SAE AIR5026
TEST CELL INSTRUMENTATION
Historical
Standard by SAE International, 1996-11-01
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About This Item
This document discusses, in broad general terms, typical present instrumentation practice for post-overhaul gas turbine engine testing. Production engine testing and engine development work are outside the scope of this document; they will use many more channels of instrumentation, and in most cases will have requirements for measurements that are never made in post-overhaul testing, such as fan airflow measurements, or strain measurements on compressor blades.
The specifications for each parameter to be measured, in terms of measurement range and measurement accuracy, are established by the engine manufacturers. Each test cell instrument system should meet or exceed those requirements. Furthermore, each instrument system should be recalibrated regularly, to ensure that it is still performing correctly.
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Standard Details
- Publication Date: 1996-11-01
- Standard Status: historical
- Publisher: SAE International
- Document Type: Aerospace Standard
- Subject: Auxiliary power units, Marine engines, Jet engines, Turbofan engines, Electronic control units, Turbojet engines, Pressure, Test facilities, Turboprop engines
- Official SAE: Doi link
Document History
- New Version Available: AIR5026B (2020-10-21)
- Previous Version: AIR5026A (2011-08-01)
- This Version: AIR5026 (1996-11-01)
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