CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR22 AND SR22T
22-11
Page 13
All
EFFECTIVITY:
Note: Use a ratcheting open-end wrench and socket for tightening bridle cable
clamp assembly to elevator cable.
Install outboard clamp assembly with bolt heads facing inboard and inboard
clamp assembly with bolt heads facing outboard. Align bolt shafts approxi-
mately perpendicular to 0.0 buttock line. Ensure maximum gap of 0.01 inch
(0.25 mm) between aft end of clamp and bridle cable end fitting.
(f) Position short end of bridle cable and clamp assembly to outboard elevator cable and
secure with bolts and nuts. Torque nuts to 55 ± 5 in-lb (6.2 ± 0.6 Nm). With elevator at 0°
deflection, ensure forward end of clamp is a minimum of 5.5 in (14.0 cm) from aft edge of
servo.
(g) Serials 22-1368 thru 22-1601, 22-1603 thru 22-1839, 22-1841 thru 22-1862, 22-1863 &
subs, 22T-0001 & subs w/o Air Conditioning: Position long end of bridle cable and clamp
assembly to inboard elevator cable and loosely secure with bolts and nuts. With elevator at
0° deflection, ensure forward end of clamp assembly is a minimum of 19.0 in (48.2 cm)
from aft edge of servo.
(h) Serials 22-1602, 22-1840, 22-1863 & subs, 22T-0001 & subs w/ Air Conditioning: Route
long end of bridle cable through mounting bracket hole and between pulley and cable
keeper.
(i) Serials 22-1602, 22-1840, 22-1863 & subs, 22T-0001 & subs w/ Air Conditioning: Position
long end of bridle cable and clamp assembly to inboard elevator cable and loosely secure
with bolts and nuts. With elevator at 0° deflection, ensure forward end of clamp assembly
is a minimum of 18.4 in (46.7 cm) from aft edge of servo.
(j) While pushing long end of bridle cable and clamp assembly aft, tighten clamp to elevator
cable. Torque nuts to 55 ± 5 in-lb (6.2 ± 0.6 Nm).
(k) Using tensiometer, verify bridle cable tension forward of bridle cable clamps is set to 25.0
± 5.0 lb (11.3 ± 2.3 kg). If bridle cable tension falls outside specified tolerance, loosen aft
clamp assembly and adjust bridle cable as required to obtain 25.0 ± 5.0 lb (11.3 ± 2.3 kg).
(l) Using tensiometer, verify elevator control cable tension forward of the bridle cable clamp
assemblies. (See Figure 06-001)
(m) Serials 22-1602, 22-1840, 22-1863 & subs, 22T-0001 & subs w/ Air Conditioning: Position
fairleads and cables to fairlead bracket and secure with screws, washers, and nuts.
(n) Remove rigging lockout pin and tool from elevator empennage bellcrank.
(o) Ensure flight control systems operate through full range of travel without binding, obstruc-
tion, or excessive friction.
(p) Ensure bridle cable remains in capstan grooves during full elevator and pitch servo travel
and bridle cable moves freely through cable guards without chafing.
(q) Serials 22-1602, 22-1840, 22-1863 & subs, 22T-0001 & subs w/ Air Conditioning: Ensure
bridle cable moves freely through mounting bracket without chafing.
(r) Install access panel RE1. (Refer to 06-00)
15 Jun 2010
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