71-00 Power Plant - Cirrus Design Authorized Service Center Home

Transcription

CIRRUS
AIRPLANE MAINTENANCE MANUAL
MODEL SR20
POWER PLANT
1. GENERAL
This chapter describes maintenance practices for the airplane systems which provide the means to induce
and convert fuel-air mixture into power such as the engine, baffling, cowling, mount, attach fittings, electrical harnesses, air intake, and engine drains.
2. DESCRIPTION
A. Engine
The airplane is powered by a Teledyne Continental IO-360-ES engine. The engine is a six cylinder,
horizontally opposed, fuel injected, air-cooled, wet sump, power plant incorporating a down01 May
2012 induction system, tuned exhaust, and provisions for front and rear mounted accessories. (See
Figure 71-001) (See Figure 71-002) (See Figure 71-003)
B. Baffling
Sheet metal baffles are installed on the engine to direct the air flow around the cylinders and other
engine compartment components. To help direct and contain air flow in the engine compartment, the
baffles utilize fiber reinforced silicon seals in contact with the cowling around the circumference of the
engine.
EFFECTIVITY:
All
71-00
Page 1
01 Jan 2012
CIRRUS
MODEL SR20
3. TROUBLESHOOTING
TROUBLE
Engine will not start.
PROBABLE CAUSE
REMEDY
Improper use of starting procedure.
Review starting procedure. See
POH.
Fuel tank empty.
Inspect and fill tank. (Refer to 1210)
Mixture control in SHUTOFF posi- Advance mixture control to RICH
tion.
position.
Engine will not run at idle RPM.
71-00
Page 2
15 Jun 2010
Fuel selector valve in OFF position.
Place selector valve in ON position to tank known to contain fuel.
Fuel vaporization.
Turn boost pump ON.
Engine flooded.
Turn off boost pump and ignition
switch. Advance throttle to full
OPEN, retard fuel control to full
LEAN, and crank engine to clear
cylinders of excess fuel. Repeat
starting procedure.
Water in fuel system.
Sample fuel. See POH. If water
present, drain and flush fuel system. (Refer to 12-10)
Fuel contamination.
Drain and flush fuel system.
(Refer to 12-10)
Defective magneto switch or
grounded magneto leads.
Check continuity. Repair or
replace switch or leads.
Spark plugs fouled.
Remove, clean, and re-gap. Refer
to the engine manufacturer's
approved service instructions.
Excessive starter slippage.
Replace starter adapter. Refer to
the manufacturer’s approved
Instructions For Continued Airworthiness.
Defective ignition system.
Inspect and replace necessary
components. (Refer to 74-00)
Induction system leak.
Inspect hose for cracks. Tighten or
replace loose or damaged hose
connections.
Fuel system malfunction.
Isolate cause and correct.
Fuel injection system improperly
adjusted.
See “Engine Fuel System Troubleshooting.” (Refer to 73-00)
Air leak in intake manifold.
Torque loose connection or
replace malfunctioning part.
EFFECTIVITY:
All
CIRRUS
TROUBLE
Rough idling.
PROBABLE CAUSE
MODEL SR20
REMEDY
Fuel injection system improperly
adjusted.
Adjust fuel system. Refer to the
manufacturer’s approved Instructions For Continued Airworthiness.
Mixture levers set for improper
mixture.
Review mixture control. See POH.
Fouled Spark Plugs.
Remove, clean and adjust gaps.
(Refer to 74-20)
Hydraulic tappets fouled.
Replace fouled tappets. Inspect
and clean oil filter at more frequent intervals.
Burned or warped exhaust valves Inspect, repair or replace cylinder.
worn seat, scored valve guides.
Replace any burned, warped or
worn exhaust valves.
Engine runs too lean at cruising
power.
Manifold valve vent obstruction.
Repair or replace manifold valve.
Fuel flow reading too low.
