Emergency stow mode and voltage protection

Page Title: Emergency stow mode and voltage protection
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MIL-T-63534(AR)

4.6.12 Velocity limit. Verify that the azimuth and elevation drive

outputs change meet the specified requirements of azimuth velocity limit and

evaluation velocity limit with application of the velocity limit.

4.6.13 Cross talk. Verify that there is no interaction between the

azimuth and elevation outputs as indicated in the specified requirements of

cross talk.

4.6.14 Gun firing interrupt signals. Verify that the gun interupt modes

meet the speed requirements of azimuth gun firing interrupt signals and

elevation gun firing interrupt signals.

4.6.15 Emergency stow mode and voltage protection. Verify that the

emergency stow operation mode meets the specified requirements of emergency

stow mode and voltage protection.

4.6.16 Current limiting, drive outputs. Verify that the current limit

for each drive output meet the specified requirement of current limiting,

drive outputs.

4.6.17 Slow slew velocity limit. Verify that the limits for azimuth and

elevation slew meet the specified requirements of slow slew velocity limit.

4.6.18 Tachometer dynamic input. Verify that the limits for the

tachometer inputs meet the llmits Of the specified requirement of tachometer

dynamic input.

4.6.19 Limit switch dynamic braking. Verify that the limits meet the

specified requirements of limit switch dynamic braking.

4.6.20 Elapsed time meter. Verify that the elapsed time meter advances

one hour when a-c power to the gun control has bee nactivated for one hour.

4.6.2.1 Workmanship. The specified requirements of assembly shall be

verified by continuous inspection of all parts and assemblies to assure

conformance to high quality workmanship.

4.6.22 Proof test (first article inspection only). Uhen specified in the

contract (see 6.2) three 3) Turret Control Units shall be forwarded to the

site specified by the contracting agency and assembled to an accepted

Universal Turret Subsystem (UTS). The Turret Control Units shall function in

accordance to the intent of the design and with no evidence of malfunction.

When approved by the contracting agency, this test may be performed at the

aircraft system level.

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