Browse Standards ARP1217A
Current REVISED 1997-05-01

Instrumentation Requirements for Turboshaft Engine Performance Measurements ARP1217A

This SAE Aerospace Recommended Practice (ARP) defines the measurement parameters that may be used by a pilot or operator to monitor the thermodynamic health of a turboshaft engine in a helicopter and the measurement system accuracies desired.
ARP1217A
1997-05-01
Latest
Revised
ARP1217
1979-05-01
Historical
Issued

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 11% off list price.
Login to see discount.
Special Offer: AeroPaks offers a customized subscription plan that is cost-effective and allows you to choose the number of downloads and Aerospace and Aerospace Material documents you need. Find more information here.
We also recommend:
STANDARD

Physical Modeling Techniques for Jet Engine Test Cell Aerodynamics

AIR4827B

View Details

STANDARD

Design Considerations for Enclosed Turboshaft Engine Test Cells

AIR4989A

View Details

STANDARD

Turboshaft/Turboprop Gas Turbine Engine Test Cell Correlation

ARP4755C

View Details

Get Involved

Want to participate in updating this standard?

X