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
4
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-2009
2- General
Characteristics
Layout
Passenger-transport
z
1 pilot + 6 passengers in standard version
1
z
1 pilot + 7 passengers in "medium density" version
Casualty-evacuation
z
1 pilot + 1 or 2 stretcher pa 2 medical attendants
z
2 1 stretcher p 2 medical attendants
Cargo carrying
z
1 pilot + 3.7 m³
(130.7 ft³) load in cabin
Equipment
Complete 7 seats in trims + carpets included in standard
Ready to operate radio package included in standard :
z
2
VHF
z
2 VOR / LOC / GLIDE
z
1
GPS
z
1
ELT
z
1 XPD mode A + C
z
1 ICS capable of 8 outlets
z
1
ADI
z
1
HSI
Weights
Note : Empty weight accuracy : within
±
2 %
kg lb
Empty weight, baseline aircraft
2
1,378
3
3,038
Useful load
4
1,049
2,313
Maximum all-up weight
2,427 5,351
Maximum cargo-swing load
1,160 2,557
Maximum all-up weight in external load configuration
2,800 6,172
1
If required by the local airworthiness authorities, the capacity can be limited to 1 pilot + 5 passengers.
2
Baseline aircraft empty weight includes oil and unusable fuel. Ballast plates can be added at the rear of the
FENESTRON
, their mass is 12.8 kg (28.2 lb) maximum. The baseline helicopter is delivered as standard with
4.8 kg (10.6 lb) ballast weight that is not included in the basic empty weight.
3
Empty weight according to baseline aircraft definition, as defined in pages 11 and 12, including the avionics suite.
4
The useful load does not include the ballast plates. Depending on the configuration, the ballast’s weight will be
deducted from the useful load.
