EUROCOPTER
FLIGHT MANUAL BO 105 CB-5/CBS-5
7 - 2
MANUFACTURER’S DATA
Rev. 1
and components of both the yaw flight control and comm/nav systems are attached to the
tail boom.
7.2.6 Landing Gear
The landing gear is of the fixed tubular skid-type comprised of two aluminum cross tubes
passing transverse through the fuselage structure and to which aluminum longitudinal skid
tubes are attached.
7.3 COCKPIT ARRANGEMENT (see Fig. 7-2)
7.3.1 Instrument Panel and Console Layout (see Fig. 7-3 thru 7-5)
The cockpit-mounted controls, indicators and annunciators shown in Figs. 7-3 thru 7-5
will be discussed later with their associated systems. Annunciator lights and their fault in-
dications are summarized under lighting equipment. Electrical fuses referred to in this sec-
tion are normally located on a fuse panel discussed later under the electrical system.
7.3.2 Crew Member Seats
Both pilot and copilot seats are adjustable fore-aft and fitted with lap safety belts.
7.4 EMERGENCY EQUIPMENT
7.4.1 Engine Overheat and Fire Detection
Two heat-sensitive detectors are located on each engine. When the ambient temperature
in either engine compartment increases beyond limits, the detector contacts open and, via
a control unit, energize the respective F warning light located on the instrument panel.
Each system is powered from the Main Bus via a fuse.
7.4.2 Portable Fire Extinguisher
A portable fire extinguisher is normally mounted on a quick-release support on the forward
edge of the pilot’s seat. The fire extinguishing agent is released by a hand-operated lever
on top of the extinguisher. Inadvertent discharge is prevented by a safety-pin on the actu-
ating lever. Operating instructions are printed on the extinguisher.
7.4.3 First Aid Kit
A first aid kit is located either in a mount on the cabin floor or in a retaining net secured on
the inside of the cargo compartment RH clamshell door.
EFFECTIVITY For IAC-AR registered helicopters only
7.4.4 Emergency VHF Radio
An emergency VHF radio P/N 105-897936, located in the cockpit beneath the pilot’s col-
lective lever, shall be operated in accordance with its appropriate instructions.
EFFECTIVITY All
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