0073 00 TM 1-6625-724-13&P 0073 00-6 Table 1. OH-58D Flight Plans and Test States Flight Plan Test States Test Condition FLI-SG 65% NR 65% NR, Flat Pitch (Use MPD) 35% TQ 35% TQ, 100% NR (Use MPD) Hover Hover (Stabilized Hover Into the wind) 60K 60 Kts, Level Flight 100K 100 Kts, Level Flight 110K 110 Kts, Level Flight L/DOWN 60 Kts at 1000 FT/Min Descent GNDTRK 65%-NR 65% NR, Flat Pitch (Use MPD) 35%-TQ 35% TQ, 100% NR (Use MPD) INT-SG 65%_ NR 65% NR, Flat Pitch (Use MPD) 35%_TQ 35%_TQ, 100% NR (Use MPD) PROBES ACC1 ACC2 ACC3 Used as required.  Operator is required to denote location and orientation of accelerometers. ACC4 TAIL 90% NR Flat Pitch, 90% NR (Use MPD) 100%NR Flat Pitch, 100% NR (Use MPD) Table 2. OH-58DM Flight Plans and Test States (Preferred Method) Flight Plan Test States Test Condition FLI-SG 65%NRC 65% NR, Pitch @ 17% eng. Tq.  (Use MPD) 35% TQ 35% TQ, 100% NR (Use MPD) Hover Hover (Stabilized Hover into the wind) 60K 60 Kts, Level Flight 100K 100 Kts, Level Flight 110K 110 Kts, Level Flight L/DOWN 60 Kts at 1000 Ft/Min Descent GNDTRK 65%Nr 65% NR, Flat Pitch (Use MPD) INT-SG 65%Nr 65%NrC 35% TQ 65% NR, Flat Pitch (Use MPD) 65% NR, Pitch @ 17% eng. Tq.  (Use MPD) 35% TQ, 100% NR (Use MPD) PROBES ACC1 ACC2 ACC3 Used as required.  Operator is required to denote location and orientation of accelerometers. ACC4 TAIL 90% NR Flat Pitch, 90% NR (Use MPD) 100%NR Flat Pitch, 100% NR (Use MPD)