SAE ARP5770
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
Mechanical Control Design Guide
Hardcopy , PDF
English
01-11-2012
28-11-2022
1. SCOPE
2. REFERENCES
3. SYSTEM CONSIDERATIONS
4. CONTROL SYSTEM INSTALLATION GUIDELINES
5. COMPONENT DESIGN GUIDELINES
6. CONTROL SYSTEM DESIGN DOCUMENTATION
7. NOTES
Specifies guidelines for the configuration and design of mechanical control signal transmission systems and subsystems.
| DocumentType |
Standard
|
| Pages |
98
|
| PublisherName |
SAE International
|
| Status |
Superseded
|
| SupersededBy |
This SAE Aerospace Recommended Practice (ARP) provides guidelines for the configuration and design of mechanical control signal transmission systems and subsystems. It is focused on the recommended practices for designing cable and pulley, pushrod and bellcrank and push-pull flexible cable control systems. These systems are typically used in some combination to transmit pilot commands into primary, secondary and utility control system commands (mechanical or electrical) or aircraft surface commands. On mechanically controlled aircraft, most pilot control commands are initiated through cockpit mounted wheels, sticks, levers, pedals or cranks that are coupled by pushrods or links to cable systems. The cable systems are routed throughout the aircraft and terminated in close proximity to the commanded surface or function where cranks and pushrods are again used to control the commanded function.
| FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
| MIL-PRF-7958 Revision D:2013 | Push-Pull Controls, Flexible and Rigid |
| MIL-F-8785 Revision C:1980 | Flying Qualities of Piloted Airplanes |
| AN665 Revision 6:2011 | Terminal-Threaded Clevis Type Tie Rod |
| MIL-DTL-83420 Revision P:2017 | Wire Rope, Flexible, for Aircraft Control, General Specification for |
| SAE AS21152D | BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, HOLLOW SHANK, SELF-ALIGNING, AIRFRAME, TYPE III, −65 TO 300 °F |
| MIL-B-8584 Revision C:1970 | Brake Systems, Wheel, Aircraft, Design of |
| MS21256 Revision G:2003 | Clip, Locking, Turnbuckle |
| MS21259 Revision K:2011 | Terminal, Wire Rope, Swaging, Stud, Long Thread |
| SAE AS21151E | BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, EXTERNAL THREAD, SELF-ALIGNING, AIRFRAME, TYPE II, −65 TO 300 °F |
| SAE AS21150E | BEARING, BALL, ROD END, DOUBLE ROW, PRECISION, SOLID SHANK, SELF-ALIGNING, AIRFRAME, TYPE I, −65 TO 300 °F |
| MIL-DTL-5541 Revision F:2006 | Chemical Conversion Coatings on Aluminum and Aluminum Alloys |
| MIL-STD-464 Revision C:2010 | Electromagnetic Environmental Effects Requirements for Systems |
| MIL-DTL-6117 Revision L:2008 | Wire Rope Assemblies, Aviation, Swaged Type |
| MIL-STD-461 Revision G:2015 | Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment |
| MIL-STD-203 Revision G:1991 | Aircrew Station Controls and Displays: Location, Arrangement and Actuation of, for Fixed Wing Aircraft |
| FAA AC 23.1309-1 : 2011 | SYSTEM SAFETY ANALYSIS AND ASSESSMENT FOR PART 23 AIRPLANES |
| SAE AS94900 | Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For |
| FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
| MIL-STD-1472 Revision G:2012 | Human Engineering |
| FAA AC 25.1309-1 : 0 | SYSTEM DESIGN AND ANALYSIS |
| MIL-DTL-5688 Revision E:2001 | Wire Rope Assemblies; Aircraft, Proof Testing and Prestretching of |
| MIL-PRF-16173 Revision E:1993 | Corrosion Preventive Compound, Solvent Cutback, Cold-Application |
| JSSG-2006 Base Document:1998 | Aircraft Structures |
| MS21251 Revision M:2002 | Turnbuckle Body, Clip Locking |
| MIL-DTL-87218 Revision E:2012 | Cable, Lockclad, for Aircraft Control |
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