Section 2 Limitations Flashcards
What is the maximum gross weight?
2910 kg
or
6415 lbs
with increased gross weight supplement 9.1-3
2950 kg
or
6503 lbs
What is the minimum gross weight?
1500 kg
or
3306 lbs
What are the floor loading limits?
600 kg/sq meter
or
122 psf
max per tie down ring
100kg
or
220 lbs
What is Vne?
155 kts up to 30 degrees at SL
155 up to 2,000’ at 10 degrees
150 above 2300kg (5071 lbs)
140 above 2720 up to 2910 (6415)
What is max Vne for OEI?
110 kts
What is max Vne for steady autorotation?
90 kts
What are the altitude limitations?
Maximum operating altitude
20,000 ft
Maximum operating altitude for hover in ground effect/takeoff and landing is
15,000 DA
For gross weight above 2720 and up to 2835
Maximum operating altitude
12,000 ft
For gross weight above 2835
Maximum operating altitude
10,000 ft
What are the ambient air temperature limits?
Minimum -35C
Maximum ISA +39C
(Max +50C)
For OAT >/= 30C cockpit ventilation must be set to maximum
For engine startup below -20C, using the aircraft battery, the battery shall be preheated to at least -20C
What are the main rotor limits above 1900 kgs (4193 lbs)
Power on
97-104%
Power off
85-106% (transient to 112%)
Explain the main rotor visual and audio warnings
97%
Steady light
Intermittent low tone
106%
Flashing light
Gong
112%
Flashing light
Continuous high tone
What are the engine starting limits?
Automatic TOT limiting at approx.
5.5 FLI or 650C
2 sec transient
8.3 FLI or 760C
Max starting peak
10.7FLI Or 875C
What is the takeoff power limit?
10.0 FLI
2 x 78% torque
869 TOT
98.7 N1
104 N2
Airspeed must be less than Vy (65 kts)
What are the max continuous power limits?
9.0 FLI
2 x 69% torque
835 TOT
97.4 N1
104 N2
What is the max continuous power limit OEI?
- 0 FLI
- 5% torque
900 TOT
100.4 N1
104 N2
What are the 2 min OEI engine limits?
13.0 FLI
125% torque
950 TOT
102.6 N1
104 N2