Aviation General Flashcards

1
Q

Indicated altitude

A

This is the altitude read directly from altimeter (uncorrected) when set to the current altimeter setting

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2
Q

Pressure altitude

A

The altitude that Is indicated when the altimeters barometric scale is set to 29.92 inch Hg. Pressure altitude is based on the standard atmosphere. It is used to determine:
True altitude
Density altitude
True airspeed

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3
Q

True altitude

A

This is our exact height above mean, sea level. Heights on aeronautical charts are given in terms of true altitude.

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4
Q

Absolute altitude

A

The actual height above the Earth surface in AGL with the altimeter setting correctly set an non-standard variation temperature taken into consideration.

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5
Q

Saskatoon ground control station

A

121.9 (Ground Control)

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6
Q

Saskatoon tower station

A

118.3

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7
Q

Atis station

A

128.4

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8
Q

DEPARTURE PROCEDURE:

A

The winds are at. _____at_____KTs, So we are anticipating Runway_______With a crosswind of_______.
Anticipating Taxi instructions of __
Upon Clearance onto the active Runway I will make a________(left, right) turn to enter the runway.
After takeoff Expecting a turn to the____(right, left)

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9
Q

TAKEOFF BREIFING

A

This will be a___________(normal, short, soft, XW) Takeoff, flaps at_______-
The calls will be:
POWER SET
ENGINE GAUGES GREEN
AIRSPEED ALIVE
I will ROTATE at ______(55KTs)
Any abnormality affecting safety before rotation, I will call REJECT, REDUCE power, Exit Runway, INFORM ATC

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10
Q

ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF

A Mad Father Introduces Wicked Magic

A

A Mad Father Introduces Wicked Magic

1 airspeed - 65 KIAS flaps up
60 KIAS flaps down
2 mixture – idle cut-off
3 fuel selector valve - off
4 ignition switch- off
5 wing flaps – as required
6 master switch - OFF

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11
Q

Engine failure-IF INSUFFICIENT RUNWAY REMAINING, I will:

A

Land up to 30 degrees left/right of centre line at best glide of 65/70KTs

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12
Q

AFTER ENGINE RUN UP:

A

CALL FOR TAXI CLEARANCE - 121.90(GROUND CONTROL)

Saskatoon ground_THIS IS…ready for taxi with information________-(ATIS)
(IF 09/15 ACTIVE) (Requesting intersection departure at______(15=Alpha;
09=bravo), remaining rwy length sufficient.
Listen to ground…Repeat REGISTRATION

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13
Q

CALL FOR CLEARANCE:

A

118.3
Saskatoon Tower_____(registration) holding short of runway________at taxiway________ ready for departure

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14
Q

Normal TAKE-OFF:

A

FLAPS ________0-10 degrees
Carb Heat _____COLD
THROTTLE ____FULL
POWER SET
ENGINE GAUGES GREEN
AIRSPEED ALIVE
LIFT NOSE _____55 KTs
CLIMB________70-80 KTs

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15
Q

400/500 ft checks

A

NO- SMOKE, FIRE, FLUIDS
LANDING LIGHT OFF
FLAPS - UP
Maintain runway heading
Climb to 2650ft

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16
Q

ENTERING TRAINING AREA

A

126.7 (ENROUTE)
Saskatoon Training area traffic______(Registration)
Where you are_________ (Altitude, Cory mine, Agrium mine-Vanscoy)
Where you will be working_________(N/S/E/W;Deslile, Vanscoy, N/S of Highway Etc,
At_______(Altitude and below)

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17
Q

RETURNING FROM TRAINING AREA:

A

118.3 (ATC)
Saskatoon Tower________(Registration)
Requesting to enter (L/R Downwind)_____
For Runway _______
For a (Touch & go, full stop)_________

(Repeat instructions or clearance) _____________(Registration)

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18
Q

PRELANDING CHECKS…

A

On downwind -mid field

Primer in - locked
Master switch———ON
Mags on both
LANDING LIGHT———ON
CARB HEAT______ HOT
Mixture__________RICH
FUEL SELECTOR——BOTH
Tap the breaks
Power reduced___1500 RPM
FLAPS 10 degrees Below VFE (arch) ——70 KTS
AIR SPEED 75
Passenger Safety Briefing

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19
Q

NORMAL LANDING:

A

1-Carb heat hot -SLOW TO 70kts 10Degrees FLAPS
2-BASE -FLAPS 20 degrees 70Kts
3-TRIM
4-TURN to FINAL-ALIGN Active RWY
5-Establish glide path - RWY (60-70kts)
Control a/s w/ attitude & decent w/pwr
6-Keep airplane in trim until Flare
7-Reduce power-idle when RWY is ensured
8-start flare 30’ above ground (pitch back, never forward)
9-keep pulling back, hold airplane off ground, until no longer flies
10- land in first 1/3 of runway (always have Go/No Go point

