compass Correction (S/S By Sae-As5823)

AN5825 - Indicator - Rate Of Climb (Use 28049)

AN5839 - Indicator, Position, Landing Gear, Individual Indicating, 28-Volt Dc (Use Ms27403)

AN5860 - Indicator & Airspeed, Pitot Static, 10&150 Knots (Use Ms28045)

AN5861 - Indicator & Airspeed, Pitot Static, 40&400 Knots

AN5862 - Indicator & Airspeed, Pitot Static, Sensitive, 50&650 Knots (Use Ms28047)

AN5863 - Indicator & Airspeed, Pitot Static, Maximum Allowable Speed, 50&650 Knots (Use Ms28048)

AND10400 - Numerals And Letters - Aircraft Instrument Dial, Standard Form Of (S/S By Ms33558)

MIL-A-18105 - Amplifier, Electronic Control, E10100, For Am-632/Asb-1A

MIL-A-19679 - Altimeter, Pressure, Counter-Pointer

MIL-A-22145 - Accelerometer Group, Counting,(Ms25447 And Ms25448) (S/S By Sae-As22145)

This specification covers the design and performance requirements for a single axis, four load-factor level counting accelermeter group referred to hereafter as "equipment".

MIL-A-22858 - Attitude Indicating System, Remote, Standby, Two Inch

This specification covers design requirements and performance requirements for procurement of a Two-Inch Remote Standby Attitude Indicating System.

MIL-A-23395 - Altimeter, Pressure, Counter-Pointer, Type Mc-3 And Mc-4

MIL-A-23728 - Accelerometer, Aircraft Mx-2911/Ajb-3A

MIL-A-25522 - Altimeter, Pressure, Drum, Pointer, Range Minus 1000 To Plus 80,000 Feet, Type Md-1 (No Superseding Document)

MIL-A-25719 - Accelerometer, Mechanical, Aircraft, Pilot'S Warning, Type Ma-1

This specification covers one type of 1.87 inch dial, -2 to +4 g range accelerometer, designated Type MA-1.

MIL-A-25915 - Accelerometer, Aircraft, Pilot'S Warning, Type Ma-2

This specification covers one type of 1-7/8 inch dial, -2 to +8 g range accelerometer, designated Type MA-2.

MIL-A-26353 - Antenna System For Receiver, Radio An-Arr-47 Design Requirements For

MIL-A-26360 - Amplifier, Electrical Control Asu-3/A

This specification covers the requirements for one type of remote attitude amplifier, designated ASU-3/A.

MIL-A-27195 - Accelerometer, Aircraft, Mechanical Abu-6/A

This specification covers one type of integrally lighted 1.875 inch dial, -2 to +8g range accelerometer designated ABU-6/A.

MIL-A-27198 - Altimeter, Pressure Aau-7/A

This specification covers the requirements for one type of precision pressure,-1000 +80,000 feet, integrally lighted altimeter, designated.

MIL-A-27229 - Altimeter, Pressure Aau-8/A

MIL-A-27261 - Accelerometer, Aircraft

This specification covers integrally lighted, 1-7/8-inch dial aircraft accelerometers having a range of -2 to +4g's.

MIL-A-27270 - Alarm-Monitor Sdu-8-A, Servo Failure

MIL-A-27271 - Alarm-Monitor Sdu-7-A, Servo Failure

MIL-A-27328 - Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-7

This specification establishes the requirements for one type of aircraft amplifier-indicator group, altitude vertical speed designated A/A24G-7.

MIL-A-27329 - Amplifier-Indicator Group, Indicated Airspeed A/A24G-6

MIL-A-27330 - Accelerometer, Electrical, Linear Tru-3/A

This specification covers a remote accelerometer, transmitter, -4 to +10g range, synchro output, designated TRU-3/A.

MIL-A-27391 - Altimeter, Pressure Aau-2/A

This specification covers the requirements for an integrally lighted pressure altimeter, designated AAU-2/A.

MIL-A-27670 - Amplifier-Indicator Group Indicated Airspeed A/A24G-10

This specification covers the requirements for one type of aircraft indicated airspeed amplifier-indicator group, designated A/A24G-10.

MIL-A-27671 - Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-11

This specification establishes the requirements for one type of aircraft altitude vertical speed amplifier-indicator group, designated A/A24G-11.

MIL-A-27721 - Altimeter, Pressure, Mechanically Compensated General Specification For

MIL-A-27721/1 - Altimeter, Pressure, Mechanically Compensated, Type Aau-13/A

MIL-A-27890 - Altimeter, Servoid, 3 Pointer Aau-12( )/A With Automatic Pressure Standby

MIL-A-38137 - Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-17

MIL-A-38138 - Amplifier-Indicator Group, Indicated Airspeed A/A24G-18

MIL-A-38140 - Altimeter, Pressure Aau-16/A

This specification covers the requirements for an integrally lighted pressure altimeter, designated AAU-16/A.

MIL-A-38264 - Amplifier, Indicator Attitude Asu-16/A

MIL-A-38307 - Accelerometer, Aircraft Mx-6663/Ajb-7

This specification covers the requirements for one type of aircraft accelerometer, designated MX-6663/AJB-7.

MIL-A-38331 - Amplifier-Power Supply Am-4080/Asn-55, Leveling

This specification covers one type of leveling amplifier - power supply, designated AM-4080/ASN-55.

MIL-A-38396 - Altimeter, Servoed, Counter-Drum-Pointer Aau-19/A With Automatic Pressure Standby

MIL-A-38397 - Altimeter, Servoed, Counter-Drum-Pointer Aau-11/A With Automatic Pressure Standby

MIL-A-58066 - Altimeter, Pressure, Parachutist'S

This specification covers one type of single pointer, single dial, pressure altimeter.

MIL-A-58088 - Altimeter, Pressure 35,000 Feet

MIL-A-5885 - Accelerometer, Aircraft

This specification covers the requirements for a 1-7/8-inch dial, 3-pointer, -5 to +10g unit (see 6.3.3) range aircraft accelerometer.

MIL-A-6509 - Altimeter, Pressure, Aircraft, -1000 To & 50,000 Feet, Type D-9

MIL-A-81402 - Altimeter-Encoder Aau-20/A

MIL-A-81403 - Altimeter-Encoder, Aau-21/A

This specification covers the requirement for one type of counter-drum-pointer integrally lighted self-contained altimeter encoder (indicator) having a range of -1,000 to +38,000 feet and a 115V AC, 400 hertz servo driven encoder.

MIL-A-81423 - Attitude Heading Reference System An/Asn-73

MIL-A-81494 - Altimeter, Pressure, Aau-24/A

MIL-A-81851 - Altimeter Aau-31/A

This specification covers the requirements for a counter-drum-pointer, integrally lighted, self-contained altimeter (indicator) having a range of -1,000 to 50,000 ft.

MIL-A-81852 - Altimeter-Encoder Aau-32/A

This specification establishes the requirements for one type of launcher adapter that can be suspended from various ejector bomb racks and permits a guided missile launcher to be mounted to its bottom surface.

MIL-A-8237 - Amplifier, Electronic Control, True Airspeed Signal, Type Ma-2

MIL-A-83212 - Altimeter, Pressure Aau-27/A

This specification covers the requirements for one type of counter-drum-pointer, integrally lighted, pressure altimeter having a range of -1,000 to +50,000 feet, designated AAU-27/A.

MIL-A-83345 - Altimeter, Encoder, Counter Drum Pointer Aau-33/A

MIL-A-85505 - Altimeter, Standby, Types I And Ii

This specification establishes the performance, design, and test requirements for Standby Altimeters Types I and II. These altimeters are counter pointer integrally lighted with 2-inch dial for display of pressure-altitude for the range of -1,000 to 50,000 feet or -1,000 to 70,000 feet as applicable to type. The altimeter utilized an electrical output which varies as a function of the barometric pressure setting.

