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Installation Instructions for Cessna Citation III Monorail Sunvisor System

Cessna Citation III · Systems Description

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Overview

This document provides installation instructions for the Rosen Monorail Sunvisor System specifically designed for the Cessna Citation III. It includes detailed steps for removing existing sun visors, installing the new monorail system, and ensuring proper functionality of the visors. The instructions emphasize the importance of following FAA regulations and include guidance on continued airworthiness and maintenance of the installed system. This document is intended for aircraft maintenance personnel and technicians involved in the installation of the sunvisor system.

  • Installation requires a logbook entry upon completion.
  • Use a 3/32 Hex Key and a 7/64 Hex Key for installation.
  • No drilling into the aircraft structure is required for rivnut installation.
  • Visors can be adjusted and moved along the monorail by turning the thumb tension knob counter-clockwise.
  • Periodic maintenance includes cleaning lenses and adjusting pivot tensions.

Document

Source

Originally published by www.aircraftspruce.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
2007
Pages
2
File size
68 KB
Publisher
www.aircraftspruce.com
How rare is it?
51Cessna Citation III registered worldwide · 0 active

Common. Rarer than 2% of the aircraft models we track.

Documentation completeness
1/7

Most owners only have the POH. Here's the essential set for the Cessna Citation III.

  • Pilot's Operating Handbook / AFM
  • Checklist
  • Maintenance Manual
  • Parts Catalog (IPC)
  • Systems & Wiring
  • Service Bulletins
  • Type Certificate (TCDS)

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In this document

Installation Steps

The installation process begins with the removal of the existing sun visors from both the pilot and copilot sides. The new Rosen monorail is then installed using existing hard points, ensuring a secure fit. Specific measurements are provided for marking rivnut locations, and the installation requires no drilling into the aircraft structure. The document details the use of screws and rivnuts to secure the monorail and emphasizes the importance of proper alignment during installation.

Continued Airworthiness Instructions

The document outlines maintenance recommendations for the sunvisor system, including periodic cleaning of the lenses with mild soap and water or an approved aviation cleaner. It also advises on adjusting the pivot tensions of the visor assemblies to maintain functionality. These instructions are crucial for ensuring the longevity and safety of the installed system.

Airworthiness Limitations

The Airworthiness Limitations Section is FAA approved and specifies that maintenance must comply with §43.16 and §91.403 of the Federal Aviation Regulations. The document states that there are no airworthiness limitations associated with the installation of the Rosen Monorail Sunvisor System.

Safety notes

  • Ensure all installation steps are followed to maintain compliance with FAA regulations.
  • Do not use abrasives on the visor lenses to prevent damage.

Full document text

86365 College View Road Eugene, Oregon USA 97405 541.747.0034 w w w . r o s e n v i s o r . c o m Page 1 of 2 Installation Instructions for Cessna Citation III Monorail Sunvisor System R1810000-3 (Kit R650-300-1) This is a FAA STC’d installation requiring a logbook entry upon completion. Doc: 9041-0181-001 Rev Date Approved B 3/8/2007 GH Please read through these instructions completely before beginning. Hardware: 1 3/32 Hex Key 1 7/64 Hex Key 4 A10K80 Rivnuts 8 PS10F12CPG02NA Retaining Clips (E-clips) • Remove present sun visors from pilot and copilot sides of the aircraft. • Remove visors from Rosen monorail by loosening thumb knobs (retaining clips have been left off for this purpose). • Locate the Rosen monorail by installing (2) two PS10F12CPG02NA screws through the side brackets on both sides of the aircraft. The side brackets pick up the existing hard points for the original visor. As the fasteners are tightened, any mismatch between the bracket and side wall will disappear. • With the monorail firmly in place, make a mark centered in the aft bracket and 1” above the window trim. This mark is for locating the A10K80 rivnut. Repeat the same procedure for the opposite side of the aircraft. • The front bracket should be flush with the center post trim. To insure this, place an upward pressure on the bracket and mark the center of each slot. These marks are to locate the two front A10K80 rivnuts. • Remove the monorail and install (4) four A10K80 rivnuts as marked (two in front and one on each side of the cockpit). Rivnuts should be installed in the Royalite trim. No holes are to be drilled into the aircraft structure. • Reinstall the monorail using (8) eight PS10F12CPG02NA screws as provided. • Remount visors on the monorail and install the retaining clips (“E” clips) on the aft portion of the thumb tension knob. This will insure that the pilots do not inadvertently over-loosen the visor clamping blocks. • To move the visors, the thumb tension knob needs to be turned in a counter-clockwise direction. Grasping the thumb tension knob, slide the visor smoothly along the monorail. To move beyond the mounting clips, the visor must be turned so that the slot in the clamping blocks can move past the monorail brackets. The mid brackets were designed so that the sliding visor would not be directly in front of the pilot’s or copilot’s face. • Your monorail system is equipped with the new swivel modification so that the visor can be rotated in the vertical axis. Rotational tension can be adjusted simply by turning the socket head cap screws in the back of the clamping block assembly. Prior to moving along the track the visor should be returned to the straight fore and aft position. 86365 College View Road Eugene, Oregon USA 97405 541.747.0034 w w w . r o s e n v i s o r . c o m Page 2 of 2 Continued Airworthiness Instructions: • (On the ground only) o Periodically clean the lenses with a soft cloth, mild soap and water or an approved aviation grade windscreen cleaner. Do not use abrasives on the lens. o Periodically adjust the pivot tensions on the visor assemblies. • Updates to this continued airworthiness sections are available on the Rosen Website. (www.rosenvisor.com) The most up to date version of this document is available on the Rosen Website. (www.rosenvisor.com) We recommend that you periodically look to make sure you are using the most current version. Airworthiness Limitations: The Airworthiness Limitations Section is FAA approved and specifies maintenance requires 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. SLIDE FROM HERE ROTATE UP TO STOW ROTATIONAL TENSION ADJUSTMENT