Phenom 300 Limitations -- Cat I Flashcards
Landing Gear Operation/Extended Speed
Vlo
Vle
250 KIAS
Minimum Control Speed
Takeoff (Phenom 300 and 300E)
Landing (Icing and No Icing)
Takeoff
P300: 97 KIAS
P300E: 99 KIAS
Landing
Icing: 95 KIAS
No Icing: 91 KIAS
Operating Maneuvering Speed (Vo)
Operating Maneuvering Speed
205 KIAS
Maximum Flap Extended Speed (Vfe)
Flap 1
Flap 2
Flap 3
Flap 4
180 KAS
170 KIAS
170 KIAS
160 KIAS
Maximum Altitude for Flaps Extended
Maximum Altitude with Extended Flaps
18,000 feet
Maximum Tire Ground Speed
Maximum Tire Ground Speed
182 KIAS
Runway
Runway Slope
Type of Runway Surface
-2% to +2%
Paved
Load factor Limit (G Loads)
Flaps UP
Flaps DOWN (1, 2, 3 and FULL)
3.00 g
2.00 g
Wind Limitations
Max takeoff and landing tailwing
Max crosswind compenent allowed to apply static takeoff power
10 knots
18 knots
SB 505-29-005
For airplanes pre-mod SB 505-29-0005, the hydraulic system accumulator pre-charge check interval:
Every 15 days of before the next flight, whichever occurs last.
WARNING
Stall Warning and Protection System must be tested
Prior to each flight
Synthetic Vision System (SVS)
What are the prohibitions associated with the use of the SVS
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.
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
24 Volts
27 Volts
330 Amps each
390 Amps each
Fuel
Maximum permitted imbalance between tanks
Minimum Fuel Tank Temperature
Max Fuel Tank Temperature (Ground/Flight)
Position of ‘XFEED’ Knob during takeoff and landing
33 US Gal (220 lbs)
-37 degrees C
52 degrees C / 80 degrees C
Off
Starter Limits (Motoring Attempt)
1st
2nd
3rd
4th
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.
Air Conditioning
For air conditioning system operation on ground:
The GPU must be used or one engine generator must be turned ON
Pressurization
Maximum Differential Pressure
Maximum Differential Overpressure
Maximum Negative Pressure
Maximum Differential Pressure for Takeoff and Landing
9.4 PSI
9.6 PSI
-0.3 PSI
0.2 PSI
Ice and rain Protection
When must the crew activate the Ice Protection System
Define “when icing conditions exist or are anticipated?”
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.
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
10,000 feet
165 KIAS
165 KIAS
150 KIAS
Ice and Rain Protection
What is the limitation regarding contaminated aircraft surfaces?
Takeoff is prohibited with frost (polished or not), ice, snow or slush adhering to wings, control surfaces, engine inlets, or other critical surfaces.
Ice and Rain Protection
In what environmental condition is flight prohibited?
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.
Ice and Rain Protection
What are the limitations regarding use of the Autopilot in icing conditions?
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.
Wing Inspection Light
When must the Wing Inspection Light be operative?
Prior to flight into known or forecast icing conditions at night.
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.
600 feet AGL
1,000 feet AGL
195 feet AGL
220 feet AGL
160 feet
180 KIAS
