LuckyDuc...
Here are some 'specs' that may help You find answers to Your question.
NOTE.
I originally intended to copy/paste info from each spec: however, there are MANY factors to consider that made this impractical. For this reason, I suggest reviewing each spec for the obvious spacing/clearance discussion... and the practical mitigating factors to be wary of, such as: installation and maintenance, routing variations/issues; affects of operational and natural environment such as temperature and moisture affects, cable tension/vibration, load-induced deflections [cables and bracket strains, flexing of wire harnesses, flexing of fluid tubing, etc]; and real-world operational testing for system friction and binding, flutter, wear-and tear, electrical bonding/isolation, etc, etc.
MIL-F-18372 [CX, 1955] FLIGHT CONTROL SYSTEMS: DESIGN, INSTALLATION AND TEST OF, AIRCRAFT (GENERAL SPECIFICATION FOR)
... replaced by...
SAE AS94900 Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For
AFGS-87242 AIR FORCE GUIDE SPECIFICATION - FLIGHT CONTROL SYSTEM GENERAL SPECIFICATION FOR
...replaced by...
JSSG-2008 VEHICLE CONTROL AND MANAGEMENT SYSTEMS [controlled distribution]
JSSG-
JSSG-2009 AIR VEHICLE SUBSYSTEMS
Regards, Wil Taylor
o Trust - But Verify!
o We believe to be true what we prefer to be true. [Unknown]
o For those who believe, no proof is required; for those who cannot believe, no proof is possible. [variation,Stuart Chase]
o Unfortunately, in science what You 'believe' is irrelevant. ["Orion"]
o Learn the rules like a pro, so you can b