R E F E R E N C E
DESCENT AND LOW LEVEL CRUISE (CONT)
(d) Gear - UP.
(e) Flaps - UP.
(f) Airspeed - In accordance with
f i g u r e 3 .
Immediately reduce airspeed if any flutter, oscilla-
tion or vibration is encountered
*(g) Plight controls - Check for any
indication of flutter, oscillation,
vibration, or malfunction.
Windows and doors - Check for
wind noise indicating air leaks.
(i) Aircraft - Level off at 10,000 feet.
*2. Elevator trim - Nose down trim stops
will be set as follows:
(a) POWER levers - Set maximum
continuous power. Do not exceed
N1, or ITT limits.
(b) PROP levers - Set 2000 RPM.
(c) Airspeed - 250 KIAS. Verify
that excess nose down trim is at
least 0.9, but does not exceed 1.4
trim wheel indicator units.
Perform the following checks prior to the final descent for