Wing Installation Diagram - Piper PA-44-180 SEMINOLE Maintenance Manual

A354
BOLT NAS464-P5LA15
NUT MS21042-5
WASHER AN960-516L (UNDER HEAD)
WASHER AN960-516 (SEE NOTE)
MAX. TORQUE 130 - 150 IN. - LBS.
SECTION A - A
A355
OF THE THREE REQUIRED WASHERS FOR THIS INSTALLATION, ONLY
THE AN960-616L AND ONE AN960-616 ARE ALLOWED BETWEEN THE
WING AND FUSELAGE FITTINGS. ALSO, IF NECESSARY, ONLY THE
SINGLE AN960-616L WASHER IS ALLOWED UNDER THE BOLT HEAD,
OTHERWISE THE WASHERS CAN BE PLACED AS DESIRED.
BOLT NAS464-P6LA6
WING FITTING
NUT MS21045-6
WASHER AN960-616 (2) (SEE NOTE)
FUSELAGE FITTING
WASHER AN960-616L (SEE NOTE)
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
NOTE
SEE NOTE
Figure 57-1. Wing Installation
3C14
0.35 MAX.
0.12 MIN.
NOTE
A MINIMUM OF ONE, THEN, REQUIRED TO
LEAVE A MAXIMUM OF 1.50 VISIBLE THREADS
OR MINIMUM OF BOLT CHAMFER EXPOSED.
B
B
Revised: May 15, 1989
SKETCH A
SKETCH B
5 7 - 4 1 - 0 1
Page 57-03