Table 1. OH-58 A/C Flight Plans and Test States

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TM-1-6625-724-13P Aviation Vibration Analyzer Manual
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TM 1-6625-724-13&P 0072 00 0072 00-3 Table 1. OH-58 A/C Flight Plans and Test States Flight Plan Test States Test Conditions FLIGHT IDLE A – 245 RPM, Flat Pitch C/A 720 – 70% NR, Flat Pitch 35% TQ A – 103% NR, 30psi TQ C/A 720 – 100% NR, 35% TQ Hover IGE Hover into the wind Climb 60Kts, at 1000 ft/min Climb 80K 80Kts, Level Flight 110K 110Kts, Level Flight L/DOWN 60Kts, 1000 ft/min Descent GRNDTRK Idle A – 245 RPM, Flat Pitch C/A 720 – 70% NR, Flat Pitch 35% tq A – 103% NR, 30 psi TQ C/A 720 – 100% NR, 35% TQ INITIAL IDLE A – 245 RPM, Flat Pitch C/A 720 – 70% NR, Flat Pitch 35% TQ A – 103% NR, 30 psi TQ C/A 720 – 100% NR, 35% TQ Hover IGE Hover into the Wind PROBES ACC1 ACC2 ACC3 ACC4 Use as Required TAIL FPGTL A – Tail Balance – Flat Pitch, 103% NR, 30 psi TQ C/A 720 – Tail Balance – Flat Pitch, 100% NR

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