Check fuel strainer for clogging.
Clean screen.
Fuel injection malfunction.
components. Refer to the manufacturer’s approved Instructions
For Continued Airworthiness.
Cracked induction tube.
Inspect, repair, or replace induction tube.
Improper manual leaning procedure.
Review leaning procedure. See
POH.
Fuel injection system maladjusted. Adjust fuel system. Refer to the
Engine runs too rich at cruising
power.
Restrictions in air intake passages.
Check passages and remove
restrictions.
Improper manual leaning of Fuel/ Review leaning procedure. See
Air mixture.
POH.
Cracked induction tube.
Inspect, repair, or replace induction tube.
Engine runs too lean or too rich at Fuel injection system maladjusted. See “Engine Fuel System Troublethrottle setting other than cruise.
shooting”. (Refer to 73-00)
Continuous fouling of spark plugs. Piston rings excessively worn or
broken.
EFFECTIVITY:
All
Replace rings. Replace cylinder if
damaged.
Piston rings are not seated.
Hone cylinder walls and replace
rings.
Running the engine too rich.
Review engine operation. See
POH.
71-00
Page 3
15 Jun 2010
CIRRUS
TROUBLE
Engine runs rough at high RPM.
PROBABLE CAUSE
MODEL SR20
REMEDY
Loose mounting bolts or damaged Torque mounting bolts. Replace
mount pads.
mount pads. (Refer to 71-20)
Plugged fuel nozzle jet.
Inspect and clean as necessary.
Refer to the manufacturer’s
approved Instructions For Continued Airworthiness.
Propeller out of balance.
Perform Adjustment/Test Dynamic Balance. (Refer to 6110)
Ignition system malfunction.
See Ignition “Troubleshooting”.
(Refer to 74-00)
Continuous missing at high RPM. Broken valve spring.
Replace as necessary. Refer to
Plugged fuel nozzle jet.
Inspect and clean as necessary.
Burned or warped valve.
Repair or replace cylinder. Refer
to the manufacturer’s approved
Hydraulic tappet dirty or worn.
Remove and replace. Refer to the
Sluggish operation and low power. Restriction in air intake passages. Inspect and clear obstruction.
Fuel injection system maladjusted. Inspect and replace necessary
components. Refer to the manufacturer’s approved Instructions
Valve seats worn and leaking. Pis- Borescope cylinders and check
ton rings worn or stuck in grooves. compression. Refer to the manufacturer’s approved Instructions
Throttle not full open.
71-00
Page 4
15 Jun 2010
EFFECTIVITY:
All
Check and adjust linkage.
(Refer to 76-10)
CIRRUS
TROUBLE
High cylinder head temperature.
PROBABLE CAUSE
MODEL SR20
REMEDY
Low octane fuel.
Drain tanks and replace with correct fuel grade. (Refer to 12-10)
Cylinder baffle seals leaking or
mis-positioned.
Inspect and repair cylinder baffles.
Debris between cylinder fins.
Thoroughly inspect and clean cylinder fins.
Excessive carbon deposits in cyl- Inspect ignition and fuel injections
inder head and on pistons.
system. Refer to the manufacturer’s approved Instructions For
Continued Airworthiness.
Magnetos out of time.
Re-time ignition system internally
and externally. Refer to the manufacturer’s approved Instructions
Magneto distributor block contami- Replace magneto.
nation.
(Refer to 74-10)
Oil leaks.
Exhaust system gas leakage.
Inspect and repair.
(Refer to 78-20)
Exhaust valve leaking.
Inspect and repair cylinder. Refer
to the manufacturer’s approved
Lean fuel/air mixture.
Review leaning procedure. See
POH.
At front of engine, damaged
crankshaft oil seal.
Replace crankshaft oil seal.
Around plugs, fittings, and gaskets Torque or replace.
due to looseness or damage.
Low compression.
EFFECTIVITY:
All
Piston rings excessively worn.
