Limitations

Question 1

Takeoff Weight Limiting Factors

Answer 1

Weight at brake release or start of T/O roll is limited by the most restrictive of the following:

• Maximum certificates takeoff weight
• Maximum runway limited takeoff weight
• Tire speed and break energy limits weights
• Maximum takeoff weight (climb limited)
• Obstacle clearance, enroute, and landing weight limitations

Question 2

Landing Weight Limiting Factors

Answer 2

The most restrictive of the following, incl. limitations for INOP EQP:

• Maximum certificated landing weight
• Maximum landing weight (runway length plus obstacle)
• Maximum landing weight (climb limited)

Question 3

Maximum Taxi & Ramp Weight

Answer 3

85,800

Question 4

Maximum Takeoff (MTOW) Weight

Answer 4

85,500

Question 5

Maximum Landing (MLW) Weight

Answer 5

74,900

Question 6

Maximum Zero Fuel (MZFW) Weight

Answer 6

69,800

Question 7

Maximum Forward Cargo (F1) Weight

Answer 7

3,306

Question 8

Maximum Aft Cargo (R1) Weight

Answer 8

2,535

Question 9

Note Overweight landing

Answer 9

Perform an “overweight landing” when a condition causes it to be safer to land overweight than to continue flight until at or below maximum certificated landing weight. QRH for procedure

Question 10

Winds and altitudes are predicated on what?

Answer 10

Peak gust value & pressure altitude

Question 11

Minimum Flight Crew

Answer 11

Pilot and Copilot

Question 12

Max crosswind for takeoff and landing (Dry)

Answer 12

35knot

Question 13

Max crosswind for takeoff and landing (Wet)

Answer 13

30knots

Question 14

Maximum headwind for CatII approaches

Answer 14

25knots

Question 15

Max crosswind for landing Vis

Answer 15

15kts

Question 16

Max tailwind for takeoff and landing

Answer 16

10kts

Question 17

Max runway slope

Answer 17

+2% , -2%

Question 18

Flap maneuvering load acceleration limit

Answer 18

Up -1 to +2.5

Down 0 to +2.0. (Flap 1 - Full)

Question 19

Max Operating Alt.

Answer 19

41,000

Question 20

Max takeoff and landing altitude

Answer 20

8,000

Question 21

Max SAT for takeoff, landing and ground start

Answer 21

52C

Question 22

Max altitude with flap extended

Answer 22

20,000

Question 23

Max flight operating altitude

Answer 23

78 North

78 South

Question 24

Min SAT for takeoff, landing and ground start

Answer 24

-40C

Note* In the event of landing below -40C, the airplane may not takeoff without further maintenance inspection.

Question 25

Minimum Operating Limit Speed.

Answer 25

Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation, is prohibited unless a lower speed is specifically authorized for flight test or training operations.

Question 26

Operational Envelope

Answer 26

In the event of a landing below -40C, the airplane may not takeoff without further maintenance inspection.

Question 27

Speed Limits WARNING

Answer 27

Maximum operating limits speeds(Vmo/Mmo) shall NOT be deliberately exceeded in any regime of flight.

Question 28

Vmo

Answer 28

320

Question 29

Mmo

Answer 29

.82

Question 30

Maximum airspeed for RAT ops.

Answer 30

Vmo/Mmo

Question 31

Turbulent airspeed below 10,000 feet

Answer 31

250kts

Question 32

Turbulent airspeed at or above 10,000feet

Answer 32

270kts/.76M

Question 33

Tire limit ground speed

Answer 33

195kts

Question 34

Max airspeed for windshield ops.

Answer 34

250kts.

Question 35

Max airspeed for windshield wiper ops failed in non-parked

Answer 35

320kts

Question 36

Max airspeed to open flight deck window

Answer 36

160kts

Question 37

Max gear extension speed Vlo

Answer 37

250kts

Question 38

Max gear extended speed Vle

Answer 38

250kts

Question 39

Max gear retraction speed Vlo

Answer 39

250kts

Question 40

Max flap 1

Answer 40

230kts

Question 41

Max flap 2

Answer 41

215kts

Question 42

Max flap 3

Answer 42

200kts

Question 43

Max flap 4

Answer 43

180kts

Question 44

Max flap 5

Answer 44

180kts

Question 45

Max flap Full

Answer 45

165kts

Question 46

Minimum Control Speed

Answer 46

Refer to QRH

Question 47

Designed Maneuvering Speed

Answer 47

Full application of rudder and aileron controls, as well as maneuvers that involve angles of attack near the stall, must be confined to speeds at or below 240kts