What will automatically happen to the other GDUs (Garmin Display Units) when/if PFD 1 Fails?
The MFD goes to PFD Reversionary Mode
PFD 2 remains the same
What will automatically happen to the other GDUs (Garmin Display Units) when/if the MFD fails?
PFD 1 & 2 goes to PFD Reversionary Mode
What will automatically happen to the other GDUs (Garmin Display Units) when/if PFD 2 fails?
PFD 1 remains unchanged
MFD remains unchanged
What is the Length, width, and height of the Phenom 100?
Length = 41' 8.4"
Width = 40' 4.3"
Height = 14' 2.6"
The AC outlet system supplies _ VAC from the Airplanes _ VDC to be used by the pax to operate a Laptop of other PED?
110 VAC
28 VDC
The static inverter is powered by the _ _ _ _ and is protected by a _ _?
28 VDC Shed Bus
Circuit Breaker
How does the static inverter protect itself if the current exceeds the predetermined value?
It has an Internal Ground Fault Circuit Interrupter (GFCI)
What is the max allowable wattage for the AC Outlets?
100W
How is the main cabin door locked to the fuselage?
By 8 latch pins (it is not a plug-in type like the emergency door)
What is provided to ensure the main cabin door is secured in the locked position?
Eight green latch indicators
Two green lock indicators
How many micro-switches are incorporated into the:
- Forward Baggage Door?
- Aft Baggage Door?
2 on the forward baggage door
1 on the aft baggage door
Door warning is provided for _, _, & _, by microswitch signals processed by the _ system.
What indications do we get in the cockpit if a door is not secured properly for takeoff?
Main Door, Emergency Door, and Baggage Door
We get both a CAS Message and a graphical representation on the system status page
Describe the Phenom 100's waste system.
The waste system consists primarily of a Recirculating Toilet Assembly (RTA) which collects and stores human wastes in a removable self-contained tank.
It is powered by the Shed Bus
What emergency equipment does our aircraft have?
Portable Fire Extinguisher
Flashlight
First Aid Kit
Water Barrier
Passenger Oxygen Maskes
Life Vest
Emergency Locator Transmitter (ELT)
Manual actuation of the outflow valve is possible only with the pressurization mode switch set to _ position, and manually opens the outflow valve to increase/decrease the cabin altitude at approximately _FPM.
MAN
300'
What does the RED X on the Cabin ALT, RATE, DELTA P, or LFE window on the MFD indicate?
Invalid, out of range, or failed
If the Air Shutoff Valve is/has
-Closed
-Open Pressurized
-Open Unpressurized
-Failed Closed
-Failed Open
what would be the indication on the environmental control system synoptic page?
Closed- white circle and white line perpendicular to the flow line
Open Press.- Green circle and green line aligned with the flow line
Open Unpress.- White circle and white line and no bleed air available
Failed Closed- white circle and white line perpendicular to theflow line covered by a yellow X
Failed Open- green circle and green line aligned with the flow line covered by a yellow X
The cockpit/cabin temperature indications are digital and settable and are colored as follows on the environmental control system synoptic page?:
Green- for actual temperature
Cyan- for set temperature
Red X- invalid, out of range, or failed
On the environmental control system synoptic page what colors/symbols indicate on, off, and failed for the evaporator/recirculation fans?
On- green circle/green windmill
Off- white circle and white windmill
Failed- yellow X covering the circle/windmill
On the environmental control system synoptic page what is indicated by a green or white ECS Flow Line?
Green- the associated flow line is pressurized
White- the associated flow line in not pressurized
On the environmental control system synoptic page the Ram Air S/O Valve is shown as a triangle linked with a flow line inside the green circle, what does Green, White or the Yellow X covering the triangle mean?
Green- Normal valve operation in flight. Open (connected to the cabin/cockpit) or closed (connected to the heat exchanger).
White- valve commanded open on ground (abnormal)
Failed
How is the Outflow Valve position indicated on the environmental control system synoptic page?
Green pointer and the words "Open" (OFV at 90 degrees); "intermediate" (OFV at any position between 90 degrees and 0 degrees); "Closed" (OFV is fully closed 0 degrees) *during ground ops only*
How is bleed line pressure indicated on the environmental synoptic page?
Boxed on right side with green numbers to indicate normal operating range or yellow dashed to indicate invalid or value out of displayable range.
How is the heat exchange status is indicated on the environmental synoptic page?
On- Green rectangle with temperature reading
Off- White rectangle with temperature reading
How is the VCS shown on the environmental control system synoptic page?
On- green circle and green triangle
Off- white circle and white triangle
Failed- Yellow X covering the circle and triangle
How is the ground cooling fan shown on the environmental control system synoptic page?
-On
-Off
-Failed
On- Green circle with an internal green windmill
Off- White circle with a white windmill
Failed- Yellow X covering circle and windmill
The bleed system is control is performed by actuating the two bleed _?
PRSOV (pressure regulating shutoff valves) located in each nacelle
Can either flow path of bleed air, regulated by the independent PRSOVs supply enough bleed air for cabin pressurization?
Yes, this is a redundant system
What is bleed air used for in the Phenom 100?
Environmental Control System (ECS)
Wing and Stabilizer de-ice
Engine anti-ice
Door seal
What is the PRSOVs (pressure regulating s/o valve) function?
to regulate the hot bleed air released to the ECS at 25 PSIG and to provide a firewall shutoff capability for the bleed air lines.