Inspect, repair or replace cylinder.
Replace piston rings. Refer to the
Valve faces and seats worn.
Inspect, repair or replace cylinder.
Excessively worn cylinder walls.
Replace cylinder and piston rings.
71-00
Page 5
15 Jun 2010
CIRRUS
TROUBLE
Poor idle cut-off.
PROBABLE CAUSE
MODEL SR20
REMEDY
Worn or improperly rigged mixture control.
Inspect cable. Replace worn linkage (if necessary). Rig properly.
(Refer to 76-10)
Engine driven fuel pump improperly adjusted.
Adjust fuel pump. Refer to the
Fuel manifold valve not seated
tightly.
Replace manifold valve. Refer to
Climbing to altitude, fuel flow fluc- Fuel vaporization.
tuates.
Operate fuel boost pump. See
POH.
Low fuel pressure.
Incorrect fuel pump adjustment.
Check and adjust fuel pump.
Malfunctioning fuel pump relief
valve.
Replace fuel pump.
Obstruction in fuel line.
Clear obstruction or replace fuel
line.
High fuel pressure.
Malfunctioning relief valve opera- Replace fuel pump.
tion in fuel pump.
Restricted recirculation passage in Replace fuel pump.
fuel pump.
Incorrect fuel pump adjustment.
71-00
Page 6
15 Jun 2010
EFFECTIVITY:
All
Check and adjust fuel pump.
CIRRUS
TROUBLE
PROBABLE CAUSE
MODEL SR20
REMEDY
Fluctuating fuel pressure.
Vapor in fuel system, excessive
fuel temperature.
Normally, operating the auxiliary
pump will clear system. Operate
boost pump. See POH.
Engine has poor acceleration.
Idle mixture too lean.
Check RPM rise and idle cutoff.
Adjust idle mixture. Refer to the
Worn control linkage.
Replace worn elements of linkage.
(Refer to 76-10)
Restricted air cleaner.
Service air filter. (Refer to 71-60)
Malfunctioning ignition system.
Check ignition cables and connections. Replace malfunctioning
spark plugs. (Refer to 74-00)
Improper Fuel/Air mixture.
Check fuel manifold connections
for leaks. Torque loose connections. Check fuel control/metering
unit and linkage for setting and
adjustment. Refer to the engine
manufacturer's approved service
instructions. Check fuel filters and
screens for debris. Check for
proper fuel pump pressure.
Restricted fuel nozzle jet.
Clean. Replace nozzle if obstruction cannot be cleared by solvent
action.
Ignition system and spark plugs
malfunctioning.
Clean, regap and test spark plugs.
Inspect, test and repair ignition
system. Replace components as
required. (Refer to 74-00)
Engine runs rough at above idle
RPM.
Engine lacks power, reduction in
maximum manifold pressure.
EFFECTIVITY:
All
Incorrectly adjusted throttle control Check movement of linkage by
linkage.
moving control from idle to full
throttle. Replace worn components. (Refer to 76-10)
Dirty air filter.
Service air filter in accordance
with the manufacturer’s approved
Instructions For Continued Airworthiness. (Refer to 71-60)
Fuel manifold valve sticking or
obstructed.
Replace manifold valve.
71-00
Page 7
15 Jun 2010
CIRRUS
TROUBLE
Low oil pressure indication on
engine gage.
MODEL SR20
PROBABLE CAUSE
REMEDY
Low oil supply. Oil viscosity too
low.
Replenish. Drain and refill with
correct viscosity. Adjust oil pressure in accordance with the manufacturer’s approved Instructions
Malfunctioning oil pump.
Repair or replace oil pump.
Weak or broken oil pressure relief Replace spring.
valve spring.
High oil temperature indication.
Engine starts but dies or will not
idle.
Prolonged ground operation.
Limit ground operation to a minimum.
Malfunctioning gage or bulb unit.
Inspect wiring, bulb unit, and
gage.
Climb angle too high.
Reduce climb angle.
Obstruction on oil cooler.
Inspect for obstruction and
remove.
Insufficient baffle sealing in area
of oil cooler.
