FSC 6610: Flight Instruments
The following documents are a part of this series:- A-A-56024 - Foil, Titanium
- A-A-58055 - Indicator, Attitude, Three Inch, Solid State Self-Contained
- AFGS-87211 - Air Data Systems, Air Force Guide Specification
- AFGS-87213 - Displays, Airborne, Electronically/Optically Generated
- AFGS-87242 - Flight Control System, General Specification For
- AN-5735 - Indicator - Directional Gyro
- AN-5736 - Indicator - Gyro Horizon
- AN-5744 - Inclinometer - Aircraft, Ball Style
- AN-5745 - Accelerometer - Aircraft
- AN-5760 - Altimeter - Pressure (Use ms-28044)
- AN-5780 - Indicator - Electrical, Wheels and Flap Position
- AN-5785 - Transmitter - Electrical, Wheels and Flap Position
- AN-5786 - Transmitter - Position, 28 Volt Dc
- AN-5787 - Transmitter - Position, Gearless
- AN-5805 - Tube - Single Throat Power Venturi
- AN-5806 - Tube - Double Throat Power Venturi for Turn and Bank Indicator
- AN-5807 - Tube - Double Throat Power Venturi for Directional Gyro and Gyro Horizon Indicators
- AN-5810 - Tube, PITOT-Static, Unheated, Monoplane Type
- AN-5811 - Tube, Pitot, Electrically Heated, 'L' Shaped, Inverted
- AN-5812 - Tube, Pitot, Electrically Heated, 'L' Shaped
- AN-5813 - Tube - Pitot, Electrically Heated
- AN-5814 - Tube, Pitot Static, l Shaped, Electrically Heated
- AN-5815 - Tube - PITOT-Static, Unheated Biplane Type
- AN-5816 - Tube - Pitot Static, Straight, Electrically Heated (Inactive)
- AN-5820 - Indicator, Bank and Turn
- AN-5821 - Filter - Turn and Bank Indicator Air
- AN-5823 - Card - Compass Correction
- AN-5825 - Indicator - Rate of Climb (Use ms-28049)
- AN-5839 - Indicator, Position, Landing Gear, Individual Indicating, 28-Volt Dc (Use ms-27403)
- AN-5860 - Indicator - Airspeed, Pitot Static, 10-150 Knots (Use ms-28045)
- AN-5861 - Indicator - Airspeed, Pitot Static, 40-400 Knots
- AN-5862 - Indicator - Airspeed, Pitot Static, Sensitive, 50-650 Knots (Use ms-28047)
- AN-5863 - Indicator - Airspeed, Pitot Static, Maximum Allowable Speed, 50-650 Knots (Use ms-28048)
- AS-14114 - Gyroscope, Displacement, Roll and Pitch (Hard Mounted) (STABILIZED Aug 2012)
- AS-22145 - Accelerometer Group, Counting (MS25447 and MS25448) (STABILIZED Aug 2012)
- AS-5813 - Tube - Pitot, Electrically Heated (STABILIZED Aug 2012)
- AS-5823 - Card-Compass Correction (STABILIZED Aug 2012)
- MIL-A-18105 - Amplifier, Electronic Control, E10100, for AM-632/ASB-1A
- MIL-A-19679 - Altimeter, Pressure, Counter-Pointer (No Superseding Document)
- MIL-A-22145 - Accelerometer Group, Counting,(MS25447 and MS25448) (Superseded by SAE-AS22145)
- MIL-A-22858 - Attitude Indicating System, Remote, Standby, Two Inch (No Superseding Document)
- MIL-A-23395 - Altimeter, Pressure, Counter-Pointer, Type MC-3 and MC-4 (No Superseding Document)
- 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
- MIL-A-25915 - Accelerometer, Aircraft, Pilot's Warning, Type ma-2 (No Superseding Document)
- MIL-A-25949 - Accelerometer, Aircraft Range -5 To +10g Units, Integrally Lighted (Superseded by MIL-DTL-259
- MIL-A-26353 - Antenna System for Receiver, Radio an-ARR-47 Design Requirements For
- MIL-A-26360 - Amplifier, Electrical Control ASU-3/a (No Superseding Document)
- MIL-A-27195 - Accelerometer, Aircraft, Mechanical ABU-6/A
- MIL-A-27198 - Altimeter, Pressure AAU-7/A
- MIL-A-27229 - Altimeter, Pressure AAU-8/a (No Superseding Document)
- MIL-A-27261 - Accelerometer, Aircraft
- 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
- MIL-A-27329 - Amplifier-Indicator Group, Indicated Airspeed A/A24G-6
- MIL-A-27330 - Accelerometer, Electrical, Linear TRU-3/A
- MIL-A-27391 - Altimeter, Pressure AAU-2/A (No Superseding Document)
- MIL-A-27670 - Amplifier-Indicator Group Indicated Airspeed A/A24G-10 (No Replacement Document)
- MIL-A-27671 - Amplifier-Indicator Group, Altitude-Vertical Speed A/A24G-11 (No Replacement Document)
- 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, Servoed, 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 (No Superseding Document)
- MIL-A-38264 - Amplifier, Indicator Attitude ASU-16/A
- MIL-A-38307 - Accelerometer, Aircraft MX-6663/AJB-7
- MIL-A-38331 - Amplifier-Power Supply AM-4080/ASN-55, Leveling (No Superseding Document)
- 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 (No Superseding Document)
- MIL-A-58088 - Altimeter, Pressure 35,000 Feet
- MIL-A-5885 - Accelerometer, Aircraft
- MIL-A-6509 - Altimeter, Pressure, Aircraft, -1000 to and 50,000 Feet, Type D-9
- MIL-A-6848 - Accelerometer, Aircraft
- MIL-A-6863 - Altimeter, Pressure, 50,000 Feet, Type MB-1A (No Superseding Document)
- MIL-A-8026 - Amplifier, Electronic Control, 2 Channel, True Airspeed and Mach Number, Type ma-1 (No Superseding Document)
- MIL-A-81402 - Altimeter-Encoder AAU-20/A
- MIL-A-81403 - Altimeter-Encoder, AAU-21/A
- MIL-A-81423 - Attitude Heading Reference System AN/ASN-73 (No Superseding Document)
- MIL-A-81494 - Altimeter, Pressure, AAU-24/a
- MIL-A-81851 - Altimeter AAU-31/A
- MIL-A-81852 - Altimeter-Encoder AAU-32/A
