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Q. Torque collar screws (item 4) to 160.0 ±5.0 in-lb (18.1 ±0.6 Nm).
R. Rotate FLAPS switch to UP position.
S. Set MASTER SWITCH to OFF position.
T. Install access panels CF4C and CF5. (Refer to AMM 06-00)
U. Install carpet. (Refer to AMM 25-10)
V. Install passenger seats. (Refer to AMM 25-10)
W. Complete airplane records by noting compliance with SB 2X-27-16 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 X S E R I E S
SB 2X-27-16
Cirrus Design SR20 Serials 1005 thru 2029. Page 4
Cirrus Design SR22 Serials 0002 thru 3459.
EFFECTIVITY:
October 02, 2009
Figure 01
Flap Actuator Modification (Page 1 of 2)
0%
50%
100%
6
SR2_SB27_1281
LEGEND
1. End Fitting
2. Rod End
3. Shaft Collar
4. Screw
5. Castellated Nut
6. Cotter Pin
7. Existing Washer
8. Existing Bolt
9. Existing Jam Nut
NOTE
Bottom out end fitting on actuator to ensure maximum thread engagement.
Bottom out rod end in end fitting. During adjustment, rod end may need to
be backed out a maximum of 2 turns.
1
9
9
7
7
7
7
2
8
5
3
3
4
TORQUE TUBE
COUPLER (REF)
PROXIMITY SENSOR
(REF)
4
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 X S E R I E S
SB 2X-27-16
Cirrus Design SR20 Serials 1005 thru 2029. Page 5
Cirrus Design SR22 Serials 0002 thru 3459.
EFFECTIVITY:
October 02, 2009
Figure 01
Flap Actuator Modification (Page 2 of 2)
0.05 inch
(1.27 mm)
MINIMUM
SR2_SB27_1282
NOTE
With flaps in 100% position, install shaft collar on actuator shaft with
0.05 ±0.01 inch (1.27 ±0.25 mm) gap between face of collar and actuator seal.
With flaps in UP position, ensure a minimum gap of 0.05 inch (1.27 mm) exists
between end fitting and torque tube coupler.
TORQUE TUBE
COUPLER
(REF)
0.05 ±0.01 inch
(1.27 ±0.25 mm)
END FITTING
(REF)
ACTUATOR SEAL
(REF)
SHAFT COLLAR
(REF)
C I R R U S SR2X
Service Bulletin
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publications.
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