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.
130 B4 09.101.01 E
33
This document is the property of
EUROCOPTER
©
; no part of it shall be reproduced or transmitted without the express prior written authorization
ο
f
EUROCOPTER
©
and its contents shall not be disclosed
. ©
EUROCOPTER-2009
HOVER CEILING O.G.E.
at maximum TOP
0
5000
10000
15000
20000
0
1000
2000
3000
4000
5000
6000
7000
-40
-30
-20
-10
0
10
20
30
40
50
OAT (°C)
Zp (m)
(ft)
IS
A
IS
A
+
2
0
IS
A
+
3
5
150
0
1600
1700
1800
1900
2000
2100
2200
2300
2400
2427
2500
2600
2700
280
0
Note : ISO weight curves from 2,427 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.