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Mission
M212-200 (Lambert)
The Mission M212 is a
single engine light aircraft of conventional configuration. It has an
unswept straight-tapered low wing. The fuselage provides side-by-side
seating and has sufficient room to accommodate four adults. In the initial
design stages, significant attention was paid to visibility, comfort and
ergonomics. The single piece forward hinging canopy provides excellent
visibility in level flight as well as in turns. In addition, the clean
arrangement ensures a good and water proof seal and keeps aerodynamic
noise low. Both the seats and rudder pedals are adjustable. Elevator and
aileron control is by sticks. The aircraft is standard equipped with full
dual controls.
Control surfaces are conventional with single slotted flaps and an
all-moving horizontal tail. The main landing gear consists of a cantilever
leaf spring and the steerable nosewheel is of the telescopic
oleo-pneumatic type. The airframe is all composite. Construction is mainly
of glass fibre and epoxy. Carbon reinforcements are used in spars and
longerons where additional stiffness is required.
specifications
powerplant
propeller
length
height
wing span
wing area
seats
empty weight
useful load
gross weight
fuel capacity
range |
DeltaHawk DH200A4
200 HP
x
24 ft 3 in
9 ft 6 in
32 ft 2 in
129 ft²
x
1620 lb
x
2535 lb
42 us gal
x |
DeltaHawk DH200A4
200 HP
x
24 ft 3 in
9 ft 6 in
32 ft 2 in
129 ft²
x
1620 lb
x
2535 lb
42 us gal
x |
performance
|
DeltaHawk DH200A4
200 HP |
DeltaHawk DH200A4
200 HP |
takeoff distance,
ground roll
rate of climb
max speed
cruise speed
landing distance, ground roll
service ceiling |
820 ft
1020 ft/min
144 kt
141 kt
x
x |
920 ft
900 ft/min
144 kt
137 kt
x
x |
limiting and recommended speeds
|
DeltaHawk DH200A4 |
XP-360 engine /Lycoming O-360 |
design manoeuvring speed (Va)
never exceed speed (Vne)
stall, power off (Vsl)
landing approach speed |
x
x
53 kts
x |
x
x
53 kts
x |
All specifications are based on manufacturer's
calculations
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