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Private Pilot Oral > EPs And Limits > Flashcards

EPs And Limits Flashcards

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Charter Pilot (Part 135) - Oral flashcards
1
Q

Vso (stall speed in landing configuration)

A

a

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2
Q

Vs1 (stall speed in specified (clean) configuration)

A

a

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3
Q

Vy (best rate of climb)

A

a

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4
Q

Vx (best angle of climb)

A

a

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5
Q

Vle (maximum landing gear extension speed)

A

a

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6
Q

Vlo (maximum landing gear operating speed)

A

a

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7
Q

Vfe (maximum flap extension speed)

A

DA 20 - 100 KIAS (takeoff) - 78 KIAS (landing)

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8
Q

Va (maneuvering speed)

A

DA 20 - 106 KIAS

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9
Q

Vno (normal operating speed)

A

DA 20 - 118 KIAS

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10
Q

Vne (never exceed speed)

A

DA 20 - 164 KIAS

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11
Q

Normal climb out speed

A

a

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12
Q

normal approach to land speed

A

a

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13
Q

what engine-out glide speed will give you maximum range

A

a

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14
Q

What is the make and horsepower of the engine

A

a

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15
Q

how may usable gallons of fuel can you carry

A

a

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16
Q

where are the fuel tanks located, and what are their capacities?

A

a

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17
Q

Where are the fuel vents for your aircraft

A

a

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18
Q

what is the octane rating of the fuel used by your aircraft

A

a

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19
Q

where are the fuel sumps located on your aircraft? When should you drain them?

A

a

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20
Q

What are the minimum and maximum oil capacities?

A

a

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21
Q

What weight of oil is being used

A

a

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22
Q

what is the maximum oil temp and pressure

A

a

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23
Q

is the landing gear fixed, manual, hydraulic or electric?

A

a

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24
Q

What are the nose wheel turning limitations for your aircraft?

A

a

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25
Q

What is the maximum allowable/demonstrated crosswind component

A

a

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26
Q

how many people will the aircraft carry safely with a full fuel load

A

a

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27
Q

what is the maximum allowable weight the aircraft can carry with baggage in the baggage compartment

A

a

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28
Q

what takeoff distance is required if a takeoff were made from a sea level pressure altitude

A

a

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29
Q

what is your maximum allowable useful load

A

a

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30
Q

solve a weight and balance problem for the flight you plan to make with one passenger at 170 pounds.

a. does your load fall within the weigh and balance envelope?
b. what is the final gross weight
c. how much fuel can be carried
d. how much baggage can be carried with full fuel?
e. Know the function of the various types of antennae on your aircraft.

A

a

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31
Q

Wing span tip to tip

A

DA 20 - 35 ft 9 in

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32
Q

length nose to tail

A

DA 20 - 23 ft 9 in

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33
Q

height

A

DA 20 - 7 ft 1 in

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34
Q

airfoil

A

DA 20 - Worthmann FX 63-137/2- HOAC

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35
Q

Wing area

A

DA 20 - 125 sq ft (11.6 m2)

36
Q

wing mean aerodynamic chord (MAC)

A

DA 20 - 3 ft 6.9 in (1.09 m)

37
Q

usable fuel

A

DA 20 - 24.0 US gal

38
Q

unusable fuel

A

DA 20 - 0.5 US gal

39
Q

Approved fuel grades

A

DA 20 - AVGAS 100 or 100LL

40
Q

propeller

A

DA 20 - two-bladed fix pitched propeller
diameter - 5 ft 9 in
pitch 62.8 inches

41
Q

max ramp weight

A

DA 20 - 1770 lbs

42
Q

max take off weight

A

DA 20 - 1764 lbs

43
Q

max landing weight

A

DA 20 - 1764 lbs

44
Q

empty weight

A

DA 20 -

45
Q

maximum bag compartment weight

A

DA 20 - 44 lbs

46
Q

white arc

A

DA 20 - 34 - 78 KIAS

47
Q

green arc

A

DA 20 - 42 - 118 KIAS

48
Q

yellow arc

A

DA 20 - 118 - 164 KIAS

49
Q

red line

A

DA 20 - 164 KIAS

50
Q 
oil pressure
red line/lower limit
green arc/normal operating
yellow arc/caution range
red line/upper limit
A 
DA 20 -  
red line/lower limit - 10 PSI 
green arc/normal operating - 30 - 60 psi
yellow arc/caution range - 10 - 30 psi, 60 - 100 psi
red line/upper limit - 100 PSI
51
Q 
oil temp
red line/lower limit
green arc/normal operating
yellow arc/caution range
red line/upper limit
A

