Cessna SEL-81-02



TITLE- TRANSMITTAL OF HET ALERT SERVICE BULLETIN NO. 048 AND LYCOMING MANDATORY SERVICE BULLETIN NO. 604
EFFECTIVITY: All model T182T airplanes that have had the original engine or turbocharger replaced with engines or turbochargers affected by the attached Hartzell Engine Technologies (HET) Alert Service Bulletin No. 048 (or latest revision) or
Lycoming Mandatory Service Bulletin No. 604 (or latest revision).


                       REASON The purpose of this service letter is to transmit the attached Hartzell Engine Technologies (HET) Alert Service Bulletin No. 048 and Lycoming Mandatory Service Bulletin No. 604. Non-compliance with HET Alert Service Bulletin No. 048 and Lycoming Mandatory Service Bulletin No.604 may allow the turbocharger turbine head to separate from the shaft. This may result in rapid reduction in or complete loss of engine power. Additionally there is the possibility of the loss of engine oil and fire.
DESCRIPTION HET has discovered that there is the potential for a compromised shaft-to-wheel head weld for HET P/N 410188-0019 T-wheel.
COMPLIANCE :INFORMATIONAL. This service letter is for informational purposes only.
REFERENCES : Model 182/T182 Series 1997 and On Maintenance Manual Model 182S

Qualty,Safety and Training

Comments

Post a Comment

Popular posts from this blog

Cessna 152 Magneto Check

MAGNETO CHECK. NEVER ADVANCE TIMING BEYOND SPECIFICATIONS IN ORDER TO REDUCE RPM DROP. Too much importance is being attached to RPM drop in single ignition. RPM drop on single ignition is a natural characteristic of dual ignition design. The purpose of the following magneto check is to determine that all cylinders are firing. If all cylinders are not firing, the engine will run extremely rough and cause for investigation will be quite apparent. The amount of RPM drop is not necessarily significant and will be influenced by ambient air temperature, humidity, airport altitude, etc. In fact, absence of RPM drop should be cause for suspicion that the magneto timing has been bumped up and is set in advance of the setting specified. Magneto checks should be performed on a comparative basis between individual right and left magneto performance. a. Start and run engine until the oil and cylinder head temperatures are in normal operating ranges. b. Advance engine speed to 1700 RPM. c. Tu...
Read more

Brake System Cessna 172

                             BRAKE SYSTEM -MAINTENANCE PRACTICES              1. Description and Operation A. The hydraulic brake system is comprised of two master cylinders, located immediately forward of the  pilot’s rudder pedals, brake lines and hoses, and single-disc, floating cylinder brake assemblies located at  each main landing gear wheel. B. The parking brake system is comprised of a pull-type handle and mechanical connections which are  linked to the rudder pedal assembly. Pulling aft on the brake handle applies mechanical pressure to the  rudder pedals, activating the brakes and locks the handle in place. Turning the handle 90 degrees will  release the parking brake and allow for normal operation through the rudder pedals. C. Brake operation is accomplished by pushing on the upper part of each rudder pedal. This motion i...
Read more

McCauley Propeller Installation fixed pitch

Image
Propeller Installation for all fixed pitch propellers (except 1A162 model propellers).                   WARNING: MAKE SURE THE MAGNETO IS GROUNDED BEFORE INSTALLING  THE PROPELLER OR CONNECTING EXTERNAL POWER.                NOTE: McCauley recommends that propeller mounting nuts (if applicable) be replaced at each  propeller installation, whenever possible. However, nuts may be reused providing the threads are in good condition and the locking material prevents turning of the nut on the  stud by hand. Propeller mounting bolts must be magnetic particle inspected in accordance  with ASTM E-1444 or replaced whenever the propeller is removed from the engine.                NOTE: The aircraft maintenance manual or STC installation instructions should always be  consulted for any specialized procedures applicable to a specific aircraft....
Read more