Eclipse EA500 PFD
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- COM,NAV, XPNDR
- pilot control of communication and navigation frequencies and X-ponder codes is provided through three PFD pages: --- --- ---- that are selectable through a rocker key below line select key five
- 50, 30, chevrons
- at extreme pitch angles greater then -- degrees up or -- degrees nose down, a series of white -------- point toward the horizon
- HSI, MAIN, CHKLST, FMS, MAP , SYS, AUDIO
- there are (7) composite mode pages
- N1 tapes, ITT tapes, Fuel quantity digital display, left
- in composite mode engine information including (3) is shown on the ----- side of the PFD
- in composite mode the ---- page is displayed as the default page
- HSI
- Vyse, cyan
- Best single engine rate of climb speed is shown on the airspeed tape with ------ in white text next to a ---- tick mark.
- OPS, black
- after being entered on the --- page of the MFD Vr rotation speed is indicated by a ----- tick mark on the airspeed tape and is shown in an outline bubble where the Mach display appears
- sold, hollow
- the airspeed bug is ----- fi being used by the FD or AP to capture a preset speed. Once the speed is captured the bug becomes ------.
- keyboard
- The only way to exit composite mode is with the -------- .
- red, above
- the airspeed tape is displayed as a --- dashed line below the stall speed for the current configuration as long as the airspeed is ----- that speed
- using the keyboard, using the rocker key select "composite" at the lower left corner of the PFD (these selections only appear if the MFD fails)
- composite mode provides reversionary capability in the event of an MFD failure. It can be selected in 2 ways
- REF
- the recommended airspeed for approach to landing is shown on the AS tape as ----
- -1000 ft, 50,000 ft
- the altitude tape has a lower limit of --------- and an upper limit of -------
- red, red
- the airspeed tape appear as a --- dashed line below the stall speed in the current configuration. If the speed is reduced below the stall speed the airspeed tape and airspeed digital display turn ---.
- amber tick mark, 50, APPROACHING MINIMUMS
- the data block under the altitude tape shows an approach minimums display. The minimum value entered under the NAV frequency page is displayed and an ----- ---- ---- will appear on the alt tape. Within ------- ft of the minimum alt the following aural alert will be heard------ ------.
- 50, "MINIMUMS"
- An "approaching minimums" aural alert occurs within ----- ft of the selected altitude (MDA). A "------" call out occurs when the aircraft arrives at minimums.
- .450, .400
- The Mach display only appears when the Mach number is ----- or above. The display disappears when the Mach number decreases to ----.
- centers, TO, current aircraft HDG
- with a NAV frequency tuned, pressing the left conc knob ------- the CDI with a ----- indication. If a freq is not tuned then pressing the conc knob synchs the course sel arrow with ---- ------ -------.
- COM SOURCE, left switch panel
- In the event of a PFD failure, radio communication will be available only if the pilot selects the opposite PFD using the --- ----- switch on the ---- ------ -----.
- 15, 30
- the flight director provides +/- -- degrees of pitch and +/- -- degrees of roll
- MFD
- composite mode is used in the event of an ----- failure
- white, black, OPS
- the final approach speed is bugged with --- text next to a single ----- tick mark on the airpseed tape when the speed is entered on the --- page of the MFD
- 1000, APPROACHING SEL ALT
- within ------ ft of a selected altitude a -------- ----- ----- text appears inside the altitude preselect window
- magnetic north, 5kts
- The wind indicator shows wind direction relative to ---- -----, if the wind speed is less than ---kts, the arrow is removed and the value replaced with -----.
- enroute- 5nm, terminal- 1.0 nm, approach- 0.3 nm
- when the FMS is the current NAV source, full scale needle deflection is dependent upon NAV mode. What is each NAV mode and its associated FSD.
- NAV source, bearing pointer (RMI), VLOC1, VLOC2, GPS1, GPS2, OFF
- on tile 3, line select key 2 selects the secondary --- ------ for the ------- ------- and may be toggled between ---- ---- ----- ----.
- NAV source, VLOC1, VLOC2, GPS1, GPS2, OFF
- on tile 3, line select key 1 selects the primary ---- ----- and may be toggled between----- ---- ---- ----.
- OPS (operations)
- ROT and REF airspeed markings must be set on the --- page on the MFD prior to flight.
- +3000 ft/m and -3000 ft/m, 3000ft/m, green diamond
- the VSI displays vertical speed between ------- and -------. If the VS exceeds ------- ft/m the digital value of the VS will be shown. If the AP is in ALT CHG mode a ------- --------- will indicate the target VS.
