Aviall Product Catalog And Source Book Page 1758 Undercarriage & Tires

CLEVELAND CONVERSION KITS CLEVELAND WHEELS & BRAKES aviall.com North America and AOG 1.800.AVIALL.1 International Sales 1.800.AVIALL.3 or +1 972.586.1985 1758 Kit Tire Wheel Standard Chrome Brake Manufacturer Number Size Assembly Disc Disc Assembly Lining Type Comments Cessna 150, F150, A150, FA150, 199-84 1 6.00-6 40-113 164-04000 164-14000 30-75 066-10500 O Converts McCauley to Cleveland 152, A152, F152, FA152, Installation per FAA Form 337 2 172RG, 177, 177RG, F177RG,182, A182, F182 172, F172, R172, FR172 199-84A 1 6.00-6 40-113 164-04000 164-14000 30-75A 066-10500 O Converts McCauley to Cleveland Installation per FAA Form 337 2 180, 180A thru 180H, 180J, 199-62 1 8.00-6 40-75D 164-03601 164-13601 30-52N 066-10500 O This kit is to be used only with 180K, 185, 185A thru 185E, Cessna Axles. P/N 1441003-1, 0541124 & A185E, not for use on aircraft equipped with A185F, 206, P206, crosswind landing gear. Installation per U206, U206F, U206G, 199-62A 8.00-6 40-75T 164-08300 N/A 30-52N 066-10500 O FAA STC SA63GL. TU206E, TU206F, TU206G 180, 180A thru 180F, 180H, 199-155 8.00-6 40-75J N/A 164-13601 30-52Y 066-10500 O High corrosion resistant kit direct 180J, 185, 185A, 185B, Replacement for 40-75D and 30-52., Installation per FAA form 337. 2 180, 180A thru 180F, 199-60 1 6.00-6 40-75B 164-01501 164-11501 30-52 066-10500 O This kit is to be used only with 180H, 180J, 185, 185A, 15 x 6.00-6 Cessna axles P/N 0541124 and 185B, A185E, A185F, 206E, 1441003-1, not for use on TU206E, TU206F, 206F, aircraft equipped with crosswind 210, 210A, 210B, landing gear. Installation per 210C, 210K, 210L, FAA STC SA52GL and SA62GL. T210K, 210M, T210C, T210L, T210M, T210N P210N-S/N P21000001 thru 199-60A 1 6.00-6 40-75B 164-01501 164-11501 30-52U 066-10500 O Installation per FAA STC SA52GL P21000150 190, 195, 195A, 195B 199-61 6.50-10 40-40C 164-00806 N/A 30-28C 066-03300 M This kit is not for use on aircraft equipped with crosswind landing gear. Installation per FAA STC SA54GL. DeHavilland Chipmunk DHC-1-21, -22, 199-79 1 6.00-6 40-97D 164-02601 164-12601 30-63P 066-10500 O Installation per FAA STC -22A SA748S0, SA1011S0 DHC-1B-2-S3, -S5 Beaver DHC-2 Mk.I, Mk II, 199-95 7.50-10 40-134 164-06306 N/A 30-99 066-06600 M Installation per FAA STC Mk. III SA1402GL or Canadian STA SA90-1 Ercoupe E, G, 415-C, 415-D & 199-69 6.00-6 40-41 164-00300 N/A 30-30 066-10500 O Installation per FAA STC SA120GL, 415-CD (S/N 813 and up) SA127GL Erco Forney F-1, F-1A Globe Swift GC1A, GC1B 199-48 1 6.00-6 40-113C 164-04300 164-14300 30-79B 066-10500 O Installation per FAA STC SA2GL Single Engine Conversion Kit Application Data (cont'd) 1 Also available with chrome plated brake discs. To order, specify kit number followed by "CHROME" 2 The installer is required to obtain FAA field approval for the modification prior to returning the aircraft to service. Consult your local Flight Standards District Office (F.S.D.O.) for pre-approval guidelines.

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