The Denali Scout
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DESCRIPTION: |
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The
Denali Scout, a variant
of the 8GCBC, features
the Lycoming IO-390-A1B6
engine paired with an MT
80 inch propeller.
The jump to 210
Horsepower (from 180)
provides exceptional
short field and climb
performance.
The
engine installation adds
several new features;
heavy-duty dynafocal
mounts, tuned 4 into 1
stainless exhaust, dual
oil coolers, and
electric fuel pump
accommodate and maximize
the performance of the
engine.
A sheet metal
cowling provides
improved access for the
wider engine.
The cowling
features large left and
right access doors with
removable upper and
lower sections.
A split
fiberglass nose bowl
retains the Scout
profile and provides
large air inlets for
engine cooling.
The
Denali Scout also comes
standard with an airfoil
tail (optional for the
standard Scout).
The 20% increase
in stabilizer area and
airfoil cross-section
provides strong control
with lightened stick
force.
Tundra tires and
vortex generators are
common options that
further increase the
utility of this powerful
airplane.
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Denali Scout Specifications |
| Powerplant |
Lycoming IO-390-A1B6 (210 hp) |
| Recommended TBO |
2000 hr |
| Propeller |
MTV-15-B/203-58 (80 in) |
| Length |
23 ft |
| Height |
8 ft 7 in |
| Wingspan |
36 ft 2 in |
| Wing area |
180 sq ft |
| Wing loading |
11.9 lb/sq ft |
| Power loading |
10.2 lb/hp |
| Seats |
2, tandem |
| Cabin length |
8 ft 10 in |
| Cabin width |
2 ft 6 in |
| Cabin height |
3 ft 11 in |
| Empty weight |
1420 lb |
| Maximum gross weight |
2150 lb |
| Useful load |
730 lb |
| Payload w/full fuel |
520 lb |
| Fuel capacity, std |
36 gal (35 gal usable) |
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216 lb (210 lb usable) |
| Fuel capacity w/opt tanks |
72 gal (70 gal usable) |
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432 lb (420 lb usable) |
| Baggage capacity, std |
100 lb, 10.4 cu ft |
| Bggage capacity, extended |
30 lb, 3.6 cu ft |
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| Performance |
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| Takeoff distance, ground roll |
388 ft |
| Takeoff distance over 50-ft obstacle |
708 ft |
| Maximum demonstrated crosswind component |
15 kt |
| Rate of climb, sea level |
1428 fpm |
| Maximum level speed, sea level |
150 mph TAS |
| Cruise speed, 6000ft |
136 mph TAS |
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72 lb/hr / 12.0 gph (75% power, best power) |
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126 mph TAS |
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50 lb/hr / 8.3 gph (65% power, best economy) |
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115 mph TAS |
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43 lb/hr / 7.2 gph (55% power, best economy) |
| Maximum operating altitude |
17500 ft |
| Service ceiling |
17500 ft |
| Landing distance over 50-ft obstacle |
816 ft |
| Landing distance, ground roll |
408 ft |
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| Limiting and Recommended Airspeeds |
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| VX (best angle of climb) |
56 mph IAS |
| VY (best rate of climb) |
82 mph IAS |
| VA (design maneuvering) |
118 mph IAS |
| VFE (max flap extended) |
102 mph IAS |
| VNO (max structural cruising) |
133 mph IAS |
| VNE (never exceed) |
166 mph IAS |
| VR (rotation) |
50 mph IAS |
| VS1 (stall, clean) |
54 mph IAS |
| VSO (stall, in landing configuration) |
45 mph IAS |
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