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CESSNA AIRCRAFT COMPANY 

MODEL 404 

MAINTENANCE MANUAL 

 

(f) 

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. 

(g) 

Install switch (23) and adjust as follows: 
1) 

With strut fully extended, 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 valve. Safety wire valve to strut. 

(i) 

Install filler plug (36) and packing (35) and safety wire. 

(j) 

Service strut. Refer to Service Main Gear Strut, Chapter 2. 

CAUTION: BEARINGS (15) HAVE A TEFLON LINING. IF LINING SHOWS DAMAGE 

OR IS WORN THROUGH REPLACE BEARING. 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 
 
 
 
 
 
 
4-10                                                 D2517-16-13 Temporary Revision Number 11 - Feb 15/2013 
Page 3A   
Jan /82 

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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