Piper Lance II User Manual

Stabilator
A - STABILATOR TRAILING EDGE UP TRAVEL
FROM NEUTRAL
14.5° .5
B STABILATOR TRAILING EDGE DOWN
TRAVEL FROM NEUTRAL
10
°
1
°
Stabilator Trim Tab
A. STABILATOR TAB TRAILING EDGE
UP TRAVEL
FROM NEUTRAL
*2.5+ 1
or *14
+± 1
°
B. STABILATOR TAB TRAILING EDGE
DOWN TRAVEL FROM NEUTRAL
*10 +±.5
°
or *11.5+.5
°
* FOR PA-32RT-300
* FOR
PA-32RT-300T
STABILATOR CHORD UNE
(NEUTRAL POSITION)
(SEE
NOTE
2)
1. Maximum
free play for
control
surface tab
Is
0.06 of an
inch measured at
tab trailing edge.
Refer to Section IV. Paragraph 4-28.
2. Neutral
position
of
stabilator
is with
the
stabilator
chord line parallel
with the top
of
the front
seat tracks.
LANCE II SERVICE MANUAL
TABLE
V-I CONTROL
SURFACE
TRAVEL
AND CABLE
TENSION
857
STABILATOR
CHORD
LINE
(NEUTRAL
POSITION)
(SEE
NOTE)
B
Neutral position of stabilator Is with the stabilator
chord line parallel with the top of the front seat
tracks.
A
B
Rudder Pedal
Neutral
Angle
AFT VERTICAL
TO
SEAT RAILS.
16
°
+ 1
°
Cable Tensions
AILERON
FLAP
STABI LATOR
STABILATOR TRIM TAB
RUDDER
40 lbs. ± 5 lbs
10 bs. 1 lb.
40 lbs. - 5 Ibs.
14 lbs. lb.
65 lbs.
- 5
lbs.
I
NOTE
CABLE TENSIONS GIVEN APPLY ONLY TO AIRPLANES WITHOUT
AUTOPILOT
BRIDLE CABLES ATTACHED.
REFER TO APPROPRIATE
AUTOPILOT
SERVICE MANUAL
FOR PROPER CABLE TENSIONS
WHEN
ATTACHING BRIDLE CABLES.
CABLE RIGGING
TENSIONS SPECIFIED
MUST BE CORRECTED
TO
AMBIENT
TEMPERATURE IN THE AREA
WHERE THE TENSION IS BEING
CHECKED USING TABLE V-Il.
Revised:
11/1/83
1F13
SURFACE CONTROLS

Piper Lance II Specifications

General

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