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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

16

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.

SECTION

PAGE

SID Section III - 32-10-07

1 Thru 6

Section 4-10

3 Thru 3B

REASON FOR TEMPORARY REVISION

1.

To add allowable damage information and assembly/disassembly procedures in Supplemental Inspection
Document Section III 32-10-07, Main Landing Gear Trailing Link.

2.

To revise Section 4-10 Main Landing Gear.

FILING INSTRUCTIONS FOR 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 publication at the appropriate locations
and remove and discard the superseded pages.

2.

For CD publications, mark the temporary revision part number on the CD label with permanent red
marker. This will be a visual identifier that the temporary revision must be referenced when the content
of the CD is being used. Temporary revisions should be collected and maintained in a notebook or binder
near the CD library for quick reference.

EXPORT COMPLIANCE

1.

This publication 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

© Cessna Aircraft Company

Содержание Cessna 404

Страница 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...

Страница 2: ......

Страница 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...

Страница 4: ......

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 16: ......

Страница 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...

Страница 18: ......

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