# TCDS E-269: Continental Aerospace Technologies, Inc.

- Type: Type certificate data sheet
- Status: Current
- Holder: Continental Aerospace Technologies, Inc.
- Revision: 18
- Revised: September 19, 2022
- Product: Engine
- Certification basis: Part 1, CAR 13
- Registered aircraft: 12, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/39/9e/399eff1815d377f282abdf82816a7d21c5a1a21cd5e0cffb1f2d028917f48d26
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D918D45BC84AD183862588C60069C506.0001
- Page: https://openairdocs.org/tcds/E-269

## Models (8)

As the data sheet lists them.

- O-470-11
- O-470-15
- O-470-11B-CI
- O-470-13
- O-470-11-CI
- O-470-11B
- O-470-4
- O-470-13A

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
E-269 
Revision 18 
CONTINENTAL AEROSPACE TECHNOLOGIES, INC. 
O-470-4, 
O-470-11, 11B, 11-CI (see NOTE 5), 11B-CI 
O-470-13, O-470-13A, O-470-15 
 
September 19, 2022 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
 
TYPE CERTIFICATE DATA SHEET NO. E-269 
 
Engines of models described herein conforming with this data sheet (which is part of type certificate No. 269) and other approved 
data on file with the Federal Aviation Administration, meet the minimum standards for use in certificated aircraft in accordance 
with pertinent aircraft data sheets and applicable portions of the Civil Air Regulations provided they are installed, operated and 
maintained as prescribed by the approved manufacturer's manuals and other approved instructions. 
 
Type Certificate Holder Continental Aerospace Technologies, Inc. (Continental®) 
2039 South Broad St. 
Mobile, Alabama 36615 
 
Type Certificate Holder Record Continental Motors, Inc. 
Company name change January 1, 2020 (Continental Aerospace Technologies, Inc.) 
 
Teledyne Continental Motors 
Ownership & name change as of April 19, 2011 (Continental Motors, Inc.) 
 
Model O-470-11, -11B O-470-13, -13A O-470-4 O-470-15 
Type 
 
Rating, ICAO or ARDC 
standard atmosphere 
Max. continuous hp., 
rpm, full throttle, at 
sea level pressure altitude 
 
Takeoff hp., 5 min., 
rpm, full throttle, at 
sea level pressure altitude 
 
Fuel (min. grade) aviation gasoline 
 
 
Lubricating oil 
Ambient air temperature 
Above 40° F. 
Below 40° F. 
Bore and stroke, in. 
Displacement, cu. in. 
Compression ratio 
Weight (dry), lb. 
6HOA 
 
 
190-2300 
 
 
213-2600 
 
 
80/87, ASTM D7547 
(UL91), ASTM 
D7547 (UL94) 
 
 
Oil grade 
SAE 50 
SAE 30 
 
5.00 x 4.00 
 
471 
 
7:1 
 
391 
- - - 
 
 
225-2600 
 
 
225-2600 
 
 
- - - 
 
 
 
 
- - - 
- - - 
 
- - - 
 
- - - 
- - - 
415 
- - - 
 
 
- - - 
 
 
- - - 
 
 
- - - 
 
 
 
 
- - - 
- - - 
 
- - - 
 
- - - 
 
- - - 
 
- - - 
- - - 
 
 
190-2300 
 
 
213-2600 
 
 
- - - 
 
 
 
 
- - - 
- - - 
 
- - - 
 
- - - 
- - - 
405 
 
 
 
 
Page No. 1 2 3 
Rev. No. 18 17 17

E-269 Page 2 
 
 
Model (Continued) O-470-11, -11B O-470-13, -13A O-470-4 O-470-15 
C.G. location (with starter, generator 
and fuel pump) 
Fwd. or rear face, engine 
crankcase, in. 
Below crankshaft, centerline, in. 
Beside crankshaft, centerline 
toward 1-3-5 side, in. 
 
Propeller shaft, SAE No. 
 
 
 
 
Carburetion 
 
 
 
Ignition, dual magnetos 
 
 
Timing, °BTC 
Spark plugs 
Oil sump capacity, qt. 
 
