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
14
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
Document
reference
Commercial
reference
Name
kg lb
Avionics
06-67031-A
06-67031-00-CI
Kannad 406AF-H - Emergency Locator Transmitter
11F
1
-
12F
2
instead of Kannad 121AF-H - Emergency Locator
Transmitter
0.1 0.2
08-22019-A
08-22019-00-CI
Garmin GTX330 - Transponder (mode S)
10H
2
-
13F
3
instead of Garmin GTX327 - Transponder (mode A+C)
0.6 1.3
08-51019-A
08-51019-00-CI
Thales H321EHM - Stand-by gyro-horizon
11H
2
instead of UI 9560 - Turn and Bank indicator
3.0 6.6
08-52012-A
08-52012-00-CI
Honeywell KCS55A - Gyro Compass
14F
4
with Honeywell KI525A - Horizontal Situation Indicator
instead of AIM 205-1BL - Gyro-directional
and Garmin GI106A - Course Deviation Indicator
3.8 8.4
08-18035-A
08-18035-00-CI
David Clark H10-13H - Headset (Qty 6)
15F
5
3.0 6.6
08-21008-A
08-21008-00-CI
Thales AHV16 - Radio altimeter
12H
2
5.6 12.3
08-83017-A
08-83017-00-CI
VEMD
data download kit
16F
6
-
17F
7
— —
08-91004-A
08-91004-00-CI
Hourmeter
0.1 0.2
1
3 frequencies: 121.5 MHz, 243 MHz, 406 MHz. Compliant with ED 62 and TSO C91A.
The Programming Data Sheet must be filled and communicated by the customer two months at the latest before
the helicopter's delivery.
2
May be a mandatory equipment, required by local airworthiness authorities or operational regulations.
3
The mode S identification must be communicated by the customer two months at the latest before the delivery.
4
With a selector switch for NAV1/NAV2 selection.
5
High level / High impedance headset.
6
Delivered in addition to the airborne kit, this kit includes two softwares and a connection wire.
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 a
serviceable GPS equipment (Compliance achieved with the baseline aircraft as defined on pages 9 and 10.
