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Test Operations Procedure (TOP) 7-3-057 Pitot-Static System Calibrations

Authors: ARMY AVIATION TECHNICAL TEST CENTER FORT RUCKER AL
 
Abstract: This Test Operations Procedure (TOP) describes the test requirements, objectives, responsibilities, and techniques/methodologies required to perform pitot-static system calibrations. This TOP is used for rotary-wing and fixed-wing aircraft. The TOP will facilitate test planning, execution, and data collection using two techniques (trailing device and pace) and the equipment required to complete pitot-static system calibrations. Variations in platform requirements are discussed within this TOP. These guidelines, along with platform specific capabilities and requirements, will enable the tester to develop a comprehensive testing strategy.

Limitations: APPROVED FOR PUBLIC RELEASE
Description: Final rept.
Pages: 35
Report Date: 10 APR 2008
Report Number: A460384
Keywords relating to this report:
*FLIGHT TESTING
*ROTARY WING AIRCRAFT
*STATICS
AIRSPEED
CALIBRATION
CENTER OF GRAVITY
DATA ACQUISITION
DATA REDUCTION
FIXED WING AIRCRAFT
METHODOLOGY
MILITARY STANDARDS
PILOTS
PITOT TUBES
STATIC PRESSURE
TEST AND EVALUATION
TEST METHODS
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