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
16
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
Document
reference
Commercial
reference
Name
kg lb
Avionics
08-22019-A
08-22019-01-CI
Garmin GTX330 - Transponder (mode S)
1
-
2
instead of Garmin GTX327 - Transponder (mode A+C)
0.7
1.5
08-51019-A
08-51019-01-CI
Thales H321EGM - Stand-by gyro-horizon
1
-
3
instead of UI 9560 - Turn and Bank indicator
3.1
6.8
08-18035-A
08-18035-00-CI
David Clark H10-13H – Headset (Qty. 7)
4
3.5 7.7
08-21008-A
08-21008-06-CI
Thales AHV16 - Radio altimeter
1
-
5
-
6
4.6 10.1
08-83017-A
08-83017-00-CI
VEMD
data download kit
7
-
8
— —
1
May be a mandatory equipment, required by local airworthiness authorities or operational regulations.
2
The mode S identification must be communicated by the customer two months at the latest before the delivery.
3
Fitted with independent battery.
4
High level / High impedance headset.
5
The Radio Altimeter includes a 100 ft warning signal. The volume of this signal can be tuned down.
6
Option available for deliveries end 2009.
7
Allows compliance to JAR OPS 3 Amendment 3 requirement, as defined in Appendix 1
to JAR OPS 3.517 (a) and (b)(5)(i). Requires absolute time data, given through a compatible connection with
serviceable GPS equipment (Compliance achieved with the standard aircraft as defined on pages 11 and 12).
8
Delivered in addition to the airborne kit, the kit includes two software and a connection wire.
