Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

Q400 Limitations > Q400 Limitations Encore > Flashcards

Q400 Limitations Encore Flashcards

1
Q

What is the minimum pavement width to turn 180°

A

85 feet
(84’5”)

AOM 2.2.14

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Encore Q400 one engine inoperative cruise distance in 60 minutes (zero wind)

A

276 NM

FOM 7.30.8

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

APU Starter limits

A

1 minute ON, 5 minutes OFF
1 minute ON, 30 minutes OFF, Maintenance action required before another start

AOM 2.3.10

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Encore takeoff emergency briefing

A 
CA: In the event of a rejected takeoff before V1, I will call reject and:
Select Disc and apply max braking
Stop the aircraft
Once stopped I will:
Set the emerg brake
Command the checklist 
Advise the flight attendants and passengers. 
FO: I will advise ATC, call 60 knots, standby to initiate the checklist as commanded
PF: In the event of an engine failure or fire after V1, I will continue the takeoff, rotate normally at Vr. 
PNF: I will call positive rate
PF: I will call gear up
Climb at V2 to flap retraction altitude
Call for the QRC at a safe altitude 
Retract the flaps on schedule 
Climb at Vclimb to 1500 feet
Call for the QRH reference items
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Min crew oxygen for takeoff

  • 2 crew
  • 3 crew
A

2 crew. 1050psi

3 crew. 1450 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Max ramp weight

A

65,400 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Max Takeoff weight MTOW

A

65,200 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Max landing weight

A

62,000 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Max zero fuel weight

A

58,000 lb

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Aft Cargo compartment # 1 and #2 total weight
max #1 weight (floor)
max #2 weight (shelf)

A 
Total = 2,800 lb
#1 floor = 2,800 lb
#2 shelf = 1,000 lb
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

maneuvering load

  • Flap retracted
  • Flap extended
A 
retracted = +2.5 g, -1.0g
extended = +2.0g, -0.0g
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Max lateral fuel imbalance

A

600 lbs

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Flap setting

  • Takeoff and initial climb
  • Cruise
  • Approach
  • Landing
A 
T/O = 5, 10, 15°
cruise = 0°
approach = 5, 10, 15°
Landing = 10, 15, 35°
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Max operating altitude
max altitude for takeoff/landing
Max alt w/ Gear and/or Flap extended
Max alt for air start

A

ops = 25,000 ft
t/o and landing = 10,000 ft
Gear/Flap = 15,000 ft
air start = 20,000 ft

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

max runway slope

A

+/- 2%

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Max tailwind

  • Takeoff flap 5
  • Takeoff flap 10/15
  • Landing flap 10/15
  • Landing flap 35
  • CAT II landing (flap 10 or 15 only)
A

10 knots, unless
Takeoff with flap 10/15 = 20 kt
Landing Flap 35 = 20 kt
for 20 knots:
-NWS is operative
-anti-skid is operative
-Flight spoilers operative in ground and flight modes
-bleed air is selected OFF prior to takeoff or landing
-Runways are not contaminated
-Takeoff are conducted with flap 10/15°
-NTOP takeoff power is used
-Takeoff is not conducted in icing conditions
-appropriate T/o performance provided on TLR
-appropriate ldng perf on TLR
-landings with flap 35, props set to 1020/max (RDC Np 850 rpm not approved)
- CAT II not authorized

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Ambient temperature limit - Flight and Ground

A

50°C or ISA +35°C, whichever is lower
minimum operating temperature is -54°C
Cold wx ramp servicing needed prior to start on ground when parked in excess of 3 hours in temps -15°C or lower

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Max crosswind component

  • Dry
  • CAT II - Canada
  • CAT II USA
A

32 knots
takeoff, landing or a hard dry or wet runway
wind gusts are included and shall not exceed the maximum
CAT II CAN = 18 knots
CAT II USA = 15 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Max headwind component CAT II landing

