Technical Data
The data set forth in this document are general in nature and for information purposes only.
For performance data and operating limitations,reference must be made to the approved flight manual and all appropriate documents.
350 B3 08.101.01 E
41
This document is the property of
EUROCOPTER
®
; no part of it shall be reproduced or transmitted without the express prior written authorization of
EUROCOPTER
®
and its contents shall not be disclosed
. ©
EUROCOPTER-2008
TAKE-OFF WEIGHT IN HOVER O.G.E.
at maximum TOP
0
1000
2000
3000
4000
5000
6000
0
5000
10000
15000
20000
-40
-30
-20
-10
0
10
20
30
40
50
OAT (°C)
PA (ft)
(m)
ISO-Weight
IS
A
IS
A
+
2
0
IS
A
+
3
5
1600
1700
1800
1900
2000
2100
2200
2250
2300
2370
2400
2500
2600
2700
2800
Zsig
ma m
ax
Note : ISO weight curves from 2,300 to 2,800 kg are curves with external load.
Note : Approved performance, as long as the engine meets the power check criteria, as defined in the Flight Manual.
Note : The Zd curve corresponds to the maximum demonstrated envelope.
Note : The ISO curves 2,300 and 2,370 are curves for the helicopter fitted with the "Kit to increase Internal Gross Weight
to 2,370 kg (5,225 lb)". This kit can only be installed on a helicopter with a High skid landing gear. For the effect of
a High skid landing gear on the performance, please refer to page
47H
38 of this Technical Data.
