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Forced

 

                            

Aeromotive

 

        

Technologies

 

DOCUMENT NO. 22001-05 

REV G, August 21, 2020 

PAGE 1 OF 11 

 

 

 

 

Instructions for Continued Airworthiness

 

 

FAA-STC SA10232SC

 

 

Supercharged O-470-L, -R, -S, and -U Engines Installed On  

Cessna Models 182B, C, D, E, F, G, H, J, K, L, M, N, P, Q and R Aircraft 

 

 
 

 
 
 
 
 
 
 

 
 

 

NOTICE 

This document must be referenced on Block 8 of FAA form 337 and added to the aircraft 
permanent record as required by 14 CFR Part 91, §91.417(a)(2)(vi) when the reference 
FAA-STC modification is accomplished on eligible aircraft.  This document complies with 
the  requirements  of  14  CFR  Part  23,  §23.1529,  in  accordance  with  14  CFR  Part  23, 
Appendix G. 

 

 
Model No.       

_________________    

 
Aircraft Serial No.   

__________________ 

 
Aircraft Registration No.  __________________

 

 

 

 
 

Summary of Contents for FAA-STC SA10232SC

Page 1: ...NOTICE This document must be referenced on Block 8 of FAA form 337 and added to the aircraft permanent record as required by 14 CFR Part 91 91 417 a 2 vi when the reference FAA STC modification is ac...

Page 2: ...Alignment marks for boost cutoff closed position changed to match installation instructions II 182 Parts list added Cessna 182 Q and R models and O 470 U engines added to header Cessna 182 Q and R mo...

Page 3: ...0 L R S and U Engines in Cessna Models 182B C D E F G H J K L M N Q and R Aircraft Instructions For Continued Airworthiness DOCUMENT NO 22001 05 REV G August 21 2020 PAGE 3 OF 11 F 10 30 2014 7 Oil ch...

Page 4: ...2 General Description 5 3 Control Operation Information Special Procedures 5 4 Servicing Information 5 5 Maintenance Instructions 6 6 Troubleshooting Instructions 8 7 Removal and Replacement Informat...

Page 5: ...1 13 revision 1 and P2006C3 13 change 3 or later approved revisions only in those areas listed herein 2 GENERAL DESCRIPTION STC SA10232SC installs supercharged Teledyne Continental Motors Model No O 4...

Page 6: ...r of the lower portion of the belt results in 25 inch of belt deflection Check again after 10 hours 5 2 REPLACEMENT OF ALTENATOR BELT 1 Loosen the two bolts securing the idler pulley and remove the be...

Page 7: ...ble nut The valve lever will be down approximately 45 to the supercharger duct and the butterfly valve will be in the full open position Check the operation of the Boost Cutoff control 5 4 OIL CHANGE...

Page 8: ...cement parts contact Forced Aeromotive at the following address Forced Aeromotive Technologies Inc 7161 S Peoria Street 18E Englewood Co 80112 www forcedaeromotive com 8 DIAGRAMS Refer to basic Cessna...

Page 9: ...ly push in the cockpit boost cutoff control and ensure the aft marks on the valve lever and housing are aligned 2 Fully pull the cockpit boost cutoff control and ensure the forward marks on the valve...

Page 10: ...nd U engines or Cessna 182E F G H J K L M N P Q and R aircraft from those which are listed in basic Cessna 182 Series Pilot Operating Handbook basic Teledyne Continental Engine Maintenance Manual or B...

Page 11: ...along with the revised pages The lower right hand corner of each revised page will reflect the revision letter That portion of text or an illustration which has been revised by the addition of or chan...

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