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GAS TURBINE STARTER (JET FUEL STARTER) SPECIFICATION
- Aerospace Standard
- AS1606
- Issued
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This specification establishes the requirements for the (TBS) jet fuel starter for the (TBS) gas turbine engine used in the (TBS) aircraft.
Recommended Content
| Aerospace Standard | Guide to Engine Lubrication System Monitoring |
| Aerospace Standard | Turbine Flowmeter Fuel Flow Calculations |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| Unnamed Dataset 3 | ||
| TABLE 1 | Performance Ratings | |
| TABLE 2 | Fuel Contamination Levels | |
| TABLE 3 | Test Performance Ratings | |
| TABLE 4 | Unit Usage | |
| TABLE 5 | Particle Sizing |
Issuing Committee
AE-6 Starting Systems and Auxiliary Power Committee
Welcome to the SAE AE-6, Starting Systems and Auxiliary Power Committee public forum area.
Scope: Devotes itself to aircraft engine starting by electrical, hydraulic, or pneumatic means using stored energy sources such as batteries, hydraulic accumulators, solid or liquid propellants, stored gas, or small gas turbine engines. Develops standards for aircraft starting systems. Charter: Establish standards for aerospace and industrial engine starting, auxiliary power, and related secondary systems. For details about SAE's online privacy policy; copyright, content license, and reliability statements; and membership information, click on the link to "Info on Privacy, Copyright, and Membership" line in the folders area below. No copyrighted material may be posted in this forum. SAE is not liable for opinions expressed or information posted to this forum. All information posted becomes the property of SAE.Reference
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