H500 Flashcards

(31 cards)

1
Q

min weight for flight

A

1538 lbs

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2
Q

Max gross wt

A

3000 lbs

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3
Q

TOT limitation, max before engine start

A

150 deg

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4
Q

Cargo deck weight limit

A

1300 lbs (115lbs/sq ft)

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5
Q

VNE

A

152 kts All Doors on

130 kts Doors off, with fuel below 35lbs, in autorotation

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6
Q

Utility cargo storage weight limit

A

50 lbs

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7
Q

TOT max continuous limit

A

738 deg with torque above 74.3 psi

755 deg with torque at or below 74.3 psi

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8
Q

Rotor break limitations

A

Must be stowed before engine start,

205 rrpm after engine shutdown

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9
Q

Rotor rpm power on normal operating range

A

487- 492rpm (102-103%N2)

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10
Q

Rotor RPM power off Min limit

A

410 rpm (87%N2)

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11
Q

Rotor rpm power on max limit

A

492 rpm (103%N2)

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12
Q

Gas producer (N1) min ground idle speed limit

A

Minimum 60%

Preferred 60-65%

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13
Q

Rotor rpm power on min limit

A

487 rpm (102%N2)

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14
Q

Rotor RPM power off Max Limit

A

523 rpm (109%N2)

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15
Q

Engine torque max take off limit

A

87.2 psi (5min)

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16
Q

Engine torque max continuous limit

A
  1. 3 psi with TOT at or below 738 deg

74. 3 psi with TOT greater than 738 deg

17
Q

TOT transient limit during startup

A

During startup and shutdown: 810 deg and above for 10 sec or less with a momentary peak of 927 deg for not more than 1 sec

18
Q

TOT max takeoff limit

A

810 deg (5 min)

19
Q

Engine torque transient limits

A
  1. 3 psi to 93.0 psi for 15 seconds at 103%N2

93. 1 to 97.6 psi for 3 seconds at 103%N2

20
Q

Gas producer (N1) transient limit

A

106% for 15 seconds

21
Q

Gas producer (N1) max continuous limit

22
Q

Engine oil temperature flight operation limits

23
Q

Power turbine speed avoid range

A

71%~88% steady state operations prohibited (pause of one second)

24
Q

Engine oil pressure flight operation limits

A

50 to 130
50 psi below 79% N1
90 psi at 79% N1
115 psi with N1 at 94% and above

25
Generator limits
Max continuous 85 amps. 85 - 150 amps for 10 minutes. Above 150 amps 2 minutes prior to takeoff battery recharging cycle only
26
Starter limits
If light off is not attained | 1 min on, 1 min off, 1 min on, 23 minutes off
27
TOT transient limit in flight
810 deg to 843 degrees for 6 seconds
28
Max operating density altitude
16,000 ft
29
Fuel filter limitations
Fuel filter light illuminate in flight, no further flights until filter service
30
certification based on what systems installed and | operable
Engine Failure Warning System (Horn & Light) Low Rotor Warning System OAT Gauge Fuel Low Caution Light
31
Doors off approved configurations
All Doors off Both Rear Doors off, Both Forward Doors off Any one Door off All loose items & unoccupied seat cushions secured