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Multi-engine

SERVICE LETTER

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: [email protected]

COPYRIGHT © 2013

Summary of Contents for Cessna 404

Page 1: ...es 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 0...

Page 2: ......

Page 3: ...llow Supplemental Inspection Document SID Section III 32 10 07 Main Landing Gear Trailing Link Section 4 10 Main Landing Gear COMPLIANCE INFORMATIONAL This service letter is for informational purposes...

Page 4: ......

Page 5: ...THIS TEMPORARY REVISION 1 For Paper Publications file this cover sheet behind the publication s title page to identify inclusion of the temporary revision in the manual Insert the new pages in the pu...

Page 6: ...Cessna Aircraft Company THIS PAGE INTENTIONALLY LEFT BLANK...

Page 7: ...Crack Size Main landing gear trailing link 0 10 Inch 2 54 mm 6 Disassembly and Assembly Procedures A Disassembly Procedures 1 Remove the trailing link Refer to Section 4 10 Main Landing Gear for main...

Page 8: ...le surface must not have dents dings or corrosion in more than three locations 2 The dents dings and corrosion can be blended and refinished if the maximum depth of the penetration is not more than 0...

Page 9: ...COMPANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT Main Landing Gear Trailing Link Figure 1 Sheet 1 D2517 16 13 Temporary Revision Number 11 Feb 15 2013 32 10 07 Page 3 Section III Cessna Aircraft Com...

Page 10: ...COMPANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT Main Landing Gear Shock Strut Figure 2 Sheet 1 D2517 16 13 Temporary Revision Number 11 Feb 15 2013 32 10 07 Page 4 Section III Cessna Aircraft Comp...

Page 11: ...RAFT COMPANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT Axle Main Landing Gear Figure 3 Sheet 1 D2517 16 13 Temporary Revision Number 11 Feb 15 2013 32 10 07 Page 5 Section III Cessna Aircraft Company...

Page 12: ...ANY MODEL 404 SUPPLEMENTAL INSPECTION DOCUMENT Trailing Link Assembly Main Landing Gear Figure 4 Sheet 1 D2517 16 13 Temporary Revision Number 11 Feb 15 2013 32 10 07 Page 6 Section III Cessna Aircraf...

Page 13: ...from barrel assembly and piston assembly using an arbor press j If bearings 15 and bushings 18 are to be replaced press bearings and bushings out of the trunnion by using an arbor press k If bushings...

Page 14: ...d screw switch in until actuation of switch occurs then make two complete revolutions past actuation point 2 Secure switch in this location by tightening locknut Safety wire locknut h Install air valv...

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 16: ......

Page 17: ...letter is for informational purposes only LABOR HOURS Not applicable MATERIAL AVAILABILITY Not applicable WARRANTY Not applicable Please contact a Cessna Service Facility for detailed information NOTE...

Page 18: ......

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