TCDS A-773

Page No. 1 2 3 4 Rev. No. 10 10 10 - Reformatted 2/94. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-773 Bellanca Revision 10 14-13 14-13-2 14-13-3 14-13-3W October 1, 1973 AIRCRAFT SPECIFICATION NO. A-773 Type Certificate Holder Bellanca Aircraft Corporation New Castle, Delaware 19720 I - Models 14-13, 4 PCLM, Approved September 25, 1946; 14-13-2, 4 PCLM, Approved June 2, 1947; 14-13-3, 4 PCLM and 14-13-3W, 2 pclm, Approved October 25, 1948. Model 14-13-2 same as 14-13 except for increased areas of stabilizer and elevators, decreased tip fin area, revised wood construction and revised elevator stops. Model 14-13-3 same as 14-13-2 except for dual landing lights in left wing leading edge, revised oleo struts and nut crackers, adjustable front seat backs and revised instrument panel. Model 14-13-3W same as 14-13-3 except for removal of rear seats. Engine Franklin 6A4-150-B3 Fuel 80 min. grade aviation gasoline. Engine limits For all operations, 2600 r.p.m. (150 hp) Airspeed limits Level flight or climb 160 m.p.h. (139 knots) (True Ind) Glide or dive 216 m.p.h. (187 knots) Flaps extended 85 m.p.h. ( 74 knots) C.G. range (landing gear 14-13: (+16.2) to (+23.6) extended) 14-13-2, 14-13-3, 14-13-3W: (+16.2) to (+24.5) Empty weight C.G. range None. Datum Leading edge of wing at rib No. 1. Rib No. 1 is 24 .in. outboard from fuselage center line. Leveling means Horizontal lugs, sta. 1 and 2. Vertical lugs, sta. 3. Maximum weight 14-13: 2100 lb. 14-13-2, 14-13-3, 14-13-3W: 2150 lb. No. seats 4 (Two at +18 or +20, Two at +50.5). Maximum baggage 60 lb. (+69). When baggage compartment per Dwg. 15086 is installed, maximum is 110 lb. (+80.5). In case of 14-13-3W station wagon compartment maximums are: Fwd. comp't: 260 lb. (+35) Aft. comp't: 413 lb. (+55) Fuel capacity 40 gal. (+29) Oil capacity 2 gal. (-36) Control surface movements 14:13 Elevator - landing gear up 18° up 19° down - landing gear down 23° up 19° down Elevator trim tab 12° up 22° down Rudder 18° left 18° right Aileron 28° up 22° down Flaps 46° down 14-13-2, 14-13-3, and 14-13-3W: Elevator 19° up 19° down Elevator trim tab 12° up 22° down Rudder 18° right 18° left Aileron 25° up 19° down Flaps 46° down A-773 Page 2 Serial Nos. eligible 1060 and up. Serial numbers 1060 through 1385 are Model 14-13. Serial numbers 1386 through 1583 are Model 14-13-2. Serial numbers 1584 and up are Model 14-13-3 and 14-13-3W. Serial numbers 1060 through 1385 are eligible as Model 14-1 3-2 providing they are revised to conform to Bellanca Dwgs. 9989, 9995, 9996 and 9918 and proper control surface movements. Required equipment In addition to the pertinent required basic equipment specified in CAR 4a, the following items of equipment must be installed: Landplane: Items 1, 103, 104, 105, 201(a), 202(a), 204(a). Skiplane: Items 1, 103, 104, 105, 208(a). Specifications Pertinent to all Models Certification basis Type Certificate No. 773 (CAR 4a) Production basis None. 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: 1. Propeller-Sensenich 74RA or any other fixed pitch wood propeller rated for 20 lb. (-56) required hp and rpm and following limits: Static rpm at maximum permissible throttle setting: Not over 2100, not under 2000. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. 2. (a) Propeller-Koppers Aeromatic Hub F200, blades 00-74A, 00-74B or 00-74C. 31 lb. (-56) Parts List Assembly No. 4275. Low pitch setting 14° at 24 in. sta. Static rpm at maximum permissible throttle setting: Not over 2550, not under 2500. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. Installation must be accomplished in accordance with Koppers "Installation Procedure and Operating Limitation No. 1B" (Without Altitude Control). (b) Altitude Control, (optional) Parts List Assembly No. 4379 6 lb. (-44) When Altitude Control is installed, the propeller installation must be made in accordance with Koppers Company Adjustment Instructions and Operating Limitations No. 54, Koppers Installation Dwg. No. 4275H and the engine must be modified in accordance with Aircooled Motors Corporation Dwgs. Nos. 18487, 18218 and SK-582-6. (c) Propeller - Kopper Aeromatic Hub F200, blades 00-74B or 00-74C 31 lb. (-56) Parts List Assembly No. 4275-1 Low pitch setting 14° at 24 in. sta., High pitch setting 26° Static rpm at maximum permissible throttle setting: Not over 2650, not under 2600. