Limits Flashcards

(76 cards)

1
Q

[Torque] Operating Range (1000 - 1700 RPM)

A

0-100%

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2
Q

[Torque] Max TQ (Props below 1000 RPM)

A

62%

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3
Q

[Torque] Max TQ (Props above 1700 RPM)

A

96%

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4
Q

[Torque] Inadvertent Excursions

A

102% (7 minutes)

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5
Q

[Torque] Transient

A

156% (20 seconds)

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6
Q

[N1] Minimum Low Idle

A

62%

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7
Q

[N1] Normal Operating Range

A

62 - 104%

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8
Q

[N1] Max

A

104%

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9
Q

[ITT] Max Low Idle

A

750 C

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10
Q

[ITT] Max Reverse

A

760 C

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11
Q

[ITT] Recommended Cruise Climb

A

785 C

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12
Q

[ITT] Max Cruise

A

820 C

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13
Q

[ITT] Takeoff / Max Continuous

A

820 C

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14
Q

[ITT] Transient

A

850 C (20 seconds)

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15
Q

[ITT] Max Starting

A

1000 (5 seconds) C

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16
Q

[Oil Temp] Minimum Starting

A

-40 C

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17
Q

[Oil Temp] Normal Operating Range / Max Reverse

A

0 - 99 C

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18
Q

[Oil Temp] Max Low Idle

A

-40 - 110 C

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19
Q

[Oil Temp] Takeoff

A

0 - 110 C

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20
Q

[Oil Temp] Max Continuous / Cruise Climb

A

0 - 110 C

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21
Q

[Oil Temp] Max Transient

A

99 - 110 (10 minutes) C

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22
Q

[Oil Temp] Recommended for Fuel Heater Ops at T/O

A

55 C

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23
Q

[Oil Pressure] Minimum Low Idle

A

60 PSI

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24
Q

[Oil Pressure] Caution Range (TQ limited to 62%)

A

60 - 90 PSI

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25
[Oil Pressure] Normal Operating Range
90 - 135 PSI
26
[Oil Pressure] Max Starting
200 PSI
27
[N2] Minimum Idle Speed
1050 RPM
28
[N2] Normal Operating Range
1450 - 1700 RPM
29
[N2] Max Reverse
1650 RPM
30
[N2] Max
1700 RPM
31
[N2] Inadvertent Excursions
1735 (7 minutes)
32
[N2] Transient
1870 (20 Seconds) RPM
33
Autofeather Requirements
Must be OPERABLE for all flights and must be ARMED for takeoff, climb, approach and landing.
34
External Power Limits
28.0 - 28.4 volts 1000 AMPS Minimum Momentary 300 AMPS Continuous
35
[Generator Load, Ground] Max (62% - 70% N1)
75%
36
[Generator Load, Ground] Max (70% - 100% N1)
100%
37
[Generator Load, Flight] Max (SL - FL210)
100%
38
[Generator Load, Flight] Max (FL 210 - 260)
90%
39
[Generator Load, Flight] Max (FL 260 - 300)
80%
40
[Generator Load, Flight] Max (FL 300 - 320)
75%
41
[Generator Load, Flight] Max (FL 320 - 350)
70%
42
[Generator Load] Max Single Engine Operations
90%
43
[Generator Load] Normal
27.5 - 29 VDC
44
Starter Limitation
30 seconds ON 5 minutes OFF 30 seconds ON 5 minutes OFF 30 seconds ON 30 minutes OFF
45
Max Ramp Weight
16,600 lbs
46
Max Takeoff Weight
16,500 lbs
47
Max Landing Weight
15,675 lbs
48
Max Zero Fuel Weight
13,000 lbs
49
Max Baggage Compartment Weight
550 lbs
50
Max on Air Stair Door
One Person
51
[Fuel] Max Imbalance
300 lbs
52
[Fuel] Min for Takeoff
265 lbs (in each)
53
[Fuel] Max Useable Quantity
5192 lbs, 775 gallons
54
Fuel Crossfeed permitted only when:
one engine is inoperative
55
Gear Cycle Limit
6 cycles (1 up - 1 down) at one every 5 minutes followed by a 15 minute cool down.
56
G-Load Flaps UP
-1.21 to 3.0
57
G-Load Flaps DOWN
0 to 2.0
58
[Vacuum Gauge] Normal from SL to 15,000 feet
4.3 to 5.9 in. Hg
59
[Vacuum Gauge] Normal from 15,000 to 35,000 feet
2.8 to 4.3 in. Hg
60
[Propeller De-Ice] Normal Operating Range
26-32 AMPS
61
When must rudder boost be operational?
For all flights
62
Max Altitude Yaw Dam INOP
19,000 (with dual aft strakes)
63
[Temperature Limits] Max from SL to 25,000 feet
ISA + 37
64
[Temperature Limits] Max above 25,000 feet
ISA + 31
65
Minimum Surface De-Ice Temp
-40
66
Ice Vane Use
ON When ambient temperatures are +5 C and below in visible moisture OFF for takeoff in ambient temperatures above +10 C
67
[Pneumatic Pressure] Normal Operating Range
12-20 PSI
68
[Pneumatic Pressure] Max
20
69
Cabin Differential Limit
6.6 PSID
70
Max Operating Altitude
35,000 feet
71
Brake De-Ice Limit
Don't use above 15 C or more than 10 minutes with wheels retracted
72
Minimum Autopilot height after Takeoff
400 ft AGL
73
Minimum Autopilot height during Cruise
1000 AGL
74
Minimum Autopilot height during Approach
79 feet AGL
75
Minimum Autopilot height during Steep Approach
160 feet AGL
76
Throttle Push
ITT 870 for 5 minutes with a torque limit of 100%