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At what stage of a flight should you change from area QNH to local QNH (if available) when descending from A075?
When is the pilot in command required to inspect and test the aircraft’s fuel system for the presence of water?
You are departing a controlled aerodrome where the Enroute Supplement indicates, “”Voice AVBL on NDB for EMERG transmissions””. If you experience communications failure, one of the actions required is that you?
Sometimes, airports will broadcast their ATIS via the NDB frequency (e.g. moorabbin). They can also transmit other broadcasts to aircraft that have suffered radio failures.
Sometimes, airports will broadcast their ATIS via the NDB frequency (e.g. moorabbin). They can also transmit other broadcasts to aircraft that have suffered radio failures.
The overwater segment of a flight in a single-engine aircraft is just beyond gliding distance from land. Which of the following items must be carried on board the aircraft?
Given: W/V = 250M/30. Runways available are 03/21 and 09/27. Which runway has the greatest headwind component for landing?
The beginning of daylight in UTC at FORREST WA (3050S 12807E) on the 7th February is closest to?
ARC to time = 0832
LMT = 0508
0508 – 0832 = 062036Z
Therefore, the answer of 062034 is closest.
ARC to time = 0832
LMT = 0508
0508 – 0832 = 062036Z
Therefore, the answer of 062034 is closest.
Given:
Forecast W/V = 150/45,
TR(T) = 080 Deg,
Variation = 10ºE,
TAS = 145 kts
Determine the approximate HDG(M) and GS.
Both winds are given in true.
On the back of the whizz wheel, place the wind on 150 and mark 45 kts.
Now place the track of 080 at the top.
This reads about 42 kts crosswind and 15 kts headwind.
Place the TAS arrow on 145 kts.
Next, read that 42 kts XW gives 17 degrees of drift.
17 degrees of left drift means you must steer 097 TRUE (087 magnetic).
You must account for E-TAS.
Read 17 degrees off the left of the TAS arrow to get an E-TAS of 139 kts.
Subtract 15kts to get a ground speed of 124 kts.
Both winds are given in true.
On the back of the whizz wheel, place the wind on 150 and mark 45 kts.
Now place the track of 080 at the top.
This reads about 42 kts crosswind and 15 kts headwind.
Place the TAS arrow on 145 kts.
Next, read that 42 kts XW gives 17 degrees of drift.
17 degrees of left drift means you must steer 097 TRUE (087 magnetic).
You must account for E-TAS.
Read 17 degrees off the left of the TAS arrow to get an E-TAS of 139 kts.
Subtract 15kts to get a ground speed of 124 kts.
You plan to fly from NARRABRI (YNBR) (3019S 14950E) direct to ST GEORGE (YSGE) (2803S 14836E). To avoid clouds after departing YNBR you divert left of planned TR along the YNBR – WALGETT railway line. At WEE WAA township (approximately 20nm WNW YNBR) you decide to track direct to YSGE. Which of the following features would provide the most accurate ground speed check between WEE WAA and YSGE?
Rose Hill is too early, and Moonie River is too late for a reasonable check; Moree is too far.
Rose Hill is too early, and Moonie River is too late for a reasonable check; Moree is too far.
The following details pertain to a direct flight from BATHURST (YBTH) (3325S 14939E) to DUBBO (YSDU) (3213S 14834E):
ATD YBTH at 2305 UTC, 2317 UTC over HILL END town (approximately 25nm from YBTH).
Using this data the estimate for YSDU is closest to?
When no specific instructions are available, which of the following would be the correct fuel/air mixture setting for take-off at a high density altitude aerodrome? The mixture should be?
On a colour-coded ASI, the maximum landing gear operating speed (VLO) is:
The white arc indicates the speeds at which flap operation is safe. The red radial line is Vne (never exceed). The blue line indicates the best rate of climb speed during single engine operations.
The white arc indicates the speeds at which flap operation is safe. The red radial line is Vne (never exceed). The blue line indicates the best rate of climb speed during single engine operations.
An increase in headwind component, while gliding at the recommended best gliding speed, would result in?
A headwind means that the aircraft’s groundspeed will be slower when compared to no wind. This means it will travel less distance until it reaches the ground.
A headwind means that the aircraft’s groundspeed will be slower when compared to no wind. This means it will travel less distance until it reaches the ground.
Which of the following is a likely reason for a yaw to the right during the take-off roll in a single-engine aeroplane fitted with an engine which rotates in a clockwise direction when view from the cockpit?
