sr22 amm - cirrus design authorized service center...

C I R R U S A I R P L A N E M A I N T E N A N C E M A N U A L M O D E L S S R 2 2 A N D S R 2 2 T

30-06Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice

Protection

EFFECTIVITY:

ICE PROTECTION - DISTRIBUTION:SERIALS 22-2438 & SUBS, 22T-0001 & SUBS W/ BASIC² ICE PROTECTION

1. DESCRIPTION

This section describes the portion of the Basic² Ice Protection System pertaining to the distribution of deic-ing fluid. The system consists of six porous panels, propeller slinger ring, four proportioning units, metering pump, filter, strainer, fluid tank, filler cap, electrical switching, and system plumbing. The system operates on 28 VDC supplied through the 5-amp ICE PROTECTION circuit breaker on Main Bus 1.

Serials 22-3849 & subs, 22T-0319 & subs: 28 VDC for the deicing fluid level sensor is supplied through the 3-amp FUEL QTY circuit breaker on MAIN BUS 1. The 28 VDC is converted to 12 VDC for the deicing fluid level sensor through the Level Sensor Power Circuit Card.

For a detailed system description refer to Chapter 30, Section 00 Ice and Rain Protection. (Refer to 30-00)

For information on deicing fluid replenishing, re-use, and storage refer to the Replenishing Section of Chapter 12 - Servicing. (Refer to 12-10)

For information on Crew Alerting System (CAS) annunciations refer to Chapter 31, Section 50 - Indicating/Recording Systems. (Refer to 31-50)

For information pertaining to the Level Sensor Power Circuit Card, see Chapter 24, Section 50 - Electrical Load Distribution. (Refer to 24-50)

01 May 2012

30-06

Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection

EFFECTIVITY:


15 Jun 2010

2. MAINTENANCE PRACTICES

A. Metering Pump - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection (See Figure 30-062)

(1) Servicing - Metering Pump

Note: To remove air from the system requires a significant amount of pressure (45-55psi), which the metering pump(s) is not capable of creating in most circum-stances. The most effective and efficient way of removing air from the porous membrane is to perform the Porous Panel Purging procedure.

The metering pump is primed by the priming pump during the first 10 seconds of operation.

(a) Cycle system ON - MAX for 10 seconds, then OFF for 10 seconds.(b) Repeat until metering pumps are primed.(c) If metering pump does not prime after 20 cycles:

1 Disconnect supply line from metering pump to filter and supply line from priming pump to wing tank.

2 Continue to cycle system ON - MAX (10 seconds) and OFF (10 seconds) until clear, air-free fluid is observed from priming pump.

3 Reconnect supply lines and perform Operational Check - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection

(2) Removal - Metering Pump(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.(b) Pull ICE PROTECTION circuit breaker.(c) Drain deicing fluid. (Refer to 12-10)(d) Remove LH passenger seat. (Refer to 25-10)(e) Remove carpeting to expose access panel CF4L. (Refer to 06-00)(f) Remove cabin access panel CF4L. (Refer to 06-00)(g) Disconnect electrical connector to metering pump.(h) Place container below coupling to catch fluid drip.(i) Disconnect nuts, olives, and O-rings securing tubing to metering pump.(j) Remove screws and washers securing priming pump to metering pump.(k) Remove bolts and washers securing metering pump to fuselage. Remove metering pump

from airplane.(3) Installation - Metering Pump

(a) Position metering pump to fuselage and secure with bolts and washers.(b) Position priming pump to metering pump and secure with screws and washers.(c) Position tubing to metering pump and secure with nuts, olives, and new O-rings.(d) Connect electrical connector to metering pump.(e) Install cabin access panel CF4L. (Refer to 06-00)(f) Install carpeting. (Refer to 25-10)(g) Install LH passenger seat. (Refer to 25-10)(h) Fill tank with approved deicing fluid. (Refer to 12-10)(i) Reset ICE PROTECTION circuit breaker.(j) Perform Servicing - Metering Pump. (Refer to 30-06)(k) Perform Operational Test - Ice Protection System. (Refer to 30-06)(l) Perform Functional Test - Metering Pump Performance. (Refer to 30-06)



Protection

EFFECTIVITY:

(4) Functional Test - Metering Pump Performance (See Figure 30-061)This procedure measures the output of the metering pump at its "critical pressure" to verify acceptable performance.

