- Holder
- Continental Aerospace Technologies, Inc.
- Revision
- 13
- Revised
- September 19, 2022
- Status
- Current
- Product
- Engine
- Certification basis
- CAR 13
- Models
- 4
- Registered
- 993 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 4
| Model | Also known as | Note |
|---|---|---|
| E225-8 | Formerly Continental, then Teledyne Continental Motors | |
| E225-9 | Formerly Continental, then Teledyne Continental Motors | |
| E225-4 | Formerly Continental, then Teledyne Continental Motors | |
| E225-2 | Formerly Continental, then Teledyne Continental Motors |
Airworthiness directives · 8
ADs whose products are models on this data sheet, matched by model and maker.
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
STCs approved under this data sheet · 30
STC SE04651CHTo allow use of l00R grade aviation fuel meeting Swift Fuel, LLC specification SPEC-l00R-22STC SE04349CHInstallation of SureFly electronic ignitionSTC SE03309CHInstallation of Engine Preheat Kit, p/n TSP6CYL-2927-115 for 115 volt application
See all 30 STCsWhat the data sheet says
From the PDF’s text layer, line by line: tables lose their columns. The PDF is the record.
E-267
Revision 13
CONTINENTAL AEROSPACE TECHNOLOGIES, INC.
E225-2, -4, -8, -9
September 19, 2022
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
TYPE CERTIFICATE DATA SHEET NO. E-267
Engines of models described herein conforming with this data sheet (which is part of type certificate No. 267) and other approved
data on file with the Federal Aviation Agency meet the minimum standards for sue 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 E225-2 E225-4 E225-8 E225-9
Type
Rating, ICAO or ARDC standard atmosphere
6H0 - - - - - -
Max. continuous hp., r.p.m., full throttle at sea
level pressure altitude
Takeoff hp., 5 min., r.p.m. full throttle at sea
225-2650
225-2650
- -
- -
- -
- -
- -
- -
level pressure altitude
Fuel (min. grade aviation gasoline)
80/87, ASTM D7547
- -
- -
- -
Lubricating oil
(UL91), ASTM D7547
(UL94)
Ambient air temperature
Above 40°F.
Oil grade
SAE 50
- -
- -
- -
Below 40°F. SAE 30 - - - - - -
Bore and stroke, in. 5.00 x 4.00 - - - - - -
Displacement, cu. in. 471 - - - - - -
Compression ratio 7:1 - - - - - -
Weight (dry), lb.
C.G. location (basic engine)
Fwd. of rear face engine crankcase, in.
359
11.75
355
11.51
347
11.75
363
11.51
Below crankshaft centerline, in. 1.42 1.76 1.42 1.76
Propeller shaft, SAE No. 20 (Spline) - - - - - -
Carburetion
Ignition, dual magnetos
Timing, °BTC
Bendix-Stromberg Model PS5C
(Continental No. 531857)
Continental S6LN-21 or S6LSC-
21 or 1 ea. S6LN-200 and -204
Right 26°, Left 26°
- -
- -
- -
- -
- -
- -
- -
- -
- -
Spark plugs See NOTE 7 - - - - - -
Oil sump capacity, qt.
NOTES
Dry
1,2,3,4,6,7
10 (7 usable)
1,2,3,4,5,6,7
Dry
1,2,3,4,5,6,7
10 (7
usable)
1,2,3,4,6,7
“- -“ indicates “same as preceding model”
Page No. 1 2
Rev. No. 13 12
E-267 2
Certification basis CAR 13 effective August 1, 1949
Type Certificate No. 267 issued July 12, 1950 for Model E225-8; E225-9 added October 30, 1950;
E225-2 added July 19, 1951; E225-4 added June 5, 1952.
Date of Application for Type Certificate June 2, 1950.
Production basis Production Certificates Nos. 7 and 508.
NOTE 1. Maximum permissible temperatures
Cylinder head 525°F. (spark plug gasket), 450°F. (well type thermocouple, downdraft cooling only)
Cylinder barrel 290°F.
Oil inlet 225°F.
NOTE 2. Fuel inlet pressure limit 9 to 15 p.s.i.
Oil pressure limits (normal operation) 30 to 60 p.s.i. Maximum (cold oil) 100 p.s.i.
NOTE 3. Accessories such as generators, starters, fuel and vacuum pumps, etc., previously listed in NOTE 3, are satisfactory
for continued use with these engines. As these are not integral engine accessories, they are not evaluated for
approval during engine certification testing. The airworthiness of such accessories is substantiated during aircraft
installation system approvals. The suitability of the accessory to the engine mounting provisions as described below,
must be determined when processing such approvals.
Accessory
Type of
Drive
Direction
of Rotation
Speed Ratio
to Crankshaft
Max. Torque
Continuous
(in. -lb.)
Static
Maximum
Overhang
Moment (in. -lb)
Generator Automotive CC 2.25:1 60 800 100
Starter Aircraft CC 1.15:1 2400
Fuel Pump AND 10000 CC 1.67:1 26 400 25
Tachometer AS 54 C 0.5:1
Optional AND 10000 C 1.364:1 90 600 65
NOTE 4. The cylinder assemblies on the E225-2 and -9 models have increased cooling fin areas and increased overall length
over the cylinders on the -4 and -8 models.
NOTE 5. E225-4 and -8 engines with S/N 30,001 thru 30,086 have two each 6th order dampers.
Engines with S/N 30,087 and above have one each 5th and 6th order dampers.
NOTE 6. E225 series engines are eligible for both tractor and pusher installations.
NOTE 7. 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 HSR83IR, SR83IR, HSR83P, SR83P, A88, HS88, HSR88, SR88, S88, SR88D, S88D
Auto Lite H15, SH15, SH15R, SH20A, SH200A
BG RB485S, 706, 706R, 706S, 706SR, RB919SR5, RB955S
Champion C27, C27S, REM38P, RHM38P, REM39N, REM40E, RHM40E, ED41N, D41N, EM41N, M41N,
EM42E, M42E
Red Seal SA190, SE190, SJ190, SE230, SJ230
....END.....