Inspect, repair, or replace engine
baffling.
Low oil supply.
Replenish.
Idle fuel adjustment screw incorrectly adjusted.
Adjust screw. Refer to the manufacturer’s approved Instructions
Spark plugs fouled.
Remove, clean, and re-gap.
(Refer to 74-20)
Water in fuel system.
Sample fuel. See POH. If water
present drain and flush fuel system. (Refer to 12-10)
Defective ignition system.
Fuel system defective or contami- Inspect, drain and flush fuel sysnated.
tem. (Refer to 12-10)
71-00
Page 8
15 Jun 2010
Fuel vaporization.
Operate boost pump. See POH.
Air leak in intake manifold.
Tighten loose connection or
replace malfunctioning part.
EFFECTIVITY:
All
CIRRUS
MODEL SR20
6
3
2
5
4
1
7
8
9
10
11
12
13
14
15
LEGEND
1. Alternator Sheave
2. Throttle Body
3. Throttle Control Cable
4. Vacuum Pump
5. Battery
6. Master Control Unit
7. Governor
8. Exhaust Gas Temperature Probe
9. Valve Cover
10. Lower Spark Plug
11. Oil Pressure Sensor
12. Cylinder Head Temperature Sensor
13. Governor Control Cable
14. Crankcase Oil Drain
15. Exhaust Collector
16. External Power Receptacle
17. Tailpipe
16
17
Serials 1005 thru 1267.
SR20_MM71_1096
Figure 71-001
Engine Components - Serials 1005 thru 1267 (Sheet 1 of 4)
EFFECTIVITY:
Serials 1005 thru 1267
71-00
Page 9
15 Jun 2010
CIRRUS
18
23
20
19
24
MODEL SR20
21
22
26
25
23
AFT VIEW
LEGEND
18. Oil Separator
19. Left Magneto
20. Tachometer Sensor Assembly
21. Right Magneto
22. Starter
23. Engine Mount Isolator
24. Engine Mount Weldment
25. Oil Filter
26. Auxiliary Alternator (if installed)
Figure 71-001
71-00
Page 10
15 Jun 2010
EFFECTIVITY:
SR20_MM71_1097
CIRRUS
28
27
MODEL SR20
30
29
34
31
33
32
FRONT VIEW
LEGEND
27. Engine Baffle
28. Alternator
29. Oil Separator Line
30. Propeller Mount
31. Heater Muffler
32. Oil Separator Vent Line
33. Muffler
34. Backup Vacuum Pump
SR20_MM71_1098
Figure 71-001
EFFECTIVITY:
71-00
Page 11
15 Jun 2010
CIRRUS
35
MODEL SR20
36
37
38
39
40
41
42
50
43
LEGEND
35. Vacuum Manifold
36. Induction Duct Assembly
37. Alternate Air Duct
38. Oil Cooler
39. Oil Filler Port
40. Dipstick
41. Wiring Harness
42. Intake Manifold
43. Plenum Chamber
44
45
47
46
48
44. Fuel Boost Pump
45. Induction Air Filter
46. Manifold Air Pressure Sensor
47. Fuel Line
48. Upper Spark Plug
49. Fuel Pump
50. Fuel Manifold Valve
Figure 71-001
71-00
Page 12
15 Jun 2010
49
EFFECTIVITY:
SR20_MM71_1099
CIRRUS
3
2
MODEL SR20
5
4
1
6
7
8
9
10
11
12
13
14
LEGEND
2. Throttle Body
4. Alternator
5. Battery
6. Governor
8. Valve Cover
9. Lower Spark Plug
17. Tailpipe
15
16
Serials 1268 thru 2015, 2016 & subs w/o Perspective Avionics
17
SR20_MM71_1582A
Figure 71-002
Engine Components - Serials 1268 thru 2015, 2016 & subs w/o Perspective Avionics (Sheet 1 of 4)
EFFECTIVITY:
Serials 1268 thru 2015, 2016 & subs w/o Perspective
Avionics
71-00
Page 13
15 Jun 2010
CIRRUS
18
23
20
19
24
MODEL SR20
21
22
23
25
AFT VIEW
LEGEND
18. Oil Separator
19. Left Magneto
21. Right Magneto
22. Starter
25. Oil Filter
SR20_MM71_1583A
Figure 71-002
71-00
Page 14
15 Jun 2010
EFFECTIVITY:
Avionics
CIRRUS
26
30
27
MODEL SR20
29
28
31
32
FRONT VIEW
LEGEND
26. Engine Baffle
27. Alternator
29. Propeller Mount
30. Heater Muffler
32. Muffler
SR20_MM71_1584A
Figure 71-002
EFFECTIVITY:
Avionics
71-00
Page 15
15 Jun 2010
CIRRUS
34
33
35
MODEL SR20
36
37
38
39
47
40
LEGEND
35. Oil Cooler
36. Oil Filler Port
37. Dipstick
38. Wiring Harness
39. Intake Manifold
40. Plenum Chamber
41
42
44
43
45
46
41. Fuel Boost Pump
44. Fuel Line
46. Fuel Pump
SR20_MM71_1585A
Figure 71-002
71-00
Page 16
15 Jun 2010
EFFECTIVITY:
Avionics
