Quiz Flashcards

(65 cards)

1
Q

How do you carry out a Manual Start?

A

MANUAL start:

1) PMS set to MANUAL.
2) Booster pumps ON and moves the STARTER switch to MAN.
3) When the oil P rises the ignition is set to IGN.
4) Move the throttle slowly forward until the ITT increases. As the ITT peak moves the throttle slowly to idle.
5) When the engine reach idle (Ng (67% ± 7%), with the throttle above the idle stop, the pilot must return the starter, ignition and fuel pump switches to AUTO.

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2
Q

What is a Manual Start?

A

MANUAL START - Throttle manually controls the rate of increase of fuel flow to the engine and therefore the rate of rise of the ITT. If the throttle is moved forward too quickly, the ITT could exceed limits or the engine could surge. Shut-down the engine if the ITT fails to rise (no light up), exceeds limits or if the Ng stabilizes below idle.

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3
Q

Why 2 peaks on ITT?

A

First peak is to test the integrity of the FCMC, while the second peak is the actual ITT of the aircraft.

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4
Q

How do you know where your fire is occurring when the captions on the DWP and MFD appears?

A
  • White smoke (electrical fire)

- Black smoke (fire caused by fuel)

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5
Q

How does the Fire Alert System work?

A

If there is a fire or overheat in the engine compartment, red FIRE warnings are given in both cockpits on the DWP and MFD. A fire around the engine expands the gas in the fire detector element. The gas pressure increases and operates a switch in the detector to complete a circuit and operates the fire detection relay.

2 gas-filled tube to sense temperature attached to outercase of enginem, powered by BATT BUS

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6
Q

Where the are the FIRE OVERHEAT DETECTORS found?

A
  • No.1 found in the hot section of gas generator case.
  • No.2 found in accessory gearbox

Red FIRE warning captions are shown on the front and rear DWP and MFD.
Grey FIRE 1 ALRT/FIRE 2 ALRT captions on MFD.

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7
Q

What is the oil T and Ps green, amber and red range in right MFD and what are the indications?

A
TEMPERATURE  
Green  
- Oil temperature from 10 to 105 degrees 
Amber  
“OIL TEMP” cap on MFD 
− Oil temperature > 105 °C (221 °F 
− Oil temperature < 10 °C (50 °F). 
Red  
“OIL TEMP” cap on MFD 
− Oil temperature > 110 °C (230 °F) 
− Oil temperature < -40 °C (-40 °F) 
− Oil temperature > 105 °C (221 °F) for longer than 10 minutes. 

PRESSURE
Green - 90 to 125 psi
Amber
“OIL PRESS” cap on MFD
− Oil pressure < 6,21 bar (90 psi) for longer than 10s with engine Ng >= 72%
− Oil pressure < 4,83 bar (70 psi) for longer than 10s
− Oil pressure > 8,62 bar (125 psi) for longer than 55s
− Oil pressure > 8,96 bar (130 psi)
Red
“OIL PRESS” cap on MFD
“OIL” cap on DWP
− Oil pressure < 4,83 bar (70 psi) for longer than 20s
− Oil pressure > 8,96 bar (130 psi) for longer than 20s
− Oil pressure > 13,72 bar (199 psi)

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8
Q

What are the PMS manual captions?

A

PMS MANUAL on MFD Alerts and ENG page
PMS (red) DWP
PMS caption on the DWP

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9
Q

Definition of chicken fuel.

A

‘Chicken Fuel’ is the minimum fuel computed from the furthest point of the navigation route, where the aircrew must initiate the chicken fuel recovery profile when it is assessed that he/she will go below ‘Chicken Fuel’ before reaching the furthest point.
(SOP 8-1 – Navigation)

Chicken fuel is calculated from the furthest point directly back to Pearce.
(SSG Chapter 25 – MEDIUM LEVEL NAVIGATION 4.1.3 Pg 5)

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10
Q

Number of propellers blades on the PC21.

A

Five-bladed, variable pitch, feathering, constant speed.

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11
Q

Definition of Min Power and Min Practicable Power.

A

Minimum Power: Power setting to maintain 140 – 160 kts (25%-35% TQ) after the initial CAPS/FRC actions.

