Misc. Flashcards

1
Q

Missed Approach Criterial

A
  1. ) Out of tolerances beyond the FAF
  2. ) Aid is suspect
  3. ) Not visual by the DA/MDA
  4. ) Cannot conduct a landing to the runway unless circling
  5. ) Visual reference is lost during a circling approach

Provides 100ft clearance on a gradient of 2.5%

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2
Q

When can you start circling to land from an approach?

A
  1. ) Within the circling area
  2. ) Weather is not less than that on the plate
  3. ) Visual reference is maintained with the runway/landing area
  4. ) Can descend below the MDA as long as you can maintain obstacle clearance for the aircraft category (400ft)
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3
Q

When can you descend below MDA?

A
  1. ) Visual reference is maintained
  2. ) Weather is not below that on the chart
  3. ) Landing can be made using standard rates of descent
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4
Q

When can you be cleared for a visual approach?

A

IFR flights:

  1. ) Within 30nm of the airfield
  2. ) Clear of cloud
  3. ) In sight of ground or water
  4. ) 5000m vis

VFR flights:
1.) Within 30nm of the airfield

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5
Q

Aircraft shall not be flown below what altitudes when VFR

A
  1. ) 1000ft amsl over populated areas

2. ) 500ft amsl above obstacles or water

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6
Q

When is an aircraft considered well clear of another aircraft?

A

500ft Vertically and 600m horizontally. Similar to class D VMC criteria

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7
Q

Pilots must obtain ATC clearance before operating in controlled airspace. In class E airspace clearance is not required when…

A
  1. ) IFR operating within the IFR pickup procedure

2. ) VFR flights

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8
Q

When operating in controlled Aerodromes the ATIS must be obtained when?

A

Prior to taxi request

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9
Q

IFR flights may request a visual departure when…

A

The cloud base will allow the aircraft to climb VMC to LSALT applicable to the departure.

Can be below it but must be able to maintain VMC

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10
Q

Where should an aircraft establish themselves on the outbound track?

A

Within 5nm of the airfield unless on a SID or instructed by ATC

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11
Q

When should a pilot change the frequency from tower?

A

Preferably within 1nm of becoming airborne

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12
Q

What are the cruising altitudes for a VFR aircraft?

A

Aircraft heading east will fly on odd numbers, aircraft flying west at even. VFR will fly 500ft above the even thousands.

East:
3500, 5500, 7500, 9500 ect
West:
4500, 6500, 8500, 10,500 ect

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13
Q

During a visual approach a pilot cannot descend below…

A

IFR flights:

  • Not less than 500ft above the lower limit of CTA
  • or the LSALT at night, whichever is higher.

VFR flights:

  • Not operate below the lowest alt permissible (500ft or 1000ft if populated areas)
  • until within 3nm if at night
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14
Q

When being vectored to 10nm final or initial when can a pilot report ‘visual’?

A

When satisfied that the conditions required for a visual approach can be met.

  • within 30nm
  • Clear or Cloud
  • in sight of ground/water
  • 5000m vis

(Can cancel IFR and operate VFR only if you meet the VFR separation requirements for that airspace)

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15
Q

In the event an IFR flight conducting a visual approach in VMC wants to ‘go around’ what must you do?

A

Fly the instrument missed approach procedure.

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16
Q

When an alternate aerodrome is required it must be…

A
  1. ) Suitable to the aircraft

2. ) Not require an alternate itself

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17
Q

When must a pilot plan for an alternate?

A
  1. ) More than SCT cloud below the alt min (second lowest appr for that Aerodrome. PC21 lowest and second lowest is the ILS due seperate independent ILS ability)
  2. ) Visibility less than the minimum
  3. ) Forecast of fog or weather that reduces weather below the requirement for visibility
  4. ) Wind exceeds limits
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18
Q

When could you carry holding fuel instead of an alternate?

A
  • If the weather is forecast to be less than alt. minima but are expected to improve. You carry fuel until that time plus 30mins
  • If the weather is above alt minima but has temporary deterioration less than alt minimal. You carry the INTER/TEMPO fuel.
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19
Q

When weather following a FM or BECMG creates a need to carry fuel when does it become valid

A

30min before and after the specified time.

Unless within the first 3 hours of a TAF3

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20
Q

During the first 3 hours of a TAF3 what what does not apply?

A
  1. ) 30 minute buffer period

2. ) Alternate or holding fuel required by reduction in visibility or Prob 30/40

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21
Q

What is the alternate minima?

