FENIX B-58 > LIMITATIONS > Flashcards

LIMITATIONS Flashcards

(68 cards)

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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
INSTRUMENT PRESSURE Caution (Yellow Arc)
5.5 – 6.5 in Hg
26
INSTRUMENT PRESSURE Normal (Green Arc)
3.5 – 5.5 in Hg
27
Load Factors * Up * Down
* Up - 4.2g * Down - 2.0g
28
MANEUVER LIMITS This is a ____ category airplane. _____ maneuvers, including spins, are \_\_\_\_\_.
* Normal category airplane. * Acrobatic maneuvers * Spins * Prohibited
29
MANEUVERS Maximum slip duration:
30 seconds
30
MANIFOLD PRESSURE Maximum (Red Radial)
29.6 in Hg
31
MANIFOLD PRESSURE Operating Range (Green Arc)
15 - 29.5 in Hg
32
Maximum Cylinder Head Temperature
460°F
33
Maximum Oil Temperature
240°F
34
Minimum Take-off Oil Temperature
75°F
35
OIL PRESSURE Minimum (Red Radial) \_\_\_\_
30 psi
36
OIL PRESSURE Maximum (Red Radial)
100 psi
37
OIL PRESSURE Operating Range (Green Arc)
30 - 60 psi
38
OIL TEMPERATURE Caution (Yellow Radial) _____
75°F
39
OIL TEMPERATURE Maximum (Red Radial) ______
240°F
40
OIL TEMPERATURE Operating Range (Green Arc) _______
75°-240°F
41
PROPELLER DEICE AMMETER Normal Operating Range (Green Arc)
14 – 18 amps
42
Redline
223
43
STARTER LIMITATIONS - Do not operate starter continuously for more than ___ seconds. - Allow starter to ___ before ____ again.
30 seconds Allow starter to cool before cranking again.
44
TACHOMETER Maximum (Red Radial)
2700 rpm
45
TACHOMETER Operating Range (Green Arc)
2000 - 2700 rpm
46
Va Manauvering speed
156
47
Vfe - 10°
147 (Fenix 5 kts. below)
48
Vfe - 30°
122 (Fenix 5 kts. below)
49
Vle / LDG Gear Ext
* 152 Kts * FENIX - 147 (Fenix)
50
Vlo Operate
147 (Fenix 5 kts. below)
51
VMCA
81 / 73 - With VGs Installed - Red Line
52
Vne Never Exceed
223
53
Vno Max Structural Speed
195
54
VSSE Simulated Single Engine
86
55
Vx Best Angle of Climb
86
56
Vxse Best Angle of Climb S.E.
96
57
Vy Best Rate of Climb Blue Line
104
58
Vyse Best Rate of Climb S.E.
100
59
WEIGHTS 4200 lbs or less CG limits
74.0-86.0
60
WEIGHTS Baggage Weights Nose compartment
300lbs Max
61
WEIGHTS Baggage Weights Rear Baggage
120 lbs Max
62
WEIGHTS Baggage Weights Aft Cabin
400 lbs Max
63
WEIGHTS Max Landing
5400 lbs
64
WEIGHTS Max Ramp
5424
65
WEIGHTS Max TOW
5400
66
WEIGHTS Max Weight CG Limit
78.0-86.0. 79.(Datum line is 83.1 forward of front jack point)
67
White Arc
74-122
68
Yellow Arc
195-223

FENIX B-58 (6 decks)

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