Installation Instructions for Cirrus SR20 and SR22 Series Aircraft Sunvisor System

Installation Instructions for Cirrus SR20 and SR22 Series Aircraft Sunvisor System
Installation Instructions for Cirrus SR20 and SR22 Series Aircraft
Sunvisor System
Doc: 9051-0174-001
Rev
Date
Approved
B
10-03-08
GH
Installing your Rosen Sunvisor System is easily performed and should take approximately 1 hour.
Please read these short instructions COMPLETELY before starting.
Installation Hardware (included)
Qty:
(1) 5/32 Allen Key
for #10-32 Cap Screw
(1) 9/64 Allen Key
1. Remove the original sunvisors from the mounting arms by
removing the two screw fasteners and nuts from each of
the lenses. (see image 1)
Image 1
2. Remove the small hex head fastening screw from the
forward side of the lower interior trim on the window frame.
(see image 2)
3. Pull back the door seal from the leading and top edge of the
door frame to expose and release the door frame trim piece.
Image 2
(see image 3)
4. Carefully manipulate the visor mounting arm and trim piece
to remove the trim piece from the aircraft. Note that the trim
piece is restrained by a Velcro strip behind the forward
Image 3
86365 College View Road
Eugene, Oregon USA 97405
www.rosenvisor.com
541.747.0034
Page 1 of 2
edge of the door frame. Be careful not to bend and crease the trim piece.
5. Use a Phillips #2 screwdriver to remove the original visor mounting block from the aircraft. Retain the
screws.
6. Remove screw and lock washer (c) to remove visor arm from mount post. Retain the fasteners.
7. Orientate the Rosen Visor mount so it lays
flat against the same surfaces as the
original mount and attach with the original
screws (a). (The receiver threads are
shake-proof.)
8. Re-install the trim piece over the mounting
post aligning all the edges with the door
frame and features.
(a)
(b)
(c)
9. Re-attach to Velcro, being careful to align
the forward trim mounting screw hole. Reinstall screw. The nut-plate attachment point
can float slightly.
10. Re-attach the door seal material by pressing
it over the trim and door frame.
11. Attach the visor (b) and install #8 cap screw
and lock washer provided (c). When
properly installed in the forward position the
red tensioning knob should be towards the
front of the aircraft nearest the wind screen.
PILOT SIDE SHOWN
12. All the pivot axis motions are adjustable and should be adjusted to the pilot’s preference before flight.
The pivot tensions should be set so the visor can be positioned smoothly and easily. Excessive
tightening can limit the ease of operation.
13. Repeat this procedure for the opposite side of the aircraft.
Continued Airworthiness Instructions:
•
•
(On the ground only)
o
Periodically clean the lenses with a soft cloth and Rosen Plastic Cleaner, Polisher &
Protectant, or mild soap and water. Do not use abrasives on the lens.
o
Periodically adjust the pivot tensions on the visor assemblies.
Updates to this continued airworthiness section are available on the Rosen Website.
(www.rosenvisor.com)
The most up to date version of this document is available on the Rosen Website. (www.rosenvisor.com)
Airworthiness Limitations:
The Airworthiness Limitations Section is FAA approved and specifies maintenance requires under
§§43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FAA
approved.
There are no airworthiness limitations associated with this installation.
86365 College View Road
Eugene, Oregon USA 97405
www.rosenvisor.com
541.747.0034
Page 2 of 2
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