Technical data

13773-001
27-10
Page 14 30 Nov 2000
H. Aileron System Pulleys (See Figure 27-105)
(1) Removal - Aileron Actuation Pulley-Console
(a) Remove carpeting and access panel CF3C from passenger compartment floor. (Refer to
6-00)
(b) Identify and loosen aileron cable tension via turnbuckle.
(c) Remove MFD. (Refer to 34-40)
(d) Remove cotter pin, castellated nut, washers, and bolt securing aileron push/pull rods to
aileron actuation pulley.
(e) Cut safety wire securing cable to aileron actuation pulley.
(f) Remove cotter pin, castellated nut, washers, spacer, and bolt securing aileron actuation
pulley to console assembly and remove from airplane.
(2) Installation - Aileron Actuation Pulley-Console
(a) Position aileron actuation pulley over console assembly ensuring lockout holes line up,
and install bolt, spacer, washers, castellated nut.
(b) Install bolt, washers, castellated nut, and cotter pin securing aileron push/pull rods to aile-
ron actuation pulley.
(c) Perform Aileron System Rigging Adjustment/Test. (Refer to 27-10)
(d) Install access panel CF3C and carpeting. (Refer to 6-00)
(e) Install MFD. (Refer to 34-40)
(3) Removal - Pulley Gang-Forward
The forward pulley gang is used to route the aileron, rudder, and elevator system control cables.
(a) Remove carpeting and access panel CF3C from passenger compartment floor. (Refer to
6-00)
(b) Identify and loosen aileron cable tension via turnbuckle.
(c) Remove carpeting and access panel CF5 from baggage compartment floor. (Refer to 6-
00)
(d) Identify and loosen rudder and elevator cable tension via turnbuckle.
(e) Remove pilot and co-pilot seats.(Refer to 25-10)
(f) Remove carpeting and access panel CF2L and CF2R from cockpit floor. (Refer to 6-00)
(g) Remove cotter pin, nut, washers, spacers, and bolt securing pulleys to console assembly
and remove components from airplane.
(4) Installation - Pulley Gang-Forward
(a) Position and install bolt, spacers, washers, nut, and cotter pin securing pulleys to console
assembly.
(b) Rig aileron system and perform Aileron System Rigging Adjustment/Test. (Refer to 27-10)
(c) Rig rudder system and perform Rudder System Rigging Adjustment and Cable Tension
Adjustment/Test. (Refer to 27-20)
(d) Rig elevator system and perform Elevator System Rigging Adjustment/Test. (Refer to 27-
30)
(e) Install access panels CF3C, CF5, CF2L, and CF2R. (Refer to 6-00)
(f) Install carpeting. (Refer to 25-10)
(5) Removal - Kick-Out Pulley
(a) Remove passenger compartment seats. (Refer to 25-10)
(b) Remove carpeting and access panel CF4C from passenger compartment floor. (Refer to
6-00)
(c) Identify and loosen aileron cable tension via turnbuckle.