en l'état ELECTRICAL EQUIPMENT
(24-Volt System)
Two 60-Amp Alternators (60 Amp to. 20,000 ft., 50 Amp at
30,000 ft.)
Battery - Nickel Cadmium, 13 Ampere-Hour Capacity Two Voltage Regulators
Electric motors for operating flaps and landing gear
Electrically Operated Cowl Flaps
Heated Pitot Tube
Heater Blower (Ventilation)
Heater Blower (Combustion Air)
Auxiliary Fuel Boost Pumps
External Power Receptacle
Fuel Vent Anti-Icer (Electric)
Heated Stall WarningCONTROLS
Conventional 3 Control System (Pilot's and Co-Pilet's)
Individual Tee Operated Brakes (Left Side)
Parking Brokes with Mand Contret
Ventilation, Meatico and Pressurization Control
Alleron, Rudder end Elevator Trim Tabs Adiustable by
Control
Wheels
Power Plant Controls in Console
Electrie landing Gear and Flop Controls
Auxiliery Londing Gear Extension Control
Alternate Static Air Source and Line DrainTow Bar
Service Information Kit
Coat Hanger
Pitot Tube Cover
Sump
Drain Wrench
Three Jack Pads
Two Engine Log Books
Airplane log Book
Control Lock Assembly
Pilot's Check List
Power Computer
SPECIAL FEATURES
Single Point Fueling
Each Wing
Quick Removable Gas Tank Caps
Inboard Main Wheel Doors close when wheels are down to keep ouf mud and dirt and prevent buffeting damage
Chair Reclining Mechanism allows vertical to horizontal adjust-
ment on three passenger chairs
Exterior Step Actuates with Landing Gear
Annunciator Panel
Static Wicks
All Specifications Subject to Change Without NoticeBencheraft)
DUKE AGO
A four to six plate, twin engine, high performance, turbo-charged, pressurized monoplane with fully retractable tricycle landing gear Standard equipment includes avionics and a full complement of engine and flight instruments. Licensed in normal category.
Designed and tested in excess of the
required load factors.1,318 4
2,380 4
the aboxe performance figures are based on maximum gross weights and are the results of flight tests of the Duke A60 conducted by Beeck, Aircraft Corporation under factory controlled conditions any
with very with individual aircraft and numerous factors affecting flight performance(requires B16 Antenna)
Glideslope Incorporated in AVN-210 (requires A-326A GS Antenna)
Beech Metal Radio Panel
Static Wicks
Single Audio Switch Panel
Mic Key Button in Pilot's Control Wheel
White Lighting
KA-25 Amplifier
Microphone, Headset and Cabin Speaker Avionics Master Switch
ENGINES AND EQUIPMENT
Two Lycoming 6-cylinder TO 541-ElA\ Turbocharged Engines rated at 380 hp, 2900 rpm for takeoff and continuous operation.
Propellers - 74? Diameter, 3 Bladed Aluminum Alloy, Constant
Speed, Full Feathering with Hydraulic Governor Starters
Fuel Boost Pumps
Exhaust Manifolds (stainless steel)
Pressure Pumps
Non-Congealing Oil Radiafors
Full-flow Oil Filters
Sonic Choke Venturis for Cabin Pressurization
LANDING GEAR AND BRAKES
Tricycle type with swiveling steerable nose wheel equipped with shimmy dampener. Beech, oil air struts on all wheelsSonic Choke Venturis for Cabin Pressurization
LANDING GEAR AND BRAKES
Tricycle type with swiveling steerable nose wheel equipped with shimmy dampener. Beech oitair struts on all wheels designed for smooth taxiing and to withstand the shock created by landing with a vertical descent component of over 600 feet per minute
Main Jires, 6.50" × 8"' (Tubeless)
Nose Wheel Tire, 6.00" x 6" (Tube)
The DraLec
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