ARROW 11
INSTJUMENT PANEL
The instrument panel is designed to be functional and professional, accommodating
complete instruments and avionics equipment for VFR and IFR flights. A wide range of
optional instruments and avionics pennits an equipment selection uniquely suited to individual
needs.
Flight instruments are grouped in a standard "T" directly in front of the pilot. Radio
navigational indicators are to the ri
g
ht of the flight instruments and are located to correspond to
the respective radio control heads. Fuel gauges are located to the right of the pilot controL wheel
and engine instruments are located to the left of the control wheel
.
The tachometer and
manifold pressure instruments are located to the left of the power guadrant and are positioned
respective of the throttle and propeller controls.
The circuit breakers are protected by a cover door.
The climatic controls, when the air conditioning system is installed, are located in the right
instrument panel above
.
the circuit breakers.
"
PITOT-STATIC SYSTEM
The system supplies both pitot a;d static pressure for the airsp
_
eed indicator, altimeter and
vertical sp�ec;t UJdicator (when installed).
Pitot
·
and static p;essure are picked up by the pitot head on the bottom of the left wing.
An optional heated pitot head, which alleviates problems with icing or heavy rain, is available.
The switch for pitot heat is located on the lower left instrument panel.
To prevent bugs and water from entering the pitot and static pressure holes, a cover should
be placed over the pitot head. A partially
-
or completely blocked
·
pitot head
will
give erratic or
zero readings on
·
the instruments.
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·
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AIRPLANE AND SYSTEMS
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