MIL-A-87211 - Air Data Systems, General Specification For (S/S By Afgs-87211)

This specification establishes the minimum performance requirements for air data systems, including airframe-mounted sensors, associated computers/interfaces/transducers, and displays/equipment.

MIL-C-23731 - Controller, Compass System C-2984/Ajb-3A

MIL-C-25651 - Computer, Air Data, Central, Type Mg-3

MIL-C-25653 - Computer, Central Air Data, Type Mg-1A

MIL-C-26601 - Controller, Third Gimbal Dck-10-A24G-1

MIL-C-27108 - Computer, Digital, Electronic Cp-266( )/G

MIL-C-27170 - Computer, Flight Director Cpu-4/A

MIL-C-27205 - Control Assembly, Gyroscope, Attitude-Heading A/A24G-5A

MIL-C-27473 - Converter (U) Central Air Data Eck-8/A24G

MIL-C-27522 - Computer, Flight Director Cpu-27/A

MIL-C-27889 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A, General Specification For And Mtu-38/A Mounting Tray

MIL-C-27889/1 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-1, F-101B And F-101F

MIL-C-27889/10 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-10, F-104A/B/C/D

MIL-C-27889/11 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-11, F-100C/D/F

MIL-C-27889/13 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-13, Rf-101 A/C

MIL-C-27889/15 - Computer, Transducer, Altitude, Encoding Cpu-46/A-15, Vc-137B

MIL-C-27889/16 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-16, Vc-137C Aircraft

MIL-C-27889/2 - Computer, Transducer, Altitude, Altitude, Encoding Cpu-46/A-2, F-4 Aircraft

MIL-C-27889/21 - Computer, Transducer, Altitude, Altitude, Encoding Cpu-46/A-21, F-8D/E

MIL-C-27889/22 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-22, Rf-8G, F-8H, F-8J, F-8K, F-8L

MIL-C-27889/26 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-26, T-39, T-39A

MIL-C-27889/27 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-27, T/Dt-33A, Rd-57B/F, B/Rb-57A

MIL-C-27889/28 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-28, C/Cv-140 Aircraft

MIL-C-27889/3 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-3, T-38 And F-5B Aircraft

MIL-C-27889/30 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-30, B/Rb-66

MIL-C-27889/32 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-32, B/Rb-57B/C/E Aircraft

MIL-C-27889/39 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-39, B-57G Aircraft

MIL-C-27889/7 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-7, F/Tf-102

MIL-C-38037 - Computer, Central Air Data Cpu-43/A

MIL-C-38167 - Compensator, Central Air Data Ecu-51/A

MIL-C-38240 - Computer, Altitude, Altitude Encoding Cpu-66, General Specification For And Mtu-39/A Mounting Tray

MIL-C-38240/1 - Computer, Altitude, Altitude Encoding Cpu-66/A-1, B-52, Kc/C-135, Rc-135A, Wc-135B, And Ec-135A, C, G, H, J, K, L, P

MIL-C-38240/14 - Computer, Altitude, Altitude Encoding Cpu-66/A-14

MIL-C-38240/2 - Computer, Altitude,Encoding Cpu-66/A-2, Rc-135C

MIL-C-38240/22 - Computer, Altitude, Altitude Encoding Cpu-66/A-22, Ta-4F, A-4C Aircraft

MIL-C-38240/24 - Computer, Altitude, Altitude Encoding Cpu-66/A-24, T-2B

MIL-C-38240/25 - Computer, Altitude, Altitude Encoding Cpu-66/A-25, A-4F

MIL-C-38240/27 - Computer, Altitude, Altitude Encoding Cpu-66/A-27, Tf-9J 150873

MIL-C-38286 - Computer, Flight Director Cpu-65/A

This specification covers the requirements for one type of universal flight director computer, designated CPU-65/A.

MIL-C-38418 - Control Assembly, Gyroscope, Attitude A/A24G-39

This specification covers the requirements for an Attitude Gyroscope Control Assembly, designated A/A24G-39, which provides pitch, roll, and heading angular displacements.

MIL-C-38436 - Converter, Signal Data Eck-52/A24U-6

MIL-C-5146 - Computation Table, Pressure Ratio Vs Mach Numbers For Supersonic Speeds

This specification presents tables for the computation of Mach numbers from 1.00 to 6.26 from the ration of differential pressure to static pressure.

MIL-C-5191 - Computer And Transmitter, True Airspeed Pitot Static, Type A-2

This specification covers one type of pitot static true airspeed computer and transmitter, designated Type A-2.

MIL-C-83000 - Control Assembly, Gyroscope, Attitude A/A24G-35

MIL-C-83013 - Computer, Flight Director Cpu-76/A

MIL-C-83014 - Computer, Flight Director Cpu-80/A

MIL-C-83149 - Computer, True Airspeed Cpu-104/A

MIL-C-83166 - Converter-Multiplexer, Signal Data, General Specification For

MIL-C-83166/1 - Converter-Multiplexer, Signal Data Ecu-66/A

MIL-C-83166/2 - Converter-Multiplexer, Signal Data Ecu-67/A

MIL-C-83166/3 - Converter-Multiplexer, Signal Data Ecu-68/A

MIL-C-83166/4 - Converter-Multiplexer, Signal Date Ecu-69/A

MIL-C-83321 - Control Assembly, Gyroscope, Attitude-Heading

MIL-C-83324 - Computer, Rotation And Go-Around Cpu-110/A

MIL-C-83344 - Converter, Altitude Code Ecu-87/A

MIL-C-83396 - Control Assembly, Gyroscope, Attitude-Heading A/A24G-42

This specification covers the requirements for an attitude-heading, gyroscope control assembly, designated A/A24G-42.

MIL-C-85247 - Computer, Air Data Cp-1005A/A

The Computer, Air Data, CP-1105A/A covered by this specification will supply impact pressure, static pressure, barometric altitude, Mach number, and true airspeed information to cockpit indicators and flight control systems for aircraft control.

MIL-C-9043 - Computer Systems, Airspeed And Mach Number, Installation Of

MIL-C-9075 - Computer And Transmitter, True Airspeed, Pitot-Static, 150-900 Knots, Type Ma-1

This specification covers one type of pitot static true airspeed computer and transmitter, designated Type MA-1.

MIL-D-23719 - Distribution Box J-1122/Ajb-3A

MIL-D-81641 - Display, Head-Up, General Specification For

This specification covers the general design, performance, and test requirements for procurement of all fixed wing aircraft Head-Up Displays.

MIL-DTL-25949 - Accelerometer, Aircraft Range -5 To 10G Units, Integrally Lighted

This specification covers integrally lighted -5 to +10g range, aircraft accelerometers.

MIL-DTL-5421 - Tubes, Pitot, Electrically Heated, Aircraft

This specification covers all types of two-wire electrically heated pitot tubes for use with airspeed indicators.

MIL-F-25664 - Flight Director System, Aircraft Ma-1

MIL-F-4960 - Flight Control Subsystem, Air Weapons Systems Requirements For Preparation Of Specifications For

MIL-F-6116 - Filter, Turn And Bank Indicator Air

MIL-F-7463 - Flight Computer System, Type A-2

MIL-F-87242 - Flight Control System General Specification For (S/S By Afgs-87242)

This specification delineates the operational needs and general parameters for a physical product family identified as Flight Control Systems (FCS) for piloted air vehicles.

