Supplemental Type Certificate

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 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 3 of 3 16. Textron (formerly Reims) F182P, F182Q, FR182 A42EU CAR 3 9050-0118-013 Revision T, 2/15/22 6/8/22 17. Textron (formerly Reims) FR172E, FR172F, FR172G, FR172H, FR172J, FR172K A18EU CAR 3 9050-0118-013 Revision T, 2/15/22 6/8/22 FAA APPROVED: ____________________________ For Acting Manager, Seattle Aircraft Certification Office REISSUED: March 24, 2003; July 5, 2022, February 8, 2023 AMENDED: June 8, 2022 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 2/20/24 V 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 E 1 1180002 Complete Assembly D 1 1180003 Complete Assembly Cessna 210 M 1 1180004 Complete System G 2 1180101 Bracket, Mounting G 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 K 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 G 1180110 7° Swivel L R1180110 Swivel Kit 1 1 1 1 1180110 7° Swivel L 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 R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 1 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS Cessna 210 NSA Sunvisor System Rosen Kit Number R1180003-0, RCS-300-3 R1180004-0, RCS-300-4 R1180003-0 R1180004-0 Product Maintenance Manual with Illustrated Parts List and Instructions for Continued Airworthiness Manual Number Rosen 9051-0118-017 Revision G August 16, 2023 Rosen Sunvisor Systems LLC 86365 College View Road Eugene, Oregon 97405 USA Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 2 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS This ICA must be followed when the R1180003-0 and R1180004-0 sunvisor system is 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: Date: . 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 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 3 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS Record of Revisions Rev Description Date Approved F Changed to CMM/IPC format. Correct typos 8/13/14 GH G Correct hex keys 8/16/23 SYS Table of Contents Record of Revisions 3 Introduction 4 General 4 Revision Service 4 Fault Isolation 5 Product Description 6 Installation Instructions R1180003 6 Installation Instructions R1180004 9 Removal 9 Weight and Balance 9 Repair 10 Instructions for Continued Airworthiness 10 Airworthiness Limitations__________________ ____________________10 System Images 11 Parts List R1180003 15 Parts List R1180004 16 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 4 of 16 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 systems used on the following Cessna aircraft models: 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. 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 R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 5 of 16 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 PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 6 of 16 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 for Kit RCS-300-3, R1180003-0 Cessna 210 without Air Conditioning This is an FAA STC’d installation requiring a log book entry upon completion. Installation should take approximately 1½ to 2 hours. Please read these short instructions COMPLETELY before starting. Tools required: Phillips screwdriver Electric drill, 3/8” bit Razor blade Hacksaw File 5/64 Allen Key 9/64 Allen Key 1/8 Allen Key Installation Hardware (included): Qty: (6) MS24671-14BP #8-32X1/2 FSHC BLK/Patch (3) 832x14C9SSSS #8-32X1/4 Cone Point BLK Set Screw (10)1428x14CPSSA ¼-28X1/4 CPS SS BLK (2) 1180104 Channel Clamp  Remove old visors mounted to overhead console.  Remove pilot side plastic trim piece covering vertical post. Remove stall warning horn from trim piece by unscrewing cover cap and sliding warning horn out.  Remove horizontal center trim piece running from pilot side post to co-pilot side post.  Expose spar near corner posts by gently pulling headliner material up off of fabric hooks riveted to forward section of spar. Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 7 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS  While sitting in pilot seat and looking up at spar, locate gusset (or angle piece) running from top of post to spar.  Pencil mark bottom of spar ¾” inboard of gusset.  Slip channel clamp (1180104) over spar, with left edge of clamp in alignment with pencil mark, and short flange facing forward.  Uniformly tighten front and rear cone screws with 1/8” Allen wrench provided. (Ensure that channel clamp is pushed up as close to spar as possible.)  Install three #8 set screws with sharp point down (these screws are used to mark horizontal trim piece in order that holes can be drilled in proper locations). Screws should be installed ‘finger tight’ only (see figure at right), as they will be removed and re-used when installing co-pilot side visor.  Carefully realign horizontal trim piece running across spar. When in original position, push firmly up against #8 pointed screws protruding from channel clamp. These marks can now be punched or drilled with 3/8 ” bit. Drill through plastic trim only, as drilling through fabric headliner will stretch or tear material.  Remove #8 screws and save for use on co-pilot side.  Stretch headliner fabric back over fabric hooks on spar. Puncture fabric at same location of three holes used to attach visor bracket to channel clamp.  Using three #8-32 Hex Flat Head screws, attach visor marked “pilot side” through headliner material to channel clamp. Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 8 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS  Fit vertical trim piece back on post. Top left corner will slightly overlap visor bracket.  