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New - McFarlane Aviation Products

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®ToolsFlap Track Wear Gauge for Cessna AircraftPart Number 950Use to determine if a Cessna flap track is worn beyond service limits.InstructionsRun the gauge plug along each slot in each flap track while verifying that the gauge willnot enter the slot. Reposition the flaps as required to gauge the entire length of each slot.If the gauge enters a slot at any point, the track is worn beyond service limits.Periodically verify the gauge diameter by measuring the gauge diameter with acalibrated micrometer.This gauge will work for all single engine Cessna aircraft except140A, 170A and 195Flap Roller Installation ToolPart Number 970• Makes installation of the aft flap roller, bushing and washers easy.• Holds parts in alignment while inserting the bolt.• Long handle allows access through the small inspection openings.• Use on Cessna 150 thru 210<strong>New</strong>!Elevator and Rudder Bearing Installation Tool for Cessna AircraftMakes pressing bearings in or out easy!Part Number 990<strong>New</strong>!This unique tool is specifically designed to prevent damage when installingand removing sintered bronze rudder and elevator hinge bearings.• Seven piece kit for all sizes of sleeve bearings.• Heat treated stainless steel will last a lifetime.• Comes in a convenient storage pouch.Compression Tester ExtensionPart NumbersEXTENSION CT1 (18mm thread)EXTENSION CT14 (14mm thread)• Wrench-free compression test extender• Quality welded construction, o-ring seal• Allows for exhaust system and baffling clearance• Makes compression testing easy• Save time and $$Manufactured by Bob BainesSpark PlugThread withO-Ring SealExtended Lengthfor ClearanceHandle forWrench-FreeOperationStandardAir FittingSeat Rail Wear Gauge for Cessna Aircraft - Fast and Positive - No More Guessing!Checks seat rail wear limitsas per FAA A.D. 87-20-03Seat Rail DirectiveThe gauge is to be used forinspection of the Cessna seat railwear. This gauge is designed tomeasure the actual radius wearnear the seat stop holes. Noticethe different sized steps in eachcorner. The sizes apply to the .36and .42 diameter limits referredto by the A.D. The .020 uppersurface wear allowance allowedby the A.D. is designed intothe gauge. This gauge is veryprecisely machined.1. Place the .36 sideof the gauge into eachhole location showingwear.2. Slide gauge backalong top center ofthe rail until it contactsthe hole edge. Makingsure to keep the gaugeparallel and square tothe unworn rail surface.Part NumberGAUGE SR13. If the step touchesthe rail and lifts thegauge up, the wear isless than .36.If the step does nottouch the rail, thewear is more than .36.Proceed to step 4.84 Order Online at www.mcfarlaneaviation.com or Call 888-750-5251 “MC” prefix denotes <strong>McFarlane</strong> <strong>Aviation</strong>, Inc. manufacture4. Use the side of the gaugemarked .42 to check if the wearat this hole is within maximumtolerance or if the rail needsreplacement.a. Follow the same procedure aslisted in Steps 1 through 3.If the step does touch the rail,the wear is within acceptablelimits and the inspection mustbe done every 100 hrs TIS(Time In Service) as listed inthe A.D.b. If the step does not hit therail, the rail has wear greaterthan .42 and the seat rail mustbe replaced.

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