Limitations Flashcards

1
Q

Runway Slope

A

+/- 2%

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2
Q

Vmo/Mmo

A

340 KIAS / .82 M

Observe Vmo pointer and gear/flap placards

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3
Q

Severe Turbulence Airspeed

A

280 KIAS / .76M

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4
Q

Max Operating Altitude

A

41,000 ft

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5
Q

Max Takeoff/Landing Alt

A

8,400 ft

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6
Q

Max Flight Ops Latitude

A

82N and 82S

Exceptions:
80W - 130W —— 70N
120E - 160E —— 60S

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7
Q

Max Tailwind T/O

A

15 kts

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8
Q

Max Tailwind Landing

A

10 kts

(Ops Adv page [-7] may allow 15kts

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9
Q

Max Demonstrated XWind

T/O and Landing

A

33 kts (NG)

32 kts (MAX)

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10
Q

Ground Wind Operating Envelope

A

XWinds > 43 kts : max thrust = taxi

Winds > 58 kts : idle thrust
except for setting T/O thrust

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11
Q

Max Taxi Weight

A

174,700 lbs

MAX-8 = 181,700

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12
Q

Max Takeoff Weight

A

174,200 lbs

Max-8 = 181,200

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13
Q

Max Landing Weight

A

146,300 lbs

MAX-8 = 152,800

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14
Q

Max Zero Fuel Weight

A

136,000 lbs

MAX-8 = 145,400

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15
Q

EVAC Systems:

Any time pax onboard one exit must be:

A

Open or Armed

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16
Q

EVAC System:

On Rev Flights when must the girt bar be inserted in all brackets?

A

Taxi, Takeoff, and Landing

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17
Q

OVERWATER:

160 seat aircraft max occupants

A

168

160 seats + 2 Pilot + 1W + 6 FA = 169

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18
Q

OVERWATER:

Max occupancy on A/C with 172 seats?

A

NONE

Extra life rafts (3 -> 4)

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19
Q

How often must the flight deck door and access system be checked?

A

Daily - prior to first flight

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20
Q

When will the flight deck door access code be used?

A

Only in emergencies

Normal procedures for normal access

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21
Q

How do you lock the door when DC Bus 2 unpowered?

A

POWER CUTOFF — OFF

DEADBOLT — LOCKED KEY INOPERABLE

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22
Q

With one or both engine bleeds on, do NOT operate the packs on HIGH under what conditions?

A

Takeoff / Approach / Landing

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23
Q

Max Cabin Diff Pressure

A

9.1 psi

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24
Q

Max Alt for unpressurized flight (after inflight depressurization)

A

14,000 ft

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25
Q

Max Alt unpressurized- dispatched

A

10,000 ft

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26
Q

Icing Conditions

  • Ground & Takeoff
  • Inflight
A

Ground: OAT = 10C
Inflight: TAT = 10
C

1) Visible moisture in any form is present
(i. e. clouds, fog w/ vis 1 mile or less, rain, snow, sleet, & ice crystals)
2) 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 engine or nacelles

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27
Q

When operating in icing, what is the limitation with regards to the Engine Ignitions?

A

They must be ON

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28
Q

Engine anti-ice must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temp is BELOW ______

A

-40*C SAT

DURD - must be on even

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29
Q

Can wing anti-ice be used in lieu of ground deice/ anti-ice?

A

NO

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30
Q

Do not operate wing anti-ice in the ground when OAT is ABOVE _____

A

10*C

31
Q

Min Autopilot engagement for T/O

A

400’ AGL

32
Q

Single channel AP min disengagement height

A

50’ AGL

33
Q

Aileron trim with autopilot engaged is _______

A

Prohibited

34
Q

Can we use dual channel AP for approach?

A

NO, prohibited

35
Q

Do not use LVL CHG on final approach below ______

A

1,000’ AFE

36
Q

If one HF radio is selected for transmission, what is the appropriate procedure?

A

Deselect other HF radio on all panels to prevent interference

37
Q

Do not operate HF radios during _____ operations.

A

Refueling

38
Q

When must the broadband switch be OFF?

