Supplemental Type Certificate

7. Textron (formerly Cessna) 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182T, R182, T182, TR182, T182T 3A13 CAR 3 9050-0118-013 Revision T, 2/15/22 6/8/22 8. Textron (formerly Cessna) 182S 3A13 FAR 23 9050-0118-013 Revision T, 2/15/22 6/8/22 FAA APPROVED MODEL LIST (AML) SA00871SE FOR INSTALLATION OF ROSEN SUNVISOR SYSTEMS COCKPIT SUN VISOR ISSUE DATE: January 25, 2001 ITEM AIRPLANE MAKE AIRPLANE MODEL TYPE CERTIFICATE NUMBER CERTIFICATION BASIS FOR ALTERATION FAA APPROVED DRAWING LIST AML AMENDED NUMBER REVISION NO. AND DATE DATE Page 2 of 3 9. Textron (formerly Cessna) 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 3A24 CAR 3 9050-0118-013 Revision T, 2/15/22 6/8/22 10. Textron (formerly Cessna) 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D, TP206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, 206H, T206H A4CE CAR 3 9050-0118-013 Revision T, 2/15/22 6/8/22 11. Textron (formerly Cessna) 207, 207A, T207, T207A A16CE FAR 23 9050-0118-013 Revision T, 2/15/22 6/8/22 12. Textron (formerly Cessna) 210, 210A, 210B, 210C, 210D, 210E, 210F, 210-5 (205), 210-5A (205A), T210F, 210G, 210H, T210H, T210G, 210J, T210J, T210L, 210K, 210L, T210K, 210M, T210M, 210N, P210N, T210N, 210R, P210R, T210R 3A21 CAR 3 9050-0118-013 Revision T, 2/15/22 6/8/22 13. Textron (formerly Cessna) 120, 140, 140A A-768 CAR 4a 9050-0118-013 Revision T, 2/15/22 6/8/22 14. Textron (formerly Reims) F150F, F150G, F150H, F150J, F150K, F150L, F150M, F152, FA150K, FA150L, FA150M, FA152, FRA150L, FRA150M A13EU CAR 3 9050-0118-013 Revision T, 2/15/22 6/8/22 15. Textron (formerly Reims) F172D, F172E, F172F, F172G, F172H, F172K, F172L, F172M, F172N, F172P, FP172D A4EU CAR 3 9050-0118-013 Revision T, 2/15/22 6/8/22 SUPPLEMENTAL TYPE CERTIFICATE 10031251 For the European Union Aviation Safety Agency Cologne, Germany, 05 April 2023 Marco CAPACCIO Section Manager Small Aircraft, Balloons & Airships See Continuation Sheet(s) Task Number: 10000245 - EASA.IM.A.S.03270 ROSEN SUNVISOR SYSTEMS L.L.C. - 303362 TE.CERT.00091-005 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 2 An Agency of the European Union This Certificate/Approval is issued by EASA, acting in accordance with Regulation (EU) 2018/1139 on behalf of the European Union, its Member States and of the European third countries that participate in the activities of EASA under Article 129 of that Regulation and in accordance with Commission Regulation (EU) No. 748/2012 to ROSEN SUNVISOR SYSTEMS L.L.C. 86365 COLLEGE VIEW ROAD EUGENE OR 97405 UNITED STATES OF AMERICA and certifies that the change in the type design for the product listed below with the limitations and conditions specified meets the applicable Type Certification Basis and, if applicable, environmental protection requirements when operated within the conditions and limitations specified below: Type Certificate Number: SEE FAA APPROVED MODEL LIST (AML) SA00871SE, DATED 8 FEBRUARY 2023. Type Certificate Holder: See FAA AML Type: See FAA AML Model: See FAA AML Original STC Number: FAA STC SA00871SE Description of Design Change: Installation of cockpit sunvisors EASA Certification Basis: The Certification Basis for the original product remains applicable to this certificate/approval. The requirements for environmental protection and the associated certified noise and/ or emissions levels of the original product are unchanged and remain applicable to this certificate/ approval. Associated Technical Documentation: Rosen Products LLC drawing lists per the attached FAA AML No. SA00187SE, reissued 1 July 2022, Task Number: 10000245 - EASA.IM.A.S.03270 ROSEN SUNVISOR SYSTEMS L.L.C. - 303362 TE.CERT.00091-005 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 2 of 2 An Agency of the European Union SUPPLEMENTAL TYPE CERTIFICATE - 10031251 or later revisions of the above listed document(s) approved/accepted on behalf of EASA in accordance with the Technical Implementation Procedures of EU/ USA Bilateral Agreement. Limitations/Conditions: Prior to installation of this change/repair it must be determined