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20
Q

OVERSHOOT

A
  • FULL POWER
  • CLIMB OUT
  • FLAPS STAGES
  • IF NEEDED:
  • Turn gently to right of runway
  • While doing avoid departure stall
    Don’t climb to high, may be aircraft crossing field
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21
Q

ON TAXIWAY AFTER LANDING:

A

121.90 (GROUND CONTROL)
Saskatoon Ground________(registration)
On taxiway ____________
Requesting Taxi to the Hanger.
(Confirm by repeating_______(registration)

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22
Q

500 ft base to final turn
Ft ASL?

A

2150 ASL

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23
Q

Stable by 200 AGL
Ft ASL?

A

1850 ASL

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24
Q

False assumption

A

False assumptions are when you make assumptions base on incorrect information or ignored information

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25
Q

Expectancy

A

As a pilot you may be expecting the take off clearance but are given a hold short
Experience could just as well serve to strengthen expectancy

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26
Q

Fixation

A

Fixing your attention on one item while something more important goes unnoticed
For example dropping your pencil, while trying to retrieve it you neglect to control the altitude

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27
Q

Ignoring bad news

A

Get home itis over bad weather report

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28
Q

High concentration

A

There is a tendency to relax and make false assumptions after periods of high concentration.
For example you successfully fly through bad weather only to land at your destination airport in good weather-but downwind

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29
Q

Regression

A

A pilot with lots of experience on one type of airplane could be vulnerable to false assumptions by operating switches that are reversed in a different type.
Example
Throttle and mixture positions
Landing gear and flaps position

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30
Q

Stress

A

Many things cause stress, lack of sleep, fatigue, heat, illness, poor diet and interpersonal problems to name a few.

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31
Q

Low stress arousal

A

Some stress is not always bad

It alerts us (arousal) and this can help us think clearly and operate efficiently

To much can result in discomfort, or even panic

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32
Q

Overload

A

Stress can be seen as an overload caused by pressures.
These can be physical pressures such as an extreme temperature and/or moisture, noise, vibration or lack of oxygen.

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33
Q

Altimeter settings

A

Station pressure reduced to Sea Level Pressure using the standard temperature of 15° C and the standard lapse rate of 1.98°C per 1000 ft

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34
Q

Turning DOWN the Altimeter sub-scale results in:

A

A LOWER indicated Altitude

35
Q

If altimeter, setting, given by an aerodrome varies more than ————-the the Altimeter needs to be re-calibrated.

A

50 feet from field elevation

36
Q

Station pressure reduced to Sea Level Pressure is know as

A

Altimeter setting

37
Q

In Determining MSL pressure we use what temperature

A

The average temperature over the past 12hrs

38
Q

To determine Alt Setting we use what temperature

A

Standard temperature

39
Q

Always try to use alt setting for nearest field preferably with/in ————miles

A

100 miles

40
Q

Decrease in pressure equals a————-in Altitude

A

Increase

41
Q

Increase in Pressure equals a ————in Altitude

A

Decrease in altitude

42
Q

What are the two methods by which the altimeter pointers can be moved?

A

1 changes in air pressure (climbing/descending)
2 strictly Mechanical (rotating the knob on the altimeter)

43
Q

FROM HIGH (pressure+temperature) TO LOW (pressure+tempere)

A

Look out below
Flying lower than altimeter reads

44
Q

FROM LOW (pressure + Temperature ) TO HIGH (pressure+temperature )

A

To much Sky
Flying higher than altimeter reads

45
Q

When Alt setting goes down in in Hg the Altimeter goes up or down?

A

Down in height

46
Q

Air pressure is:

A

The sum force applied by all the air molecules in the atmosphere above us.