CIRRUS
MODEL SR20
5
3
2
1
6
7
8
9
10
11
12
13
14
4
LEGEND
2. Throttle Body
4. Alternator
5. Battery
6. Governor
8. Valve Cover
9. Lower Spark Plug
17. Tailpipe
15
Serials 2016 & subs w/ Perspective Avionics
16
17
SR20_MM71_3035
Figure 71-003
Engine Components - Serials 2016 & subs w/ Perspective Avionics (Sheet 1 of 4)
EFFECTIVITY:
71-00
Page 17
15 Jun 2010
CIRRUS
18
19
MODEL SR20
26
21
22
20
23
25
24
23
AFT VIEW
LEGEND
18. Oil Separator
19. Left Magneto
21. Right Magneto
22. Starter
25. Oil Filter
26. Compressor
NOTE
Serials w/ Air Conditioning.
SR20_MM71_3036A
Figure 71-003
71-00
Page 18
19 Sep 2010
EFFECTIVITY:
CIRRUS
27
28
30
29
31
MODEL SR20
32
33
FRONT VIEW
LEGEND
27. Engine Baffle
28. Alternator
30. Propeller Mount
31. Heater Muffler
33. Muffler
SR20_MM71_3037A
Figure 71-003
EFFECTIVITY:
71-00
Page 19
19 Sep 2010
CIRRUS
35
34
36
MODEL SR20
37
38
39
40
48
41
LEGEND
36. Oil Cooler
37. Oil Filler Port
38. Dipstick
39. Wiring Harness
40. Intake Manifold
41. Plenum Chamber
42
43
45
44
46
47
42. Fuel Boost Pump
45. Fuel Line
47. Fuel Pump
SR20_MM71_3038A
Figure 71-003
71-00
Page 20
19 Sep 2010
EFFECTIVITY:
CIRRUS
MODEL SR20
4. MAINTENANCE PRACTICES
A. Engine
(1)
Removal - Engine
CAUTION:
Place a tail stand of suitable capacity under tail of airplane before removing
engine.
Note:
Label each component when disconnected to facilitate reinstallation. Protect
openings exposed as a result of removing or disconnecting components against
entry of foreign material by installing covers or sealing with tape.
(a)
(b)
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)
(k)
(l)
Place all electrical switches in the cockpit in the OFF position.
Serials 2065 & subs w/ Air Conditioning: Pull COMPRESSOR/CONTROL PANEL circuit
breaker.
Set fuel selector valve to the OFF position.
Remove engine cowling. (Refer to 71-10)
Remove battery. (Refer to 24-30)
Drain gascolator and fuel lines. (Refer to 12-10)
Drain engine oil sump. (Refer to 12-10)
Remove spinner and propeller. (Refer to 61-10)
Disconnect magneto primary lead wires at magnetos. (Refer to 74-10)
Disconnect electrical cable at starter. (Refer to 80-10)
Disconnect exhaust gas temperature probe. (Refer to 77-20)
Remove exhaust system. (Refer to 78-10)
CAUTION:
(m)
(n)
(o)
(p)
(q)
(r)
(s)
(t)
(u)
(v)
(w)
EFFECTIVITY:
All
When removing throttle and governor control cables, note EXACT size,
position, and number of attaching washer or spacers for reference on reinstallation. Use care to avoid bending cable controls too sharply.
Disconnect throttle and mixture control cables at engine. Remove clamps securing cables
to engine and pull cables aft, clear of engine. (Refer to 76-10)
Disconnect governor control cable at governor. (Refer to 61-20)
Disconnect alternate air control cable at induction duct assembly. (Refer to 71-60)
Serials 2065 & subs w/ Air Conditioning: Disconnect compressor. (Refer to 21-50)
1
Discharge air conditioning system. (Refer to 12-10)
2
Disconnect resistor wire from wire harness.
3
Disconnect compressor hoses from firewall.
4
Cap fittings and hoses.
Disconnect all environmental air flexible hoses and ducts and remove from airplane.
(Refer to 21-00)
Disconnect tachometer sensor lead at connector. (Refer to 77-10)
Disconnect manifold air pressure sensor lead at connector. (Refer to 77-10)
Disconnect oil pressure sensor lead at connector. (Refer to 79-30)
Disconnect electrical wires at alternator(s). (Refer to 24-30)
Disconnect all clamps and ties attaching wires or cables to engine and pull wires and
cables aft, clear of engine.
