DESCENT AND LOW LEVEL CRUISE
Maximum rate (Vmo) descent. If the test
pilot is satisfied that the entire aircraft is
maximum rate descent check as follows:
accordance with figure 3.
(b) POWER levers - IDLE.
(c) PROP levers - Set 1700 RPM.
(d) Gear - UP.
(e) Flaps - UP.
Airspeed - In accordance with figure
oscillation or vibration is encountered.
*(g) Flight controls - Check for any
vibration, or malfunction.
*(h) Windows and doors - Check for
wind noise indicating air leaks.
Aircraft - Level off at 10,000 feet.
Elevator trim - Nose down trim stops will
be set as follows:
(a) POWER levers - Set maximum
continuous power. Do not exceed
N1 or TGT limits.