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FENIX B-58 > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

1
Q

CYLINDER HEAD TEMPERATURE

Maximum (Red Radial)

A

460°F

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2
Q

CYLINDER HEAD TEMPERATURE

Operating Range (Green Arc)

A

200°- 460°F

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3
Q

EMERGENCY DESCENT SPEED

A

152

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4
Q

EMERGENCY PROCEDURES ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT After positive control of the airplane is established: EMERGENCY PROCEDURES

A

ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT
1. Gear and Flaps· UP
2. Throttle (inoperative engine} - CLOSED
3. Propeller (inoperative engine) - FEATHER
4. Power (operative engine) - AS REQUIRED
5. Airspeed - MAINTAIN SPEED (100 kts. MAX) UNTIL OBSTACLES ARE CLEARED After positive control of the airplane is established:
6. Secure inoperative engine:
7. a) Mixture Control - IDLE CUT-OFF b) Fuel Selector – OFF c) Auxiliary Fuel Pump – OFF d) Magneto - Start Switch – OFF e) Alternator Switch – OFF f) Cowl Flap – CLOSED
8. Electrical Load - MONITOR (Maximum load of 1.0 on remaining engine)

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5
Q

EMERGENCY PROCEDURES ENGINE FIRE IN FLIGHT

A

Shut down the affected engine according to the following procedure and land immediately. Follow the applicable single-engine procedures in this section.
1. Fuel Selector Valve - OFF
2. Mixture Control - IDLE CUT-OFF
3. Propeller - FEATHERED
4. Aux Fuel Pump - OFF
5. Maqneto / Start Switch - OFF
6. Alternator Switch - OFF

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6
Q

EMERGENCY PROCEDURES ENGINE FIRE ON THE GROUND

A

ON THE GROUND
1. Mixture Controls - IDLE CUT-OFF
2. Continue to crank affected engine
3. Fuel Selector Valves - OFF
4. Battery and Alternator Switches - OFF
5. Extinguish with Fire Extinguisher

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7
Q

EMERGENCY PROC ENGINE FAILURE DURING TAKE-OFF
If insufficient runway remains for stopping:

A

ENGINE FAILURE DURING TAKE-OFF
1. Throttles - CLOSED
2. Braking - MAXIMUM If insufficient runway remains for stopping:
3. Fuel Selector Valves – OFF
4. Battery, Alternator, and Magneto / Start Switches – OFF

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8
Q

Engine Limitations

  • Max Cyl Head Temp
  • Max Oil Temp
  • Min Oil Temp
  • Takeoff Oil Pressure
  • Max Oil Pressure
  • Instrument Pressure
A
  • Max Cyl Head Temp - 460°
  • Max Oil Temp - 240°
  • Min Oil Temp Takeoff - 75°
  • Min Oil Pressure - 30 psi
  • Max Oil Pressure - 100 psi
  • Instrument Pressure - 2.5-6.5”
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9
Q

ENGINE LIMITATIONS
Maximum Oil Pressure

A

100 psi

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10
Q

ENGINE LIMITATIONS

Minimum Oil Pressure (Idle)

A

30 psi

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11
Q

FLIGHT LOAD FACTORS (5400 POUNDS)
Positive maneuvering load factors: Flaps Down

A

Flaps Down 2.0 g

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12
Q

FLIGHT LOAD FACTORS (5400 POUNDS)
Positive maneuvering load factors: Flaps up

A

Flaps up 4.2 g

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13
Q

FUEL
Do not take off if Fuel Quantity Gauges indicate in ____ or with less than __ gallons in each wing fuel system

A

Yellow Arc
13 gallons

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14
Q

FUEL FLOW

  • RED (Min)
  • GREEN (Cruise)
  • GREEN Wide (T.O. / Climb)
  • RED (Max)
A
  • Red ……………………………………. 1.5 psi
  • Green (Cruise) ………………….. 9.7 - 17.0 gph
  • Green Wide (T.O. / Clmb) … 17.8 - 24.3 gph
  • Red (Max) …………………………. 17.5 psi
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15
Q

FUEL FLOW AND PRESSURE
Cruise Power (Green Arc)

A

9.7 – 17.0 gph

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16
Q

FUEL FLOW AND PRESSURE
Minimum (Red Radial)

A

1.5 psi

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17
Q

FUEL FLOW AND PRESSURE

Take-off and Climb Power (Wide Green Arc)

A

17.8 gph - 24.3 gph

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18
Q

FUEL LIMITATIONS
Total Usable

A

194 Gallons

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19
Q

FUEL QUANTITY
Yellow Arc

A

1/8 Full

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20
Q

FUEL
The fuel cross-feed system is to be used during _____ conditions in level flight only.