DA 20 -
red line/lower limit - 75 degrees F
green arc/normal operating - 170 - 220 degrees F
yellow arc/caution range - 75 - 170 degrees F / 220 - 240 degrees F
red line/upper limit 240 degrees F

52
Q

fuel pressure indicator
red line / lower limit
red line / upper limit

A

DA 20 -
red line / lower limit - 3.5 psi
red line / upper limit - 16.5 psi

53
Q

engine failure after take-off with flaps in T/O position

A

60

54
Q

maneuvering speed

A

106

55
Q

airspeed for best glide

A

73

56
Q

precautionary landing

A

55

57
Q

emergency landing with engine off wing flaps in T/O position

A

60

58
Q

emergency landing with engine off wing flaps in ldg position

A

55

59
Q

emergency landing engine off wing flaps cruise

A

64

60
Q

Engine Failure during take off run

A 
throttle - idle
brakes - as required
flaps - cruise
mixture - idle cut-off
ignition switch - off
gen/bat master switch - off
61
Q

engine failure after take off

Insufficient Engine Power

A 
airspeed - 60 KIAS
throttle - full
mixture - full rich 
alternate air - on
fuel shut off valve - open
ignition switch - both
fuel pump - on
62
Q

engine failure after take off

Shortly Before Landing

A 
mixture - idle cut off
fuel shut off valve - closed
ignition switch - off
flaps - as required
gen/bat master switch - off
63
Q

engine failure during flight

engine running roughly

A

mixture - full rich
alternate air - open
fuel shut-off valve - open
fuel pump - on
ignition switch - cycle L - BOTH - R - BOTH
throttle - at present position
no improvement - reduce throttle to minimum required power, land as soon as possible

64
Q

loss of oil pressure

A

oil temp - check
if oil pressure drops below green arc above 2100 RPM- land at the nearest suitable airport
if oil pressure drops below green arc and oil temp is rising - reduce throttle to minimum required power and land as soon as possible. Be prepared for engine failure and an emergency landing

65
Q

loss of fuel pressure

A

fuel pump - on, and land at the nearest suitable airport
if fuel pressure is not restored - land at nearest suitable airport. Be prepared for engine failure and an emergency landing

66
Q

restarting the engine with propeller windmilling

A 
airspeed - 73 KIAS
mixture - full rich
fuel shut-off valve - open
ignition switch - both
fuel pump - on
fuel prime - on
throttle - 3/4 in forward
After successful re-start
oil pressure - check
oil temp - check
fuel prime - off
electrically powered equipment - on if required
67
Q

restarting the engine with propeller at fuel stop

A 
airspeed - 73 KIAS
electrically powered equipment - off
Gen/Bat master switch - on 
Mixture - full rich
fuel shut off valve - open
fuel pump - on
fuel prime - on
throttle - 3/4 in forward
ignition switch - start
ignition switch with push to start (optional) START (turn then push)
after successful re-start
oil pressure - check
oil temp - check
fuel prime - off
electrically powered equipment - on if required
68
Q

gliding

A

wing flaps - cruise
airspeed at 1764 lbs - 73 KIAS
glide ratio 11:1

69
Q

emergency landing with engine off

A 
airspeed (flaps T/O) - 60 KIAS
airspeed (flaps LDG) - 55 KIAS
airspeed (flaps cruise) - 64 KIAS
Fuel shut-off valve - closed
mixture - idle cut off
ignition switch - off
safety belts - secured
radio - transmit 121.5 mhz, giving location and intentions
flaps - as required
Gen/Bat master switch - off
after touch down - apply brakes
70
Q

precautionary landing with engine power available

A

1) search for a suitable place to land. Special attention must be given to wind direction and obstacles in the approach path
2) safety belts - secured
3) initiate descent
4) mixture - full rich
5) throttle - as required
6) trim - as required
7) wing flaps - as required (observe permissible speed)
8) over fly selected landing area (not below 500 ft/150m above ground) to confirm suitability and that approach route is free of obstacles
9) climb up to pattern altitude
10) low pass over flight at a safe altitude to observe any possible obstacles, such as cables, fences, ditches
11) climb up to pattern altitude
12) radio - transmit, giving location and intentions