47
Q

AIM

A

Aeronautical Information Manuel

48
Q

Colder than standard temp will place the aircraft———than the alt indicates

A

LOWER

49
Q

FROM HOT TO COLD ————

A

You are being BOLD
(Indicated alt will be higher than true)

50
Q

Pressure Altitude

A

Altitude that is indicated when the barometric scale on the Altimeter is set to 29.92 in Hg

51
Q

ISA

A

Sea level
Perfectly dry
Lapse rate 1.98°C per 100ft
29.92 in Hg pressure

52
Q

Pressure altitude is used to determine:

A

Density altitude
True Altitude
True airspeed

53
Q

Density Altitude =

A

Pressure altitude corrected for non standard temperature variations (actual temperature for the pressure altitude)
Also the height the aircraft thinks it is flying Above Sea Level

54
Q

High density altitude means:

A

The aircraft feels like it is at a high altitude (poorer performance)

55
Q

True altitude is

A

Our exact Height above sea level

56
Q

Absolute altitude is

A

Our exact height above terrain

57
Q

Calculating True Altitude RULE OF THUMB METHOD

A

Multiply 4ft per 1000ft for each 1 degree Celsius the temperature varies from ISA
Eg:
-outside air temp is 0°C
-ISA at 5000 feet is 15° (Sea level) - 10° (2°C/1000 ft) = 5°C
- 0° -5° equals -5° colder than ISA
- 5 (thousand) x 4 feet = 20 feet
- 20 feet x -5= -1000 feet
- actual altitude is 5000 ft - 100 feet = 4900 feet

58
Q

True altitude rule of thumb equation:

A

True altitude= indicated altitude + ( ISA deviation x4/1000) x indicated altitude

59
Q

Take off and landing performance data in POH and AFM are typically given in

A

Density Altitude

60
Q

ENGINE FAILURE ABOVE 500FT:

A

Best glide of 65/70Kts, reassess at that time, with a potential to turn back to the airfield

61
Q

Lapse rate =

A

The rate of change of temperature with height (1.98°C per 1000 feet)

62
Q

Inversions

A

Temp of the atmosphere increases with an increase in altitude
(When an inversion occurs the air is very stable)

63
Q

5 phases of Landings

A

Approach
Round out
Flare
Touchdown
Rollout

64
Q

Forward slip=

A

Moving forward
Path over the ground
(Rudder all the way to floor (or as much as you can manage), use aileron to keep airplane moving in forward flight path)

65
Q

Side slip

A

Moving forward and sideways path over ground. Point ailerons in the way you want to go and just enough rudder to keep lined up with runway.

66
Q

Wind shear

A

Rapidly changing wind.
“Tearing” of the wind as it changes abruptly.
It could be horizontal, such as from a low level, jetstream, or vertical, such as from convective weather.

67
Q

NOTAMS

A

1 Continuity number
2 NOTAM type (new, replace, cancel)
3 Qualifier line
4 FIR (flight info region)
5 Code group 5 letters (1st Q)
6 Traffic type I, V or IV
7 NOTAM purpose (N,B,O,M, K)
8 Applicable scope of NOTAM
9 Lower limit/upper limit
10 Geographical Coordinates
11 Radius of area of Influence
12 Item A location indicator
13 Item B start time
14 Item C end time
15 Item D if occurs on specific time
16 Item E English text decoded NOTAM
17 Item F lower limit for NOTAM
18 item G upper limit airspace restrictions/ Nav warnings

68
Q

P6SM

A

Plus 6 statute miles visibility

69
Q

Intensity symbols

A

(-) light
(No sign) moderate
(+) Heavy

70
Q

IFR

A

Less than 1000 feet AGL, and or less than 3SM

71
Q

MVFR

A

Between 1000 and 3000 AGL, and or between 3 to 5SM

72
Q

VFR

A

More than 3000 feet AGL and or more than 5SM

73
Q

LCL

A

Local
Special coverage 25% or less

74
Q

PTCHY

A

Patchy
26 to 50% coverage

75
Q

XTENSV

A

Extensive
Greater than 50% coverage

76
Q

Instruments needed for date VFR:

A

Magnetic compass
Airspeed indicator
Sensitive altimeter: (to Needles)
Time piece
Engine instruments:
Tachometer
Oil pressure
Oil temperature
Fuel gauge is for each main tank
MP gauge (for aircraft with variable pitch propeller’s, super charged, or turbo, charged engine, or helicopters)
Radio if operating in an MS or class B, C, or D airspace

77
Q

Position and anti-collision lights:

A

Navigation position lights:
Red light on the left wing tip
Green light on right wing tip
White light on the tail

Anticollision lights
Flashing white, red, or both

78
Q

What anticollision late is required if flying at night with passengers?

A

If functioning landing light

79
Q

FLAPS

A

Devices on the wing to increase lift and drag by increasing the camber of the wing

80
Q

Defined night
EECT-BMCT

A

EECT-BMCT
The time between the end of evening, civil twilight, and the beginning of morning civil twilight

81
Q

Computed heading =

A

Magnetic heading 

82
Q

What will change the stalling angle of attack? 

A

Flaps setting, and contamination will change the stolen angle of attack

83
Q

What will change the stalling speed of an aircraft? 

A

Weight, CG & bank angle.