Checked Limitations

Question 1

What are the weather minimums for a Circle-to-land approach maneuver?

Answer 1

Weather minimums are a 1000 ft ceiling and 3 miles visibility. Both ceiling and visibility criteria are required. Review the Jeppesen Approach chart to see if it specifies minimums higher than 1000/3. If so, then those higher minimums are required to execute the circle-to-land approach maneuver.q

Question 2

What MDA should you use on a circle-to-land maneuver?

Answer 2

Use a MDA of 1000 feet above airport elevation unless restricted to a higher altitude in the circle to land minimums section on the approach chart.

Question 3

Maximum Operating Pressure Altitude?

Answer 3

41,000 feet

Question 4

When should you not operate the Air conditioning packs in HIGH?

Answer 4

With engine bleed air switches ON, do not operate the air conditioning packs in HIGH for takeoff, approach, or landing.

NOTE: The Fire Protection non-normal procedures (QRH) take precedence over the statement regarding no air conditioning packs in HIGH during takeoff, approach, or landing. The CARGO FIRE and Smoke or Fumes Removal checklists require the operating pack switch(es) to be placed in HIGH in order to increase ventilation for smoke removal.

Question 5

Can you hold in icing conditions with flaps extended?

Answer 5

Holding in icing conditions with flaps extended is prohibited.

Question 6

Do not operate wing anti-ice on the ground when the OAT is above ___

Answer 6

10C

Question 7

Can wing anti-ice be used as a substitute for ground de-icing/anti-icing

Answer 7

Do not use wing anti-ice as a substitute for ground deicing/anti-icing and inspection procedures which are necessary to comply with operating rules.

Question 8

What are the restrictions associated with the weather radar?

Answer 8

Do not operate the weather radar during fueling, near fuel spills, or near people

Question 9

(NG) On the ground, what are the limits associated with engine driven engine generator operation?

Answer 9

(NG) On the ground, limit one generator operation (engine driven) to a maximum of 215 amps.

Question 10

(MAX) What is the limitation associated with one generator (engine driven) operation on the MAX?

Answer 10

(MAX) Limit one generator operation (engine driven) to a maximum of 215 amps on the ground or in the air.

Question 11

Do not remove AC power from the aircraft for at least ___ seconds after IRS shutdown

Answer 11

Do not remove AC power from the aircraft for at least 30 seconds after IRS shutdown

Question 12

Circuit Breakers. Inflight reset limitation

Answer 12

The in-flight reset of a tripped circuit breaker should only be accomplished when directed by the QRH. Allow approximately two minutes for cooling before resetting.

Question 13

Resetting a tripped circuit breaker other than when directed by the QRH must be done as follows:

Answer 13

A tripped circuit breaker may only be reset once. Allow approximately two minutes for cooling before resetting. An in-flight reset should only be accomplished if, in the judgment of the Captain, regaining use of that system is critical to the safe conduct of the flight.

Question 14

(NG) Max EGT for Ground Start

Answer 14

725C

Question 15

Operate engines at or near idle, after rollback, for a minimum of how long prior to applying takeoff thrust?

Answer 15

2 minutes (NG)
3 Minutes (MAX)

Question 16

How long should you operate the engines at or near idle prior to shutdown?

Answer 16

1 minute (NG)
3 minutes (MAX)

Question 17

Limitation on Reverse thrust

Answer 17

Intentional selection of reverse thrust in flight is prohibited.

Question 18

APU Max Altitude for OPeration

Answer 18

41000 FT

Question 19

APU Max Altitude electric only

Answer 19

41000 FT

Question 20

APU Max altitude bleed air only

Answer 20

17000 FT

Question 21

APU max altitude for bleed and electric

Answer 21

10000 FT

Question 22

Do not extend flaps above _____ ft pressure altitude

Answer 22

20,000 FT

Question 23

Alternate flap duty cycle limitation

Answer 23

Alternate flap duty cycle in flight is one complete cycle, then 5 minutes off. A complete cycle is movement from position 0 to 15 and back to 0. The ALTERNATE FLAP position switch must be in the OFF position for 15 seconds before reversing the direction of flap movement.

Question 24

In flight, do not extend the speedbrake lever beyond the______

Answer 24

flight detent

Question 25

Do not use speedbrakes in flight below _____ AGL

Answer 25

1000 AGL

Question 26

In flight, do not use speed brake with flaps greater than __

Answer 26

10

Question 27

-700 W Speed Brake Wing Load Alleviation system limitation

Answer 27

Do not operate the aircraft at speeds in excess of 320 knots at weights over 143,000 lb if the speedbrake wing load alleviation system is inoperative.

Question 28

Max Fuel Tank Temperature

Answer 28

49 C

Question 29

Min fuel tank temperature

Answer 29

-37C
Note: Jet A freeze point is -40C and other listed fuels freeze at lower temperatures.

Question 30

Main tanks must be full if the center fuel tank quantity is greater than

Answer 30

1000 lbs.
NOTE: 1000 pounds may be retained in the center tank provided the effects of balance have been considered
NOTE: Center tank fuel pumps must be ON for all operations with more than 1000 pounds of fuel in the center tank
NOTE: some MEL items can override this limitation

Question 31

For ground operation, when may center tank fuel pump switches be positioned to ON?

Answer 31

For ground operation, center tank fuel pump switches must not be positioned to ON unless the center tank fuel quantity exceeds 1000 lbs, except when defueling or transferring fuel.
NOTE: Fuel may be transferred from tank to tank or the aircraft may be defueled with Passengers onboard, provided the fuel quanityt in the tank from which fuel is being taken is maintained at not less than 2000 lb. Deplane all passengers and non-essential crew members when defueling a tank or transferring fuel from a tank that has a fuel quantity below 200 lb until the process has been completed and the respective fuel boost pumps are turned off.

Question 32

Corresponding center tank fuel pump switch must be positioned to OFF when?

Answer 32

Corresponding center tank fuel pump switch must be positioned to OFF when a center tank LOW PRESSURE light illuminates.

NOTE: When on the ground, if the center tank fuel pump LOW PRESSURE light illuminates with useable fuel greater than 1000 lbs in the center tank, refer to 16.12.6 Center Tank Fuel Pump LOW PRESSURE light illuminated on the ground

NOTE: When established in level flight attitude, both center tank pump switches should be positioned ON again if the center tank contains useable fuel.

NOTE: If the center tank is empty, both center tank fuel pump switches must be positioned OFF when the first center tank fuel pump LOW PRESSURE light illuminates.

Question 33

Center tank fuel pumps must not be ON unless personnel are available on the flight deck to do what?

Answer 33

Center tank fuel pumps must not be ON unless personnel are available on the flight deck to monitor the low pressure lights.

Question 34

Can flight deck crews reset a tripped fuel CB?

Answer 34

Flight Deck Crews must not reset tripped fuel quantity indicator, fuel pump, or fuel pump control circuit breakers.

Question 35

Cargo Bay Fire Suppression Limitation

Answer 35

Aircraft must land within 60 minutes (8E and MAX8E: 180 minutes) of initial discharge of the fire suppression system.

Question 36

TCAS: What must flight crews do when they get a TA or RA?

Answer 36

Flight crews must immediately respond to TCAS information (both TAs and RAs) by using the TCAS (traffic avoidance) guidelines located in AOM Chapter 5. 18 Non normal maneuvers

Question 37

TCAS: pilot authorizations

Answer 37

Pilots are authorized to deviate from an ATC clearance to the extent necessary to complete with the TCAS II Resolution Advisory