A

emergency

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21
Q

FUEL
Total Capacity

A

200 Gallons

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22
Q

GREEN ARC

A

84-195

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23
Q

ICE PROTECTION Ice protection equipment installed on this aircraft ____ been demonstrated to meet requirements for flight into known icing conditions.

A

has not

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24
Q

INSTRUMENT PRESSURE
Caution (Yellow Arc)

A

2.5 – 3.5 in Hg

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25
Q

INSTRUMENT PRESSURE

Caution (Yellow Arc)

A

5.5 – 6.5 in Hg

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26
Q

INSTRUMENT PRESSURE

Normal (Green Arc)

A

3.5 – 5.5 in Hg

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27
Q

Load Factors

  • Up
  • Down
A
  • Up - 4.2g
  • Down - 2.0g
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28
Q

MANEUVER LIMITS

This is a ____ category airplane. _____ maneuvers, including spins, are _____.

A
  • Normal category airplane.
  • Acrobatic maneuvers
  • Spins
  • Prohibited
29
Q

MANEUVERS
Maximum slip duration:

A

30 seconds

30
Q

MANIFOLD PRESSURE
Maximum (Red Radial)

A

29.6 in Hg

31
Q

MANIFOLD PRESSURE
Operating Range (Green Arc)

A

15 - 29.5 in Hg

32
Q

Maximum Cylinder Head Temperature

A

460°F

33
Q

Maximum Oil Temperature

A

240°F

34
Q

Minimum Take-off Oil Temperature

A

75°F

35
Q

OIL PRESSURE

Minimum (Red Radial) ____

A

30 psi

36
Q

OIL PRESSURE
Maximum (Red Radial)

A

100 psi

37
Q

OIL PRESSURE
Operating Range (Green Arc)

A

30 - 60 psi

38
Q

OIL TEMPERATURE
Caution (Yellow Radial) _____

A

75°F

39
Q

OIL TEMPERATURE
Maximum (Red Radial) ______

A

240°F

40
Q

OIL TEMPERATURE
Operating Range (Green Arc) _______

A

75°-240°F

41
Q

PROPELLER DEICE AMMETER
Normal Operating Range (Green Arc)

A

14 – 18 amps

42
Q

Redline

A

223

43
Q

STARTER LIMITATIONS - Do not operate starter continuously for more than ___ seconds. - Allow starter to ___ before ____ again.

A

30 seconds
Allow starter to cool before cranking again.

44
Q

TACHOMETER
Maximum (Red Radial)

A

2700 rpm

45
Q

TACHOMETER
Operating Range (Green Arc)

A

2000 - 2700 rpm

46
Q

Va Manauvering speed

A

156

47
Q

Vfe - 10°

A

147
(Fenix 5 kts. below)

48
Q

Vfe - 30°

A

122
(Fenix 5 kts. below)

49
Q

Vle / LDG Gear Ext

A
  • 152 Kts
  • FENIX - 147 (Fenix)
50
Q

Vlo Operate

A

147
(Fenix 5 kts. below)

51
Q

VMCA

A

81 / 73 - With VGs Installed - Red Line

52
Q

Vne Never Exceed

A

223

53
Q

Vno Max Structural Speed

A

195

54
Q

VSSE Simulated Single Engine

A

86

55
Q

Vx Best Angle of Climb

A

86

56
Q

Vxse Best Angle of Climb S.E.

A

96

57
Q

Vy Best Rate of Climb Blue Line

A

104

58
Q

Vyse Best Rate of Climb S.E.

A

100

59
Q

WEIGHTS
4200 lbs or less CG limits

A

74.0-86.0

60
Q

WEIGHTS
Baggage Weights Nose compartment

A

300lbs Max

61
Q

WEIGHTS
Baggage Weights Rear Baggage

A

120 lbs Max

62
Q

WEIGHTS
Baggage Weights Aft Cabin

A

400 lbs Max

63
Q

WEIGHTS
Max Landing

A

5400 lbs

64
Q

WEIGHTS
Max Ramp

A

5424

65
Q

WEIGHTS
Max TOW

A

5400

66
Q

WEIGHTS
Max Weight CG Limit

A

78.0-86.0.
79.(Datum line is 83.1 forward of front jack point)

67
Q

White Arc

A

74-122

68
Q

Yellow Arc

A

195-223

FENIX B-58 (6 decks)

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