MIL-G-22860 - Gyroscope Assembly, Displacement

MIL-G-23081 - Gyroscope Indicator System, Vertical

The equipment covered by this specification is a Vertical Gyroscope Indicator System operated by 115/200 volt, 400 Hertz, 3-phase, 4-wire wye power supply.

MIL-G-23082 - Gyroscope, Displacement, Pitch And Roll (S/S By Mil-G-23081)

MIL-G-23083 - Gyroscope, Rate Switching Ms 17399

The equipment covered by this specification is used in aircraft to monitor vertical gyros during aircraft turns.

MIL-G-23701 - Gyroscope, Rate Switching An/Asn-52

MIL-G-27739 - Gyroscope, Displacement Sbu-7/A

MIL-G-38478 - General Requirements For Angle Of Attack Based Systems

MIL-G-81559 - Gyroscope Assemblies And Attitude And Directional Reference Instruments For Aircraft, Packaging Of

This specification covers procedures for the packaging of sensitive gyroscope assemblies and other attitude and directional reference instruments for aircraft (see 6.1).

MIL-H-6507 - Housing Assembly, Station, Pressure Altimeter, Type H-2A

MIL-I-0025593 - Indicator, Attitude, Remote, Type Mm-4A (Use Mil-I-27709)

MIL-I-17213 - Inclimometer, Ship, Mk 3 Mod 0 Dr Pendulum Type

MIL-I-18079 - Installation Of Angle Of Attack And Sideslip Systems

This specification covers general requirements for the installation of angle of attack and sideslip systems which involve the use of transmitters of local angle of attack or local angle of sideslip.

MIL-I-18095 - Indicator, Turn And Slip, 115V, 3-Phase 1-7/8 Size, Types Md-3 And Md-5

MIL-I-18804 - Indicator, Vertical Speed, 0 - 6000 Fpm, 2 Inch

This specification covers design and all performance requirements for the 2-inch nominal size vertical speed indicator with a range of 0-6000 feet per minute ascent and descent.

MIL-I-18856 - Indicator, Angle Of Attack, 28V Dc Ms28062 And Ms28067

This specification covers design and all performance requirements for the 1-7/8 inch dial, MS28067, and 2-3/4 inch dial, MS28062, 28v d.c. angle of attack indicators. Configuration of each indicator shall be governed by the dash number for the Military Standard Drawing.

MIL-I-19570 - Indicator, Airspeed And Mach Number, Pitot Static, 80 To 850 Knots

MIL-I-21203 - Indicator, Attitude, Spherical, Direct Reading, Fast Erecting, Electric Gyro

This specification covers certain design and all performance requirements for procurement of spherical, direct reading, fast erecting, electric gyro attitude indicators in 5 by 5-1/4 inch cases.

MIL-I-21718 - Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots

This specification covers certain design requirements and all performance requirements for one type of pitot static, maximum allowable airspeed indicator, range 40 to 400 knots.

MIL-I-21735 - Indicator, Airspeed And Mach Number, Pitot Static, 60 To 650 Knots

The indicator covered by this specification shall indicate airspeed and Mach number with the indicated airspeed range from 60 to 650 knots, Mach range from 0.4 to 2.0 Mach, at altitudes from - 1,000 to 50,000 feet, and as listed on MS28089.

MIL-I-22068 - Indicator, Turn And Slip, Air-Driven, 2-Inch Case, Aru-8/A And Aru-9/A

MIL-I-22366 - Indicators, Vertical Velocity, Rapid Response, Acmoleration Sensitive

MIL-I-22433 - Indicator, Turn And Slip, Air Driven 2-Inch Case, 20 Degree Inclined Axis

MIL-I-22694 - Indicator, Latitude-Longitude Id-887 (*) /U

MIL-I-22859 - Indicator, Attitude Remote (Two Inch)

MIL-I-23043 - Indicator, Attitude, Two Inch Self-Contained Standby (S/S By Mil-I-81454)

MIL-I-23084 - Indicator, Attitude, Remote 3-Inch Case (S/S By Mil-G-23081)

MIL-I-23085 - Indicator, Attitude, Remote 5-Inch Case (S/S By Mil-G-23081)

MIL-I-23366 - Indicator, Horizontal Situation Id-1013(*)/A

This specification covers design and all performance requirements for the procurement of one type of course-bearing-heading-situation display indicator, which is a component of the integrated flight instrumentation system.

MIL-I-23524 - Indicator, Attitude-Director, Remote, Id 1329A (V)

This specification covers design and all performance requirements for two types of a remote attitude-director indicator, which is a component of the integrated flight instrumentation system. The indicator displays pitch and roll attitude and azimuth information with full freedom about each axis and flight director information controlled by remote circuits.

MIL-I-23671 - Indicator, Ms-17264, Airspeed And Mach Number, Integrally Lighted, Pitot-Static, 80 To 850 Knots

This specification establishes the performance, acceptance, and certain design requirements for the Airspeed and Mach Number, Integrally Lighted Indicator.

MIL-I-23724 - Indicator, Attitude Id-694/Ajb-3

MIL-I-23725 - Indicator-Programmer Id-695A/Ajb-3

MIL-I-23732 - Indicator, Attitude-Director Id-811/Ajb-3A

MIL-I-23985 - Indicator, Attitude-Director, Remote, 3-Inch Case, Ms18119

MIL-I-25120 - Indicator, Instrument Landing, Airport Runway

This specification covers one type of electrical indicating instrument, designated Indicator Instrument Landing, Airport Runway, that is used to indicate the position of an aircraft relative to the end of a runway at an airport.

MIL-I-25137 - Indicator, Airspeed, Mach Number And Maximum Allowable Speed,Type Me-4

MIL-I-25355 - Indicator, Instrument Landing, Airport Runway

This specification covers one type of electrical indicating instrument designated Indicator, Instrument Landing, Airport Runway.

MIL-I-25479 - Indicator, Mach Number, Sensitive, Servoed, Range .5 To 1.0, Type Me-5

This specification covers one type of servo operated, sensitive Mach number indicator, designated Type ME-5.

MIL-I-25592 - (Use Mil-I-27710)

MIL-I-25593 - Indicator, Attitude, Remote, Type Mm-4

MIL-I-25742 - Incilometer, Aircraft Aru/1-A

MIL-I-25893 - Indicator, Indicated Airspeed And Mach Number Avu/3-A

MIL-I-25931 - Indicator, Position, Landing Gear, Symbol-Indicating, Integrally Lighted

MIL-I-25941 - Indicator, Turn And Slip, 2- Inch Size, Integrally Lighted

This specification covers the requirements for integrally lighted, 2-inch size, turn and slip indicators.

MIL-I-25943 - Indicator, Vertical Velocity Aau-4/A Integrally Lighted, 0 To 35,000 Fpm

MIL-I-26359 - Indicator, Attitude, Remote Aru-4/A

MIL-I-26486 - Indicator, Indicated Airspeed Avu/4-A, 40-400 Knot Range

MIL-I-26608 - Indicator, Position Alu/2-A, Integrally Lighted, 28V Dc

MIL-I-2700 - Indicators, Position Angle (Inclinometers) (For Binoculars For Lookout)

MIL-I-27193 - Indicator, Attitude Aru-2B/A

This specification covers one type of remote attitude director indicator, designated ARU-2B/A.

MIL-I-27194 - Indicator, Airspeed, Mach Number And Maximum Allowable Speed Avu-9-A

MIL-I-27196 - Indicator, Vertical Velocity Aau-9/A, Integrally Lighted

This specification establishes the requirements for one type of integrally lighted vertical velocity indicator, range 0 to 6,000 feet per minute climb and descent.

MIL-I-27203 - Indicator, Position, Wing Flap

This specification covers the requirements for 28V dc integrally lighted wing flap position indicators.

