Limitations Flashcards
Max Altitude
15,000ft
Temperature Range
-40°C up to ISA +35°C
Max Weight
4600kg
(4800kg with sup 30)
Min Weight
3300kg
VLE
Vne - 8kts
VLO
130kts
Aircraft Length
14.64m (48ft)
Rotor Diameter
12.12m (39.76ft)
D Value
15D
Max Occupants
10
Max Tow & Taxi weight
4650kg
Vne (Power On)
165kts
Vne (Power-Off)
125kts
Max airspeed AEO with Tq above 100%
90kts
Vmini
50kts
Max airspeed for IFR approach up to 5000ft
130kts
Max airspeed with one AP failed
120kts
Max airspeed for operation of windscreen wipers
140kts
Minimum airspeed in autorotation
50kts
Max airspeed for opening & closing the sliding door and with one door locked open
80kts
Max airspeed with both sliding doors locked open
100kts
Max taxi speed
40kts GS
Max rolling takeoff and landing speed
60kts GS
Max speed for emergency landing
60kts GS
What must the pilots do when the hydraulic fluid is below +20°C?
Must fly attentive
Starting & stopping the rotors envelope
+/- 5deg = 50kts
Otherwise 40kts
Sloping limits
10U/7D/10L/10R
AEO <90kts PI Ranges
100% = Max Continuous
101-111% = 30 min Take-Off
111% = Max 30 min
125 = Max Transient (10s)
AEO >90kts PI ranges
100% - Max Cont.
125% - Max trans. (10s)
OEI PI Ranges
140% = Max Cont
Where is the Empty Weight found?
Chart C of Section 6
What is Chart B used for (W&B)
Used to computer the helicopter Empty Weight after the helicopter is weighed.
