MIL-F-18372(Aer)
Type I - Mechanical Control System - An irreversible control system wherein the pilot
actuates the secondary control surfaces or devices of the aircraft through a
set of mechanical linkages consisting of cables, pulleys, sectors and/or push-pull
or torque tubes with horns, bellcranks, etc.
Type II - Power Operated Control System - An irreversible control system wherein the pilot
actuates a switch which causes a power unit (electro-mechanical actuator or
hydraulic control) to move the trim surfaces or devices.
1.2.3 Flight Path Angle and Speed Controls - Controls for the actuation of the flight path angle
and speed controls systems may be of the following types:
Type I - Power Operated Control - A control system wherein the pilot actuates a switch or
hydraulic control valve which causes a power unit (electro-mechanical or hydraulic)
to move the flight path angle or speed control devices.
Type II - Automatic - A control system wherein the control surface is automatically
actuated by the aerodynamic forces.
2. APPLICABLE DOCUMENTS
2.1 The following specifications, standards, drawings, and publications, of the issue in effect
on the date of invitation for bids, forms a part of this specification.
SPECIFICATIONS :
Military
MIL-B-7949 Bearing; Ball, Anti-Friction, Airframe
MIL-B-6038 Bearing; Ball, Bellcrank, Anti-Friction, Airframe
MIL-B-6039 Bearings; Ball, Rod End, Anti-Friction, Airframe
MIL-B-5628 Bearings; Plain, Airframe
MIL-B-5629 Bearings; Rod End, Plain, Airframe
MIL-C-1511 Cable; Steel (Carbon), Flexible, Preformed
MIL-C-5424 Cable; Steel (Corrosion Resistant), Flexible-Preformed (For Aeronautical Use)
MIL-C-5688 Cable; Assemblies; Aircraft, Proof-Testing and Prestretching of
MIL-C-5638 Casing; Control Cable Flexible, Aircraft
MIL-F-8785(ASG) Flying Qualities of Piloted Airplanes
MIL-A-8629(Aer) Airplane Strength and Rigidity
MIL-H-8501 Helicopter Flying Qualities, Requirements for
MIL-S-8698(ASG) Structural Design Requirements, Helicopters
MIL-T-8679 Test Requirements-Ground, Helicopters
MIL-H-5440 Hydraulic Systems; Design, Installation and Tests of Aircraft (General
Specification For)
MIL-J-6193 Joints; Universal, Plain, Light and Heavy Duty, Aircraft
MIL-L-44380 Lubrication of Aircraft, General Specification For
MIL-P-7034 Pulleys, Control, Anti-Friction Bearing, Grease-Lubricated Aircraft
JAN-T-781 Terminal; Cable; Steel (For Swaging)
MIL-T-6117 Termianl - Cable Assemblies; Swaged Type
MIL-T-5685 Turnbuckles; Aircraft
MIL-T-5522 Test Procedure For Aircraft Hydraulic System
MIL-W-5013 Wheel and Brake Assemblies; Aircraft
MIL-P-5518 Pneumatic Systems; Design, Installation and Tests in Aircraft
Bureau of Aeronautic
SD-24 General Specification for the Design and Construction of Airplanes for the
United States Navy
SR-6 Contract Design Data Requirements for Aircraft
SR-38 Demonstration-of Piloted Airplanes
SR-159 Stability and Control Calculations
SR-189 Aerodynamic, Structural, and Power Plant Requirements for Helicopter.
2
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