Limitations Flashcards

1
Q

Flight Crew

A

May operate from either crew seat if dual controls and left DU are installed; otherwise pilot shall operate from right seat

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Max allowable cabin & baggage floor loading?

A

55lbs/sq ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Max cabin floor load

A

1200lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Max baggage compartment floor load

A

540lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Doors off configuration?

A

Any combination is approved for VMC flight. With hinged passenger doors removed, sliding door shall be full open or removed.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Max internal gross weight

A

7000lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Minimum gross weight

A

4400lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Basic Vne

A

155kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Max sideward/rearward flight, crosswind/tailwind hover

A

35kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Vne OEI op’s

A

140kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Minimum speed IFR

A

45kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Vne Searchlight extended

A

135kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Vne one or both crew doors removed

A

140kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Vne hinged or sliding aft doors removed

A

90kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Vne at 104% Nr

A

60kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Auto Min rate of descent

A

53kts

17
Q

Max operating altitude

A

20,000ft

18
Q

Slope limitations

A

10 degree side and nose up, 5 degrees nose down

19
Q

Max operating temp

A

125f/52c

20
Q

Min operating temp

A

40f/40c

21
Q

Powerplant

A

Pratt & Whitney 207D1/207D2

22
Q

Power turbine Np limit

A

continuous: idle - 100%
Max cont: 100%
Max continuous 60kts or less: 104%
Transient (20 seconds): 104-112%

23
Q

MGT start limits

A

Max (2 seconds): 875
Normal: 0-650

24
Q

Total Torque (QT)

A

Cont: 0-100%
Max cont: 100%
Transiet QT (5 seconds): 105%

25
Q

OEI Torque limiti

A

Cont: 0-50%
Max Cont: 50%
2 Minute: 50-64%
30 second: 64-66%
Max OEI: 66%

26
Q

Engine oil px

A

Min: 20%
Cont: 21-80%
Max: 80%
Max during warm up, 10 minutes: 99%

27
Q

Transmission Oil px

A

idle: 25-80 psi
cont 41-80 psi
Max: 80 psi
Max during warm up, 10 minutes: 130 psi

continued flight in 25-40 psi range is permitted. Appropriate maintenance is required prior to next flight.

28
Q

Transmission oil temp

A

cont: 15-110c
Max: 110c

29
Q

Rotor RPM - Power On

A

Cont: 99-100%
Max cont: 100%
Max cont, 60kts or less: 104%
Nr/Np excursions (100 +/- 3%) due to normal maneuvering or power changes are permitted

30
Q

Rotor RPM - Power Off

A

Minimum: 85%
Cont: 85-107%
Max: 107%

31
Q

Hydraulic Px

A

Minimum: 1250 psi
Cont: 1250-1800 psi
Max: 1800psi

32
Q

Max Hydraulic Temp

A

120c

33
Q

Fuel capacity

A

Basic usable: 215 gallons

34
Q

Rotor Diameter

A

36 feet

35
Q

Max GW external

A

8000lbs

36
Q

Engine Oil Temperature

A

14-127c

37
Q

Hyd fluid temp

A

-20-120c

38
Q

Fuel low light

A

15 minutes/engine remaining

39
Q

Length

A

38’6’ nose to tail
43 blade to tail