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1

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

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.

2

Maximum Continuous EGT

925º C

3

Flight Deck Door Access System

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

4

Use of aileron trim is prohibited when?

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

5

Passenger Evacuation

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.

6

Wing Anti-Ice System

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).

7

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

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

8

Maximum Takeoff EGT

950º C

9

[FLIGHT CONTROLS] Maximum flap extension altitude is

20,000 ft. pressure altitude

10

Do not operate HF radios...

during refueling

11

Do not engage the autopilot...

for takeoff below 400 feet AGL.

12

Takeoff Flaps Certification... 

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

13

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

prohibited

14

Maximum Start EGT

725º C

15

Turbulent airspeed

280 KIAS/.76M

16

[FUEL] Center tank fuel pumps must not be...

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

17

Reverse Thrust Limitation...

Intentional selection of reverse thrust in flight is prohibited.

18

Maximum speeds

Observe Vmo pointer and gear/flap placards

19

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

50 feet AGL

20

[FLIGHT CONTROLS] Flaps 15 normal landings are

prohibited.

 

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

21

Maximum Takeoff and Landing Tailwind Component

15 knots

22

Cabin Altitude Briefing

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

23

Maximum Operating Altitude

41,000 feet

24

[FLIGHT CONTROLS] Do not deploy the speedbrakes...

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

25

Engine Anti-Ice System

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

26

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

beyond the FLIGHT DETENT.

27

Vertical Situation Display

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

28

[FUEL] Do not reset...

a tripped fuel pump circuit breaker.

29

[FUEL] Minimum fuel temperature is

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

30

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

10,000 ft