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 08.100.01 E
9
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
3-
AS350 B3
ECUREUIL
- Baseline Aircraft Definition
The helicopter in the definition, presented hereafter, meets the certification standards for day and night VFR operations, set by the following
airworthiness authorities : EASA, FAA, TC. This list is not restrictive and the status of approval by other airworthiness authorities must be
checked. Additional equipment item may be required by the relevant operational regulation (most of them are available in catalogue).
GENERAL
The
AS350 B3
®
is certified with a pilot being on the right side
The standard aircraft is delivered with right side controls and
fixed parts of the removable dual controls (the removable parts
of removable dual controls are optional)
Fuselage comprising the cabin and 3 luggage holds, with floor
tie-down nets and access doors
Tail boom with stabilizer, anti-torque rotor and fin with tail skid
High Skid landing gear with long footsteps (on right side and on
left side), capable of taking handling wheels
Lifting points
Mooring
fixtures
Structural reinforcements for wire strike protection system
External paint : fuselage according to standard paint schemes.
Unless modified by optional item, the main rotor head cover
and the skid landing gear are painted in grey.
Internal paint : grey (prevailing colour)
Interior signs and markings : available in either French or
English
CABIN
Cabin floor in light-alloy sheet-metal
with tie-down rings
2
pilot and copilot high-back energy-absorbing seats,
adjustable in reach, removable, complete with cushions, safety
belts and shoulder harnesses
2 two-place rear bench-seats, foldable separately, complete
with cushions, safety belts and shoulder harnesses
2 pilot and copilot jettisonable doors each fitted with a sliding
window and with improved side-visibility window
z
1 RH large front door
z
1 LH front door
Rear right door-extension for passengers and cargo
1 rear left sliding door
Locks on every access to cabin and luggage compartments
Lock on fuel cap
2 tinted upper panes
1 ceiling housing the ventilation ducts and controls (ventilation
controls, rotor brake and fuel cut-off)
Cabin
heating
Demisting system for front windscreens
Ram air ventilation duct
Fixed parts for pilot and copilot windshield wipers
1 pilot map case
1
fire-extinguisher
Flight
Manual
Interior harmony according to definition in force
INSTRUMENTS
Instruments units : available in either metric or English units
1 airspeed indicator
1
altimeter
1 vertical speed indicator
1 rotor tachometer indicator
1
clock
1 warning panel
1 magnetic compass
1 heated pitot head
1 external side slip indicator
1 control box for light and electrical generation
2 cockpit breaker panels
1 I.C.S. connection to audio warning issued from
VEMD
®
1 LCD Dual screen Vehicle and Engine Multifunction Display
(
VEMD
®
) providing the following information:
z
First limitation indicator (FLI)
torquemeter
exhaust gas temperature (T4)
gas generator tachometer (Ng, delta Ng)
z
Engine oil temperature/pressure
z
Fuel quantity and fuel flow and estimated remaining time to
fly
z
Ammeter and voltmeter
z
Outside Air Temperature (OAT)
z
Enhanced usage monitoring functions
IGE/OGE performance calculations
engine cycles counting
engine power check
overlimits
display
z
VEMD
®
and peripheral maintenance information
z
Data downloading capability (software and connection wire
as option)
