HP d212 Manual do Utilizador descarregar pdf (Página 158)

FMS-D212-725-1

Page 5-4

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:

Unapproved Date: 07.06.01

5.4 Doors Open or Removed

Opening or removing doors results in CG changes. Door configuration shall

be symmetrical for both sides of fuselage. Door weights and moments table

(Table 5-3) lists weight and moment adjustments which should be made in

determining GW and CG when doors are opened or removed.

5.5 Cockpit and Cabin Loading

A minimum crew weight of 170 pounds (77.1 kilograms) in cockpit is

required. Except for two aft passenger seats, crew and passengers may be

loaded in any sequence without exceeding GW CG limits approved for flight.

Note

Outboard facing seats should not be occupied

unless at least four passengers are seated in

forward and/or aft facing seats.

5.5.1 Cabin Deck Loading

Cabin deck cargo loading limit is 100 pounds per square foot (0.048

kilograms per square centimeter).

WARNING

HELICOPTER CG SHALL BE COMPUTED FOR ALL

CARGO/BAGGAGE CONFIGURATIONS BEFORE

FLIGHT. REFER TO TABLE 5-2 FOR PERSONNEL

WEIGHTS AND MOMENTS IN ENGLISH AND METRIC

UNITS.

1 2 ... 153 154 155 156 157 158 159 160 161 162 163 ... 176 177

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