MIL-I-27214 - Indicator, Directional Gyro

MIL-I-27215 - Indicator, Gyro Horizon

MIL-I-27279 - Indicator, Mach Number Avu-11/A, Integral Lighting

MIL-I-27280 - Indicator, Indicated Airspeed Avu-10/A

This specification covers one type of integrally lighted, pitot static airspeed indicator, designated AVU-10/A.

MIL-I-27392 - Indicator, Indicated Airspeed Avu-2/A (Use Mil-I-27851)

MIL-I-27433 - Indicator, True Airspeed, Synchro Repeater Avu/12-A

MIL-I-27619 - Indicators, Attitude Director

This specification covers three types of remote attitude-director indicators with superimposed flight-director information.

MIL-I-27623 - Indicator, Attitude, Remote Standby, 2 Inch

This specification covers the requirements for 2-inch remote standby attitude indicators.

MIL-I-27672 - Indicator, Position Alu-4/A, Horizontal Stabilizer

This specification covers the requirements for one type of 28V integrally lighted horizontal stabilizer position indicator, designated ALU-4/A.

MIL-I-27673 - Indicator, True Airspeed Avu-15/A

This specification covers one type of true airspeed indicator, designate AVU-15/A.

MIL-I-27680 - Indicator, Altitude Aru-12/A, Remote

This specification covers a remote attitude indicator, designated ARU-12/A.

MIL-I-27709 - Indicator, Altitude, Aru-14/A, Remote

This specification covers the requirements for one type of remote attitude indicator, designated ARU-14/A.

MIL-I-27710 - Indicator, Attitude, Remote

This specification covers the requirements for remote attitude indicators.

MIL-I-27727 - Inclinometer, Aircraft

MIL-I-27851 - Indicator, Indicated Airspeed Avu-17/A

MIL-I-38139 - Indicator, Vertical Velocity Aau-18/A, Integrally Lighted

This specification covers the requirements for a 2-inch red and white integrally lighted, vertical velocity indicator having a range of from 0 th 6,000 fpm climb and descent, designated AAU-18/A.

MIL-I-38258 - Indicator, Attitude Aru-18/A, Director

This specification covers one type of remote attitude director indicator, designated ARU-18/A.

MIL-I-38263 - Indicator, Attitude Aru-17/A, Remote

MIL-I-38335 - Indicator, Pressure Agu-11/A, Hydraulic 0-4,000 Psi, Integrally Lighted (Use Mil-I-25861)

MIL-I-38442 - Indicator, Attitude Director Aru-24/A

MIL-I-5072 - Instrument Systems, Pitot-Static Tube Operated, Installation Of

This specification covers the general requirements for the installation of all types of pitot-static, tube-operated instrument systems.

MIL-I-5098 - Indicator Rate Of Climb (Use Mil-I-7721)

MIL-I-5126 - Indicator, Directional, Gyroscopic, Magnetic Compass, Type V-7A

MIL-I-5133 - Indicator, Attitude, Type J-8

This specification covers one type of electrically driven attitude gyro indicator, designated type J-8.

MIL-I-5154 - Indicator, True Airspeed, Type-M-5

This specification covers one type of pitot static true airspeed indicator, designated Type M-5.

MIL-I-5170 - Indicator, Position, Horizontal Stabilizer

This specification covers one type of 28V dc, horizontal stabilizer position indicator.

MIL-I-5184 - Indicator, Position

This specification covers the requirements for one type of 28V dc, wing flaps position indicator.

MIL-I-5356 - Indicator, Airspeed, Pitot Static, Type L-7A

This specification covers one type of pitot static air-speed indicator, designated Type L-7A.

MIL-I-5392 - Indicator, Airspeed, Pitot Static, Type K-3

This specification covers one type of pitot static, sensitive, maximum allowable speed, range 40 to 400 knots, air-speed indicator, designated Type K-3.

MIL-I-5415 - Indicator: Air Speed, Pitot-Static Pressure, General Specification For

This specification covers the general requirements for all types of 2.750 inch round dial pitot-static airspeed indicators.

MIL-I-5416 - Indicator, Indicated Airspeed, 10-150 Knots

This specification covers one type of pitot static airspeed indicator, range 10 to 150 knots.

MIL-I-5417 - Indicator, Indicated Airspeed, 40-400 Knots

This specification covers one type of pitot static airspeed indicator, range 40 to 400 knots designated MS28046.

MIL-I-5418 - Indicator, Airspeed, Pitot Static, Sensitive, 50-650 Knots

This specification covers certain design and all performance requirements for the procurement of one type of sensitive pitot static airspeed indicator, range 50 to 650 knots.

MIL-I-5419 - Indicator, Indicated Airspeed, Pitot Static, Maximum Allowable Speed, 50-650 Knots

This specification covers a pitot-static, maximum allowable airspeed indicator, range 50-650 knots as listed on MS28048.

MIL-I-5488 - Indicator, Turn And Slip, 28V, Dc, 2-3/4 Size, Type Md-10

This specification covers certain design requirements and all performance requirements for procurement of 2 3/4 inch, 28 volt, direct current, turn and slip indicators.

MIL-I-5489 - Indicator, Turn, And Slip, Air Driven, 3-Inch Size

MIL-I-5600 - Indicator, Wind Direction, Yaw, Synchro Style, Type D-1

MIL-I-5721 - Indicator, Indicated Airspeed, 20-250 Knots

This specification covers pitot static airspeed indicators, range 20 to 250 knots.

MIL-I-5741 - Indicator, Directional, Gyroscopic, Type C-5C

MIL-I-58067 - Indicator, Vertical Velocity, Rapid Response Acceleration Sensitive, General Specification For

This specification covers a rapid response acceleration-sensitive vertical velocity indicator.

MIL-I-5949 - Instrument, Flight And Engine, Aircraft, Functional Tests And Tolerances Of

MIL-I-5997 - Instrument And Instrument Panels, Aircraft, Installation Of

MIL-I-6115 - Instrument Systems, Pitot Tube And Flush Static Port Operated, Installation Of

This specification covers the general requirements for the installation of all types of pitot tube and flush static port-operated instrument systems for use on aircraft to provide a source for dynamic and static pressures.

MIL-I-6165 - Indicators, Gyro Horizon, Non-Tumbling Fast Erecting, Electric

MIL-I-6447 - Indicator, True Airspeed, Type M-1A

This specification covers one type of pitot-static true airspeed indicator, range 100-450 knots, designated type M-1A.

MIL-I-6501 - Indicator, Attitude, External Remote Vertical Gyro Stabilized, Type B-1A

MIL-I-6568 - Indicator, Airspeed, Pitot Static, Type F-5 (Supersedes 21093)

MIL-I-6569 - Indicator, Airflow, Pressurized Cabin, Type A-3

MIL-I-7066 - Indicator, Position, Flaps, 0-30 Degree Marking, 2-Inch Size

MIL-I-7202 - Indicator, Altitude Variation, Type Z-1

MIL-I-7232 - Indicator, Mach Number, Synchro Repeater, Range 0.4 To 1.0

MIL-I-7315 - Insert, Dead Reckoning Computer (Supersedes 27637)

MIL-I-7356 - Indicator, True Airspeed, Pitot Static, Type M-4

MIL-I-7833 - Indicator, Airspeed And Mach Number, Pitot Static, 80 To 650 Knots (Use Mil-I-21735)

MIL-I-81274 - Indicator, Latitude-Longitude Id-888(*)/U

The equipment covered by this specification shall compute and provide a continuous indication of the present position, in latitude and longitude, of an aircraft in flight.

