FSC-6610: Flight Instruments
Documents
- MIL-I-83336 – Indicator, Attitude, Self-Contained, 3-Inch General Specification for (No S/S Document)
- MIL-I-83336/1 – Indicator, Attitude, Self-Contained, 3-INCH, ARU-44/A-1 (No S/S Document)
- MIL-I-83336/2 – Indicator, Attitude, Self-Contained, 3-Inch, ARU-44/A-2 (No S/S Document)
- MIL-I-83336/3 – Indicator, Attitude, Self-Contained, 3-Inch, ARU-30/A-1 (No S/S Document)
- MIL-I-83336/4 – Indicator, Attitude, Self-Contained, 3-Inch, ARU-30/A-4 (No S/S Document)
- MIL-I-83336/5 – Indicator, Attitude, Self-Contained, 3-Inch, ARU-30/A-3 (No S/S Document)
- MIL-I-83362 – Indicator, Position, Takeoff Trim ALU-12/A
- MIL-I-83365 – Indicator, Horizontal AQU-10/A (No S/S Document)
- MIL-I-83392 – Indicator, Attitude (No S/S Document)
- MIL-I-83868 – Indicator, Position Horizontal Stabilizer (No S/S Document)
- MIL-I-8394 – Indicator, Airspeed, Pitot Static, Sensitive, 50-700 MPH, Fluorescent Markings, Type F-6 (Supersedes 21208) (No S/S Document)
- MIL-I-85506 – Indicator, Indicated Airspeed, Standby Types I, II, and III (No S/S Document)
- MIL-I-8687 – Indicator, Turn and Slip, Air-Driven, 2-Inch Size (No S/S Document)
- MIL-I-8762 – Indicator, Trim, Control Surface, Type O-1 (Supersedes 27462-C) (No S/S Document)
- 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 (No S/S Document)
- MIL-I-9182 – Indicator, Phase Sequence, 200 Volt 400 Cycle AC, Type A-1 (Supersedes 32645) (No S/S Document)
- MIL-I-9471 – Indicator, Indicated Airspeed, Pitot Static, Type MN-1 (No S/S Document)
- 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) (No S/S Document)
- MIL-M-7507 – Machmeter, Pitot Static, Range .3 to 1.0, Type A-1
- MIL-O-87243 – OFFENSIVE AVIONICS (NO S/S DOCUMENT)
- MIL-P-25632 – PITOT STATIC TUBE, ELECTRICALLY HEATED, TEMPERATURE CONTROLLED, 115 VOLT, 400 HZ, TYPE MA-1 (NO S/S DOCUMENT)
- MIL-P-25757 – PITOT STATIC TUBE TRU-1/A, ELECTRICALLY HEATED
- MIL-P-25945 – PITOT TUBE, ELECTRICALLY HEATED, TEMPERATURE CONTROLLED (NO S/S DOCUMENT)
- MIL-P-26292 – PITOT AND STATIC PRESSURE SYSTEMS, INSTALLATION AND INSPECTION OF (NO S/S DOCUMENT)
- MIL-P-27478 – PITOT TUBE TRU-42/A (NO S/S DOCUMENT)
- MIL-P-38005 – PITOT-STATIC TUBE (NO S/S DOCUMENT)
- MIL-P-38046 – PITOT STATIC TUBE TRU-59( )/A
- MIL-P-38136 – PITOT STATIC TUBE, COMPENSATED TRU-62/A (NO S/S DOCUMENT)
- MIL-P-38244 – PITOT STATIC TUBE TRU-74/A, ELECTRICALLY HEATED (NO S/S DOCUMENT)
- MIL-P-7968 – POSITION INDICATING ASSEMBLIES, ELECTRICAL, WHEELS AND FLAPS (NO S/S DOCUMENT)
- MIL-P-81655 – Pitot Static Tube, L-Shaped, Compensated, Electrically Heated, General Specification for (No S/S Document)
- MIL-P-83206 – PITOT STATIC TUBE, L SHAPED, COMPENSATED, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT)
- MIL-P-83207 – PITOT- STATIC TUBE, NOSE BOOM, COMPENSATED, GENERAL SPECIFICATION FOR (NO S/S DOCUMENT)
- MIL-PRF-27197 – Indicator, Airspeed, Mach Number and Maximum Allowable Speed (No S/S Document)