that the interrelationship between this change/repair and any other previously installed change and/ or repair will introduce no adverse effect upon the airworthiness of the product. - End - 86365 College View Road Eugene, Oregon USA 97405 (541) 747 0034 www.rosenvisor.com Page 1 of 2 Cessna Singles NSA Sunvisor System Date Rev Approved 5/22/25 W SYS 120-207 Side Mount 172-207 Center Mount 210 P210 Drawing List Doc. # 9050-0118-013 FAA STC SA00871SE Kit RCS-300 Drawing Number Description -1 -2 -3 -4 Rev 1 1180001 Complete Assembly F 1 1180002 Complete Assembly E 1 1180003 Complete Assembly Cessna 210 P 1 1180004 Complete System H 2 1180101 Bracket, Mounting H 2 1180102 Bracket, Mounting, Cessna 172-207 M 2 1180103 Bracket, Mounting L 2 1180104 Module Mounting Clamp G 2 1180105 Mounting Bracket D 2 2 2 2 1180110 7° Swivel M 2 2 2 2 1020001 Original Block R - - - - 1010000-5 Complete Slide Assembly G 2 2 2 2 1010001-5 Female Slide - Universal M 2 2 2 2 1010002-3 Male Slide - Universal U 2 2 2 2 1010003 Lens Strip H 2 2 2 2 1180301-001 Lens (RCS-200-1) F Replacement Kit for RCS-300-1 1180100-001 Mounting Assembly D 1180101 Bracket, Mounting H 1180110 7° Swivel M R1180110 Swivel Kit 1 1 1 1 1180110 7° Swivel M 1 1 1 1 Lube Packet 86365 College View Road Eugene, Oregon USA 97405 (541) 747 0034 www.rosenvisor.com Page 2 of 2 R1010000-KIT-5 Universal Slide with Lens Strip Kit A 1010000-5 Complete Slide Assembly G 1010003 Lens Strip H MS24693-C48BP #8-32 X .375 Flat Head Phillips SS Black Patch Screw R1180301-001 Lens Kit F 1 1 9051-0118-012 Cessna Singles (Except 177 & 210) PMM/IPL/ICA G 1 1 9051-0118-017 Cessna 210 PMM/IPC/ICA G Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 1 of 19 Cessna Singles (except 177, 190/195 & 210) NSA Sunvisor System Rosen Kit Number R1180001-0 (RCS-300-1) R1180002-0 (RCS-300-2) R1180001-0 R1180002-0 Product Maintenance Manual with Illustrated Parts List and Instructions for Continued Airworthiness Manual Number Rosen 9051-0118-012 Revision G February 21, 2018 Rosen Sunvisor Systems LLC 86365 College View Road Eugene, Oregon 97405 USA 800-284-7677 Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 2 of 19 This ICA must be followed when the R1180001-0 and R1180002-0 Sunvisor systems are installed in accordance with Supplemental Type Certificate (STC) No. SA00871SE, dated January 25, 2001, amended April 8, 2005. The information contained in this document supplements or supersedes the basic manual only in those areas listed herein. For limitations, procedures, and performance information not contained in this manual, consult the basic aircraft ICA or Maintenance Manual. STATEMENT OF Rev D CERTIFICATION This manual complies with Federal Aviation Association (FAA) Airworthiness Requirements _Part 23 ______________. FAA Acceptance: Allison Buss Date: 3/29/18 . The above certification does not apply to revisions or amendments made after the date of initial certification by other Approved Organizations. Revisions or amendments made by other Approved Organizations must be separately certified and recorded on separate record sheets Record of Revisions Rev Description Date Approved F Changed to CMM/IPC format. Correct typos 8/15/14 GH G Updated, Changed to PMM Format 2/21/18 GH Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 3 of 19 Table of Contents Record of Revisions …………………………………………………………………….3 Introduction ………………………………………………………………………………4 General ………………………………………………………………………………….4 Revision Service ………………………………………………………………………..4 Fault Isolation ……………………………………………………………………………5 Product Description ……………………………………………………………………..6 Installation Instructions …………………………………………………………………6 Section I Models 120, 140, 150, 152, 170, 172, 180, and 182 ……………6 Section IA Models 172-207 Before 1980 (excluding 177, 190/195) ………8 Section II Models 172-207 1980 and Later (excluding 177, 190/195)……9 Section III - Operating Instructions ………………………………………………….11 Fault Isolation ……………………………………………………………………….12 Removal ……………………………………………………………………………..12 Weight and Balance ………………………………………………………………..12 Repair ………………………………………………………………………………..12 Instructions for Continues Airworthiness (ICA) …………………………………13 Airworthiness Limitations …………………………………………………………..13 Section IV – System Images , IPC and Parts listing R1180001-0 ………………………………………………………………………..14 R1180002-0 ………………………………………………………………………..17 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 4 of 19 Introduction 1. General a. This Rosen Product Maintenance Manual provides use, maintenance and supplemental airworthiness instructions for the cockpit Sunvisor system used on all Cessna aircraft models listed on FAA Approved Model List (AML) SA00871SE except for the 210 models. 