MIL-I-81400 - Instruments, Aircraft, General Specification For

MIL-I-81454 - Indicator, Gyroscope, Vertical Reference Id-1481(*)/A

This specification covers design and all performance requirements of a self-contained attitude indicator for aircraft use.

MIL-I-81496 - Indicator, Attitude, 2-Inch Id-1602/A

MIL-I-81606 - Indicator, Attitude, 3 Inch Id-1617/A And Id-1712/A

MIL-I-81683 - Indicator, Attitude Reference Self-Contained, 3-Inch, Id-1791/A

The equipment covered by this specification is a Self-Contained Vertical Gyro Indicator System for Military Aircraft.

MIL-I-8238 - Indicator System, True Airspeed, Multiple Station, Installation Of

MIL-I-8241 - Indicator, True Airspeed, Type Q-1

MIL-I-8269 - Indicator, Airspeed, Mach Number And Maximum Allowable Speed, Pitot Static, Type Me-2 (S/S By Mil-I-25137)

MIL-I-83117 - Indicator, Angle Of Attack

MIL-I-83128 - Indicator, Vertical Velocity

MIL-I-83152 - Indicator, Indicated-Airspeed Avu-22/A (Indicator-Transducer)

This specification covers an integrally white lighted, 3-inch, round-dial, pitot-static, indicated airspeed indicator and transducer,designated AVU-22/A.

MIL-I-83188 - Indicator, Attitude Standby Aru-22/A, Self-Contained

MIL-I-83266 - Indicator, Angle Of Attack Aru-29/A (S/S By Mil-I-83117)

MIL-I-83272 - Indicator, Attitude Director Aru-25/A, 3 Inch Remote

MIL-I-83334 - Indicator, Indicated Airspeed Avu-23/A

MIL-I-83336 - Indicator, Attitude, Self-Contained, 3-Inch General Specification For

MIL-I-83336/1 - Indicator, Attitude, Self-Contained, 3-Inch, Aru-44/A-1

MIL-I-83336/2 - Indicator, Attitude, Self-Contained, 3-Inch, Aru-44/A-2

MIL-I-83336/3 - Indicator, Attitude, Self-Contained, 3-Inch, Aru-30/A-1

MIL-I-83336/4 - Indicator, Attitude, Self-Contained, 3-Inch, Aru-30/A-4

MIL-I-83336/5 - Indicator, Attitude, Self-Contained, 3-Inch, Aru-30/A-3

MIL-I-83362 - Indicator, Position, Takeoff Trim Alu-12/A

This specification covers the requirements for a 1-inch takeoff trim position indicator, designated ALU-12/A.

MIL-I-83365 - Indicator, Horizontal Aqu-10/A

MIL-I-83392 - Indicator, Attitude

MIL-I-83868 - Indicator, Position Horizontal Stabilizer

MIL-I-8394 - Indicator, Airspeed, Pitot Static, Sensitive, 50-700 Mph, Fluorescent Markings, Type F-6 (Supersedes 21208)

MIL-I-85506 - Indicator, Indicated Airspeed, Standby Types I, Ii, And Iii

This specification establishes the performance, design, and test requirements for Standby Indicated Airspeed Indicators Types I,II, and III. The airspeed indicators develop indicated airspeed as a function of the difference between pitot and static pressures.

MIL-I-8687 - Indicator, Turn And Slip, Air-Driven, 2-Inch Size

MIL-I-8691 - Indicator, Azimuth, Id-307/Arn (Asg)

This specification covers one type of airborne instrument, designated ID-307/ARN, for use with a receiver-transmitter for presentation of the bearing of an aircraft from a navigation beacon.

MIL-I-8762 - Indicator, Trim, Control Surface, Type O-1 (Supersedes 27462-C)

MIL-I-87928 - Indicator, Attitude, Type Aru-51/A

This specification covers the requirements for one type of remote attitude director indicator (ADI) designated ARU-51/A.

MIL-I-9139 - Indicator, Pilot'S Data, Bombing Navigational Computer, Type A-1

MIL-I-9142 - Indicator, True Airspeed, Bombing Navigational Computer, Type M-2

MIL-I-9182 - Indicator, Phase Sequence, 200 Volt 400 Cycle Ac, Type A-1 (Supersedes 32645)

MIL-I-9471 - Indicator, Indicated Airspeed, Pitot Static, Type Mn-1

MIL-M-38445 - Monitor, Attitude, Aircraft A/A24U-12

MIL-M-5388 - Machmeter; Pitot Static Operated, Range 0.5 To 1.5, Type A-2B

This specification covers one type of 2-3/4 inch round dial, pitot static-operated machmeter, designated Type A-2B.

MIL-O-87243 - Offensive Avionics

MIL-P-25632 - Pitot Static Tube, Electrically Heated, Temperature Controlled, 115 Volt, 400 Hz, Type Ma-1

This specification covers the one type of electrically heated pitot-static tube capable of accurately sensing total and static pressures at speeds up to mach 3.

MIL-P-25757 - Pitot Static Tube Tru-1/A, Electrically Heated

MIL-P-25945 - Pitot Tube, Electrically Heated, Temperature Controlled

MIL-P-26292 - Pitot And Static Pressure Systems, Installation And Inspection Of

This specification covers the requirements for the installation and inspection of pitot-static tubes, pitot tubes, and flush static ports on aircraft and missiles.

MIL-P-27478 - Pitot Tube Tru-42/A

MIL-P-38005 - Pitot-Static Tube

This specification covers the requirements for aerodynamically compensated pitot-static tubes.

MIL-P-38046 - Pitot Static Tube Tru-59( )/A

MIL-P-38136 - Pitot Static Tube, Compensated Tru-62/A

This specification covers the requirements for an aerodynamically compensated pitot-static tube, designated TRU-62/A.

MIL-P-38244 - Pitot Static Tube Tru-74/A, Electrically Heated

MIL-P-81655 - Pitot Static Tube, L-Shaped, Compensated, Electrically Heated, General Specification For

This specification covers the general requirements for aerodynamically compensated, L-shaped, pitot static tubes.

MIL-P-83206 - Pitot Static Tube, L Shaped, Compensated, General Specification For

MIL-P-83207 - Pitot- Static Tube, Nose Boom, Compensated, General Specification For

MIL-PRF-27197 - Indicator, Airspeed, Mach Number And Maximum Allowable Speed

This specification covers nonlighted and integrally lighted combination indicated airspeed (IAS) and mach number indicators.

MIL-PRF-38135 - Indicator, Indicated Airspeed Avu-19/A, Standby

This specification covers the standby, integrally-lighted, 1-7/8 inch, round dial pitot static airspeed indicator, designated AVU-19/A.

MIL-PRF-83174 - Transmitter, Accelerometer, Axial

This specification covers three types of axial accelerometer transmitters.

MIL-PRF-83419 - Altimeter, Servo Controlled, Automatic Pressure Standby

This specification covers integrally-lighted altimeters that have an electromechanically servo driven pointer and a digital display of corrected altitude. The altimeters operate in the normal mode to display altitude transmitted by altitude computers or central air data computers. The altimeters incorporate an integral pressure sensor with electronic outputs to aid operation in the normal mode and to provide altitude inputs for the electronic display of pressure altitude when operated in the standby mode. The altimeters also incorporate an electrical output of barometric pressure setting which is required by some aircraft. A method is provided on the bezel of the altimeter for the selection of barometric setting to be displayed in either inches of mercury (in. hg) or millibars (mb). The altimeters are designed to operate from the following power sources: 115V, 400Hz (primary), 28V DC (secondary), and 18V DC (battery mode) from an optional rear mounted battery module. Altimeters meeting the requirements of this specification are interchangeable with AAU-19/A, AAU-19A/A, and AAU-19B/A, AAU-34/A, and AAU-37/A Altimeters.