Minimum Practicable Power: Power setting to reduce to stabilise the nature of the engine problem. If the affected system returns to within ops limits at a particular setting, that power setting should be used for recovery.

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12
Q

What is the sequence of landing gear retract and extension?

A

Retract: Right >Left> Nose
Extend: Nose> Left > right

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13
Q

Where is the WOW switch located on the aircraft?

A

Main landing gear and nose landing gear itself. Total 3 WOW switches.

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14
Q

Why does the nose wheel have more pressure than the Main wheels?

A

Nose wheel to support the weight of the engine,

Main wheels to absorb the impact on landing

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15
Q

Why does the SKID DWP caption goes out when GPU connected?

A

The GPU supplies power to the BATT BUS, which supplies power to the TRIM/AIL PWR switch.

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16
Q

How long for the flaps to come down?

A

UP to T/O: 4-5sec

T/O to LDG: 4-5sec

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17
Q

How long for gears to come down?

A

Gears extension: 5 sec

retraction: 4 sec

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18
Q

How long for Airbrakes to come down?

A

Airbrake retract/extend: 2 sec

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19
Q

What are the angle ranges for rudder & elevator trim?

A

Elevator trim max deflection: 3.5 nose up and -7.5 nose down
Rudder trim: -4 nose left, +19(?) nose right

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20
Q

What are the trim timing limits?

A

Yaw trim timing limits: minimum 19s, max 23s

Roll trim timing limits: min 17s, max 21s

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21
Q

What is the trim offset on the rudder when the aircraft is on the ground? (sect 9.25)

A

When in the on-ground mode the TAD sets the rudder trim to the fixed take-off position of 7.5° nose right

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22
Q

Purpose of winglets on the PC21.

A

Reduces wingtip vortices, reducing induced drag.

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23
Q

How many circuit breakers are in the front cockpit and what are they?

A
  1. PFD front, IRS primary power
    SFD front, Air intake
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24
Q

Which page on FMS can check the validity? And what are the messages.