A

24 knots

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Minimum Runway width

A

98 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q 
Vmo
0-8000 ft
10,000
18,000
20,000
25,000
A 
0-8000 ft = 245 kt
10,000 = 282 knot
18,000 = 286 knot
20,000 = 275 knot
25,000 = 248 knot
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q 
Vfe
Flap 5
10
15
35
A

Flap 5 = 200 kt
10 = 181 kt
15 = 172 kt
35 = 158 kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Va

A

204 kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Vlo

A

200 kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Q

Vle

A

215 kt

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
26
Q

Vb rough air

A

210 kt

27
Q

Alternate gear extension speed or gear door malfunction

A

185 knot

28
Q

Max tire ground speed

A

182 knots

29
Q

MTOP time limit

A

10 minutes

30
Q

Transient engine exceedance time limit

A

20 seconds

31
Q

Min oil temperature for power above flight idle

A

0°C

32
Q

Min oil temp to ensure engine inlet ice protection on takeoff

A

55°C

33
Q

Min oil temp to ensure engine inlet ice protection in flight

A

within 3 minutes of setting takeoff power

65°C

34
Q

minimum oil temperature to unfeather a prop

A

-18°C

35
Q

Engine starter cranking limits

A

70 seconds ON, 2 minutes OFF,
70 seconds ON, 2 minutes OFF,
70 seconds ON, 30 minutes OFF

36
Q

Min SAT for re-light while airborne

A

-40°C

37
Q 
Reduced takeoff power prohibited if:
1
2
3
4
5
6
7
A
  • First flight of the day
  • tailwind exceeds 10 knots
  • contaminated runway
  • anti-skid inop
  • MTOP and uptrim disabled
  • known or suspected adverse wind, wind shear, or other that negatively affect climb path
  • landing gear will remain extended
38
Q

Takeoff power setting limitation

A

setting takeoff power prior to brake release with the nose of the airplane more than 45° out of wind is prohibited with wind speeds greater than 8 knots

39
Q 
Reduced Np Landings prohibited when:
1
2
3
4
5
A
  • tailwind exceeds 10 knots
  • anti-skid inop
  • CAT II approach is flown
  • Flight spoilers are in GND mode
  • Runway is contaminated
40
Q

Engine intake bypass doors open

MTOP and MCP are limited to:

A

Max ambient temp of ISA +25°C

41
Q

Takeoff with Bleed ON prohibited when:
1
2

A
  • operations conducted with maximum takeoff power and uptrim disabled
  • tailwind exceeds 10 knots
42
Q

Landing with Bleed ON is prohibited when:

A

Tailwind component exceeds 10 knots

43
Q

APU Limits (other than start):

  • Operational restrictions
  • Pax on board
  • Fuelling
  • Min temperature
  • Max temperature
  • APU louvres installed Max temperature
A
  • Ground operations only
  • Shut down prior to takeoff
  • Not operated unattended with passengers on board
  • Not operated during Gravity refuelling
  • Not operated below -54°C
  • When APU shutdown in OAT below -35°C for greater than 1 hour, it must be preheated prior to start
  • Not above +50°C or ISA +35°C, whichever is lower
  • Not above +21°C with APU Louvres installed
44
Q

Typical Fuel grade

A

JET A, JET A1

45
Q

Wide Cut Fuel grade

-Wide cut fuel grade restriction

A

JET B, JP-4
Dispatch with either of these wide cut fuels is prohibited with OAT or SAT warmer than -20°C
(with JET B or JP-4 if fuel TANK temp exceeds 35°C, max altitude is 20,000ft)

46
Q

Useable Fuel:

  • Each wing tank
  • Total
A

Each wing = 5862 lb

Total = 11724 lb

47
Q

Auxiliary Fuel Pump Limitation

A

Tank 1 and Tank 2 Aux fuel pumps, Must be on for takeoff and landing

48
Q

Fuel Heater

-Fuel temperature limits

A

Continuous inflight operation with fuel heater outlet temperature indication below 0°C or above 71°C prohibited