MIL-R-38127 - Repeater, Servoed, Aru-16( )/A

MIL-R-38370 - Recording Set, Flight Data A/A24U-10

This specification covers a flight data (VGH) recording set, designated A/A24U-10.

MIL-R-38371 - Reproducer, Flight Data Mxu-386/E

MIL-R-38435 - Recording Set, Signal Data A/A24U-6

This specification covers the requirements for an airborne signal data recording set, designated A/A24U-6.

MIL-R-7972 - Remote Pilot Kit, K-3, (System ,B,)

MIL-R-83165 - Recorder, Signal Data Mxu-553/A

MIL-S-23535 - System, Integrated Flight Instrumentation

This specification covers certain design and all performance requirements for the procurement of an Integrated Flight Instrumentation System.

MIL-STD-1293 - Electro-Mechanical Command Instrument System For Rotary Wing Aircraft

This standard describes the primary control/display requirements for helicopter Command Instrument System (CIS) although it does not preclude unique or noval presentations over and above the basic instrument requirements.

MIL-STD-1524 - Table Of Differential Pressure In Relation To Calibrated Airspeed

MIL-STD-843 - Altimeter, Pressure, General Test Requirement For ( No S/S Document)

This standard defines those tests which should be performed on pressure altimeters prior to acceptance, after extended periods of storage, or after servicing.

MIL-STD-884 - Electronically Or Optically Generated Displays For Aircraft Control And Combat Cue Information

The purpose of this standard is to establish design requirements for electronically and optically generated aircraft which provide visual cues of flight and combat information for fixed-wing aircraft.

MIL-T-19229 - Transmitter, Angle Of Attack Or Sideslip, Local, Ms28006

This specification covers design and all performance requirements for procurement of angle of attack or sideslip transmitters, for use with an indicator flight data computers armament computers and approach power control systems. The configurator of each transmitter shall be governed by the appropriate cash number of MS28060.

MIL-T-21959 - Transmitter, True Airspeed, Pitot Static, 100 To 300 Knots, Tru-24/A

MIL-T-25066 - Transmitter, Altitude, Range Minus 1000 To Plus 80,000 Feet, Type Mc-4

MIL-T-25627 - Transmitter, Synchro, Angle Of Attack Or Sideslip

This specification covers the requirements for angle of a attack or sideslip synchro transmitters.

MIL-T-25944 - Transmitter, Vertical Velocity Tru&9-A, 0 To 35,000 Fpm

MIL-T-26609 - Transmitter, Position

This specification covers the requirements for sealed position transmitter.

MIL-T-27207 - Transmitter, Mach Number Tru&28-A

MIL-T-38241 - Transducer, Pressure, Altitude Tru-73/A

MIL-T-38306 - Transmitter, Rate Gyroscope T-970/Ajb-7

This specification covers one type of remote rate-of-turn gyroscope transmitter, designated T-970/AJB-7.

MIL-T-5420 - Tubes, Pitot Static, Electrically Heated, Aircraft

This specification covers two types of two-wire electrically heated pitot static tubes.

MIL-T-5583 - Transmitter, Position, 28 Volts Dc

This specification covers certain design and all performance requirements for the procurement of position transmitters for operation on 28-volts direct current.

MIL-T-5601 - Transmitter, Wind Direction, Pitch Or Yaw, Type R&1 (Supersedes 21262)

MIL-T-6704 - Tester, Airspeed Indicator

MIL-T-7200 - Transmitter, Altitude Variation, Type S&3

MIL-T-7215 - Transmitter, Airspeed, Pitot Static, Type T-1

MIL-T-83164 - Transducer Assembly, Aircraft A/A24J-16 (Use Mil-T-83460)

MIL-T-83208 - Transmitter, Accelerometer, Angular

MIL-T-83460 - Transducer, Motional Pickup Tru-164/A

This specification covers a differential (airspeed)-absolute (altitude) pressure transducer for aircraft applications, designated TRU-166/A.

MIL-T-9130 - Transmitter, Altitude, Range Minus 1000To Plus 80,000 Feet, Type Mc-2

MIL-T-9218 - Transmitter, Position, Type Me&1

MIL-V-17344 - Vial Inclinometer (For Illuminated Sights)

MS14114 - ( Images) Gyroscope, Displacement, Roll And Pitch (Hard Mounted) (S/S By Sae-As14114)

MS17249 - Indicator, Remote Attitude

MS17264 - Indicator, Airspeed And Mach Number, Integrally Lighted Pitot Static, 80 To 850 Knots

MS17313 - Indicator, Gyro Horizon, Manually Caged, Electric, Type Mb-1

MS17373 - Indicator, Attitude, Two-Inch, Self-Contained

MS17398 - ( Images) Gyroscope, Displacement, Roll And Pitch

MS17399 - ( Images) Gyroscope, Rate Switching

MS17400 - ( Images) Indicator, Attitude, Remote - 3 Inch Case

MS17401 - ( Images) Indicator, Attitude, Remote - 5 Inch Case

MS17869 - ( Images) Indicator, Horizontal Situation, Id-1013/A

MS18028 - ( Images) Indicator, Attitude - Director, Remote (Ifis)

MS18119 - Indicator, Attitude-Director, Remote, 3Inch Case

MS21349 - ( Images) Case, Instruments, Vertical Scale, Standard Dimensions For

MS23009 - ( Images) Accelerometer-Aircraft, Integrally Lighted Abu-4A/A And Abu-4B/A

MS24499 - ( Images) Tube, Pitot, Electrically Heated L Shaped

MS24500 - Tube, Pitot, Electrically Heated, L Shaped, Inverted

MS24501 - Tube&Pitot, Electrically Heated

MS24550 - ( Images) Transmitter, Position

MS24579 - Indicator&Gyro Horizon

MS24580 - Indicator&Directional Gyro

MS25333 - ( Images) Indicator, Indicated Airspeed, Pitot Static Maximum Allowable Speed, 40-400 Knots

MS25396 - ( Images) Transmitter, Remote Compass (Thin Wing)

MS25447 - ( Images) Transducer, Counting Accelerometer

MS25448 - ( Images) Indicator, Counting Accelerometer

MS25449 - Indicator, Turn And Slip, Air Driven, 2-Inch Case, Inclined Axis

MS25450 - Altimeter, Pressure, Counter-Pointer, Type Mc-3 And Mc-4

MS25454 - ( Images) Indicators, Vertical Velocity, Rapid Response, Acceleration Sensitive

MS25495 - Indicator, Directional Gyro, Electric

MS25499 - ( Images) Light, Instrument, Post Type

MS27150 - ( Images) Indicator, Attitude, Remote, Standby

MS27189 - Inclinometer. Aircraft

MS27202 - ( Images) Indicator, Position, Landing Gear, Symbol-Indicating, Integrally Lighted

MS27301 - Case, Instrument, Aircraft (Use Ms27572)

MS27376 - Pitot-Static Tube, 115 Volt, 400 Cycle, Fuselage Mounted

MS27403 - ( Images) Indicator, Position, Landing Gear, 28 Volt Dc

MS27464 - Mounting Base For Ask-26/A24G-27 Electronic Control Amplifier

MS27582 - Indexer, Angle Of Attack

MS27795 - Dial And Markings, Indicator, Position, Trim Tab

MS28001 - Indicator, Position, Flaps, 0-30 Degree Marking, 2-Inch Size, 28-Volt Dc

MS28002 - Indicator-Position, Control Surfaces, 1-3/8 Inch Dial, 28 Volts Dc

MS28003 - ( Images) Indicator, Position, Flaps, 2-Inch Size, 28-Volt Dc

MS28013 - ( Images) Indicator - Position, Horizontal Stabilizer (See Notice 5 For Replacement Information)

