Cessna Service Bulletin, SB04-71-01
Engine Cowl Flap Rivet Inspection
|182T||18280945 thru 18281262|
|T182T||T18208001 thru T18208223|
Reason: It has been determined that some airplanes were delivered with two rivets missing from the engine cowl flap support brackets where they attach to the inboard cowl flap support assemblies.
Compliance: Recommended: should be accomplished within the next 100 hours of operations or 12 months, whichever occurs first.
CREDIT EXPIRATION DATE: 26 April 2005