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(23) Install four (4) Hi-Lok bolts thru each intercostal, frame, angle and two (2) thru frame and wing
spar, just under intercostal. All four locations are left, right, fwd and aft of top wing spar. See
Figures 5 and 8.
(24) Install four (4) angles that form two (2) tee's in bottom of fuselage. Tap with a plastic mallet thru
aft channels in the frame under wing spar until they clear the fwd frame under spar. Then using
small vise grips attach to angles and tap thru fwd frame channels an equal amount.
(25) Inside fuselage align angles evenly with Kleco fasteners to existing holes one on each side of
stringer.
(26) Below fuselage place short tee angles between floor angles and rivet together with four (4)
rivets on top. Then go inside and rivet both ends to bottom stringer.
(27) Ensure there are no metal splinters on chips between skins prior to installing close outs.
(28) Apply sealant to all skins and close out skins on bottom of aircraft. See Figure 7. Apply sealant
1/4" each side of rivets.
(29) Install close outs in place with Kleco fasteners and insert rivets from bottom.
(30) Inspect rivets.
(31) Install fwd pilot's seat belt brackets with bolts.
(32) Install cat grommets on all passage holes in bottom spar.
NAS6607-9, BOLT
NAS1149F0763P, WASHERS
(FIVE REQ., ONE UNDER HEAD,
ONE TO THREE BETWEEN FITTINGS,
REMAINING UNDER NUT.
TWO NAS1149F0732P WASHERS,
ONE BETWEEN FITTINGS,
ONE UNDER NUT,
MAY BE SUBSTITUTED FOR
ONE NAS1149F0763P WASHER.)
MS21044-N7, NUT
(TORQUE TO 550 IN.-LBS.)
57-40-00
PAGE 14
Apr 15/07
PIPER AIRCRAFT, INC.
PA-46-500TP, MALIBU MERIDIAN
MAINTENANCE MANUAL
LOOKING AFT AT FWD SPAR
(TYPICAL, LEFT AND RIGHT)
Installation of Inboard Wing
Figure 6
89635 V
6K14
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