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Phenom 300 > Phenom 300 Limitations -- Cat I > Flashcards

Phenom 300 Limitations -- Cat I Flashcards

1
Q

Landing Gear Operation/Extended Speed

Vlo
Vle

A

250 KIAS

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2
Q

Minimum Control Speed

Takeoff (Phenom 300 and 300E)
Landing (Icing and No Icing)

A

Takeoff
P300: 97 KIAS
P300E: 99 KIAS
Landing
Icing: 95 KIAS
No Icing: 91 KIAS

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3
Q

Operating Maneuvering Speed (Vo)

Operating Maneuvering Speed

A

205 KIAS

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4
Q

Maximum Flap Extended Speed (Vfe)

Flap 1
Flap 2
Flap 3
Flap 4

A

180 KAS
170 KIAS
170 KIAS
160 KIAS

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5
Q

Maximum Altitude for Flaps Extended

Maximum Altitude with Extended Flaps

A

18,000 feet

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6
Q

Maximum Tire Ground Speed

Maximum Tire Ground Speed

A

182 KIAS

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7
Q

Runway

Runway Slope
Type of Runway Surface

A

-2% to +2%
Paved

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8
Q

Load factor Limit (G Loads)

Flaps UP
Flaps DOWN (1, 2, 3 and FULL)

A

3.00 g
2.00 g

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9
Q

Wind Limitations

Max takeoff and landing tailwing
Max crosswind compenent allowed to apply static takeoff power

A

10 knots
18 knots

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10
Q

SB 505-29-005

For airplanes pre-mod SB 505-29-0005, the hydraulic system accumulator pre-charge check interval:

A

Every 15 days of before the next flight, whichever occurs last.

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11
Q

WARNING

Stall Warning and Protection System must be tested

A

Prior to each flight

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12
Q

Synthetic Vision System (SVS)

What are the prohibitions associated with the use of the SVS

A

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

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13
Q

Electrical

Minimum battery voltage required for engine start
Minimum GPU voltage required for battery charging
Maximum generator load on Ground
Maximum generator load in Flight

A

24 Volts
27 Volts
330 Amps each
390 Amps each

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14
Q

Fuel

Maximum permitted imbalance between tanks
Minimum Fuel Tank Temperature
Max Fuel Tank Temperature (Ground/Flight)
Position of ‘XFEED’ Knob during takeoff and landing

A

33 US Gal (220 lbs)
-37 degrees C
52 degrees C / 80 degrees C
Off

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15
Q

Starter Limits (Motoring Attempt)

1st
2nd
3rd
4th

A

60 second cool-down
60 second cool-down
15 minutes cool down
30 minutes cool down

Note: After four sequential motorings, cycle may be repeated following a 30 minute cool-down period.

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16
Q

Air Conditioning

For air conditioning system operation on ground:

A

The GPU must be used or one engine generator must be turned ON

17
Q

Pressurization

Maximum Differential Pressure
Maximum Differential Overpressure
Maximum Negative Pressure
Maximum Differential Pressure for Takeoff and Landing

A

9.4 PSI
9.6 PSI
-0.3 PSI
0.2 PSI

18
Q

Ice and rain Protection

When must the crew activate the Ice Protection System
Define “when icing conditions exist or are anticipated?”

A

Crew must activate the ice protection system when icing conditions exist or are anticipated as per Section 3, Normal Procedures.
Icing conditions may exist whenever:
1. The SAT on the ground or for takeoff, or TAT in flight, is 10 degrees C or below and visible moisture is any form is present.
2. SAT on the ground is 10 degrees C or below and ramps, taxiways, or runways are contaminated with surface snow, ice, standing water, or slush.

19
Q

Operation In Icing Conditions

Maximum Takeoff and Landing Altitude
Minimum Airspeed (flap and gear up):
* Wing and Stablizer Anti-Ice System Inhibited
* Wing and Stablizer Anti-Ice system Armed
* Wing and Stablizer Anti-Ice System Uninhibited

A

10,000 feet

165 KIAS
165 KIAS
150 KIAS

20
Q

Ice and Rain Protection

What is the limitation regarding contaminated aircraft surfaces?

A

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

21
Q

Ice and Rain Protection

In what environmental condition is flight prohibited?

A

Flight in freezing drizzle or freezing rain is prohibited.
The pilot must immediately exit the freezing rain or freezing drizzle conditions by changing altitue or course.

22
Q

Ice and Rain Protection

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

A

Autopilot use is prohibited in the following conditions:
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.

23
Q

Wing Inspection Light

When must the Wing Inspection Light be operative?

A

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

24
Q

Autopilot/Yaw Damper

Minimum Engagement Height (dual engine)
Minimum Engagement Height (single engine)
Minimum Use Height (dual engine)
Minimum Use Height (single engine)
Alitude Loss (maneuvering/cruise)

Yaw Damper OFF airspeed is limited to ____ if in icing conditions.

A

600 feet AGL
1,000 feet AGL
195 feet AGL
220 feet AGL
160 feet

180 KIAS

Phenom 300 (11 decks)

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