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Boxed Limitations Flashcards

AOM Vol I Chapter 2

1
Q

Maximum Operating Altitude

A

41,000’

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2
Q

Maximum Altitude Takeoff and Landing

A

8,000’

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3
Q

Minimum Altitude Takeoff and Landing

A

-1,000’

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4
Q

Maximum Allowable Load Factors,
Flaps up
Flaps down

A

2.5g to -1.0g

+2g to 0g

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5
Q

Maximum runway slope

A

+/- 2%

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6
Q

Approved Runway Surface

A

Paved

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7
Q

Maximum Tailwind Takeoff and Landing

A

10 knots

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8
Q

Maximum crosswind for takeoff and landing

Dry Runway

A

28 knots sustained, with gusts to 38

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9
Q

Maximum crosswind for takeoff and landing

Wet runway

A

28 knots

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10
Q

Maximum crosswind for takeoff and landing

Compacted Snow

A

20 knots

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11
Q

Maximum crosswind for takeoff and landing

Standing Water/slush/Wet Snow/Dry snow

A

18 knots

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12
Q

Maximum crosswind for takeoff and landing

Runway with Ice (including wet ice)

A

12 Knots

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13
Q

Why is there a Maximum crosswind for static takeoff of 30 knots

A

possibility of compressor stall

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14
Q

Maximum wind limits for CAT II approach

Headwind

A

25 knots

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15
Q

Maximum wind limits for CAT II approach

Tailwind

A

10 knots

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16
Q

Maximum wind limits for CAT II approach

Crosswind

A

12 Knots

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17
Q

Maximum temperature for takeoff and landing

A

ISA +35C

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18
Q

Minimum temperature for takeoff

A

-40C (a maintenance inspection is required for landing below -40 C

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19
Q

Maximum taxi speed (CPS)

Straight DRY or WET

A

30 knots

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20
Q

Maximum taxi speed (CPS)

Straight contaminated

A

15 knots

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21
Q

Minimum Flight Speed All Altitudes (CPS)

A

Except as described in normal/abnormal/emergency procedures, the airplane may never be operated below the “green dot” speed

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22
Q

Operating Speed Limits

Vmo

A

320 KIAS

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23
Q

Operating Speed Limits

Mmo

A

82 Mach

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24
Q

Maximum Turbulent Air Penetration Speed

Less than 10,000’ MSL

A

250 KIAS

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25
Q

Maximum Turbulent Air Penetration Speed

Greater than or equal to 10,000’ MSL

A

270 KIAS/ .76 Mach (whichever is less)

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26
Q

Minimum Ram Air Turbine (RAT) Speed

A

130 KIAS

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27
Q

Oxygen Quantity

Green

A

Normal operating range (minimum for dispatch with three crewmembers on the flight deck).

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28
Q

Oxygen Quantity

Cyan

A

Normal operating range (minimum for dispatch with two crewmembers on the flight deck).

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29
Q

Oxygen Quantity

Amber

A

Cautionary operating range (dispatch is not allowed)

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30
Q

Cabin Pressurization Limits

Up to 37,000’

A

7.8 psi

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31
Q

Cabin Pressurization Limits

Above 37,000’

A

8.3 psi

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32
Q

Cabin Pressurization Limits

Maximum Differential Overpressure

A

8.7 psi

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33
Q

Cabin Pressurization Limits

Maximum Differential Negative Pressure

A

-0.5 psi

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34
Q

Cabin Pressurization Limits

Maximum Differential Pressure fo Takeoff and Landing

A

0.2 psi

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35
Q

Single Pack Operation

Maximum Altitude for Single Pack Operation

A

FL310

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36
Q

Minimum Autopilot Altitudes (CPS)

Minimum height to engage on takeoff

A

Acceleration Altitude

(The autopilot may be engaged on takeoff at or above acceleration altitude, after horizontal and vertical flight director modes are selected. This is because the FD takeoff mode (TO) sometimes reverts to FPA after AP engagement.)

