Tech Questions Flashcards
Cat B speeds?
Circling area?
Vat 91-120 IAF 120-180 FAF 85-130 circling 135 Missed approach 150 Reversal procedure 140kts
2.66NM (300ft obst. clearance)
Cat C speeds?
Circling area?
Vat 121-140 IAF 160-240 FAF 115-160 Circling 180 missed approach 240 4.2NM (400ft obst. clearance)
Speed and time limitations on holding
Below FL140 230IAS (170kts CAT A&B) (1min hold)
FL140 - FL200 240IAS (1.5min hold)
Above FL200 265IAS
Above the highest MSA in turbulence and with ATC permission the lesser or 280kts or M0.8
Qualifying aircraft requirements to use reduced take off minima?
What are the take off minima?
Not qualifying?
limitations to the take-off requirements?
Chapter 15 Part 91 MOS
Qualifying multi-engine aeroplane means an IFR aeroplane that is:
(a) either:
(i) a multi-engine jet-powered aeroplane with an MTOW of more than 2 722 kg;
or
(ii) a multi-engine turboprop-powered aeroplane with an MTOW of more than
5 700 kg that is:
(A) operated by at least 2 pilots; or
(B) operated by 1 pilot and fitted with operative auto-feather; and
(b) in the event of an engine failure — capable of maintaining terrain clearance until
reaching the minimum height for IFR flight.
Able to meet climb gradient requirements
min 800m vis
or 550m if edge lighting is Max 60m intervals and centreline lighting or markings. If no ATC, must be day and at an airport that requires radios
The take-off minima mentioned in this section apply to a take-off that:
(a) is not a low-visibility take-off; and
(b) is not conducted using a qualifying multi-engine aeroplane.
(2) The take-off minima are:
(a) a cloud ceiling of 300 ft; and
(b) visibility of 2 000 m.
A pilot in command must not commence a take-off if, at the time of take-off:
(a) the meteorological conditions are less than the take-off minima for the aircraft; or
(b) the meteorological conditions that would exist if it were necessary to return to
land at the departure aerodrome because of engine failure, are not:
(i) at or above the landing minima for any IAP that the pilot in command is able
to conduct at the aerodrome; or
(ii) such as to allow a visual approach for the return to land.
What are the minima and requirements for approaches?
NPA
and
PA
Part 91 MOS
15.09
Landing minima requirements
(1) Landing minima obtained from an instrument approach chart must be selected in
accordance with:
(a) the specified aircraft performance category; and
(b) aircraft LNAV and VNAV capabilities.
(2) Landing minima must meet the requirements of section 15.10.
Selected minima must never be blow the chart value, AFM or company document(exposition/ops-manual)
15.10
Precision Approach Procedure:
800 m — (ii) the approach lighting system normally available beyond 420 m from the runway threshold is inoperative;
runway threshold is inoperative;
1 200 m — (iv) the approach lighting system normally available beyond 210 m from the runway threshold is inoperative;
1 500 m — but only if the approach lighting system normally available for the
runway is inoperative;
1.5x times either the RVR or the visibility specified on the instrument approach
chart for the IAP being conducted — but only if:
(i) a lighting failure has occurred on a runway at a controlled aerodrome; and
(ii) doubled spacing of runway edge lights results.
What is the missed approach climb gradient?
2.5%
provides min 100ft clearance
When can we use the 0.8km visibility criteria?
Minima for cat 1 can be used except
1.5km required if HIAL NA
1.2KM required unless:
Aircraft manually flown with FD to DA or with AP to DA coupled to LOC and GS or GLS
Aircraft has warning system for primary attitude and heading reference system failure
High intensity runway edge lighting available
800m required If RVR information in threshold NA
How would we determine this visibility is present?
+
Using the attached ILS chart please brief me the approach as if conducting a multi crew
operation?
-
What engines are fitted to the aircraft we operate?
Prat and Whitney Canada PW100 Series
Describe the emergency decent procedure on your aircraft?
Flap up
Gear down
power as required (idle)
Nose down 20degrees
Which ports do we operate to?
14 domestic major cities
40 regional cities
Sydney and Melbourne hub ports (Eastern)
Sun state - Brisbane, Cairns and Adelaide (southern)
What is the voltage of the electrical system on your current aircraft?
28V system
with a 24V battery and a
28V 70amp alternator
What engines are fitted to the Dash 8 200/300/400?
How many seats
Q200 -PW123C 36seats
Q300 -PW123E 50seats
Q400 -PW150A 74seats
Describe the air con system in the aircraft you fly?
Direct Ram air.
Heating system.
- Cold air flows into the shroud through the front stub pipe. The cold air goes around the muffler and gets
hot. The hot air then flows out through the rear stub-pipe and into the cabin heating system. - When either heating lever is moved to on, it closes the bypass valve and the hot air moves through the wing into the cabin.