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attachment 2 section i ? technical specifications commuter coach ...

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Page 48<br />

ATTACHMENT 2<br />

once at any point, including pre-bending and installation. Rigid lines shall be supported consistent with<br />

standard automotive practice. Nylon lines may be grouped and shall be continuously supported.<br />

The compressor discharge line between powerplant and body mounted equipment shall be flexible<br />

convoluted copper or stainless steel line, or may be flexible teflon hose with a braided stainless steel<br />

jacket. Other lines necessary to maintain system reliability shall be flexible teflon hose with a braided<br />

stainless steel jacket. End fittings shall be standard SAE or JIC brass or steel, flanged, reusable, swivel<br />

type fittings. Flexible hoses shall be as short as practicable and individually supported. They shall not<br />

touch one another or any part of the <strong>coach</strong> except for the supporting grommets. Flexible lines shall be<br />

supported at 2 foot intervals or less. Airlines shall be installed to minimize air leaks. Each <strong>coach</strong> shall<br />

not leak down more than 6 psi. as indicated on the instrument panel mounted air gauges, within 15<br />

minutes from the point of governor cut-off.<br />

All reservoir supply and delivery airlines shall be sloped toward reservoirs and routed to prevent water<br />

traps. Grommets shall protect the airlines at all points where they pass through understructure<br />

components. Provision shall be made to apply shop air to a convenient location in the engine<br />

compartment and at the front of the <strong>coach</strong> and shall include a Schrader standard bore valve. The engine<br />

compartment Schrader valve shall be located ahead of a quarter turn valve. Air for the compressor shall<br />

be filtered through the main engine air cleaner system. All air reservoirs shall meet the requirements of<br />

SAE Standard J10 and shall be equipped with clean-out plugs and quarter-turn drain valves. These<br />

valves and any automatic moisture ejector valves shall be protected from road hazards by major<br />

structural members. Reservoirs shall have an internal siphon hose for the drain valve. The air system<br />

shall be protected by a pressure relief valve set at 150 psi and shall be equipped with check valves and<br />

pressure protection valves to assure partial operation in case of line failures.<br />

The main airline check valve located between the air compressor and the first reservoir must be<br />

accessible for maintenance. Means shall be provided to establish the check valve to be in working<br />

order.<br />

A model Bendix AD-IP air dryer shall be provided and installed according to component<br />

manufacturer’s recommendations. The air drier shall be rated at 90 watts. A Bendix Puraguard filter,<br />

shall be provided. The Puraguard filter shall be installed between the air dryer and the wet tank.<br />

Separator shall be within four feet of the air dryer. Inlet air temperature is not to exceed 150 degrees F<br />

from the compressor.<br />

3.6 GENERAL CHASSIS<br />

3.6.1 WHEELS AND TIRES<br />

3.6.1.1 WHEELS<br />

Wheels shall be Alcoa hub piloted polished aluminum wheels with Durabrite coating. All wheels shall<br />

be interchangeable and shall be removable without a puller. Wheels shall be compatible with tires in<br />

size and load-carrying capacity. Front wheels and tires shall be balanced as an assembly. Wheels shall<br />

be capable of accommodating Michelin, Load Range L radial tires. One spare wheel, complete with<br />

mounted tire shall be provided.

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