TCDS ATC 662

MODELS: General Dynamics (Consolidated Vultee) (Barkley-Grow) T8P-1, 10 PCI-SM I.C. NUMBER: ATC 662 Engines 2 PEW Wasp Jr. SB with one 4-1/2 N and one 9 N' Fuel 80 minimum octane, 97 minimum octane for take-off Placard limits Maximum, except take-off 34.5 in. Hg.. 2200 rpm (400 hp) manifold pressure variation with altitude to 5000 ft.) 53.5 in. Hq., 2200 rpm 36.5 in. Hg., 2300 rpm (450 hp) Placard speeds Level flight or climb - 209 mph True Ind. Glide or dive - 270 mph True Ind. Flaps extended - 117 mph True Ind. Level flight or climb - 193 mph True Ind. Glide or dive - Flaps extended - 117 mph True Ind. Placard ceiling Landplane - 0 ft. usable in standard air at a750 lbs. with either engine inoperative and the inoperative propeller idling in high pitch Seaplane - 0 ft. usable in standard air at 9200 lbs. with either engine inoperative and the inoperative propeller idling in high pitch Fuel capacity 156 gallons (two tanks in each wing) oil capacity 16 gallons (two tanks, 8 gallons each 2 at -61, 2 at -94, 2 at - (2163) No. passengers Baggage 430 1bs. (Nose compartment 250 1bs. (-228) ; aft of cabin compartment (includes anchor and line 30 lbs. and ladders 23 1bs. when carried) Standard weight Landplane - 8750 1bs. (See NOTES 3 and 4) C.G. limits Landplane (-137.2) and (-125.4) Seaplane (-137.3) and (-127.2) - 91.42 in. L. E. MAC (- 154.4) Spec. basis Approred Type Certificate No. 662 Serial Nos. 1 and up manufactured prior to 10/25/40 eligible. Approval expired that date due to Vultee Aircraft, Inc. (now Consolidated-Tultee) EQUIPMENT: increase) (tue is front face of the rear cabin bulkhead) (* Means net (See NOTE 6) Class I: (a) Landplane 101. Two engine ring cowls 51 1bs. (-204) 102. Two exhaust collector rings (including 103. carburetor heaters) Two oil radiators (UAP 5") 110 1bs. 21 Ibs. (-166) (-191) 104- Two starters (Eclipse E-160) 71 1bs. (-184) 105. Generator (Eclipse D) 25 amp. 22 1bs. (- 191) 106. Battery (Exide or Blectric 6-IT-13-1) 65 1bs. (-2191 107. 30x13-6 wheels (Goodyear 6HBM) with 6-ply heavy duty tires (27-1/2 1bs. air pressure) (Wheels must be placarded for this tire.) 148 Ibs. (-153) 108- 13.25 in. streamline tail wheel and 6-ply heavy duty tire (40 1bs. air pressure) (Wheel must be placarded for this tire and pressure.) 8 1bs. (+136) 109. Shock struts (Aerol SP-325 BG) 65 1bs. (-153) 110- Tail wheel shock strut (Warner Aero BG Drawing No. B-1200) 12 1bs. (+134 20 1bs. - 1431 Cabin heaters 112. 113. Wheel fairings Flap control motor (Elec. Spec. HCA-2 .65 hp) 49 155- (-153) (-74) 114. Two propellers - Hamilton Standard hubs 2D30, blades 6167A-6 to 6167A-8 inclusive. it. propellers 316 1bs. (-219) or 6106A-12 to 6101A-14 inclusive. Miameter pel/er maximum, 8'9-3/4" Diameter 326 1bs. (-219) minimum. 116. Residual fuel and oil 13 1bs. (-140) (b) Seaplane: Items 101 to 106. inclusive, 111, 112, 114 and 115 PLUS 151. Edo 65-9225A float installation (including water rudders, struts and fairings) 1162 1bs. (-130) 153: Seaplane fittings Auxiliary fin (Drawing Y-160) 42 1bs. 6 1bs. (-107) (+1361 class I1: 200. Miscellaneous items as noted in approved weight and balance report 201. Constant speed propeller controls installation 13 1bs. 1-192 202. 203. Exhaust analyzer (Cambridge) Vacuum pumps (2) (Pesco Type B-A-1) 11 1bs. 16 1bs. (-194) 1-175 204. Radio, variable. Structure has been substantiated as follows: (a) (b) In nose compartment On floor under pilots' chair 40 1bs. 57 1bs. (C) (₫) on floor under co-pilot's chair on fuselage roof 40 10 1bs. 1bs. (e) on instrument panel (controls) 17 1bs. (Е) Twin antenna 11 1bs. (9) Single antenna 10 1bs. (п) Bonding 26 1bs. 205. 206. Two flares and brackets (3 min.) Miscellaneous instruments 10 1bs. 50 Ibs. (+42) 01 (-217) (-199) 207. Iwo landing lights (A & W, type A-7) and passing light 3 1bs. (-161) 0I (-253) 208. Pressure fire extinguisher (Richlux c0-2 -- 7-1/2 1b. charge) 29 1bs. (-216) 209. 210. 211. Toilet equipment 30 gallon nacelle fuel tank (1 or 2) Radio shielding 28 1bs. 30 1bs. 21 1bs. each (-133) (-5) (-196) 212. TWO oil radiators (UAP 5 1bs.* (-166) 213. Battery (Exide 6PHM-13) 11 1bs. * (-219) 214. Three place divan 74 1bs. (-104) 215. 216. Closet (clothing) Rear partition and doors 25 8 1bs. 1bs. (-46) (-24) 217. Food compartment 34 1bs. (-57) Class III: 301. Shock struts Clev. Pneu. Tool Co. No. 7881 14 1bs.. (-153) Cler. Pneu. Tool Co. No. 7887 32 lbs.* (-153) 302. Pilots compartment hatch (Drawing 2-P-064) 3 lbs.* (-221) NOTE 1. Serial Nos. 1 and 2 are eligible as 8-place aircraft only. Placard lavatory door for these serial numbers, Not to be occupied during take-off or landing", unless otherwise substantiated by pertinent weight and balance report. NOTE 2. Eligible for export as follows subject to inspection for equipment specified in Chapter XII of Inspection Handbook: (10/25/40) - Skiplane - not eligible. However, structure of serial numbers and up complies with Canadian ski gear requirements when modified in accordance with Drawing IX-1731-D. Serial Nos. 4 and up incorporate these modifications. 7881 (Item 301a) must be used with roll-on type skis and 7887 (Item 301b) must be used with streamline type. Seaplane - maximum standard weight 9200 1bs. All other countries except Australia and Great Britain. 1 eligible as landplane only at 8250 1bs. standard weight with the following: Split flap under fuselage. Certain castings of aluminum alloy instead of magnesium alloy. Adjustable trim tabs on both rudders. C.G. limits (-137.2) and (-123.4). Serial No. 2 eligible as landplane only at 9250 1bs. standard limits (-137.2) and (-123.4). Serial No. 2 and up may have extensions on rudder and right aileron adjustable trim tabs. NOTE 5. Placard one wing tank filler neck or cap: "97 minimum octane fuel only." Placard fuel tank selector valve to use this tank for take-off and landing. Weight and balance report including list of equipment included in certificated weight empty, and loading instructions when necessary, must be submitted for each aircraft with original inspector's report and each subsequent report covering change in such equipment.