Stability and control flight tests were conducted on the OH-4A helicopter to determine the stability and control characteristics throughout the flight envelope for the unarmed (clean) and armed configurations. Ninety-three test flights were conducted for 75:30 hours productive test time. All test data were hand recorded from sensitive instruments or recorded on an oscillograph. The quantitative test results and qualitative pilot's comments indicate that the OH-4A complied with most of the stability and control requirements of MIL-H-8501A.


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