(a) Acquire necessary tools, equipment, and supplies.

* or equivalent.(b) Remove LH passenger seat, carpeting, and cabin access panel CF4L. (Refer to 25-10)(c) Disconnect metering pump from J1391 connector and install metering pump voltage mea-

surement harness in series between aircraft and pump connectors. (d) Disconnect and cap tubing attached to pressure output port of the desired metering pump. (e) Connect 5/16-inch tubing of Pump Flow Test Rig to pressure output port of pump. (f) Position outlet of Pump Flow Test Rig into a clean, empty container.(g) Connect 28 ±1 VDC external power to external power receptacle.

Note: Do not exceed aircraft bus voltages while operating ground power supply.

(h) Test pressure for metering pump.1 Record Aircraft Serial Number (ASN) and date of Functional Test.2 Set System Mode switch to HIGH, and activate metering pump by setting System

Switch to ON.3 Observe voltage of metering pump and adjust its operating voltage to:

• Metering pump without MOD NO. 1: 27.10 VDC nominal via ground power sup-ply.

• Metering pump with MOD NO. 1 and Above: 27.80 VDC nominal via ground power supply.

CAUTION: Ensure supplied voltage of ground power supply does not drift in excess of ±0.02 VDC during test.

(i) Perform metering pump flow rate:1 Using Pump Flow Test Rig, restrict fluid flow from metering pump until output pres-

sure is increased to 50 psi.

Description P/N or Spec. Supplier Purpose

Graduated Cylinder, 500mL(5.0mL divisions maximum)

- Any Source Measure flow rate of pump.

Pump Flow Test Rig T11071* Cirrus Design Purge deicing fluid from elevator tip porous panels.

Digital Volt Meter(0.01V Resolution)

- Any Source Maintain controlled external power.

Collection container, 5-gallon

- Any Source Collect fluid.

Voltage Measurement Harness (2)

T11070* Any Source Connect in series between air-craft and pump connectors.

Variable Power Supply 28V (50 Amp Capacity)

- Any Source Maintain controlled external power.

15 Jun 2010

30-06


EFFECTIVITY:


15 Jun 2010

2 To measure flow rate of metering pump, use stopwatch and graduated cylinder (5.0mL divisions maximum) to take a volume measurement for precisely 1 minute.

Note: The measured volume will be the flow rate of metering pump.

3 Repeat metering pump Flow Rate a minimum of two times and average the results. The result is the metering pump Output flow rate.

4 When metering pump Output Flow Test is complete, set System Switch to OFF.5 Disconnect tubing of Pump Flow Test Rig from metering pump. 6 Reconnect aircraft tubing to pressure output port of metering pump. (Refer to 20-80)

(j) Verify measured output of pump is between 161 and 171 mL/min.(k) If required, replace metering pump(s). (Refer to 30-06)(l) Remove voltage measurement harnesses from metering pump. (m) Reconnect metering pump to J1391 connector. (n) Install LH passenger seat, carpeting, and cabin access panel CF4L. (Refer to 25-10)



Protection;

EFFECTIVITY:

Figure 30-061 Metering Pump Performance - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection;

psi0

20

4060

80

100

Connect pump flow test rig to output port of pump to be tested.

SR22_MM30_3317

LEGEND 1. Pump Pressure Output Port 2. Pump Flow Test Rig

1

NOTE

Install voltage measurement harness in series betweenaircraft and pump connectors.

PUMP(REF)

2

TO CONTAINER

P706(REF)

Serials 22-2334, 22-2420, 22-2438 thru 22-3402,22-3403 & subs, 22T-0001 & subs w/ Basic 2 Ice Protection.

15 Jun 2010

30-06


EFFECTIVITY:


15 Jun 2010

B. Priming Pump - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection (See Figure 30-062)

(1) Removal - Priming Pump(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.(b) Pull ICE PROTECTION circuit breaker.(c) Drain deicing fluid. (Refer to 12-10)(d) Remove LH passenger seat. (Refer to 25-10)(e) Remove carpeting to expose access panel CF4L. (Refer to 06-00)(f) Remove cabin access panel CF4L. (Refer to 06-00)(g) Disconnect electrical connector to priming pump.(h) Place container below coupling to catch fluid drip.(i) Disconnect nuts, olives, and O-rings securing tubing to priming pump.(j) Remove screws and washers securing priming pump to metering pump. Remove priming

