Memory Items (Full Deck)

Question 1

Aircraft Weights

Answer 1

Max Ramp – 18497
Max Takeoff – 18387
Max Landing – 17042
Max Zero-Fuel – 14220

Question 2

Landing Gear Operation/Landing Speed

Answer 2

250 KIAS

Question 3

Minimum Control Speed
(takeoff flaps)

Answer 3

P300/P300E – 97 KIAS
P300(E) – 99 KIAS
(second with PW535E1)

Question 4

Minimum Control Speed
(landing in “No Icing Conditions”

Answer 4

P300/P300E – 91 KIAS
P300E – 99 KIAS
(second with PW535E1)

Question 5

Minimum Control Speed
(landing in “Icing Conditions”

Answer 5

P300/P300E – 95 KIAS
P300E – 99 KIAS
(second with PW535E1)

Question 6

Operating Manuvering Speed (Vo)

Answer 6

205 KIAS

Question 7

Maximum Flap Extended Speeds (Vfe)

Answer 7

Flap 1 – 180 KIAS
Flap 2 –170 KIAS
Flap 3 – 170 KIAS
Flap 4 – 160 KIAS

Question 8

Maximum Altitude For Flaps Extended

Answer 8

18,000 feet

Question 9

Maximum Tire Ground Speed

Answer 9

182 KIAS

Question 10

Runway Limitations
Runway Slope
Type of Surface

Answer 10

Slope – -2% - +2%
Type – Paved only

Question 11

Load Factor Limit (G Loads) with Flaps UP

Answer 11

3.00 g

Question 12

Load Factor Limit (G Loads) with Flaps DOWN
(1, 2, 3, and FULL)

Answer 12

2.00 g

Question 13

Baggage Loading

Answer 13

LH FWD Cabinet – 44 lbs
Lav Cabinet – 33 lbs
AFT Baggage Compartment – 463 lbs
FWD Baggage Compartment – 110
Refreshment Center – 71 lbs
Side-Facing Divan Stowage – 36 lbs

Question 14

Max Takeoff and Landing Tailwind Component

Max X-wind component for static takeoff

Answer 14

10 knots

18 knots

Question 15

For airlines pre-mod SB 505-29-0005, the hydraulic system accumulator pre-charge check internal

Answer 15

Every 15 days or before the next flight, whichever occurs last

Question 16

Stall Warning and Protection System must be tested how often?

Answer 16

Prior to each flight

Question 17

What are the prohibitions associated with the use of the SVS?

Answer 17

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

Question 18

Minimum battery voltage required for engine start

Answer 18

24 volts

Question 19

Minimum GPU voltage required for battery charging

Answer 19

27 volts

Question 20

Maximum Generator Load
(on Ground)

Answer 20

330 AMPS each

Question 21

Maximum Generator Load
(in Flight)

Answer 21

390 AMPS each

Question 22

Max Usable Fuel Quantity Per Tank

Answer 22

P300/P300E – 399.4 gallons or 2,676 lbs

P300E – 403.1 gallons or 2702 lbs

Question 23

Unusable Fuel Quantity Per Tank

Answer 23

P300/P300E – 3.75 gallons or 25.13 lbs

P300E – 3.7 gallons or 24.2 lbs

Question 24

Maximum Fuel Capacity

Answer 24

P300/P300E – 806.2 gallons or 5,401 lbs

P300(E) – 813.6 gallons or 5,427.6 lbs

Question 25

Maximum Permitted Imbalance Between Tanks

Answer 25

33 gallons or 220 lbs

Question 26

Minimum Fuel Tank Temperature

Answer 26

-37 degrees C

Question 27

Maximum Fuel Tank Temperature (On Ground and In Flight)

Answer 27

52 degrees C 80 degrees C

Question 28

Position of 'XFEED' Knob during Takeoff and Landing

Answer 28

OFF

Question 29

Limitations for Max Thrust Takeoff Thrust

Answer 29

Max Thrust -- 10 min and 725 degrees C Takeoff Thrust -- 5 min and 700 degrees C

Question 30

Starter Limits

Answer 30

1st motoring -- 60 sec 2nd motoring -- 60 sec 3rd motoring -- 15 minutes 4th mototing -- 30 minutes

Question 31

Air Conditioning Limitation

Answer 31

For air conditioning system operation on ground, the GPU must be ON or one engine generator must be turned ON

Question 32

Pressurization Limitations

Answer 32

Max Diff -- 9.4 psi Max Diff Overpressure -- 9.6 psi Max Diff Neg Pressure -- -0.3 psi Max Diff Pressure for takeoff and landing -- 0.2 psi

Question 33

When must the crew activate the Ice Protection System

Answer 33

Crew must activate the ice protection system when iciing conditions exist or are anticipated, as per Section 3, Normal Procedures.

Question 34

Icing Conditions (definitions)

Answer 34

1. The SAT on GND or for takeoff, or TAT in flight, is 10 degrees C or below and visible moisture in any form is present (such as clouds, fog with visibility or one mile or less, rain, snow, sleet, or ice crystals) 2. SAT on the GND is 10 degrees C or below and ramps, taxiways, or runways are contaminted with surface snow, ice standing water, or slush

Question 35

Operations In Icing Conditions

Answer 35

Max Takeof and Landing Alt -- 10,000 feet Minimum Airspeed WHSAIS Inhibited -- 165 KIAS WHSAIS Armed -- 165 KIAS WHSAIS Uninhibited -- 150 KIAS

Question 36

What is the limitation regarding contaminated aircraft surfaces?

Answer 36

Takeoff is prohibited with frost (polished or not), ice, snow or slush adhering to wings, control surfaces, engine inlets, or other critical surfaces.

Question 37

In what environmental condition is flight prohibited?

Answer 37

* Flight in freezing drizzle or freezing rain is prohibited. * The pilot must immediately exit the freezing rain or freezing drizzle consitions by changing altitude or course.

Question 38

Autopilot use is prohibited in the following conditions:

Answer 38

1. Severe icing 2. Unusual control force or control deflection, or unusually large control forces to move flight controls when the autopilot is disconnected. 3. Indications of frequent autopilot re-trimming during straight and level flight.

Question 39

When must the Wing Inspection Light be operative?

Answer 39

Prior to flight into known or forecast icing consitions, at night.

Question 40

Autopilot/Yaw Damper

Answer 40

Min Engagement (AEO) -- 600 feet AGL Min Engagement (OEI) -- 1,000 feet AGL Min Use Height (AEO) -- 195 feet AGL Min Use Height (OEI) -- 220 feet AGL Altitude Loss (maneruvering/cruise) -- 160 feet Yaw Damp OFF airspeed is limited to 180 KIAS if in icing conditions.