CAPRONI VIZZOLA
C 22 J
4-6
4.3.3.
Interior Inspection
1.
Parachute .............................................. As required
2.
Pilot’s seat
...................................................... Adjust
3.
Pedals ............................................................. Adjust
4.
Safety Harness........Condition and security of the locking device
5.
Headphone and microphone ......................Connect
6.
Oxygen hose .......................... Connect (if required)
7.
Parking Brake ...................................................... Set
8.
Flight Controls ................................................... Free
9.
Pitot Heat ........................................................... OFF
10.
DME ................................................................... OFF
11.
Altitude Alerter .................................................. OFF
12.
Radio 1 & 2 ......................................................... OFF
13.
VOR 1 & 2 ........................................................... OFF
14.
Transponder ....................................................... OFF
15.
ADF ..................................................................... OFF
16.
Turn and Slip ...................................................... OFF
17.
Attitude Indicator .............................................. OFF
18.
Lights (Landing, Nav, Anticol, internal) .............. OFF
19.
Airbrakes ..................................................... CLOSED
20.
Hot Air control ............................................ CLOSED
21.
Defogger ..................................................... CLOSED
22.
Throttle Friction ............................................. Adjust
23.
Throttle ............................................................. IDLE
24.
Emergency Throttle ........... Fully counter-clockwise
CAUTION
If the throttle is not in the idle position, after the startup the engine will immediately at
RPMs higher than idle. This could damage the engine
25.
External power .............. Connected (not simulated)
NOTE
In order to preserve the life of the battery, the engine startup is only to be done by aircraft
battery when an external power source 28 VDC/20A is not available.
26.
BATT switch ......................................................... ON
Warning Panel Lights
27.
GEN lights (amber) ..........................................
“ON”
28.
OIL lights .........................................................
“ON”
29.
LOW PRES light ...............................................
“ON”
30.
PUMP lights .....................................................
“ON”
31.
Lights
-
FIRE
-
HIGH PRESS
-
And engine instrument filamentsPRESS to TEST
Engine Control Panel
32.
Fuel Shut-Off flights .....................................
“SHUT”