MS28017 - Indicator - Position, Nose Wheel Steering, 2 Inch Size, 28 Volt Dc

MS28021 - ( Images) Indicator - Indicated Air Speed, Pitot Static, 20-250 Knots

MS28023 - ( Images) Indicator - Position, Wing Flaps, Percent Marking

MS28024 - ( Images) Indicators, Turn And Slip, 4-Minute Turn, 2 3/4 Inch Dial

MS28025 - ( Images) Accelerometer - Aircraft (See Notice 4 For Replacement Information)

MS28031 - Indicator - Indicated Airspeed, Pitot Static, 100-850 Knots

MS28036 - ( Images) Indicator-True Airspeed, Type M-1A

MS28040 - Transmitter - Angle Of Attack Or Sideslip, Local, 28 Volt Dc

MS28041 - ( Images) Indicator, Turn And Slip, 28V Dc, 1-7/8 Inch Dial

MS28044 - Altimeter, Pressure, 50,000 Feet

MS28045 - ( Images) Indicator, Indicated Airspeed Pitot Static, 10-150 Knots

MS28046 - Indicator, Indicated Airspeed, Pitot Static, 40-400 Knots

MS28047 - ( Images) Indicator, Indicated Airspeed, Pitot Static, 50-650 Knots

MS28048 - ( Images) Indicator, Indicated Airspeed, Pitot Static Maximum Allowable Speed, 50-650 Knots (Asg)

MS28049 - ( Images) Indicator, Vertical Speed, 3 Inch (See Notice 4 For Replacement Information)

MS28060 - Indicator, Turn And Slip, 115 Volts, 3-Phase, 1-7/8 Inch Size

MS28062 - Indicator, Angle Of Attack, 2 3/4 Dial, 28 Volt D.C. (S/S By Ms28067)

MS28067 - ( Images) Indicator, Angle Of Attack, 1-7/8 Dial, 28 Volt D. C.

MS28069 - Indicator, Turn And Slip, 28V Dc, 2-3/4 Inch Size Type Md-10

MS28073 - Indicator, Control, Gyro Horizon, Type Mb-3 (P-1 Automatic Pilot)

MS28074 - Altimeter, Pressure, Counter-Pointer

MS28075 - ( Images) Indicator, Vertical Speed, 0-6000 Fpm, 2-Inch

MS28086 - ( Images) Indicator, Attitude, Spherical, Direct Reading, Fast Erecting, Electric Gyro

MS28087 - Valve, Pressuring Regulating, Turn And Slip Indicator, Type Me-1

MS28088 - ( Images) Indicator, Turn And Slip (Three Phase)

MS28089 - ( Images) Indicator, Airspeed And Mach Number, Pitot Static, 60 To 650 Knots

MS28090 - Indicator, Airspeed & Mach Number, Pitot Static, 80 To 650 Knots (S/S By Ms28089)

MS28095 - ( Images) Indicator, Airspeed And Mach Number, Pitot Static, 80 To 850 Knots

MS28096 - Indicator, Turn And Slip, Air Driven, 2 Inch Size

MS28097 - Indicator, Turn And Slip, Air Driven, 3 Inch Size

MS28098 - Indicator, Turn And Slip, Air Driven, 2-Inch Case, Aru-8A And Aru-9/A

MS3318 - ( Images) Case, Instrument, 5 X 4-1/4 Size, Standard Dimensions For

MS33545 - ( Images) Case Instrument, 5 X 5-1/4, Standard Dimensions For

MS33558 - ( Images) Numeral And Letters, Aircraft Instrument Dial, Standard Form Of

MS33635 - Instrument, Flight, Basic, Standard Arrangement Of (For Navy Use See Ms28112)

MS33785 - ( Images) Instrument Arrangement, Standard, Basic For Fixed And Rotary Wing Aircraft

MS90367 - ( Images) Indicator, Electrical, Wheels And Flaps Position

QPL-18804-16 - Indicator, Vertical Speed, 0-6000 Fpm, 2-Inch (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-18856-8 - Indicator, Angle Of Attack, 28V Dc Ms28062 And Ms28067

QPL-19229-7 - Transmitter, Angle Of Attack Or Sideslip, Local

QPL-19570-2 - Indicator, Airspeed And Mach Number, Pitot Static, 80 To 850 Knots

QPL-19679-3 - Altimeter, Pressure, Counter-Pointer

QPL-21718-1 - Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots

QPL-21735 - Indicator, Airspeed And Mach Number, Pitot Static, 60 To 650 Knots

QPL-21959 - Transmitter, True Airspeed, Pitot Static, 100 To 300 Knots, Tru-24/A

QPL-22068 - Indicator, Turn And Slip, Air-Driven, 2-Inch Case, Aru-8/A And Aru-9/A

QPL-22145-6 - Accelerometer Group, Counting

QPL-22433-1 - Indicator, Turn And Slip, Air Driven, 2-Inch Case, 20 Deg. Inclined Axis

QPL-22858-4 - Attitude Indicating System, Remote Standby, Two Inch

QPL-23395-6 - Altimeter, Pressure, Counter-Pointer, Type Mc-3 And Mc-4

QPL-23671-5 - Indicator, Ms17264, Airspeed And Mach Number, Integrally Lighted, Pitot Static, 80 To 850 Knots (See Notice 1 For Replacement Information)

QPL-25137-15 - Indicator, Airspeed, Mach Number And Maximum Allowable Speed, Type Me-4

QPL-25479-5 - Indicator, Mach Number, Sensitive, Servoed, Range .5 To 1.0, Type Me-5

QPL-25522-1 - Altimeter, Pressure, Drum&Pointer, Range&1000 To Plus 80,000 Feet, Type Md&1

QPL-25627-17 - Transmitter, Synchro, Angle Of Attack Of Sideslip (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-25632-4 - Pitot-Static Tube, Electrically Heated, Temperature Controlled, 115 Volt, 400 Cycle,Type Ma-1

QPL-25653-6 - Computer, Central Air Data, Type Mg-1A

QPL-25719-9 - Accelerometer, Aircraft, Pilot'S Warning, Type Ma-1

QPL-25757-3 - Pitot Static Tube Tru-1/A, Electrically Heated

QPL-25915-9 - Accelerometer, Aircraft, Pilot'S Warning, Type Ma-2

QPL-25931-7 - Indicator, Position, Landing Gear, Symbol-Indicating, Integrally Lighted

QPL-25941-10 - Indicator, Turn And Slip, 2 Inch Size 1Ntegrally Lighted

QPL-26359-1 - Indicator, Attitude, Remote Aru-4/A

QPL-26360-1 - Amplifier, Electrical Control Asu-3/A

QPL-26601-2 - Controller, Third Gimbal Dck-10/A24G-1

QPL-26609-5 - Transmitter, Position

QPL-26689-9 - Horizontal Situation Indicator Aqu-2/A (Indicator, Multiple, Air Navigation Aqu-2/A)

QPL-27170-6 - Computer, Flight Director Cpu-4/A

QPL-27193-18 - Indicator, Attitude, Aru-2B/A

QPL-27195-9 - Accelerometer, Aircraft, Abu-6/A

QPL-27196-5 - Indicator, Vertical Velocity Aau/9-A, Integrally Lighted

QPL-27197-24 - Indicator, Air Speed, Mach Number And Maximum Allowable Speed (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-27198-8 - Altimeter, Pressure

QPL-27203-18 - Indicator, Position, Wing Flap (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-27229-16 - Altimeter, Pressure Aau-8/A