Serials 1005 thru 1267: Disconnect vacuum lines at vacuum pumps. (Refer to 37-10)
71-00
Page 21
19 Sep 2010
CIRRUS
WARNING:
(x)
(y)
(z)
(aa)
MODEL SR20
Residual oil and fuel draining from engine hoses and lines constitutes
a fire hazard. Caution must be used to prevent the inadvertent pooling
of such materials when lines or hoses are disconnected.
Disconnect oil breather vent line at the oil separator.
Disconnect fuel pump supply line at pump and cap line.
Disconnect fuel return line at aft baffle and cap line.
Disconnect fuel system vent line at tee located beneath engine.
CAUTION:
Prior to removing engine attach bolts, ensure all hoses, wires, lines, cables,
cable ties, and clamps are disconnected or removed from positions which
would interfere with engine removal.
(ab) Attach hoist at forward and aft lifting rings.
(ac) Loosen bolts securing engine to engine mounts.
(ad) Lift engine with hoist just enough to relieve weight from engine mounts.
CAUTION:
(2)
Note location and position of engine mount isolators prior to engine removal
for reference on reinstallation.
(ae) Remove grounding straps, nuts, washers, and bolts securing engine to engine mount.
(af) Slowly hoist engine away from airplane, guiding the detached parts out as the engine is
removed.
(ag) Preserve engine in accordance with the manufacturer’s approved Instructions For Continued Airworthiness.
Installation - Engine
Note:
Remove all protective caps and identification tags as each component is installed.
Prior to installing engine, install all components that were removed from engine
after engine was removed from airplane.
(a)
(b)
(c)
(d)
(e)
(f)
(g)
(h)
(i)
(j)
(k)
(l)
(m)
(n)
(o)
(p)
71-00
Page 22
19 Sep 2010
De-preserve engine in accordance with the manufacturer’s approved Instructions For
Continued Airworthiness.
Insert all upper isolators onto engine mount points and slowly lower engine onto engine
mount weldment so isolators are loosely held in place.
Assemble engine mount isolators. (Refer to 71-20)
Install engine mount bolts, washers, and nuts. Torque nuts to 450 - 500 in-lb (51 - 56 Nm).
(Refer to 71-20)
Remove hoist and tail stand.
Serials 1005 thru 1267: Connect vacuum lines to vacuum pumps. (Refer to 37-10)
Connect oil breather vent line at the oil separator.
Connect fuel pump supply line at pump.
Connect fuel return line at aft baffle.
Connect fuel vent line at tee located beneath engine.
Connect alternator leads and wiring at alternator(s). (Refer to 24-30)
Connect oil pressure sensor lead. (Refer to 79-30)
Connect manifold pressure sensor lead. (Refer to 77-10)
Connect tachometer sensor lead. (Refer to 77-10)
Attach and connect all environmental air flexible hoses and ducts. (Refer to 21-00)
Serials 2065 & subs w/ Air Conditioning: Connect compressor. (Refer to 21-50)
EFFECTIVITY:
All
CIRRUS
MODEL SR20
1
2
3
(q)
(r)
(s)
(t)
(u)
(v)
(w)
(x)
(y)
(z)
(aa)
(ab)
(ac)
(ad)
(ae)
(af)
(ag)
(ah)
EFFECTIVITY:
All
Connect resistor wire to wire harness.
Remove caps from fittings and hoses.
Connect 5/8 inch (19 mm) compressor hose to firewall. Torque hose and fittings to
250 to 350 in-lb (28.2 - 39.5 Nm).
4
Connect 1/2 inch (16 mm) compressor hose to firewall. Torque hose and fittings to
180 to 240 in-lb (20.3 - 27.1 Nm).
Connect alternate air control cable at induction duct assembly. (Refer to 71-60)
Connect governor control cable. (Refer to 61-20)
Connect throttle and mixture control cables. Adjust power control cables. (Refer to 76-10)
Install exhaust system. (Refer to 78-10)
Connect exhaust gas temperature probe. (Refer to 77-20)
