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Rihn Design Series DR-109
Type
Two seat aerobatic aircraft - competition and aerobatic training
Design Features
Low wing monoplane with a specially designed symmetrical airfoil,
16% thick, conic nose and flat sides. Large symmetrical ailerons.
Wire braced tail surfaces. Solo from rear seat. Cockpit equipped
with dual control sticks, dual rudder pedals, dual throttle, dual
propeller controls, dual trim controls, dual brakes, and dual
instrumentation.
Structure
Fuselage has a welded steel tube truss covered with sheet metal from
the firewall aft to the cockpit, aft the tail. Aluminum sheet metal
turtledeck. The tail surfaces are fabric covered and wire braced
with steel tube spars and bent up steel sheet metal ribs. The one
piece wing is all wood, Douglas Fir Box main spar, Douglas Fir
spars, plywood ribs and plywood covered. Large span ailerons are
built of wood and are plywood covered. The fiberglass engine cowl in
a two piece, split horizontally and is easily removable for ease in
maintenance.
Flying Controls
Pushrod actuated ailerons and elevator, cable actuated rudder.
Ailerons are mass balanced and aerodynamically counterbalanced. Each
aileron is fitted with a ground adjustable balance surface suspended
below the aileron. A trim tab on each elevator also acts as a servo
tab to reduce stick pressures.
Power Plant
Three engine options are available: AEIO-360 A1E6, 200 HP , AEIO-540
D4A5, 260 HP, AEIO-540 L1B5, 300 HP. The prototype DR-109 is
equipped with an AEIO-540 D4A5, 260 HP. Driving an MTV-9, three
blade variable pitch constant speed propeller. The main fuel tank is
located in the fuselage ahead of the cockpit, capacity is 30
gallons, auxiliary fuel for cross country is located in the wing,
capacity is 16 gallons. Total fuel capacity is 46 gallons.
Landing Gear
Non-retractable tail wheel type, main gear is a one piece aluminum
spring, tail wheel is steerable and full swivel mounted on a
cantilever steel spring. Main wheels are 5.00 x 5 with hydraulic
disk brakes.
Accommodation
Each cockpit seat has an adjustable seat back nominally reclined to
30 degrees and is equipped with a five point aerobatic seat belt
system.
Systems
Electrical system of 12 volts. Electric engine starter. Terra VHF
radio. Terra transponder with encoder. Grand Rapids Technology
Engine Information System (front and rear cockpit). Sigtronics voice
activated intercom.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
Lycoming
200/260/300 HP
x
22 ft
5.5 ft
24 ft
114 sq ft
2
1260/1350/1420
lbs
690/900/900
lbs
1950/2250/2320
lbs
30/45 x-country
404/450/430 mi |
performance
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
600 ft
x
192/205/215 mph
168/178/185
x
x |
limiting and recommended speeds
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
x
58 Solo/60 Dual mph
x |
All specifications are based on manufacturer's
calculations
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