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CAE Phenom 300E1
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66
Aviation
Professional
10/07/2021
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Term
Max Ramp
Weight
(MRW)
 Definition
18,617 lbs
Term
Max Takeoff
Weight
(MTOW)
 Definition
18,551 lbs
Term
Max Landing
Weight
(MLW)
 Definition
17,272 lbs
Term
Max
Zero-fuel
Weight
(MZFW)
 Definition
14,263 lbs
Term
LANDING GEAR OPERATION/EXTENDED SPEED
(VLO & VLE)
Maximum speed at which the Landing Gear can be safely
extended & retracted (VLO):_______
Maximum speed at which the airplane can be flown with
the Landing Gear extended & locked (VLE):_______
 Definition
Maximum speed at which the Landing Gear can be safely
extended & retracted (VLO):250 KIAS
Maximum speed at which the airplane can be flown with
the Landing Gear extended & locked (VLE):250 KIAS
Term
Minimum Control Speed (VMC) for takeoff
(takeoff flaps):
 Definition
99 KIAS
Term
Minimum Control Speed (VMC) for landing
(landing flaps) in ‘No Icing Conditions’:
 Definition
99 KIAS
Term
Operating Maneuvering Speed (VO):
 Definition
205 KIAS
Term
MAXIMUM FLAP EXTENDED SPEED (VFE)
Flap 1 ..................................................................________
Flap 2..................................................................________
Flap 3..................................................................________
Flap Full..............................................................________
 Definition
Flap 1 ...................................................................180 KIAS
Flap 2 ..................................................................170 KIAS
Flap 3 ..................................................................170 KIAS
Flap Full ..............................................................160 KIAS
Term
Maximum altitude with extended Flaps:
 Definition
18,000 ft
Term
Maximum Tire Ground Speed:
 Definition
182 Kts
Term
Runway slope..................................................._________
Type of runway surface ...................................._________
 Definition
Runway slope..................................................-2% to +2%
Type of runway surface ..................................... Paved
Term
Load Factor Limit (G loads) with Flaps UP:
 Definition
3.00 g
Term
Load Factor Limit (G loads) with Flaps DOWN (1, 2, 3 &
FULL):
 Definition
2.00 g
Term
Maximum loading:
LH Forward Cabinet ......................................................................_______
Lavatory Cabinet ..........................................................................._______
Aft Baggage Compartment............................................................_______
Forward Baggage Compartment ..................................................._______
Refreshment Center......................................................................_______
Side-Facing Divan Stowage Compartments..................................______
 Definition
LH Forward Cabinet .............................................................. 44 Lb (20 Kg)
Lavatory Cabinet ................................................................... 33 Lb (15 Kg)
Aft Baggage Compartment................................................ 463 Lb (210 Kg)
Forward Baggage Compartment ......................................... 110 Lb (50 Kg)
Refreshment Center.............................................................. 71 Lb (32 Kg)
Side-Facing Divan Stowage Compartments....................... 36 Lb (16.5 Kg)
Term
Max takeoff and landing tailwind
component.........................................................
Max crosswind component allowed
to apply static takeoff power ..............................
 Definition
Max takeoff and landing tailwind
component......................................................... 10 KTS
Max crosswind component allowed
to apply static takeoff power .............................. 18 KTS
Term
Hydraulic System Accumulator pre-charge check interval:
 Definition
15 consecutive calendar days or before the
next flight, whichever occurs last
Term
Stall Warning and Protection System must be tested:
 Definition
Prior to each flight
Term
What are the prohibitions associated with the use of the
SVS?
 Definition
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.
Term
Minimum battery voltage required for engine start:
 Definition
24 V
Term
Minimum GPU voltage required for battery charging:
 Definition
27 V
Term
Maximum generator load on Ground:
 Definition
330 Amps each
Term
Maximum generator load in Flight:
 Definition
390 Amps each
Term
Maximum usable fuel quantity per tank:
 Definition
2702 lbs
Term
Unusable fuel quantity per tank:
 Definition
24.2 lbs
Term
Maximum fuel capacity:
 Definition
5427.6 lbs
Term
Maximum permitted imbalance between tanks:
 Definition
220 lbs
Term
Minimum Fuel Tank Temperature:
 Definition
–37°C
Term
Maximum Fuel Tank Temperature (on Ground):
 Definition
52°C
NOTE: MAXIMUM FUEL TEMP CAN BE EXCEEDED UP TO 80°C
IN FLIGHT
Term
Position Of ‘XFEED’ Knob during Takeoff & Landing:
 Definition
′OFF′
Term
Max Thrust
 Definition
10 minutes 725 °C
Term
Takeoff
Thrust
 Definition
5 minutes 700 °C
Term
Maximum
Continuous
 Definition
680 °C
Term
Maximum
Climb
 Definition
680 °C
Term
Ground Idle
 Definition
Min 55.1 (OEI)
Min 51.2 (AEO)
Term
Flight Idle
 Definition
55.1
Term
Starting
 Definition
5
seconds 765 °C
Term
Transient
 Definition
20 seconds 765 °C
Term
MOTORING ATTEMPT 1,2,3,4
 Definition
1st 60 seconds
2nd 60 seconds
3rd 15 minutes
4th 30 minutes
Term
For air conditioning system operation on ground_______.
 Definition
For air conditioning system operation on ground the GPU
must be used or one engine generator must be turned ON
Term
Maximum Differential Pressure ........................... PSI
Maximum Differential Overpressure......................PSI
Maximum Differential Negative Pressure ............... PSI
Maximum Differential Pressure for Takeoff and Landing ............................ PSI
 Definition
Maximum Differential Pressure ......................9.4 PSI
Maximum Differential Overpressure.................9.6 PSI
Maximum Differential Negative Pressure ............. -0.3 PSI
Maximum Differential Pressure for Takeoff and Landing .......................0.2 PSI
Term
When must the crew activate the Ice Protection System?
 Definition
Crew must activate the ice protection system when icing
conditions exist or are anticipated, as per Section 3, Normal
Procedures.
Term
Define: ”when icing conditions exist or are anticipated”?
 Definition
Icing conditions may exist whenever;
1) The Static Air Temperature (SAT) on the ground or for takeoff, or
Total Air Temperature (TAT) in flight, is 10°C or below and visible
moisture in any form is present (such as clouds, fog with visibility of
one mile or less, rain, snow, sleet or ice crystals).
2) SAT on the ground is 10°C or below and ramps, taxiways, or
runways are contaminated with surface snow, ice, standing water,
or slush.
Term
Maximum Takeoff and Landing Altitude Icing conditions ........ft

