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SWA-737 > Limitations (checked) > Flashcards

Limitations (checked) Flashcards

1
Q

Min fuel tank temp

A

-37 C

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2
Q

Radar operation limitation

A

Not while fueling
Not near fuel spills
Not near people

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3
Q

When must the center tank pumps be turned off

A

CL: when both center tank fuel pump LOW PRESSURE lights illuminate.

NG: Corresponding center tank fuel pump switch must be turned off when it’s LOW PRESSURE light illuminates.

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4
Q

Ground Opps with center tank fuel pumps

A

Must not be selected to ON unless Center Tank has exceeds 1000 lbs, except when refueling

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5
Q

Max altitude for APU bleed air and Electric at the same time in NG

A

NG: 10,000ft

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6
Q

After starting, what are the limitations for engine stabilization

A

Two minutes at or near idle prior to applying takeoff thrust

5 minutes recommended on first flight of the day

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7
Q

Max operating pressure altitude for 300/500

A

37,000

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8
Q

You are ready to take off. You have 900 lbs in the center fuel tank, what position should the center fuel pump switches be in?

A

OFF

Note: CL: Center tank fuel pumps switches must be ON for takeoff with more than 1000 lbs of fuel in the center tank

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9
Q

Holding in icing conditions

A

Holding is icing conditions with flaps extended is PROHIBITED

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10
Q

Max altitude for Flap Exteninson

A

20,000

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11
Q

What are the limitations for a tripped circuit breaker

A

Only reset once

Allow 2 minutes cooling before reset

Inflight resent only accomplished when it’s systems use is critical to safe operation of flight and or directed by QRH.

Do not cycle (pull & reset) unless
~ directed by QRH
~ directed by procedure listed in AOM, FOM, MEL
~ coordinated and approved by maintenances

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12
Q

Max altitude for APU Bleed Air ONLY in NG

A

17,000

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13
Q

Max altitude for APU Electrical ONLY in 300/500

A

CL: 35,000

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14
Q

Speed brake - min altitude for use

A

1000 AGL

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15
Q

Speed brake in flight use limitations

A

Do not extend beyond flight detent

Do not use unless flaps fully retracted

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16
Q

Min time to cool down engine after landing before shutdown

A

Operate at or near idle for min 1 minute prior to shutdown

17
Q

Max altitude for operating APU Electrical ONLY in NG

A

41,000

18
Q

EGT Limitation for ground start

A

725 c

Will not provide redline protection, but will shutdown engine if it detects an impending hot start

19
Q

Max altitude for operating APU in NG

A

41,000

20
Q

Max fuel tank temp

A

+49 C

21
Q

Max altitude for APU Bleed Air ONLY in 300/500

A

17,000

22
Q

TCAS Limitations

A

Flight crews must immediately respond to TCAS information (both TA and RA) by using TCAS (Traffic Avoidance) guidelines located in the QRH Maneuvers Chapters

Pilots are authorized to deviate from an ATC Clearance to the extent necessary to comply with TCAS II Resolution Advisory (RA)

23
Q

Max operating pressure altitude NG

A

41,000

24
Q

Alternate Flaps Limitation

A

Alternate flaps duty cycle in flight is one complete cycle then 5 minutes off.

A complete cycle is movement from 0 to 15 and back to 0.

The Alternate Flap Switch must must be in the OFF for 15 seconds before reversing the direction of flap movement.

25
Q

Max altitude for operating APU Bleed Air and Electric in 300/500

A

CL: 10,000

26
Q

What is the checked limitation on Thrust Reverser

A

For ground use only

27
Q

Limitation for Pack operation for Takeoff, Approach & Landing

A

With engine bleed switches ON,

DO not operate packs in HIGH for Takeoff, Approach & Landng

28
Q

You are ready for takeoff, you have 1500 lbs of fuel in the center tank, what position should you center fuel pump switches be in?

A

Both ON

CL: Center pump fuel switches must be ON for takeoff with more than 1000 lbs of fuel in the center tank

29
Q

Cargo bay fire suppression limitation

A

Must land within 60 minutes of initial discharge of the fire suppression system

195 mins for the 800 ETOPS model

30
Q

Fuel distribution limitations

A

Use center tank to depletion then use wing tanks

Note: May leave 1000 lbs in center tank provided the balance affects have been considered

31
Q

Minimum duct pressure for Ground Start

A

CL: 30 PSI reduced by 0.5psi per 1000 ft Pressure Altitude above sea level

32
Q

Limitations for operating with 1 generator while on ground

A

NG: Max (engine driven) 215 amps

33
Q

Min time before removing AC power after IRS shutdown

A

30 secs

34
Q

Max altitude for operating APU (300/500)

A

CL: 35,000

35
Q

4 fuel limitations while on the ground at the gate

A

~ Wing tanks must be full if center tank has more than 1000 lbs in them

~ Center tank fuel pumps must NOT be positioned ON unless the center tank fuel qty exceeds 1000 lbs, except when de-fueling or transferring fuel

~ Center tank fuel pumps must NOT be positioned ON unless personnel are available on the flight deck to monitor LOW PRESSURE lights

~ Flight crews MUST NOT reset tripped fuel quantity, fuel pump, fuel pump control circuit breakers.

36
Q

Limitations of Circle To Land

A

Both 1000 ft ceiling AND 3 SM vis

Review Jepp for specific wx mins greater than 1000/3. Higher mins are controlling

Use a MDA of 1000 ft above field elevation unless restricted to higher altitude in circle approach section of Jepp.

SWA-737 (21 decks)

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