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  Cannot reach critical altitude in Lycoming or Continental aircraft engine

1. Improperly adjusted wastegate valve. You may need to adjust the wastegate on new engines to reach critical altitude. On Continental TSIO360 E,EB,F,FB,G,GB and Continental LTSIO360 E,EB engines adjust critical altitude in accordance with Continental Service Bulletin M84-6 Revision 1 or latest edition. This procedure involves the following: A. Takeoff rated manifold pressure and rpm are obtained at approximately 40 degrees throttle travel. B. Engine critical altitude adjustment is controlled by a ground adjustable screw-type wastegate on the exhaust bypass pipe at the turbocharger location. This adjustment is preset and only minor changes should be required. Adjustment is as follows: Approximately 1000 feet increase in critical altitude per one revolution of screw clockwise; approximately 1000 feet reduction in critical altitude per one revolution of screw counterclockwise. Unlock and lock jam nut before adjustment.

2. Leaky exhaust system. Inspect for any white exhaust stains on the exhaust system.

3. Malfunctioning turbocharger. Remove exhaust or air inlet connections and check rotor assembly for possible rubbing on housing, damaged rotor or malfunctioning bearings. Spin turbine by hand to check for free rotation.

4. Wastegate does not go to full closed position. Cap off the actuator discharge, apply 60-65 pounds of oil pressure to inlet. When the wastegate closes, measure the clearance between butterfly and housing. Lubricate shaft with Mouse Milk.

5. Suck-open door on compression discharge housing not fully closed or door gasket damaged (TIO-540 engines).

6. Faulty Absolute Controller. If engine loses power, consider leaking poppet valve or oil leaking into induction system because of broken boot bellows. Remove controller and check for oil in induction housing.

7. Faulty density controller. The density controller is used to regulate wide-open throttle power (and manifold pressure). When density reaches a level at which spring tension is overcome, the controller outlet port opens.

8. Improperly adjusted controllers.

9. Insufficient oil pressure to close wastegate. Pressure required to close wastegate varies with model but is generally between 15-30 psi.

10. Improper adjustment of density controller on Lycoming T/LTIO- 540 engines. Full rated power is set by adjusting the density controller per Lycoming Service Instruction 1187G or latest edition.

11. Aerostar, failed waste-gate actuator. Failed actuator piston rings. If the drain line is routed to the crankcase, then no oil loss is apparent. The first symptom is loss of critical altitude. Disconnect the actuator drain line from the crankcase, plug the hole in the case, and wire a jar so the line drains into the jar. A short test fight will put oil into the jar if the actuator rings are bypassing oil. On Cessna's you can usually put a Q-tip up the drain line and see if it comes out clean or not.

12. Leak in intake system allowing hot cowling air into induction system. If the air induction system is not getting all of its air from outside the cowling then the engine is operating at higher intake air temperature than normal. All air for combustion should be coming from outside the cowl. Inspect for leaks in the transaction duct from the air box to the air scoop. Confirm filter cover to air box fit snug. Check the air box magnets and the alternate air door hinge. 



 

 


 

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Disclaimer: sacskyranch.com contains abundant information relating to aircraft maintenance. The information provided  is not intended to supercede or supplement the F.A.A. approved  maintenance and/or operator’s manuals. Those F.A.A. approved manuals must be utilized when performing maintenance and/or operating aircraft.