PLACARDS AND MARKINGS - EMERGENCY EXIT WARNING PLACARD INSTALLATION
CESSNA T206 · Parts Catalog
Overview
This service bulletin, SEB-11-05, addresses the installation of an emergency exit warning placard for various Cessna 206 models. It is mandatory for compliance during the next 100-hour or annual inspection, or within 12 months of publication. The bulletin outlines the necessary parts and instructions for installation, emphasizing the importance of proper placement for visibility from the pilot's seat. It also includes compliance requirements and maintenance practices that must be followed. The document is intended for aircraft owners and mechanics involved in maintaining Cessna 206 series aircraft.
- This service bulletin is mandatory for Cessna 206 series aircraft.
- The installation must be completed at the next 100-hour or annual inspection, or within 12 months of publication.
- The emergency exit warning placard must be visible from the pilot's seat during all phases of flight.
- The required part for installation is the S4645-16 Emergency Exit Warning Placard.
- Flap positions of 10 degrees or greater may impede evacuation from the cargo door.
Document
Source
Originally published by www.gocivilairpatrol.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Parts Catalog
- Year
- 2024
- Pages
- 6
- File size
- 263 KB
- Publisher
- www.gocivilairpatrol.com
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In this document
Effectivity
The service bulletin applies to several models of the Cessna 206 series, including serial numbers from 206-0001 to U206G 206-07020. This includes various U206 models and their respective serial ranges.
Compliance
Compliance with this service bulletin is mandatory and must be completed during the next 100-hour or annual inspection, or within 12 months of the bulletin's publication date.
Installation Instructions
The bulletin provides detailed instructions for installing the S4645-16 Emergency Exit Warning Placard. The placard must be installed in a location visible to the pilot, and the installation process includes cleaning the area with Isopropyl Alcohol and ensuring proper adhesion.
Material Information
The part required for this installation is the S4645-16 Emergency Exit Warning Placard. It is advised to contact a Textron Aviation Authorized Service Facility for current costs and availability.
Safety Notes
Pilots should be aware that flap positions of 10 degrees or greater may impede evacuation from the cargo door. Proper installation of the placard is crucial for safety.
Safety notes
- Installation of the emergency exit warning placard is crucial for safety during evacuation.
- Flap positions of 10 degrees or greater may impede evacuation from the cargo door.
Full document text
Single Engine SERVICE BULLETIN MANDATORY SEB-11-05 TITLE PLACARDS AND MARKINGS - EMERGENCY EXIT WARNING PLACARD INSTALLATION EFFECTIVITY MODEL SERIAL NUMBERS 206 206-0001 thru 206-0275 U206 U206-0276 thru U206-0437 U206A/TU206A U206-0438 thru U206-0656 U206B/TU206B U206-0657 thru U206-0914 U206C/TU206C U206-0915 thru U206-1234 U206D/TU206D U206-1235 thru U206-1444 U206E/TU206E U20601445 thru U20601700 U206F/TU206F U20601701 thru U20603521 U206G/TU206G 676, U20603522 thru U20607020 REASON To install the emergency exit warning placard on the cockpit instrument panel or another location directly visible while sitting in the pilots's seat. NOTE: The installation of the emergency exit warning placard may also be completed by a pilot with respect to local civil aviation regulations. NOTE: Pilots should be aware of the potential for impeding of the aft cargo door with the flaps extended. DESCRIPTION This service document provides part and instructions to install the emergency exit warning placard that warns that flap positions 10 degrees or greater may impede evacuation from the cargo door. COMPLIANCE MANDATORY. This service document must be accomplished at the next 100-hour/Annual inspection or within 12 calendar months of publish, whichever occurs first. A service document published by Textron Aviation may be recorded as completed in an aircraft log only when the following requirements are satisfied: 1) The mechanic must complete all of the instructions in the service document, including the intent therein. 2) The mechanic must correctly use and install all applicable parts supplied with the service document kit. Only with written authorization from Textron Aviation can substitute parts or rebuilt parts be used to replace new parts. 3) The mechanic or airplane owner must use the technical data in the service document only as approved and published. 