supplemental type certificate 10084369 - Rosen Sunvisor Systems

Rosen Kit Number R1182200-0, RC320-300-1 Component Maintenance Manual with Illustrated Parts List and Instructions for Continued Airworthiness Manual Number Rosen 9051-0118-016 Revision E 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 R1182200) Rosen Sunvisor Systems LLC Data 9051-0118-016 Rev E Page 3 of 11 Company Proprietary Information. This document may not be disclosed without the permission of RSS Record of Revisions Rev Description Date Approved E 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 9-10 Parts List 11 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1182200) Rosen Sunvisor Systems LLC Data 9051-0118-016 Rev E Page 4 of 11 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: 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F. 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 R1182200) Rosen Sunvisor Systems LLC Data 9051-0118-016 Rev E Page 5 of 11 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 R1182200) Rosen Sunvisor Systems LLC Data 9051-0118-016 Rev E Page 6 of 11 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): 5/16 Wrench Socket Installation Hardware (included): Qty: (2) 1182201 Swivel Stud (2) 1182202 Angle Washer (2) 1428LNSS 1/4-28 Locking Nut (2) MS16995-27B 8-32X5/8 Socket Head Cap Screw (4) 8HCLW #8 High Collar Washer (1) 5/32 Hex Key (1) 9/64 Hex Key Remove the original sunvisors from your Cessna 320. This will reveal a #10-32 hard mounting point in the aircraft.  Run the 1/4-28 locking nut completely onto the threaded mounting stud provided. Slide the angle washer onto the stud as shown.  Thread the #10-32 threaded portion of the mounting stud into the hard point in the airframe. Use a 5/16 wrench on the flats provided on the mounting stud. Be careful not to burr or damage the stainless steel diameter on the mount as it will score the inside of the clamping mechanism.  After the stud has been secured in place, use a deep socket to tighten the 1/4-28 locking nut, making sure the angle washer fits the contour of the overhead trim. When tightened, the locking nut and trim adapter should lock the mounting stud in place to prevent rotation when the Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1182200) Rosen Sunvisor Systems LLC Data 9051-0118-016 Rev E Page 7 of 11 Company Proprietary Information. This document may not be disclosed without the permission of RSS visor is turned. When tightened, the distance from the trim adapter to the bottom of the mounting stud is .925”, which allows for .050” clearance between the visor clamping mechanism and the trim adapter. If necessary, loosen the 1/4-28 locking nut and screw the stud in or out using the 5/16 flats, and retighten.  Lubricate the clamp and stud, then mount the sunvisor assembly onto the stud and secure with the #8-32 screw and lock washer provided. Tension the screw to provide proper resistance to motion.  Repeat this procedure for the opposite side of the aircraft.  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 the forward use position this system adds 2.04 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 R1182200) Rosen Sunvisor Systems LLC Data 9051-0118-016 Rev E Page 9 of 11 Company Proprietary Information. This document may not be disclosed without the permission of RSS Illustrations Fig 1 Fig 2 Pilot side Copilot Side Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1182200) Rosen Sunvisor Systems LLC Data 9051-0118-016 Rev E Page 10 of 11 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fig 3 Fig 4 Fig 5 Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1182200) Rosen Sunvisor Systems LLC Data 9051-0118-016 Rev E Page 11 of 11 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 R1182200-0 Complete System, both sides RC320-300-1 System 2 2 R1182200-1 Pilot Side Assembly RC320-300- 1L 1 2 3 R1182200-2 Copilot Side Assembly RC320-300- 1R 1 3 4 1010000-5 Slide Assembly 2 3 5 1020100-001 Assembly, Mod Block NSA 2 3 6 1182201 Swivel Stud 2 3 7 1182202 Angle Washer 2 3 8 1428 LNSS Nut 1/4-28 Locking SS 2 3 9 MS16995-27B Screw #8-32 X .625 HEX SHCS SST BLK 2 3 10 8HCLW Washer #8 High Collar Lock 4 3 11 MS16995-28B Screw #8-32 X .75 HEX SHCS SST BLK 2 3 12 MS24693- C48BP Screw #8-32 X .375 Phillips Flathead 100 (Black Patch) 6 3 13 1160401-002 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 Washer SS (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