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Guardian C90B > Limitations > Flashcards

Limitations Flashcards

1
Q

Max operating speed Vmo

A

226 kts

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2
Q

Max demonstrated cross wind

A

25 kts

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3
Q

Takeoff speeds (flaps up)

A

Vr 97 kts
V2 104 kts

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4
Q

Best angle of climb Vx

A

101 kts

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5
Q

Best rate of climb Vy

A

112 kts

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6
Q

Single engine best angle of climb Vxse

A

100 kts

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7
Q

Cruise climb speeds

A

0 to 10,000 150 kts
10,000 to 20,000 130 kts
20,000 to 25,000 120 kts

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8
Q

Maneuvering speed

A

163 kts

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9
Q

Turbulent air penetration speed

A

161 kts

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10
Q

Max airspeed for effective windshield anti-ice

A

226 kts

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11
Q

Minimum ice penetration speed

A

140 kts

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12
Q

Final landing approach speed (flaps down) at 9600

A

101 kts

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13
Q

Minimum intentional engine shutdown speed (Vsse)

A

97 kts

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14
Q

Single engine best rate of climb Vyse

A

108 kts

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15
Q

Minimum control speed Vmca

A

80 kts

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16
Q

Single engine enroute climb

A

108 kts

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17
Q

Emergency descent

A

182 kts

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18
Q

Max range glide speed

A

125 kts

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19
Q

What bank angle with single engine gives the best performance

A

3 to 5 degrees into good engine

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20
Q

Max ramp weight

A

10,545

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21
Q

Max takeoff weight

A

10485

22
Q

Max landing weight

A

9832

23
Q

Max zero fuel weight

A

9378

24
Q

Load factor limits

A

Flaps up. +3.28/-1.31
Flaps down. + 2.0/0.00

25
Q

Max flap extension speeds Vfe

A

Vfe
Appr 184
Down 148

26
Q

Max landing gear operating speeds Vlo
-extension
-retraction

A

Vlo
Extension 182
Retraction 163

27
Q

Max landing gear extended Vle

A

Vle
182

28
Q

Max ITT for start

A

1090 c

29
Q

Min oil temp for starting

A

-40 c

30
Q

Starter limits

A

40 seconds on, 60 seconds off
40 seconds on, 60 seconds off
40 seconds on, 30 mins off

31
Q

Total usable fuel

A

384 gal, 2573 lbs
Per side 192 gal, 1286
Each wing tank 131 gal, 877 lbs
Each nacelle tank 61 gal, 409 lbs

32
Q

Fuel imbalance

A

200 lbs

33
Q

Fuel Cross feed only permitted when:

A

Electric boost pump failure
Engine failure

34
Q

Operating with low fuel pressure

A

Low fuel pressure is limited to 10 hours before overhaul or replacement of the engine driven fuel pump

35
Q

Boost pumps

A

Both must be operating for takeoff

36
Q

Propeller speed limits

A

Transient. 2420 rpm
Reverse. 2100 rpm
All other conditions 2200 rpm

37
Q

Max operating pressure alt

A

30,000’

38
Q

Max outside air temp limit

A

ISA + 37 c

39
Q

Cabin pressurization limit

A

5.1 psi or delta P

40
Q

Landing gear cycle limits (1 up and 1 down)

A

One every three minutes for a total of ten cycles followed by a 15 min cool down

41
Q

Engine anti ice temp

A

+5 c and lower

42
Q

Min airspeed for flying in ice

A

140 kts

43
Q

Min temp for operating de-ice boots

A

-40 c

44
Q

Minimum fuel for takeoff

A

265 or yellow arc

45
Q

Use of aviation gas is limited to:

A

150 hours per engine
Flights limited to 8000’ with boost pump inop
Cross feed must be operational

46
Q

Max torque

A

Dash 21 1315

Dash 135 1520

47
Q

Max continuous ITT

A

Dash 21 695

Dash 135 805

48
Q

Max transit ITT

A

Dash 21 825

Dash 135 880

49
Q

Max reverse prop rpm

A

Dash 21 2100

Dash 135 1815

50
Q

Max transit prop rpm

A

Dash 21 2420

Dash 135 2090

51
Q

Stall speeds

A

Vso. 78
Vs. 88

52
Q

Flaps up landing speed

A

115

Guardian C90B (11 decks)

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