4) The mechanic or airplane owner must apply the information in the service document only to aircraft serial numbers identified in the Effectivity section of the document. SEB-11-05 November 25, 2024 Page 1 of 4 Textron Aviation Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT © 2024 SEB-11-05 Page 2 November 25, 2024 Single Engine SERVICE BULLETIN MANDATORY SEB-11-05 5) The mechanic or airplane owner must use maintenance practices that are identified as acceptable standard practices in the aviation industry and governmental regulations. No individual or corporate organization other than Textron Aviation is authorized to make or apply any changes to a Textron Aviation-issued service document or flight manual supplement without prior written consent from Textron Aviation. Textron Aviation is not responsible for the quality of maintenance performed to comply with this document, unless the maintenance is accomplished at a Textron Aviation-owned Service Center. APPROVAL Textron Aviation received FAA approval for the technical data in this publication that changes the airplane type design. FLIGHT CREW OPERATIONS No Changes CONSUMABLE MATERIAL You must use the consumable materials that follow, or their equivalent, to complete this service document. NAME NUMBER MANUFACTURER USE Isopropyl Alcohol Commercially Available To clean surfaces prior to bonding. TOOLING No specialized tooling is required to complete this service document. WEIGHT AND BALANCE INFORMATION Negligible REFERENCES None PUBLICATIONS AFFECTED Model 206 (1964-1973) Illustrated Parts Catalog Model 206 and T206 (1974-1986) Illustrated Parts Catalog ACCOMPLISHMENT INSTRUCTIONS 1. (Refer to Figure 1, Sheet 1.) Install the S4645-16 Emergency Exit Warning Placard as follows: NOTE: The installation of the placard should be in a location that the pilot has a clear view of the placard throughout all phases of flight. NOTE: S4645-16 Emergency Exit Warning Placard silkscreen legend to be black on white background. A. Use the placard or the dimensions of the S4645-16 Emergency Exit Warning Placard as shown within the figure to measure and identify a suitable location on the instrument panel or another location directly visible while sitting in the pilot's seat." B. Clean the placard installation area using Isopropyl Alcohol and lint free cloth. C. Remove the protective backing and carefully set the placard in place, starting at one end and securing contact progressively toward the other end avoiding wrinkling and air bubbles. D. If necessary, use a rubber roller or plastic spatula to press the placard firmly in place. 2. Make an entry in the airplane logbook that states compliance and method of compliance with this service document. Single Engine SERVICE BULLETIN MANDATORY SEB-11-05 Figure 1. Emergency Exit Warning Placard Installation (Sheet 1) SEB-11-05 November 25, 2024 Page 3 SEB-11-05 Page 4 November 25, 2024 Single Engine SERVICE BULLETIN MANDATORY SEB-11-05 MATERIAL INFORMATION Order the part below to install this modification. NEW P/N QUAN- TITY KEY WORD OLD P/N INSTRUCTIONS/ DISPOSITION S4645-16 1 Emergency Exit Warning Placard N/A Install * Please contact a Textron Aviation Authorized Service Facility for current cost and availability of parts listed in this service document. Single Engine OWNER ADVISORY SEB-11-05 TITLE PLACARDS AND MARKINGS - EMERGENCY WARNING PLACARD INSTALLATION TO: Cessna Model 206, U206, U206A/TU206A, U206B/TU206B, U206C/TU206C, U206D/TU206D, U206E/TU206E, U206F/TU206F, and U206G/TU206G Aircraft Owner REASON To install the emergency exit warning placard on the cockpit instrument panel or another location directly visible while sitting in the pilots's seat. NOTE: The installation of the emergency exit warning placard may also be completed by a pilot with
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respect to local civil aviation regulations. NOTE: Pilots should be aware of the potential for impeding of the aft cargo door with the flaps extended. COMPLIANCE MANDATORY. This service document must be accomplished at the next 100-hour/Annual inspection or within 12 calendar months of publish, whichever occurs first. LABOR HOURS For planning purposes only: WORK PHASE LABOR-HOURS Modification As Required MATERIAL AVAILABILITY PART NUMBER AVAILABILITY COST S4645-16 * * * Please contact a Textron Aviation Authorized Service Facility for current cost and availability of parts listed in this service document. WARRANTY None NOTE: As a convenience, service documents are now available online to all our customers through a simple, free-of-charge registration process. If you would like to sign up, please visit the Customer Access link at support.txtav.com to register. SEB-11-05 November 25, 2024 Page 1 of 1 Textron Aviation Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800 This document contains technical data and is subject to U.S. export regulations. This information has been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E991 COPYRIGHT © 2024