QPL-27269-4 - Horizontal Situation Indicator Group Af/A24J-1

QPL-27279-10 - Indicator, Mach Number Avu-11/A, Integral Lighting

QPL-27280-7 - Indicator, Indicated Airspeed Avu-10/A

QPL-27328-7 - Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-7

QPL-27329-2 - Amplifier-Indicator Group, Indicater Airspeed A/A24C-6

QPL-27330-5 - Transmitter, Accelerometer, Linear Tru-3/A

QPL-27391-7 - Altimeter, Pressure Aau-2/A

QPL-27473-1 - Converter, Central Air Data Eck-8/A24G

QPL-27478-5 - Pitot Tube Tru-42/A

QPL-27522-1 - Computer, Flight Director Cpu-27/A

QPL-27619-18 - Indicators, Attitude Director (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-27623-17 - Indicator, Attitude, Remote Standby, 2 Inch

QPL-27670-1 - Amplifier-Indicator Group, Indicated Airspeed A/A24G-10

QPL-27671-1 - Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-11

QPL-27672-9 - Indicator, Position Alu-4/A, Horizontal Stabilizer, Integrally Lighted

QPL-27673-7 - Indicator, True Airspeed Avu-15/A

QPL-27680-7 - Indicator, Attitude Aru-12/A, Remote

QPL-27710-13 - Indicator, Attitude Remote

QPL-27851-9 - Indicator, Indicated Airspeed Avu-17/A

QPL-27889/1-1 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-1

QPL-27889/2-1 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-2, F-4 Aircraft

QPL-27889/3-1 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-3, T-38 Aircraft

QPL-27889-7 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A, General Specification For And Mtu-38/A Mounting Tray

QPL-38005-7 - Pitot-Static Tube

QPL-38046-1 - Pitot Static Tube Tru-59( )/A

QPL-38135-1 - Indicator, Indicated Airspeed Avu-19/A, Standby

QPL-38137-4 - Amplifier Indicator Group, Altitude Vertical Speed A/A24G-17

QPL-38138-4 - Amplifier-Indicator Group, Indicated Airspeed

QPL-38139-5 - Indicator, Vertical Velocity Aau-18/A Integrally Lighted Standby

QPL-38140-8 - Altimeter, Pressure Aau-16/A

QPL-38167-1 - Compensator, Central Air Data Ecu-51/A

QPL-5098-1 - Indicator, Rate Of Flow

QPL-5133-6 - Indicator, Attitude, Type J-8

QPL-5154-2 - Indicator, True Airspeed, Type M-5

QPL-5170-10 - Indicator, Position, Horizontal Stabilizer

QPL-5184-23 - Indicator, Position (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-5191-2 - Computer And Transmitter, True Airspeed, Pitot Static, Type A-2

QPL-5356-8 - Indicator, Airspeed, Pitot Static, Type L-7A

QPL-5388-7 - Machmeter, Pitot Static Operated, Range .5 To 1.5, Type A-2B

QPL-5392-6 - Indicator, Airspeed, Pitot Static, Type K-3

QPL-5416-16 - Indicator, Indicated Airspeed, 10-150 Knots

QPL-5417-4 - Indicator, Airspeed, Pitot Static, 40-400 Knots

QPL-5418-3 - Indicator, Airspeed, Pitot Static, Sensitive, 50-650 Knots

QPL-5420-5 - Tube, Pitot Static, Electrically Heated, Aircraft

QPL-5421-10 - Tube, Pitot, Electrically Heated, Aircraft

QPL-5488-4 - Indicator, Turn And Slip, 28V.D.C., 2-3/4 Size, Type Md-10

QPL-5489-4 - Indicator, Turn And Slip, Air Driven, 3 Inch Size

QPL-5583-25 - Transmitter, Position, 28 Volts Dc (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-5721-8 - Indicator, Indicated Airspeed, Pitot Static 20-250 Knots

QPL-5741-3 - Indicator, Directional, Gyroscopic, Type C-5C

QPL-5885-9 - Accelerometer, Aircraft

QPL-6447-8 - Indicator, True Airspeed, Type M-1A

QPL-6568-1 - Indicator, Airspeed, Pitot Static, Type F-5

QPL-6839-28 - Indicator, Position, Landing Gear (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-6848-2 - Accelerometer, Aircraft Drawing An5745

QPL-6863-4 - Altimeter Pressure 50,000 Feet, Type Mb - 1

QPL-7063-13 - Indicator, Position, Rudder Trim Tab

QPL-7064-9 - Indicator, Position, Elevator Trim Tab

QPL-7065-15 - Indicator, Position, Aileron Trim Tab (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-7066-10 - Indicator, Position, Flaps, 0-30 Degree Markings, 2-Inch

QPL-7067-10 - Indicator, Position, Flaps, 0-60 Degree Marking, 2 Inch Size

QPL-7132-4 - Indicator, Position, Nose Wheel Steering

QPL-7231-13 - Indicator, True Airspeed, Synchro Repeater, Type N-1

QPL-7356-1 - Indicator, True Airspeed, Pitot Static, Type M-4

QPL-7373-9 - Computer, True Airspeed And Machnumber, Type C-2A

QPL-7627-3 - Indicator, Turn And Slip, 28V, 1-7/8 Inch Dial

QPL-7721-11 - Indicator, Vertical Speed, 3-Inch

QPL-7783-1 - Indicator, Angle Of Attack

QPL-7785-3 - Transmitter, Angle Of Attack Or Sideslip, Local

QPL-7805-4 - Indicator, Turn And Slip, 4-Minute Turn

QPL-7833-4 - Indicator, Airspeed And Mach Number, Pitot Static

QPL-7906-3 - Indicator, Gyro Horizon, Manually Caged, Electric Type Mb-1

QPL-7968-6 - Position Indicating Assemblies, Electrical, Wheels And Flaps

QPL-8026-2 - Amplifier, Electronic Control, 2 Channel, True Airspeed And Mach Number, Type Ma-1

QPL-81403-3 - Altimeter-Encoder, Aau-21A

QPL-81454-4 - Indicator, Gyroscope Vertical Reference Id-1481(*)/A

QPL-81494-2 - Altimeter, Pressure, Aau-24/A

QPL-81606-1 - Indicator, Attitude 3 Inch Id-1617/A

QPL-81655-5 - Pitot Static Tube, L-Shaped Compensated, Electrically Heated

QPL-81851-8 - Altimeter Aau-31/A (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-81852-9 - Altimeter Encoder Aau-32/A (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-8237-3 - Amplifier, Electric Control, True Airspeed Signal, Type Ma-2

QPL-8241-6 - Indicator, True Airspeed, Type Q-1

QPL-8315-7 - Indicator, Airspeed And Mach Number, Pitot Static, Type Me-1

QPL-83344-2 - Converter, Altitude Code Ecu-87/ A

QPL-83345-2 - Altimeter, Encoder, Counter Drum Pointer Aau-33/A

QPL-83392-2 - Indicator, Attitude

QPL-83419-12 - Altimeter, Servo Controlled, Automatic Pressure Standby (Replaced By The Qualified Products Database (Qpd) See Notice 1 For Additional Information)

QPL-8580-2 - Indicator, Tachometer, Helicopter, 0-4,000 Rpm, Type Ma-1

QPL-8687-1 - Indicator, Turn And Slip, Air Driven, 2-Inch Size

QPL-9075-7 - Computer And Transmitter, True Airspeed, Pitot-Static, 150-900 Knots, Type Ma-1

QPL-9130 - Transmitter, Altitude, Range -1,000 To &80,000 Feet, Type Mc-2

QPL-9182-3 - Indicator, Phase Sequence, 200 Volt 400 Cycle Ac, Type A-1

Type Me&1