Cirrus SR22 User manual

CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
06-00
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EFFECTIVITY:
DIMENSIONS AND AREAS
1. GENERAL
This section describes those diagrams and text which shows the area, dimensions, stations, access doors,
and physical locations of the structural members of the airplane. Also included is the cardinal rigging
dimensions.
2. AIRPLANE DIMENSIONS AND AREAS
The airplane is divided into reference points in inches. These reference points provide a means of quickly
identifying the locations of components. Three axes are used as reference points.
The following terms are used for the reference points:
FS - Fuselage Station is a horizontal reference designation starting in front of the nose of the airplane
WS - Wing Station is measured outboard from the centerline of the fuselage to the wing tip.
WL - Water Line is a vertical reference designation measured parallel to the ground.
BL - Buttock Line is a horizontal reference designation starting at the airplane centerline. Right or left is
added to indicate direction from airplane centerline.
A. General
Length (Overall)................................................................................... 25.92 ft ..................... 7.90 m
Height (Maximum) ................................................................................. 8.80 ft ..................... 2.70 m
Wing Span (Overall) ............................................................................ 38.25 ft ................... 11.65 m
Propeller Diameter (Maximum) ............................................................. 6.50 ft ..................... 1.98 m
B. Cabin
Cabin Width......................................................................................... 49.00 in. ............... 124.00 cm
Cabin Height........................................................................................ 50.00 in. ............... 127.00 cm
Cabin Length ..................................................................................... 122.00 in. ............... 309.00 cm
Cabin Volume .................................................................................... 137.00 ft³.................... 3.83 m³
Baggage Compartment Height............................................................ 39.00 in. ................. 99.00 cm
Baggage Compartment Width............................................................. 40.00 in. ............... 101.00 cm
Baggage Compartment Length ........................................................... 36.00 in. ................. 91.00 cm
Baggage Compartment Volume .......................................................... 32.00 ft³.................... 0.90 m³
C. Wings
Span .................................................................................................... 38.25 ft ................... 11.65 m
Area................................................................................................... 144.90 ft².................. 13.46 m²
Wing Loading ...................................................................................... 23.46 lb/ft² ............ 114.45 kg/m²
Aspect Ratio ........................................................................................ 10.00 ...................... 10.00
Wing Dihedral - Serials 0002 thru 2437 ................................................ 4.50°....................... 4.50°
Wing Dihedral - Serials 2438 & subs..................................................... 5.50°....................... 5.50°
D. Flaps
Span ...................................................................................................... 8.80 ft ..................... 2.68 m
Area..................................................................................................... 10.80 ft².................... 1.00 m²
E. Ailerons
Span ...................................................................................................... 4.70 ft ..................... 1.43 m
Area....................................................................................................... 4.37 ft².................... 0.41 m²
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EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
15 Apr 2007
F. Horizontal Stabilizer
Span .................................................................................................... 13.17 ft ..................... 4.01 m
Area..................................................................................................... 25.75 ft².................... 2.39 m²
Aspect Ratio .......................................................................................... 5.59 ........................ 5.59
G. Elevator
Span .................................................................................................... 12.00 ft ..................... 3.66 m
Area....................................................................................................... 7.73 ft².................... 0.72 m²
H. Vertical Stabilizer
Span ...................................................................................................... 5.52 ft ..................... 1.65 m
Area..................................................................................................... 15.93 ft².................... 1.48 m²
Aspect Ratio .......................................................................................... 1.84 ........................ 1.84
I. Rudder
Span ...................................................................................................... 5.42 ft ..................... 1.65 m
Area....................................................................................................... 5.26 ft².................... 0.49 m²
J. Landing Gear
Wheel Track (Main To Main) - Serials 0002 thru 2437 ........................ 10.83 ft ..................... 3.30 m
Wheel Track (Main To Main) - Serials 2438 & subs............................... 9.10 ft ..................... 2.77 m
Wheel Base (Main To Nose).................................................................. 7.26 ft ..................... 2.21 m
3. ACCESS PANELS
A. Cabin Floor (See Figure 06-005)
Maintenance practices pertinent to the cabin floor access panels are found in Chapter 53, Fuselage.
(Refer to 53-20)
B. Wing (See Figure 06-006)
Maintenance practices pertinent to the wing access panels are found in Chapter 57, Wings. (Refer to
57-30)
C. Empennage (See Figure 06-007)
Maintenance practices pertinent to the empennage access panels are found in Chapter 53, Fuselage.
(Refer to 53-30)

CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
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EFFECTIVITY:
4. CONTROL SURFACE TRAVELS AND CABLE TENSION SETTINGS
A. Aileron
Aileron Up Travel: 12.5° ±1.0°
Aileron Down Travel: 12.5° ±1.0°
Aileron Trim Deflection: 6.0° ±1.0°
Aileron Cable Tension: 30-40 lb
B. Elevator
Elevator Up Travel: 25.0° +0° / -1.0°
Elevator Down Travel: 15.0° ±1.0°
Elevator Trim Deflection: -10.5° ±1.0°, +17° Minimum
Elevator Cable Tension: 30-40 lb
C. Rudder
Maximum Right Rudder Deflection: 20.0° ±1.0°
Maximum Left Rudder Deflection: 20.0° ±1.0°
D. Flaps
Flap UP: 0.0° ±0.5°
Flap 50%: 16.0° ±0.5°
Flap 100%: 32.0° ±0.5°
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Page 4 Serials 0002 thru 2437
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
15 Apr 2007
Figure 06-001
Airplane Principal Dimension - Serials 0002 thru 2437 (Sheet 1 of 2)
WATER LINE (WL)
BL 0.0
BUTTOCK LINE (BL)
350.0
300.0
250.0 200.0 150.0
0.0
50.0
100.0
WL 100.0
150.0
50.0
SR22_MM06_1322A
200.0
LBL 229.5
RBL 229.5
LBL 77.3
BL 0.0
RBL 77.3
LBL 63.1
RBL 63.1
Typical LBL
RBL 87.7
LEMAC
FS 133.1
230.0
150.0
100.0
50.0
200.0
150.0
100.0
50.0
MAC 47.7"
Reference datum located at
fuselage station 0.0.
NOTE
(FS)
FUSELAGE
STATION
FS
55.6
FS
100.0
FS
38.3
FS
157.4
FS
222.0
FS
350.2
WL
165.5
BUTTOCK LINE (BL)
230.0
Serials 0002 thru 2333, 2335 thru 2419, 2421 thru 2437.

CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
06-00
Page 5
Serials 2438 & subs
EFFECTIVITY:
Figure 06-001
Airplane Principal Dimension - Serials 2438 & subs (Sheet 2 of 2)
WATER LINE (WL)
BL 0.0
BUTTOCK LINE (BL)
350.0
300.0
250.0 200.0 150.0
0.0
50.0
100.0
WL 100.0
150.0
50.0
SR22_MM06_2609
200.0
LBL 229.5
RBL 229.5
LBL 77.3
BL 0.0
RBL 77.3
LBL 54.8
RBL 54.8
Typical LBL
RBL 87.7
LEMAC
FS 133.1
230.0
150.0
100.0
50.0
200.0
150.0
100.0
50.0
MAC 47.7"
Reference datum located at
fuselage station 0.0.
NOTE
(FS)
FUSELAGE
STATION
FS
55.6
FS
100.0
FS
38.3
FS
157.4
FS
222.0
FS
350.2
WL
165.5
BUTTOCK LINE (BL)
230.0
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EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
15 Apr 2007
Figure 06-002
Fuselage Stations
0.0
50.0
100.0
150.0
350.0
250.0 200.0 300.0
FS 291.3
FS 130.3
FS 121.4
FS 100.0
FS 55.6
FS 38.3
FS 200.8 FS 222.0
FS 218.1
FS 249.3
FS 350.2
100.0
150.0
WL 83.9
50.0
WL 57.7 WL 61.9
FS 157.5
(FS) Fuselage
Station
Water
Line
(WL)
WL 94.0
WL 159.5
WL 165.5
WL 105.8
Serials 2334, 2420, 2438 & subs.
Serials 0002 thru 2333, 2335 thru 2419, 2421 thru 2437.
0.0
Reference datum located at
fuselage station 0.0.
50.0
100.0
150.0
350.0
250.0 200.0 300.0
FS 291.3
FS 130.3
FS 121.4
FS 100.0
FS 55.6
FS 38.3
FS 200.8 FS 222.0 FS 218.1
FS 249.3
Note
FS 350.2
100.0
150.0
WL 83.9
50.0
WL 56.5 WL 61.9
SR22_MM06_1323A
FS 157.5
(FS) Fuselage
Station
Water
Line
(WL)
WL 94.0
WL 159.5
WL 165.5
WL 105.8

CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
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Page 7
Serials 0002 thru 2437
EFFECTIVITY:
15 Apr 2007
Figure 06-003
Wing Stations - Serials 0002 thru 2437
Serials 0002 thru 2333, 2335 thru 2419, 2421 thru 2437.
SR22_MM06_1324
WS 141.4
AILERON HINGES
FLAP HINGES
FLAP HINGES
AILERON HINGES
WS 88.6
WS 197.5
WS 88.6
MAINSPAR
WS 141.4
QTR CHORD
WS 197.5
REAR
SHEAR WEB
WS 0.0
WS 20.0
WS 40.0
WS 60.0
WS 80.0
WS 120.0
WS 160.0
WS 140.0
WS 20.0
WS 40.0
WS 60.0
WS 80.0
WS 100.0
WS 120.0
WS 140.0
WS 160.0
WS 240.0
WS 180.0
WS 200.0
WS 180.0
WS 200.0
WS 100.0
REAR
SHEAR WEB
WS 220.0
WS 220.0
WS 240.0

06-00
Page 8 Serials 2438 & subs
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
Figure 06-003
Wing Stations - Serials 2438 & subs
SR22_MM06_2580
WS 140.2
AILERON HINGES
FLAP HINGES
FLAP HINGES
AILERON HINGES
WS 86.6
WS 196.0
WS 86.6
MAINSPAR
WS 140.2
QTR CHORD
WS 196.0
REAR
SHEAR WEB
WS 0.0
WS 20.0
WS 40.0
WS 60.0
WS 80.0
WS 120.0
WS 160.0
WS 140.0
WS 20.0
WS 40.0
WS 60.0
WS 80.0
WS 100.0
WS 120.0
WS 140.0
WS 160.0
WS 240.0
WS 180.0
WS 200.0
WS 180.0
WS 200.0
WS 100.0
REAR
SHEAR WEB
WS 220.0
WS 220.0
WS 240.0
15 Apr 2007

CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
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EFFECTIVITY:
15 Apr 2007
Figure 06-004
Elevator Stations
ELEVATOR HINGES
ELEVATOR HINGES
MAINSPAR
BL 72.0
BL 36.0
BL 72.0
BL 36.0
SR22_MM06_1968
NOTE
Bottom view - lower skin
removed for clarity.
BL 80
BL 60
BL 40
BL 20
BL 20
BL 40
BL 60
BL 80
BL 0.0
REAR SPAR
FORWARD SPAR
MID SPAR

06-00
Page 10 Serials 0002 thru 1601, 1603 thru 1820, 1822 thru
1839, 1841 thru 1862
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
Figure 06-005
Floor Access Panels - Serials 0002 thru 1601, 1603 thru 1820, 1822 thru 1839, 1841 thru 1862
Serials 0002 thru 1601, 1603 thru 1820, 1822 thru 1839, 1841 thru 1862.
CF1L
CF1R
CF2L
CF2R
CF3L
CF3C
CF3R
CF4L
CF4C
CF4R
CF5
CB6
CB7
CF8
CF1R
CF2R
CF3C
CF3R
CF4C
CF4R
CF5
CB6
CF1L
CF2L
CF3L
CF4L
CB7
CF8
LEGEND
Engine Mount Through-Bolt
Engine Mount Through-Bolt
Pilot Seat
Co-Pilot Seat
Passenger Seat
Rudder-Aileron Interconnect
Pitot-Static Water Trap
Flight Control Cables
Trim System Relays
Flight Control Cables
Marker Beacon Antenna
ELT
CAPS
Transponder Antenna
-
-
-
-
-
-
-
-
-
-
-
-
-
-
SR22_MM06_1832
15 Apr 2007

CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
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Page 11
Serials 1602, 1821, 1840, 1863 & subs
EFFECTIVITY:
15 Apr 2007
Figure 06-005
Floor Access Panels - Serials 1602, 1821, 1840, 1863 & subs (Sheet 2 of 2)
CS1R
CS1L
CF1L
CF1R
CF2L
CF2R
CF3L
CF3C
CF3R
CF4L
CF4C
CF4R
CF5
CB6
CB7
CF8
CS1L
CS1R
CF1R
CF2R
CF3C
CF3R
CF4C
CF4R
CF5
CB6
CF1L
CF2L
CF3L
CF4L
CB7
CF8
LEGEND
Engine Mount Through-Bolt
Engine Mount Through-Bolt
Pilot Seat
Co-Pilot Seat
Passenger Seat
Rudder-Aileron Interconnect
Pitot-Static Water Trap
Flight Control Cables
Trim System Relays
Flight Control Cables
Marker Beacon Antenna
ELT
CAPS
Transponder Antenna
Spar Tunnel
Spar Tunnel
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
-
SR22_MM06_2277

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Page 12 Serials 0002 thru 2437
EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
Figure 06-006
Wing Access Panels - Serials 0002 thru 2437 (Sheet 1 of 2)
LW15
RW6
SR22_MM06_1325B
RW10
RW14
LW2
RW2
LW5
LW6
LW1
LW13
LW10
LW11
LEGEND
LW1/RW1 - Wing Root, Aft
LW2/RW2 - Wing Root, Fwd
LW3/RW3 - Fuel Tank, Root
LW4/RW4 - Wing Inboard
LW5/RW5 - WS 37
LW6/RW6 - Wing Mid, Fwd
LW7/RW7 - Wing Mid, Aft
LW8/RW8 - WS 68
LW9/RW9 - WS 89
LW10/RW10 - Fuel Tank, Mid
LW11/RW11 - Fuel Tank, Outboard
LW12/RW12 - WS 121
LW13/RW13 - Wing Outboard, Aft
LW14/RW14 - NACA Vent
LW15 - Aileron Cove
LW16/RW16 - Wing Outboard, Fwd
LW3
RW8
LW4
RW11
RW12
RW13
RW3
LW7
LW8
LW9
LW12
RW7
RW5
RW4
LW14
RW9
RW1
RW16
LW16
Serials 0002 thru 2333, 2335 thru 2419, 2421 thru 2437.
15 Apr 2007

CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
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Page 13
Serials 2438 & subs
EFFECTIVITY:
15 Apr 2007
Figure 06-006
Wing Access Panels - Serials 2438 & subs (Sheet 2 of 2)
RW13
LW3
LW2
RW6
LW7
LW5
LW10
LW9
LW6
RW3
LW1
RW10
RW5
LW4
LW8
LW11
LW12
LW13
RW12
RW9
RW1
RW8
RW4
RW7
LEGEND
LW1/RW1 - Wing Root
LW2 - De-icing Fluid Tank
LW3/RW3 - Fuel Tank, Root
LW4/RW4 - Wing Inboard
LW5/RW5 - NACA Vent, Inboard
LW6/RW6 - Fuel Tank, Inboard
LW7/RW7 - Fuel Tank, Mid
LW8/RW8 - Fuel Tank, Outboard
LW9/RW9 - Wing Mid
LW10/RW10 - NACA Vent, Outboard
LW11 - Aileron Cove
LW12/RW12 - Wing Outboard
LW13/RW13 - Aileron Hinge
SR22_MM06_2455

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EFFECTIVITY:
CIRRUS AIRPLANE MAINTENANCE MANUAL MODEL SR22
Figure 06-007
Empennage Access Panels
SR22_MM06_1833A
RE3
LE2
RE1
LE1
RE2
Elevator Push Pull Rod
Pitch Trim Cartridge
Pitch Trim Motor Assembly
Rudder Push Pull Rod
Avionics Bay
-
-
-
-
-
LEGEND
LE1
LE2
RE1
RE2
RE3
NOTE
Serials 0821 & subs.
15 Apr 2007