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Standard

Aircraft Accessory Drag Torque During Engine Starts

1999-04-01
CURRENT
AIR1087B
This SAE Aerospace Information Report (AIR) presents a discussion of drag torques of engine accessories operating at cold temperature. Various conditions of temperature, speed, and acceleration rates are reviewed showing the merits of each method and recommending a standard test method.
Standard

Index of Starting System Specifications and Standards

2001-12-07
CURRENT
AIR1174B
This report lists military and industry specifications and standards which are used in aerospace engine starting and auxiliary power systems. Listings are provided as follows: Section 2. Topic Listing Section 3. Numerical Listing Section 4. Alphabetical Listing Only those hardware standards which have been specifically designed for engine starting systems are listed. Revisions and amendments which are current for these specifications and standards are not listed.
Standard

INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS

1970-07-15
HISTORICAL
AIR1174
This report lists military and industry specifications and standards which are used in aerospace engine starting systems. Only those hardware standards which have been specifically designed for engine starting systems are listed. Revisions and amendments which are current for these specifications and standards are not listed.
Standard

INDEX OF STARTING SYSTEM SPECIFICATIONS AND STANDARDS

1991-05-01
HISTORICAL
AIR1174A
This report lists military and industry specifications and standards which are used in aerospace engine starting and auxiliary power systems. Only those hardware standards which have been specifically designed for engine starting systems are listed. Revisions and amendments which are current for these specifications and standards are not listed.
Standard

Gas Energy Limited Starting Systems

1999-04-01
CURRENT
AIR1467B
This SAE Aerospace Information Report (AIR) presents information on gas energy limited propulsion engine starting systems employed in commercial and military applications and remote industrial sites. The types of systems discussed utilize solid propellant cartridge gas, monopropellant hydrazine gas, bipropellant gas, compressed stored gas, and cryogenic stored nitrogen. Presented information conveys design features, performance capabilities and system limitations with methods of computing results.
Standard

A MEANS OF TESTING TURBOJET ENGINE STARTER PERFORMANCE

1963-11-01
HISTORICAL
ARP715
This Recommended Practice covers a means of determining the performance acceptability of new production or overhauled starters that will be used for cranking turbine engines and is intended for use where torque measuring equipment is not available or desirable. This method determines acceptability of the overall performance of the starter on a flywheel test stand, rather than the performance at specific speed conditions. It allows a slight variation of output torque outside specified limits, as long as the overall performance is up to standard.
Standard

PERFORMANCE ACCEPTANCE TESTING OF AIR TURBINE STARTERS

1994-02-01
CURRENT
ARP715A
This Aerospace Recommended Practice describes two performance acceptance test methods to determine the performance acceptability of new production and overhauled air turbine starters. Before a new or overhauled starter is delivered to a customer, the starter is subjected to a performance acceptance test in accordance with an acceptance test procedure. The performance acceptance test is intended to ensure that the customer receives a starter that meets or exceeds minimum starter performance requirements.
Standard

PNEUMATIC GROUND POWER SUPPLIES FOR STARTING AIRCRAFT

1978-01-01
HISTORICAL
AIR944A
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. The state-of-the-art in small gas turbines has advanced to a point where they are competitive with the more conventional ground power supplies in practically all areas.
Standard

PNEUMATIC POWER SUPPLIES FOR STARTING AIRCRAFT

1988-10-01
HISTORICAL
AIR944
The information 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 plants are available in numerous configurations to 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. The state-of-the-art in small gas turbines has advanced to a point where they are competitive with the more conventional ground power supplies in practically all areas.
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.
Standard

PNEUMATIC GROUND POWER SUPPLIES FOR STARTING AIRCRAFT

1990-02-01
HISTORICAL
AIR944B
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.
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