MIL-DTL-62013E(AT)
3.3.8.3 Communication and electrical circuits. Communication and electrical circuits shall
maintain continuity from end to end, without shorts from pin to pin, or from pin to connector shell
(see 4.5.2 and 4.5.12.3).
3.3.8.4 System voltage characteristics. Electrical system voltage characteristics shall fall
within the limits for transient and steady state voltage requirements specified in MIL-STD-1275
(see 4.5.12.4).
3.3.8.5 Electromagnetic interference suppression. The vehicle, when operating, shall
meet the requirements for EMI/EMC suppression in Army ground vehicles as specified in
MIL-STD-461 (see 4.5.12.5).
3.3.8.6 Heaters. The personnel and cargo area heaters shall start and operate
satisfactorily on 20 Vdc, using diesel fuel conforming to A-A-52557 (see 4.5.2 and 4.5.12.6).
3.3.9 Controls. All electrical, mechanical and hydraulic controls shall operate without
malfunction throughout all ranges of operation under all vehicle operating conditions (see 4.5.2
and 4.5.13).
3.3.10 Adjustment mechanisms. All adjustment mechanisms shall function properly and
maintain adjustment within required settings during all vehicle operating conditions (see 4.5.2
and 4.5.14).
3.3.11 Stowed material. All interior and exterior on vehicle material (OVM), when
stowed on the vehicle in the spaces provided, shall fit properly and not interfere with the
operation of the vehicle and components in any manner (see 4.5.15).
3.3.12 Folding blast covers (M730A1). The folding blast covers shall provide protection
for the crew compartment when launching a missile. The blast covers shall fold open and remain
open to permit vehicle operation without cover closing on operator (see 4.5.16).
3.3.13 Tailgate (M730A1). The tailgate shall hinge downward and support the weight of
two men during manual missile loading of the launcher. When closed the tailgate shall be sealed
to restrict the entrance of water into the vehicle during fording and flotation operations
(see 4.5.17).
3.3.14 Air transportability (M730A1). The vehicle when mated with its missile pallet
shall be capable of Phase II transport in a C-130 aircraft (see 4.5.18).
3.4 Break-in run. Unless otherwise specified (see 6.2), prior to being subjected to testing,
each vehicle shall be given a break-in run (see 4.5.3). Break-in is not intended to be a part of any
test but is carried out by the contractor to ensure that the vehicle is in a safe, operable condition
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