Limitations Flashcards

1
Q

Vmc (Mininmum control speed)

A

Flaps 10*- 64 ias

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2
Q

Vx (best angle)

A

Flaps 0*- 87 ias

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3
Q

Vy (best rate)

A

Flaps 0*- 100 ias

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4
Q

Vyse (Best rate single engine)

A

Flaps 10*- 80 ias

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5
Q

Vmc Autofeather U/S (minimu control speed)

A

Flaps 10*- 68 ias

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6
Q

Vfe (flaps extended speed)

A

Flaps 10- 103 ias /Flaps 10-35- 93 ias

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7
Q

V1 RGR Flaps 20*

A

74 ias

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8
Q

Vmo (Maximum Operating Speed) mod 6/1291

A
Sea level  166 ias
6700ft   166 ias
10000ft 156 ias
15000ft 141 ias
20000ft  126 ias
25000ft  112 ias
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9
Q

Vp (Manuvering Speed)

A

132 ias

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10
Q

Vb (gust penetration speed)

A

132 ias

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11
Q

Max SHP

A

Flat rated 620 (680)

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12
Q

Max Take-off and Max continuous TORQUE

A

50 PSI

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13
Q

Max Take-off and Max continuous T5

A

725

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14
Q

Max Take-off and Max continuous NG% (2)

A

101.6 (2)-For every 10 *C below -30 *C Ambient temp reduce NG by 2.2%

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15
Q

Max Take-off and Max continuous Np% (9)

A

96 (9)- In the event of primary prop gov fail to gov at 96% it is acceptable to use engine as long as prop overspeed gove maintains speed at 101.5% or less. Lans as soon as practical

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16
Q

Max Take-off and Max continuous Oil Press PSI

A

80 to 100 PSI

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17
Q

Max Take-off and Max continuous Oil Temp *C (4)

A

10 to 99 *C (4)-Durin cold wx opps 55 *C is recomended for fuel leaving oil-to-fuel heat exchanger fuel above freezing temp

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18
Q

Max Climb/ Max Cruise SHP

A

620 SHP (680)

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19
Q

Max Climb/ Max Cruise TORQUE

A

50 PSI

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20
Q

Max Climb/ Max Cruise T5 *C

A

695 *C

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21
Q

Max Climb/ Max Cruise Np% (9)

A

96 (9)- In the event of primary prop gov fail to gov at 96% it is acceptable to use engine as long as prop overspeed gove maintains speed at 101.5% or less. Lans as soon as practical

22
Q

Max Climb/ Max Cruise Oil Press PSI

A

80 to 100 PSI

23
Q

Max Climb/ Max Cruise Oil Temp *C (4)

A

0 to 99 C* (4)-Durin cold wx opps 55 *C is recomended for fuel leaving oil-to-fuel heat exchanger fuel above freezing temp

24
Q

Max Idle T5 *C (5)

A

660 C (5)-At Idle the T5 temp approaches 660C, either increase NG or reduce engine loads (for exemple, turn off generator) to stay below 660*c idle limt

25
Q

Max Idle Oil press PSI (3)

A

40 Minimum (3)-Normal oil press in flight is 80 to 100 with Ng above 72% and oil temp above 60*C. Oil press below 80 PSI in flight is undesireble(use reduce power and report to maintenave). OIl PSI under 40 is unsafe land asap or shut down engine. Ground opps 40 to 80 PSi is acceptable

26
Q

Max Idle Oil Temp*C

A

-40 to 99*C

27
Q

Max Starting T5 (8)

A

925 to 980-10 second, 980 to 1090-2 second, starts above 850 should be reported

28
Q

Max Starting Oil Temp*C

A

-40 Minimum

29
Q

Max Acceleration (transient) TORQUE

A

68.7 PSI (6) 2 second Max

30
Q

Max Acceleration (transient) T5*C

A

825*C (6) 2 second Max

31
Q

Max Acceleration (transient) NG%

A

102.6

32
Q

Max Acceleration (transient) Np%

A

110

33
Q

Max Acceleration (transient) Oil Temp*C (4)

A

0 to 99*c (4)-Durin cold wx opps 55 *C is recomended for fuel leaving oil-to-fuel heat exchanger fuel above freezing temp

34
Q

Max Reverse (7,11) SHP

A

620 SHP (7)-Reverse power is limited to 1 minute (11)-In flight opp of the pwer lever aft of IDLE is prohibited

35
Q

Max Reverse (7,11) TORQUE

A

50 PSI (7)-Reverse power is limited to 1 minute (11)-In flight opp of the pwer lever aft of IDLE is prohibited

36
Q

Max Reverse (7,11) T5*C

A

725*C (7)-Reverse power is limited to 1 minute (11)-In flight opp of the pwer lever aft of IDLE is prohibited

37
Q

Max Reverse (7,11) NG%

A

101.5 (7)-Reverse power is limited to 1 minute (11)-In flight opp of the pwer lever aft of IDLE is prohibited

38
Q

Max Reverse (7,11) Np%

A

91% +/- 1 (7)-Reverse power is limited to 1 minute (11)-In flight opp of the pwer lever aft of IDLE is prohibited

39
Q

Max Reverse (7,11) Oil Press PSI

A

80 to 100 PSI (7)-Reverse power is limited to 1 minute (11)-In flight opp of the pwer lever aft of IDLE is prohibited

40
Q

Max Reverse (7,11) Oil Temp*C

A

0 to 99*C (7)-Reverse power is limited to 1 minute (11)-In flight opp of the pwer lever aft of IDLE is prohibited

41
Q

Generator and loadmeter

A

Greater than 0.5/ on ground/ idle NG+15%/ Any temp/ to keep T5 below 660*C

  1. 8 Max/ on ground/ Greater than 7*C/ Gen cooling
  2. 0 Max/ on ground/ 7*C or less/ Gen capacity
  3. 0 max/ in flight/ Any temp/ Gen capacity
42
Q

Starter limitation

A

25 seconds ON, 1 minute OFF, Then

25 seconds ON, 1 minute OFF, Then

25 seconds ON, followed by 30 minute cooling preiod

43
Q

Max take-off weight

A

12,500 lbs

44
Q

Max landing weight

A

12,300 lbs

45
Q

Max ramp weight

A

12,600 lbs

46
Q

Compartment C1-C11 max load limit

A

1,333 lbs each

47
Q

Foward Baggage compartment load limit

A

300 lbs

48
Q

Aft baggage compartment load limt

A

500 lbs including 150 lbs shelf limit

49
Q

Max floor loading

A

Cabin - 200 lbs per square foot

Forward and aft baggage compartment - 100 lbs per square foot

50
Q

Max XWIND

A

27