49
Q

Max Battery Load for Takeoff (Main, Aux and Stby)

A

0.1

50
Q

Minimum Battery Temp for Takeoff

A

-20°C

51
Q

Max altitude with Landing Gear and/or Flaps Extended

A

15,000 feet

52
Q
  • Normal Cabin Diff
  • Max Cabin Diff
  • Max Cabin Diff (taxi, takeoff, landing)
  • Max Cabin Altitude when pressurized
A

5.46 psi (+/- 0.1)
5.95 psi
0.5 psi
8,000 feet

53
Q

Wheel Brake Cooling Limits

  • Refer to Chapter 5 - Brake energy and Minimum Turn around time and QRH page 3-51, 52
  • (minimum turnaround time is)
A

10 minutes

QRH page 3-51, 3-52

54
Q

In order to hear radio/INT over flight deck speakers…

A

Both Pilot and Co-pilot HOT MIC switches must be OFF

55
Q

Integrated Standby (ISI) limit

A

a/c not operated further than 1 hour (60-mins) from suitable airport

56
Q

To ensure uninterrupted operation of PFD, MFD, ED, the electrical power must be cycled OFF, then ON every…

A

24 hours/every flying day

57
Q

Icing conditions definition:

  • On Ground
  • Airborne
A

On Ground:
Icing conditions exist when the SAT on the ground and for takeoff is 10°C or below, or the SAT in flight is 5°C or below and visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet or ice crystals). Ice accretion on aerodynamic surfaces is not considered to exist at temperatures of -40°C or below

Icing conditions also exist when the SAT on the ground and for takeoff is 10°C or below when operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on the engines, nacelles, or engine sensor probes

Note: Icing conditions are considered to exist at takeoff where visible moisture (cloud ceiling) is present at 1,000’ AGL or below at a SAT of 5°C or less

58
Q

Engine Intake Bypass Doors:

  • Icing requirement
  • MTOP/MCP limit with bypass doors open
A
  • Must be open in icing conditions

- With bypass doors open, MTOP and MCP are limited to Max ambient temperature of ISA +25°C

59
Q

Airframe Deice boots must be activated when…

A
  • First sign Ice is detected on any part of the aircraft - Set FAST (or SLOW)
  • Must run for a minimum of 2 boot cycles after leaving icing conditions
60
Q

AFCS - Autopilot Limits:

Minimum Disengagement height:

  - Landing Flap 0°
  - Landing Flap 5, 10 and 15°
  - Landing Flap 35°
  - CAT II
  - Engine Failure - Icing/turbulence restriction - Minimum engagement height after takeoff
A

Flap 0 - minimum altitude 1,000’ AGL
Flap 5, 10, 15 - 200 feet or 100’ AGL if CAT 2
Flap 35 - can be used to 200’ AGL, Not authorized for CAT 2
CAT II - 100’ AGL
Engine Failure - Disengage AP and re-engage following trimming; Disengage by 1,000’ AGL on landing
Icing/Turbulence- Must be disengaged in severe icing or severe turbulence
Height after t/o - 1000’ AGL to engage AP

61
Q

VNAV Vertical Path Angle limit:

  • Enroute/terminal
  • Approach
A 
Enroute/terminal = 6°
Approach = 4°
63
Q

Forward cargo compartment weight limit

A

910 lbs

64
Q

Wardrobe weight limit

A

160 lbs

65
Q

Takeoff and/or landing with tailwinds between 10-20 knots may be conducted provided:

12 things

A
  • Nosewheel steering is operative
  • Antiskid operative
  • Flight spoilers operative in ground mode
  • Bleed air is OFF for takeoff and landing
  • Runways are not contaminated
  • Takeoff conducted with Flap 10 or 15
  • NTOP Takeoff power used
  • Takeoff not conducted in icing conditions
  • Appropriate takeoff performance in TLR
  • Appropriate landing performance in TLR
  • Landings with Flap 35, 1020 NP
  • CAT II not authorized

Q400 Limitations (1 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions