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10  |  Copyright © 2015 Airmotive Engineering Corp.

3.2 Warm Up and Taxi

Engine cooling is dependent upon airflow through the cowling and oil cooler.  

The section of the propeller in front of the cowl cooling inlet is generally very 

ineffective, and forward speed of the airplane may be necessary during high 

temperature conditions to keep the engine from overheating.  Overheating 

during ground operation can produce a condition called “Glazed Cylinder Bores” 

at any time in the engine’s life, but the cylinders are most susceptible during the 

first few operating hours. Reference is made to SB 88-7-1 and Manual M101: 

 

Break-In Instructions for Cylinder Overhaul or Cylinder Replacement

The engine should be warm enough for taxi as soon as it takes throttle with no 

hesitation.  Trying to keep taxi distances short is not always possible, and there 

should be no significant engine distress from long taxi distances after engines 

are properly broken-in.  However, the engine temperature should be monitored, 

especially during hot weather.  Additionally, taxi safety should not be compromised!  

If high temperatures are noted during taxi, then the engine installation should be 

examined to establish and fix the root cause.

3.3 Run-Up

Follow the airplane manufacturer’s recommendations for similar engines. 

 

However, the following procedure may be used. 

If possible, head airplane into wind.

Mixture:  FULL RICH

Throttle:  1700 RPM

Ignition:  Switch to left and then right, a slight change in RPM is normal but engine 

should continue to run smooth on either ignitions.

Carburetor Heat Control (Carburetor Engines):  PULL OUT AND VERIFY RPM 

DECREASE

3.4 Take-Off and Climb

Mixture:  FULL RICH  (Note:  at high altitudes, some leaning to obtain smooth 

operation may be required)

Carburetor Heat Control (Carburetor Engines):   OFF  (Full in position on most 

airplanes) 

 

 

 

 

 

Throttle: ADVANCE SLOWLY AND SMOOTHLY  (If engine does not respond properly 

to throttle, then abort take-off and determine cause)

Carburetor heat may be required during climb to prevent the formation of ice on the 
air throttle valve.  The use of carburetor heat causes the engine to run slightly richer, 
and some roughness may be experienced. Sometimes this can be helped by leaning 
the mixture slightly. 

Summary of Contents for 340CC

Page 1: ......

Page 2: ...tional Inc corporate offices Trademarks ECi Nickel Carbide and TITAN are trademarks or registered trademarks of Engine Components International Inc All other company product or service names reference...

Page 3: ...tem 6 1 6 Ignition System 6 2 0 Specific Modifications 7 3 0 Operating Instructions 9 3 1 Starting Engine 9 3 2 Warm Up and Taxi 10 3 3 Run Up 10 3 4 Take Off and Climb 10 3 5 Cruise 11 3 6 Let Down 1...

Page 4: ...steel rocker cover sealing the upper valve train from the environment The cylinder barrels are made of thru hardened steel that will have a Nickel Carbide coating for additional corrosion and wear pre...

Page 5: ...engine lubrication and with a suction screen to prevent debris from circulating through the engine The sump has a pad on the bottom to attach the carburetor The 340CC oil sump is fabricated from alumi...

Page 6: ...pump on engines utilizing a carburetor 1 4 Ignition Systems The ignition system used on the TITAN 340CC engine is an electronic system produced by Lightspeed Engineering The cylinders are machined fo...

Page 7: ...re In Hg 28 5 Maximum Continuous horsepower 80 Bore 5 125 Stroke 4 125 Displacement cubic inches 340 4 Compression ratio 9 1 Firing order 1 3 2 4 Maximum Ignition Timing 25 BTDC Accessory Direction of...

Page 8: ...Basic Engine Configuration Cub Crafters oil sump and induction tubes Hollow front main crankshaft with plug for fixed pitch propeller Starter ring gear and support caburetor magnetos ignition system...

Page 9: ...ne area to see if significant blow by is evident Check the area behind the starter ring gear if possible to ensure that the front oil seal is not leaking Oil dripping from the cowling in any location...

Page 10: ...weather Additionally taxi safety should not be compromised If high temperatures are noted during taxi then the engine installation should be examined to establish and fix the root cause 3 3 Run Up Fo...

Page 11: ...between 20 and 90 F and the humidity is high 6 After cruise power and mixture have been set allow the engine to stabilize and monitor manifold pressure RPM and engine temperatures NOTE There are many...

Page 12: ...increases should be made to verify the engine is ready to resume full power if required NOTE Reduced throttle exposes more carburetor butterfly to the airflow and the possibility of carburetor ice is...

Page 13: ...mergency automotive premium grade fuel may be used Acceptable fuel pressures are as follows Fuel Pressure Limits Inlet to carburetor psi 0 5 to 8 0 Oil Sump Capacity TITAN 340CC Maximum Quantity 6 US...

Page 14: ...100 4 3 Operational Limitations Engine Type Operation RPM HP Fuel Cons gal hr Max Oil Cons qts hr Max Cyl Head Temp F TITAN 340CC Take Off 2700 180 16 2 0 25 475 Recommended Cruise See Below See Below...

Page 15: ...d Engine 15 4 4 Overhaul Period The O 340CC engines have been tested to the protocol established in ASTM F2339 06 to an overhaul period of 2400 hours Overhaul periods are subject to many factors and m...

Page 16: ...www titanengine com...

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