Mooney M20V - Page 232

MOONEY INTERNATIONAL CORPORATION
M20V SERVICE AND MAINTENANCE MANUAL
Page
Date
7
MAR 2017
Rev Date
FWD INBD
7
6
F
8
9
J
REACH 7
THRU HERE
RIG
PIN HOLE
VIEW AT
L/H WING
LOOKING UP
3/16” RIG PIN
HOLE
AILERON STOP ADJUSTMENTS
FIGURE 27−2
STA. 25.50
TRAVEL BOARD
LOCATION 1/2”
ABOVE C/L OF
RIVET ROW
LEVELING
SCREWS
SKIN
LAP
STA. 16.00
TRAVEL BOARD
LOCATION 1/4”
OB C/L OF
RIVET ROW
SKIN
LAP
STA. 147.75
TRAVEL BOARD
LOCATION BETWEEN
FLAP & AILERON
TRAVEL BOARD LOCATIONS
FIGURE 27−3
A
B
RUDDER PEDAL ADJUSTMENT
FIGURE 27−4
2. Rudder Rigging and Adjustment.
A. Raise aircraft nose wheel off ground. See Sec-
tion 7−10−00.
B. Set stabilizer trim control in neutral position (sta-
bilizer parallel with aircraft center line).
C. Clamp pilot’s rudder pedals (A), (Fig. 27−4), in
neutral position.
D. Adjust AFT rod end bearing indicated at position
“B” Figure 27−4, approx. 11 turns out to start.
AFT
L
1
C
RUDDER & ELEVATOR TRAVEL ADJUSTMENT
FIGURE 27−5
E. Adjust control tube (C) at rear tailcone bulkhead
bellcrank (Fig.27−5) approx. 12 turns out as to start.
F. Adjust control tube (D) (Fig. 27−6), rod end bear-
ing (2), 11 turns out to start.
G. Adjust rod end bearing (B) (Fig. 27−4) to posi-
tion rudder setting 1
o
to the right.
27-20-00