Limitaciones PA-28 Flashcards

1
Q

Va

A

129

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2
Q

Vne

A

171

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3
Q

Vno

A

140

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4
Q

Vfe

A

115

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5
Q

Vs

A

64

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6
Q

Vso

A

55

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7
Q

Vx

A

74

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8
Q

Vy

A

85

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9
Q

Vr

A

60

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10
Q

Vapp (Flap Dn)

A

76

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11
Q

Vglide (Recommended)

A

80

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12
Q

Max Cross Wind - KTS

A

15

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13
Q
A
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14
Q

Fuel grade

A

100 LL

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15
Q

Total capacity

A

50 GAL

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16
Q

Maximum Weight

A

1950 lbs

17
Q

Maximum Baggage

A

100

18
Q

Maximum Horsepower

A

150 HP

19
Q

Maximum continuous RPM

A

2700

20
Q

Static RPM - Maximum

A

2425

21
Q

Static RPM - Minimum

A

2150

22
Q

Oil Pressure (PSI) Max.

A

85 PSI

23
Q

Oil Pressure (PSI) Min.

A

60 PSI

24
Q

Oil Temperature (F°) Max.

A

245

25
Q

Oil Temperature (F°) Min

A

75

26
Q

Fuel Pressure - Maximum

A

8

27
Q

Fuel Pressure - Min.

A

0.5

28
Q

Maneuver (MPH) (Utility Category): Chandelles, Lazy eights y Steep Turns

A

129

29
Q

Maneuver (MPH) (Utility Category): Spin

A

Stall

30
Q

Maneuver (MPH) (Normal Category): Chandelles, Lazy eights, Steep Turns and Spin

A

PROHIBITED

31
Q

1.- ENGINE FAILURE BEFORE ROTATE

Throttle
Brakes APPLY
Aircraft control

A

IDLE
APPLY
MAINTAIN DIRECTIONAL CONTROL

32
Q

ENGINE FAILURE DURING TAKEOFF
Sufficient runway
Insufficient runway remains
Airspeed
If exist obstructions
Flaps

A

LAND STRAIGHT AHEAD
SAFE AIRSPEED
MAKE SHALLOW TURN
AS REQUIRED Normally, flaps should be fully
extended for touchdown.

33
Q

ENGINE FAILURE INMMEDIATELY AFTER TAKEOFF
POWER OFF LANDING
Airspeed
Ignition OFF
Master Switch
Fuel Selector
Mixture
Seat belt and harness

If sufficient altitude has been gained to attempt a restart:
Airspeed
Fuel Selector
Electric fuel pump
Mixture
Carburetor heat
If power is not regained. proceed with power off landing.

A

MAINTAIN SAFE AIRSPEED
OFF
OFF
OFF
CUT-OFF
TIGHT

MAINTAIN SAFE AIRSPEED
SWITCH TO TANK
ON
RICH
ON

34
Q

ENGINE FAILURE DURING FLIGHT
Fuel Selector
Electric fuel pump
Mixture RICH
Carburetor heat
Engine gauges
Primer
When power is restored
Carburetor heat
Electric fuel pump
If power is not restored prepare for

A

SWITCH TO TANK
ON
CHECK for indication of cause of power loss
LOCKED

OFF
OFF

POWER OFF LANDING

35
Q

ENGINE FIRE DURING START
Starter
Mixture
Throttle
Electrical fuel pump
Fuel selector

If fire continues
Master
Aircraft

A

CRANK ENGINE
CUT-OFF
FULL OPEN
OFF
OFF

OFF
EVACUATE

36
Q

ENGINE FIRE IN FLIGHT
Source of fire

A

CHECK

37
Q

Electrical fire (smoke in cabin):

Master Switch
Vents
Cabin Heat
Land

A

OFF
OPEN
OFF
AS SOON AS POSIBLE

38
Q

Engine Fire

Fuel Selector
Throttle
Mixture
Electric Fuel Pump
Heater and defroster
Proceed with

A

OFF
CLOSED
CUT-OFF
OFF
OFF
POWER OFF LANDING