Eiri KY PIK-20 E - Page 20

PIK-20 E Flight manual
A
4.1.3 In full view of the pilot
Pre-flight check
Loading and ballast .................................................checked
Barograph (if installed) ............................................ on
Parachute ................................................................ secured
Seat and rudder pedals ..........................................adjusted
Safety bareness ...................................................... fastened
Canopy ....................................................................locked
Main switch .............................................................. on
Engine and engine gauges . ...................................... tested and checked
Flight instruments ....................................................checked
Flaps ......................................................................... set
Trim ......................................................................... set
Airbrakes ..................................................................closed and locked
Controls ....................................................................free
Choke ........................................................................ off
Fuel cock ............................... (in tow: off) .............. on
Electrical fuel pump ............. (in tow: off) .............. on
Tow rope (in tow) .................................................... coupled
Before landing
Engine ...................................................................... retracted
Water ballast ............................................................drained
Landing gear ............................................................ down
Flaps ..........................................................................12°. . .16° down
Trim ..........................................................................set for landing
4.1.4 Other placards
Adjacent to tow coupling ............
Above the main wheel ................
Adjacent to static pressure entry
on fuselage skin ...........................
Adjacent to oxygen control valve
(if installed) .................................
On fuselage nose (inside) ............
RATED LOAD 6000 N (1320 lbs)
2.5 bar (35 psi)
STATIC PRESSURE KEEP CLEAR
DURATION TABLE
BALLAST
EIRI KY
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Kisällinkatu 8
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