- white, cyan (blue)
- best Vyse is indicated on the airspeed indicator with ----- text and a single ---- (color) tick marik
- 200, ALTITUDE DEVIATION
- For RVSM protection a deviation indicator is at the top of the altitude tape. If current altitude deviates +/- ---ft an amber -------- --------- text appears and an altitude aural alert sounds
- MFD, PFD, COM SOURCE
- In the event of a PFD failure all flight information will be available in 2 places: the standby indications on the --- and copilot ---. To assure radio communications, the pilot must select the opposite PFD using the --- ----- switch on the left switch panel.
- 28.00, 31.00
- The Baro set knob is restricted to a range of ------ in Hg to ----- in Hg
- T/O, LDG
- ---- on the airspeed tape indicates the maximum allowable speed with flaps extended in takeoff configuration. ------ indicates the maximum allowable speed with flaps extended in approach configuration.
- high, AM (airway marker)
- When an ILS/LOC frequency is not selected as the primary NAV source or an ILS/LOC approach is not loaded into the FMS, the marker beacon sensitivity is automatically set to ----- and the following signal is displayed -- in white text
- solid, solid
- the heading bug is ----- if being used by the AP/FD to capture a preset heading. Once captured the ------ bug remains ----- while in heading mode.
- COM, COM, 10
- the --- page is the default page on the PFD, all other pages will default to the --- page within -- seconds
- trim indicators, landing gear position, flap position, right
- in composite mode system information including (3) is shown on the ----- side of the PFD
- "overspeed" displayed in RED letters and on the airspeed tape with a red and black striped band with airspeed in red digits
- overspeed is displayed on the PFD as
- main, MAP, FMS, CKLST, SYS, AUDIO, TILE 4, LSK 5
- If the MFD fails and the PFD is put in composite mode, there are 2 selectable pages on the PFD using the lower left rocker switch. The ---- page is the default page. It shows 5 line selectable keys on the left side. These are: (5). CAS messages are displayed in the center of tile - . Acknowledgement of CAS messages is done with right line select key number - .
- morse code, Navaid identifier, numeric frequency
- The ACS automatically identifies the NAV frequency by listening to the ----- ---- identifier and comparing it to the navaid database. When the frequenc is identified, the ------ ---------- replaces the ------- ---------.
- in a window below the altimeter tape and as an amber horizontal line on the altimeter tape
- minimums are entered on the PFD NAV page in the minimums line select window using line select key 1, the minimums will also be displayed:
- ROT
- the recommended airspeed for pitch rotation is shown on the AS tape as -----
- airspeed indicator
- the upper and lower limits for each flap operating range are shown on the
- thumbwheel, ACP
- with the AP engaged vertical speed is changed by adjusting the pitch with the ---- ------ on the ---.
- weight off wheels
- ----- ----- ----- automatically transitions the transponder from GND or SBY to ALT mode
- 1000, APPROACHING SEL ALT, aural
- within --- ft of a pre-selected altitude, a white ----------- --- --- text appears inside the altitude pre-select window. this corresponds to the aproaching selected altitude ----- alert.
- 10, 2.5
- When a VOR is selected a full scale CDI deflection indicates a full scale deviation of -- degrees, whena localizer is selected as the primary navigation source a full scale CDI deflection indicates a deviation of --- degrees.
- red X
- if the pressure altitude is determined to be invalid, the PFD removes all altitude data including the scale, bug, numeric value, and trend vector. A " --- -" is displayed where the scale was.
- aircraft and engine system information
- when in composite mode the PFD has 2 additional tiles that show (2)
- remove altitude display and replace it with a red X
- if the PFD detects invalid pressure altitude data from the ADC, the PFD display will:
- red, red
- if Vmo or Mmo is exceeded the airspeed tape turns --- and the digital airspeed display turns ---.
- Vref, Vyse, Vrot, T/O, LDG (max speed with flap settings of either 1/2 or full)
- several V speeds are displayed on the airspeed tape (5)
- MFD
- If either or both PFD(s) is are in composite mode with the MFD working the system functions can no longer be controlled with the ---
- amber, needle and TO/FROM FLAG
- when the CDI exceeds full deflection the D bar turns -----. If the NAV signal is interrupted or is intermittant the ----- and --/---- flag disappear.
- solid red band, flap position, angle of attack, angle of attack rate of change
- stall warning will activate when airspeed reaches the ----- ----- ----- on the airspeed tape. Stall warning is a function of (3) and will change as the aircraft maneuvers
- black
- maximum T/O and LDG flap operatin speeds are indicated by a ----- tick mark on the airspeed tape
- 300 ft/min, 6
- the altimeter shows a trend tape when the altitude is changing at a rate above -------- . the trend vector displays the altitude ----- seconds in the future.