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SFC - SATM > Ch 6: Circuits > Flashcards

Ch 6: Circuits Flashcards

1
Q

Ch 4 Rev: Max AoB for climbing turn… (Pg 67)

A

15°

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2
Q

Ch 4 Rev: Procedure for levelling off from a climb… (Pg 67)

A

AASPT
A - Anticiapte
A - Attitude
S - Speed
P - Power
T - Trim

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3
Q

Rev: It is imperative the ___ is w/in the white arc before ____ (Pg 67)

A

Airspeed, extending flaps

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4
Q

Take-Off Safety Speed (VToss): (Pg 67)

A

Min speed to which as AC must be accelerated to achieve TODR, = Stall speed (Vs) x safety factor of 20%

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5
Q

Landing Reference Speed (VREF): (Pg 67)

A

Airspeed the aeroplane will cross the threshold at = published in POH, = stall speed (Vs) in landing config x 1.3 (30%)

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6
Q

Maximum Take-Off Weight (MTOW): (Pg 67)

A

Max weight at which AC can take-off at, specified in POH

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7
Q

Take-off Runway Available (TORA): (Pg 67)

A

Declared surface available for AC to take-off on

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8
Q

Take-off Distance Available (TODA): (Pg 67)

A

Distance available for take-off from beginning of runway to 50ft AGL, inc runway, stop-way and clearway

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9
Q

Take-Off Distance Required (TODR): (Pg 67)

A

Distance aeroplane will require to accelerate from a standing start and reach 50ft AGL whilst achieving VTOSS (take-off safety speed)
Determined by Performance charts x safety factor of 15%

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10
Q

Landing Distance Available (LDA): (Pg 67)

A

Length of runway available and suitable for ground run

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11
Q

Landing Distance Required (LDR): (Pg 67)

A

Distance required for an AC to come from height of 50ft AGL to a complete stop x factor of 15%

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12
Q

Static RPM: (Pg 67)

A

Acceptable range of engine RPM with aeroplane at beginning of take-off roll, indicating sufficient power production by the engine

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13
Q

Circuit legs: (Pg 68)

A

1 Upwind, 2 Crosswind, 3 Downwind, 4 Base, 5 Final

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14
Q

Upwind = (Pg 68)

A

Initial Leg after TO, consists of climb to at least 500ft AGL, whilst tracking along extened centreline of RW

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15
Q

Crosswind = (Pg 68)

A

Carrying out 15° AoB climbing turn through 90°heading change to track perpendicular to RW, climb continued to 1000ft AGL

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16
Q

Downwind = (Pg 68)

A

Initiated when upwind threshold of RW = 45° to aeroplane’s position, downwind = reciprocal of RW

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17
Q

Base = (Pg 68)

A

Consists of descending turn through 90° heading change, should begin when aeroplane’s position = 45° to RW landing threshold, should descend to 500ft AGL

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18
Q

Final = (Pg 68)

A

Descent from 500ft AGL along extended centreline of RW

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19
Q

Factors affecting performance: (Pg 68)

A

Wind, Weight, Slope, Surface, Air Density, Flaps

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20
Q

Wind affects TODR + LDR: (Pg 68)

A

Headwind TODR = Reduced, LDR = Reduced
Tailwind TODR = Increased, LDR = Increased

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21
Q

Weight affects TODR + LDR: (Pg 69)

A

TODR = Increase, LDR = Increase

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22
Q

Slope affects TODR + LDR: (Pg 69)

A

Downslope TODR = Reduced, LDR = Increase
Upslope TODR = Increase, LDR = Reduced

23
Q

Surface affects TODR + LDR: (Pg 69)

A

Grass surface TODR = Increase, LDR = Reduced

24
Q

Air Density affects TODR + LDR: (Pg 69)

A

Increased AD TODR = Increase, LDR = Increase

25
Q

Flaps affect TODR + LDR: (Pg 69)

A

Flaps extended TODR = Increase, LDR = Reduce

26
Q

Touchdown Options: (Pg 70)

A

Full stop, Touch + Go, Stop + Go

27
Q

Full stop = (Pg 70)

A

Touching down on RW to complete stop, or slow enough to taxi off RW

28
Q

Touch + Go = (Pg 70)

A

Normal landing followed by immediate TO w/out stopping or braking, allows for smoother swifter circuit training

29
Q

Stop + Go = (Pg 70)

A

AC brought to complete stop, allowing pilot to conduct all checks from static start to complete stop again

30
Q

Go-Arounds = (Pg 70)

A

Aborting approach to land or from landing phase and conducting climb back to circuit height and set up for another attempt
Should be conducted whenever any doubt

31
Q

Factors used to determine Go-Around: (Pg 70)

A
  • Greater than 40° AoB required on BASE/FINAL
  • Large ‘S’ Turns to regain centreline
  • Not lined up by 400ft AGL on FINAL
  • No clearance to touch-down by 200ft AGL
  • Too close to preceding AC in BASE/FINAL
  • RW not clear
  • Wind-shear beyond ability of pilot encountered
  • Not touched down by 1/3 length of RW
  • High and/or dangerous bounce encountered during landing
  • Unsatisfied w/ approach
32
Q

