P300 Limitations

Question 1

Aircraft Weights

Max Ramp,
Max Takeoff,
Max Landing,
Max Zero Fuel

Answer 1

MRW 18497
MTOW 18387
MLW 17042
MZFW 14220

Question 2

MAX Landing Gear Extension (VLO)

Answer 2

250 kts

Question 3

Max speed at which the airplane can be flown with Landing Gear extended and locked. (VLE)

Answer 3

250 kts

Question 4

Min Control Speed (VMC) for takeoff (takeoff flaps).

Answer 4

97 kts

Question 5

VMC Landing - No Icing Conditions

Answer 5

91 kts

Question 6

VMC Landing - Icing Conditions

Answer 6

95 kts

Question 7

Operating Maneuvering Speed (Vo)

Answer 7

205 kts

Question 8

Max Flaps Extended Speed.

Flap 1,2,3,FF

Answer 8

F1 - 180 kts, F2 - 170 kts, F3 - 170 kts, FF - 160 kts

Question 9

Max altitude with flaps extended.

Answer 9

18,000 ft

Question 10

Max Tire Groundspeed

Answer 10

182 kts

Question 11

Runway Slope:

Type of runway surface:

Answer 11

-2 to +2 percent

Paved

Question 12

Load Factor Limit with Flaps UP

Answer 12

3.00 g

Question 13

Load Factor Limit with Flaps DOWN (1,2,3, FF)

Answer 13

2.00 g

Question 14

Baggage Loading:

Forward,
LH Forward,
Side Facing Divan,
Refreshment Center,
LAV Cabinet,
AFT Baggage

Answer 14

FB 110
LH CAB 44
Side Divan 36
Refreshment 71
LAV 33
AFT 463

Question 15

Max takeoff and landing tailwind

Max Crosswind component to apply static takeoff power

Answer 15

10 kt tailwind

18 kt crosswind

Question 16

Hydraulic system pre-charge check interval

Answer 16

15 consecutive calendar days or before next flight, which ever occurs last

Question 17

Stall Warning and Protection System must be tested:

Answer 17

Prior to each flight

Question 18

Prohibitions associated with the use of the SVS

Answer 18

Use of SVS as primary information to base decisions and/or plan maneuvers, to navigate or to avoid terrain, obstacles, or traffic is prohibited.

Question 19

Min battery voltage for engine start

Answer 19

24 V

Question 20

Min GPU voltage required for battery charging

Answer 20

27 V

Question 21

Max generator load on Ground

Answer 21

330 Amps each

Question 22

Max generator load in Flight

Answer 22

390 Amps each

Question 23

Max usable fuel quantity per tank

Answer 23

2676 lbs

Question 24

Unusable fuel quantity per tank

Answer 24

25.13 lbs

Question 25

Max fuel capacity

Answer 25

5401 lbs

Question 26

Max permitted imbalance between tanks

Answer 26

220 lbs

Question 27

Min fuel tank temperature

Answer 27

-37 C

Question 28

Max fuel temperature on ground

Answer 28

52 C note: Max fuel temp can be exceeded up to 80 C in flight

Question 29

Position of XFEED knob during Takeoff and Landing

Answer 29

OFF

Question 30

Operating Limits MAX Thrust

Answer 30

TL 10 min Max ITT 725 N1 100 N2 101 Oil Press 45 to 160 Oil Temp 10 to 132.2

Question 31

Operating Limits Takeoff

Answer 31

TL 5 min ITT 700 N1 100 N2 101 Oil Press 45 to 160 Oil Temp 10 to 132.2

Question 32

Operating Limit Max Continuous

Answer 32

TL na ITT 680 N1 100 N2 101 Oil Press 45 to 160 Oil Temp 10 to 132.2

Question 33

Operating Limit Max Climb

Answer 33

TL na ITT 680 N1 100 N2 101 Oil Press 45 to 160 Oil Temp 10 to 132.2

Question 34

Operating Limit Ground Idle

Answer 34

TL na ITT na N1 - N2 min 55.1 (OEI) 51.2 (AEO) Oil Press 25 to 160 Oil Temp. -40 to 132.2

Question 35

Operating Limit Flight Idle

Answer 35

TL na ITT na N1 - N2 55.1 Oil Press 25 to 160 Oil Temp -

Question 36

Operating Limit Starting

Answer 36

TL 5 sec ITT 765 N1 - N2 - Oil Press - Oil Temp -40 min

Question 37

Operating Limits Transient 20 Seconds

Answer 37

TL 20 sec ITT 765 N1 102 N2 103 Oil Press 0-20 Oil Temp -

Question 38

Operating Limits Transient 200 Seconds

Answer 38

TL 200 seconds ITT - N1 - N2 - Oil Press - Oil Temp 140.5 max

Question 39

Operating Limits Transient 400 Seconds

Answer 39

TL - N1 - N2 - Oil Press 20-270 Oil Temp -

Question 40

Starter Limits

Answer 40

1st 60 sec 2nd 60 sec 3rd 15 min 4th 30 min Note: After fourth sequential motoring, cycle may be repeated following a 30 minute cool-down period.

Question 41

Air Conditioning operation on the ground

Answer 41

GPU must be used or ONE engine generator must be turned on.

Question 42

Pressurization: Max Diff, Max Diff Overpressure, Max Negative Pressure, Max Diff for TO and Landing

Answer 42

Max Diff 9.4 psi Max Over 9.6 psi Max Neg -0.3 psi Max TO/Land 0.2 psi

Question 43

Ice and Rain Protection When must the crew activate the Ice Protection System

Answer 43

When icing conditions exist or are anticipated. As per Section 3, Normal Procedures

Question 44

Operation in Icing Conditions: Max TO and Land Altitude Min Airspeed (flap and gear up): Wing and Stab Anti-Ice inhibited Wing and Stab Anti-Ice armed Wing and Stab Anti-Ice Uninhibited

Answer 44

10000 ft 165 kias 165 kias 150 kias

Question 45

Wing Inspection Light When must the Wing Inspection Light be operative

Answer 45

Prior to flight into known or forecast Icing conditions at night.

Question 46

Auto Pilot / Yaw Damper Min Engagement Height (Dual Engine) (Single Engine)

Answer 46

600 ft AGL 1000 ft AGL

Question 47

Auto Pilot / Yaw Damper Min Use Height (Dual Engine) Min Use Height (Single Engine)

Answer 47

195 ft AGL 220 ft AGL

Question 48

Autopilot / Yaw Damper Altitude Loss (maneuvering / cruise) Yaw Damper OFF is limited to XXX kts if in Icing conditions.

Answer 48

160 ft 180 kias

Question 49

Define: When icing conditions exist or are anticipated

Answer 49

SAT on ground or takeoff or TAT in flight is 10C or below and visible moisture in any form is present (clouds, fog, vis 1 mile or less, rain, snow, sleet or ice crystals) SAT on ground 10C or below and ramps, taxiways are contaminated with snow, ice, standing water, or slush

Question 50

What is the limitation regarding contaminated surfaces

Answer 50

Takeoff prohibited with frost, ice, snow, slush adhering to wings, control surfaces, engine inlets, or other critical surfaces

Question 51

In what environmental condition is flight prohibited

Answer 51

Freezing rain or drizzle Pilot must immediately exit the freezing rain or freeze drizzle conditions by changing altitude or course

Question 52

What are the limitations regarding use of the Autopilot in icing conditions

Answer 52

Autopilot use is prohibited in the following conditions Severe icing Unusual control force or control deflection or unusually large control forces to move flight controls when autopilot is disconnected Indications of frequent autopilot re-trimming during straight and level flight