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
31
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EUROCOPTER
®
; no part of it shall be reproduced or transmitted without the express prior written authorization of
EUROCOPTER
®
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. ©
EUROCOPTER-2008
Additional Avionic equipment that can be added depending on operational needs or
the requirements of the authorities in certain countries if not included in the
standard package
Document
reference
Commercial
reference
Name
kg lb
08-10006-A
08-10006-01-CI
Collins HF9X00 - HF/SSB
15.7 34.6
08-18024-A
08-18024-00-CI
Headset extension cord
0.1 0.2
08-18035-A
08-18035-00-CI
David Clark H10-13H - Headset
103F
1
0.5 1.1
08-18037-A
08-18037-00-CI
ICS installation compatible with Bose Aviation X headset
104F
2
1.0 2.2
08-18043-A
08-18043-00-CI
Bose Aviation X headset
0.5 1.1
08-21008-A
08-21008-00-CI
Thales AHV16 - Radio altimeter
105F
3
5.6 12.3
08-24011-B
08-24011-04-CI
Honeywell KR87 + KI229 - ADF + RMI
6.2 13.7
08-25003-A
08-25003-00-CI
Honeywell KN63 - DME
4.3 9.5
08-70003-A
08-70003-00-CI
Sagem 85T31 - 3-axis autopilot with failure
passivation unit
26.0 57.3
08-83017-A
08-83017-00-CI
VEMD
data download kit
106F
4
-
107F
5
— —
08-91004-A
08-91004-00-CI
Hourmeter
0.1 0.2
The radio/com/nav. equipment weight figures included in this chapter are average values. As the installation of those
equipment may vary from one a/c to an other, the weight of a complete configuration with multiple items may not be the
simple sum of all individual weights.
1
High level / High impedance headset.
2
Includes ICS stereo jacks: in addition to the standard jacks for pilot and copilot and in replacement of the standard
jacks for passengers. Provides electrical supply for the use of Bose X headset without battery pack.
3
May be a mandatory equipment, required by local airworthiness authorities or operational regulations.
4
Delivered in addition to the airborne kit, this kit includes two softwares and a connection wire.
5
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).
