AQP Flashcards
1
Q
Double Engine Failure CRJ200
A
Continuous Ignition: ON
Airspeed: Not less than 240 Knts
2
Q
Stabilizer trim runaway CRJ 200
A
Assume manual control and override runaway
Disconnect BOTH stab trim
Transfer controls to pilot left hand side
Pull circuit breaker 2F5 and 4A1
3
Q
Double engine failure CRJ 700/900
A
Continuous Ignition: On N2 less than 40%: Thrust levers shutoff ADG: Pull handle Stab Trim Channel 2: Confirm engaged Target Airspeed: Above FL340 .7 Mach Below FL340 240 kts
4
Q
Excessive asymmetry or loss of braking
A
Release Brakes momentarily
Anti Ski: off
Reapply brakes
5
Q
No light off
A
Affected thrust lever: shutoff
Ignition: off
Dry motor: Until starter time limit
6
Q
Start abort CRJ700
A
Affected thrust lever: shutoff
Dry motor: Until ITT below 120 C or starter time limit
Affected engine: stop
7
Q
First officer obligations during rejected takeoff
A
Monitor airplane deceleration status
Verify reverse thrust
Advise ATC
Checklists
8
Q
Obligations during evacuation
A
Assist PIC Checklists Tell Flight attendant Deplane with fire extinguisher and crash axe Keep passengers away at least 500 feet
9
Q
What is an NTSBO Briefing
A
Nature of emergency Time Signal: for evacuation deplaning Brace: if necessary BRACE BRACE BRACE Other
10
Q
When would it be necessary to Don O2 masks
A
Cabin Alt Warning
Smoke
11
Q
What do you say when on oxygen
A
Captain on o2 first officer on o2
12
Q
Max Takeoff Weight CRJ200
A
53,000
13
Q
Max TO Weight CRJ700
A
75,000
14
Q
Max TO Weight CRJ900
A
84,500
15
Q
Max Landing Weight CRJ200
A
47,000
16
Q
Max Landing Weight CRJ700
A
67,000
17
Q
Max Landing Weight CRJ900
A
75,100
18
Q
Max Operating altitude
A
37,000 feet
19
Q
Vlo ReT CRJ200/700/900
A
200 kts
20
Q
RVSM Mach speed CRJ200/700/900
A
.85/.83./.82
21
Q
Min spoiler speed CRJ200
A
App +20
22
Q
Min Spoiler Speed CRJ700/900
A
App plus 10
23
Q
What is approach speed definition
A
Flaps maneuvering or straight in
24
Q
Engine Start Duty Cycle CRJ200
A
60 10
60 10
60 5 minutes
60 5 minutes
25
Engine Start Duty Cycle CRJ700
```
90 10s
90 10s
90 5min
90 5min
90 5min
```
26
Dry Motor Cycle CRJ200
90s 5m off
| 30s 5m off
27
Dry Motor Cycle CRJ700/900
```
90s 5m
30s 5m
30s 5m
30s 5m
30s 5m
```
28
CRJ 200 Anti Ice for takeoff
OAT <=5
Visible moisture in any form including any precipitation, fog, mist, or clouds < 400 feet AGL; or
Runway is wet or contaminated
WINGS AND COWLS
29
CRJ 700/900 Anti Ice for Takeoff
* Visible moisture in any form (visibility ≤1 SM or any precipitation)
* The runway is contaminated:
30
When is reduced thrust prohibited
* Cowl and/or wing anti-ice are/is selected ON
* The runway is contaminated
* Tailwind components are in excess of 5 knots
* Windshear warnings are forecasted or reported
* Anti-skid is inoperative
* Takeoff behind a heavy or larger aircraft
* CRJ 200: Flaps 8 takeoff
31
What is the minimum thrust settings for 3A and 3B engines
3A1: 85
3B1: 83.5
32
What is emergency fuel
Thirty minutes remaining
33
What are the emergency fuel values 200/700/900
200: 1050
700: 1500
900: 1550
34
What defines minimum fuel
Landing with less than specified min fuel values. It provides go around fuel plus emergency fuel.
35
What are the min fuel values 200/700/900
200: 1500
700: 2100
900: 2150
36
Missed approach fuel burn
200: 450lbs
700: 600lbs
37
When is a new release required?
a) In the opinion of a dispatcher or PIC a new release is required.
b) A change in aircraft is made.
c) Before a flight departs an originating station after a delay of more
than two hours.
d) The flight is unable to depart in accordance with the release
previously issued by the dispatcher.
e) A flight returns to the airport from which it last departed.
f) A flight departs after making an unscheduled landing
38
How many static wicks
Right Wing STATIC DISCHARGERS (6 CRJ 200) (7 CRJ 700), (9 CRJ 900)
Tail STATIC DISCHARGERS (12 or 14 CRJ 200), (13 CRJ 700/900)
39
When is a cold weather preflight inspection necessary
* The OAT is ≤5ºC, or
* Atmospheric conditions conducive to icing exist, or
* The aircraft has remained overnight and may have been subject to contamination, or
* A through flight and residual ice from the inbound leg may have accumulated, or
* The wing fuel temperature is ≤0ºC
40
When can a terminating check be waved
• The outbound crew must be at the aircraft prior to the inbound crew commencing the
Terminating Checklist
• The aircraft must remain powered
• The outbound crew must perform an external preflight inspection
• The inbound crew is responsible for resolving all known discrepancies prior to leaving the
aircraft
41
How to do the cold wx preflight inspection
Visually inspect the critical surfaces and components for frozen
contaminants. In addition, inspect the wing area by running hand along
the leading edge and upper surface (or other location approved by the
PIC) to detect surface features. It must be assumed the surface is
contaminated if any surface features cannot be visually distinguished or
felt that would otherwise be apparent under non-icing conditions.
