Transient Flight Conditions - Kazan Helicopters Mi-17-1V Flight Manual

Ml1-17-1B. Flight manual
220 to 210 km/h at altitudes from 1000 to 2000 m
210 to 195 km/h at altitudes from 2000 to 3000 m.
(b) At the
maximnrn
takeoff weight of 13000 kg:
215 to 205 km/h at altitudes up to 1000 m
205 to 195 km/h at altitudes from 1000 to 2000 m
(3) The recommended horizontal flight speed for traffic circuit flying is 160 km/h.
(4) In turbulent atmosphere (at severe bumping) fly at lAS indicated in para. 4.26.
(5) It is allowed to execute turns banked up to 30° at the normal takeoff
weight and up to 20° at the maximum takeoff weight.
(6) Abstain from prolonged flying at speeds within the range from 20 to
50km/h accompanied by abnormal vibration of the helicopter.
(7) Listed below are the Pilot-Navigator's duties in flight:
(a) Gently hold the flight controls during takeoff and landing.
(b) Refine the calculated data.
(c) Monitor the flight and navigation instruments.
(d) Carry on visual orientation, execute navigation calculations rapidly
and correctly.
(e) Retune the radio navigation equipment to work the problems of
reaching a selected area, approach and aiming at the landing point.
(f) Periodically, every 10 to 15 min in flight, check the fuel consumption
and the fuel reserve. The check over, set the fuel flow-meter selec-
tor switch to FLOW (PACX).
(g) Always know the flight duration up to the moment of landing.
(h) Be capable to restore orientation in flight.
(i) Follow the Captain's instructions.
(8) Listed below are the Flight Flight Engineer's duties during takeoff, flight
and landing:
(a) Monitor the power plant instruments.
(b) Check the correct distribution of load between the generators and
adjust it, if necessary.
(c) Monitor the operation of the hydraulic system.
(d) Turn on the compartments heating or ventilation systems by the
Captain's order. With the KO-50 combustion heater on, the storage
batteries heating should be turned off.
(e) Upon the Captain's permission periodically enter the cargo com-
partment to check the fuel, oil and hydraulic systems for freedom
from leaks, and the cargo for reliable tie-down.
(f) Immediately report to the Captain on all malfunctions detected.
(g) If possible icing is anticipated in flight or severe snowfall occurs, pe-
riodically inspect the condition of the engines air intakes looking
through the inspection window made in the power plant access door
and immediately report to the Captain about appearance of indica-
tions of icing.
4.7. Transient flight conditions
(1) To proceed from vertical climb to hovering upon attainment of a selected
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