NOTES 
 
8.8 
 
.8 

 
4 flange 
 
 
 
 
Bendix-Stromberg 
Model PS-5C 
(Continental No. 
531857) 
 
Scintilla S6LN-21 
(Continental NO. 
531676) 
 
Right 26, Left 26 
 
(See NOTE 6) 
 
10; 7 usable 
 
1, 2, 3, 4, 5, 6 
 
9.8 
 
.2 
.1 
 
 
Special integral 
flange 4-7/8 in. 
O.D. with six ½ in. 
bolt holes in 4 in. 
dia. circle 
 
- - - 
 
 
 
Scintilla S6LN-23 
(Continental No. 
533173) 
 
- - - 
 
- - - 
 
Dry 
 
1, 2, 3, 4, 6 
 
- - - 
 
- - - 
- - - 
 
 
- - - 
 
 
 
 
Bendix-Stromberg 
Model PS-5CD 
(Continental No. 
538685) 
 
- - - 
 
 
- - - 
 
- - - 
 
- - - 
 
1, 2, 3, 4, 6 
 
- - - 
 
- - - 
- - - 
 
 
- - - 
 
 
 
 
Bendix-Stromberg 
Model PS-5C 
(Continental No. 
625098) 
 
Scintilla S7LN-21 
(Continental No. 
531676) 
 
- - - 
 
- - - 
 
10; 7 usable 
 
1, 2, 3, 4, 6 
“- - -“ indicates “same as preceding model” 
“” indicates “does not apply” 
 
Certification Basis Part 13 of the Civil Air Regulations effective August 1, 1949 as amended by 13-1. 
Type Certificate No. 269 issued January 19, 1951 
Application for Type Certificate dated October 23, 1950 
 
Production Basis P.C. 7 (All models except O-470-11B and -11B-C1) 
P.C. 508 (All models with “R” suffix on serial number except O-470-11B and -11B-C1) 
 
NOTE 1. Maximum permissible temperatures: 
Cylinder head O-470-11, -11B, -15 
325° F. (spark plug gasket) 
450° F. (bayonet thermocouple downdraft cooling) 
O-470-4, -13, -13A 
465°F. (bayonet thermocouple downdraft cooling) 
 
Cylinder barrel 315° F. 
Oil inlet 225° F. 
 
NOTE 2. O-470-11, -11B, -13, -13A, -4, -15 O-470-11-CI, -11B-CI 
Fuel inlet pressure limits: Fuel inlet pressure limits: 
9 to 15 p.s.i.g.  Min. minus 2.25 p.s.i.g. 
Max. plus 10 p.s.i.g. 
Oil pressure limits: Oil pressure limits: 
30 to 60 p.s.i.a. 30 to 60 p.s.i.a.

E-269 Page 3 
 
 
NOTE 3. The following accessory drive or mounting provisions are available: 
 
 
Original 
Accessory 
 
Type 
 
Dwg. No. 
Direction 
of 
Rotation* 
Speed Ratio 
to 
Crankshaft 
Maximum Torque 
(in.-lb.) 
Continuous Static 
Max. Overhang 
Moment 
(in.-lb.) 
Starter XIV-A AND 20004 C 1.0  3600 300 
Generator        
(O-470-11 -11B, -15 XII-A AND 20002 C 2.37 500 2200 400 
(O-470-13, -13A, -4) XII-A AND 20002 C 3.094 350 1000 400 
Fuel Pump XIII-A AND 20003 CC .94 25 450 
Tachometer XV-A AND 20005 CC .50 7 50 
Fluid P Pump X AND 20000 C 1.43 100 800 25 
Fluid P Pump XI-A AND 20001 C 1.45 250 1650 75 
Spare XV-A AND 20005 CC .50 7 50 
Governor XX AND 20010 C 1.03 125 825 
*C - Clockwise viewing drive pad; 
CC - Counterclockwise 
 
NOTE 4. Model O-470-11B is identical to the O-470-11 except that it incorporates the model O-470-15 cylinder and 
piston assemblies. 
 
Model O-470-11 incorporates two 6th order dampers. 
 
Model O-470-13A is identical to the O-470-13 except that an additional tachometer drive is provided through 
the camshaft gear and incorporates one 5th and one 6th order crankshaft damper. 
 
Model O-470-15 is identical to the O-470-11 except that a four 6th order damper crankshaft is used with the 
same size propeller flange specified on the model O-470-13. Model O-470-15 incorporates propeller control 
provisions. Also, revised engine mount brackets and long skirt pistons are used with this engine. 
 
O-470-13 engines incorporating crankshaft with one 5th and one 6th order dampers have the numeral 5 
stamped on the outer circumference of the crankshaft propeller flange. O-470-13 engines with two 6th order 
dampers have no numeral stamped on the flange. 
 