- MIL-A-8237 - Amplifier, Electronic Control, True Airspeed Signal, Type MA-2 (No Superseding Document)
- MIL-A-83212 - Altimeter, Pressure AAU-27/A
- MIL-A-83345 - Altimeter, Encoder, Counter Drum Pointer AAU-33/a
- MIL-A-83419 - Altimeter, Servo Controlled, Automatic Pressure Standby
- MIL-A-85505 - Altimeter, Standby, Types I and II
- MIL-A-87211 - Air Data Systems, General Specification for (Superseded by AFGS-87211)
- MIL-A-87247 - Avionics Equipment, Defensive, Airborne, Specification for (U)
- 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 (No Superseding Document)
- MIL-C-26601 - Controller, Third Gimbal DCK-10-a24G-1 (No Superseding Document)
- MIL-C-27170 - Computer, Flight Director CPU-4/A (No Superseding Document)
- MIL-C-27205 - Control Assembly, Gyroscope, Attitude-Heading a/a24G-5a (No Superseding Document)
- 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 (No Superseding Document)
- MIL-C-27889/1 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-1, F-101B and F-101F (No Superseding Document)
- MIL-C-27889/10 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-10, F-104a/B/C/D (No Superseding Document)
- MIL-C-27889/11 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-11, F-100C/D/F (No Superseding Document)
- MIL-C-27889/13 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-13, Rf-101 a/C (No Superseding Document)
- MIL-C-27889/15 - Computer, Transducer, Altitude, 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 (No Superseding Document)
- MIL-C-27889/21 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-21, F-8D/E (No Superseding Document)
- MIL-C-27889/22 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-22, Rf-8g, F-8H, F-8J, F-8K, F-8l (No Superseding Document)
- MIL-C-27889/26 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-26, T-39, T-39a (No Superseding Document)
- MIL-C-27889/27 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-27, T/DT-33a, Rd-57B/F, B/RB-57a (No Superseding Document)
- MIL-C-27889/28 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-28, C/CV-140 Aircraft (No Superseding Document)
- MIL-C-27889/3 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-3, T-38 and F-5B Aircraft (No Superseding Document)
- MIL-C-27889/30 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-30, B/RB-66 (No Superseding Document)
- MIL-C-27889/32 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-32, B/RB-57B/C/E Aircraft (No Superseding Document)
- MIL-C-27889/39 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-39, B-57g Aircraft (No Superseding Document)
- MIL-C-27889/7 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-7, F/TF-102 (No Superseding Document)
- 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 (No Superseding Document)
- 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
- MIL-C-38418 - Control Assembly, Gyroscope, Attitude A/A24G-39
- MIL-C-38436 - Converter, Signal Data ECK-52/a24U-6
- MIL-C-5146 - Computation Table, Pressure Ratio vs Mach Numbers for Supersonic Speeds (No Superseding Document)
- MIL-C-5191 - Computer and Transmitter, True Airspeed Pitot Static, Type A-2 (No Superseding Document)
- MIL-C-7373 - Computer, True Airspeed and Machnumber, Type C-2a
- MIL-C-83000 - Control Assembly, Gyroscope, Attitude a/a24G-35
- MIL-C-83013 - Computer, Flight Director Cpu-76/a (No Superseding Document)
- MIL-C-83014 - Computer, Flight Director Cpu-80/a (No Superseding Document)
- MIL-C-83149 - Computer, True Airspeed Cpu-104/a (No Superseding Document)
- 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 (No Superseding Document)
- MIL-C-83166/3 - Converter-Multiplexer, Signal Data ECU-68/a
- MIL-C-83166/4 - Converter-Multiplexer, Signal Data ECU-69/a (No Superseding Document)
- MIL-C-83321 - Control Assembly, Gyroscope, Attitude-Heading (No Superseding Document)
- MIL-C-83324 - Computer, Rotation and go-Around Cpu-110/a (No Superseding Document)
- MIL-C-83344 - Converter, Altitude Code ECU-87/a (No Superseding Document)
- MIL-C-83396 - Control Assembly, Gyroscope, Attitude Heading a/a24G-42 (No Superseding Document)
- MIL-C-85247 - Computer, Air Data CP-1005a/a
- 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
- MIL-D-23719 - Distribution Box J-1122/AJB-3a
- MIL-D-81641 - Display, Head-Up, General Specification For
- MIL-D-87213 - Displays, Airborne, Electronically/Optically Generated (Superseded by AFGS-87213a)
- MIL-DTL-25627 - Transmitter, Synchro, Angle of Attack or Sideslip
- MIL-DTL-25949 - Accelerometer, Aircraft Range -5 to 10G Units, Integrally Lighted
- MIL-DTL-27193 - Indicator, Attitude ARU-2B/A
- MIL-DTL-5184 - Indicator, Position
- MIL-DTL-5421 - Tubes, Pitot, Electrically Heated, Aircraft
- MIL-DTL-6839 - Indicator, Position, Landing Gear
- MIL-DTL-7627 - Indicator, Turn and Slip, 28V DC
- MIL-DTL-9490 - Flight Control Systems - Design, Installation and Test of Piloted Aircraft, General Specification for
- 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 (Controlled Distribution) (Superseded by AFGS-87242)
