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FMS-D212-725-1
Page 1-17
• COPYRIGHT © 2007 BY DART AEROSPACE LTD •
This document is private and confidential and is supplied on the express condition that it is not to be used for any
purpose or copied or communicated to any other person without written permission from Dart Aerospace Ltd.
Revision:
G
TC Approved Date: 13.08.09
1.11 Ambient Temperature
Maximum sea level ambient air temperature for operation is +49°C (+120°F)
decreases with altitude at standard lapse rate (2°C per 1000 feet H
P
). For
S/N 30687, 30576, 30817 and 30599 (G1), minimum ambient air temperature
at all altitudes is -54°C (-65°F). For all other S/N (G2) minimum ambient air
temperature at all altitudes is -30°C (-26°F). Refer to Weight-altitude-
temperature limitations for takeoff, landing and in ground effect maneuvers
chart (Figure 1-4). G1 is generation 1 aircraft with AC instruments. G2 is
generation 2 aircraft with DC instruments.
Engine de-icing shall be turned ON for flight in visible moisture at
temperatures below +4.4°C (+40°F).
The maximum ambient temperature for use of engine de-icing is +4.4°C
(+40°F).
Figure 1-9a – Pressure Altitude vs Ambient Air Temperature Chart
(For S/N 30687, 30576, 30817, 30599)
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