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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 R 2 2
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 mHeight (Maximum) ................................................................................. 8.80 ft ..................... 2.70 mWing Span (Overall) ............................................................................ 38.25 ft ................... 11.65 mPropeller Diameter (Maximum) ............................................................. 6.50 ft ..................... 1.98 m
B. Cabin
Cabin Width......................................................................................... 49.00 in. ............... 124.00 cmCabin Height........................................................................................ 50.00 in. ............... 127.00 cmCabin Length ..................................................................................... 122.00 in. ............... 309.00 cmCabin Volume .................................................................................... 137.00 ft³.................... 3.83 m³Baggage Compartment Height............................................................ 39.00 in. ................. 99.00 cmBaggage Compartment Width............................................................. 40.00 in. ............... 101.00 cmBaggage Compartment Length ........................................................... 36.00 in. ................. 91.00 cmBaggage Compartment Volume .......................................................... 32.00 ft³.................... 0.90 m³
C. Wings
Span .................................................................................................... 38.25 ft ................... 11.65 mArea................................................................................................... 144.90 ft².................. 13.46 m²Wing Loading ...................................................................................... 23.46 lb/ft² ............ 114.45 kg/m²Aspect Ratio ........................................................................................ 10.00 ...................... 10.00Wing 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 mArea..................................................................................................... 10.80 ft².................... 1.00 m²
E. Ailerons
Span ...................................................................................................... 4.70 ft ..................... 1.43 mArea....................................................................................................... 4.37 ft².................... 0.41 m²
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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 R 2 2
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EFFECTIVITY:
F. Horizontal Stabilizer
Span .................................................................................................... 13.17 ft ..................... 4.01 mArea..................................................................................................... 25.75 ft².................... 2.39 m²Aspect Ratio .......................................................................................... 5.59 ........................ 5.59
G. Elevator
Span .................................................................................................... 12.00 ft ..................... 3.66 mArea....................................................................................................... 7.73 ft².................... 0.72 m²
H. Vertical Stabilizer
Span ...................................................................................................... 5.52 ft ..................... 1.65 mArea..................................................................................................... 15.93 ft².................... 1.48 m²
Aspect Ratio .......................................................................................... 1.84 ........................ 1.84
I. Rudder
Span ...................................................................................................... 5.42 ft ..................... 1.65 mArea....................................................................................................... 5.26 ft².................... 0.49 m²
J. Landing Gear
Wheel Track (Main To Main) - Serials 0002 thru 2437 ........................ 10.83 ft ..................... 3.30 mWheel Track (Main To Main) - Serials 2438 & subs............................... 9.10 ft ..................... 2.77 mWheel 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)
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 R 2 2
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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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 R 2 2
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EFFECTIVITY:
Figure 06-001Airplane 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 LBLRBL 87.7
LEMACFS 133.1230.0
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)FUSELAGESTATION
FS55.6
FS100.0
FS38.3
FS157.4
FS222.0
FS350.2
WL165.5
BUTTOCK LINE (BL)230.0Serials 0002 thru 2333, 2335 thru 2419, 2421 thru 2437.
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 R 2 2
EFFECTIVITY:
Figure 06-001Airplane 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 LBLRBL 87.7
LEMACFS 133.1230.0
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)FUSELAGESTATION
FS55.6
FS100.0
FS38.3
FS157.4
FS222.0
FS350.2
WL165.5
BUTTOCK LINE (BL)230.0
06-00Serials 2438 & subs
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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 R 2 2
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EFFECTIVITY:
Figure 06-002Fuselage Stations
0.0
50.0
100.
0
150.
0
350.
0
250.
0
200.
0
300.
0F
S 2
91.3
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
50.0WL 57.7 WL 61.9
FS
157
.5
(FS) Fuselage Station
WaterLine(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 atfuselage station 0.0.
50.0
100.
0
150.
0
350.
0
250.
0
200.
0
300.
0F
S 2
91.3
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
50.0WL 56.5 WL 61.9
SR22_MM06_1323A
FS
157
.5
(FS) Fuselage Station
WaterLine(WL)
WL 94.0
WL 159.5
WL 165.5
WL 105.8
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 R 2 2
06-00Serials 0002 thru 2437
Page 715 Apr 2007EFFECTIVITY:
Figure 06-003Wing 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
REARSHEAR 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
REARSHEAR WEB
WS 220.0
WS 220.0
WS 240.0
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 R 2 2
EFFECTIVITY:
Figure 06-003Wing 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
REARSHEAR 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
REARSHEAR WEB
WS 220.0
WS 220.0
WS 240.0
06-00 Serials 2438 & subs
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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 R 2 2
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Figure 06-004Elevator Stations
ELEVATOR HINGES
ELEVATOR HINGES
MAINSPAR
BL 72.0
BL 36.0
BL 72.0
BL 36.0
SR22_MM06_1968
NOTEBottom view - lower skinremoved 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
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 R 2 2
EFFECTIVITY:
Figure 06-005Floor 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.