pump from airplane.(2) Installation - Priming Pump

(a) Position priming pump to metering pump and secure with screws and washers.(b) Position tubing to priming pump and secure with nuts, olives, and new O-rings.(c) Connect electrical connector to priming pump.(d) Install cabin access panel CF4L. (Refer to 06-00)(e) Install carpeting. (Refer to 25-10)(f) Install LH passenger seat. (Refer to 25-10)(g) Fill tank with approved deicing fluid. (Refer to 12-10)(h) Reset ICE PROTECTION circuit breaker.(i) Perform Servicing - Metering Pump. (Refer to 30-06)(j) Perform Operational Test - Ice Protection System. (Refer to 30-06)



Protection

EFFECTIVITY:

C. Filter Element - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection (See Figure 30-062)

(1) Removal - Filter Element(a) Drain deicing fluid. (Refer to 12-10)(b) Remove LH passenger seat. (Refer to 25-10)(c) Remove carpeting to expose access panel CF4L. (Refer to 06-00)(d) Remove cabin access panel CF4L. (Refer to 06-00)(e) Place container below coupling to catch fluid drip.(f) Disconnect nuts, olives, and O-rings securing tubing to Filter Element.(g) Remove bolts and washers securing Filter Element to fuselage. Remove Filter Element

from airplane.(2) Disassembly - Filter Element

(a) Remove bolts, washers, and nuts securing brackets to filter element. Discard filter ele-ment.

(3) Assembly - Filter Element

Note: Ensure filter is installed so air bleed screw is located on top and flow arrow indicates the proper direction with respect to the metering pump/proportion-ing units and inlet/outlet placards on the filter bracket.

(a) Position new filter element between brackets and secure with bolts, washers, and nuts. Torque nuts to 15 in-lb (1.69 Nm).

(4) Installation - Filter Element(a) Position Filter Element to fuselage and secure with bolts and washers.(b) Position tubing to Filter Element and secure with nuts, olives, and new O-rings.(c) Fill tank with approved deicing fluid. (Refer to 12-10)(d) Perform Adjustment/Test - Air Bleed Valve. (Refer to 30-06)(e) Install cabin access panel CF4L. (Refer to 06-00)(f) Install carpeting. (Refer to 25-10)(g) Install LH passenger seat. (Refer to 25-10)(h) Perform Operational Test - Ice Protection System. (Refer to 30-06)

(5) Adjustment/Test - Air Bleed Valve(a) Loosen bolts, washers, and nuts securing air bleed retainer clip. Rotate air bleed retainer

clip as needed to access air bleed screw.(b) Place container below air bleed valve to catch fluid drip.(c) Loosen air bleed screw.(d) Set BAT 1 switch to ON position.(e) Serials 22-2438 thru 22-3402 w/ Basic² Ice Protection: Set ICE PROTECT mode switch to

MAX position.(f) Serials 22-3403 & subs, 22T-0001 & subs w/ Basic² Ice Protection: Set ICE PROTECT

mode switch to HIGH position.(g) Set ICE PROTECT power switch to ON position.(h) Allow system to run until clear, air-free deicing fluid is emitted from air bleed valve.(i) Tighten air bleed screw.(j) Set ICE PROTECT power switch to OFF position.(k) Set BAT 1 switch to OFF position.(l) Rotate air bleed retainer clip into position and secure with bolts, washers, and nuts. Torque

bolts to 15 in-lb (1.69 Nm).

15 Jun 2010

30-06


EFFECTIVITY:


15 Jun 2010

D. In-line Strainer - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection (See Figure 30-062)

(1) Servicing - In-Line Strainer


(b) Remove in-line strainer. (Refer to 30-06)(c) Using flow arrow indicator, determine outlet end of strainer.(d) Loosen outlet end of strainer to remove strainer from housing assembly.(e) Remove and discard o-ring from strainer.(f) Visually inspect strainer screen for particles.(g) Clean strainer screen with water until all particles are removed. Allow strainer to air dry.(h) Visually inspect housing assembly interior for contaminants.(i) Flush housing assembly with water until all contaminants are removed. Allow housing

assembly to air dry.(j) Position new o-ring on strainer. Slide o-ring up to hex head of strainer screen.(k) Install strainer to housing assembly. Torque strainer to 170 - 190 in-lb (19.2 - 21.4 Nm).(l) Install in-line strainer. (Refer to 30-06)

(2) Removal - In-line Strainer(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.(b) Pull ICE PROTECT A and ICE PROTECT B circuit breakers.(c) Drain deicing fluid. (Refer to 12-10)(d) Remove access panel CF3L. (Refer to 06-00)(e) Place container below coupling to catch fluid drip.(f) Disconnect nuts, olives, and O-rings securing tubing to strainer.(g) Remove strainer from airplane.

