Limitations

Question 1

Max Flap Extension Altitude

Answer 1

20,000 Ft. Pressure altitude

Question 2

Speed Brake lever Limitation

Answer 2

Do not extend in flight beyond the flight detent

Question 3

Flight Control Limitations

Answer 3

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw as they ma result in structural failure at any speed, including below VA

Question 4

Holding in icing conditions

Answer 4

Prohibited with flaps extended

Question 5

Landing with Flaps 15

Answer 5

normal landings are prohibited, but only allowed when required by a non normal procedure.

Question 6

Maximum Take off EGT

Answer 6

950 degrees C

Question 7

Maximum Continuous EGT

Answer 7

925 degrees C

Question 8

Maximum Start EGT

Answer 8

725 degrees C

Question 9

Certified for what flaps settings for takeoffs

Answer 9

1, 5, 10, 15, and 25

Question 10

Maximum Take Off and Landing Tailwind Component

Answer 10

15 Knots

Question 11

Maximum speeds

Answer 11

Observe Vmo pointer and gear/flap placards

Question 12

Turbulent Airspeed

Answer 12

280 kias or .76m

Question 13

Maximum Operating Altitude

Answer 13

41,000 ft.

Question 14

Minimum Runway Width

Answer 14

98 feet or 30 meters

Question 15

Flight Deck Door Access System

Answer 15

Verify that an operational check of the flight deck door access system has been accomplished once each flight day

Question 16

Passenger Evacuation with one or more occupants in cabin

Answer 16

all entry door evacuation slide system must be armed and engagement of the girt bar with door sill verified prior to taxi, takeoff, or landing

Question 17

Passenger Evacuation with no occupants in cabin

Answer 17

only the two forward escape slide retantaion bars much be installed during taxi, takeoff, and landing

Question 18

prohibited Use of HF radios:

Answer 18

during refueling

Question 19

Cabin Altitude Briefing

Answer 19

First flight of the day or changes of flight crew members: PIC shall ensure the cabin altitude warning indications and procedures are briefed in accordance with SOP

Question 20

Engine Anti-Ice System use

Answer 20

On during all ground and flight operations when Icing Conditions exist or anticipated, except during climb and cruise when SAT is below -40 degrees c.

Must also be on prior to and during descent in icing conditions including temps. below -40 degrees c.

Question 21

Wing Anti-ice system use

Answer 21

Do not use Wing anti-ice as a sub. for ground deicing

Do not operate wing anti-ice on the ground when OAT is above 10 degrees C.

Question 22

Use of aileron trim

Answer 22

Prohibited with autopilot engaged

Question 23

Engage of the autopilot after takeoff

Answer 23

Prohibited below 400 ft. agl.

Question 24

Single channel operation during app., Autopilot shall not remain engaged below:

Answer 24

50 feet agl.

Question 25

Use of Thrust reverses is prohibited when:

Answer 25

in flight

Question 26

Reduced thrust procedures in prohibitive when:

Answer 26

Contaminated runway, anti skid inop., EEC is in alternate mode, prob. of windshear

Question 27

Deployment of the speed brakes in flight is prohibited:

Answer 27

at radio alt. less than 1,000 ft.

Question 28

Fuel Pump Circuit Breaker Limitation

Answer 28

Do not reset

Question 29

Maximum Fuel Temp.

Answer 29

49 degrees C

Question 30

Minimum fuel temp.

Answer 30

Fuel freeze point of the fuel being uses +3 degrees c or -43 degrees C which ever is higher

Question 31

The on position of the Center fuel pump switches must not be used for ground operation unless:

Answer 31

center tank fuel quantity exceeds 1000 pds. (453kgs.) except when defueling or transferring fuel.

Question 32

Center Fuel pump switches must not be on to fuel APU unless:

Answer 32

personnel are available in the flight deck to monitor low pressure lights

Question 33

Operation with assumed Temp. reduced takeoff is not permited:

Answer 33

when anti skid is inop

Question 34

APU Bleed Air and Electrical Load Limitations

Answer 34

APU Bleed + electrical load, maximum altitude is 10,000 ft

APU bleed, maximum altitude is 17,000 ft

APU electrical load, maximum altitude 41,000

Question 35

Do not use LVL CHG when?

Answer 35

on final approach below 1000ft. agl.