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CESSNA AIRCRAFT 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 Company

Sep 1/2006

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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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