Min Airspeed (flap/gear up):
Wing and Stabilizer Anti-Ice System Inhibited...............KIAS

Wing and Stabilizer Anti-Ice System Armed..................KIAS

Wing and Stabilizer Anti-Ice System Uninhibited ...........KIAS
 Definition
Maximum Takeoff and Landing Altitude .....................10,000 ft

Min Airspeed (flap/gear up):
Wing and Stabilizer Anti-Ice System Inhibited.........170 KIAS

Wing and Stabilizer Anti-Ice System Armed............170 KIAS

Wing and Stabilizer Anti-Ice System Uninhibited ....155 KIAS
Term
What is the limitation regarding contaminated aircraft
surfaces?
 Definition
Takeoff is prohibited with frost (polished or not), ice, snow or slush adhering to the wings, control surfaces, engine inlets or other critical surfaces.
Term
In what environmental condition is flight prohibited?
 Definition
- Flight in freezing drizzle or freezing rain is prohibited.
- The pilot must immediately exit the freezing rain or
freezing drizzle conditions by changing altitude or course.
Term
What are the limitations regarding use of the Autopilot in
icing conditions?
 Definition
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.
Term
When must the Wing Inspection Light be operative?
 Definition
Prior to flight into known or forecast icing conditions,
at night.
Term
Minimum Engagement Height (dual engine)..................ft AGL
Minimum Engagement Height (single engine)................ft AGL
Minimum Use Height (dual engine)..........................ft AGL
Minimum Use Height (single engine)..........................ft AGL
Altitude Loss (maneuvering/cruise)..................................ft
Yaw Damper OFF airspeed is limited to if in icing conditions
 Definition
Minimum Engagement Height (dual engine)............600 ft AGL

