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North American X-15 Flight manual
USAF SERIES
X-15
AIRCRAFT
This publication supplements FHB-23-1. Reference
to this supplement will be made on the title page of
the basic manual by personnel responsible for maintaining
the publication in current status.
7 February 1962
1. PURPOSE
To provide information on airplane control surface deflections during
captive-flight checks of the MH-96 adaptive flight control system
installed on Airplane AF56-6672.
2. GENERAL
During captive-flight checks of this system, transient control surface
deflections have caused concern regarding the possibility of exceeding
captive flight limitations for control surface deflection.
3. INSTRUCTIONS
Test data concerning transient control surface deflections occuring
during captive-flight checks of the MH-96 system has been analyzed.
It has been determined that the maximum control surface deflections
encountered are well within the limitations given in Section V under
Captive Flight Limitations.
END
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