Forced Aeromotive Technologies FAA-STC SA10232SC User manual

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. __________________

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 2 OF 11
LOG OF REVISIONS
Revision
Number
Revision
Date
Approval Affected
Pa
g
es
Description of Revision
IR 03/05/2004 All New
A
B
C
08/06/2004
01/04/2005
06/17/2006
6
10 11 12
13
All
5, 8
9
10
13
11
13
5.3, para 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 models and
O-470-U engines added to
section 2 and 15.
O-470-U added to section 15,
engine operation
Kit # changed to match PMA
Cessna 182 Q and R models and
O-470-U engines added to
eligibility list
O-470-U pulley added
Heat shields added
Weldon fuel pump P/Ns A8164A
and A8164B added to parts list.
Editorial correction
Belt added
D 12/21/2008 5
10
13
Multi-groove belt replacement
Added item 5, 6, 18.
Added item 103, 104.
E 2/27/2013 10-13 Removed kit list.

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 3 OF 11
F 10/30/2014 7 Oil change, self oiled
superchargers
G 8/21/2020 6 Belt tension settings

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 4 OF 11
Table of Contents
1. Introduction .......................................................................................................... 5
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 Information ............................................................... 8
8. Diagrams .............................................................................................................. 8
9. Special Inspection Requirements ......................................................................... 8
10. Application of Special Treatments ........................................................................ 9
11. Data ..................................................................................................................... 9
12. Special Tools ........................................................................................................ 9
13. Additional Information for Commuter Category Aircraft ........................................ 9
14. Recommended Overhaul Period .......................................................................... 9
15. Airworthiness Limitations .................................................................................... 10
16. Revision ............................................................................................................. 11
17. Assistance .......................................................................................................... 11

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 5 OF 11
1. INTRODUCTION
This document outlines the compliance with 14 CFR 23.1529 “Instructions for
Continued Airworthiness” for Forced Aeromotive Technologies, Inc.
Supplemental Type Certificate (STC) No. SA10232C.
NOTICE:
Section 15, titled “Airworthiness Limitations” is FAA approved and specifies
maintenance required under 43.16 and 91.403 of the Federal Aviation
Regulations unless an alternative program has been FAA approved. To remain
in compliance with the STC, the aircraft shall be maintained in accordance with
these limitations.
This document supplements or supersedes the Cessna “Service Manual”, part
numbers D138-1-13, revision 1, D637-1-13, 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-470-L, -R, -S, or -U engines in the appropriate Cessna Models 182E, F, G, H,
J, K, L, M, N, P, Q and R aircraft. This STC also installs dual electrical fuel
pumps, fuel pump circuit breakers and switches, a fuel pressure gage, low fuel
pressure and alternator inop annunciators, a cockpit controlled boost cutoff push-
pull cable, and various placards.
This STC cannot be incorporated unless STC SA10233SC has been performed
on either the appropriate O-470-L, -R, -S, or -U engine which installs the belt-
driven Vortech VS-1 supercharger on the engine, alters the inductions system for
the supercharger, and installs a boost cutoff control valve.
3. CONTROL, OPERATION INFORMATION, SPECIAL PROCEDURES
Refer to basic Cessna Maintenance or Service Manual, basic Pilot’s Operating
Handbook and Airplane Flight Manual Supplement 22001.
4. SERVICING INFORMATION
Refer to basic Cessna Maintenance or Service Manual.