CIVIL AERONAUTICS ADMINISTRATION TC No. A-533 Models: WACO YKC YKC-S YKS-6 ZKS-6 See (Specifications Pertinent to All Models and Notes) Date: January 3, 1949 AIRCRAFT SPECIFICATION NO. A-533 Manufacturer: Waco Aircraft Co. Troy, Ohio

I - Models YKC, YKC-S and YKS-6. 4-5 PCL-SB (See Note 1 for explanation of model designation). Engine: Jacobs L-4 Engine limits: For all operations, 2000 rpm (225 H.P.) Airspeed limits: Not available Propeller limits: Not available C.G. range: Landplane: (-14.4) to (-2.4) Seaplane : (-12.7) to (-3.7) E.W.C.G. range: Landplane: (-10.4) to (-15.0) Seaplane : (-12.3) to (-13.1) Both valid as 3, 4 or 5 place, with or without optional fuel tanks. If empty weight C.G. falls within range given, it is unnecessary to check critical forward and aft C.G.positions. These ranges are not valid for non-standard arrangements, except as noted herein. Maximum weight: (a) Landplanes serials 3873 to 3877, inclusive, and 3975 (not equipped with spoilers) are eligible at 2850 lbs. (b) Landplanes serials 3978 and up eligible at 3000 lbs. These serials also eligible at 3250 lbs. provided: (1) Landing gear per Waco Dwg. 20497 is installed and structural changes per pages 8 and 9 of Waco Report 383 are made, and (2) Wing spoilers or Model UMF vertical tail surfaces are installed. (c) Seaplanes: 3250 lbs. No. seats: 3, 4 or 5 (Front - 2.5, rear +27). Five-place airplanes must have: (a) Additional safety belt on rear seat. (b) Baggage capacity reduced to 70 lbs., unless actual weight and balance substantiates lesser restriction. Maximum baggage: 100 lbs. (+49) Fuel capacity: 50 gals. (-11) (Two 25-gal. tanks in upper wings) Oil capacity: 5 gals. (-44) Serial Nos. eligible: 3873 and up mfd. prior to Sept. 30, 1939. Approval expired as of that date. Required equipment: Landplanes: Items 101, 102, 103, 104, 107, 108 109, 110. Seaplanes : Items 101, 104, 109, 110, 151, 152 153, 154, 155 156. Seaplanes serials 3873 to 3877, inclusive, and 3975 must have wing spoilers installed in accordance with approved data.

II - Model ZKS-6, 4-5 PCL-SB (Same as Model YKS-6, except engine installation. See Note 1 for explanation of model designation). Engine: Jacobs L-5 Engine limits: Take-off and climb 2000 rpm (285 hp) For all other operations 1910 rpm (250 hp) Airspeed limits: Level flight or climb 140 mph True Ind. Glide or dive 168 mph True Ind. Propeller limits: Not available C.G. range: ) Empty weight C.G. range: ) Maximum weights: ( Same as given under Part I above. No. seats: ) Maximum baggage: ) Fuel capacity: 50 gals. (-11) (Two 25-gal. tanks in upper wings) Fuel valves must be placarded: "Both tanks should be turned to "ON" position during take-off, climb and landing". Oil capacity: 5 gals. (-44) Serial Nos. eligible: 3873 and up manufactured prior to September 30, 1939. Approval expired as of that date. Required equipment: Landplanes: Items 101, 102, 103, 104, 107, 108, 109, 110, 323. Seaplanes : Items 101, 104, 109, 110, 151, 152, 153, 154, 155, 156, 323.

Specifications Pertinent to All Models: Datum: Leading edge lower wing Leveling means: Not available Certification basis: Approved type certificate No. 533. (Expired September 30, 1939) Export eligibility: will be supplied on request to Office of Aviation Safety, Washington. Equipment: A plus (+) or minus (-) sign preceding the weight of an item indicates net weight change when that item is installed. Propellers and Propeller Accessories: 109. Propeller - wood (fixed pitch) 45 lbs. (-79.5) 204. Propeller - Hamilton Standard hub 2B20, blades 6109A-6 to 6109A-16 incl., or 6135A-6 to 6135A-16 incl., - Diameter 8'6" maximum, 7'7" minimum. (For use with Jacobs L-4 only) 104 lbs. 305. Propellers (a) Adj. pitch metal - Ham. Std. +37 lbs. (-80) (b) Fixed pitch metal - Curtiss 55501 +9 Lbs. (-80) Engines and Engine Accessories - Fuel and Oil System: 101. Engine ring cowl 22 lbs. 102. Starter (direct electrical) 20 lbs. 153. Starter 30 lbs. 155. Heater 5 lbs. (-51) 306. Fuel capacity (a) 70 gals. (Two 35 gal. tanks in upper wings) +18 lbs. (-11) (b) 100 gals. (Two 35 gal. tanks in upper wings and two 15 gal. +53 lbs. (-11) tanks in lower wings) 307. Four or 6 1/2 gal. oil tank No weight change 312. Engine crankcase cooling disc (Mounted on forward part of 3 lbs. engine crankcase). 314. (a) Heater 5 lbs. (-51) (b) Ventilator 2 lbs. 318. Lux remote fire extinguisher 19 lbs. (+12) or (-48) 323. Oil cooler

Specifications Pertinent to All Models: (Cont.) Landing Gear: 107. 8-in. streamline tail wheel (+181) 108. 6.50-10 wheels (Autofan) with 7:50-10 or 8:50-10 tires (-24) (wheels must be placarded for these tires) 151. Edo P-3300 or 38-3430 floats 304. Wheel streamlines 24 lbs. (-24) 315. 7:50-10 cactus proof tubes 10 lbs. (-24) 316. Tail wheel lock (+87) 324. Skis Use actual weight (a) Washington Aircraft 3600 (b) Federal SA-6 Electrical Equipment: 103. Generator 13 lbs. 104. Battery - ahead of firewall 42 lbs. 154. Generator 10 lbs. 301. Landing lights - Grimes retractable 11 lbs. (+7) 320. Generator - Eclipse LV-180 18 lbs. Interior Equipment: 110. "Throwover" type control column 201. Ambulance equipment (litter) 12 lbs. (+97) 303. Flexible instrument panel 5 lbs. (-34) 308. Flares (a) Three 1 1/2 min. 17 lbs. (+70) (b) Five 1 min. 13 lbs. (+70) 319. "Y" type control column 321. Baggage compartment and door 3 lbs. (+54) Miscellaneous: 152. Large vertical surfaces including extra fin underneath fuselage replacing tail wheel. 156. Wing root fairing 310. Air brakes 10 lbs. (0) 317. Extra door and wing walk 16 lbs. (+19)

NOTES Note 1. Yearly models: 1934 YKC or ZKS 1935 YKC-S or ZKS-S 1936 YKS-6 or ZKS-6 In the case of the 1936 designation: First letter shows engine; second letter shows wing; third letter shows type; number indicates year. - END -