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37
Q

Minimum Autopilot Altitudes (CPS)

Minimum height to engage on go-around

A

400’ AGL

The autopilot may be engaged during a go-around at or above 400’ AGL provided GA mode is active.

38
Q

Minimum Autopilot Altitudes (CPS)

Minimum En Route Height

A

500’ AGL

39
Q

Minimum Autopilot Altitudes (CPS)

Minimum height for non precision

A

MDA

40
Q

Minimum Autopilot Altitudes (CPS)

Minimum height for precision approach

A

70’ AGL

(The autopilot may remain engaged during a go-around from a coupled ILS approach if the go-around is initiated at an altitude at or above 70’ AGL.)

41
Q

Minimum Autopilot Altitudes (CPS)

Special instrument approach

A

As specified in the Procedure

Some instrument approach procedures publish a minimum autopilot altitude for the approach procedure.

42
Q

Battery Volt limit

Maintenance is required if the battery volt is less than

A

21v

43
Q

Battery Temperature Limit

The minimum battery temperature from the APU to start

A

-20C

44
Q

Taxi and landing lights (CPS)

When airplane is stopped, taxi and landing lights must be

A

OFF

this prevents cracking of the lenses

45
Q

Taxi and Landing Lights (CPS)

For takeoff and in flight the taxi nose light must be

A

OFF

46
Q

No Break Power Transfer

To avoid power transfer interruptions when connecting or disconnecting an electrical source (CPS)

A

Confirm power transfer on the electrical synoptic page or wait 10 seconds

47
Q

Flap Altitude Limit

Maximum altitude for flap extended

A

20,000’

48
Q

Flap Speed Limits

Flaps 1

A

230

49
Q

Flap Speed Limits

KIAS Flaps 2

A

215

50
Q

Flap Speed Limits

KIAS Flaps 3

A

200

51
Q

Flap Speed Limits

KIAS Flaps 4

A

180

52
Q

Flap Speed Limits

KIAS Flaps 5

A

180

53
Q

Flap Speed Limits

KIAS Flaps Full

A

165 KIAS

54
Q

Flaps 4 Limitation (CPS)

A

Flaps 4 may be used for takeoff/go around only. The use of flaps 4 during the approach and landing regime is prohibited

55
Q

Maximum usable fuel

A

20,785 lbs

56
Q

Imbalance

Maximum fuel imbalance in flight

A

794 lbs

57
Q

Minimum fuel tank temperature

A

-40 C

58
Q

Takeoff and landing

During takeoff and landing the crossfeed selector knob must be

A

OFF

59
Q

Cold weather operation

A hydraulic system warm-up must be accomplished before starting the engines if the reservoir temperatures are below

A

-18C

60
Q

Freezing Rain and Freezing Drizzle

IF abnormal ice formation is observed on areas of the airplane that do not usually accrete ice

A

the flight is operating in a Super cooled large droplet (SLD) condition. Exit the SLD condition as soon as possible

61
Q

The MCDU TO DATASET MENU must be set to ENG when SAT is 5C to 10C and:

A
  1. IF there is any possibility of encountering visible moisture up to 1700 ft AFE or
  2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engine nacelles, or engine sensor probes.
62
Q

The MCDU TO DATASET MENU must be set to ALL when the SAT is less than 5 C and:

A
  1. IF there is any possibility of encountering visible moisture up to 1700 ft AFE or
  2. Operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines, or freeze on engine nacelles, or engine sensor probes.
63
Q

Icing conditions exist in flight whenever the Static Air Temperature (SAT) on the ground or for takeoff, or Total Air Temperature (TAT) in flight, is

A

10°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, and ice crystals).

64
Q

If either one or both ice detectors are failed, the crew must

A

set the mode selector to ON when icing conditions exist or are anticipated below 10°C TAT with visible moisture.

65
Q

Airspeed Limit

Maximum speed to operated the windshield wipers

A

250 knots

66
Q

Landing Gear Speed Limits
Vlo for extension
Vlo for retraction
Vle

A

250 KIAS

(VLO is the maximum speed at which the landing gear can be safely extended and retracted.
VLE is the maximum speed at which the airplane can be safely flown with the landing gear extended and locked.)

