Eiri KY PIK-20 E - Page 14

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PIK-20

E

Flight

manual

The

canopy

is

hinged

to

the

fuselage

nose

cone

and

can

be

opened

by

pushing

the

both

white

levers

forward

at

both

sides

of

the

frame.

Jettisoning

occurs

by

pushing

the

canopy

levers

forward

and

by

pulling

the

red

knob

right

in

the

instrument

panel

and

lifting

the

canopy.

The

grey

coloured

pedal

adjustment

knob

is

located

in

front

of

the

control

stick

on

the

right,

below

the

instrument

panel.

The

seat

back

ad



justment

knob

is

on

the

left

side

of

the

cockpit.

The

neck

rest

,

if

fitted,

can

be

adjusted

by

lifting

the

support

rod

and

moving

the

neck

rest

to

desired

position.

2.8

Fuel

system

The

29

litres

(7.7

gal

U.S.)

capacity

fuel

tank

is

situated

behind

the

backrest.

1

litre

(0,25

gal

U.S.)

of

unusable

fuel

is

included.

Filling

ope



ning

is

on

the

left

side

of

the

fuselage

between

the

rear

canopy

frame

and

wing.

The

fuel

tank

vent

is

in

the

cap

on

the

left

side

of

the

fusela



ge.

Accumulated

water

and

sediment

can

be

drained

and

checked

by

using

the

sampler

cup

when

draining

the

fuel

tank

daily

prior

to

first

flight.

The

drain

valve

is

situated

on

the

left

side

of

the

fuselage.

The

in



line

fuel

filter

is

situated

after

the

fuel

cock

in

the

baggage

compart



ment.

The

electrical

auxiliary

pump

is

situated

down

in

the

engine

com



partment.

The

engine

has

an

impulse

driven

primary

fuel

pump.

2.9

Electrical

system

PIK-20

E

is

equipped

with

12

V

electrical

system

consisting

of

12

Ah

bat



tery

in

the

engine

compartment

or

below

the

instrument

panel

and

an

alternator.

The

power

is

rectified

and

regularized

with

a

Tympanium-

type

rectifier.

The

engine

has

an

0.4

hp

electrical

starter.

2.10

Water

ballast

system

The

40

litre

nylon

reinforced

plastic

bags

are

filled

through

the

draining

hole

on

the

underside

of

the

fuselage

behind

the

geardoors.

Notel:

1

mis

the

maximum

filling

height

(distance

from

the

funnel

to

the

wing).

Higher

pressure

than

this,

0.1

Bar

(kp/cm

2

),

can

cause

seri

ous

damages

to

the

wing.

No

pressurized

filling

system

is

allowed.

EIRI

KY

Kisällinkatu

8

SF-15170

Lahti

17

page

I

-6

Revision

1.21.8.-79

Revision

4.21.1.-80

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Service Manual49 pages