- MIL-F-9490 - Flight Control Systems - Design, Installation& Test of Piloted Aircraft, General Specification
- MIL-G-22860 - Gyroscope Assembly, Displacement
- MIL-G-23081 - Gyroscope Indicator System, Vertical
- MIL-G-23082 - Gyroscope, Displacement, Pitch and Roll (Superseded by MIL-G-23081)
- MIL-G-23083 - Gyroscope, Rate Switching MS 17399
- MIL-G-23701 - Gyroscope, Rate Switching an/ASN-52 (No Superseding Document)
- 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
- MIL-H-27269 - Horizontal Situation Indicator Group AF/a24J-1 (No Superseding Document)
- MIL-H-6507 - Housing Assembly, Station, Pressure Altimeter, Type H-2a (Supersedes 94-27320)
- MIL-HDBK-2084 - General Requirements for Maintainability of Avionic and electronic Systems and Equipment
- MIL-I-17213 - Inclimometer, Ship, Mk. 3 Mod. O Dr Pendulum Type
- MIL-I-18079 - Installation of Angle of Attack and Sideslip Systems (No Superseding Document)
- 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
- MIL-I-18856 - Indicator, Angle of Attack, 28V Dc Ms28062 and Ms28067
- MIL-I-19570 - Indicator, Airspeed and Mach Number, Pitot Static, 80 To 850 Knots (No Superseding Document)
- MIL-I-21203 - Indicator, Attitude, Spherical, Direct Reading, Fast Erecting, Electric Gyro
- MIL-I-21718 - Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots
- MIL-I-21735 - Indicator, Airspeed and Mach Number, Pitot Static, 60 To 650 Knots
- 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 (Superseded by MIL-I-81454)
- MIL-I-23084 - Indicator, Attitude, Remote 3-Inch Case (Superseded by MIL-G-23081)
- MIL-I-23085 - Indictor, Attitude, Remote 5-Inch Case (Superseded by MIL-G-23081)
- MIL-I-23366 - Indicator, Horizontal Situation Id-1013(*)/a
- MIL-I-23524 - Indicator, Attitude-D1Rector, Remote, Id 1329a (V)
- MIL-I-23671 - Indicator, ms-17264, Airspeed and Mach Number, Integrally Lighted, PITOT-Static, 80 To 850 Knots (No Superseding Document)
- 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 (No Superseding Document)
- MIL-I-25120 - Indicator, Instrument Landing, Airport Runway
- MIL-I-25137 - Indicator, Airspeed, Mach Number and Maximum Allowable Speed, Type me-4 (No Superseding Document)
- MIL-I-25355 - Indicator, Instrument Landing, Airport Runway
- MIL-I-25479 - Indicator, Mach Number, Sensitive, Servoed, Range .5 to 1.0, Type ME-5
- MIL-I-25593 - Indicator, Attitude, Remote, Type MM-4
- MIL-I-25742 - Inclinometer, 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 (No Superseding Document)
- MIL-I-25941 - Indicator, Turn and Slip, 2- Inch Size, Integrally Lighted
- 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 (No Superseding Document)
- 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-26689 - Indicator, Horizontal Situation, AQU-2/A
- MIL-I-2700 - Indicators, Position Angle (Inclinometers) (for Binoculars for Lookout)
- MIL-I-27193 - Indicator, Attitude 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
- MIL-I-27197 - Indicator, Airspeed, Mach Number & Maximum Allowable Speed
- MIL-I-27203 - Indicator, Position, Wing Flap
- MIL-I-27214 - Indicator, Directional Gyro
- MIL-I-27215 - Indicator, Gyro Horizon
- MIL-I-27279 - Indicator, Mach Number AVU-11/a, Integral Lighting (No Superseding Document)
- MIL-I-27280 - Indicator, Indicated Airspeed AVU-10/a (No Superseding Document)
- MIL-I-27392 - Indicator, Indicated Airspeed AVU-2/a (See MIL-I-27851)
- MIL-I-27433 - Indicator, True Airspeed, Synchro Repeater AVU-12-a
- MIL-I-27619 - Indicators, Attitude Director
- MIL-I-27623 - Indicator, Attitude, Remote Standby, 2 Inch (No Superseding Document)
- MIL-I-27672 - Indicator, Position ALU-4/a, Horizontal Stabilizer
- MIL-I-27673 - Indicator, True Airspeed AVU-15/A
- MIL-I-27680 - Indicator, Altitude ARU-12/a, Remote (No Superseding Document)
- MIL-I-27709 - Indicator, Altitude, ARU-14/a, Remote (No Superseding Document)
- MIL-I-27710 - Indicator, Attitude, Remote
- MIL-I-27727 - Inclinometer, Aircraft
- MIL-I-27848 - Indicator, Horizontal Situation AQU-4/A
- MIL-I-27851 - Indicator, Indicated Airspeed AVU-17/a (No Superseding Document)
- MIL-I-38135 - Indicator, Indicated Airspeed AVU-19/a, Standby
- MIL-I-38139 - Indicator, Vertical Velocity AAU-18/A, Integrally Lighted
- MIL-I-38258 - Indicator, Attitude ARU-18/a, Director (No Superseding Document)
- MIL-I-38263 - Indicator, Attitude ARU-17/a, Remote
- MIL-I-38335 - Indicator, Pressure AGU-11/a, Hydraulic 0-4,000 Psi, Intergrally Lighted (Use MIL-I-25861)
- MIL-I-38442 - Indicator, Attitude Director ARU-24/a (No Superseding Document)
- MIL-I-5072 - Instrument Systems, PITOT-Static Tube Operated, Installation of (No Superseding Document)
- 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 (No Superseding Document)
- MIL-I-5154 - Indicator, True Airspeed, Type-M-5
- MIL-I-5170 - Indicator, Position, Horizontal Stabilizer
- MIL-I-5184 - Indicator, Position
- MIL-I-5356 - Indicator, Airspeed, Pitot Static, Type L-7a (No Superseding Document)
- MIL-I-5392 - Indicator, Airspeed, Pitot Static, Type K-3 (No Superseding Document)