67
Q

Tire Speed Limit

Maximum ground speed

A

195 Knots

68
Q

E170

Minimum runway/taxiway width for a 180 degree turn

A

54’ 8”

69
Q

E175

Minimum runway/taxiway width for a 180 degree turn

A

59’ 2”

70
Q

Baro, Air Data VHF 1 and Radar Limitations

A

Baro altimeter minimums must be used for all CAT I approaches

71
Q

The VOR flight director mode is prohibited

A

This VOR flight director mode is inhibited. VOR navigation using the flight director must be predicated on HDG mode and VHF (green) needles or LNAV mode (magenta)

72
Q

IESS Limitations

A

Back course approaches using the IESS are prohibited

73
Q

Miscellaneous APU limits

Start environment Min and Max temperatures

A

-54c
and
APU temperature matches the Airplane Operational Envelope Temperature Limitations in AOM I, 2-2.7.3.

74
Q

Miscellaneous APU limits

Max altitude for Start

A

30,000’

75
Q

Miscellaneous APU limits
Maximum Altitude For:
APU GEN

A

33,000’

76
Q

Miscellaneous APU limits
Maximum Altitude For:
Bleed Air

A

15,000’

77
Q

Miscellaneous APU limits
Maximum Altitude For:
APU-Assisted Engine Start

A

21,000’

78
Q

Miscellaneous APU limits

Minimum battery voltage to start the APU

A

21v

79
Q

APU Starter Duty Cycle Limits
Start number 1 and 2
Maximum Time:
Cool-Down Time

A

60 seconds

60 seconds

80
Q

APU Starter Duty Cycle Limits
Start number 3
Maximum Time:
Cool-Down Time

A

60 seconds

5 minutes

81
Q

Before Starting the APU after an Engine is Shutdown

Wait for the engine to go below:

A

30% N2

(This procedure is necessary to ensure that battery 2 is available to the airplanes electrical network as a back-up and not isolated for the APU start.)

82
Q

Engine Temperature Limits

ITT Start

A

815 C

83
Q

Automatic Takeoff Thrust Control System (ATTCS)

For takeoff, the ATTCS must be

A

ON

84
Q

Warm up and Cool Down (CPS)

Engine warm-up and cool down period

A

2 minutes

the cool down time begins at weight on wheels after landing

85
Q

Starter Duty Cycle Limits
Start Number 1 and 2
Maximum time (ground and flight):
Cool Down time

A

90 seconds on ground
120 seconds in flight

Cool down 10 seconds

86
Q

Starter Duty Cycle Limits
Start Number 3 through 5
Maximum time (ground and flight):
Cool Down time

A

90 seconds on ground
120 seconds in flight

Cool down 5 minutes

(After five sequential start attempts, a cycle may be repeated following a 15-minute cool-down period.)

87
Q

Engine Thrust

Powerback Operations

A

PROHIBITED

88
Q

Thrust Reverser Limitations

The engines must be idle by

A

60 KIAS

89
Q

Thrust Reverser Limitations

The engines must be out of reverse by

A

30 KIAS

(For operations on contaminated runways, reverse thrust may be used below the speeds indicated above at the discretion of the crew (e.g., full reverse to a complete stop may be used if necessary to stop the airplane safely).)

90
Q

An assumed temperature (FLEX) takeoff is not allowed if any of the following conditions exist:

A
  1. The runway is contaminated. Refer to AOM I, 7-3.3 Takeoff on Wet, Slippery or Contaminated Runways.
  2. The antiskid system is inoperative.
  3. The Takeoff performance section of the takeoff report does not include FLEX takeoff data.
  4. Compass airport information pages (CCI) prohibit an assumed temperature takeoff.
  5. Any time LLWS is reported or present
  6. Any time there is significant weather which may produce windshear (i.e. Thunderstorms)
  7. The PIC determines the conditions for an assumed temperature takeoff are unsafe.

CP (5 decks)

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