- MIL-PRF-38135 – Indicator, Indicated Airspeed AVU-19/A, Standby (No S/S Document)
- 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 S/S 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 S/S DOCUMENT)
- MIL-STD-1524 – TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED (NO S/S DOCUMENT)
- MIL-STD-843 – ALTIMETER, PRESSURE, GENERAL TEST REQUIREMENT FOR ( NO S/S DOCUMENT)
- MIL-STD-884 – ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION (NO S/S DOCUMENT)
- MIL-T-19229 – TRANSMITTER, ANGLE OF ATTACK OR SIDESLIP, LOCAL, MS28006 (NO S/S DOCUMENT)
- MIL-T-21959 – TRANSMITTER, TRUE AIRSPEED, PITOT STATIC, 100 TO 300 KNOTS, TRU-24/A (NO S/S DOCUMENT)
- MIL-T-25066 – TRANSMITTER, ALTITUDE, RANGE MINUS 1000 TO PLUS 80,000 FEET, TYPE MC-4 (NO S/S DOCUMENT)
- 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 S/S Document)
- MIL-T-5420 – Tubes, Pitot Static, 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 S/S 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-83208 – TRANSMITTER, ACCELEROMETER, ANGULAR
- MIL-T-83460 – TRANSDUCER, MOTIONAL PICKUP TRU-164/A (NO S/S 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-V-17344 – VIAL INCLINOMETER (FOR ILLUMINATED SIGHTS)
- MS14114 – GYROSCOPE, DISPLACEMENT, ROLL AND PITCH (HARD MOUNTED) (S/S BY SAE-AS14114)
- MS17249 – INDICATOR, REMOTE ATTITUDE (NO S/S DOCUMENT)
- MS17264 – INDICATOR, AIRSPEED AND MACH NUMBER, INTEGRALLY LIGHTED PITOT STATIC, 80 TO 850 KNOTS (NO S/S DOCUMENT)
- MS17313 – INDICATOR, GYRO HORIZON, MANUALLY CAGED, ELECTRIC, TYPE MB-1 (NO S/S DOCUMENT)
- MS17373 – INDICATOR, ATTITUDE, TWO-INCH, SELF-CONTAINED
- MS17398 – Gyroscope, Displacement, Roll and Pitch
- MS17399 – Gyroscope, Rate Switching
- MS17400 – Indicator, Attitude, Remote - 3 Inch Case
- MS17401 – Indicator, Attitude, Remote - 5 Inch Case (No S/S Document)
- MS17869 – Indicator, Horizontal Situation, ID-1013/A (No S/S Document)
- MS18028 – Indicator, Attitude - Director, Remote (IFIS) (No S/S Document)
- MS18119 – INDICATOR, ATTITUDE-DIRECTOR, REMOTE, 3INCH CASE (NO S/S DOCUMENT)
- MS21349 – Case, Instruments, Vertical Scale, Standard Dimensions for (No S/S Document)
- MS23009 – Accelerometer-Aircraft, Integrally Lighted ABU-4A/A and ABU-4B/A
- MS24499 – TUBE, PITOT, ELECTRICALLY HEATED L SHAPED (NO S/S DOCUMENT)
- MS24500 – TUBE, PITOT, ELECTRICALLY HEATED, L SHAPED, INVERTED (NO S/S DOCUMENT)
- MS24501 – TUBE&PITOT, ELECTRICALLY HEATED
- MS24550 – Transmitter, Position
- MS24579 – INDICATOR&GYRO HORIZON
- MS24580 – INDICATOR&DIRECTIONAL GYRO
- MS25333 – Indicator, Indicated Airspeed, Pitot Static Maximum Allowable Speed, 40-400 Knots
- MS25396 – TRANSMITTER, REMOTE COMPASS (THIN WING) (NO S/S DOCUMENT)
- MS25447 – Transducer, Counting Accelerometer
- MS25448 – 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 (NO S/S DOCUMENT)
- MS25454 – INDICATORS, VERTICAL VELOCITY, RAPID RESPONSE, ACCELERATION SENSITIVE (NO S/S DOCUMENT)