Airworthiness Directives - Page 7

FAA AD 2002-17-53: This Emergency AD is prompted by reports of 17 crankshaft failures in LTIO-540 and TIO-540 engines, rated at 300 HP or higher, that were assembled with certain crankshafts that were manufactured using a hammer-forged process. This AD is applicable to all Textron Lycoming LTIO-540 and TIO-540 engines,...

This AD applies to certain de Havilland Inc. Models DHC-2 MK. I, DHC-2 MK. II, and DHC02 Mk. III Airplanes

This AD applies to all aircraft employing magnetos and using Bendix ignition switches.

This AD requires inspecting (one-time) the fuel line and map light switch in the left hand forward door post for chafing or arcing on certain Cessna Aircraft Company (Cessna) Model 172N, R172K, F172N, and FR172K airplanes and repairing any damage found.

This AD is applicable to General Aviation aircraft equipped with certain UPS Aviation Technologies, Inc., Model Apollo SL30 very-high-frequency navigation/communication (VHF NAV/COMM) radios.

This AD requires a one-time inspection for proper engine idle speed and fuel control mixture setting and adjustment, as necessary.  This AD also requires incorporating engine operating procedures into the pilots operating handbook.

This AD requires you to repetitively replace the existing Aeroquip V-band exhaust clamp.

This AD is applicable to Textron Lycoming IO-540 and O-540 engines equipped with Slick Aircraft Products magnetos.