A
  1. ) Cloud more than SCT below HAT/HAA
  2. ) Visibility below that on the chart plus 2000m
  3. ) For aerodromes without an instrument approach procedure - LSALT +500ft and 8000m vis
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22
Q

When is the 80lbs I’d approach fuel required?

A

More than SCT below LSALT + 500ft and vis <5000m

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23
Q

What are the minimum fuel requirements downwind?

A

<200lbs downwind - “minimum fuel”

<140lbs downwind - “Pan pan”

<70lbs downwind - “Mayday”

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24
Q

Special VFR allows…

A
  • 1600m visibility

- Clear of cloud

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25
Q

Class D VMC requirements

A
  • 1000ft above
  • 500ft below
  • 600m horizontally
  • SVFR able
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26
Q

Class C/E VFR requirements:

A

> 10,000ft - 1000ft vertically, 1500m horizontally, 8k visibility

<10,000ft - 1000ft vertically, 1500m horizontally, 5km visibility

SVFR available

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27
Q

Class G VMC Conditions

A

Same as class C conditions

<3000ft, clear of cloud, 5km visibility

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28
Q

Prohibited, Restricted, Danger areas

A

Prohibited - no flight under any circumstances

Restricted:
RA1 - Can plan through and expect a clearance
RA2 - Cannot plan through, clearance not assured
RA3 - Cannot plan through, no clearance

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29
Q

RNAV Approach capture regions:

A

Straight in fix is 70’ either side of the final approach track

The ‘wing’ fixes are 180’ aligned with the final approach track

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30
Q

Accurate QNH provided by…

A

ATC
ATIS
Casa approved observers
Valid for 15 mins from the time of receipt

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31
Q

ATC light codes in the air

A

Steady Green - Land if not collision risk exists
Steady red - give way and continue circling
Flashing green - return to land
Flashing red - Aerodrome unsafe

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32
Q

ATC light codes on the ground

A

Steady green - take off if no collision risk exists
Steady red - stop
Flashing green - taxi If no collision risk exists
Flashing red - taxi clear of RWY
Flashing white - return to starting point

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33
Q

Idle descent profile

A
  • 8’ CDM
  • 7’ PFD
    1. 2nm/1000ft
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34
Q

Cruise descent profile

A

25% TQ
-4’ CDM
-3’ PFD
2nm/1000ft

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35
Q

Clean glide profile

A

140KIAS
-4’ CDM
0’ PFD
2nm/1000ft

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36
Q

Glide profile (Gear and TO flap)

A
130KIAS
-8’ CDM
-4’ PFD
1nm/1000ft
Top of HUD glass
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37
Q

Glide Profile (Gear and LDG Flap)

A
125KIAS
-12’ CDM
-8’ PFD
0.8nm/1000ft
Horizon just under the canopy bow
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38
Q

Glide cone formula

A

(Alt. -3.5) x 2

(8000ft - 3.5) x 2

4.5 x 2 = 9nm glide cone

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39
Q

Aerobatics not to be conducted…

A

Below 3000ft or above built up areas

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40
Q

Spins

A

3s per turn
500ft per turn for planning
Initiate recovery 6000ft above ground/cloud
Recovered by 3000ft above cloud or ground

Eject by LSALT if above cloud

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41
Q

G Warm

A

Conducted if more than 3G expected

All solo operations

If not flown for 14 days

180’ turn and pull to 3G and squeeze to 4G

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42
Q

Controllability check

A
  • Climb not below 3000ft at an airspeed greater or equal to that which the damage occurred.
  • Reduce airspeed to the highest of the following. Threshold speed, stall tone, half control deflection or abnormal handling
  • Recover by straight in approach at that speed +10kts

If engine damage expected, don’t change power until over the field and able to recover by PFL

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43
Q

RADALT setting during, 2D approach, 3D approach, circling

A

2D approach - 250FT
3D approach - HAT
Circling - 400FT

44
Q

Pc - 21 wind limitations

A
  • 24kts crosswind
  • Steady 30kts or gusting 35 for ejection
  • 35kts for canopy
  • 10kts tailwind (nothing of it’s wet)
45
Q

Runway length required

A

5000ft +5% per 1000ft elevation

Must conduct an aborted T/O if full power not applied with 4000ft remaining

46
Q

G limits for different configurations

A

-4 to 8
Gear extended -4 to 8
Gear in transition 0 to 2
Flaps extended or in transition 0 to 4

47
Q

Battery voltage for start

A
-10’ = 24.3v
0’ = 24.1v
10’ = 24.0v
20’ = 23.9v

External power required for less than 23.9v and Batt must be charged if less than 23.6

