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.

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.

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 7 OF 11
5.3 ADJUSTMENT OF BOOST CUT-OFF CABLE
1. Accurate cable adjustment is necessary for proper supercharger
performance.
2. To adjust the cable for proper operation, rotate the valve lever upward (the
valve is now closing) aligning the marks on the valve shaft and the valve
housing so that the mark on the shaft is rotated two mark widths past the
mark on the housing. Notice that the lever is slightly above a 90 angle
(perpendicular) to the intake duct. Tighten the clamp on the cable housing so
that the valve lever will touch the cable housing and stop its upward
movement at this point.
3. After making sure that the Boost Cutoff control in the cockpit is in the full
forward position, loosen the cable nut and press the lever downward and
align the marks on the valve shaft and the shaft housing and tighten the cable
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, SELF LUBRICATED SUPERCHARGERS
Oil should be changed every 100 hours. Oil level should be checked every 50
hours. Self oiling superchargers can be identified by the lack of oil lines going
into and out of the supercharger and by the presence of the oil dipstick at the top
of the supercharger for checking the oil level.
Checking the oil level:
1. Ensure that the .06” copper washer is located on the dipstick base.
2. Thread the clean dipstick into the unit until is seats.
3. Once the dipstick has seated, remove the dipstick from the unit. Fluid
should register in the crosshatched area on the dipstick.
4. DO NOT OVERFILL. Drain excess fluid from the unit if it is above the
maximum level on the dipstick.
Changing the oil:
Empty the supercharger of oil by opening the drain at the bottom. When
completely drained refill the supercharger with up to 4 ounces of oil. Verify
proper oil level by using the dipstick. Do not overfill. USE ONLY
APPROVED OIL SUPPLIED BY
Forced Aeromotive Technologies, Inc.
7161 S. Peoria Street 18E
Englewood, CO 80112
www.forcedaeromotive.com

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 8 OF 11
6. TROUBLESHOOTING INSTRUCTIONS
For troubleshooting guidance contact Forced Aeromotive Technologies, Inc. for
assistance.
Forced Aeromotive Technologies, Inc.
7161 S. Peoria Street 18E
Englewood, CO 80112
www.forcedaeromotive.com
7. REMOVAL AND REPLACEMENT INFORMATION
Remove and replace as specified in Forced Aeromotive Installation Drawing II-
182, Rev. C, dated 02/24/04 or later FAA approved revision. For replacement
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 182 Series Maintenance or Service Manual and Forced
Aeromotive Installation Drawing II-182, Rev. C, dated 02/24/04 or later FAA
approved revision.
9. SPECIAL INSPECTION REQUIREMENTS
Conduct routine inspections on the engines, airframe, and propeller in
accordance with appropriate basic Teledyne Continental Motors Engine
Maintenance Manual, basic Cessna 182 Series Maintenance Manual, and basic
Hartzell Propeller Maintenance Manual except as noted below.
9.1 INSPECTION OF SUPERCHARGER AND ALTERNATOR BELTS
For every 100 flight hours, conduct routine inspections on the alternator and
supercharger belts for wear.
9.2 INSPECTION OF SUPERCHARGER OIL NOZZLE

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 9 OF 11
Ateachannualinspection,removethesuperchargeroilinletlineandremovetheoil
nozzle.Cleanthenozzlewithcompressedairandreplaceitandreconnecttheoilline.
9.3 INSPECTION OF BOOST CUT-OFF CONTROL CABLE RIGGING
Ateachannualinspection,ensuretheboostcutoffcableandvalveareriggedaccording
tothefollowingsteps.

1.Fully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
leverandhousingarealigned.

If marks are not aligned, adjust boost cutoff control cable according to Section
5.3 of this document.
There are no mandatory replacement times on any new components.
10. APPLICATION OF SPECIAL TREATMENTS
None
11. DATA
None
12. SPECIAL TOOLS
None Required
13. ADDITIONAL INFORMATION FOR COMMUTER CATEGORY AIRCRAFT
Not Applicable
14. RECOMMENDED OVERHAUL PERIOD
Engine: 1400 Hours after STC installation, or next required overhaul per
Continental Motors O-470 series Overhaul Manual, P/N X30586A, which ever
comes first.
Supercharger: 2000 Hours after STC installation

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 10 OF 11
15. AIRWORTHINESS LIMITATIONS
NOTICE:
This section 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.
There are no changes to the airworthiness limitations of the O-470-L, -R, -S, and
–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 Basic Cessna 182
Series Maintenance Manual except for the following:
ENGINE OPERATION
Manifold Pressure ............................................................................ 28 inHg
Propeller Speed ........................ (O-470-L, -R, -S engines)…..….2600 RPM
.............................................................. (O-470-U engines)……..2400 RPM
FUEL
Minimum Fuel Grade .............................................................. 100LL (Blue)
INSTRUMENT MARKINGS
Manifold Pressure Gage:
Red-Line ........................................................................................... 28 inHg
Normal Operating Range (Green-Arc) ........................................ 15-23 inHg
Fuel Pressure Gage:
Warning (Red-Arc) ....................................................................... 0-1.5 psig
Cautionary (Yellow-Arc) ........................................................... 1.5-4.0 psig
Normal (Green Arc) ................................................................... 4.0-7.0 psig
There are no changes to the airworthiness limitations of the propeller from those
which are listed in the basic Cessna 182 Series Maintenance Manual or basic
Hartzell Propeller Maintenance Manual.
16. REVISION

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 11 OF 11
Each time this ICA is revised or reissued, the revised ICA will be distributed to
operators using a Service Letter/Bulletin by Forced Aeromotive Technologies.
This revision will include a new Log of Revisions page 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 change in, information is denoted by a solid revision bar located
adjacent to the area of change, and placed along the outside margin of a page.
Revision bars show only information changed within latest revision.
17. ASSISTANCE
For assistance with ICA issues not addressed herein, contact Forced Aeromotive
Technologies at the following address or phone number.
Forced Aeromotive Technologies, Inc.
7161 S. Peoria Street 18E
Englewood, Co 80112
www.forcedaeromotive.com
END