CF1LCF1R 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-BoltEngine Mount Through-BoltPilot SeatCo-Pilot SeatPassenger SeatRudder-Aileron InterconnectPitot-Static Water TrapFlight Control CablesTrim System RelaysFlight Control CablesMarker Beacon AntennaELTCAPSTransponder Antenna
--------------
SR22_MM06_1832
06-00 Serials 0002 thru 1601, 1603 thru 1820, 1822 thru 1839, 1841 thru 1862
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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 R 2 2
06-00Serials 1602, 1821, 1840, 1863 & subs
Page 1115 Apr 2007EFFECTIVITY:
Figure 06-005Floor Access Panels - Serials 1602, 1821, 1840, 1863 & subs (Sheet 2 of 2)
CS1RCS1L
CF1LCF1R CF2L CF2R CF3L CF3C CF3R CF4L CF4C CF4R CF5 CB6 CB7 CF8CS1LCS1R
CF1R
CF2R
CF3CCF3R
CF4CCF4R
CF5
CB6
CF1L
CF2L
CF3L
CF4L
CB7
CF8
LEGENDEngine Mount Through-BoltEngine Mount Through-BoltPilot SeatCo-Pilot SeatPassenger SeatRudder-Aileron InterconnectPitot-Static Water TrapFlight Control CablesTrim System RelaysFlight Control CablesMarker Beacon AntennaELTCAPSTransponder AntennaSpar TunnelSpar Tunnel
----------------
SR22_MM06_2277
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 R 2 2
EFFECTIVITY:
Figure 06-006Wing 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
LEGENDLW1/RW1 - Wing Root, AftLW2/RW2 - Wing Root, FwdLW3/RW3 - Fuel Tank, RootLW4/RW4 - Wing InboardLW5/RW5 - WS 37LW6/RW6 - Wing Mid, FwdLW7/RW7 - Wing Mid, Aft LW8/RW8 - WS 68LW9/RW9 - WS 89LW10/RW10 - Fuel Tank, MidLW11/RW11 - Fuel Tank, OutboardLW12/RW12 - WS 121LW13/RW13 - Wing Outboard, AftLW14/RW14 - NACA VentLW15 - Aileron CoveLW16/RW16 - Wing Outboard, Fwd
LW3
RW8
LW4
RW11
RW12
RW13
RW3
LW7LW8
LW9
LW12
RW7RW5
RW4
LW14
RW9
RW1
RW16
LW16
Serials 0002 thru 2333, 2335 thru 2419, 2421 thru 2437.
06-00 Serials 0002 thru 2437
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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 R 2 2
06-00Serials 2438 & subs
Page 1315 Apr 2007EFFECTIVITY:
Figure 06-006Wing Access Panels - Serials 2438 & subs (Sheet 2 of 2)
RW13
LW3
LW2RW6
LW7
LW5LW10
LW9
LW6
RW3
LW1
RW10
RW5LW4
LW8
LW11
LW12
LW13
RW12
RW9
RW1RW8
RW4
RW7
LEGENDLW1/RW1 - Wing RootLW2 - De-icing Fluid TankLW3/RW3 - Fuel Tank, RootLW4/RW4 - Wing InboardLW5/RW5 - NACA Vent, InboardLW6/RW6 - Fuel Tank, InboardLW7/RW7 - Fuel Tank, MidLW8/RW8 - Fuel Tank, Outboard LW9/RW9 - Wing MidLW10/RW10 - NACA Vent, OutboardLW11 - Aileron CoveLW12/RW12 - Wing OutboardLW13/RW13 - Aileron Hinge
SR22_MM06_2455
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 R 2 2
EFFECTIVITY:
Figure 06-007Empennage Access Panels
SR22_MM06_1833A
RE3
LE2
RE1
LE1
RE2
Elevator Push Pull RodPitch Trim CartridgePitch Trim Motor AssemblyRudder Push Pull RodAvionics Bay
-----
LEGENDLE1LE2RE1RE2RE3
NOTE
Serials 0821 & subs.
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