Piper Aircraft Corporation Malibu Mirage PA-46-350P, Airplane Maintenance Manual

Page: 588 / 1956

PAGE 10
Feb 28/07
3E20
27-50-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
(10) To install arm assembly: (See Figure 2.)
(a) Install two 82695-97 bushings in hole in tube assembly. Move aft link arms over hole in
tube assembly. Move arm assembly yoke over hole, placing one each NAS1149F0663P
and NAS1149F0632P washers between yoke and aft link arms. Insert AN24-34A bolt
through yoke, arms, and actuator. Secure bolt with NAS1149F0432P washer and
MS21042-4 nut.
(b) Secure the arm assembly to the pushrod assembly.and link “E” with an AN4-13A bolt,
NAS1149F0463P washer, and MS21042-4 nut.
(11) To install the 85097-2 pushrod assembly: (See Figure 2.)
(a) Secure the pushrod assembly to the cam assembly with an AN24-14A bolt, one each
NAS1149F0463P and NAS1149F0432P washers, and a MS21042-4 nut.
(b) Secure the pushrod assembly to the arm assembly and link “E” with an AN4-13A bolt,
NAS1149F0463P washer, and MS21042-4 nut.
(12) To install “E” link: (See Figure 2.)
(a) Position link “E” between support brackets.
(b) Install AN4H30 bolt, one each NAS1149F0463P and NAS1149F0432P washers (under
nut), and AN310-4 nut. Tighten nut finger tight plus one to two castellations. Ensure that
the link is free to pivot, then install MS24665-132 cotter pin. Safety with MS20995C32
wire.
(c) Secure link “E” to the pushrod and the motor-actuator unit with two 82695-96 bushings,
NAS1149F0463P washer (under nut), NAS1149F0432P washer (under bolt head),
AN4-16A bolt, and MS21042-4 nut.
(d) Secure link “E” to connecting arm assembly and pushrod assembly with an AN4-13A bolt,
NAS1149F0463P washer, and MS21042-4 nut.
C. Flap Motor-Actuator (See Figure 2.)
(PIR-85068 AL.)
(1) Removal
(a) Lower flaps to the full down position
WARNING: PULL ELECTRIC FLAP CIRCUIT BREAKER, DISCONNECT BATTERY,
AND CHECK THAT NO EXTERNAL POWER IS CONNECTED TO
AIRPLANE IN ORDER TO ENSURE THAT NO ELECTRICAL POWER IS
BEING APPLIED TO FLAP SYSTEM.
(b) Disconnect flap actuator motor wiring.
(c) Remove the AN4-16A bolt, MS21042-4 nut, NAS1149F0463P washer, NAS1149F0432P
washer, and two 82695-96 bushings connecting left end of actuator left flap drive pushrod
and “E” link.
(d) Remove the AN24-34A bolt, MS21042-4 nut, two 82695-97 bushings, an
NAS1149F0432P washer, two NAS1149F0663P and two NAS1149F0632P washers
securing right pushrod clevis to the tube assembly, the aft link assembly, and the arm
assembly.
(e) Remove motor-actuator and attached tube from aircraft.
(f) Remove the two MS51966-112 set screws from actuator jackscrew coupling.
(g) Unscrew tube from actuator.
NOTE: Motor and actuator remain together as one unit.