TCDS A-614

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A-614 Revision 2 AERONCA LC LCS March 7, 2005 AIRCRAFT SPECIFICATION NO. A-614 Type Certificate Holder National Aeronca Association 806 Lockport Road P.O. Box 2219 Terre Haute, IN 47802 Name change from Aeronca to National Aeronca Association March 7, 2005. I - Model LC, 2 PCLM, Approved July 25, 1936. Engine Warner Scarab Jr. Engine limits Maximum, except takeoff -- in. Hg., 2025 rpm (90 hp) Takeoff (one minute) -- in. Hg., 2025 rpm (90 hp) Airspeed limits Level flight or climb - 120 mph Ind. Glide or dive - 162 mph Ind. Flaps (See Item 17) - 108 mph Ind. Propeller Maximum permissible diameter 88 in. C.G. range (+11.5) and (+17) Empty weight C.G. range Not available Maximum weight 1680 lbs. Number of Passengers 1 (+19) Maximum baggage 115 lbs. (+39) Fuel capacity 28 gallons (one tank at 19 gallons in right wing (+27) and one at 9 gallons in fuselage (-11.5) Oil capacity 3 gallons (-21) Serial Nos. eligible 2015, 2021, 2028, and up manufactured prior to September 30, 1939 eligible. Approval expired as of that date. II - Model LCS, 2 PCSM, Approved July 25, 1936. Engine Warner Scarab Jr. Engine limits Maximum, except takeoff -- in. Hg., 2025 rpm (90 hp) Takeoff (one minute) -- in. Hg., 2025 rpm (90 hp) Airspeed limits Level flight or climb - 110 mph Ind. Glide or dive - 149 mph Ind. Propeller Maximum permissible diameter 86 in. C.G. range (+12) and (+16.7) Empty weight C.G. range Not available Maximum weight 1852 lbs. Number of Passengers 1 (+19) Maximum baggage 102 lbs. (+39) (including anchor and line) Fuel capacity 28 gallons (one tank at 19 gallons in right wing (+27) and one at 9 gallons in fuselage (-11.5) Oil capacity 3 gallons (-21) Serial Nos. eligible 2015, 2021, 2028, and up manufactured prior to September 30, 1939 eligible. Approval expired as of that date. Specifications Pertinent to all Models Datum Center section leading edge Leveling means Not available Certification basis Approved Type Certificate 614 (expired) (Aero. Bulletin 7-A) A-614 Page 2 of 2 Equipment: Class I: Landplane: 1. 3 inch wheels (Goodyear 3 LMBM) with 18x8-3 tires 2. 8 in. streamline tail wheel 3. Engine ring cowl 9 lbs. (-37) 4. Wheel streamlines 22 lbs. 5. Wood - fixed or adjustable pitch 15 lbs. (-45) Seaplane: Items 3 and 5 plus 7. Edo 47-1965 floats with water rudder 263 lbs. Class III. 10. Flares - three 1 min. (re duce baggage 15 lbs.) 10 lbs. (+80) 11. Flares - five 1 min. (reduce baggage 23 lbs.) 15 lbs. (+80) 12. Flares - three 1-1/2 min. (reduce baggage 26 lbs.) 17 lbs. (+80) 13. Landing lights (Grimes retractable) 10 lbs. (+19) 14. Battery and box (Exide 6TS7-1) 33 lbs. (+39) 15. Battery and box (Exide E-AC-7-1) 13 lbs. (+39) 16. Starter (Eclipse Y-150) 20 lbs. (-22) 17. Airbrake (flaps) (Landplane only) 6 lbs. (+11) 18. Cabin heater 4 lbs. (-22) 19. Special finish 8 lbs. (+60) 20. Special instruments 6 lbs. (- 5) 21. Battery 32 lbs. (+39) 22. Radio (RCA AVR-7 or 7A) 23 lbs. (+39) 23. Two 6-volt hot shot batteries for radio 20 lbs. (+39) 24. Battery (Reading 3-BRL-9) 9 lbs. (+39) 25. Carburetor heater 6 lbs. (-16) 26. Emergency window (left side) Note 1: Eligible for export as fo llows subject to inspection for equipment specified in Chapter XII of Inspection Handbook: (April 9, 1937) (a) Canada - Landplane - Skiplane -- not eligible - Seaplane -- not eligible (b) All other countries except Great Britain and Australia. Note 2: Aircraft eligible are also approved with: (a) Conventional or differential aileron cont rol with cable and push-pull tube control systems respectively. (b) Flap operating mechanism in cluding automobile window type lift. (c) Brake operating mechanism, including pedals, located between the rudder pedals and interconnected to a hand lever at the upper left side of the cabin. (d) Balanced elevators replacing unbalanced type. (Balanced type have increased area and increased tab area.) -END-