(3) Installation - In-line Strainer(a) With flow arrow indicator pointing towards the metering pump, position tubing to strainer

and secure with nuts, olives, and new O-rings.(b) Install access panel CF3L. (Refer to 06-00)(c) Reset ICE PROTECT A and ICE PROTECT B circuit breakers.(d) Fill tank with approved deicing fluid. (Refer to 12-10)(e) Perform Servicing - Metering Pump. (Refer to 30-06)(f) Perform Operational Test - Ice Protection System. (Refer to 30-06)

Description P/N or Spec. Supplier Purpose

O-ring Refer to IPC, Ice Pro-tection System Instal-lation, Distribution

Any Source Seal.



Protection

EFFECTIVITY:

E. Horizontal Proportioning Unit - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protec-tion (See Figure 30-062)

(1) Removal - Horizontal Proportioning Unit(a) Remove access panel CB6. (Refer to 06-00)(b) Place container below coupling to catch fluid drip.(c) Disconnect nuts, olives, and O-rings securing tubing to proportioning unit.(d) Remove bolts and washers securing proportioning unit to access panel.

(2) Installation - Horizontal Proportioning Unit(a) Position proportioning unit to access panel and secure with bolts and washers.

Note: Ensure proportioning unit is installed in the correct direction and verify each supply line is connected to the correct port.

(b) Position tubing to proportioning unit and secure with nuts, olives, and new O-rings.(c) Install access panel CB6. (Refer to 06-00)(d) Perform Operational Test - Ice Protection System. (Refer to 30-06)

15 Jun 2010

30-06


EFFECTIVITY:


15 Jun 2010

F. Wing and Propeller Proportioning Unit - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection (See Figure 30-062)

(1) Removal - Wing and Propeller Proportioning Unit(a) Remove LH crew seat. (Refer to 25-10)(b) Remove carpeting. (Refer to 25-10)(c) Remove access panel CF2L. (Refer to 06-00)(d) Place container below coupling to catch fluid drip.(e) Disconnect nuts, olives, and O-rings securing tubing to proportioning unit.(f) Remove bolts, washers, and spacers securing proportioning unit to bracket.

(2) Installation - Wing and Propeller Proportioning Unit(a) Position proportioning unit to bracket and secure with bolts, washers, and spacers.

Note: Ensure proportioning unit is installed in the correct direction and verify each supply line is connected to the correct port.

(b) Position tubing to proportioning unit and secure with nuts, olives, and new O-rings.(c) Install access panel CF2L. (Refer to 06-00)(d) Install carpeting. (Refer to 25-10)(e) Install LH crew seat. (Refer to 25-10)(f) Perform Operational Test - Ice Protection System. (Refer to 30-06)



Protection

EFFECTIVITY:

G. Fluid Tank - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection (See Figure 30-062)

The fluid tank on these airplanes is integral to the LH wing and may not be removed.

(1) Approved Repair - Fluid TankThe following procedures are to be used for sealing integral fluid tanks made of composite mate-rials. If a repair must be made to a bondline, joint or seam, the repair should be made using a sealant that meets or exceeds MIL-S-8802. (Refer to 20-10) If the leak is from a small pinhole located away from any bondlines, joints or seams, the repair must be made using a Type 2, Class 1 non-structural resin system. Repair procedures for composites are covered in Chapter 51-00. (Refer to 51-00)

WARNING: Prevent fluid drain from becoming restricted when sealing fluid tank.


(b) Drain fluid tank. (Refer to 12-10)(c) Remove wing access panel LW2. (Refer to 06-00)(d) Solvent clean the area to be repaired with acetone. (Refer to 20-30)

CAUTION: Use caution not to sand through resin coat exposing fibres. Sanding through the resin coat and exposing fibers will be cause for composite repair.

(e) Lightly sand the composite areas to be sealed with 200-grit sandpaper. Sand an area larger than the initial repair area.

