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LANCE II SERVICE MANUAL

3. Should the travel not be correct, the travel may be set by rotating the bellcrank

stops in or out. Stops

are located in the

wing attached to

the rib that is adjacent

to the aileron

bellcrank.

Repeat

this procedure

for the

other aileron.

e. Check

the bellcrank

stops

to assure

that the

bellcrank

contact is

made

simultaneously,

but

still have cushion

before contacting

the

control wheel

stops. Maintain

.030

to .040

clearance

between sprocket

and adjustable

stop bolts

on the

tee bar.

f. Check

to insure

that the left

aileron up and

the right

aileron down

stops are contacted

simultaneously

and

vice versa. Adjust

stops

as required.

Check

control

operation

for

binding

chafing,

and

bolts

and

turnbuckles

for

safety.

h. Install

access

plates

and panels.

i. Should

an out-of-trim

condition

persist

despite all the

rigging corrections

that

can be

made,

there is

a possibility

that the trailing

edge of

the aileron has

been used

to move the

aircraft

forward.

This

can result

in a slight

bulging

of the aileron

contour

at the

trailing edge

which will cause

an out-of-rig condition that

is very difficult to correct.

5-12. STABILATOR CONTROLS.

5-13.

REMOVAL

OF STABILATOR

CONTROL

CABLES.

(Refer

to Figure

5-5.)

a. To remove

either

the forward

or aft stabilator

cables,

first remove

the access panel

the aft section of the fuselage.

Disconnect

the desired control

cable

at the turnbuckle

(16)

in the aft section

of the

fuselage.

c. Either

forward

stabilator cable

(2 or 3)

may be removed

by the

following procedure:

1. Remove

the floor

tunnel cover

in the aft

area of the

cabin by removing

the

trim

plate,

the carpet

over

the tunnel

and the

cover attachment

screws.

2. Remove

the cable

guard plate

( I I) from

the underside

of the

pulley cluster

(19) in

the

aft area of the

tunnel opening

by removing the

guard attachment

screws.

Revised:

10/3/80

1G3

SURFACE

CONTROLS

Manufacturer	Piper Aircraft
Max Takeoff Weight	3, 600 lb (1, 633 kg)
Crew	1
Horsepower	300 hp
Seats	6
Length	27 ft 7 in (8.41 m)
Capacity	5 passengers

Piper Lance II User Manual

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Piper Lance II Specifications

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