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Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly

CESSNA 414A · Systems Description

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Overview

This document is a Component Maintenance Manual (CMM) for the Rosen Sunvisor System, specifically designed for use in the Cessna 414A and other models in the Cessna 300 and 400 series. It provides detailed instructions for installation, maintenance, and continued airworthiness of the sunvisor system. The manual is intended for maintenance personnel and technicians responsible for the upkeep of the sunvisor systems in these aircraft. It includes information on fault isolation, repair procedures, and a parts list, ensuring that users can effectively maintain the system and comply with airworthiness directives.

  • The Rosen Sunvisor System installation adds 2.09 lbs at the mount point.
  • Installation requires specific tools: Phillips screwdriver, 5/32 Allen Key, and 9/64 Allen Key.
  • Installation takes approximately 1 hour and requires a logbook entry.
  • Common faults include visors not extending and lenses not rotating smoothly, with specific corrective actions provided.
  • The manual includes a comprehensive parts list for maintenance and repairs.

Document

Source

Originally published by www.gallagheraviationllc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Systems Description
Year
2015
Pages
18
File size
573 KB
Publisher
www.gallagheraviationllc.com
How rare is it?
411CESSNA 414A registered worldwide · 379 active

Common. One of the most common aircraft types we track.

Documentation completeness
5/7

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In this document

Introduction

The introduction outlines the purpose of the Rosen Component Maintenance Manual, which provides maintenance and airworthiness instructions for the cockpit sunvisor system used in various Cessna aircraft, including the 414A. It emphasizes the importance of using the latest revision of the document and directs users to contact Rosen for technical support.

Installation Instructions

This section details the installation process for the Rosen Sunvisor System, which is an FAA STC’d installation requiring a logbook entry. The installation is estimated to take approximately 1 hour and requires specific tools such as a Phillips screwdriver and Allen keys. The instructions include steps for removing existing visors and attaching the new system.

Weight and Balance

The Weight and Balance section specifies that the installation of the sunvisor system adds 2.09 lbs at the mount point. It advises that the original visors must be weighed and removed from the calculation to ensure accurate weight and balance assessments.

Fault Isolation

This section provides troubleshooting guidance for common issues with the sunvisor system, such as a visor not extending or lenses not rotating smoothly. It outlines probable causes and corrective actions to resolve these faults.

Parts List

The parts list includes detailed information on components of the sunvisor system, including part numbers and descriptions. This section is crucial for maintenance personnel to identify and order replacement parts as needed.

Safety notes

  • Ensure to use the latest revision of the manual for compliance with airworthiness directives.
  • Installation must be logged in the aircraft's logbook to maintain airworthiness.

Full document text

86365 College View Road Eugene, Oregon USA 97405 541.747.0034 www.rosenvisor.com Page 1 of 4 Cessna 300 and 400 Series Aircraft Drawing List RCS-300/400-00 DL Doc. # 9050-0118-003 Drawing Reference Description Rev. A34CE (Cessna T303) (RC303-300-1) 1182100 Complete Assembly D 1180302 Lens C 1182101 Back Plate A 1182102 Mounting Bracket A 1010000-5 Complete Slide Assembly F 1010001-5 Female Slide M 1010002-3 Male Slide T 1010003 Lens Strip G 1020100-001 Assembly, Mod Block NSA F 1020002-001 Mod Block A P 1020003-001 Modified ‘B’ Block Standard V 1160102-1 Bonanza Style Swivel H 9051-0118-014 Installation Instructions for Cessna 303 Sunvisor System D Continued.. Date Revision Approved 2/15/22 K SYS 86365 College View Road Eugene, Oregon USA 97405 541.747.0034 www.rosenvisor.com Page 2 of 4 Drawing Reference Description Rev. 3A10, A2CE, A7CE, A25CE, A28CE (Cessna 310-400 Series Aircraft) (RC300/400- 300-1) (RCS-300-6) 1180000-006 Complete Assembly E 1180400-011 Assembly, Side, Pilot’s F 1180400-012 Assembly, Side, Co-Pilot’s F 1180100-010 Mounting Assembly D 1180109 Mounting Bracket H 1160102-1 Bonanza Style Swivel H 1020100-001 Assembly, Mod Block NSA F 1020002-001 Mod Block A P 1020003-001 Modified ‘B’ Block Standard V 1010000-5 Complete Slide Assembly F 1010001-5 Female Slide M 1010002-3 Male Slide T 1010003 Lens Strip G 1180301-002 Lens F 9051-0118-015 Installation Instructions for Cessna 310-400 Series Sunvisor System D Continued.. 86365 College View Road Eugene, Oregon USA 97405 541.747.0034 www.rosenvisor.com Page 3 of 4 Drawing Reference Description Rev. 3A25 (Cessna 320 Series) (RC320-300-1) 1182200 Complete Assembly E 1182201 Swivel Stud A 1182202 Angle Washer A 1020100-001 Assembly, Mod Block NSA F 1020002-001 Mod Block A P 1020003-001 Modified ‘B’ Block Standard V 1010000-5 Complete Slide Assembly F 1010001-5 Female Slide M 1010002-3 Male Slide T 1010003 Lens Strip G 1160401-002 Lens L 9051-0118-016 Installation Instructions for Cessna 320 Series Sunvisor System E Continued.. 86365 College View Road Eugene, Oregon USA 97405 541.747.0034 www.rosenvisor.com Page 4 of 4 Drawing Reference Description Rev. A7CE (Cessna 414A and 421B only) (R1181300-0) 1181300 Complete Assembly D 1181201 421B Swivel C 1020100-001 Assembly, Mod Block NSA F 1020002-001 Mod Block A P 1020003-001 Modified ‘B’ Block Standard V 1010000-5 Complete Slide Assembly F 1010001-5 Female Slide M 1010002-3 Male Slide T 1010003 Lens Strip G 1180301-002 Lens F 9051-0118-022 Installation Instructions for Cessna 414A, 421B Series Sunvisor System D Kits R1160102-1 Bonanza Style Swivel Kit 1160102-1 Bonanza Style Swivel H Magnalube R1010000-KIT-5 Universal Slide with Lens Strip Kit A 1010000-5 Complete Slide Assembly F 1010003 Lens Strip G MS24693-C48BP #8-32 X .375 Flat Head Phillips SS Black Patch Screw R1181201 Cessna 421B Swivel Kit 1181201 421B Swivel C 43-SPP 7/16 E-clip R1180302 T303 Lens Kit C R1180301-002 310-400 Series Lens Kit F R1160401-002 320 Lens Kit L Rosen Sunvisor Systems CMM / IPC for Sunvisor Assembly (p/n R1180000-006) Rosen Sunvisor Systems LLC Data 9051-0118-015 Rev D Page 1 of 12 Company Proprietary Information. This document may not be disclosed without the permission of RSS Cessna 310-400 series NSA Sunvisor System 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

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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

Type certificate, explained

What's in the CESSNA 414A TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS A7CERev 47· Issued 2007
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