- MIL-I-5415 - Indicator; Air Speed, PITOT-Static Pressure, General Specification for (No Superseding Document)
- MIL-I-5416 - Indicator, Indicated Airspeed, 10-150 Knots
- MIL-I-5417 - Indicator, Indicated Airspeed, 40-400 Knots (No Superseding Document)
- MIL-I-5418 - Indicator, Airspeed, Pitot Static, Sensitive, 50-650 Knots
- MIL-I-5419 - Indicator, Indicated Airspeed, Pitot Static, Maximum Allowable Speed, 50-650 Knots
- MIL-I-5488 - Indicator, Turn and Slip, 28V., Dc, 2-3/4 Size, Type md-10 (No Superseding Document)
- 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 (No Superseding Document)
- MIL-I-5741 - Indicator, Directional, Gyroscopic, Type C-5C (No Superseding Document)
- MIL-I-58067 - Indicator, Vertical Velocity, Rapid Response Acceleration Sensitive, General Specification for
- MIL-I-5949 - Instrument, Flight and Engine, Aircraft, Functional Tests and Tolerances of (No Superseding Document)
- MIL-I-5997 - Instrument and Instrument Panels, Aircraft, Installation of (No Superseding Document)
- MIL-I-6115 - Instrument Systems, Pitot Tube and Flush Static Port Operated, Installation of
- MIL-I-6165 - Indicators, Gyro Horizon, Non-Tumbling Fast Erecting, Electric
- MIL-I-6447 - Indicator, True Airspeed, 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-6726 - Inclinometer, Aircraft
- MIL-I-6839 - Indicator, Position, Landing Gear
- MIL-I-7028 - Instrument and Instrument Boards, Aircraft, Installation of (No Superseding Document)
- MIL-I-7062 - Indicator, Position, Control Surfaces, 28 Volt DC, General Specification for
- MIL-I-7063 - Indicator, Position, Rudder Trim Tab (No Superseding Document)
- MIL-I-7064 - Indicator, Position, Elevator Trim Tab
- MIL-I-7065 - Indicator, Position, Aileron Trim Tab
- MIL-I-7066 - Indicator, Position, Flaps, 0-30 Degree Marking, 2-Inch Size (No Superseding Document)
- MIL-I-7067 - Indicator, Position, Flaps, 0-60 Degree Marking, 2-Inch Size (No Superseding Document)
- MIL-I-7132 - Indicator, Position, Nose Wheel Steering
- MIL-I-7202 - Indicator, Altitude Variation, Type Z-1
- MIL-I-7231 - Indicator, True Airspeed, Synchro Repeater, Type N-1 (No Superseding Document)
- 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-7482 - Indicator, Straight Line, Shoran Type a&2
- MIL-I-7627 - Indicator, Turn & Slip, 28V Dc
- MIL-I-7721 - Indicator, Vertical Speed, 3-Inch
- MIL-I-7783 - Indicator, Angle of Attack
- MIL-I-7802 - INDICATOR, MS28088, TURN AND SLIP (THREE PHASE) Indicator, MS28088, Turn and Slip (Three Phase)
- MIL-I-7803 - Indicator, Directional Gyro, Electric
- MIL-I-7805 - Indicators, Turn and Slip, 4-Minute Turn (Superseded by MIL-I-7627C)
- MIL-I-7833 - Indicator, Airspeed and Mach Number, Pitot Static, 80 To 650 Kn0Ts (Use MIL-I-21735)
- MIL-I-7906 - Indicator, Gyro Horizon, Manually Caged, Electric, Type MB-1
- MIL-I-81274 - Indicator, Latitude-Longitude Id-888(*)/U (No Superseding Document)
- MIL-I-81400 - Instruments, Aircraft, General Specification for (No Superseding Document)
- MIL-I-81454 - Indicator, Gyroscope, Vertical Reference Id-1481(*)/a
- MIL-I-81496 - Indicator, Attitude, 2-Inch Id-1602/a
- MIL-I-81606 - Indicator, Attitude, 3 Inch Id-1617/a and Id-1712/a (No Superseding Document)
- MIL-I-81683 - Indicator, Attitude Reference Self-Contained, 3-Inch, Id-1791/a
- MIL-I-8238 - Indicator System, True Airspeed, Multiple Station, Installation Of
- MIL-I-8241 - Indicator, True Airspeed, Type Q-1 (No Superseding Document)
- MIL-I-8269 - Indicator, Airspeed, Mach Number and Maximum Allowable Speed, Pitot Static, Type me-2 (See MIL-I-25137)
- MIL-I-83034 - Indicator, Horizontal Situation AQU-6A/A
- MIL-I-83117 - Indicators, Angle of Attack (No Superseding Document)
- MIL-I-83128 - Indicator, Vertical Velocity (No Superseding Document)
- MIL-I-8315 - Indicator, Airspeed and Mach Number, Pitot Static, Type me-1 (No Superseding Document)
- MIL-I-83152 - Indicator, Indicated-Airspeed AVU-22/A (Indicator-Transducer)
- MIL-I-83188 - Indicator, Attitude Standby ARU-22/a, Self-Contained (No Superseding Document)
- MIL-I-83266 - Indicator, Angle of Attack ARU-29/a (Superseded 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 (No Superseding Document)
- MIL-I-83336 - Indicator, Attitude, Self Contained, 3 Inch General Specification for (No Superseding Document)
- MIL-I-83336/1 - Indicator, Attitude, Self Contained, 3 Inch, ARU-44/A-1 (No Superseding Document)
- MIL-I-83336/2 - Indicator, Attitude, Self-Contained, 3-Inch, ARU-44/A-2 (No Superseding Document)
- MIL-I-83336/3 - Indicator, Attitude, Self Contained, 3 Inch, ARU-30/A-1 (No Superseding Document)
- MIL-I-83336/4 - Indicator, Attitude, Self-Contained, 3-Inch, ARU-30/A-4 (No Superseding Document)
- MIL-I-83336/5 - Indicator, Attitude, Self-Contained, 3-Inch, ARU-30/A-3 (No Superseding Document)
- MIL-I-83362 - Indicator, Position, Takeoff Trim ALU-12/A
- MIL-I-83365 - Indicator, Horizontal Situation AQU-10/a (No Superseding Document)
- MIL-I-83392 - Indicator, Attitude (No Superseding Document)
- MIL-I-83868 - Indicator, Position Horizontal Stabilizer (No Superseding Document)
