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B 737NG (pitu) > Limitations > Flashcards

Limitations Flashcards

1
Q

Runway Slope Limits

A

+/- 2%

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2
Q

Maximum Demonstrated Crosswind

A

36 kts without winglets

33 kts with winglets

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3
Q

Maximum Speed (Vmo/Mmo)

A

320 kias

0.82 m

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4
Q

Turbulent Air Penetration Speed

A

280 kias / .76m

250 kias when below 15,000 ft and below MLW

(AOM Vol. 1 SP.16.21)

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5
Q

Maximum Altitude

A

41,000 ft

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6
Q

Maximum Takeoff and Landing Altitude

A

8,400 ft
or
12,000 ft with Hight Altitude Option

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7
Q

Maximum Cabin Differential Pressure

A

9.1 psi

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8
Q

Maximum Altitude for APU Bleed and Electrical use

A

10,000 ft

*Under Captain’s Emergency Authority, APU has demonstrated the capability to supply both bleed air and electrical power up to 20,000 ft.

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9
Q

Maximum Altitude for APU Bleed Only Use.

A

17,000 ft

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10
Q

Maximum Altitude for APU Bleed and Electrical Use on Ground

A

15,000 ft

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11
Q

Maximum Altitude For APU Electrical Use Only

A

41,000 ft

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12
Q

Minimum Altitude for Autopilot use After Takeoff

A

400 ft AGL

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13
Q

Minimum Altitude for Autopilot “ON” During Non-Precision Approach

A

50 ft Below Minimums

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14
Q

Maximum Engine Limits

A

Redline

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15
Q

Minimum Engine Limits

A

Redline

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16
Q

Engine Caution Limits

A

Amber

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17
Q 
Engine Ignition Must Be On For:
\_\_\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_\_\_
\_\_\_\_\_\_\_ \_\_\_\_\_\_\_
\_\_\_\_\_\_\_\_\_\_\_
A

Takeoff
Landing
Heavy Rain
Anti-Ice

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18
Q

Maximum Flaps Extension Altitude

A

20,000 ft

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19
Q

Minimum Altitude For Speed Brake Use.

A

1,000 ft

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20
Q

Alternate Flap Duty Cycle (down and back up)

A

0-15-0 = 5 min.

> 15 = 25 min.

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21
Q

Fuel System Minimum Temperatures

A

-43˚C or 3˚C above fuel freezing

Whichever is warmer

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22
Q

Fuel System Maximum Temperatures

A

49˚C

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23
Q

Random Fuel Imbalance

A

1,000 lbs for Taxi, Takeoff, Landing

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24
Q

Icing Condition Temperature

A

10˚C/50˚F or below

25
Q

Air Data Inertial Reference Unit (ADIRU) Alignment Must Not be Attempted at Latitudes Greater Than

A

78º 15 min

26
Q

Maximum Flight Operating Latitude

A

82º north and south

27
Q

Flight Deck Door Operational Check Must be Checked

A

once a day

28
Q

Escape Slide Retention Bar

A

must be installed for taxi, takeoff and landing

29
Q

Standby Altimeter for RVSM Accuracy

A

does not meet accuracy requierements for RVSM

30
Q

Maximum Altitude Difference Between Captain’s and FO’s Altimeters for RVSM Use While in Flight

A

200 ft

31
Q

Maximum Difference Between the Captain’s and FO’s Altimeters on the Ground for RVSM Use

A

airport elevation up to 5000ft = 50 ft

obove 5000ft = 60ft

32
Q

Maximum Difference of Captain’s and FO’s Altimeters to Airport Field Elevation While on Ground

A

75ft

33
Q

With Engine Bleed on do Not Run A/C Packs in _______ for Takeoff, Approach, or Landing

A

high

34
Q

Engine TAI Must Be On When _______

A

in icing conditions or icing conditions are expected

Exception: during climb when Tº is below -40º SAT

35
Q

De-Icing with Type II and IV fluids for Airplanes without Stiffened Elevator Tabs.

A

max speed 270kts auntil maintenance procedures are accomplished

36
Q

Autopilot Single Channel Approach Minimum Disengagement Altitude

A

50ft AGL

RA 100ft for airports above 8400ft

37
Q

Maximum allowable wind components for Autoland Operations

Headwind: _________
Crosswind: _________
Tailwind: __________

A

25
20
10

38
Q

Maximum and Minimum Glideslope Angles for Autoland

A

3.25º and 2.5º

39
Q

Maximum Pressure Altitude for use of Autoland

A

8400ft

40
Q

Use of VHF communications with ATC on the ground

A

use radio that is connected to top antenna

41
Q

Use of auxiliary power outlets in the flight deck

A

requires regulatory approval

42
Q

Reverse Thrust Limitation

A

intentional inflight use is prohibited

43
Q

APU Bleed Valve Must Be Closed When

A
  • a ground air is connected and isolation valve open
  • eng 1 bleed valve open
  • eng 2 bleed valve open and isolation valve open
44
Q

APU Bleed Valve May Be Open During Engine Start But:

A

avoid power settings above idle

45
Q

Holding In Icing Conditions With Flaps Extended

A

prohibited

46
Q

Do Not Extend Speed Brake Lever Beyond _____ ______ When InFlight

A

flight detent

47
Q

Maximum Speed for Use of Speed Brakes

A

use of speed brakes at speeds in excess of 320kts can cause severe vibration and damage the horizontal stabilizer

48
Q

Rapid and Large Alternating Control Inputs

A

avoid - may result in structural failure even below Va

49
Q

Time Between Actuations of The Alternate Flap Switch

A

15 sec - avoid damage to motor`s clutch

50
Q

When QFE is Selected, Use of VNAV, LNAV, and Veridical Situation Display is _______

A

prohibited

51
Q

Regarding the PFD, If QFE is Used Instead of QNH: _____________

A

slection of QFE must be made in the FMS

52
Q

Use of Look Ahead Terrain Alerting:
a - Without GPS or
b - With GPS and an Older GPWS Computer

A

is prohibited

53
Q

Limitation On Use of Look Ahead Terrain Alerting (GPWS)
A - ____________________
B - ____________________

A

A - do not use terrain display for navigation

B - do not use within 15 min of takeoff, approach or landing at airports contained in the GPWS database

54
Q

Weather Radar Limitations

A

do not operate in a hangar or 50ft from personnel and fuel spills except in TEST mode

55
Q

Scheduled Fuel Imbalance

A

zero

56
Q

Main Fuel Tanks Must Be Full If ___________

A

center tanks has more than 1000 lbs

57
Q

Anti-Skid INOP

A

assumed temperature reduced thrust takeoff is not permitted

58
Q

Brakes

A

do not apply until after touchdown

B 737NG (pitu) (2 decks)

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