Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly

Rosen Kit Number RC300/400-300-1, RCS-300-6 Component Maintenance Manual with Illustrated Parts List and Instructions for Continued Airworthiness Manual Number Rosen 9051-0118-015 Revision D March 31, 2015 Rosen Sunvisor Systems LLC 86365 College View Road Eugene, Oregon 97405 USA Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 3 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS Record of Revisions Rev Description Date Approved D Update to CMM/IPC format. Correct typos 3/31/15 GH Table of Contents Record of Revisions 3 Introduction 4 General 4 Revision Service 4 Fault Isolation 5 Product Description 6 Installation Instructions 6 Removal 7 Weight and Balance 7 Repair 7 Instructions for Continued Airworthiness 8 Airworthiness Limitations__________________ ___________________ _ 8 Illustrations 9-11 Parts List 12 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 4 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS Introduction 1. General a. This Rosen Component Maintenance Manual provides use, maintenance and supplemental airworthiness instructions for the cockpit sunvisor system used on the following Cessna aircraft models: 310, 310A, 310B, 310C, 310D, 310E, 310F, 310G, 310H, E310H, 3101, 310J, 310J-1, E310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R, 335, 340, 340A, 336, 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 421, 421A, 421C, 425, 404, 406, 441. b. Rosen reserves the right to revise this document for changed procedures, improved parts or changes to the system or components. c. All technical support, spare sales, repairs or modifications are to be directed directly to Rosen Sunvisor Systems LLC. RSS must be contacted for future revision of this document as it is possible this does not contain the latest revisions. 2. Revision Service Current revision status and revisions to this document may be obtained from Rosen Sunvisor Systems’ website: www.rosenvisor.com. We recommend that you periodically check to make sure you are using the most current version. Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 5 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fault Isolation 1. General a. This section identifies Probable Causes and Corrections for possible faults. Problem Probable Cause Corrective Action Visor does not extend on arm Tension Thumb knob too tight Loosen knob and slide using knob Lens does not rotate smoothly on vertical axis Vertical pivot tension incorrectly set Re-tension vertical pivot Lens does not rotate smoothly on horizontal axis Horizontal pivot tension incorrectly set Re-tension horizontal pivot Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 6 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS Product Description General a. The Rosen Sunvisor System consists of two visor assemblies which have been designed to improve pilot comfort during standard cockpit operations. The visor assemblies are fastened to the airframe in the same mounting positions as the factory installed visors. Installation Instructions This is an FAA STC’d installation requiring a log book entry upon completion. Installation should take approximately 1 hour. Please read these short instructions COMPLETELY before starting. Tools Required (not included): Phillips Screwdriver 5/32 Allen Key 9/64 Allen Key Installation Hardware (included): Qty: (4) #10-32 Flat Head Screw NOTE: On Cessna 310’s this system will only fit applications that have the original ball joint style equipment as shown.  Using a Philips screwdriver, remove (2) stock ball mount visors.  If your mounting holes are positioned fore and aft in relationship to the centerline of your aircraft, your swivel should look like this when viewed from behind:  If your mounting holes are positioned perpendicular to the centerline of your aircraft, your swivel should look like this when viewed from behind: Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 7 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS  If necessary, reconfigure swivel mount bracket as indicated.  This image is the pilot’s side of a longitudinal configuration.  Attach your new Rosen sunvisors using the #10-32 Flat Head Screws provided. NOTE: The red Thumb Screw knob should be forward, away from the operator.  Repeat for the other side.  Installation is now complete.  Visors will stow in different positions, but generally the system will stow overhead when in the forward position. Removal a. Reverse installation procedure. Weight and Balance Because operators calculate Weight and Balance differently the actual station number must be determined by the installer’s calculations. With the visor located in forward use position this system adds 2.09 lbs. located at the mount point of the visor. When the original visors are removed they must be weighed and removed from the calculation. Repair General a. All components that do not meet the requirements for continued use must be replaced. Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 9 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS Illustrations Fig 1 Fig 2 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 10 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fig 3 Fig 4 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 11 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fig 5 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 12 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS Part List Fig. No Fig. Item Part Number Description Reference Eff QTY 1 1 R1180000-006 Complete Assembly RCS-300-6 RC300/400- 300-1 System 2 2 1180400-011 Lens Assembly, Pilot RCS-300-6P RC300/400- 300-1P 1 2 3 1180400-012 Lens Assembly, Copilot RCS-300-6C RC300/400- 300-1C 1 3 4 1010000-5 Slide Assembly 2 3 5 1020100-001 Assembly, Mod Block NSA 2 3 6 MS24693- C274B Srew #10-32 X .75 FLH PHIL 100 SST BLK 4 3 7 1160102-1 Bonanza Style Swivel 2 3 8 MS24693- C48BP Screw #8-32 X.375 Phillips Flathead 100 (Black Patch) 10 3 9 1180109 Mounting Bracket 2 3 10 MS16995-27B Screw #8-32 X .625 HEX SHCS SST BLK 2 3 11 8HCLW Washer #8 High Collar Lock 4 3 12 MS16995-28B Screw #8-32 X .75 HEX SHCS SST BLK 2 3 13 1180301-002 Lens 2 3 14 1010003 Lens Strip 2 4 15 1010001-5 Female Slide-Universal 2 4 16 1010002-3 Male Slide-Universal 2 4 17 90295A110 Nylon Washer .06 X .405 OD- .175 ID 2 4 18 B-19679 Compression Spring (Red Knob) 2 4 19 99-701 Ø1/2 Knurled Red Knob 8-32 X 7.5 2 5 20 1020003-001 Mod Block B 2 5 21 1020002-001 Mod Block A 2 5 22 2801-0010 SS Washer (5710-61-30 Seastrom) 4 5 23 10HCLW Washer #10 High Collar Lock 2 5 24 MS16996-12B Screw #10-32 X .75 Hexagon Socket Cap 2