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Forced

   

Aeromotive

   

Technologies

 

 

FAA-STC SA10232SC 

Supercharged O-470-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 6 OF 11 

 

5.  MAINTENANCE INSTRUCTIONS 

 

Refer to basic Cessna 182 Series Maintenance Manual for information other than 
what is provided below. 

 
5.1  REPLACEMENT OF SUPERCHARGER BELT  

 
1.  Loosen the two bolts securing the idler pulley and remove the belt.  
2.  After placing the new belt on the pulleys, adjust the tension by pressing the 

idler pulley down against the belt and tightening the adjustment bolts. Tighten 
a new belt until a 12-14 pound pull on the center of the lower portion of the 
belt results in a .25 inch of belt deflection.  

3.  After 2 flight hours re-check belt tension. Tighten the belt until a 10-11 pound. 

pull on the center of the lower portion of the belt results in a .25 inch of belt 
deflection.  

4.  For aircraft equipped with a multi-v belt, after 2 hours, re-tension the belt until 

a 10-11 pound pull on the center 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  belt  from  the 

supercharger.  

2.  Remove  the  SCAT  connected  to  the  supercharger  airbox  and  remove  the 

airbox  from  the  supercharger  by  loosening  the  clamp  and  sliding  the  airbox 
forward. The carburetor heat control can remain connected.  

3.  Disconnect  the  oil  line  to  the  supercharger  at  its  connection  to  the 

supercharger.  Loosen  the  upper  clamp  on  the  supercharger  oil  drain  hose 
located at the rear of the supercharger and behind the alternator. 

4.  Remove the two nuts and bolts at the upper rear of the supercharger mount 

that  connect  the  mount  to  the  L-shaped  bracket  which  is  bolted  to  the  left 
accessory pad. 

5.  Loosen  the  one  bolt  and  remove  the  two  metal  stop  nuts  that  hold  the 

supercharger to the crankcase. 

6.  Remove the supercharger by sliding it out from the engine and up, pulling the 

oil drain from the oil drain hose (the clamp loosened in step 3). 

7.  Replace  the  alternator  belt  with  appropriate  belts  and  using  procedures 

outlined in the basic Cessna Maintenance or Service Manual. 

8.  Replacement of the supercharger is the reverse of the removal procedure. 

 
 

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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