Limitations [Memory Items Only]

Question 1

[FLIGHT CONTROLS] Avoid rapid and large alternating control inputs, especially in combination with

Answer 1

Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g., large side slip angles) as they may result in structural failure at any speed, including below VA.

Question 2

Maximum Continuous EGT

Answer 2

925º C

Question 3

Flight Deck Door Access System

Answer 3

Verify that an operational check of the flight deck door access system has been accomplished according to approved procedures once each flight day.

Question 4

Use of aileron trim is prohibited when?

Answer 4

Use​ of​ aileron​ trim​ with​ autopilot engaged​ is prohibited.

Question 5

Passenger Evacuation

Answer 5

On flights with ONE OR MORE occupants in the cabin, all entry door evacuation slide systems must be armed and engagement of the girt bar with door sill verified prior to taxi, takeoff, or landing.

On flights with NO cabin occupants, only the two forward escape slide retention bars (girt bars) must be installed during taxi, takeoff, and landing.

Question 6

Wing Anti-Ice System

Answer 6

Do not use wing anti-ice as a substitute for ground deicing/anti-icing and inspection procedures that are necessary to comply with TEM Deicing manual procedures.

Do not operate wing anti-ice on the ground when the OAT is above 10°C (50°F).

Question 7

[FUEL] For ground operation, center tank fuel pump switches…

Answer 7

must not be positioned to “ON” unless the center tank fuel quantity exceeds 1000 pounds, except when defueling or transferring fuel.

Question 8

Maximum Takeoff EGT

Answer 8

950º C

Question 9

[FLIGHT CONTROLS] Maximum flap extension altitude is

Answer 9

20,000 ft. pressure altitude

Question 10

Do not operate HF radios…

Answer 10

during refueling

Question 11

Do not engage the autopilot…

Answer 11

for takeoff below 400 feet AGL.

Question 12

Takeoff Flaps Certification…

Answer 12

Certified for flaps 1, 5, 10, 15 and 25 takeoffs.

Question 13

[FLIGHT CONTROLS] Holding in icing conditions with flaps extended is…

Answer 13

prohibited

Question 14

Maximum Start EGT

Answer 14

725º C

Question 15

Turbulent airspeed

Answer 15

280 KIAS/.76M

Question 16

[FUEL] Center tank fuel pumps must not be…

Answer 16

“ON” unless personnel are available in the flight deck to monitor low pressure lights.

Question 17

Reverse Thrust Limitation…

Answer 17

Intentional selection of reverse thrust in flight is prohibited.

Question 18

Maximum speeds

Answer 18

Observe Vmo pointer and gear/flap placards

Question 19

For single channel operation during approach, the autopilot shall not remain engaged below

Answer 19

50 feet AGL

Question 20

[FLIGHT CONTROLS] Flaps 15 normal landings are

Answer 20

prohibited.

A Flaps 15 landing may be performed when required by a non-normal procedure.

Question 21

Maximum Takeoff and Landing Tailwind Component

Answer 21

15 knots

Question 22

Cabin Altitude Briefing

Answer 22

As part of the takeoff briefing before engine start for the first flight of the day or following any change of either flightcrew member, the PIC shall ensure the Cabin Altitude Warning indications and procedures are briefed in accordance with normal procedures of this manual

Question 23

Maximum Operating Altitude

Answer 23

41,000 feet

Question 24

[FLIGHT CONTROLS] Do not deploy the speedbrakes…

Answer 24

in flight at radio altitudes less than 1,000 feet.

Question 25

Engine Anti-Ice System

Answer 25

The engine anti-ice system must be ON during all ground and flight operations when Icing Conditions exist or are anticipated, EXCEPT during climb and cruise when Static Air Temperature (SAT) is below -40°C.

Engine anti-ice must be on prior to and during descent in icing conditions, including temperatures below -40° SAT

Question 26

[FLIGHT CONTROLS] In flight, do not extend the SPEED BRAKE lever…

Answer 26

beyond the FLIGHT DETENT.

Question 27

Vertical Situation Display

Answer 27

When installed, all Non-ILS/Non-Precision Approaches, the PM must have the Vertical Situation Display (VSD) selected ON to enhance Ground/Terrain situational awareness

Question 28

[FUEL] Do not reset…

Answer 28

a tripped fuel pump circuit breaker.

Question 29

[FUEL] Minimum fuel temperature is

Answer 29

fuel freeze point of the fuel being used +3° C or –43° C, whichever is higher.

Question 30

[APU] With APU bleed + electrical load, maximum altitude is

Answer 30

10,000 ft

Question 31

[Reduced Thrust] Use of assumed temperature reduced thrust procedures is not allowed when:

Answer 31

• The runway is contaminated with standing water, ice, slush, or snow
• With anti-skid inoperative
• With EEC is in Alternate mode
• The probability of windshear exists

Question 32

[APU] With APU bleed, maximum altitude is

Answer 32

17,000 ft

Question 33

Minimum Runway Width

Answer 33

98 feet (30 meters)

Question 34

[APU] With APU electrical load, maximum altitude

Answer 34

41,000 ft

Question 35

[LANDING GEAR] Operation with assumed temperature reduced takeoff thrust…

Answer 35

is not permitted with anti-skid inoperative.

Question 36

Do not use LVL CHG on final approach below

Answer 36

1,000 feet AFE.

Question 37

[FUEL] Maximum fuel temperature is

Answer 37

49° C.