Connect starter electrical cable. (Refer to 80-10)
Connect magneto primary lead wires. (Refer to 74-10)
Install propeller and spinner. (Refer to 61-10)
Ensure any other lines, hoses, electrical leads, clamps, and ties disconnected during
removal of engine are installed.
Fill engine with proper grade and amount of engine oil. (Refer to 12-10)
Install battery. (Refer to 24-30)
Set fuel selector valve to the ON position, open throttle and mixture to full, turn on electric
full pump, and check fuel lines for leaks.
Perform Airplane Operational and Functional Check. (Refer to 05-30)
Install engine cowling. (Refer to 71-10)
Serials 2065 & subs w/ Air Conditioning: Perform Inspection/Check - System Plumbing
Refrigerant Leak Test. (Refer to 21-50)
Serials 2065 & subs w/ Air Conditioning: Charge air conditioning system. (Refer to 12-10)
Serials 2065 & subs w/ Air Conditioning: Reset COMPRESSOR/CONTROL PANEL circuit
breaker.
Serials 2065 & subs w/ Air Conditioning: Perform Operational Test - Air Conditioning System. (Refer to 21-50)
71-00
Page 23
19 Sep 2010
CIRRUS
MODEL SR20
B. Engine Baffling (See Figure 71-004)
CAUTION:
Proper baffling installation and care is critical to engine cooling. If baffles or seals are
broken or misshaped, the amount of air flowing past a particular cylinder or component
will increase. The increased airflow in one area causes a reduction of airflow past other
components and leads to higher temperatures in some parts of the engine. Ensure baffles are installed correctly and seals fit and direct airflow in the proper direction.
Various lines, hoses, wires, and controls are routed through some baffles. Ensure that
these components are reinstalled correctly after baffle installation.
(1)
(2)
Removal - Engine Baffling
(a) Remove engine cowling. (Refer to 71-10)
(b) Serials 1005 thru 1147: Remove screws and washers connecting wires to landing light
assembly. (Refer to 33-40)
(c)
Disconnect any lines, hoses, wires, and controls routed through baffling.
(d) Remove tension springs.
(e) Remove bolts, screws, washers, and nuts securing baffling to engine.
(f)
Remove baffling from airplane.
Installation - Engine Baffling
(a)
Acquire necessary tools, equipment, and supplies.
Description
High Temperature Silicone
Sealant
(b)
(c)
(d)
(e)
(f)
71-00
Page 24
15 Jun 2010
P/N or Spec.
RTV 736
Supplier
Dow Corning
Purpose
Sealant.
Position baffling to engine and secure with bolts, screws, washers, and nuts.
Install tension springs.
Connect any lines, hoses, wires, and controls routed through baffling.
Serials 1005 thru 1147: Install screws and washers connecting wires to landing light
assembly. (Refer to 33-40)
Install engine cowling. (Refer to 71-10)
EFFECTIVITY:
All
CIRRUS
MODEL SR20
1
1
7
3 2
Serial 1005 thru 1422.
1
1
6
3
2
4
3
5
2
3
3 4
5
3
4
3
NOTE
6
3
2
Fasten using engine hardware plus washer.
LANDING LIGHT
(REF)
Serials 1005 thru 1422:
Fasten using bolts in place of screws.
4
LEGEND
1. Baffle Assembly
2. Bolt
3. Washer
4. Nut
5. Screw
6. Tension Spring
7. Grommet
SR20_MM71_1879A
Figure 71-004
Engine Baffling Installation
EFFECTIVITY:
All
71-00
Page 25
15 Jun 2010
CIRRUS
Intentionally Left Blank
71-00
Page 26
15 Jun 2010
EFFECTIVITY:
All
MODEL SR20

71-00 Power Plant - Cirrus Design Authorized Service Center Home

Transcription

Similar documents

Untitled - Aeronautics

G8.3 And GTA8.3. - Cummins Engines

Kewatec_EASY

engines - Yamaha

automotive features in a compact package.

The Holset VG Turbocharger

Photo : VL1500BT

FD620D

Carburettor Check Sheet GX25

Bayliner 4050 Bodega