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 PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 5 of 19 Product Description General The Rosen Sunvisor System consists of two visor assemblies which have been designed to improve pilot comfort during standard cockpit operations. In many cases the visor assemblies are fastened to the airframe in the same mounting positions as the factory installed visors. Installation Overview Please read this entire instruction set prior to beginning installation for important information pertaining to your installation.  For all pre-1980 aircraft including 120, 140, 150, 152, 170, 172, 180, and 182 models that do not have threaded mounting provisions on the forward face of the forward bulkhead spar use Rosen kit R1180001-0 and proceed to section I, page 6.  For all pre-1980 aircraft including 170, 172, 180, and 182 that have threaded mounting provisions on the forward face of the forward bulkhead spar use Rosen kit R1180001-0 and proceed to section IA, page 8.  For all post 1980 aircraft except 152, 177, and 190/195 use Rosen kit R1180002-0 and proceed to section II page 9. Figure – A 120-207 R1180001-0(RCS-300-1) Models prior to 1980 and some early 1960 210s with side or no mounting provisions. Figure – B 172-207 R1180002-0(RCS-300-2) 1980 and later models with Centralized mounting provisions. Forward Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 6 of 19 Section I Installation of Rosen NSA Sunvisor System For 120, 140, 150, 152, 170, 172, 180 and 182 Built with no factory installed visor mounting provisions R1180001-0 (RCS-300-1) 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: Short Phillips screwdriver 9/64 Allen Key 5/32 Allen Key #8-32 Rivnut Installation Tool Installation Hardware (included): Qty: (4) #8-32 x 1 Socket Head Cap Screws (4) #8 washers (4) A8K75 Rivnut  Take the unit marked “pilot’s side”, position it as shown in Figure D and slide the bracket as far outboard on the front overhead spar as possible.  Holding the bracket in that same position, rotate the visor to the side and extend it to the rear. This is to ensure that the bracket position is not so far outboard that there is a problem moving the visor to the side position. #8 Washer Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 7 of 19  Now move the visor to the front and retracted position (keeping the bracket in the same position.) Rotate the visor as if you were going to position it overhead to the rear and make sure it will not hit the top center console.  When the visor is positioned correctly, mark the location for two rivnut holes in the bottom of the bracket.  Install the A8K75 rivnuts provided. NOTE: Proper experience and tools are required for rivnut installation. If there is upholstery material covering the spar remove a large enough diameter to clear the rivnut face. Use a drill stop to avoid drilling more than ¼ inch into the spar. Once the 0.221” diameter hole is drilled add a key notch to the hole to lock the rivnut. P = 0.062 and H=0.057 Be sure the key on the rivnut aligns with the key notch in the mounting hole.  After installation of the rivnuts, install the pilot visor assembly with the socket head cap screws and washers provided.  Repeat this same procedure for the copilot side. Note: The red slide tensioning knob should point toward the windshield and should not be visible to the pilot when the visor is in use.  The visors should appear as in Figure C when you look through the front windshield from outside the aircraft.  