A

The ident page.
VOR DME NAV LOST
DME DME NAV LOST
DME CTRL 1 LOST

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25
Why do we set 40-50% power setting on brakes during Power Checks? sect 9.12(canopy)
Holding brakes and selecting 40% TQ ensures: - Normal engine indications and safety pin positions are checked and correct. -CAPS come on at 38% - Provides rapid engine acceleration to MAX power - To ease directional control after brake release. (Section 8 - Operational tips PG.10)
26
Length of MDC chord and how do you activate the external CFS Handle?
15ft/ 4.572m Move the fluorescent cover to reveal the release button. Push the button to release the handle Pull the handle away from the a/c
27
Why instructor max crosswind is limit by 24kts?
AFM (Section 4 Part 2: Normal Procedures airspeed limitations) State that MAX demonstrated crosswind component = 24kts Value recommended by Pilatus Effects of crosswind speeds beyond 24kts on airframe unknown, hence use safe recommended limit set by Pilatus
28
How many ways are there to release the leg restraints?
Two ways 1)The quick release catch 2)crocodile clips We do not use the quick release during strap-out as the leg restraints may get stuck.(difficult to reattach quick release catch)
29
Why BATT more than 23.6V @ startup?
If BATT 1 voltage is below 23.6, BATT 1 should be recharged before attempting engine start. If engine starts at low BATT 1 voltage, the BATT BUS voltage may drop below the level required to keep the avionics that it supports online.
30
What are the X and Y channels on TACAN UFCP?
X channel when you're looking at ground based NAV aids. Military uses the Y freqs a lot for formation distance info. Set two channels 63 apart and you can pick up a distance from each other (29 & 92). Source: google (???)
31
When do we do FIRHAD checks?
From Pearce training area, FIRHAD checks are to be completed before leaving the training area. Areas other than PTA, FIRHAD checks are to be completed prior to joining airfield.
32
What is the button to switch the navigation origin on left MFD to GPS from hybrid?
NAV SOURCE. | Under the MSN>STS page
33
Definition of ASOR?
Air Safety Occurrence Report
34
Transition height and layer for Australia?
10000ft and 11000ft respectively
35
Why is the nose cone tilted?
The nose cone (therefore the engine is tilted) is tilted due to the tilting of the engine which is offset to counter torque effect to keep the trim changes minimum during flight. The angles are 3.5 degrees nose right and 4 degrees nose down.
36
What is the taxiing speed?
Less than 10 knots in apron 15 knots in echo 20 knots for the rest of taxiways
37
The pc 21 d link only allows you to see pc21 a/c and civil a/c. Why?
Hawks and PC9 do not have advanced avionics with the ADS- B. (automatic dependence surveillance broadcast)
38
Transient definition?
Transient a period where the condition of the a/c exist for a short period of time. 20s according to AFM. (oil press)
39
How to calculate total wave height for flying over water?(16/3) Due to effectiveness for S&R operations SO B-4
Square root[ (sea state)^2 x (swell height^2) ] In oceanography, a sea state is the general condition of the free surface on a large body of water – with respect to wind waves and swell – at a certain location and moment. The swell height we give is an average of the largest 1/3rd of all waves. Something very much like the average set wave. It's measured from the trough (very lowest point) to peak (very highest point) of each wave.
40
Second Mandatory Go- Around criteria word for word?
More than 45o AOB (Trainees) / 60o AOB (instructors) required on base turn.
41
What are Restricted + Prohibited + Danger Area?
Prohibited area: No flights allowed. Flight within a prohibited area is not allowed. Restricted Area: Airspace is restricted in accordance with specified time. Pilots desiring to enter must request from ATC clearance to enter. When clearance is granted, pilot must abide by all rules. Danger Area: Airspace within which dangerous activities to a/c may exist at specified times. Approval of flight within a danger area outside controlled airspace is not required. ``` RECAP Examples of Restricted airspace. R178 R134 A/B/C/D R146 A/B/C R184 R153, 155, 156 ``` Danger areas D197 D193 (outer low flying area)
42
What is the time the engine shuts down when the fuel hyd cut off is pulled?
10-11s from 50% TQ | 16-17s from IDLE ~
43
What is the braking distance of PC21 and the rolling distance?
Rolling: 2000ft | Braking dist: 3000ft (SSG)
44
Max surface winds for PC-21?
When reported surface is 30kts or greater, wind gust 35kts or greater, flying operations will cease.
45
What are the types of Restricted Areas?
``` West Australian Exercise Airspace (WAXA) Bindoon Army Range Muchea Air Weapons Range Lancelin Weapons Range (SI-OPS 3-2 – Pg 1) ```
46
What is Gnagara Release?
GNANGARA RELEASE (From SI OPS 3-1) Purpose: facilitate VFR a/c positioning for visual approach to RWY 36 Restrictions: SFC – A010 (can request till A015) Position: Portion of Perth civil airspace to north of Gnangara road. West of west swan road and the great northern highway. Notes: remain 1.5nm clear of Gnangara release southern boundary
47
Definition of BINGO and JOKER fuel word for word?