(f) Remove all large contaminates using a stiff bristle brush.(g) Solvent clean all surfaces to be sealed with isopropyl alcohol. (Refer to 20-30)(h) Mix sealant. (Refer to 51-30)

Item P/N or Spec. Supplier Purpose

Methyl Ethyl Ketone (MEK)

ASTM D740 Type 1or 2

Any Source General cleaning.

Non-structural Resin Repair System

Shell EPON 862/heloxy 68 & Teta 3234 resin system Type 2 Class 1

Shell Oil Seal pinholes that are away from bondlines, joints or seams.

Gloves - Any Source Protect hands.

Cotton cloth (clean and lint free)

- Any Source General cleaning.

Application Brush (nylon) - Any Source Tank repair.

Compressed Air (clean, oil and moisture free)

- Any Source General cleaning.

Sealant Gun - Any Source Apply sealant.

Sandpaper - Aluminum Oxide

200 grit Any Source Prepare surface.

15 Dec 2014

30-06


EFFECTIVITY:


15 Jun 2010

(i) Fillet, fay or injection seal as required. Brush sealant or resin over repair area making sure brushed area is larger than the repaired area. (Refer to 20-10)

(j) Allow sealant to fully cure. (Refer to 51-20)(k) Install wing access panel LW2. (Refer to 06-00)(l) Using hex key, close drain valve.(m) Fill tank with approved deicing fluid. (Refer to 12-10)(n) Perform Operational Test - Ice Protection System. (Refer to 30-06)(o) Visually inspect tank seams for any signs of leakage or stains. If any leaks are present,

repair tank as needed. (Refer to 30-06)



Protection

EFFECTIVITY:

H. Outlet Strainer - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection (See Figure 30-062)

(1) Removal - Outlet Strainer(a) Drain deicing fluid. (Refer to 12-10)(b) Remove wing access panel LW2. (Refer to 06-00)(c) Remove wing root access panel LW1. (Refer to 06-00)(d) Disconnect nut, olive, and O-ring securing tubing to Outlet Strainer.(e) Remove Outlet Strainer from wing rib bushing.

(2) Installation - Outlet Strainer(a) Install Outlet Strainer into wing rib bushing.(b) Position tubing to Outlet Strainer and secure with nut, olive, and new O-ring.(c) Install wing access panel LW2. (Refer to 06-00)(d) Install wing root access panel LW1. (Refer to 06-00)(e) Fill tank with approved deicing fluid. (Refer to 12-10)(f) Perform Operational Test - Ice Protection System. (Refer to 30-06)

15 Jun 2010

30-06

Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection & w/ Perspective Avionics

EFFECTIVITY:


01 May 2012

I. Deicing Fluid Level Sensor - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection & w/ Perspective Avionics (See Figure 30-062)

CAUTION: Serials 22-2438 thru 22-3848, 22T-0001 thru 22T-0318: Do not allow isopropyl alcohol or acetone to contact sensor dial or cracking and crazing will occur.

(1) Removal - Deicing Fluid Level Sensor(a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions.(b) Pull ICE PROTECTION circuit breaker.(c) Remove wing access panel LW1. (Refer to 06-00)(d) Disconnect sensor connector from wire harness.(e) Serials 22-2438 thru 22-3848, 22T-0001 thru 22T-0318: Sensor dial

1 Remove screws securing sensor dial to sending unit. Remove sensor dial from air-plane.

(f) Sending unit1 Drain deicing fluid. (Refer to 12-10)2 Serials 22-2438 thru 22-3848, 22T-0001 thru 22T-0318: Remove screws securing

sending unit to wing rib. Remove sending unit and gasket from airplane.3 Serials 22-3849 & subs, 22T-0319 & subs: Remove screws and washers securing

sending unit to wing rib. Remove sending unit and gasket from airplane.(2) Installation - Deicing Fluid Level Sensor

(a) Sending unit1 Install gasket onto sending unit.2 Serials 22-2438 thru 22-3848, 22T-0001 thru 22T-0318: Position sending unit and

gasket to wing rib and secure with screws. Torque screws up to 30 in-lb (3.39 Nm) plus nut drag.

3 Serials 22-3849 & subs, 22T-0319 & subs: Position sending unit and gasket to wing rib and secure with screws and washers. Torque screws up to 30 in-lb (3.39 Nm) plus nut drag.