Now turn to the Operating Instructions in Section III, Page 11. Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 8 of 19 Section IA Installation of Rosen NSA Sunvisor System For 172 – 207 (excluding 177, 190/195) Manufactured before 1980 with factory installed mounting provisions R1180001-0 (RCS-300-1) 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: Phillips screwdriver. 9/64 Hex Key 5/32 Hex Key Installation Hardware(included): Qty: (4) #10-32 x 1 Socket Head Cap Screws (4) #10 washers  If factory visors are installed use a short Philips screw driver to remove the #10-32 screws securing the visors.  Take the visor assembly marked “pilot side” and using the #10 socket head cap screws and black anodized washers provided, install the unit so that the bracket fits tight up against the front mounting face of the spar. The same hard mounting points are used as the original visor.  If installed, remove the original visors retainers from the center mount along with any unnecessary mounting hardware.  Repeat for the copilot side.  Note: the red slide tensioning knob should point towards the windshield and should not be visible to the pilot when the visor is in use.  Now turn to the Operating Instructions in Section III, Page 11. Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 9 of 19 Section II For 172 – 207 (excluding 177, 190/195) 1980 and Later Models Installation of Rosen NSA Sunvisor System R1180002 (RCS-300-2) 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: Short Phillips screwdriver 9/64 Allen Key 5/32 Allen Key Hardware: 4 #10-32 x 1 Socket Head Cap Screws 4 #10 washers  The main difference between the R1180002-0 (RCS-300-2) assembly and the R1180001-0 (RCS-300-1) part is the length of the bracket which picks up the Cessna visor mounting holes.  Use short Phillips screwdriver to remove the #10 fasteners from the center of the plastic type Cessna visor.  Using the #10 socket head cap screws, washers and 9/64” Allen Key provided, attach the visor assembly marked “pilot side” by inserting the screw through the slots at the end of the bracket. Note: Attach the bracket to the windshield side of the forward bulkhead spar, so that the bracket mounting face is not visible from the pilot seat. If attached to the overhead on the seat side, the visor assembly will be too close to the pilot’s face. The red slide tensioning knob should point toward the windshield and should not be visible to the pilot when the visor is in use.  Ensure that the bracket fits tight against the overhead.  Repeat the same procedure for the copilot visor assembly.  If you look aft through the front windshield from the outside of the aircraft, the visor assembly should appear as it does in Figure E. Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 10 of 19 Figure E - post 1980 Center Mount  Now turn to the Operating Instructions in Section III, Page 11. Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 11 of 19 Section III Operating Instructions NOTE: The operating instructions are identical for both the R1180001-0 and R1180002-0 systems.  The Rosen NSA Sunvisor System™ for the Cessna single engine line has two-axis pivot and, although level when placed across the front windshield, it rotates down at about a 7º incline as you rotate it to the side. This incline is to give the Cessna pilot more coverage low on the sides for that late or early morning sun.  Rotational tension can be adjusted by small adjustments to the socket head cap screws in the side or front of the main swivel block as shown in Figure F.  When installed correctly, the slide tension knob is located inboard when the visors are rotated to either side window of the aircraft. Tension can be adjusted on the slide to make it easier or more difficult to operate. Once the tension is set the visor can be moved by just gripping the visor material.  