Model O-470-4 which was previously designated as O-470-13B is identical to the Model O-470-13A except 
for the carburetor. 
 
NOTE 5. Models O-470-11 and -11B are eligible for incorporation of Continental continuous flow fuel injection 
equipment No. 5843 replacing carburetion system, with a weight increase of approximately 3 lb. When this 
modification is accomplished the suffix letters “CI” are to be added to the model designation. 
 
NOTE 6. The following spark plugs and/or those listed in Section 6-4.9 of the latest revision of M-0, Standard Practice 
Maintenance Manual, are approved on this engine: 
 
AC: SR83P, HSR83P, S88D, HS88, HSR88, SR88D 
Auto Lite:  SH2M, SH15, SH15R, SH20, SH20A, SH200A 
BG: RB485S, 706S, 706SR, 919SR, 919SR5, RB955S, RB963S, HRB963S 
Champion RC26S, C27S, REM38P, RHM38P, RED39N, REM39N, RHD39N, RHM39N, RED40E, 
REM40E, RHM40E, ED41N, EM41N, EM42E 
Red Seal: SE190, SJ190, SE230, SJ230 
 
NOTE 7. Model O-470-11 engines which have been modified in accordance with U.S. Army Aviation and Surface 
Material Command Work Requirement No. WR-55-2810-112-B(1) issued 5 April 1963 and revised 13 
February 1964, and designated Model O-470-11A, are considered to be equivalent to and interchangeable 
with Model O-470-11. 
 
 
 
