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SERVICE LETTER
Multi-engine
MEL-05-01
REVISION TRANSMITTAL
TO: Cessna Distributors, Cessna Service Facilities, and affected Owners of Record
SUBJECT: Cessna Conquest Service Letter MEL-05-01 Revision 1: Notification of Release of Temporary
Revision Number 11 for the Model 404 Service Manual.
REASON
To provide corrected copies of the attached temporary revision.
Miscellaneous changes as required.
Please replace any copy of MEL-05-01 with the attached copy of MEL-05-01 Revision 1, which is printed in
its entirety.
NOTE: You must discard the temporary revision transmitted by MEL-05-01 and replace it with the temporary
revision transmitted by MEL-05-01 Revision 1.
LOG OF REVISIONS
Page No.
Date
1
April 25, 2013
Original Issue - February 19, 2013
MEL-05-01
Revision 1 - April 25, 2013
Page 1 of 1
Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271,
Email: customercare@cessna.textron.com
COPYRIGHT © 2013

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Summary of Contents for Textron Cessna 404

  • Page 1 April 25, 2013 Original Issue - February 19, 2013 MEL-05-01 Revision 1 - April 25, 2013 Page 1 of 1 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271, Email: customercare@cessna.textron.com COPYRIGHT © 2013...
  • Page 3 Page 1 of 1 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271, Email: customercare@cessna.textron.com 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.
  • Page 5 TEMPORARY REVISION NUMBER 11 DATED 15 FEBRUARY 2013 MANUAL TITLE Model 404 Service Manual MANUAL NUMBER - PAPER COPY D2517-16-13 TEMPORARY REVISION NUMBER D2517-16TR11 MANUAL DATE 1 August 1976 REVISION NUMBER DATE 1 September 2006 This Temporary Revision consists of the following pages, which affect and replace existing pages in the paper copy manual and supersede aerofiche information.
  • Page 6 (THIS PAGE INTENTIONALLY LEFT BLANK) © Cessna Aircraft Company...
  • Page 7 CESSNA AIRCRAFT COMPANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT SUPPLEMENTAL INSPECTION NUMBER: 32-10-07 Title Main Landing Gear Trailing Link Effectivity Airplanes 404-0001 thru 404-0859. Inspection Compliance INITIAL REPEAT 10,000 Landings or 15 Years 2,000 Landings or 4 Years Purpose Detailed inspection of the main landing gear trailing link for cracks due to fatigue, overload, and corrosion.
  • Page 8 CESSNA AIRCRAFT COMPANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT Inspection Method Visual/Magnetic Particle. Repair/Modification Replace the main landing gear trailing link if a crack is found. Refer to the Service Manual. Allowable damage on Upper Machined Barrel and Lower Machined Barrel. Refer to Figure 2. The upper piston surface must not have dents, dings or corrosion, in more than five locations.
  • Page 9 CESSNA AIRCRAFT COMPANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT Main Landing Gear -Trailing Link Figure 1 (Sheet 1) 32-10-07 D2517-16-13 Temporary Revision Number 11 - Feb 15/2013 Page 3 Section III Sep 1/2006 © Cessna Aircraft Company...
  • Page 10 CESSNA AIRCRAFT COMPANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT Main Landing Gear Shock Strut Figure 2 (Sheet 1) 32-10-07 D2517-16-13 Temporary Revision Number 11 - Feb 15/2013 Page 4 Section III Sep 1/2006 © Cessna Aircraft Company...
  • Page 11 CESSNA AIRCRAFT COMPANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT Axle Main Landing Gear Figure 3 (Sheet 1) 32-10-07 D2517-16-13 Temporary Revision Number 11 - Feb 15/2013 Page 5 Section III Sep 1/2006 © Cessna Aircraft Company...
  • Page 12 CESSNA AIRCRAFT COMPANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT Trailing Link Assembly - Main Landing Gear Figure 4 (Sheet 1) 32-10-07 D2517-16-13 Temporary Revision Number 11 - Feb 15/2013 Page 6 Section III Sep 1/2006 © Cessna Aircraft Company...
  • Page 13 CESSNA AIRCRAFT COMPANY MODEL 404 MAINTENANCE MANUAL   (3) Remove fork (12) from trunnion (5) by removing roll pin (14) from fork pin (16), and remove nut (10), washers and fork pin from trunnion. Remove spacer (13) from fork. (4) Remove roller (17) from fork pin (16) by removing nut and bolt. NOTE: If it is necessary to remove the axle from the trailing link assembly.
  • Page 14 CESSNA AIRCRAFT COMPANY MODEL 404 MAINTENANCE MANUAL   Insert piston assembly into barrel. Slide spacer (32) into barrel bearing (31) scraper ring and retainer scraper over piston. Secure bearing in barrel with retainer ring (30). Safety wire retainer ring. Install switch (23) and adjust as follows: With strut fully extended, screw switch in until actuation of switch occurs;...
  • Page 15 CESSNA AIRCRAFT COMPANY MODEL 404 MAINTENANCE MANUAL   (THIS PAGE INTENTIONALLY LEFT BLANK)  D2517-16-13 Temporary Revision Number 11 - Feb 15/2013 4-10 Page 3B Jan /82...
  • Page 17: Warranty

    Page 1 of 1 Cessna Aircraft Company, Cessna Customer Service, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-5800, Fax 1-316-517-7271, Email: customercare@cessna.textron.com 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.