“Bingo” Fuel is the fuel state at which the mission in the area will be terminated and will allow for a normal recovery via low level at 200 KIAS to land before reaching minimum fuel. “Joker” Fuel is a fuel state nominated by QFI or Formation Leader to assist in sortie management. (SOP 2-15 – General Flying)
48
Emergency and Minimum fuel quantity and what do these values mean.
Emergency Fuel - 110 lbs at FAF / IP Allows 1 missed approach and land visually at the same airfield before reaching aircraft minimum safe operating fuel state (50lbs). Minimum Fuel - 230 lbs at FAF / IP Allows 1 missed approach and divert to land before reaching emergency fuel. Sufficient for either VRIAP to Gingin or Radar Vectors for INST APP finals to Perth. (SOP 2-15 – General Flying) One Circuit Fuel- 60lbs The minimum planned fuel is 230 lbs at FAF/IP, which allows for one missed approach and divert to land before reaching emergency fuel. Sufficient for either VRIAP to Gingin or Radar Vectors for INST APP finals to Perth (SOP 8-1 - Navigation) The minimum fuel at the IP/FAF is 230 lbs (add 100 lbs for solo). (SSG Chapter 25 – MEDIUM LEVEL NAVIGATION 4.1.3 Pg 5 )
49
What is WANNAMAL Lane? (08/02)
The Wannamal Lane is centered on the 356 radial, and extends between the 354 and 358 radials, from 15-45 TAC. Vertical limits are A050-A120. Operations in PTAs B or C normally route via the Wannamal Lane. Position ‘Northgate’ is situated at 15 TAC in the Wannamal Lane. (SI-OPS 3-1 – Pg 5)
50
What is a CIRA? What is PEA/GIN CIRA?
Circuit Area (CIRA) Pearce and Gingin CIRAs are from surface to 3,500ft AMSL. (SO B11-1)
51
What is Merlo Release?
The Merlo Release is civil airspace that is released to Pearce when Perth is operating on RWY 03 or 06 (northeast plan). The Merlo Release comprises civil airspace above R153 A and B, and that portion of the PTH TMA within 9 TAC, SFC-A040. When Pearce is operating to RWY 36, the Merlo Release facilitates instrument approaches on the 7 TAC arc, and positioning for visual approach via initial. When Perth is operating on RWY 21 or 24 (southwest plan) the Merlo release is not available, and instrument approaches to RWY 36 will be denied or delayed. The Pearce ATIS will then include the phrase ‘Merlo Release not available.’ Under such circumstances the Gnangara Release is still available. Perth VOR (PTH) Terminal Control Area (TMA) (SI-OPS 3-4 – Pg 4
52
Flexible descent purpose?
Flexible descent – Speed, power and airbrake as required. You must plan for a proper descend from FL150 to 8000/7000ft as required. You must achieve the required altitude before you reach the Class C/E airspace boundary. Use 240KIAS for all descends. If it appears that you will not achieve the required height by the airspace boundary use a flexible descend. (SSG Chapter 25 – MEDIUM LEVEL NAVIGATION 6.7 Pg 12 )
53
What is the value of the pressure when the EO2 gauge is in the "green"?
EO2 psi is roughly charged to 1800 psi In between the green zone. Not too high psi to cater for gas expansion and not too low to maintain the green section.
54
Average area elevation?
Our area elevation is roughly 2000ft AGL.
55
LEARNING POINT 1
All DXOs, except Mr Leng(DANGLE), are not 8G cleared. Training G limit:7G If 7G is exceeded, sortie can be continued provided all occupants are 8G qualified. If limit is exceeded for a 2nd time, terminate sortie and RTB. SXO informed.
56
LEARNING POINT 2
If the propeller has not started you can walk near the red line.
57
What is the firing sequence for the ejection seat? Why is it designed this way?
Ejection seat: Front seat will go left and the rear seat will go right due to the underseat rocket motor. The front will go after the back to minimize risk of inadvertent collision during ejection due to the forward motion of the aircraft the air resistance may cause the front to be in the path of the back ejector if the front ejects first.
58
LEARNING POINT 3
Note for temperature limitations in standing orders. All values are greater than or equals to. E.g. 36 degrees and more. No a/c change/no first solo flight
59
How many descent profiles are there? What are they?
``` 5 types of descent profiles. 1. Flexible 2. Normal descent 3. Glide descent 4. Rapid descent 5. Instrument descent > above 5000ft, fast rate of descent conducted at 200kts, AB out, 25%TQ >below 5000ft, slow rate of descent, 170KTS, AB out, 25% TQ ```
60
LEARNING POINT 4
Sims be careful of the mon VHF and UHF. Comm1 shd be VHF and comm2 on UHF
61
LEARNING POINT 5
EO2 position. Down means inactivate/not pulled. Up means activated/pulled. Use your left hand to pull up during your caps & checks.
62
What is the formula for load factor?
Load Factor: 1/cosAOB
63
LEARNING POINT 6
``` For kneeboard cards, please note that R134 heights are wrong. The correct heights are as followed 143 alpha: SFC – A050 143 bravo: SFC – A090 143 charlie: SFC- A040 143 delta : A040 – A090 ```
64
LEARNING POINT 7
During throttle off movement especially for the caps, remember to simulate pressing down the detent switch. Before moving throttle from idle to off
65
LEARNING POINT 8
During your Engine fire on the ground. The egress action to show your instructor is to simulate turning the QRF. (recap: 15 degrees will allow you to connect your straps. And turning through 30 degrees will quick release)