Gyroscopic effect, slipstream effect and torque reaction all cause a yawing moment to the left. CASA love this question.
Gyroscopic effect, slipstream effect and torque reaction all cause a yawing moment to the left. CASA love this question.
At which speed (IAS) should a piston-engine aeroplane be flown to achieve maximum endurance in level flight?
This is not the stall speed. The speed for best endurance is a speed that requires minimum power. Below this speed, the increase in induced drag becomes a lot greater and so a lot more power is required. Below the best endurance speed is known as the “region of reverse command.”
This is not the stall speed. The speed for best endurance is a speed that requires minimum power. Below this speed, the increase in induced drag becomes a lot greater and so a lot more power is required. Below the best endurance speed is known as the “region of reverse command.”
The cloud type most likely to be associated with heavy continuous rain is:
These are grey and are often a dark cloud layer. The base is hard to distinguish due to continuously falling rain or snow.
These are grey and are often a dark cloud layer. The base is hard to distinguish due to continuously falling rain or snow.
An approaching fast moving cold front may sometimes be recognised by the accompanying:
This is fast moving low cloud and severe turbulence and low cloud right along the front.
This is fast moving low cloud and severe turbulence and low cloud right along the front.
1.3.4.2(a)(i)
“An aircraft with a maximum seating capacity of 6 is to be refueled. Under which (of the following) conditions are ambulatory passengers permitted to remain on board?”
Note I believe this is an old superseded question – however it may still be in there. Under the original CAO 20.9 there used to be a clause stating 20 pax as follows, and thus the answer would have been “under no circumstances”. However, this clause has been removed.
However there are exemptions to this rule:
The answer is in CAO 20.9 & VFRG General > Pilot responsibilities > Refuelling
From CAO 20.9
The VFRG States:
For refuelling see: ADVISORY CIRCULAR AC 91-25v1.0 Fuel and oil safety November 2021
For Flight Operations Regulations commencing on 2 December 2021
CASR 91.470 – Fire Hazards, 91.485 Equipment or electronic devices operating near aircraft, 91.055 Aircraft not to be operated in manner that creates a hazard
For refuelling see: ADVISORY CIRCULAR AC 91-25v1.0 Fuel and oil safety November 2021
For Flight Operations Regulations commencing on 2 December 2021
CASR 91.470 – Fire Hazards, 91.485 Equipment or electronic devices operating near aircraft, 91.055 Aircraft not to be operated in manner that creates a hazard
Calculate the approximate density altitude using the following.
Elevation 3000 FT
QNH 1013
Temp 20ºC
1. Find pressure height = Elevation + (1013-QNH) x 30 e.g. 3000ft at QNH 1013, = 3000+ (1013-1013) x 30 = 3000+ 0 = 3000 ft
2. For the next part of the calculation ONLY, round pressure height to nearest 500ft
3. Find ISA temp = temp – 2 x the thousands of feet (at the PH) e.g. 20 C at 3000= 15 – 2 * 3 = 9
4. Take ISA temp away from OAT e.g. 20°C to get ISA deviation = 20° – 9° = 11° ISA dev
5. Multiply ISA deviation by 120 to get pressure correction height e.g. 120 x 11 = 1320 ft
6. Add elevation to pressure correction height to get density altitude e.g. 3000ft + 1320 ft = 4320 ft
1. Find pressure height = Elevation + (1013-QNH) x 30 e.g. 3000ft at QNH 1013, = 3000+ (1013-1013) x 30 = 3000+ 0 = 3000 ft
2. For the next part of the calculation ONLY, round pressure height to nearest 500ft
3. Find ISA temp = temp – 2 x the thousands of feet (at the PH) e.g. 20 C at 3000= 15 – 2 * 3 = 9
4. Take ISA temp away from OAT e.g. 20°C to get ISA deviation = 20° – 9° = 11° ISA dev
5. Multiply ISA deviation by 120 to get pressure correction height e.g. 120 x 11 = 1320 ft
6. Add elevation to pressure correction height to get density altitude e.g. 3000ft + 1320 ft = 4320 ft
1. Find pressure height = Elevation + (1013-QNH) x 30
2. Round pressure height to nearest 500ft
3. Find ISA temp = temp – 2 x the thousands of feet eg 26C at 2000 = 26 – 2 * 2 = 22
4. Take ISA temp away from OAT to get ISA deviation
5. Multiply ISA deviation by 120 to get pressure correction height
6. Add elevation to pressure correction height for to get density altitude
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