...END...
```

## ADs (23, in force first)

- [AD 2023-17-04](https://openairdocs.org/ad/2023-17-04): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Oct 26, 2023
- [AD 2010-11-04](https://openairdocs.org/ad/2010-11-04): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 190 more. Effective Jun 16, 2010
- [AD 2000-23-21](https://openairdocs.org/ad/2000-23-21): Crankshaft · Continental Motors IO-360-A, IO-360-AB, IO-360-B and 164 more. Effective Dec 12, 2000
- [AD 99-19-01](https://openairdocs.org/ad/99-19-01): No. 2 and No. 5 Crankshaft Inspections · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 127 more. Effective Sep 30, 1999
- [AD 98-17-11](https://openairdocs.org/ad/98-17-11): Crankshafts · Continental Motors A-65-3, A-65-8, A75-8 and 90 more. Effective Oct 19, 1998
- [AD 97-21-02](https://openairdocs.org/ad/97-21-02): Cylinders · Continental Motors E165-2, E165-3, E165-4 and 61 more. Effective Oct 27, 1997
- [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996
- [AD 93-08-17](https://openairdocs.org/ad/93-08-17): Oil Pick-Up Tube · Continental Motors IO-470-A, IO-470-C, IO-470-D and 104 more. Effective Aug 23, 1993
- [AD 93-10-02](https://openairdocs.org/ad/93-10-02): Missing Cylinder Valve Retainer Key · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 180 more. Effective Aug 12, 1993
- [AD 91-19-03](https://openairdocs.org/ad/91-19-03): Oil Filter · Continental Motors 6-285-A, 6-285-B, 6-285-BA and 169 more. Effective Sep 29, 1991
- [AD 89-04-02](https://openairdocs.org/ad/89-04-02): Carburetors · Continental Motors O-470-11, O-470-11-CI, O-470-11B and 175 more. Effective Mar 8, 1989
- [AD 88-03-06](https://openairdocs.org/ad/88-03-06): Oil Filter · Continental Motors GTSIO-520-C, GTSIO-520-D, GTSIO-520-E and 155 more. Effective Apr 15, 1988
- [AD 81-16-05](https://openairdocs.org/ad/81-16-05): Magnetos · Lycoming Engines AEIO-320-E1B, AEIO-320-E2B, AEIO-360-B1G6 and 234 more. Effective Aug 6, 1981
- [AD 63-15-01](https://openairdocs.org/ad/63-15-01): Exhaust Valves · Continental Motors E165-2, E165-3, E165-4 and 41 more. Effective Dec 31, 1969
- [AD 67-01-04](https://openairdocs.org/ad/67-01-04): Oil Filters · Full flow oil filter (Superior Flow STC SA401SW or 2 others). Effective Jan 2, 1967
- [AD 63-22-03](https://openairdocs.org/ad/63-22-03): Carburetors · Continental Motors GO-300-A, GO-300-B, GO-300-C and 143 more. Effective Dec 2, 1963
- [AD 56-06-01](https://openairdocs.org/ad/56-06-01): Piston Pin Assembly · Continental Motors E165-2, E165-3, E165-4 and 41 more
- [AD 2022-04-04](https://openairdocs.org/ad/2022-04-04) (historical): Reciprocating Engine Oil System · F & M Enterprises' Model C6LC, C6LC-S or C6LC-L oil filter… (Stratus Tool Technologies STC SE09356SC or 2 others). Effective Mar 29, 2022
- [AD 2000-08-51](https://openairdocs.org/ad/2000-08-51) (historical): Crankshaft · Teledyne Continental Motors IO-360-A, IO-360-AB, IO-360-B and 158 more
- [AD 2009-24-51](https://openairdocs.org/ad/2009-24-51) (historical): Hydraulic lifters · Teledyne Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 156 more
- [AD 2009-24-52](https://openairdocs.org/ad/2009-24-52) (historical): Hydraulic lifters · Continental Motors FSO-470-A, GIO-470-A, GTSIO-520-C and 192 more
- [AD 97-15-01](https://openairdocs.org/ad/97-15-01) (historical): Pistons · Teledyne Continental Motors E165-2, E165-3, E165-4 and 61 more
- [AD 99-09-17](https://openairdocs.org/ad/99-09-17) (historical): Crankshaft · Teledyne Continental Motors IO-470-A, IO-470-C, IO-470-D and 114 more

## Registered aircraft by registry model (OpenAirDocs)

- [Continental 0-470-11](https://openairdocs.org/engine/continental-0-470-11): 4 aircraft (registry code 17364)
- [Continental O-470-13A](https://openairdocs.org/engine/continental-o-470-13a): 3 aircraft (registry code 17405)
- [Continental 0-470-15](https://openairdocs.org/engine/continental-0-470-15): 2 aircraft (registry code 17369)
- [Continental 0-470-4](https://openairdocs.org/engine/continental-0-470-4): 2 aircraft (registry code 17368)
- [Continental 0-470-13A](https://openairdocs.org/engine/continental-0-470-13a): 1 aircraft (registry code 17367)
- [Continental 0-470-11B](https://openairdocs.org/engine/continental-0-470-11b): 0 aircraft (registry code 17365)
- [Continental 0-470-13](https://openairdocs.org/engine/continental-0-470-13): 0 aircraft (registry code 17366)

## STCs approved under this data sheet (33)

- [STC SE04651CH](https://openairdocs.org/stc/SE04651CH): To allow use of l00R grade aviation fuel meeting Swift Fuel, LLC specification SPEC-l00R-22. Swift Fuels LLC
- [STC SE208SO](https://openairdocs.org/stc/SE208SO): Installation of ice indicator in the carburetor.. LegacySTC.com
- [STC SE04349CH](https://openairdocs.org/stc/SE04349CH): Installation of SureFly electronic ignition. SureFly Partners Ltd.
