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737 > Limitations > Flashcards

Limitations Flashcards

1
Q

Immediate Action Items for:

Cabin Altitude Warning or Rapid Depressurization / Emergency Descent

A
  1. Oxygen Masks and Regulators - On, 100%
  2. Crew Communications - Establish
  3. Seatbelt sign - On

Ref: QRC

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2
Q

Immediate Action Items for:

Engine Start - Aborted Start

A

Engine start lever (affected engine) - CUTOFF

Ref: QRC

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3
Q

Landing Crosswind Component - Runway CC 6

A

37 knots

Ref: FM 1.20.7

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4
Q

Landing Crosswind Component - Runway CC 5

A

37 knots

Ref: FM 1.20.7

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5
Q

Takeoff Crosswind Component - Runway CC 6

A

33 knots

Ref: FM 1.20.7

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6
Q

Takeoff Crosswind Component - Runway CC 5

A

25 knots

Ref: FM 1.20.7

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7
Q

Maximum Cabin Pressure Differential

A

9.10 PSI

Ref: FM 1.30.3

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8
Q

Minimum duct pressure for two pack operation from one bleed source

A

20-25 PSI

Ref: FM 1.30.3

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9
Q

Icing conditions exist on the ground and for takeoff when:

A

OAT is 10C or below with visible moisture, standing water, slush, or snow

Ref: FM 1.30.4

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10
Q

Icing conditions exist in flight when:

A

TAT is 10C or below with visible moisture

Ref: FM 1.30.4

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11
Q

Window heat must be on ____ minutes prior to takeoff.

A

10

Ref: FM 1.30.5

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12
Q

Autopilot minimum engagement height

A

400 feet AGL

Ref: FM 1.30.6

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13
Q

Autoland maximum headwind

A

25 knots

Ref: FM 1.30.5

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14
Q

Autoland maximum crosswind

A

15 knots

Ref: FM 1.30.7

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15
Q

Autoland maximum tailwind

A

10 knots (except 900[401-412] with flaps 30)

Ref: FM 1.30.5

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16
Q

Autopilot use prohibited ____ feet radio altitude at airport pressure altitudes above ____ feet.

A

100; 8400

Ref:

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17
Q

Minimum altitude for autopilot use on approach for

  • ILS/GLS coupled approaches
  • Non-precision approaches
A

50 feet AGL
50 feet below MDA/DA

Ref:

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18
Q

Maximum runway pressure altitude for autoland

A

8400 feet

Ref:

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19
Q

Maximum and minimum glideslope angles for autoland

A

2.5 - 3.25 degrees

Ref:

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20
Q

Do not use LVL CHG on final approach below ____

A

1000 ft AFE

Ref: FM 1.30.10

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21
Q

Minimum battery voltage for APU start

A

23 volts

Ref:

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22
Q

Minimum Oil Pressure for NG, MAX

A

NG - 13 PSI
MAX - 17.4 PSI

Ref:

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23
Q

Maximum EGT for Start - NG, MAX

A

NG - 725C
MAX - 753C

Ref: FM 1.30.13

24
Q

Maximum continuous EGT - NG, MAX

A

NG - 925C
MAX - 1013C

Ref: FM 1.10.13

25
Q

Minimum Engine Oil Quantity for Start

A

70%

Ref:

26
Q

Wait a minimum of ____ for APU shutdown cycle to complete, then turn ____ switch to OFF (NG)

A

120 seconds

Ref:

27
Q

Maximum Flap Extension Altitude

A

20,000 feet

Ref: FM 1.30.17

28
Q

In flight, the speed brake lever should not be extended beyond the _______ detent with greater than flaps ___ selected.

A

ARMED; 10

Ref: FM 1.30.18

29
Q

Maximum airspeed to extend the flaps with the alternate system

A

230 knots

Ref: FM 1.30.18

30
Q

Maximum speed with Mach Trim Fail

A

280 knots / 0.82 mach

Ref:

31
Q

Minimum inflight fuel temperature for Jet A and Jet A-1

A

-37C and -44C, respectively

Ref:

32
Q

Maximum tire groundspeed

A

NG - 195 knots
MAX - 204 knots

Ref:

33
Q

Maximum Operating Pressure Altitude

A

41,000 feet

Ref:

34
Q

Autobrake action for RTO occurs above ____ wheel speed.

A

90 knots for NG, 88 knots for MAX

Ref:

35
Q

G Limits for Flaps up and Flaps down

A

Flaps up: -1.0 - 2.5
Flaps down: 0 - 2.0

Ref: FM 1.20.2

36
Q

Maximum takeoff/landing pressure altitude

A

10,000 feet

Ref:

37
Q

Minimum Runway Width

A

100 feet

Ref:

38
Q

Maximum Takeoff/Landing Tailwind Component

A

15 knots

Ref:

39
Q

MMO

A

0.82 Mach

Ref: FM 1.20.4

40
Q

Maximum Gear Retraction Speed

A

235 knots

Ref:

41
Q

Maximum Gear Extension Speed

A

270 knots / 0.82 Mach

Ref:

42
Q

Maximum Gear operating/extended speed

A

320 knots / 0.82 Mach

Ref:

43
Q

Maximum severe turbulence penetration speed - cruise

A

TURB N1 setting from cruise page

Ref:

44
Q

Recommended Severe Turbulence Penetration Speed - climb and descent

A

280 knots / 0.76 Mach

Ref:

45
Q

Minimum Ground Time After Landing - Carbon Brakes

A

48 minutes

Ref:

46
Q

Do not deploy the speed brakes at radio altitudes less than _____

A

1000 feet

Ref:

47
Q

While extending or retracting the flaps with the ALTERNATE FLAPS position switch, allow _____ seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again.

A

15

Ref:

48
Q

A fully charged battery can supply standby power for a minimum of _____ minutes.

A

30

Ref:

49
Q

The battery provides ____ volts DC.

A

28

Ref:

50
Q

Battery voltage range is ____ to ____ volts

A

22, 30

Ref:

51
Q

The Transformer Rectifiers convert ____ volt _____ to ____ volt ____

A

115 volt AC, 28 volt DC

Ref:

52
Q

What busses are powered by the standby power system?

A

DC standby bus, AC standby bus, battery bus

Ref:

53
Q

Fuel LOW Alert illuminates when fuel quantity is less than ______ lbs in the related main tank, and remains until fuel tank quantity is increased to ______ lbs.

A

2000, 2500

Ref:

54
Q

The Fuel CONFIG Alert displays when either engine is running, both center tank pump switches are OFF, and center tank fuel quantity is greater than ______ lbs.

A

1600

Ref:

55
Q

The Fuel IMBAL Alert displays when main tanks differ by more than ______ lbs and remains until the imbalance is reduced to ____ lbs.

A

1000; 200

Ref:

737 (3 decks)

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