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AE-6 Starting Systems and Auxiliary Power Committee Power and Propulsion Aircraft Fuels and Energy Sources Vehicles, Equipment, and Performance

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Standard

Introduction to Starting Systems
2004-04-13
CURRENT
AIR4151
This SAE Aerospace Information Report (AIR) covers basic aircraft engine start systems fundamentals. It presents various ground power sources and aircraft “on board” starting units. Also included are descriptions of start system components and interconnections which together comprise an engine starting system.
Standard

RECIPROCATING ENGINE PNEUMATIC STARTERS
1994-02-01
CURRENT
AIR4152
The purpose of this SAE Aerospace Information Report (AIR) is to present a brief discussion of pneumatic starters for reciprocating engines. This AIR also provides a general analysis guide for preliminary sizing of pneumatic starter systems for reciprocating engines.
Standard

COMMERCIAL AIRCRAFT AUXILIARY POWER UNIT INSTALLATIONS
1991-01-29
CURRENT
AIR4204
This Aerospace Information Report (AIR) reviews the factors to be considered in determining the location and arrangement for auxiliary power unit (APU) installations for airborne applications and reviews requirements for flight suitability. As treated in this discussion, the APU normally includes a power section (or engine), a starting system, an electronic control unit (ECU), a gearbox with accessory mounting pads, and an oil cooling system. The accessories that are driven by the APU, such as CSD's (constant speed drives), alternating current (AC) generators, hydraulic pumps, or air compressors, are not covered here except insofar as they make demands on the APU. The various installation components and systems that are covered here are outlined by the table of contents. Turbine-type APU's are by far the most highly developed and universally used airborne units, so their installation will dominate the discussion in this document.
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

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

AIRCRAFT HYDRAULIC START MOTOR
1994-02-01
CURRENT
AS714A
This Aerospace Standard (AS) establishes the requirements for hydraulic start motors suitable for use in starting a gas turbine engine, and the methods to be used for demonstrating compliance with these requirements.
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