48
Q

IF PFD profiles

A

CLIMBS:
Climb - 180KIAS and ~15’ PFD
Max angle - 130KIAS and ~ 20’ PFD

DESCENTS:
Std - idle, 240KIAS, -7’ PFD
Idle - 25% TQ, 240KIAS, -5’ PFD

S&L:
160KIAS - 4’ PFD, 25% TQ
240KIAS - 0’ PFD, 54% TQ

49
Q

Radial Intercepts

A

If ‘outbound’ just put the radial HDG

If ‘inbound’ you calculate the reciprocal

Anticipation:

(60/DME) x 1.5

30’ intercept = 1/3
45’ intercept = 1/2
60’ intercept = 2/3
90’ intercept = 3/3

50
Q

SID climb gradients

A
  1. 0% = 540fpm
  2. 3% = 600fpm
  3. 6% = 650fpm

0.3% = +50fpm
Gradient % = RoC/Ground speed

51
Q

What emergency training is prohibited in the aircraft

A
  • Deliberate shutdown of an engine
  • EFATO and turn back training
  • Emergencies that require simulation of a service selection
52
Q

What altitude can low flying be conducted?

A

Surveyed areas - 150ft

Unsurveyed - 250ft HAOW 600m

53
Q

What independent NAVAIDS/ navigational equipment does the PC-21 have?

A

VOR and ILS - Two independant receivers

DME - One independent transmitter receiver

GLSSU - Two receivers that can be considered independent provided;

  1. Both seats are occupied
  2. If solo the FMS with the appropriate RNAV is set and loaded with no discontinuities
54
Q

ALTSEL should be set to:

A
  • Assigned altitude
  • MAPt altitude
  • LSALT
  • Airspace Limit
55
Q

Under training, can you conduct full stop landings with Trim Ail power off?

A

No

56
Q

What speed should you reduce braking when landing due anti skid and what speed does the ant skid cut out

A

Reduce at 25kts and anti skid cuts out at 10kts

57
Q

Aerobatics is defined as…

A

> 45’ in pitch
90’ AoB
IAS < Vs x 1.3

58
Q

What’s the definition of an emergency situation/MAYDAY

A

Non routine occurrence when injury or aircraft damage occurs or is threatened and immediate remedial action is warranted

59
Q

What is the definition of an Abnormal situation

A

Non routine occurrence, less severe and urgent than an emergency when remedial action is warranted as soon as practicable

60
Q

Definition of ‘Land as soon as Practicable’

A

Abort the mission and land at the nearest suitable airfield for safe operation of the jet

61
Q

Definition of land as soon as practicable

A

May abort or continue the mission, divert or land at the planned destination taking into consideration the situation, aircraft condition, aircraft performance, weather, airfield services

62
Q

Flight manual definition of a warning?

A

Operating procedure which if not rectified immediately could result in injury or death

63
Q

Flight manual definition of caution?

A

Operating procedure which if not strictly observed could result in damage to equipment

64
Q

What is TOD

A

Take off distance from brakes release to clearing a 50ft screen height

65
Q

What is TOR

A

Take off run, distance from brakes release to lift off

66
Q

What is LDG distance?

A

Distance from 50ft screen height to a full stop

67
Q

If a spot height is enclosed by a contour line. How do you calculate LSALT?

A

Spot height +1000ft +360ft rounded up

68
Q

How do you calculate the LSALT if you’ve got contours?

A

Round up to the next contour height. +1000ft +360ft

69
Q

When can you proceed with an instrument approach without entering a hold?

A
  • ATC have cleared you for the approach

- you’re within the DME arc requirements

70
Q

Engine ITT limits during; Start, ground ops, normal ops

A

Start
>860 for 20s
>910 for 5s
>1000 never

Ground
NG between 50.7% and 63% >750 for 10s

Air
>860 for 20s
>910

71
Q

Max TQ in the air

A

4202ft lbs

72
Q

The PT61B has two main sections, what are they?

A

Gas generator section:
Contains a compressor sections and a combustion section

Power turbine section:
Drives the Accessory gearbox

73
Q

What is driven by the accessory gearbox?

A
Gen 1 
Gen 2
Fuel Pump (Low and high pressure)
Hydraulic pump 
Oil pumps
74
Q

How does the PMS control engine output?

A

By adjusting fuel flow and propeller speed based of blade angle in conjunction with PCL position

75
Q

What component make up the PMS

A
  • Propeller Interface Unit
  • Permenant magnet alternator
  • Fuel Metering unit
  • Data Collection unit
  • Power Management Unit
76
Q

Where should the PCL be when selecting PMS to manual?