4 Fill tank with approved deicing fluid. (Refer to 12-10)(b) Serials 22-2438 thru 22-3848, 22T-0001 thru 22T-0318: Sensor dial

1 Position sensor dial to sending unit and secure with screws. (c) Connect sensor connector to wire harness.(d) Install wing access panel LW1. (Refer to 06-00)(e) Reset ICE PROTECTION circuit breaker.(f) Perform Operational Test - Ice Protection System. (Refer to 30-06)

(3) Functional Test - Deicing Fluid Level Sensor(a) Drain deicing fluid tank until empty. (Refer to 12-10)(b) Set BAT1 and AVIONICS switches to ON(c) Verify the indicated fluid quantity is 0.0 - 0.1 US gallons when the tank is empty.(d) Replenish the deicing fluid tank with 3.5 US gallons of fluid. (Refer to 12-10)(e) Verify indicated fluid quantity is 3.5 ±0.2 US gallons.(f) Set BAT 1 and AVIONICS switches to OFF positions.



Protection

EFFECTIVITY:

J. Drain Valve - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection (See Figure 30-062)

(1) Removal - Drain Valve(a) Perform Deicing Fluid Draining. (Refer to 12-10)(b) Remove wing access panel LW2 or RW2. (Refer to 06-00)(c) Remove nut, spacer (if installed with drain valve assembly), and o-ring securing drain

valve to access panel.(2) Installation - Drain Valve

(a) Install nut, spacer (if included with drain valve assembly), and o-ring securing drain valve to access panel.

(b) Drain valve assembly w/ spacer: Torque nut to 60 - 70 in-lb (6.8 - 7.9 Nm).(c) Drain valve assembly w/o spacer: Torque nut to 90-100 in-lb (10.2 - 11.3 Nm).(d) Install wing access panel LW2 or RW2. (Refer to 06-00)(e) Perform Deicing Fluid Replenishment. (Refer to 12-10)

K. Ice Protection Switch - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection

The ice protection switch is integral to the bolster panel. For maintenance practices pertinent to the bolster panel, see Electronic Panels and Multipurpose Parts. (Refer to 31-10)

L. Operational Test - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection

(a) Set BAT 1 switch to ON position.

Note: Increasing the system flow rate (MAX vs. NORM) will increase the arterial pressure of the system which promotes the complete wet-out of the porous panels.

(b) Set ICE PROTECT power switch to ON position.(c) Set ICE PROTECT mode switch to MAX position.(d) Verify evidence of deicing fluid along the entire length of porous panels and from slinger

ring assembly feed tube.(e) Visually inspect components and fittings for evidence of leaking fluid.(f) Set ICE PROTECT power switch to OFF position.(g) Set BAT 1 switch to OFF position.

15 Jun 2010

30-06


EFFECTIVITY:


15 Jun 2010

b

Figure 30-062Ice Protection System - Serials 22-2438 & subs, 22T-0001 & subs w/ Basic² Ice Protection (Sheet 1 of 7)

SR22_MM30_2394B




Protection

EFFECTIVITY:


6

16

TO HORIZONTALPROPORTIONING

UNIT

FEED LINEFROM FLUID

TANK

TO WING ANDPROPELLER

PROPORTIONINGUNIT

SR22_MM30_2395C

7

FUSELAGE BELLY(REF)

5

5

109

TYPICAL DETAIL

LEGEND 1. Filter Element 2. Washer 3. Bolt 4. Metering Pump 5. Nylon Tubing 6. Fitting 7. Test Port 8. Cap 9. Cable Tie10. Tie Down11. O-ring12. Olive13. Aluminum Nut14. Grommet15. Screw16. Priming Pump17. In-line Strainer Assembly

8

23

1

2

3

4

17

1312

11

5

14

2

15


15 Dec 2014

30-06


EFFECTIVITY:


15 Dec 2014


AIR BLEED SCREW(REF)

22

SR22_MM30_3096B

LEGEND 2. Washer 3. Bolt 5. Nylon Tubing11. O-ring12. Olive13. Aluminum Nut17. In-line Strainer Assembly18. Bracket19. Filter20. In-line Strainer21. Nut22. Retainer Clip23. Safety Wire Tab

17

1312

11

20

5

11

3

3

23

2

18

19

18

223

21

222

21

2

Serials 22-2334, 22-2420, 22-2438 thru 22-3402,22-3403 & subs, 22T-0001 & subs w/ TKS Ice Protection.




Protection

EFFECTIVITY:


Serials22-2438 thru

22-2643.

