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FENIX B-58 > LIMITATIONS COPY > Flashcards

LIMITATIONS COPY Flashcards

1
Q

Load Factors
Up
Down

A

Up - 4.2g

Down - 2.0g

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2
Q

FUEL FLOW

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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3
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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4
Q

FUEL

Total Capacity

A

Total Capacity 200 Gallons

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5
Q

Maximum Cylinder Head Temperature

A

Maximum Cylinder Head Temperature 460°F

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6
Q

Maximum Oil Temperature

A

Maximum Oil Temperature 240°F

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7
Q

Minimum Take-off Oil Temperature

A

Minimum Take-off Oil Temperature 75°F

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8
Q

ENGINE LIMITATIONS

Minimum Oil Pressure (Idle)

A

Minimum Oil Pressure (Idle) 30 psi

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9
Q

ENGINE LIMITATIONS

Maximum Oil Pressure

A

Maximum Oil Pressure 100 psi

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10
Q

FUEL LIMITATIONS

Total Usable

A

Total Usable 194 Gallons

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11
Q

STARTER LIMITATIONS

  • Do not operate starter continuously for more than ___ seconds.
  • Allow starter to ___ before ____ again.
A
  • Do not operate starter continuously for more than 30 seconds.
  • Allow starter to cool before cranking again.
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12
Q

OIL TEMPERATURE

Caution (Yellow Radial) ___

A

Caution (Yellow Radial) 75°F

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13
Q 
OIL TEMPERATURE
Operating Range (Green Arc)	\_\_\_\_
A

Operating Range (Green Arc) 75°-240°F

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14
Q

OIL TEMPERATURE

Maximum (Red Radial) ___

A

Maximum (Red Radial) 240°F

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15
Q

OIL PRESSURE

Minimum (Red Radial) ____

A

Minimum (Red Radial) 30 psi

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16
Q 
OIL PRESSURE
Operating Range (Green Arc)
A

Operating Range (Green Arc) 30 - 60 psi

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17
Q

OIL PRESSURE

Maximum (Red Radial)

A

Maximum (Red Radial) 100 psi

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18
Q

FUEL FLOW AND PRESSURE

Minimum (Red Radial)

A

Minimum (Red Radial) 1.5 psi

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19
Q 
FUEL FLOW AND PRESSURE
Cruise Power (Green Arc)
A

Cruise Power (Green Arc) 9.7 gph – 17.0 gph

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20
Q

FUEL FLOW AND PRESSURE

Take-off & Climb Power (Wide Green Arc)

A

Take-off & Climb Power (Wide Green Arc) 17.8 gph - 24.3 gph

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21
Q 
MANIFOLD PRESSURE
Operating Range (Green Arc)
A

Operating Range (Green Arc) 15 - 29.5 in Hg

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22
Q

MANIFOLD PRESSURE

Maximum (Red Radial)

A

Maximum (Red Radial) 29.6 in Hg

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23
Q 
TACHOMETER
Operating Range (Green Arc)
A

Operating Range (Green Arc) 2000 - 2700 rpm

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24
Q

TACHOMETER

Maximum (Red Radial)

A

Maximum (Red Radial) 2700 rpm

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25
Q 
CYLINDER HEAD TEMPERATURE
Operating Range (Green Arc)
A

Operating Range (Green Arc) 200°- 460°F

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26
Q

CYLINDER HEAD TEMPERATURE

Maximum (Red Radial)

A

Maximum (Red Radial) 460°F

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27
Q

INSTRUMENT PRESSURE

A

Caution (Yellow Arc) 2.5 – 3.5 in Hg

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28
Q

INSTRUMENT PRESSURE

Normal (Green Arc)

A

Normal (Green Arc) 3.5 – 5.5 in Hg

29
Q

INSTRUMENT PRESSURE

Caution (Yellow Arc)

A

Caution (Yellow Arc) 5.5 – 6.5 in Hg

30
Q

PROPELLER DEICE AMMETER

Normal Operating Range (Green Arc)

A

Normal Operating Range (Green Arc) 14 – 18 amps

31
Q

WEIGHTS

Max Ramp

A

Max Ramp - 5424

32
Q

WEIGHTS

Max TOW

A

Max TOW - 5400

33
Q

WEIGHTS

Max Landing

A

Max Landing - 5400

34
Q

WEIGHTS

Max Weight CG Limit

A

Max Weight CG Limit - 78.0-86.0.

Datum line is 83.1 forward of front jack point

35
Q

WEIGHTS

4200 lbs or less CG limits

A

4200 lbs or less CG limits - 74.0-86.0

36
Q

WEIGHTS
Baggage Weights
Nose compartment

A

Baggage Weights

Nose compartment - 300lbs Max

37
Q

WEIGHTS
Baggage Weights
Aft Cabin

A

Baggage Weights

Aft Cabin - 400 lbs Max

38
Q

WEIGHTS
Baggage Weights
Rear Baggage

A

Baggage Weights

Rear Baggage - 120 lbs Max

39
Q

FUEL QUANTITY

Yellow Arc

A

Yellow Arc E – 1/8 Full

40
Q

MANEUVER LIMITS

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

A

This is a normal category airplane. Acrobatic maneuvers, including spins, are prohibited.

41
Q

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

A

Positive maneuvering load factors:

Flaps up 4.2 g

42
Q

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

A

Positive maneuvering load factors:

Flaps Down 2.0 g

43
Q

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

A

ICE PROTECTION
Ice protection equipment installed on this aircraft has not been demonstrated to meet requirements for flight into known icing conditions.

44
Q

FUEL

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

A

FUEL

Do not take off if Fuel Quantity Gauges indicate in Yellow Arc or with less than 13 gallons in each wing fuel system

45
Q

FUEL

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

A

FUEL

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

46
Q

MANEUVERS

Maximum slip duration:

A

Maximum slip duration: 30 seconds

47
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:

  1. Fuel Selector Valves – OFF
  2. Battery, Alternator, and Magneto / Start Switches – OFF
48
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:

  1. Secure inoperative engine:
    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
  2. Electrical Load - MONITOR (Maximum load of 1.0 on remaining engine)
49
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
50
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
51
Q

Vne Never Exceed

A

223

52
Q

Vno Max Structural Speed

A

195

53
Q

Va Manauvering speed

A

156

54
Q

Vfe - 10°

A

147 (Fenix 5 kts. below)

55
Q

Vfe - 30°

A

115 (Fenix 5 kts. below)

56
Q

Vle / Ldg Gear Ext

A

147 (Fenix 5 kts. below)

57
Q

Vlo Operate

A

147 (Fenix 5 kts. below)

58
Q

VMCA

A

81 / 73 - With VGs Installed - Red Line

59
Q

VSSE Simulated Single Engine

A

86

60
Q

Vy Best Rate of Climb Blue Line

A

104

61
Q

Vx Best Angle of Climb

A

96

62
Q

Vyse Best Rate of Climb S.E.

A

100

63
Q

Vxse Best Angle of Climb S.E.

A

86

64
Q

Emerg Descent

A

152

65
Q

Redline

A

223

66
Q

White Arc

A

74-122

67
Q

Green Arc

A

84-195

68
Q

Yellow Arc

A

195-223

FENIX B-58 (6 decks)

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