certificated aircraft engines february 2004 ssp-204
certificated aircraft engines february 2004 ssp-204
certificated aircraft engines february 2004 ssp-204
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PISTON – (6) SIX CYLINDER SERIES<br />
T/O† E S/N<br />
Model HP RPM Fuel C.R. Description Suffix<br />
O-540-J1B5D 235 2400 100/100LL 8.50:1 Same as –J1A5D but with D6LN-3200 Retard Breaker -40<br />
dual Magneto<br />
O-540-J1C5D 235 2400 100/100LL 8.50:1 Same as –J1A5D but with rear mounted HA-6 -40<br />
horizontal carburetor<br />
O-540-J1D5D 235 2400 100/100LL 8.50:1 Same as –J1C5D but with D6LN-3200 Retard Breaker -40<br />
dual Magneto<br />
O-540-J2A5D 235 2400 100/100LL 8.50:1 Same as –J1A5D but with fixed pitch propeller -40<br />
O-540-J2B5D 235 2400 100/100LL 8.50:1 Same as –J1B5D but with fixed pitch propeller -40<br />
O-540-J2C5D 235 2400 100/100LL 8.50:1 Same as –J1C5D but with fixed pitch propeller -40<br />
O-540-J2D5D 235 2400 100/100LL 8.50:1 Same as –J1D5D but with fixed pitch propeller -40<br />
O-540-J3A5 235 2400 100/100LL 8.50:1 Same as –J3A5D but has Slick 6251 (impulse -40<br />
coupling) and 6250 Magnetos<br />
O-540-J3A5D 235 2400 100/100LL 8.50:1 Same as –J1A5D but has heavier counterweights for -40<br />
use with Hartzell extended hub controllable propeller<br />
O-540-J3C5D 235 2400 100/100LL 8.50:1 Same as –J1C5D but has heavier counterweights for -40<br />
use with McCauley controllable propeller<br />
O-540-L3C5D 235 2400 100/100LL 8.50:1 Similar to –J3C5D except for long reach spark plugs, -40<br />
high pressure fuel pump, piston cooling oil jets and<br />
turbocharger scavenge pump<br />
IO-540-A1A5 290 2575 100/100LL 8.70:1 High compression tuned induction, Retard Breaker -48<br />
Magnetos, Bendix fuel injector<br />
IO-540-B1A 290 2575 100/100LL 8.70:1 Same as –A1A5 except for updraft exhaust cooling -48<br />
IO-540-B1B5 290 2575 100/100LL 8.70:1 Same as –B1A5 except for Simmonds fuel injector -48<br />
IO-540-B1C5 290 2575 100/100LL 8.70:1 Same as –B1A5 except it has external servo bleed in -48<br />
fuel injection system<br />
IO-540-C1B5 250 2575 100/100LL 8.50:1 Same as O-540-A1D5 but with Bendix fuel injector -48<br />
IO-540-C1C5 250 2575 100/100LL 8.50:1 Same as –C1B5 but has AN fuel pump -48<br />
IO-540-C2C 250 2575 100/100LL 8.50:1 Conversion of O-540-A2B to Bendix fuel injection -48<br />
and AN fuel pump drive<br />
IO-540-C4B5 250 2575 100/100LL 8.50:1 Same as –C1B5 but with more effective counter- -48<br />
weights for use with Hartzell “compact” propeller<br />
IO-540-C4C5 250 2575 100/100LL 8.50:1 Same as –C4B5 but has AN fuel pump drive -48<br />
IO-540-C4D5 250 2575 100/100LL 8.50:1 Same as –C4D5D except has two Magnetos -48<br />
IO-540-C4D5D 250 2575 100/100LL 8.50:1 Same as –C4B5 but with D6LN-3000 impulse coupling -48<br />
Magneto<br />
IO-540-D4A5 260 2700 100/100LL 8.50:1 Same as O-540-E4A5 but with Bendix fuel injection -48<br />
† Take-Off.<br />
20
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