Aviall Product Catalog And Source Book Page 1759 Undercarriage & Tires

CLEVELAND CONVERSION KITS CLEVELAND WHEELS & BRAKES aviall ability aviall.com 1759 Kit Tire Wheel Standard Chrome Brake Manufacturer Number Size Assembly Disc Disc Assembly Lining Type Comments Homebuilt Aircraft General usage 2 199-102 (1) 5.00-5 40-78B 164-01700 164-11700 30-9 066-10600 O Magnesium wheel (standard energy brake) General usage 2 199-156 5.00-5 40-230 164-09900 N/A 30-181A 066-10600 O Aluminum brake (increased energy brake) Magnesium wheel General usage 199-152 5.00-5 40-151 164-08500 N/A 30-133 066-10500 O Magnesium wheel (high energy brake) Magnesium brake 199-152A 5.00-5 40-151A 164-08500 N/A 30-133 066-10500 O Aluminum wheel Magnesium brake General usage 199-197 5.00-5 40-151 164-08500 N/A 30-164 066-06200 M Magnesium wheel (very high energy brake) Magnesium brake General usage 2 199-103 (1) 5.00-5 40-78A 164-01700 164-11700 30-9C 066-10600 O Aluminum wheel (1 1 /2" axle) Aluminum brake General usage 2 199-104 (1) 6.00-6 40-59A 164-07500 164-17500 30-59A 066-11200 O Magnesium wheel (1 1 /2" axle) Magnesium brake General usage 2 199-105 (1) 6.00-6 40-113X 164-04000 164-14000 30-75X 066-10500 O Aluminum wheel (1 1 /2" axle) Aluminum brake General usage 199-204 6.00-6 40-281 164-23400 N/A 30-214 066-10500 O Magnesium wheel (1 1 /4" axle) 7.00-6 Magnesium brake 8.00-6 Navion A, B, D, E, F, G, H 199-52 7.00-8 40-98D 164-02701 N/A 30-66B 066-11000 O Main and nose wheel (Main) (Main) Installation per FAA STC SA36GL 6.00-6 40-76B (Nose) (Nose) A, B, D, E, F, G, H 199-52A 7.00-8 40-98D 164-02701 N/A 30-66B 066-11000 O Mains only, installation per FAA STC SA46GL Piper J3, PA11, PA12, PA13, 199-71 1 6.00-6 40-60 164-06700 164-16700 30-60A 066-10600 O Magnesium wheel, installation PA14, PA15, PA16, PA17, 7.00-6 per FAA Form 337 3 PA18, PA20, PA18-150, 8.00-6 PA18A-150 J3, PA11, PA12, PA13, 199-71A 1 6.00-6 40-60A 164-06700 164-16700 30-60A 066-10600 O Aluminum wheel, installation PA14, PA15, PA16, PA17, 7.00-6 per FAA Form 337. 3 PA18, PA20, PA18-150, 8.00-6 PA18A-150 Stinson 108 Series 199-87 (1) 7.00-6 40-97D 164-02601 164-12601 30-63Q 066-10500 O This kit available only from Univair. Installation per Univair TC approval. 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 For detail design/rating information, refer to Cleveland drawing 50-76, general arrangement - wheels and brakes, 5" and 6" 3 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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