TCDS TC 2-583

AMERICAN EAGLECRAFT COMPANY MODELS: American Eaglet A-31-1B, 2 PO-CIM T.C. NOMBER: 2-583 (Approved 7/3/46) Engine Continental A-50-8 or A-50-8F Fuel 73 minimum octane aviation gasoline Engine limits For all operations, 1900 rpm (50 hp) Airspeed limits Level flight or climb - 100 mph True Ind. Glide or dive - 120 mph True Ind. Propeller limits Static rpm at maximum permissible throttle Not more than 1750, not less than Not more than 76 in., not less than 74.5 in. C.G. range (*12.4) (21.2 percent MAC) to (+18.6) (31.8 percent MAC) At 1100 1bs. maximum weight: (+17.0) (29.1 percent MAC) to (+18.6) (31.8 percent MAC) (Straight line variation between forward limits for intermediate weight) Datum Wing leading edge (with airplane level) MAC 58.4 in I.E. of MAC at (0) Leveling means Top longeron on left side in cockpit Maximum weight NO - seats 2 (front at (+15), rear at (+42)) Baggage Fuel capacity 0i1 capacity 1 gallon (-38) Control surface Elevator Up 18 degrees Down 19 de movements Aileron 17 degrees 18 de Right 48 degrees Left 48 de Stabilizer Fixed Serial Nos. eligible 1201 and up (See NOTE A) Required equipment Airloithloess Certificate only (CAR 04a) Certification basis Production basis None (See NOTE A) eligible for export as follows in Chapter XII of Manual of Procedure. subject to inspection for equipment sp Canada - Landplane - eligible skiplane - eligible All other countries except Australia and New Zeland. Equipment: Items included in required list under specifications pertinent to individual models may not be removed unless replaced by approved equiv The effect upon balance of all equipment changes must be computed the aircraft operations record revived accordingly Values in inches shown in parenthesis after each item represent horizontal arrs to the C.G. of the item measured minus (-) (+) to the rear of the datum. A plus (+) (-) sign preceding weight of an optional item indicates the net weight change between tha the equivalent required item. Propeller and Propeller Accessories Propeller (including hub) Fahlin D371-48(76) 16 1bs. (-56) 0 other fixed pitch wood propeller eligible for the engine and power and which meets the static rpm and diameter specified under "Propeller limits" on Page 1. Engine and Engine Accessories 101. Carburetor air heater 2 1bs. 1-38 Landing Gear Goodyear Model 3-LNBM with 18x8-3 4-ply tires 26 1bs. (+2) Goodyear Model I6NBD with 6.00-6 4-ply tires 25 1bs. (+2) 202. Tail wheel Uniloy Model 3000-A1 with Pirestone 6x2 solid tire • 1DS. 1+20 Scott type 3000B-2 • 1bs. 1+20 Interior Equipment 401. Cabin enclosure (American Eaglecraft Drawing D-27-02) 8 1bs. (+29 Miscellaneous (not listed above) 600. Miscellaneous items as noted in the approved weight and balance report. Each aircraft manufactured must, prior to original certificat satisfactorily pass: An inspection for workmanship, materials and conformity to tr pertinent technical data before any covering, metal final finish is applied. All woodwork may be varnished. A final inspection of the completed aircraft. (c) A check of the flight characteristics. NOTE 1- the rollowing permanent placard should be dispidyed on int instrument panel in full view of the pilot "INTENTIONAL ACROBATICS PROHIBITED. SOLO FROM FRONT SEAT ONLY."