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(i) Rotate air bleed retainer clips into position and use crowfoot wrench to secure with bolts,
washers, and nuts. Torque bolts to 15 in-lb (1.69 Nm) and apply torque seal. (Refer to
AMM 30-05)
(j) Set ICE PROTECT power switch to ON position.
(k) Set PUMP BKUP switch to ON position.
(l) Verify flow is observed at all porous panels for a minimum of 10 minutes.
(m) Set PUMP BKUP switch to OFF position.
(3) Purge wing porous panels.
(a) Position TKS cart in front of wing to be purged.
(b) Connect porous panels to TKS cart.
1 Remove cable tie securing coupler to wing.
2 Disconnect 5/16-inch supply line feeding the coupler so that coupler remains connected
to line leading to porous panel.
3 Connect TKS cart line to porous panel line with coupler.
4 Connect short length of tubing to 5/16-inch supply line and position other end of tubing
into collection container.
5 Repeat for other porous panel so that both panels on wing being purged are connected
to the TKS cart.
(c) Perform Procedure - Purge Air. (Refer to Section G.)
(d) Perform Procedure - Panel Performance Inspection. (Refer to Section H.)
C I R R U S S E R V I C E B U L L E T I N MOD E L S R 2 2
SB 2X-30-03 R1
Cirrus Design SR22 Serials 3003, 3310, 3326, 3403 Page 9
thru 3424, 3463, and 3499 w/ FIKI ice protection system.
EFFECTIVITY:
November 23, 2009
(e) Close shut-off valves at in-line pressure gauges corresponding to panels being purged.
(f) Disconnect in-line pressure gauges from coupler assemblies.
(g) Set ICE PROTECT mode switch to HIGH position.
(h) Bleed air by energizing system on aircraft and run in "high" mode until full flow into collection
containers without air bubbles is achieved.
Note: Make connections quickly to minimize introducing air into the system lines.
(i) Remove short lengths of tubing from 5/16-inch supply lines.
(j) Connect coupler assemblies to 5/16-inch supply lines. Torque nuts to 48 in-lb (5.4 Nm)
and apply torque seal.
(k) Install cable tie securing coupler to wing.
(l) Repeat on opposite wing.
(4) Purge horizontal stabilizer porous panels.
(a) Position TKS cart in front of avionics bay.
(b) Remove cable tie securing both 5/16-inch coupler assemblies to fuselage wall (downstream
of the aft proportioning unit).
(c) Disconnect both 5/16-inch supply lines feeding the couplers so that couplers remain connected
to lines leading to porous panels.
(d) Connect TKS cart lines to porous panel lines with couplers.
(e) Connect short lengths of tubing to the 5/16-inch supply lines and position other ends of
tubing into collection containers.
(f) Perform Procedure - Purge Air. (Refer to Section G.)
(g) Perform Procedure - Panel Performance Inspection. (Refer to Section H.)
(h) Close shut-off valves at in-line pressure gauges corresponding to panels being purged.
(i) Disconnect in-line pressure gauges from coupler assemblies.
(j) Set ICE PROTECT mode switch to HIGH position.
(k) Bleed air by energizing system on aircraft and run in "high" mode until full flow into collection
containers without air bubbles is achieved.
Note: Make connections quickly to minimize introducing air into the system lines.
(l) Remove short lengths of tubing from 5/16-inch supply lines.
(m) Connect coupler assemblies to 5/16-inch supply lines. Torque nuts to 48 in-lb (5.4 Nm)
and apply torque seal.
(n) Install cable tie securing coupler assemblies to fuselage wall.
(5) Purge elevator tip porous panels.
(a) Position TKS cart in front of avionics bay.
(b) Remove cable tie securing both 3/16-inch coupler assemblies to the fuselage wall (downstream
of aft proportioning unit).
(c) Install the 3/16-inch to 5/16-inch reducer to each of the TKS cart lines.
(d) Disconnect both 3/16-inch supply lines feeding the coupler so that coupler remains connected
to line leading to proportioning unit.
(e) Connect TKS cart lines to porous panel lines.
(f) Connect short lengths of tubing to the 3/16-inch supply lines and position other ends of
tubing into collection containers.
(g) Perform Procedure - Purge Air. (Refer to Section G.)
(h) Perform Procedure - Panel Performance Inspection. (Refer to Section H.)
(i) Close shut-off valves at in-line pressure gauges corresponding to panels being purged.
(j) Disconnect in-line pressure gauges from coupler assemblies.
C I R R U S S E R V I C E B U L L E T I N MOD E L S R 2 2
SB 2X-30-03 R1
Cirrus Design SR22 Serials 3003, 3310, 3326, 3403 Page 10
thru 3424, 3463, and 3499 w/ FIKI ice protection system.
EFFECTIVITY:
November 23, 2009
(k) Set ICE PROTECT mode switch to HIGH position.
(l) Bleed air by energizing system on aircraft and run in "high" mode until full flow into collection
　
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本文鏈接地址：30-00 ICE AND RAIN PROTECTION - Alteration of TKS Anti-Ice S(5)