Cessna 150M - Wing Strut

/
1. Mooring Ring
2.
Upper Fairing
3. Screw
4. Washer
5. Nut
6.
Bolt
7. Wing Attachment
Fitting
8. Spacer
9. Fuselage Attachment
Fitting
10. Lower Fairing
* NOTE
Lubricate bolt and
hole per Section 2.
B
4
Detail A
9
Detail B
IWARNING'
On 15074635 thru 15074799 and
A1500415 thru A1500427 Cessna
Single-engine Service Letter
SE73 -20 should be complied with.
Figure 4 -2. Wing Strut
lare ABS. A formed metal leading edge is
riveted to the assembly to complete the structure.
The elevator trim tab actuator is contained within
the horizontal stabilizer. The underside of the stab-
ilizer contains a covered opening which provides ac-
cess to the actuator. Hinges are located on the rear
spar assembly to support the elevators.
4-18. REMOVAL AND INSTALLATION.
a. Remove elevators and rudder in accordance
with procedures outlined in Sections 8 and 10.
b. Remove vertical fin in accordance with pro-
cedures outlined in paragraph 4-14.
c. Disconnect elevator trim control cables at
4-4 Change 3
clevis and turnbuckle inside tailcone, remove pulleys
which route the aft cables into horizontal stabilizer,
and pull cables out of tailcone.
d. Remove bolts securing horizontal stabilizer to
fuselage.
e. Remove horizontal stabilizer.
f. Install horizontal stabilizer by reversing pre-
ceding steps. Rig control systems as necessary.
Check operation of tail navigation light and flashing
beacon.
4-19. REPAIR. Horizontal stabilizer repair should
be accomplished in accordance with applicable in-
structions outlined in Section 18.