- [STC SE02352CH](https://openairdocs.org/stc/SE02352CH): Installation of Challenger cleanable oil filter assembly. Challenger Aviation Products Inc.
- [STC SE03309CH](https://openairdocs.org/stc/SE03309CH): Installation of Engine Preheat Kit, p/n TSP6CYL-2927-115 for 115 volt application. Hartzell Propeller Inc.
- [STC SE04577CH](https://openairdocs.org/stc/SE04577CH): Install an electronic engine ignition system. Electroair Acquisition Corp
- [STC SE01966WI](https://openairdocs.org/stc/SE01966WI): Use of GAMI G100UL High Octane Unleaded Avgas in spark ignition piston aircraft engines. General Aviation Modifications Inc.
- [STC SE10348SC](https://openairdocs.org/stc/SE10348SC): This STC application is to allow replacement of the existing oil filter screen assembly. Stratus Tool Technologies LLC
- [STC SE26WE](https://openairdocs.org/stc/SE26WE): Piston ring 250000, 250000+2W and250000+10W on Continental E Series piston 534895, O-470 piston 534895, 626992 and 537883 and IO-470 piston534895.. Continental Motors, Inc.
- [STC SE34WE](https://openairdocs.org/stc/SE34WE): Installation of Electro-Coatings, Inc., piston rings on Continental pistons.. Continental Motors, Inc.
- [STC SE8776SW](https://openairdocs.org/stc/SE8776SW): Installation of coated cylinders and piston rings.. Continental Motors, Inc.
- [STC SE976SW](https://openairdocs.org/stc/SE976SW): General modification to engine changing O-470-11 to O-470-11-13-15.. Stephen Noyes
- [STC SE699SW](https://openairdocs.org/stc/SE699SW): Modification of 0-470-13 engine to 0-470-13-11 in Cessna 305A aircraft.. Stephen Noyes
- [STC SE1780NM](https://openairdocs.org/stc/SE1780NM): Installation of Precise Flight standby vacuum system (SVS III).. Precise Flight Inc
- [STC SE01943CH](https://openairdocs.org/stc/SE01943CH): Add the following approved fuels:  unleaded automotive gasoline 87 minimum antiknock index, per ASTM Specification D-439 or D-4814 of any volatility class, A through E, or 82UL AVGAS per ASTM D-6227.. Experimental Aircraft Association Inc.
- [STC SE693GL](https://openairdocs.org/stc/SE693GL): Superseded by STC SE01943CH.  Add the following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index.. EAA Aviation Foundation
- [STC SE5743NM](https://openairdocs.org/stc/SE5743NM): Intallation of adapter for externally mounted oil filter.. Aviation Development Corporation
- [STC SE264SW](https://openairdocs.org/stc/SE264SW): Marvel-Schebler MA-4-5 carburetor.. Air Repair Inc
- [STC SE09513SC](https://openairdocs.org/stc/SE09513SC): Installation and usage of Exxon 20W50 Multigrade aircraft engine oil conforming to Exxon Oil Formulation WS-3013.. Exxon Company USA
- [STC SE09319SC](https://openairdocs.org/stc/SE09319SC): Modify oil pan adding a new oil sump drain.. Texas Skyways Inc
- [STC SE00350SE](https://openairdocs.org/stc/SE00350SE): Installation of sump mounted chip detector.. Aviation Development Corporation
- [STC SE452NE](https://openairdocs.org/stc/SE452NE): Installation and usage of 'Mobil AV 1' aviation oil.. Mobil Research & Development Corp
- [STC SE23SW](https://openairdocs.org/stc/SE23SW): Installation of Bendix RS-5BD1 or RSA-5AD1 fuel injection system.. Bendix Corporation
- [STC SE5879SW](https://openairdocs.org/stc/SE5879SW): Use of Phillips X/C II 20W-50 and25W-60 oil (OSS 55875) in all Avco reciprocating aircraft engines from 65 to 450 BHP.. Phillips Petroleum Co
- [STC SE2094CE](https://openairdocs.org/stc/SE2094CE): Add the following approved fuel: unleaded automotive gasoline, 87 minimum antiknock index and leaded automotive gasoline, 88 minimum antiknock index (RON+MON)/2. Intermixing with aviation gasoline also approved.. Petersen Aviation Inc
- [STC SE1642SW](https://openairdocs.org/stc/SE1642SW): Modified cylinder assembly G-626820C or G-625859.. Gary Aerospace Corp
- [STC SE1760SW](https://openairdocs.org/stc/SE1760SW): Replacement of original cylinder barrels with P/N G-534894A.. Gary Aerospace Corp
- [STC SE244NE](https://openairdocs.org/stc/SE244NE): Installation of Mattituck plasma flame sprayed cylinder barrels in Teledyne reciprocating engines.. Mattituck Airbase, Inc
- [STC SE1445SO](https://openairdocs.org/stc/SE1445SO): Use of Aero-blend oil additive in Teledyne (non turbocharged) aircraft engines.. ProTec
- [STC SE89WE](https://openairdocs.org/stc/SE89WE): Installation of Bendix Model P.s-5BDl Fuel Injection
System. North Island Navy Flying Club
- [STC SE12GL](https://openairdocs.org/stc/SE12GL): Installation of oil filler cap.. Ray Whyte Electric Products Co.
- [STC SE16WE](https://openairdocs.org/stc/SE16WE): Bendix S-600 low tension ignition system.. Salinas Engine Works
- [STC SE44WE](https://openairdocs.org/stc/SE44WE): Use of Kling Aviation Oil, Specifications KL-100, KL-200 and KL-300 in Continental and Lycoming engines.. Kling Oil Company

---
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