A

Aft of <55’ or the nominal fuel scheduling will not be implimented limiting power

77
Q

When is the power of the engine limited?

A

Below 80kts it’s limited to 1080hp and 2836ft lbs

Above 80kts it increases linearly to 1600hp and 4202ft lbs by 200kts

78
Q

When will the engine do an auto shutdown on start up, what will happen after and how long?

A

When limits are exceeded (Hung Start, no light up, ITT exceeded)

Dry run for 10-30s

*moving the PCL FWD of 3’ will disable the auto shutdown and will not do the dry run. Will not retain it within limits

79
Q

How does the engine fire detection system work?

A

Two ‘loops’ one around the hot section and one around the accessory gear box.

Gas expands due to heat and triggers a warning.

80
Q

Aerobatics tank capacity and duration

A

13L
23lbs
45s

81
Q

When will fuel booster pumps engage to correct a fuel imbalance?

A

> 55lbs

Will stop if >121lbs

82
Q

Where is fuel information displayed?

A
EMD
ENG page
SYS page
FUEL page
NAV page
83
Q

What does the main hydraulic system and servo system operate?

A
Main system:
Landing Gear
Flaps up and down
Air brake
Servo manifold
Servo Manifold:
Powered Ailerons
Roll Spoilers
Powered brakes
Anti skid
84
Q

Normal hyd pressure range and emergency hydraulic pressure range.

A

Normal:
1860 - 3390psi

Emergency:
2810 - 3740psi

85
Q

What are the different modes of braking?

A

Mode 3: Powered brakes and Anti-skid

Mode 2: Powered brakes

Mode 1: Manual Braking

86
Q

Locked wheel crossover

A

Operates above 25kts when a speed differential of 30% between wheels

87
Q

What speed does anti-skid disable?

A

10kts

88
Q

Normal operating limits of the autopilot?

A

20’ pitch
30’ roll

Maximum engagement attitudes:
50’ pitch
75’ roll

89
Q

When will the autopilot disconnect?

A
  • Either disconnect button is operated
  • Trim operated for 1 second
  • Stall tone sounds
  • Trim/Ail power off
  • greater than 50’ pitch 75’ roll
90
Q

Normal oil temperature range

A

10 - 105’

Allowed up to 10mins at 110’

91
Q

Normal oil pressure range?

A

90 - 125psi

92
Q

Manoeuvring speed for the rudder

A

220kts

Deflection decreases from full to 30% at 370

93
Q

Manoeuvring speed for elevator

A

220kts

Do not make abrupt control movements above this speed

94
Q

When do you contact tower on an RNAV?

A

Intermediate Approach Fix

95
Q

What is the sector entry saying?

A

One is big
Two is small
Threes the biggest of them all

96
Q

How to you do a sector one entry into a hold?

A

Overhead the fix fly outbound for 1/1.5 mins then turn into the hold to intercept the inbound course.

97
Q

How do you do a sector two entry?

A

You fly overhead the fix and into the hold using a 30’ offset for maximum 1.5 mins. Then turn to intercept the inbound track

98
Q

What speed do you fly the hold in the 21 for max endurance?

A

160KIAS clean

99
Q

How do you correct being late or early for a time one target?

A

The number of second you are late is your speed change in KTS and the planned speed for that leg in NM/min is the duration in mins.

12s early on a 240kt leg = 228kts for 4 mins

100
Q

What is the 1:60 rule?

A

1’ error = 1nm error over 60nm

Distance off track / distance to run

101
Q

What is the standard closing angle (SCA)?

A

SCA = 60/nmmin and you hold that for the number of mins you are nm out

3nm out 60/4 = 15’

Hold for 3 mins

Distance out / distance to intercept x 60 = angle

102
Q

How do you calculate drift?

A

Your crosswind component / TAS IN NMmin = drift correction

Clock code for the crosswind component

103
Q

When will the Overspeed Gear/Flap be indicates?

A

183KIAS

104
Q

During an auto start, if the PCL is more than 3’ FWD what will happen.

A

The automatic shutdown and dry run function is disabled and the pilot will have to initiate a shutdown if limits are exceeded

105
Q

Define CAVOK

A

Vis >10km
No significant weather
No TCU or CU
No cloud below 5000ft in 25nm or lowest sector altitude

106
Q

Warning associated with closing the canopy?

A
  • CFS striker plate is unobstructed
  • Visor down, mask on, glove on
  • no pers within 10m of blast area
107
Q

What is the Alternate minima?

A

More than SCT below HAT + 500ft
Vis below that on the chart
Fog/mist