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Pump#2 only. (Refer to Section M.)
(c) Serials 3003 and 3420: Perform Procedure - Metering Pump Flow Output for Pump#1 and
Pump#2. (Refer to Section M.)
(11) Aircraft temperature between -30°C to 0°C: Perform the following steps.
(a) Fill both glycol tanks on aircraft with anti-ice fluid. (Refer to AMM 12-10)
(b) Fill pressure tank on TKS cart ¾ full with anti-ice fluid and replace access lid.
Note: Ensure access lid gasket is in place.
(c) Perform Procedure - Porous Panel Purge. (Refer to Section F.)
(d) Perform Procedure - Ground Flow Test #1. (Refer to Section I.)
(12) Aircraft temperature above 0°C: Perform Procedure - Ground Flow Test #2 (Refer to Section J.)
(13) Remove voltage measurement harnesses from Pump#1 and Pump#2.
(14) Reconnect Pump#1 to J1391 connector and Pump#2 to J1392 connector.
(15) Remove drain troughs from wing, horizontal stabilizer, vertical stabilizer, and elevator tips.
(16) Remove tygon tubing from propeller slinger ring nozzle.
(17) Remove drop cloth from avionics bay.
(18) Install LH passenger seat, carpeting, and cabin access panel CF4L. (Refer to AMM 25-10)
(19) Install wing access panels LW4, LW9, RW4, and RW9. (Refer to AMM 6-00)
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 7
thru 3424, 3463, and 3499 w/ FIKI ice protection system.
EFFECTIVITY:
November 23, 2009
(20) Install empennage access panel RE3. (Refer to AMM 6-00)
(21) At LH edge of bolster switch panel, peel graphic overlay indicating “FLIGHT INTO KNOWN
ICING IS PROHIBITED” from bolster panel. (See Figure 3)
(22) Solvent clean installation surface of removed graphic overlay. (Refer to AMM 20-30)
(23) Insert the AFMS into POH.
(24) Update MFD checklists.
(a) Proceed online to the following website:
http://servicecenters.cirrusdesign.com/techpubs/mfdchecklists_sr22perspective.asp
(b) Save and unzip the appropriate checklist data file to your computer:
Serials w/o Turbo: Click SR22 Prspctv FIKI Rev 0.zip (without Turbo, with FIKI).
Serials w/ Turbo: Click SR22 Prspctv FIKI Turbo Rev 0.zip (with Turbo, with FIKI).
(c) Remove SD card with old checklists from MFD card slot.
(d) Copy chklist.ace and startup_scrn.zip to SD card.
(e) In the aircraft, set BAT 1, BAT 2, and AVIONICS switches to OFF positions.
(f) Insert SD card into MFD card slot.
(g) Set BAT 1 and AVIONICS switches to ON positions.
(h) After system initialization, under the Database status window on main startup screen of
MFD, verify checklists files are loaded.
(i) Set BAT 1 and AVIONICS switches to OFF positions.
(25) Retain Ground Flow Test Card or record test results in Aircraft Logbook.
(26) Complete airplane records by noting compliance with SB 2X-30-03 R1 in Aircraft Logbook.
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 8
thru 3424, 3463, and 3499 w/ FIKI ice protection system.
EFFECTIVITY:
November 23, 2009
F. Procedure - Porous Panel Purge.
(1) If purging with anti-ice fluid, purge arterial lines and components.
(a) Set ICE PROTECT mode switch to HIGH position.
(b) Set ICE PROTECT power switch to ON position.
CAUTION: With both pumps running, flow rate will be doubled and anti-ice fluid will be
exhausted in approximately 35 minutes. Do not allow glycol tanks to run dry.
(c) Set PUMP BKUP switch to ON position.
CAUTION: Ground operation of windshield sprayer will result in anti-ice fluid spraying
over the top of the fuselage. Ensure personnel are not in path of spray.
(d) Prime main pumps by depressing WINDSHIELD button (energizes windshield pump for 3
seconds) every 3 to 5 seconds until fluid squirts out of both windshield nozzles.
(e) At filter assembly, observe tubing at filter outlets. Allow system to run until no air is seen
exiting either filter.
(f) Set ICE PROTECT power switch to OFF position.
(g) Set PUMP BKUP switch to OFF position.
(2) If purging with anti-ice fluid, bleed air from filters and purge lines to panels.
(a) Using crowfoot wrench, loosen bolts, washers, and nuts securing air bleed retainer clips to
both filters. Rotate air bleed retainer clips as needed to access air bleed screws. (Refer to
AMM 30-05)
(b) Position container below air bleed valves to catch fluid drip.
(c) Loosen air bleed screws.
(d) Set ICE PROTECT mode switch to HIGH position.
(e) Set ICE PROTECT power switch to ON position.
(f) Allow system to run until clear, air-free anti-ice fluid is emitted from air bleed valves.
(g) Tighten air bleed screws.
(h) Set ICE PROTECT power switch to OFF position.
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30-00 ICE AND RAIN PROTECTION - Alteration of TKS Anti-Ice S(4)