Carefully mark location on trim piece that will be notched out to fit around bracket. (PLEASE NOTE: It is better to make small cuts and repeat procedure several times, as opposed to making a notch that is too big the first time!)  Cut out notch and file cut edges of trim piece smooth.  Install warning horn in trim piece and re-attach trim piece to post.  Repeat procedure for co-pilot side.  Properly installed visor systems should hang level across windshield and swing unobstructed to side window. (See figures below) Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 9 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS Installation Instructions for R1180004-0, Kit RCS-300-4 Cessna 210 with Air Conditioning and all P210 models This is an FAA STC’d installation requiring a log book entry upon completion. Installation should take approximately 15 to 30 minutes. Please read these short instructions COMPLETELY before starting. Tools required: Phillips screwdriver 9/64 Allen Key Installation Hardware (included): Qty: (4) MS16995-30B #8-32 x 1 Socket Head Cap Screw (2) PS8C16CPG02NA #8-32x1” Pan Head, Nylon Washered Screw (4) AN960-C8L #8 Washer (2) A8K75 #8-32 Rivnut  Remove both old visors using a Phillips screwdriver.  Mount the visor assembly marked “Pilot’s Side” on the pilot’s side of the aircraft with the two #8-32 Socket Head Cap Screws and washers (supplied) and the 9/64” hex key (supplied). These mount into the original hard points in the aircraft. Slots are provided to allow for miss mounting of the original visors.  Tighten the pilot’s side visor securely.  Repeat the procedure for the co-pilot’s side. Note: If at any point in the future you feel there is too much flex in the bracket when the visor is extended to the rear, an 8-32 rivnut and an 8-32x1” washered fastener are included to mount to the spar using the extra 3/16” hole in the black anodized bracket. 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 stow position (in forward position and folded up) the R1180003-0 system adds 2.1lbs., and the R1180004-0 system adds 2.4 lbs Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 10 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS 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. Instructions for Continued Airworthiness  (On the ground only) o Periodically clean the lenses with a soft cloth, mild soap and water or Rosen Cleaner, Polisher and Protectant. Do not use abrasives on the lens. o Periodically adjust the pivot tensions on the visor assemblies. o Periodically clean slide with a no residue alcohol based cleaner and inspect for wear and damage. 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 R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 11 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS Illustrations and IPC R1180003 Fig 1 Fig 2 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 12 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fig 3 Fig 4 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 13 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS R1180004 Fig 5 Fig 6 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 14 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS Fig 7 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 15 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS Part List R1180003 Fig. No Fig. Item Part Number Description Reference Eff QTY 1 1 R1180003-0 Complete System RCS-300-3, R1180000- 003 System 2 2 R1180003-1 Pilot Side Assembly RCS-300-3P, 1180400-005 1 2 3 R1180003-2 Copilot Side Assembly RCS-300-3C, 1180400-006 1 3 4 1428X14CPSSA ¼ x 28 X .25 Socket Set Screw (Cone Point) 10 3 5 832X716FSHCS SBP #8-32 X .4375 Flat Head Socket Screw 82 Black Patch 4 3 6 1180103 Bracket, Mounting 2 3 7 1180110 Cessna Swivel 2 3 8 MS16995-27B #8-32 X .625 Hexagon Socket Head Cap Screw SST BLK 4 3 9 8HCLW #8 High Collar Lock Washer 4 3 10 MS24693- C48BP #8-32 X .375 Phillips Flathead Screw 100 Black Patch 6 3 11 1180301-001 Lens 2 3 12 1010003 Lens Strip 2 3 13 1010000-5 Complete Slide Assembly 2 3 14 1020001 Block Original 2 3 15 MS24671-14BP #8-32 X .500 Flat Head Socket Screw (Black Patch) 6 3 16 1180104 Module Mounting Clamp 2 4 17 99-701 Ø1/2 Knurled Red Knob 8- 32 x 7.5 2 4 18 B-19679 Compression Spring (Red Knob) 2 4 19 90295A110 Nylon Washer .06 x .405 OD-.175 ID 2 4 20 1010001-5 Female Slide-Universal 2 4 21 1010002-3 Male Slide-Universal 2 832X14C9SSSS #8-32 X .25 Cone Point Set Screw SS BLK 3 Rosen Sunvisor Systems PMM / IPC for Sunvisor Assembly (p/n R1180003, R1180004) Rosen Sunvisor Systems LLC Data 9051-0118-017 Rev G Page 16 of 16 Company Proprietary Information. This document may not be disclosed without the permission of RSS Part List R1180004 Fig. No Fig. Item Part Number Description Reference Eff QTY 5 1 R1180004-0 Complete System RCS-300-4 System 6 2 R1180004-1 Pilot Side Assembly RCS-300-4P 1 6 3 R1180004-2 Copilot Side Assembly RCS-300-4C 1 7 4 AN960-C8L #8 Washer 4 7 5 832X716FSHCS SBP #8-32 X .4375 Flat Head Socket Screw 82 Black Patch 4 7 6 1180110 Cessna Swivel 2 7 7 1020001 Block Original 2 7 8 MS16995-27B #8-32 X .625 Hexagon Socket Head Cap Screw SST BLK 4 7 9 8HCLW #8 High Collar Lock Washer 4 7 10 MS24693- C48BP #8-32 X .375 Phillips Flathead Screw 100 Black Patch 6 7 11 1180301-001 Lens 2 7 12 1010003 Lens Strip 2 7 13 1010000-5 Complete Slide Assembly 2 7 14 MS16995-30B #8-32 X 1.00 Socket Head Cap Screw 4 7 15 1180105-001 Mounting Bracket Pilot 1 7 16 1180105-002 Mounting Bracket Copilot 1 4 17 99-701 Ø1/2 Knurled Red Knob 8-32 x 7.5 2 4 18 B-19679 Compression Spring (Red Knob) 2 4 19 90295A110 Nylon Washer .06 x .405 OD- .175 ID 2 4 20 1010001-5 Female Slide-Universal 2 4 21 1010002-3 Male Slide-Universal 2 PS8C16CPG02 NA #8-32 X 1.00 Panhead Truss Screw 2 A8K75 #8-32 Rivnut 2