Computer Testing Supplement for IA.indb - Aviation Supplies ...

Page No. 1 2 3 4 5 6
Rev. No. 35 36 36 36 36 36
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
TYPE CERTIFICATE DATA SHEET NO. E-273
E-273
Revision 36
CONTINENTAL
O-470-A, -B, -E, -G, -H, -J, -K, -L, -M,
-N, -P, -R, -S, -T, -U
O-470-B-CI, -G-CI, K-CI, L-CI, M-CI
(NOTE 6)
IO-470-A, -C
September 29, 1995
Engines of models described herein conforming with this data sheet (which is part of type certificate No. 273) 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 Teledyne Continental Motors
P.O. Box 90
Mobile, Alabama 36601
Model O-470-A O-470-E O-470-J
O-470-K, -L,
-R, -S O-470-B, -M, -N
Type
Rating, ICAO or ARDC
standard atmosphere
Max. continuous hp, rpm, at
6HOA - - - - - - - - - - - -
sea level pressure altitude
Takeoff hp, 5 min., rpm, full
throttle at sea level pressure
225-2600 225-2600 225-2550 230-2600 240-2600
altitude 225-2600 225-2600 225-2550 230-2600 240-2600
Fuel, (aviation gasoline,
minimum grade)
80/87 - - - - - - - - - 91/96
Lubricating oil, ambient air See NOTE 9 - - - - - - - - - - - -
temperature: Above 40° F. Oil Grade SAE 50 - - - - - - - - - - - -
Below 40° F. Oil Grade 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
378 390 378 404 (-K, -L)
401 (-R, -S)
410
Accessory case, in. 12.8 - - - - - - 12.0 11.3
Below crankshaft center
0.1 - - - - - - 0.3 0.5
line, in.
Beside crankshaft center
line, toward 1-3-5 side, in.
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