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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
``` CYLINDER HEAD TEMPERATURE Operating Range (Green Arc) ```
Operating Range (Green Arc) 200°- 460°F
26
CYLINDER HEAD TEMPERATURE | Maximum (Red Radial)
Maximum (Red Radial) 460°F
27
INSTRUMENT PRESSURE
Caution (Yellow Arc) 2.5 – 3.5 in Hg
28
INSTRUMENT PRESSURE | Normal (Green Arc)
Normal (Green Arc) 3.5 – 5.5 in Hg
29
INSTRUMENT PRESSURE | Caution (Yellow Arc)
Caution (Yellow Arc) 5.5 – 6.5 in Hg
30
PROPELLER DEICE AMMETER | Normal Operating Range (Green Arc)
Normal Operating Range (Green Arc) 14 – 18 amps
31
WEIGHTS | Max Ramp
Max Ramp - 5424
32
WEIGHTS | Max TOW
Max TOW - 5400
33
WEIGHTS | Max Landing
Max Landing - 5400
34
WEIGHTS | Max Weight CG Limit
Max Weight CG Limit - 78.0-86.0. | Datum line is 83.1 forward of front jack point
35
WEIGHTS | 4200 lbs or less CG limits
4200 lbs or less CG limits - 74.0-86.0
36
WEIGHTS Baggage Weights Nose compartment
Baggage Weights | Nose compartment - 300lbs Max
37
WEIGHTS Baggage Weights Aft Cabin
Baggage Weights | Aft Cabin - 400 lbs Max
38
WEIGHTS Baggage Weights Rear Baggage
Baggage Weights | Rear Baggage - 120 lbs Max
39
FUEL QUANTITY | Yellow Arc
Yellow Arc E – 1/8 Full
40
MANEUVER LIMITS | This is a ____ category airplane. _____ maneuvers, including spins, are _____.
This is a normal category airplane. Acrobatic maneuvers, including spins, are prohibited.
41
FLIGHT LOAD FACTORS (5400 POUNDS) Positive maneuvering load factors: Flaps up
Positive maneuvering load factors: | Flaps up 4.2 g
42
FLIGHT LOAD FACTORS (5400 POUNDS) Positive maneuvering load factors: Flaps Down
Positive maneuvering load factors: | Flaps Down 2.0 g
43
ICE PROTECTION Ice protection equipment installed on this aircraft ____ been demonstrated to meet requirements for flight into known icing conditions.
ICE PROTECTION Ice protection equipment installed on this aircraft has not been demonstrated to meet requirements for flight into known icing conditions.
44
FUEL | Do not take off if Fuel Quantity Gauges indicate in ____ or with less than __ gallons in each wing fuel system
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
FUEL | The fuel cross-feed system is to be used during _____ conditions in level flight only.
FUEL | The fuel cross-feed system is to be used during emergency conditions in level flight only.
46
MANEUVERS | Maximum slip duration:
Maximum slip duration: 30 seconds
47
EMERGENCY PROC ENGINE FAILURE DURING TAKE-OFF If insufficient runway remains for stopping:
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
48
EMERGENCY PROCEDURES ENGINE FAILURE AFTER LIFT-OFF AND IN FLIGHT After positive control of the airplane is established: EMERGENCY PROCEDURES
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: 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 7. Electrical Load - MONITOR (Maximum load of 1.0 on remaining engine)
49
EMERGENCY PROCEDURES ENGINE FIRE ON THE GROUND
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
EMERGENCY PROCEDURES ENGINE FIRE IN FLIGHT
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
Vne Never Exceed
223
52
Vno Max Structural Speed
195
53
Va Manauvering speed
156
54
Vfe - 10°
147 (Fenix 5 kts. below)
55
Vfe - 30°
115 (Fenix 5 kts. below)
56
Vle / Ldg Gear Ext
147 (Fenix 5 kts. below)
57
Vlo Operate
147 (Fenix 5 kts. below)
58
VMCA
81 / 73 - With VGs Installed - Red Line
59
VSSE Simulated Single Engine
86
60
Vy Best Rate of Climb Blue Line
104
61
Vx Best Angle of Climb
96
62
Vyse Best Rate of Climb S.E.
100
63
Vxse Best Angle of Climb S.E.
86
64
Emerg Descent
152
65
Redline
223
66
White Arc
74-122
67
Green Arc
84-195
68
Yellow Arc
195-223

FENIX B-58 (6 decks)

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