TCDS 4A1

Page No. 1 2 3 Rev. No. - - - Reformatted 2/94. DEPARTMENT OF COMMERCE CIVIL AERONAUTICS ADMINISTRATION 4A1 ANDERSON-GREENWOOD 14 October 2, 1950 AIRCRAFT SPECIFICATION NO. 4A1 Manufacturer Anderson, Greenwood & Company Houston, Texas I - Model 14, 2 PCLM (Normal Category), Approved September 20, 1950 Engine Continental C90-12FP Fuel 80 minimum octane aviation fuel Engine limits For all operations, 2475 rpm (90 hp) Airspeed limits Maneuvering 109 mph True Ind. Max. struct. cruising 132 mph True Ind. Never exceed 148 mph True Ind. Flaps extended 94 mph True Ind. C.G. range (+95.3) to (+98.5) at 1400 lbs. (+95.3) to (+100.9) at 1150 lbs. or less Straight line variation between points given. 1400 1300 1200 1100 1000 900 LBS 95 96 97 98 99 100 101 INCHES Empty weight C.G. range None Datum 88.5 in. ahead of wing center section leading edge. Leveling means Lugs on keel beam under cabin floor. Maximum weight 1400 lbs. No. seats 2. (+71) Maximum baggage 250 lbs. (+91) Fuel capacity 24 gals. (+95) Oil capacity 4.8 qts. (+113) 4A1 Page 2 Control surface movements Wing flaps 44° down Stabilizer Fixed Elevator 25° up 17° down Elevator tab 40° up 33° down Aileron 45° up 6° down Rudder 20° left 20° right Serial Nos. eligible 1 and up Required equipment 1, 2, 201(a), 202(a), 205(a), 206(a), 401, 601. Specifications Pertinent to All Models Certification basis Type Certificate No. 4A1 (CAR 3, Normal Category) Production basis None. Prior to original certification a CAA representative must perform a detailed inspection for workmanship, materials, and conformity with the approved technical data, and a check of the flight characteristics. Export eligibility Eligible for export to all countries subject to the provisions of ASR 312 (MOP 2-4 contains same information). 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. Hartzell adjustable pitch propeller, hub model HA-12UF-1, blades model 19 lbs. (+136.5) L7214. Pitch settings at 24 in. sta.: 18.75° to 20°. Static rpm at maximum permissible throttle setting: Full throttle - not over 2030, not less than 1810. No additional tolerance permitted. Diameter - not over 72 in., not under 70.5 in. 2. Extension hub - propeller Anderson, Greenwood Part No. 14-5006"A" 2 lbs. (+132) Engine and Engine Accessories - Fuel and Oil System 101. Starter - Delco Remy, Cont. No. 50309 16 lbs. (+107) Landing Gear 201. Two main wheel-brake assemblies, 6.00-6, Type III (a) Goodyear Model LF6HBD 12 lbs. (+110) Wheel Assembly No. 511960-M Brake Assembly No. 9520517 202. (a) Two main wheel 4-ply rating tires, 6.00-6, Type III 18 lbs. (+110) (with regular tubes). 205. One nose wheel, 5.00-4, Type III. (a) Goodyear Model 4NBM 3 lbs. (+15) Assembly No. 9520289 206. (a) One nose wheel, 4-ply rating tire, 5.00-4, Type III, 6 lbs. (+15) (with regular tube). Electrical Equipment 301. Battery - Reading S-24-12V 23 lbs. (+26) 302. Generator - Delco Remy, 12 amp. Cont. No.40435 10 lbs. (+107) 303. Regulator - Delco Remy, Cont. No. 40483 2 lbs. (+27) Interior Equipment 401. CAA Approved Airplane Flight Manual, dated September 19, 1950 4A1 Page 3 Miscellaneous 601. Aileron, flap, and elevator seal tape, Anderson, Weight negligible Greenwood Dwg. No. 14-8049. Installation as per Final Assembly Dwg. No. 14-0005. 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 and at all times thereafter (except in the case of air carrier operators having an approved weight control system). NOTE 2. The following placard must be displayed on the instrument panel in full view of the pilot: (a) "This airplane must be operated in accordance with the operating limitations specified in the CAA Approved Airplane Flight Manual." (b) "Operate in Normal Category in compliance with approved Flight Manual. Acrobatics (including spins) Prohibited." END