Minimum Engagement Height (single engine)........1000 ft AGL

Minimum Use Height (dual engine)...................195 ft AGL

Minimum Use Height (single engine)...................220 ft AGL

Altitude Loss (maneuvering/cruise)............................160 ft
Yaw Damper OFF airspeed is limited to 180 KIAS if in icing conditions
Term
SMOKE/FIRE/FUMES
(FAA & ANAC)
 Definition
1. Oxygen Masks. . . DON, EMER
(then 100% after 2 minutes)
2. Dilution Valve. . . . . .CLOSED
3. Smoke Goggles. . . . . . . DON
4. Communication. . .ESTABLISH
5. DUMP Button. . . . . . PUSH IN
LAND AS SOON AS POSSIBLE
Term
SMOKE EVACUATION
(FAA & ANAC)
 Definition
1. Oxygen Masks . . .DON, EMER
(then 100% after 2 minutes)
2. Dilution Valve. . . . . .CLOSED
3. Smoke Goggles. . . . . . . DON
4. Communication. . ESTABLISH
5. Oxygen Knob. . . CREW ONLY
6. DUMP Button. . . . . . PUSH IN
7. ECS Knob. . . . . . . .OFF VENT
LAND AS SOON AS POSSIBLE
Term
DUAL ENGINE FAILURE
 Definition
1. Thrust Levers. . . . . . . . IDLE
2. Oxygen Masks. . .DON, 100%
3. Communication. . ESTABLISH
LAND AS SOON AS POSSIBLE
Term
EMERGENCY DESCENT
 Definition
1. SIGNS/OUTLET Switch. . . . PED-BELTS/OFF
2. Altitude. . . . . . . . . . . . . . . . 10,000 FT OR MEA
WHICHEVER IS HIGHER
3. Thrust Levers. . . . . . . . IDLE
4. SPEED BRAKE Switch. . OPEN
5. Airspeed..MAX 250 KIAS/MMO
6. LDG GEAR Lever. . . . . . . DN
7. Transponder. . . . . . . . .7700
8. ATC. . . . . . . . . . . . .NOTIFY
Term
EMERGENCY EVACUATION
 Definition
1. Thrust Levers. . . . . . . . IDLE
2. Emer/Parking Brake. . . . . ON
3. START/STOP Knobs. . . .STOP
4. SHUTOFF 1 & 2 Buttons. . . . . PUSH IN
5. PRESN MODE Switch. . . MAN
6. DUMP Button. . . . . . PUSH IN
7. ATC. . . . . . . . . . . . . NOTIFY
8. Evacuation. . . . . . .PERFORM
9. BATT 1 & 2 Switches. . . .OFF
Term
ENGINE ABNORMAL START
 Definition
Affected Engine:
1. START/STOP Knob. . . . STOP
Term
ENGINE FIRE, SEVERE DAMAGE OR SEPARATION
 Definition
Affected Engine:

1. Thrust Lever. . . . . . . . .IDLE
2. START/STOP Knob. . . . STOP
3. SHUTOFF Button. . . PUSH IN
*Wait 30 seconds*
If fire persists:
4. BOTTLE Switch. . . . . . DISCH
LAND AS SOON AS POSSIBLE
Term
CAB ALTITUDE HI
 Definition
1. Oxygen Masks. . DON, 100%
2. Communication. . ESTABLISH
3. SIGNS/OUTLET Switch. . . . . PED-BELTS/OFF
4. Altitude. . . . . . . . . . . . . . . . 10,000 FT OR MEA
WHICHEVER IS HIGHER
5. Thrust Levers. . . . . . . . IDLE
6. SPEED BRAKE Switch. . . . OPEN
7. Airspeed..MAX 250 KIAS/MMO
8. LDG GEAR Lever. . . . . . . DN
9. Transponder. . . . . . . . .7700
10. ATC. . . . . . . . . . . . NOTIFY
Term
ELEC EMERGENCY
 Definition
1. PRESN MODE Switch. . . MAN
2. CABIN ALT Switch. . . . . . . . HOLD DOWN FOR
10 SECONDS
If at or above 25,000 ft:
Rudder Pedals. . . . . . . . FIXED
If above 10,000 ft:
CAB ALTITUDE HI
Procedure (EAP2-3 ACCOMPLISH
Term
ELEC XFR FAIL
 Definition
1. ELEC EMER Button. . . . PUSH IN
LAND AS SOON AS POSSIBLE
Term
E1 (2) FIRE
 Definition
Affected Engine:
1. Thrust Lever. . . . . . . . IDLE
2. START/STOP Knob. . . . STOP
3. SHUTOFF Button. . . PUSH IN
On ground or if in the air fire Persists after 30 seconds in flight:
4. BOTTLE Switch. . . . . .DISCH
LAND AS SOON AS POSSIBLE
Term
TAKEOFF WITH ENGINE FAILURE AT OR ABOVE
V1
 Definition
At VR rotate the airplane according to the table below;
FLAP POSITION 1
PITCH ANGLE 10.5; FLAP POSITION 2 PITCH ANGLE 8
With Positive rate of climb:
1. LDG GEAR. . . . . . . . . . . .UP
2. Airspeed. . . . . . . . . . . . . V2
Term
REJECTED TAKEOFF
(AT OR BELOW V1)
 Definition
1. Thrust Levers. . . . . . . . IDLE
2. Brakes. . . . . . . . APPLY MAX
3. Directional Control. . . . . . . MAINTAIN
Term
WINDSHEAR
 Definition
1. Thrust Levers. . . . . . . . MAX
2. Autopilot. . . . . . DISENGAGE
3. Pitch Angle (nose up). . . 15°
Term
GEAR LEVER CAN NOT BE MOVED UP
 Definition
If associated with engine failure and obstacle clearance,
simultaneously proceed:
1. DN LCK REL Button. . .PRESS
2. LDG GEAR Lever. . . . . . . UP
Term
INADVERTENT PUSHER ACTUATION
(FAA & ANAC)
 Definition
1. QUICK DISCONNECT Button. . PRESS/HOLD
2. PUSHER CUTOUT Button. . . PUSH IN
Term
LG WOW SYS FAIL
 Definition
If associated with engine failure and obstacle clearance,
simultaneously proceed:
1. DN LCK REL Button. . . . . PRESS
2. LDG GEAR Lever. . . . . . . UP
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