TCDS TC 714

MODEIS: Waco ARE, HRE (Army UC-72C), SRE (Army UC-72) I-C. NUMBER: 714 I - MODEL ARE 5 PCLB (Approved 2/1/40) Engine Jacobs I-6MB Fuel 80 minimum octane aviation gasoline Engine limits махіти, except take-off (Sea level) 24.5 in.Ag.. 2100 rpm (300 hp) (Straight line manifold pressure variation with 23.5 in.Hg.. 2100 rpm (300 hp) Take-off (one Airspeed limits Level flight or climb - 200 mph (T. I.A.S.) Glide or dive - 270 mph Flaps extended - Propeller limits Maximum permissible diameter 110 inches C.G. range Maximum weight No. seats (one at (-13), three at (+22)) (pilot at (-13)) Maximum baggage Fuel capacity 125 gallons (62-1/2 gallon tank in each upper wing (-14) (See Item 208) o1_ capacity 6-1/4 gallons (-56) Control surface movements Not available Serial numbers eligible Required equipment Items 101, 102, 111, and up per NOTE A (a) ' 112 103, 104, 105, 106, 107, 108, 109, 110(a), II - MODEL SRE (Army UC-72), 5 PCIB (Approved 4/6/40) Engine P & W Wasp Jr. SB with one 4-1/2 N and one 9 N (See also Item 212) Fuel 80 minimum octane aviation gasoline for maximum, except take-off and take-off at 400 hp; 87 minimum octane aviation gasoline for take-off Engine limits except take-off (See also Item 212) (Sea level) 34.5 in.Hg.. 2200 rpm (400 hp) (Straight line manifold pressure variation with altitutde to 5000 ft.) 33.6 in.Hg.. 2200 rpm (400 hp) Take-off (one minute) 34.5 in.Hg., 2200 rpm (400 hp) 36.5 in.Hg.. 2300 rpm (450 hp) Airspeed limits Level flight or climb - 200 mph (I.I.A.S.) Glide or dive - 270 mph Flaps extended - 108 mph Propeller limits Maximum permissible diameter 108 inches C.G. range Maximum weight No. seats 5 (one at (-13), three at (+22)) (pilot at (-13)) Maximum baggage 100 1bs. (+52) Fuel capacity 125 gallons (62-1/2 gallon tank in each upper wing) (See Item 209) cil capacity Control surface movements Not available Serial numbers 5076 and up per NOTE A and all AAF numbers Required equipment Items 101, 105. 110(2). 111, 103, 104, 105, 106, 107, 108, III - MODEL HRE (Army UC-72C), 5 PCIB (Approved 11/1/40) Engine Fuel Maximum except take-off2300 rgm (300 k.p) 87 minimum octane aviation gasoline Engine limits Airspeed limits level flight or climb (one minute) ' - 200 mph 2200 km (285 hp) (T.I.A.S.) Glide or dive - 257 mph laps extended - 108 mpr C.G. range Maximum weight No. seats (one at (-13), three at (+22)) (pilot at (-13)) Maximum baggage (See NOTE 2) Fuel capacity (62-1/2 gallon tank in each upper wing) (-14) (See Item 208) oil capacity (See Item 208) control surface movement Not available Serial numbers eligible 5097 and up per NOTE A and all AAF numbers Required equipment Items 101, 102(c) 113 and 114 103. 104. 105. 106. 107, 108, 109, 111, 112, SPECIFICATIONS PERTINENT TO ALL MODELS Datum Leading edge of lower wing Ieveling means Lower surface of left upper wing Certification basis Type Certificate No. 714 (CAR 4a) Production basis None (See NOTE A) Export eligibility Eligible for export as follows, subject to provisions of MOP 2-4: (a) Canada - Landplane - eligible - Skiplane - not eligible. (b) All other countries except New Zealand. EQUIPMENT: Fropellers and Propeller Accessories 102. Propeller (a) Controllable metal (Hamilton Standard 2B20 hub, 6135A-9 or 6135A-10 blades. Diameter 8'3-1/8" maximum, 817/8" minimum, low pitch setting 13 degrees) 105 1bs. (-92) (k) Constant speed metal (Hamilton Standard 2D30 hub, 6167A-12, 6167A- 13, 6101A-18 or 6101A-19 blades. Diameter 8'6-1/8" maximum, 8'3-7/8" minimum, low pitch setting 10 degrees) ___ 150 1bs. (-89) (c) Controllable metal (Lycoming-Smith P220 propeller with S0200806 or s0220806 clades, low pitch setting 217. Propeller - 10 degrees) fixed --_ (26) S91 121 pitch metal (Curtiss 55501) (Static rpm at maximum permis- sible throttle setting - not more than 1910; not less than 1660. Diameter - not more than 99 inches, not less than 96 inches). -50 1bs. (-92) 224. (a) Constant speed propeller governor and governor control (Drawing 47-761. Pitch range 12 degrees to 27 degrees. FOI installation with item 102 (a) . 7 1bs. (-61) (k) Constant speed propeller governor and governor control (Drawing 47075) . Pitch range 10 degrees to 23 degrees. For installation with item 102 (b). 