HP d212 Manuel d'utilisateur Page 162

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FMS-D212-725-1
Page 5-8
• 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:
A
Unapproved Date: 07.06.01
Table 5-2 – Sample Loading Problem (Metric Units)
Helicopter serial numbers 35049 and subsequent
Weight
(Kg)
CG
(MM)
Moment
(Kg-
MM/100)
Basic
Operating
Weight
Licensed Empty Weight 2614.8 3690.4 96485.7
+ Oil 11.1 4298.3 477.1
+ Pilot* 77.1 1194.0 920.6
Payload
+ Passengers (5 man seat)* 385.6 2972.0 11460.0
+ Passengers (4 man seat)* 308.4 2210.0 6815.6
+ Cargo Compartment* 81.6 6629.4 5409.6
Basic Operating Weight + Payload 3478.6 3495.0 121578.6
Takeoff
Conditions
Basic Operating Weight + Payload 3478.6 3495.0 121578.6
+ Takeoff Fuel (820.7 liters Jet A)* 674.3 3876.0 26135.9
Takeoff Weight, CG and Moment 4152.9 3556.9 147714.5
Most Critical
FWD CG
Conditions
Basic Operating Weight + Payload 3478.6 3495.0 121578.6
+ Critical Fuel (274.8 liters Jet A)* 242.1 3233.0 7827.1
Critical Weight, CG and Moment 3720.7 3478.0 129405.7
Landing
Conditions
Basic Operating Weight + Payload 3478.6 3495.0 121578.6
+ Landing Fuel (227.1 liters Jet A)* 185.1 3299.5 6107.3
Landing Weight, CG and Moment 3663.7 3485.2 127685.9
(* Information obtained from loading charts)
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