- 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
- MIL-I-8687 - Indicator, Turn and Slip, Air-Driven, 2-Inch Size (Superseded by MIL-I-5489C)
- MIL-I-8691 - Indicator, Azimuth, Id-307/Arn (Asg)
- MIL-I-8762 - Indicator, Trim, Control Surface, Type O&1 (Supersedes 27462&C)
- MIL-I-87928 - Indicator, Attitude, Type 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 (Supersedes 34054&a)
- 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
- MIL-M-6756 - Measuring and Leveling Provisions (for Aircraft) (Superseded by MIL-W-25140B)
- MIL-M-7507 - Machmeter, Pitot Static, Range .3 to 1.0, Type A-1
- MIL-P-25632 - Pitot Static Tube, Electrically Heated, Temperature Controlled, 115 Volt, 400 Hz, Type ma-1 (No Superseding Document)
- MIL-P-25757 - Pitot Static Tube TRU-1/a, Electrically Heated
- MIL-P-25945 - Pitot Tube, Electrically Heated, Temperature Controlled (No Superseding Document)
- MIL-P-26292 - Pitot and Static Pressure Systems, Installation and Inspection of (No Superseding Document)
- MIL-P-27478 - Pitot Tube TRU-42/a (No Superseding Document)
- MIL-P-38005 - PITOT-Static Tube (No Superseding Document)
- MIL-P-38046 - Pitot Static Tube TRU-59( )/a
- MIL-P-38136 - Pitot Static Tube, Compensated TRU-62/a (No Superseding Document)
- MIL-P-38244 - Pitot Static Tube TRU-74/a, Electrically Heated (No Superseding Document)
- MIL-P-7968 - Position Indicating Assemblies, Electrical, Wheels and Flaps (No Superseding Document)
- MIL-P-81655 - Pitot Static Tube, L-Shaped, Compensated, Electrically Heated, General Specification For
- MIL-P-83206 - Pitot Static Tube, l Shaped, Compensated, General Specification for (No Superseding Document)
- MIL-P-83207 - PITOT- Static Tube, Nose Boom, Compensated, General Specification for (No Superseding Document)
- MIL-PRF-27197 - Indicator, Airspeed, Mach Number and Maximum Allowable Speed
- MIL-PRF-38135 - Indicator, Indicated Airspeed AVU-19/A, Standby
- MIL-PRF-83174 - Transmitter, Accelerometer, Axial
- MIL-PRF-83419 - Altimeter, Servo Controlled, Automatic Pressure Standby
- MIL-R-38127 - Repeater, Servoed, ARU-16( )/a
- MIL-R-38370 - Recording Set, Flight Data a/a24U-10
- MIL-R-38371 - Reproducer, Flight Data MXU-386/E
- MIL-R-38435 - Recording Set, Signal Data a/a24U-6 (No Superseding Document)
- 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
- MIL-STD-1293 - Electro-Mechanical Command Instrument System for Rotary Wing Aircraft (No Superseding Document)
- MIL-STD-1524 - Table of Differential Pressure in Relation To Calibrated Airspeed (No Superseding Document)
- MIL-STD-843 - Altimeter, Pressure, General Test Requirement for ( No Superseding Document)
- MIL-STD-884 - Electronically or Optically Generated Displays for Aircraft Control and Combat Cue Information (No Superseding Document)
- MIL-T-19229 - Transmitter, Angle of Attack or Sideslip, Local, Ms28006 (No Superseding Document)
- MIL-T-21959 - Transmitter, True Airspeed, Pitot Static, 100 To 300 Knots, TRU-24/a (No Superseding Document)
- MIL-T-25066 - Transmitter, Altitude, Range Minus 1000 To Plus 80,000 Feet, Type mc-4 (No Superseding Document)
- MIL-T-25627 - Transmitter, Synchro, Angle of Attack or Sideslip
- MIL-T-25944 - Transmitter, Vertical Velocity TRU-9-a, 0 To 35,000 Fpm
- MIL-T-26609 - Transmitter, Position
- 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 (No Superseding Document)
- MIL-T-5420 - Tubes, Pitot Static, Electrically Heated, Aircraft
- MIL-T-5421 - Tube, Pitot, Electrically Heated, Aircraft
- MIL-T-5583 - Transmitter, Position, 28 Volts DC
- MIL-T-5601 - Transmitter, Wind Direction, Pitch or Yaw, Type R-1 (Supersedes 21262)
- MIL-T-6704 - Tester, Airspeed Indicator (No Superseding Document)
- MIL-T-7200 - Transmitter, Altitude Variation, Type S-3
- MIL-T-7215 - Transmitter, Airspeed, Pitot Static, Type T-1
- MIL-T-7785 - Transmitter, Angle of Attack or Sideslip, Local
- MIL-T-83164 - Transducer Assembly, Aircraft a/a24J-16 (Use MIL-T-83460)
- MIL-T-83174 - Transmitter, Accelerometer, Axial
- MIL-T-83208 - Transmitter, Accelerometer, Angular
- MIL-T-83460 - Transducer, Motional Pickup TRU-164/a (No Superseding Document)
- MIL-T-9130 - Transmitter, Altitude, Range Minus 1000To Plus 80,000 Feet, Type mc-2
- MIL-T-9218 - Transmitter, Position, Type me-1
- MIL-U-25592 - Use MIL-I-27710
- MIL-V-17344 - Vial Inclinometer (for Illuminated Sights)
- MS-14114 - Gyroscope, Displacement, Roll and Pitch (Hard Mounted) (Superseded by SAE as-14114)
- MS-17249 - Indicator, Remote Attitude (No Superseding Document)
- MS-17264 - Indicator, Airspeed and Mach Number, Integrally Lighted Pitot Static, 80 To 850 Knots (No Superseding Document)
- MS-17313 - Indicator, Gyro Horizon, Manually Caged, Electric, Type mb-1 (No Superseding Document)
- MS-17373 - Indicator, Attitude, Two-Inch, Self-Contained
- MS-17398 - Gyroscope, Displacement, Roll and Pitch
- MS-17399 - Gyroscope, Rate Switching
- MS-17400 - Indicator, Attitude, Remote - 3 Inch Case
- MS-17401 - Indicator, Attitude, Remote - 5 Inch Case