7 Ibs. (-58) Engines and Engine Accessories - Fuel and Oil System 101. Engine cowl 103. Starter (Eclipse (NACA) 35 lts. 8 1-77) "35 1bs. #R-70T 110. Oil radiator E-80) 20 1bs. (-55) 20 1bs. (-55) 20 1bs. (-57) (a) One (Winchester 5 inches) 5 1bs. (-77) (D) TWO (Winchester 4 inches) 8 1bs. (-74) --_ 205. larger starter *10 1bs. (-58) *10 1bs. (09-) *10 1bs. (-59) 208. Tanks (a) Auxiliary 38 gallon fuel tank 35 1bs. (25+) (k) 8-1/2 gallon oil tank 8 1bs. (-56) (c) 58-1/2 gallon aluminum alloy replacing 62-1/2 gallon Fairprene wing tanks (Aero. services, Inc. Drawings numbers 100 and 101) +20 158. (-19) +20 lbs. - 74 +20 1bB: (-14) 211. Vacuum pump +4 1bs. - 43 212. Engines (must have one 4-1/2N and one Use actual weight 9 N damper) increase (a) PEW Wasps Jr. SB-2 (limits same as SB) (k) PEW Wasps Jr. SB-3 (limits same as SB) (C) P&W Wasps Jr. T1B2 Limits - Maximum, except take-off (Sea level) 35 in Ng.. 2200 rpm (400 hp) (Straight line manifold pressure variation with altitude to 3800 ft.) 34 in.Hg.. 2200 pm (400 hp) Take-off (one minute) 35 in.Hg.. 2200 rpm (400 hp) 37.5 in.Hg.. 2300 rpm (450 hp) (d) PEW Wasps Jr. T1B3 (limits same as T1B2. Item 212 (c) above) (e) Military R-985-AN-4 (limits same as SB) (f) Military R-985-AN-6 or -AN-6B (limits same as SB) (g) M1litary R-985-AN- 12 or -AN-12B (limits same as SP) (h) Military R-985-AN- 14B (limits same as SB) (1) Military R-985-25 (limits same as I1B2, Item 212 (c) above) (J) Military R-985-AN-1 Or -AN-3 (limits same as I1B2, Item 212 (c) above 223. Interconnected throttle-mixture control (Drawing 47073) No weight change Landing Gear and Floats 106. Wheel cuffs 4 1bs. (-33) W Ibs. (-33) 107- 7.50-10 wheels (Goodyear) with brakes and 6-ply tires (wheels must be placarded for these tires) 63 1bs. (-33) 63 1bs. (-33) 63 1bs. (-33) 108. 10x3 heavy duty tail wheel and 4-ply tire 5 1bs. (+196) 5 1bs. (+196) 5 Its. (+196) 210. Cactus proof inner tubes +12 1DS. (-33) *12 lts. (-33) + 12 Its. (-33) 216. wheel streamlines 22 lbs. (-33) 22 1bs. (-33) 19 1bs. (-33) 222. Steerable tail wheel (Drawing 48811) No weight change No weight change No weight change Electrical Equipment 104. Generator (15 amp.) 21 158. (-55) 21 1bs. (-60) SRE 27"158.1 (-59) 105. Battery and box (Exide 6-TS-13-1) 42 1bS. (-68) (*65) 42 1bs. (+65 OI +108) 42 1bs. (*65) 112. Shielding 11 Ibs. 11 lbs. (-68) 11 1bs. (-68) 113 or 220. Bonding 6 1bs. (-3) 6 1bs. (-3) 6 1bs. (-3) 114 or 219. Landing lights (Grimes retractable) 10 1bs. (-38) 11 Ibs. (-23) 11 Ibs. (-23) 204. Larger generator *10 1bs. +10 1bs. (-55) +10 1ks. (-57) 225. Battery and box (Reading (R-33-L)) 32 1bs. (-63) 32 1hs. (-63) Interior Equipment ARE SRE 109. Control column - throw over type 11 1bs. (-33) 11 1bs. (-33) 11 1bs. (-33) 111. Cabin heater and ventilating system 8 lbs. 6 lbs. 8 lts. 2(a) Are nuishers Pressure Pressure (Lux) 20 1bs. (+22) (-53) 20 lts. 8 lts. (+22) (-53) 15 1hs. 20 lbs. (-53) (+22) 202. Parachute seats * 30 1Ds. 1-13 +27 +41 lts. (-23) +30 168. (-73) +41 Its. (C) Front +30 1bs. 207. (a) Cargo type compart- ment (Drawing 49073) (loading instructions required) + 36 1bs. (+32) 36 ibs. (+38) 36 lbs. (*32) (t) Large baggage door + 16 lbs. (+52) +16 1bs. 209. Control column - "y" type +4 1bs. (-33) +4 1bs. (-33) +4 Ibs. (-33) 214. Flares (three 1-1/2 minute) 17 1bs. (+78) 17 1bs. (+78) 17 1bs. (+78) Miscellaneous (not listed above) ARE SRE 200. Extra door and wing walk + 16 10. (+19 *16 155 (+19) + 16 1bs. (+ 19) 218. Quick release door 1 1b. 1 1b. 1 1b. (+ 19) NOTE A. Each aircraft manufactured after 4/13/43 for civil use, must, prior to original certification, satisfactorily pass: An inspection for workmanship, materials and conformity before any covering, metal priming or final finish is applied. All' woodwork may be varnished. (L) Final inspection of the completed aircraft. Check of flight characteristics. The following placards must be displayed in full view of the pilot: "Use left wing tank before using right tank. Operate auxiliary fuel pump while flying on left tank until auxiliary tank gage shows empty. NOTE 2. Weight and balance report must be submitted for each aircraft with original inspector's report and each subsequent report covering a change Loading instructions, when necessary, must be included in he Aircraft Operations record and the baggage compartment must be placarde‹ accordingly.