LANCE
II SERVICE
MANUAL
SECTION IV
STRUCTURE
4-1. DESCRIPTION. This section explains the removal and installation procedures for the
structural surfaces of
the airplane. For the removal, installation
and rigging and adjustment
procedures of the controlling components of the various structural surfaces, refer to Section
V.
NOTE
When torquing structural assemblies, standard torque values
are to be used as found in Table II-II of this manual or FAA
Advisory Circular 43.13-1A, unless otherwise stated in this
section.
4-2.
REMOVAL
AND
REPLACEMENT.
4-3. REMOVAL AND REPLACEMENT
OF WING
ASSEMBLY.
NOTE
The major subassemblies
of the wing may
be removed
individually or the wing may be removed as a unit. To
remove
a wing, a fuselage
supporting cradle is required.
4-4. REMOVAL AND REPLACEMENT OF WING TIP.
a. The
wing tip is removed using
the following steps.
1. Remove the screws from around the wing tip.
2. Pull the tip away from the wing assembly far enough to gain access for removal
of electrical connections
for strobe and position
lights.
3. Remove the tip from the wing.
b. Replacement of wing tip is reverse of removal instructions.
Issued:
1/3/78
STRUCTURE
1D23
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