Stall Warning; Pitot-Static System; Cockpit - Cub Crafters CC11-100 Pilot Operating Handbook

CUB CRAFTERS SECTION 7
CC11-100 AIRCRAFT AND SYSTEMS

7.5.12 STALL WARNING

The stall warning system is activated by a vane located
on the leading edge of the left wing. As the aircraft
approaches the stall, a horn will sound. The system is
calibrated so that the horn will come on at least 6 mph or
5 knots above the stall speed.

7.5.13 PITOT-STATIC SYSTEM

The pitot system senses dynamic pressure through a
tube that is aligned with the flow of air and is located in
the leading edge of the jury strut on the left wing.
The static pressure source for each instrument is vented
to the inside of the cabin. Because of this, the indications
for airspeed, altitude, and rate of climb will be affected by
opening the windows, door, or cabin air vents.
7.6

COCKPIT

Entry to the cockpit is through a door and window
arrangement on the right side of the aircraft. The window
is latched to the door using rotating tangs that engage
slots in the door. The door is opened using a rotating
handle. The window must be raised until it engages the
latch on the wing. Close the door by rotating the door
handle and pulling it closed. Release the handle once the
door is fully closed, allowing the latching pins to engage
in the fuselage. Release the window latch on the wing
and lower the window closed. Engage the tangs in the
door.
A window on the left-hand side of the fuselage operates
in a similar manner to that on the right.
Some aircraft are equipped with removable windows.
Consult the Aircraft Maintenance Manual for instructions
on removable and installation.
SC10000AFM
Issued: 08/01/06 REPORT
Date of Revision: 11/23/18 Page Number: 7-11