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

Page: 581 / 1956

PAGE 3
Feb 28/07 3E13
27-50-00
PIPER AIRCRAFT, INC.
PA-46-350P, MALIBU MIRAGE
MAINTENANCE MANUAL
3. Flap Controls
A. Removal
(PIR-85068 AL.)
(1) To remove link “E”: (See Figure 2.)
(a) Remove AN4-13A bolt, NAS1149F0463P washer, and MS21042-4 nut that secures link
“E” to the arm assembly and pushrod assembly.
(b) Remove the AN4-16A bolt, MS21042-4 nut, NAS1149F0463P washer, NAS1149F0432P
washer, and two 82695-96 bushings that secures link “E” to the pushrod and the motor-
actuator unit.
(c) Remove safety wire from AN4H30 bolt that secures link “E” to its support bracket. Remove
the bolt, AN310-4 nut, one each NAS1149F0463P and NAS1149F0432P washers (under
nut), and cotter pin.
(d) Remove link “E”.
(2) To remove the 85097-2 pushrod assembly: (See Figure 2.)
(a) Remove AN4-13A bolt, NAS1149F0463P washer, and MS21042-4 nut connecting the
pushrod assembly to the arm assembly and link “E.”
(b) Remove AN24-14A bolt, one each NAS1149F0463P and NAS1149F0432P washers, and
MS21042-4 nut connecting the pushrod assembly to the cam assembly.
(c) Remove the 85097-2 pushrod assembly.
(3) To remove arm assembly: (See Figure 2.)
(a) Remove AN4-13A bolt, NAS1149F0463P washer, and MS21042-4 nut connecting the
arm assembly to the pushrod assembly.and link “E”.
(b) Remove the AN24-34A bolt, MS21042-4 nut, two 82695-97 bushings, an
NAS1149F0432P washer, two NAS1149F0663P and two NAS1149F0632P washers that
secure the arm assembly to the tube assembly and aft link assembly.
(c) Remove arm assembly.
(4) To remove the aft link assembly: (See Figure 2.)
(a) Disconnect the flap position indicator cable from arm of the aft link assembly by removing
the PS10036 swing keeper.
(b) Remove the AN24-34A bolt, MS21042-4 nut, two 82695-97 bushings, an
NAS1149F0432P washer, two NAS1149F0663P and two NAS1149F0632P washers that
secure the aft link assembly to the tube assembly and arm assembly.
(c) Remove safety wire from AN4H34 bolt that secures the aft link to its support bracket.
Remove the bolt, AN310-4 nut, two NAS1149F0463P washers (under nut), and and cotter
pin.
(d) Remove link.
(5) To remove the flap drive pushrod assembly: (See Figures 2 and 3.)
(a) Loosen appropriate hose clamp on small end of bellows.
(b) For left flap drive pushrod:
1 Remove the AN4-16A bolt, MS21042-4 nut, NAS1149F0463P washer,
NAS1149F0432P washer, and two 82695-96 bushings that secures the pushrod
clevis to link “E” and the actuator- motor assembly.
2 Remove NAS464-P5A9 bolt, and MS 21042-5 nut that secures the pushrod clevis to
the left inboard bellcrank assembly.