What is the heat exchanger for?
To cool the bleed air either by ram air (in-flight) or the ground cooling fan (on the ground) prior to being delivered to the ECS
What happens to the PRSOV in the event of a single engine takeoff condition?
It is automatically closed
The Environmental Control System (ECS) provides temperature control for what?
Cockpit/Cabin
Cabin air recirculation
Conditioned air supply for gaspers
Fan air cooling for avionics
Emergency ram air ventilation for cockpit smoke clearance
Air temperature is controlled through?
Temperature Modulating Valves (TMVs) which mix cooled air from the heat exchangers with hot bleed air from the engines (PRSOVs)
How is the air flow regulated to maintain adequate and safe supply pressure at any engine operating condition?
By Flow Control Shutoff Valves (FCSOV)
When additional cooling is required, the environmental control system automatically operates the _?
VCS- vapor cycle air conditioning system
Describe the VCS.
The VCS has 2 evaporators (evaporators transfer the heat load generated in the a/c to the refrigerant) independently controlled and connected to a single compressor and condenser. The compressor module pumps the refrigerant to the condenser/heat exchanger pack where the energy contained in the fluid is dissipated through an indirect heat txfr with ram air. The fluid then passes through the evaporator monted expansion valves where it is vaporized, loses energy, and is directed to the evaporators. One evaporator is installed at the right side of the cockpit partition and another is installed in the cabin back side. The pack utilizes ram air to purge the heat from the VCS in the condenser and the excess heat from the engine bleed air-to-air heat exchanger and absorbs the excess heat of the engine air bleed.
Describe the function of the RAM- Air Ventilation system?
It supplies ram air to decrease bleed air temperature in the heat exchanger and can also supply fresh air to the cockpit and pax cabin in case of a loss of bleed air from both engines. (Fresh air on the ground can be attained by turning the bleeds to off)
Where do the:
-Passenger gaspers
-Pilot gaspers
get there air supply from?
Pilot- cockpit bleed line (right side)
Cabin- cabin bleed line (left side)
How is emergency ventilation accomplished?
Through an emergency ram air ventilation valve which is normally closed but can be commanded open when the Bleed knob is positioned to Off/Vent (both PRSOVs closed) in flight.
How is the outflow valve commanded to modulate airflow?
Through a dual channeled Electronic Control and Monitoring Unit (ECMU)
1 channel for auto mode the other is for manual pressurization control through the pressurization panel in the cockpit
During MFD reversionary mode is it possible to change the planned LFE?
No, the manual pressurization setting must be used
Does the VS mode have to be activated for the thumb wheel selector to become effective?
Yes
What does the CPL button do?
Alternates the pilot and copilot AFCS side as data source. A green arrowhead on the FMA indicates the respective source selected.
What does the quick disconnect button (The Big Red Button) disengage?
Autopilot
Yaw Damper
Trim
Pusher
Acknowledge and silence the autopilot disconnection alert and aural tone
What does the Control Wheel Steering Button allow?
Allows pilot to override the autopilot pitch and roll function with no effect to yaw damper or turn coordination until released.
What are some of the conditions that must be satisfied to make the autopilot available?
Flight Director is available
AFCS Control Unit is operational and communicating with the PFD 1 and/or MFD
Required AHRS parameters consumed by AP are valid and not miscompared
AP Servo monitors do not report failure
AP interface monitors do not report failure
GIA monitors do not report failure
AP related power-up tests completed successfully
Roll attitude is w/in +/- 45o
Pitch attitude is w/in +/- 25o
The autopilot engages when the AP pushbutton is pressed, if all of the following conditions are satisfied:
Autopilot is available
Automatic pitch trim is available
Normal Pitch Trim channel is selected
Pitch trim position is not asymmetric
Stall warning is not active
Any half of pilot or copilot manual trim switch is not active
Pilot or copilot Quick Disconnect switch is not pressed
Takeoff mode is not active, if airplane is on ground
What does the self-monitoring yaw servo provide?
Dutch roll damping
Turn coordination in response to yaw rate, roll angle, vertical acceleration, and airspeed
The Yaw Damper is available for engagement if all of the following conditions are satisfied:
AFCS Control Unit is operational and communicating with the PFD 1 and/or MFD
Required AHRS parameters consumed by YD are valid and not miscompared
YD servo monitors do not report failure
YD interface monitors do not report failure
GIA monitors do not report failure
YD related power-up tests completed successfully
Lateral acceleration is within +/- 0.25g
Yaw Damper engages when AP or YD pushbutton is pressed if all of the following conditions are satisfied:
Yaw Damper is available
Stall Warning is not active
Pilot or copilot Quick Disconnect switch is not pressed
Takeoff mode is not active if airplane is on ground
Transition from IAS to MACH occurs around what altitude?
Climb- 31500 or Mach .55
Descent- 30500 or IAS of 250
GP/GS mode are available when?
GP- is WAAS based glidepath available provided a GPS approach is loaded, CDI is on GPS, and APR button is pressed
GS- is available for LOC/ILS approaches provided the Localizer frequency is tuned, CDI is selected to LOC (green needles), and APR button is pressed
What is the roll angle limited to in Low Bank Mode?
15o
In HDG mode turns can be commanded more than 180o but less then 340o to continue a turn in the direction the bug was spun?
True
The VAPP mode provides greater sensitivity for signal tracking than VOR navigation Mode?