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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
Air Data Inertial Reference Unit (ADIRU) Alignment Must Not be Attempted at Latitudes Greater Than
78º 15 min
26
Maximum Flight Operating Latitude
82º north and south
27
Flight Deck Door Operational Check Must be Checked
once a day
28
Escape Slide Retention Bar
must be installed for taxi, takeoff and landing
29
Standby Altimeter for RVSM Accuracy
does not meet accuracy requierements for RVSM
30
Maximum Altitude Difference Between Captain's and FO's Altimeters for RVSM Use While in Flight
200 ft
31
Maximum Difference Between the Captain's and FO's Altimeters on the Ground for RVSM Use
airport elevation up to 5000ft = 50 ft obove 5000ft = 60ft
32
Maximum Difference of Captain's and FO's Altimeters to Airport Field Elevation While on Ground
75ft
33
With Engine Bleed on do Not Run A/C Packs in _______ for Takeoff, Approach, or Landing
high
34
Engine TAI Must Be On When _______
in icing conditions or icing conditions are expected Exception: during climb when Tº is below -40º SAT
35
De-Icing with Type II and IV fluids for Airplanes without Stiffened Elevator Tabs.
max speed 270kts auntil maintenance procedures are accomplished
36
Autopilot Single Channel Approach Minimum Disengagement Altitude
50ft AGL RA 100ft for airports above 8400ft
37
Maximum allowable wind components for Autoland Operations Headwind: _________ Crosswind: _________ Tailwind: __________
25 20 10
38
Maximum and Minimum Glideslope Angles for Autoland
3.25º and 2.5º
39
Maximum Pressure Altitude for use of Autoland
8400ft
40
Use of VHF communications with ATC on the ground
use radio that is connected to top antenna
41
Use of auxiliary power outlets in the flight deck
requires regulatory approval
42
Reverse Thrust Limitation
intentional inflight use is prohibited
43
APU Bleed Valve Must Be Closed When
- a ground air is connected and isolation valve open - eng 1 bleed valve open - eng 2 bleed valve open and isolation valve open
44
APU Bleed Valve May Be Open During Engine Start But:
avoid power settings above idle
45
Holding In Icing Conditions With Flaps Extended
prohibited
46
Do Not Extend Speed Brake Lever Beyond _____ ______ When InFlight
flight detent
47
Maximum Speed for Use of Speed Brakes
use of speed brakes at speeds in excess of 320kts can cause severe vibration and damage the horizontal stabilizer
48
Rapid and Large Alternating Control Inputs
avoid - may result in structural failure even below Va
49
Time Between Actuations of The Alternate Flap Switch
15 sec - avoid damage to motor`s clutch
50
When QFE is Selected, Use of VNAV, LNAV, and Veridical Situation Display is _______
prohibited
51
Regarding the PFD, If QFE is Used Instead of QNH: _____________
slection of QFE must be made in the FMS
52
Use of Look Ahead Terrain Alerting: a - Without GPS or b - With GPS and an Older GPWS Computer
is prohibited
53
Limitation On Use of Look Ahead Terrain Alerting (GPWS) A - ____________________ B - ____________________
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
Weather Radar Limitations
do not operate in a hangar or 50ft from personnel and fuel spills except in TEST mode
55
Scheduled Fuel Imbalance
zero
56
Main Fuel Tanks Must Be Full If ___________
center tanks has more than 1000 lbs
57
Anti-Skid INOP
assumed temperature reduced thrust takeoff is not permitted
58
Brakes
do not apply until after touchdown

B 737NG (pitu) (2 decks)

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