- MS-17869 - Indicator, Horizontal Situation, ID-1013/A
- MS-18028 - Indicator, Attitude - Director, Remote (IFIS)
- MS-18119 - Indicator, Attitude-Director, Remote, 3Inch Case (No Superseding Document)
- MS-21349 - Case, Instruments, Vertical Scale, Standard Dimensions For
- MS-23009 - Accelerometer-Aircraft, Integrally Lighted ABU-4a/a and ABU-4B/a
- MS-24351 - Case, Instrument, 1 Inch Dial Standard DIMEN-Sions for (Use ms-33580)
- MS-24499 - Tube, Pitot, Electrically Heated l Shaped (No Superseding Document)
- MS-24500 - Tube, Pitot, Electrically Heated, l Shaped, Inverted (No Superseding Document)
- MS-24501 - Tube-Pitot, Electrically Heated
- MS-24550 - Transmitter, Position
- MS-24579 - Indicator-Gyro Horizon
- MS-24580 - Indicator-Directional Gyro
- MS-25333 - Indicator, Indicated Airspeed, Pitot Static Maximum Allowable Speed, 40-400 Knots
- MS-25396 - Transmitter, Remote Compass (Thin Wing) (No Superseding Document)
- MS-25447 - Transducer, Counting Accelerometer
- MS-25448 - Indicator, Counting Accelerometer
- MS-25449 - Indicator, Turn and Slip, Air Driven, 2-Inch Case, Inclined Axis
- MS-25450 - Altimeter, Pressure, Counter-Pointer, Type mc-3 and mc-4 (No Superseding Document)
- MS-25454 - Indicators, Vertical Velocity, Rapid Response, Acceleration Sensitive (No Superseding Document)
- MS-25495 - Indicator, Directional Gyro, Electric
- MS-25499 - Light, Instrument, Post Type (No Superseding Document)
- MS-27150 - Indicator, Attitude, Remote, Standby (No Superseding Document)
- MS-27189 - Inclinometer. Aircraft
- MS-27202 - Indicator, Position, Landing Gear, Symbol-Indicating, Integrally Lighted (No Superseding Document)
- MS-27301 - Case, Instrument, Aircraft (Use ms-27572)
- MS-27376 - PITOT-Static Tube, 115 Volt, 400 Cycle, Fuselage Mounted (No Superseding Document)
- MS-27403 - Indicator, Position, Landing Gear, 28 Volt DC
- MS-27464 - Mounting Base for ask-26/a24G-27 Electronic Control Amplifier (No Superseding Document)
- MS-27582 - Indexer, Angle of Attack (No Superseding Document)
- MS-27795 - Dial and Markings, Indicator, Position, Trim Tab
- MS-28001 - Indicator, Position, Flaps, 0-30 Degree Marking, 2-Inch Size, 28-Volt Dc
- MS-28002 - Indicator-Position, Control Surfaces, 1-3/8 Inch Dial, 28 Volts Dc (No Superseding Document)
- MS-28003 - Indicator, Position, Flaps, 2-Inch Size, 28-Volt Dc (No Superseding Document)
- MS-28013 - Indicator - Position, Horizontal Stabilizer
- MS-28017 - Indicator - Position, Nose Wheel Steering, 2 Inch Size, 28 Volt Dc
- MS-28021 - Indicator - Indicated Air Speed, Pitot Static, 20-250 Knots (No Superseding Document)
- MS-28023 - Indicator - Position, Wing Flaps, Percent Marking
- MS-28024 - Indicator, Turn - Slip, 4 Minute Turn, 2 3/4 Inch Dial
- MS-28025 - Accelerometer - Aircraft
- MS-28031 - Indicator - Indicated Airspeed, Pitot Static, 100-850 Knots
- MS-28036 - Indicator-True Airspeed, Type M-1A
- MS-28040 - Transmitter - Angle of Attack or Sideslip, Local, 28 Volt Dc
- MS-28041 - Indicator, Turn and Slip, 28V DC, 1-7/8 Inch Dial
- MS-28044 - Altimeter, Pressure, 50,000 Feet (No Superseding Document)
- MS-28045 - Indicator, Indicated Airspeed Pitot Static, 10-150 Knots
- MS-28046 - Indicator, Indicated Airspeed, Pitot Static, 40-400 Knots (No Superseding Document)
- MS-28047 - Indicator, Indicated Airspeed, Pitot Static, 50-650 Knots (No Superseding Document)
- MS-28048 - Indicator, Indicated Airspeed, Pitot Static Maximum Allowable Speed, 50-650 Knots (Asg)
- MS-28049 - Indicator, Vertical Speed, 3 Inch
- MS-28060 - Indicator, Turn and Slip, 115 Volts, 3-Phase, 1-7/8 Inch Size
- MS-28062 - Indicator, Angle of Attack, 2 3/4 Dial, 28 Volt D.C. (Superseded by ms-28067)
- MS-28067 - Indicator, Angle of Attack, 1-7/8 Dial, 28 Volt D. C.
- MS-28069 - Indicator, Turn and Slip, 28V Dc, 2-3/4 Inch Size Type md-10
- MS-28073 - Indicator, Control, Gyro Horizon, Type mb-3 (P-1 Automatic Pilot)
- MS-28074 - Altimeter, Pressure, Counter-Pointer (No Superseding Document)
- MS-28075 - Indicator, Vertical Speed, 0-6000 Fpm, 2-Inch
- MS-28086 - Indicator, Attitude, Spherical, Direct Reading, Fast Erecting, Electric Gyro
- MS-28087 - Valve, Pressuring Regulating, Turn and Slip Indicator, Type me-1
- MS-28088 - Indicator, Turn and Slip (Three Phase)
- MS-28089 - Indicator, Airspeed and Mach Number, Pitot Static, 60 To 650 Knots
- MS-28090 - INDICATOR, AIRSPEED and MACH NUMBER, PITOT STATIC, 80 TO 650 KNOTS (SUPERSEDED BY MS-28089)
- MS-28095 - Indicator, Airspeed and Mach Number, Pitot Static, 80 To 850 Knots (No Superseding Document)
- MS-28096 - Indicator, Turn and Slip, Air Driven, 2 Inch Size
- MS-28097 - Indicator, Turn and Slip, Air Driven, 3 Inch Size
- MS-28098 - Indicator, Turn and Slip, Air Driven, 2-Inch Case, ARU-8a and ARU-9/a
- MS-3318 - Case, Instrument, 5 X 4-1/4 Size, Standard Dimensions for
- MS-33545 - Case Instrument, 5 X 5-1/4, Standard Dimensions for
- MS-33558 - Numeral and Letters, Aircraft Instrument Dial, Standard Form of
- MS-33635 - Instrument, Flight, Basic, Standard Arrangement of (for Navy Use See ms-28112)
