5powerplant
Pratt & Whitney 206C
6rotorhead and tailrotor type
fully articulated, teetering
7Main electrical system
28V DC
9minimum allowable helipad size
15mX15m, elevated= 20mX20m
10max nose up attitude
10*
11max nose wheel angle
40*
13min rotor NR before you are able to move the cyclic
85%
15with 102% nr, maximum IAS?
120kts
16Max crosswind component (class 1)
20kts
17torque limits OEI
max continuous= 124% , max 2.5min=142% , transient=156%, max 180%
18torque limits AEO
continuous=100%, transient=110%
22minimum IFR airspeed
50kt
23min speed in IFR approach
55kt
25max taxi speed
20kt straight, 10kt turning
26minimum gross weight
1850kg
28max floor load
500kg/m2
29servo system 1
1.6L, utilities and tail
30servo system 2
3L , utilities and emergencies
31what happens to cofg when fuel is consumed
moves forward
32transmission oil capcity
11L
34tail rotor oil capacity
0.2L
35max engine oil temp
120*C
36eng starter disengaged at X%
50%
37RRPM below what % before rotor brake can be applied
40%
38normal clear area TDP
15ft 30kt
40short field (helipad) TDP
80ft 0kt
43power off NR limits
min 90%, max 110%
44transienr NR figure AEO
112.4%
45max oil pressure for oil start
200psi
46how many thermocouples per engine exhaust
8
47how long to gyros take to shut down before towing
20mins
49how many fuel nozzles and what types
5 hybrid nozzles for startup, 7 air blast nozzles