13) final approach
a) mixture - full rich
b) throttle - as required
c) fuel pump - on
d) wing flaps - LDG
e) airspeed - 55 KIAS

14) touch-down is to be made with minimum airspeed, nose wheel should be kept above ground as long as possible

15) after touch-down
a) brake - as required
b) fuel shut-off valve - closed
c) mixture - idle cut off
d) ignition switch - off
e) Gen/Bat master switch - off

71
Q

engine fire during engine start up on the ground if the engine starts

A

throttle - 1800 RPM for a few minutes

engine - shutdown and inspect

72
Q

engine fire during engine start up on the ground if the engine fails to start

A 
ignition switch - continue cranking
throttle - max pwr
mixture - idle cutoff
fuel shut off valve - closed
cabin heat - off
fuel pump - off
gen/batt master switch - off
ignition switch - off
airplane - evacuate
fire - extinguish
engine - inspect
73
Q

engine fire during flight

A 
fuel shut off valve - closed
cabin heat - closed
airspeed - 73 KIAS
fuel pump - off
perform emergency landing with engine off according to paragraph 3.3.3
74
Q

electrical fire including smoke during flight

A

1) gen/bat master switch - off
2) cabin air - open
3) fire extinguisher - use only if smoke development continues
4) avionics master switch - off
5) electrically powered equipment - off
6) circuit breakers - pull all circuit breakers
7) circuit breakers - push BATTERY
8) gen/bat master switch - ON BAT 1/2 only
9) circuit breakers - push gen & gen control
10) gen/bat master switch - on
11) circuit breakers - on the AVIONIVS panel push the MASTER and MASTER CONTROL circuit breakers
12) avionics master switch - on
13) circuit breakers - push to activate systems as requried
14) radio - on
15) land as soon as possible

75
Q

electrical fire including smoke on the ground

A

1) gen/bat master switch - off

IF Engine is Running

2) throttle - idle
3) mixture - idle cut off
4) fuel shut off valve - closed
5) ignition switch - off
6) canopy - open
7) fire extinguisher - discharge as required

76
Q

cabin fire during flight

A 
gen/bat master switch - off
cabin air - open
cabin heat - closed
fire extinguisher - discharge as required
land as soon as possible
77
Q

icing unintentional flight into icing area

A

a) leave icing area (through change of altitude or change of flight direction to reach area with higher outside air temp
b) continue to move control surfaces to maintain their movability
c) alternate air - on
d) increase RPM to avoid icing of propeller blades (observe maximum RPM)
e) cabin heat - on defrost

78
Q

recovery from unintentional spin

A

throttle - idle
rudder - full applied opposite to direction of spin
control stick - ease forward
rudder - neutral after rotation has stopped
wing flaps - cruise
elevator - pull cautiously. bring airplane from descent into level flight position. do not exceed maximum permissible speed

79
Q

landing with defective tire on main landing gear

A

a) final approach with wing flaps in landing position
b) land airplane on the side of runway opposite to the side with the defective tire to compensate for change in direction which is to be expected during final rolling
c) land with wing slightly tipped in the direction of the non-defective tire. To increase the maneuverability during rolling, the nose-wheel should be brought to the ground as soon as possible after touch-down
d) to ease the load on the defective tire, the aileron should be fully applied in the direction of the non-defective tire

80
Q

electrical power failure - total electrical power failure

A

battery circuit breaker - if tripped, reset
gen/bat master switch - check on
master switch - off if power not restored
if unsuccessful - land at nearest suitable airport

81
Q

electrical power failure - generator failure

A

gen/bat master switch - cycle generator master switch off-on
generator circuit breaker - if tripped, reset
generator control circuit breaker - if tripped reset
if generator can not be brought on line - switch off all non flight essential electrical consumers. monitor ammeter and voltmeter land at nearest suitable airport

82
Q

low voltage indication (needle in yellow arc)

A

a

83
Q

flap system failure

A

a

84
Q

starter relay failure

A

a

85
Q

avionics system failure

A

a

86
Q

trim system failure

A

a

87
Q

instrument panel lighting failure

A

a

Private Pilot Oral (12 decks)

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