Table 1. UH-1H/M Flight Plans and Test States

TASK 1 - TEST EQUIPMENT INSTALLATION/CHECKOUT - TM-1-6625-724-13P_518

TM-1-6625-724-13P Aviation Vibration Analyzer Manual
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TM 1-6625-724-13&P 0074 00 0074 00-3 Table 1. UH-1H/M Flight Plans and Test States Flight Plan Test States Test Condition FLIGHT IDLE 226 Rotor RPM (Nr) FPG100 Flat Pitch, 324 Rotor RPM (Nr) HOVER Hover 60K 60 Kts, Level Flight 90K 90 Kts, Level Flight 110K 110 Kts, Level Flight L/DOWN L/Down: 70 Kts at 1000 Ft/Min Descent GNDTRK Idle 226 Rotor RPM Fpg100 Flat Pitch, 324 Rotor RPM (Nr) INITIAL IDLE Flat Pitch, 226 Rotor RPM (Nr) FPG100 Flat Pitch, 324 Rotor RPM (Nr) HOVER Hover PROBES ACC1 Used as required ACC2 User must denote ACC3 location and orientation ACC4 tail Fpgtl Tail Balance - Flat Pitch, 324 Rotor RPM (Nr)

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