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Standard

Safety Criteria for Pneumatic Starting Systems

1999-03-01

CURRENT

AIR1639A

This SAE Aerospace Information Report (AIR) presents safety criteria for pneumatic type engine starting system design and component hardware. Included are safety criteria in design of both starter control valves and starters as well as in design of airframe control systems. Safety topics concern starter valve operation and material application, airframe controls and instrumentation installations and starter rotor integrity and containment.

Standard

SAFETY CRITERIA FOR PNEUMATIC STARTING SYSTEMS

1994-02-01

HISTORICAL

AIR1639

Standard

CARBURETOR FLANGE, AIRCRAFT 2 Bolt - Single Barrel - No. 3 and 4

1995-05-01

HISTORICAL

AS62

Standard

VALVE, STARTER CONTROL, PNEUMATIC, AIRCRAFT ENGINE GENERAL SPECIFICATION FOR

1992-05-08

CURRENT

AS1607A

This specification covers the general requirements for pneumatic control valves for use with the starters on aircraft gas turbine engines. This specification shall be used in conjunction with AS943, ARP949, and AIR1639.

Standard

D-C STARTER-GENERATOR, ENGINE, GENERAL SPECIFICATION FOR

1994-09-01

CURRENT

ARP892

This recommended practice covers requirements for turbine engine-generators designated as follows:

Standard

GAS TURBINE STARTER (JET FUEL STARTER) SPECIFICATION

1992-09-01

CURRENT

AS1606

This specification establishes the requirements for the (TBS) jet fuel starter for the (TBS) gas turbine engine used in the (TBS) aircraft.

Standard

AIRCRAFT HYDRAULIC STARTERS

1965-04-01

HISTORICAL

AS714

This Aerospace Standard establishes the common requirements for hydraulic starters, suitable for use in aircraft and missiles, and the methods to be used for demonstrating compliance with these requirements.

Standard

STARTER, PNEUMATIC, AIRCRAFT ENGINE, GENERAL SPECIFICATION FOR

1968-01-01

HISTORICAL

AS943

The starters covered by this specification shall be designed to operate on compressed air from ground support equipment, engine interbleed or on board air supply.

Standard

Pneumatic Ground Power Supplies for Starting Aircraft

2004-04-06

CURRENT

AIR944C

The material contained in this report has been simplified to facilitate its use. Specific manufacturers should be contacted for more detailed information. Many of the basic power supplies are available in numerous configurations and some provide shaft power or electrical power in addition to the pneumatic capability. Vehicles for the ground transportation of the power supplies are also varied to fit specific requirements.