15

32 25

2

34

Serials 22-3439 & subs,22T-0311 thru 22T-0314,22T-0316 thru 22T-0317,

22T-0319 & subs.

WINGCOLLECTOR

TANK RIB(REF)

3

23

29

34

24

35

15

WINGCOLLECTOR

TANK RIB(REF)

LEGEND 2. Washer 5. Nylon Tubing 9. Cable Tie10. Tie Down11. O-ring12. Olive15. Screw21. Nut24. Bulkhead Fitting25. Gasket26. Filler Cap27. Ring28. Clamp29. Drain Valve30. Outlet Strainer31. Bushing32. Blanking Plate34. Sending Unit35. Base, Sender36. Spacer

SR22_MM30_2397E

15

15 2

2

2

2

3225 5

5

5

1211

11

11

24

2428

26

27

28

5

21

21

21

31

29

30


36

Serials 22-2334 thru 22-3650.

24

15

Serials 22-2438 thru 22-3438w/ Perspective Avionics,22T-0001 thru 22T-0310,

22T-0315, 22T-0318.

2

01 Feb 2013

30-06


EFFECTIVITY:


15 Jun 2010


LEGEND 2. Washer 3. Bolt 5. Nylon Tubing 6. Fitting 7. Test Port 8. Cap 9. Cable Tie10. Tie Down11. O-ring12. Olive13. Aluminum Nut18. Bracket37. Porous Panel38. Proportioning Unit, Horizontal39. Coupler40. Spiral Wrap

SR22_MM30_2396C

5

11

5

11

1312

38

1213

32

ACCESS PANEL CB6(REF)

13

13

11

11

TO PROPORTIONING UNIT

TO METERING PUMP

TO HORIZONTALPOROUS PANEL Serials 22-2334, 22-2420, 22-2438 thru 22-3402,

22-3403 & subs, 22T-0001 & subs w/ Basic 2 Ice Protection.


40

5

13

12

11

37

12

39

5

12



Protection

EFFECTIVITY:


LEGEND 2. Washer 3. Bolt 5. Nylon Tubing 9. Cable Tie10. Tie Down11. O-ring12. Olive13. Aluminum Nut15. Screw18. Bracket21. Nut24. Bulkhead Fitting31. Bushing36. Spacer41. Slinger Ring42. Hose Assembly43. Adel Clamp44. Fluid Line45. Reducer46. Feed Tube

221

2

2

2

Serials 22T-0001 & subs.

21

343

36

43

3

2

21

4224 18

4544

24

45

23

43

10

95

31

46

41

243

3

42

2

18

1524

2

44241112

13

212

FUSELAGE (REF)

TO METERING PUMP

FIREWALL(REF)

TO RH WING

TO LH WING

FORWARDFLOOR(REF)

SR22_MM30_2398BSerials 22-2334, 22-2420, 22-2438 thru 22-3402,22-3403 & subs, 22T-0001 & subs w/ Basic 2 Ice Protection.

21

221

212

PROPORTIONING UNIT(REF)Cover exposed metal of bulkhead fitting

with RTV 736 Sealant.

NOTE

Existing hardware part of baffle assembly.

15 Jun 2010

30-06


EFFECTIVITY:


01 Feb 2013


LEGEND 2. Washer 3. Bolt 5. Nylon Tubing11. O-ring12. Olive13. Aluminum Nut18. Bracket36. Spacer37. Porous Panel39. Coupler47. Proportioning Unit, Wing & Prop

513

1211

513

1211

47

36

11

23 12

13

5

1112

13

5

18


TO FIREWALL

SR22_MM30_3101A

TO METERINGPUMP


Serials 22-2334, 22-2420, 22-2438 thru 22-3402, 22-3403 & subs, 22T-0001 & subs w/ Basic2 Ice Protection.

1312

11

3911

12

13

55

13

12

11

37

Port #5 to outboard RHporous panel/coupler.

Port #4 to inboard RHporous panel/coupler.

NOTE

Port #1 to outboard LHporous panel/coupler.

Port #2 to inboard LHporous panel/coupler.


Serials 22-2334, 22-2420, 22-2438 thru 22-3402, 22-3403 & subs, 22T-0001 & subs w/ Basic 2 Ice Protection.

1312

11

3911

12

13

55

13

12

11

37

sr22 amm - cirrus design authorized service center...

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