Standard visor placements are shown in Figure G. Note: In Figure H, rivnut and mounting screw from bottom is only used when no factory fasteners are provided. In flight the visors can be placed fully forward or aft as shown in Figure H, but for flight-line stowing the visor must be left in the overhead or rearward position. Note: Do not use your Rosen sunvisors for heat protection when parked on the ramp for extended periods. The visors should be left hanging vertically when not in use. Figure G Figure H Figure F Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 12 of 19 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 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. For weight and balance the following weights are used: R1180001-0 2.2 Lbs. R1180002-0 2.8 Lbs. With the visor located in the stow position (in forward position and folded up) the weight is located at the mount point datum 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 PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 13 of 19 Instructions for Continued Airworthiness  (On the ground only) o Periodically clean the lenses with a soft cloth, mild soap and water or Rosen Cleaner. Do not use abrasives on the lens. o Periodically adjust the pivot tensions on the visor assemblies. o Periodically clean and lightly re-lubricate slide. Airworthiness Limitations The Airworthiness Limitations Section is FAA approved and specifies maintenance required 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. Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 14 of 19 Section V Illustrations and IPC for R1180001-0 Fig 1 Fig 2 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 15 of 19 Fig 3 Fig 4 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 16 of 19 Part List R1180001-0 Fig. No Fig. Item Part Number Description Reference Eff QTY 1 1 R1180001-0 Complete System RCS-300-1 System 2 2 R1180001-1 Pilot Side Assembly RCS-300-1P 1 2 3 R1180001-2 Copilot Side Assembly RCS-300-1C 1 3 4 1180101 Bracket, Mounting 2 3 5 1020001 Block, Original 2 3 6 1010003 Lens Strip 2 3 7 1180301-001 Lens RCS-200-1 2 3 8 1180110 Cessna Swivel 2 3 9 1010000-5 Slide Assembly-Universal 2 4 10 1010001-005 Female slide, Universal 2 4 11 99-701 ½ diameter Knurled Red Knob #8-32 X .50 2 4 12 B19679 Compression Spring (Red Knob) 2 4 13 90295A110 Washer Nylon .06 X .405 OD X .175 ID 2 4 14 1010002-3 Male Slide, Universal 2 3 15 8HCLW Washer #8 Lock High Collar STL Blk 4 3 16 MS16995-27B SCR #8-32 X .625 Hex SHCS SST Blk 4 3 17 832X716FSHCS SBP SCR #8-32 X .437 FLH HX SH 82 SST Blk P 4 3 18 AN960-C8L Washer #8 4 3 19 A8K75 #8-32 Rivnut Grip .010-.075 4 3 20 MS16995-30B SCR #8-32 X 1.00 HX SHCS SST Blk 4 3 21 MS16996-14B SCR #10-32 X 1.00 HX SHCS SST Blk 4 3 22 MS24693C48BP SCR #8-32 X .375 FLH Phil 100 SST Blk P 6 3 23 AS-10 Washer Flat .500 X .200 X .062 4 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 17 of 19 Illustrations and IPC for R1180002-0 Fig 6 Fig 5 3 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 18 of 19 Fig 7 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180001-0, R1180002-0) Rosen Sunvisor Systems LLC Data Information may only be used in Conjunction with Rosen Products 9051-0118-012 Rev G Page 19 of 19 Part List R1180002-0 Fig. No Fig. Item Part Number Description Reference Eff QTY 5 1 1180002-0 Complete System RCS-300-2 System 6 2 1180002-1 Complete Assembly, Pilot RCS-300-2P 1 6 3 1180002-2 Complete Assembly, Copilot RCS-300-2C 1 7 4 1180102-001 Mounting Bracket, Pilot 1 7 5 1180102-002 Mounting Bracket, Copilot 1 7 6 1180110 Cessna Swivel 2 7 7 1020001 Block Original 2 7 8 1010003 Lens Strip 2 7 9 1010000-5 Slide Assembly, Universal 2 4 10 1010001-005 Female slide, Universal 2 4 11 99-701 ½ diameter Knurled Red Knob #8-32 x .50 2 4 12 B19679 Compression Spring (Red Knob) 2 4 13 90295A110 Nylon Washer .06 X .405 OD X .175 ID 2 4 14 1010002-3 Male Slide, Universal 2 7 15 1180301-001 Lens RCS-200-1 2 7 16 8HCLW Washer #8 Lock High Collar STL Blk 4 7 17 MS16996-14B SCR #10-32 X 1.00 Hex SHCS SST Blk 4 7 18 MS16995-27B SCR #8-32 X .625 HEX SHCS SST Blk 4 7 19 832X716FSHC SSBP SCR #8-32 X .437 FLH HX SH 82 SST Blk P 4 7 20 MS24693- C48BP SCR #8-32 X .375 FLH Phil 100 SST Blk P 6 7 21 AS-10 Washer Flat .500 X .200 X .062 4