A

Aircraft de-icing, taxing under skybridge, or while in hangar

(PAX Oxygen switch is nearby)

39
Q

Engine limit markings:

Max/Min
Cautionary
Normal

A
Max/Min = red
Cautionary = amber
Normal = white
40
Q

Engine Ignition Must be used when? (4 conditions)

A

AUTO or CONT:
Takeoff
Landing
Anti-Ice

Operation in Heavy Rain (CONT)

41
Q

EECs in ALTN for Takeoff

What are the limitations?

A

1) Both EECs in ALTN
2) 26K max thrust (27K if planned)
——TO for MAX-8
3) DO NOT use FMC N1 or QRH V-speeds
4) Auto-throttles use is PROHIBITED

42
Q

When can 27K bump thrust be used?

A

If authorized by Dispatch and on load agent generated TPS.

KSNA excluded

43
Q

Intentional selection of REV thrust inflight is _________.

A

PROHIBITED

44
Q

APU Bleed + Elec Load MAX ALT

A

10,000 ft

45
Q

APU bleed only MAX ALT

A

17,000 ft

46
Q

APU ELEC only load MAX ALT

A

41,000 ft

47
Q

APU suggested starting ALT

A

25,000 ft

48
Q

When must the APU bleed valve be closed? (3)

A

1) ground air CONNECTED and isolation valve OPEN
2) engine 1 bleed OPEN
3) isolation valve and engine 2 bleed OPEN

*APU bleed may be open during engine start but limit thrust to idle

49
Q

Cooling period between 3 consecutive starts of APU

A

15 min cooling period

50
Q

Operation with Assumed Temperature Reduced T/O Thrust is not permitted with ________ INOP

A

Anti-skid

51
Q

Min oil quantity for departure

A

12 qts

MAX-8 = 17qts

52
Q

MAX ALT with flaps extended

A

20,000 ft

53
Q

Flap position when holding in icing

A

UP

54
Q

Do NOT deploy speed brakes in flight with RA < ____ ft

A

1,000 ft

55
Q

In flight do NOT extend speed brakes beyond ______ detent

A

FLIGHT

56
Q

Avoid rapid and large alternating control inputs (esp in combination with large changes in pitch, roll, or yaw) as they may result in structural failure at any speed including below ______.

A

Va (maneuvering)

57
Q

When extending or retracting via ALTERNATE FLAPS, how long should you wait between activations?

A

15 seconds

58
Q

After complete extend/retract cycle (i.e. 0 to 15 to 0) what is the cooling period?

A

5 mins

59
Q

Use of HUD (Head Up Display) with which RA INOP is prohibited?

A

RA 1

60
Q

Max allowable in flight difference between CA and FO altitudes (RVSM) is:

A

200 ft

61
Q

Max allowable on the ground difference between CA and FO altitudes for RVSM:

A
50 ft (SL to 5,000’)
60 ft (5,001 to 10,000’)
62
Q

MAX on the ground diff between CA or FO and field elevation for RVSM:

A

75 ft

63
Q

Does the standby ALR meet altimeter accuracy requirements for RVSM?

A

NO

64
Q

MAX tank fuel temp

A

49*C

65
Q

MIN fuel tank temp prior to T/O and inflight

A
  • 43*C

OR

3*C above freezing point temp limit

*higher is limiting

66
Q

Random fuel imbalance limit

A

1,000 lbs

67
Q

If center tank contains more than 1,000 lbs, what limit is there for main ranks 1 and 2?

A

They must be full of center tank has more than 1,000 lbs

68
Q

Is ballast fuel authorized?

A

NO

69
Q

Do NOT apply brakes until after ________.

A

Touchdown

70
Q

Can EGPWS terrain display be used for navigation?

A

NO

71
Q

To comply with a GPWS warning can pilots deviate from ATC clearances?

A

YES

72
Q

When must EGPWS be inhibited (TERR INHIBIT)?

A

When directed by F4 message

[Operations from/to runways and airports not in databases or approaches that have been identified as potentially producing false terrain alerts]

73
Q

When must you not operate the Weather radar?

A

In Hangar and within 50’ of fueling ops, fuel spills, and people