- MS-90367 - Indicator, Electrical, Wheels and Flaps Position
- QPL-18804 - Indicator, Vertical Speed, 0-6000 FPM, 2-Inch (Replaced by the Qualified Products Database (QPD) see Notice 1 for Additional Information)
- QPL-18856 - Indicator, Angle of Attack, 28V Dc Ms28062 and Ms28067 (No Superseding Document)
- QPL-19229 - Transmitter, Angle of Attack or Sideslip, Local (No Superseding Document)
- QPL-19570 - Indicator, Airspeed and Mach Number, Pitot Static, 80 To 850 Knots (No Superseding Document)
- QPL-19679 - Altimeter, Pressure, Counter-Pointer (No Superseding Document)
- QPL-21718 - Indicator, Airspeed, Pitot Static, Maximum Allowable Speed, 40-400 Knots (No Superseding Document)
- 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 (No Superseding Document)
- QPL-22068 - Indicator, Turn and Slip, Air-Driven, 2-Inch Case, ARU-8/a and ARU-9/a
- QPL-22145 - Accelerometer Group, Counting
- QPL-22433 - Indicator, Turn and Slip, Air Driven, 2-Inch Case, 20 Deg. Inclined Axis
- QPL-22858 - Attitude Indicating System, Remote Standby, Two Inch (No Superseding Document)
- QPL-23395 - Altimeter, Pressure, Counter-Pointer, Type mc-3 and mc-4 (No Superseding Document)
- QPL-23671 - Indicator, Ms17264, Airspeed & Mach Number, Integrally Lighted, Pitot Static, 80 To 850 Knots (See Notice for Replacement Information)
- QPL-25137 - Indicator, Airspeed, Mach Number and Maximum Allowable Speed, Type me-4
- QPL-25479 - Indicator, Mach Number, Sensitive, Servoed, Range .5 To 1.0, Type me-5 (No Superseding Document)
- QPL-25522 - Altimeter, Pressure, Drum&Pointer, Range&1000 To Plus 80,000 Feet, Type Md&1
- QPL-25627 - Transmitter, Synchro, Angle of Attack of Sideslip
- QPL-25632 - PITOT-Static Tube, Electrically Heated, Temperature Controlled, 115 Volt, 400 Cycle,Type ma-1
- QPL-25653 - Computer, Central Air Data, Type mg-1a (No Superseding Document)
- QPL-25719 - Accelerometer, Aircraft, Pilot S Warning, Type ma-1 (No Superseding Document)
- QPL-25757 - Pitot Static Tube TRU-1/a, Electrically Heated
- QPL-25915 - Accelerometer, Aircraft, Pilot S Warning, Type ma-2 (No Superseding Document)
- QPL-25931 - Indicator, Position, Landing Gear, Symbol-Indicating, Integrally Lighted (No Superseding Document)
- QPL-25941 - Indicator, Turn and Slip, 2 Inch Size 1Ntegrally Lighted (No Superseding Document)
- QPL-26359 - Indicator, Attitude, Remote ARU-4/a
- QPL-26360 - Amplifier, Electrical Control ASU-3/a
- QPL-26601 - Controller, Third Gimbal DCK-10/a24G-1
- QPL-26609 - Transmitter, Position (No Superseding Document)
- QPL-26689 - Horizontal Situation Indicator AQU-2/a (Indicator, Multiple, Air Navigation AQU-2/a) (No Superseding Document)
- QPL-27170 - Computer, Flight Director Cpu-4/a (No Superseding Document)
- QPL-27193 - Indicator, Attitude, ARU-2B/A
- QPL-27195 - Accelerometer, Aircraft, ABU-6/a (No Superseding Document)
- QPL-27196 - Indicator, Vertical Velocity Aau/9-a, Integrally Lighted (No Superseding Document)
- QPL-27197 - Indicator, Airspeed, Mach Number and Maximum Allowable Speed
- QPL-27198 - Altimeter, Pressure (No Superseding Document)
- QPL-27203 - Indicator, Position, Wing Flap
- QPL-27229 - Altimeter, Pressure AAU-8/a (No Superseding Document)
- QPL-27269 - Horizontal Situation Indicator Group AF/a24J-1 (No Superseding Document)
- QPL-27279 - Indicator, Mach Number AVU-11/a, Integral Lighting (No Superseding Document)
- QPL-27280 - Indicator, Indicated Airspeed AVU-10/a
- QPL-27328 - Amplifier-Indicator Group, Altitude-Vertical Speed a/a24G-7 (No Superseding Document)
- QPL-27329 - Amplifier-Indicator Group, Indicater Airspeed a/a24C-6
- QPL-27330 - Transmitter, Accelerometer, Linear TRU-3/a (No Superseding Document)
- QPL-27391 - Altimeter, Pressure AAU-2/a (No Superseding Document)
- QPL-27473 - Converter, Central Air Data ECK-8/a24g
- QPL-27478 - Pitot Tube TRU-42/a (No Superseding Document)
- QPL-27522 - Computer, Flight Director Cpu-27/a
- QPL-27619 - Indicators, Attitude Director
- QPL-27623 - Indicator, Attitude, Remote Standby, 2 Inch (No Superseding Document)
- QPL-27670 - Amplifier-Indicator Group, Indicated Airspeed a/a24G-10
- QPL-27671 - Amplifier-Indicator Group, Altitude-Vertical Speed a/a24G-11
- QPL-27672 - Indicator, Position ALU-4/a, Horizontal Stabilizer, Integrally Lighted (No Superseding Document)
- QPL-27673 - Indicator, True Airspeed AVU-15/a (No Superseding Document)
- QPL-27680 - Indicator, Attitude ARU-12/a, Remote
- QPL-27710 - Indicator, Attitude Remote
- QPL-27848 - Indicator, Horizontal Situation AQU-4/A
- QPL-27851 - Indicator, Indicated Airspeed AVU-17/a (No Superseding Document)
- QPL-27889 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/a, General Specification for and MTU-38/a Mounting Tray (No Superseding Document)
- QPL-27889/1 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-1
- QPL-27889/2 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-2, F-4 Aircraft
- QPL-27889/3 - Computer, Transducer, Altitude, Altitude Encoding Cpu-46/A-3, T-38 Aircraft
- QPL-38005 - PITOT-Static Tube
- QPL-38046 - Pitot Static Tube TRU-59( )/a
- QPL-38135 - Indicator, Indicated Airspeed AVU-19/a, Standby
- QPL-38137 - Amplifier Indicator Group, Altitude Vertical Speed a/a24G-17 (No Superseding Document)
- QPL-38138 - Amplifier-Indicator Group, Indicated Airspeed (No Superseding Document)
- QPL-38139 - Indicator, Vertical Velocity AAU-18/a Integrally Lighted Standby (No Superseding Document)
- QPL-38140 - Altimeter, Pressure AAU-16/a (No Superseding Document)
- QPL-38167 - Compensator, Central Air Data ECU-51/a (No Superseding Document)
- QPL-5098 - Indicator, Rate of Flow (No Superseding Document)
- QPL-5133 - Indicator, Attitude, Type J-8 (No Superseding Document)
- QPL-5154 - Indicator, True Airspeed, Type M-5 (No Superseding Document)
- QPL-5170 - Indicator, Position, Horizontal Stabilizer (No Superseding Document)
- QPL-5184 - Indicator, Position
- QPL-5191 - Computer and Transmitter, True Airspeed, Pitot Static, Type A-2
- QPL-5356 - Indicator, Airspeed, Pitot Static, Type L-7a (No Superseding Document)
- QPL-5388 - Machmeter, Pitot Static Operated, Range .5 To 1.5, Type A-2B (No Superseding Document)
- QPL-5392 - Indicator, Airspeed, Pitot Static, Type K-3 (No Superseding Document)
- QPL-5416 - Indicator, Indicated Airspeed, 10-150 Knots (No Superseding Document)
- QPL-5417 - Indicator, Airspeed, Pitot Static, 40-400 Knots
- QPL-5418 - Indicator, Airspeed, Pitot Static, Sensitive, 50-650 Knots (No Superseding Document)
- QPL-5420 - Tube, Pitot Static, Electrically Heated, Aircraft
- QPL-5421 - Tube, Pitot, Electrically Heated, Aircraft
- QPL-5488 - Indicator, Turn and Slip, 28V.D.C., 2-3/4 Size, Type md-10 (No Superseding Document)
- QPL-5489 - Indicator, Turn and Slip, Air Driven, 3 Inch Size
- QPL-5583 - Transmitter, Position, 28 Volts DC
- QPL-5721 - Indicator, Indicated Airspeed, Pitot Static 20-250 Knots
- QPL-5741 - Indicator, Directional, Gyroscopic, Type C-5C (No Superseding Document)
- QPL-5885 - Accelerometer, Aircraft
- QPL-6447 - Indicator, True Airspeed, Type M-1a (No Superseding Document)
- QPL-6568 - Indicator, Airspeed, Pitot Static, Type F-5
- QPL-6839 - Indicator, Position, Landing Gear
- QPL-6848 - Accelerometer, Aircraft Drawing an5745
- QPL-6863 - Altimeter Pressure 50,000 Feet, Type Mb - 1 (No Superseding Document)
- QPL-7063 - Indicator, Position, Rudder Trim Tab (No Superseding Document)
- QPL-7064 - Indicator, Position, Elevator Trim Tab (No Superseding Document)
- QPL-7065 - Indicator, Position, Aileron Trim Tab
- QPL-7066 - Indicator, Position, Flaps, 0-30 Degree Markings, 2-Inch (No Superseding Document)
- QPL-7067 - Indicator, Position, Flaps, 0-60 Degree Marking, 2 Inch Size (No Superseding Document)
- QPL-7132 - Indicator, Position, Nose Wheel Steering
- QPL-7231 - Indicator, True Airspeed, Synchro Repeater, Type N-1
- QPL-7356 - Indicator, True Airspeed, Pitot Static, Type M-4
- QPL-7373 - Computer, True Airspeed and Machnumber, Type C-2a
- QPL-7507 - Machmeter, Pilot Static, Range .3 To 1.0, Type A-1 (Cancelled, No Superseding Document)
- QPL-7627 - Indicator, Turn and Slip, 28V, 1-7/8 Inch Dial
- QPL-7721 - Indicator, Vertical Speed, 3-Inch
- QPL-7783 - Indicator, Angle of Attack
- QPL-7785 - Transmitter, Angle of Attack or Sideslip, Local
- QPL-7805 - Indicator, Turn and Slip, 4-Minute Turn
- QPL-7833 - Indicator, Airspeed and Mach Number, Pitot Static
- QPL-7906 - Indicator, Gyro Horizon, Manually Caged, Electric Type mb-1 (No Superseding Document)
- QPL-7968 - Position Indicating Assemblies, Electrical, Wheels and Flaps (No Superseding Document)
- QPL-8026 - Amplifier, Electronic Control, 2 Channel, True Airspeed and Mach Number, Type ma-1
- QPL-81403 - Altimeter-Encoder, AAU-21a (No Superseding Document)
- QPL-81454 - Indicator, Gyroscope Vertical Reference Id-1481(*)/a (No Superseding Document)
- QPL-81494 - Altimeter, Pressure, AAU-24/a
- QPL-81606 - Indicator, Attitude 3 Inch Id-1617/a (No Superseding Document)
- QPL-81655 - Pitot Static Tube, L-Shaped Compensated, Electrically Heated (No Superseding Document)
- QPL-81851 - Altimeter AAU-31/A
- QPL-81852 - Altimeter Encoder AAU-32/A
- QPL-8237 - Amplifier, Electric Control, True Airspeed Signal, Type ma-2 (No Superseding Document)
- QPL-8241 - Indicator, True Airspeed, Type Q-1 (No Superseding Document)
- QPL-8315 - Indicator, Airspeed and Mach Number, Pitot Static, Type me-1 (No Superseding Document)
- QPL-83344 - Converter, Altitude Code ECU-87/ A
- QPL-83345 - Altimeter, Encoder, Counter Drum Pointer AAU-33/a (No Superseding Document)
- QPL-83392 - Indicator, Attitude (No Superseding Document)
- QPL-83419 - Altimeter, Servo Controlled, Automatic Pressure Standby
- QPL-8580 - Indicator, Tachometer, Helicopter, 0-4,000 Rpm, Type ma-1
- QPL-8687 - Indicator, Turn and Slip, Air Driven, 2-Inch Size
- QPL-9075 - Computer and Transmitter, True Airspeed, PITOT-Static, 150-900 Knots, Type ma-1 (No Superseding Document)
- QPL-9130 - Transmitter, Altitude, Range -1,000 To &80,000 Feet, Type mc-2
- QPL-9182 - Indicator, Phase Sequence, 200 Volt 400 Cycle Ac, Type A-1