Go-Around technique: (Pg 71)

A
  • Apply FULL power
  • Balance w/ rudder, adopt climb attitude ~Vy
  • After +ve RoC, retract flaps 1 stg at time
  • Position aeroplane to side of RW, over TW ‘Bravo’
  • After TO checks once at safe altitude
  • If able, notify ATC of go-around
33
Q

Start-Up + Ground Ops: (Pg 71)

A
  • Copy ATIS details on freq 120.9
  • Bankstown Grd 119.9 req start up for circuits
  • Start up procedure
  • Taxi to manoeuvring area req taxi clearance for circuits
  • Clearance initially for run-up bays, further clearance given out once ready
  • Bankstown circuit freq = Bankstown tower 123.6, contacted at holding point
34
Q

Line-Up procedure: (Pg 73)

A
  • Lights = as req
  • Transpoder ALT mode
  • Pitot Heat = as req
  • Windsock checked
  • DI/Compass = Aligned and checked
35
Q

Rolling checks: (Pg 73)

A
  • Static RPM = achieved
  • Ts + Ps = Green
  • Airspeed alive + increasing
36
Q

At ___ carry out ____ checks (Pg 73)

A

300ft, after Take-Off

37
Q

After TO checks: (Pg 73)

A
  • Flaps = retracted
  • Power = check
  • Engine instruments = green
  • Lights as req in circuit
  • Ref point = selected
38
Q

At 400ft conduct ____: (Pg 73)

A

Effective lookout in direction of upcoming crosswind, once behind the wing can conduct downwind turn

39
Q

Crosswind Work Cycle: (Pg 74)

A

ALAP
A - maintain Vy
L - Scan for preceeding AC and spacing
A - “”
P - (1) IAS = Vy (2) Alt = anticipate target height (3) DI = RW heading +/- 90°

40
Q

Downwind initiated when RW threshold is ___: (Pg 74)

A

45°

41
Q

Downwind Work Cycle: (Pg 74)

A

H - Height = 1000ft AGL
H - Heading = Maintain downwind track
S - Speed = Maintain NC
S - Spacing = RW centreline should cut through wing ~1/3 from wingtip at wings level

42
Q

Pre-landing procedure = (Pg 75)

A

B - Brakes = Check brake pressure/park brake off
U - Undercarriage = Fixed
M - Mixture = Full RICH
F - Fuel = Fullest tank
I - Instruments = Green
S - Switches = Lights, batt, alt EFP ON, mags BOTH
H - Hatches/Harnesses = Fastened and adjusted

43
Q

Approach config: (Pg 75)

A

P - 1700RPM
A - Initially maintain 1/3 grnd, reduce IAS + adjust for 1/2 grnd
S - Verbalise white arc, set 2 stages flaps (VREF = 75kts)
T - Use liberally

44
Q

Base work cycle: (Pg 76)

A

A - Attitude = Set + Maintain 1/2 grnd
A - Airspeed = Trimmed for 75kts
A - Aspect = Judge is too high/low/near/far

45
Q

Base leg = (Pg 76)

A

500ft AGL on extended centreline of RW

46
Q

Final Approach = (Pg 76)

A

Aim point = ‘numbers’ in normal approach, should remain constant 1/3 in windscreen

47
Q

Final Approach Work Cycle: (Pg 76)

A

A - Aim point = RW numbers 1/3 windscreen
A - Airspeed = 75kts reducing towards VREF by 300ft AGL
A - Aspect = Judgement of centreline

48
Q

When passes 300ft on final…. (Pg 76)

A
  • Flaps = as req
  • Carby heat = Full OFF
  • Clearance = Obtained and RW clear
  • Windsock = Speed and direction confirmed
49
Q

Round-Out, Hold-Off + Touchdown: (Pg 77)

A
  • Progressively reducing rate of descent to zero, ~ 1 foot of grnd
  • As Aimpoint moves under nose, smoothrly reduce power to idle, look far end of RW
  • Use rudder to keep nose straight, and aileron to maintain centreline
  • Apply back-pressure to remain S + L
50
Q

Hold-Off: (Pg 77)

A
  • Gradually increasing back-pressure to combar rate of sink, and prevent from touching down
  • Smoothly relax back-pressure and allow nose-wheel to touchdown on centreline
51
Q

Touch + Go: (Pg 77)

A
  • Carry out landing as above, once safely on grnd and under control, reclaim centreline w/ rudder
  • Retract flaps and apply full power and check RPM
  • Check engine instruments = green, IAS increasing towards VR
52
Q

After Landing checks: (Pg 78)

A

F - Flaps retracted
F - Fuel Pump OFF
E - Engage = Obtain taxi clearance from ATC (119.9)
L - Lights = Landing and Strobe OFF
L - Lean mixture for taxi
T - Trim = neutral
T - Transponder = SBY/GND

53
Q
A
54
Q
A

SFC - SATM (12 decks)

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