
FMS-D212-725-1
Page 5-7
• 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 5-1 – Sample Loading Problem (English Units)
Helicopter serial numbers 35049 and subsequent
Weight
(Lbs)
CG
(Inch)
Moment
(In-Lbs)
Basic
Operating
Wei
ht
Licensed Empty Weight 5764.5 145.3 837508
+ Oil 24.0 175.2 4146
+ Pilot* 170.0 47.0 7990
Payload
+ Passengers (5 man seat)* 850.0 117.0 99450
+ Passengers (4 man seat)* 680.0 87.0 59160
+ Cargo Compartment* 180.0 261.0 46980
Basic Operating Weight + Payload 7668.5 137.6 1055234
Takeoff
Conditions
Basic Operating Weight + Payload 7668.5 137.6 1055234
+ Takeoff Fuel (216.8 gallons Jet A)* 1486.0 152.7 226837
Takeoff Weight, CG and Moment 9154.5 140.0 1282071
Most Critical
FWD CG
Conditions
Basic Operating Weight + Payload 7668.5 137.6 1055234
+ Critical Fuel (72.6 gallons Jet A)* 534.0 127.3 67953
Critical Weight, CG and Moment 8202.5 136.9 1123187
Landing
Conditions
Basic Operating Weight + Payload 7668.5 137.6 1055234
+ Landing Fuel (60 gallons Jet A)* 408.0 129.9 52999
Landing Weight, CG and Moment 8076.5 137.2 1108233
(* Information obtained from loading charts)
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