42
How much ice can be on the lower wing
Frost only up to 1/8th inch
43
What defines cold soaked
Wings containing very cold fuel and precip falls onto the airplane causing ice....airframe and bulk fuel at or below 0c
44
When the airplane is cold soaked how long must te engine be motored and checked for what
Before the first flight of the day, when the airplane is cold soaked, the engines must be motored
for 60 seconds and fan rotation verified before engine start is initiated.
The engines must remain at idle until oil pressure reaches normal operating range
After being cold soaked, the thrust reversers must be actuated until the deploy and stow cycles
are less than five seconds (CRJ 200) or two seconds (CRJ 700/900), prior to departure.
45
How is the pretakeoff contamination check completed
1) Visually inspect the representative surfaces for evidence of frozen contamination.
2) When the representative surfaces are free of frozen contaminants and takeoff will
occur within the HOT, the aircraft is considered clean and may takeoff.
3) Repeat the Deicing Procedure when:
a) The representative surfaces are not free of frozen contaminants, or
b) It cannot be determined that representative surfaces are free of frozen
contaminants, or
c) The fluid has failed, or
d) The HOT has been exceeded.
46
When is a pre-takeoff contamination check required?
When HOT exceeded or conditions changed or heavy snow 700/900 only
47
What are the critical surface areas
1) Wing leading edge, wing forward and rear upper surfaces (including winglets),
and associated flight controls
2) Horizontal stabilizer leading edge, forward and rear upper surfaces, and associated
flight controls
3) Vertical stabilizer and associated flight controls
4) Engine inlets
5) Critical areas that must be free of frozen contaminants are:
• Air data probes/sensors
• AOA vanes
• Antennas
• Fuel drains and NACA vent scoops
• APU intake/exhaust
• Landing gear
• Flight deck windshields and windows
48
What are the dashes on the Vmd table
Dashed lines on the Speed Cards VMD speed line do not provide a speed with
adequate bank protection for turns in excess of 15°. Bank angles in excess of 15° and holding
at these altitudes and weights are prohibited.
49
When does a HOT begin?
HOT begins when the final application of the deicing/anti-icing
fluid commences and expires when the deicing/anti-icing fluid loses its effectiveness,
e.g., when ice or snow begins to form on or in the fluid.
50
What defines moderate ice pellets
De Ice Card 0.11 inch to 0.30 inch per hour; more than 0.01 inch to 0.03 inch in 6 minutes.
51
During De Ice what elements need to be established?
Pre: ABC
Post: E
52
When has anti-ice failed?
A. A fluid is considered failed when it is no longer able to absorb frozen precipitation.
Under these circumstances, the assumption must be the contamination is adhering
to the critical surfaces.
B. Failed fluids can be difficult to recognize as a layer of clear ice may have formed under
the fluid, or ice crystals have formed in the fluid creating a surface roughness for takeoff
that can significantly degrade aircraft performance or controllability.
C. A failed fluid usually loses all its glossiness and resembles a dulled, crystalline
appearance. The ability to discern structural detail (rivets, screws, seams) through the
fluid is lost. While snowfall on a wing may be readily apparent, any clear ice that may
have formed underneath is not.
D. Accumulated snow on a wing on top of deice/anti-ice fluids means the fluid has failed
and will not blow off on the takeoff roll. Similarly, Type I fluid when used alone can
refreeze in a matter of a few minutes after the holdover time has expired under certain
precipitation conditions, especially freezing drizzle and freezing rain. Failed fluid takes
on the appearance of a dull rough coating of frost.
53
What do you do if the type 4 has failed
Do it again
54
What are the minimum runway lengths
1) The required minimum runway length for landing for all aircraft types
is 5,400 ft.
2) The minimum runway length for landing may be reduced to the following
lengths at SAAT Level 3 or lower airports, when that airport’s field
elevation is less than 4,000 ft:
a) CRJ 200 and ERJ 175: 5,000 ft
b) CRJ 700: 5,200 ft
55
What is the full maneuvering speed
Full maneuvering capability is available at V2+20 with the takeoff flap setting extended during
the initial climb.
Full maneuvering capability is available at VFTO with flaps retracted during the initial climb.
56
What altitude on a single engine departure procedure turn be established
No turns below 1000ft AFE unless otherwise specified
57
Simple special IMC no radar what altitude must be complied with
In IMC, if radar vectors are not available, comply with the special
procedure until 3,000’ AFE at which time you may proceed on course (as applicable).
Simple-Special Procedures, when required, are provided on the top of each page of
takeoff runway analysis.
58
Simple special VMC no radar what altitude
Simple-Special Procedures
| are mandatory in IMC. They are also mandatory in VMC until reaching 1,000' AFE
59
what defines a wet runway
A runway is wet when it is neither dry nor contaminated. For purposes of condition reporting
and airplane performance, a runway can be considered wet when more than 25 percent of
the runway surface area within the reported length and the width being used is covered by
any visible dampness or water that is 1/8 in (3 mm) or less in depth.
60
Wet Runway RCC value
5
61
Crosswind max 10 kts with what RCC values
a) NIL BA is reported.
b) RwyCC reports of 1 or 2 are reported with a crosswind component
greater than 10 kt.
c) BA reports of POOR are being reported with a crosswind component
greater than 10 kt.
d) Wet Ice, Water over Compacted Snow, or Dry Snow/Wet Snow over
Ice are reported with RwyCC values less than 1 or BA NIL.
62
Braking action or RCC value?
When there is a discrepancy between a PIREP and a RwyCC, the most
conservative estimation between the two shall be used.