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. Installation must be accomplished in accordance with Koppers "Installation Procedure and Operating Limitations No. 84" (Without Altitude Control) Eligible only with item 110 engine. Tachometer must be red-lined at 2650 rpm. A-773 Page 3 3. Propeller - Sensenich, Controllable; Hub model CS3FR5, blade model 37 lb. (-56) PC376B4-2. (eligible with Item 110 engine only) Pitch settings at 3/4 radius: Low 13°; High 19.5°. Diameter: Not over 74 in., not under 72.5 in. 4. Propeller - Koppers Aeromatic; Hub F200H; Blades 00-74B 31 lb. (-56) Parts List Assembly No. 4275AH-1 Altitude Control Parts List Assembly No. 4370 6 lb. (-44) Low pitch setting 14° at 24 in. sta. Static rpm at max. permissible throttle setting: Not over 2650, not under 2600. No additional tolerance permitted. Diameter: Not over 74 in., not under 72.5 in. Installation must be accomplished in accordance with Koppers, "Adjustment Instructions and Operating Limitations No. 65" (Eligible only with Item 110 engine. Tachometer must be red-lined at 2650 rpm). Engine and Engine Accessories - Fuel and Oil System 101. Starter - Delco-Remy, part No. 10750 16 lb. (-26) 102. Generator - Autolite, part No. 10119 (15 amp) 12 lb. (-24) 103. Fuel pump - A.C. diaphragm type, part No. 11921 2 lb. (-31) 104. Oil cooler - Fedders (1311H) or heat exchangers (102) 6 lb. (-30) 105. Carburetor heater 2 lb. (-30) 106. Fuel strainer - Koehler K2250-B 107. Two mufflers - Kay Industries - (Bellanca Dwg. 15062) +1 lb. ea. (-34) 108. Generator - Delco-Remy 25 amp., part No. 1101887 +4 lb. (-24) 109. Oil filter - Fram PB5, kit No. K-501 Fram Installation Dwg. 61627 5 lb. (-19) 110. Engine - Franklin, 6A4-165-B3 (Negligible wt. change) Engine limits - 2800 rpm (165 hp) Fuel - 80 minimum octane aviation gasoline (Eligible with Item 2(c), 3 and 4 propellers only) Installation eligible only when original basic Franklin 6A4-150-B3 engine installation components utilized with no changes to aircraft structure. Landing Gear 201. Two main wheel-brake assemblies, 6.00-6, Type III, (a) Goodyear Model 6 IBD, 15 lb. (+8) Wheel Assembly No. 511413-M Brake Assembly No. 511640-M (b) Goodrich Model 605MD, No weight change Wheel Assembly No. D-3-105-MD Brake Assembly No. D-2-524 (c) Firestone Model DFA207, -1 lb. (+8) Wheel Assembly No. DFA180 Brake Assembly No. CFA252 (d) Goodyear Model CL6HBD (Castering wheels) 31 lb. (+8) Wheel Assembly No. 9530375/76 Brake Assembly No. 9530369/68 (Install in accordance with Bellanca Dwg. 18224) 202. Two main wheel, 4-ply rating, Type III tires, with regular tubes, (a) 6.00-6 18 lb. (+8) (b) 7.00-6 +3 lb. (+8) A-773 Page 4 204. Tail Wheel Assembly (a) Firestone Model CFA160, 6x2.00 2 lb. (+192) (b) Same as (a), steerable per Bellanca Dwgs. 15085 and 15091 +4 lb. (+192) (c) Maule Hub and Axle Model SFS-P8 Use actual wt. change General Tire 8.00 SC per Bellanca Dwg. 18222 208. Two Main Skis Use actual wt. change (a) Federal Model A2500, Federal Installation Dwg. 11R185 (b) Federal Model A2500A, Federal Installation Dwg. 11R185 (c) Federal Model A3500, Federal Installation Dwg. 11R185 (d) Federal Model A3500A, Federal Installation Dwg. 11R185 210. One Tail Ski Use actual wt. change Federal Model AT-3500 211. Electric landing gear retraction installation per Bellanca +7 lb. (+18.5) Dwg. No. 15103 Electrical and Radio Equipment 301. Battery - Reading R-24L 24 lb. (-17) 302. Radio equipment 12 lb. (-11) 303. Antenna and mast 1 lb. (+6) 304. Landing light - Grimes ST-250 3 lb. (+21) 305. Dual landing light installation - G.E. No. 4509 2 lb. (+9) Interior Equipment 401. Flares (5 one-minute, International) 17 lb. NOTE 1. Current weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be in each aircraft at the time of original certification at all times thereafter (except in the case of air carrier operators having an approved weight control system). NOTE 2. The following placards must be installed in full view of the pilot: (a) "Intentional Spinning Prohibited." (b) "Front seats must be occupied when used as three place." (Applicable to Model 14-13). ...END...