EASy II Update

Revision: 4Revision Date: 04/12/11

Dassault EASy CockpitEASy II Update

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The enclosed technical data is export classified as EAR99. Its export is being transmitted under U S Export Administrationexport is being transmitted under U.S. Export Administration

Regulations designation NLR (No License Required) and is to be used solely by the individual / organization to whom it is

addressed Diversion contrary to U S export laws and regulationsaddressed. Diversion contrary to U.S. export laws and regulations is prohibited.

HONEYWELL CONFIDENTIAL: This copyrighted work and all information are the property of Honeywell International Inc., contain trade secrets and may not, in whole or in part, be used, duplicated, or disclosed sec e s a d ay o , o e o pa , be used, dup ca ed, o d sc osed

for any purpose without prior written permission of Honeywell International Inc. All Rights Reserved.

Honeywell Proprietary2

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EASy II Retrofit vs In-Production AircraftEASy II Retrofit vs. In Production Aircraft

Future Falcons will be produced with EASy II baseline i i l tiavionics plus options

All in-service EASy aircraft can be upgraded to this basic avionics suite including options although packages are slightly different

Honeywell Proprietary

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EASy II Hardware & SoftwareSy a d a e & So t a e

Basic EASy II: EASy II Option 1: FMS v7.1 Take-off mode 2nd Electronic Checklist

WAAS GPS with LPV RNP AR < 0.3*

EASy II Option 2: Several Feature

Improvements WAAS GPS

y p ADS-B Out

EASy II Option 3 SmartViewTM

RNP 0.3 AR Capability AGM IIs Pentium M Processors

SmartView EASy II Option 4

Automatic Descent Mode EASy II Option 5 New MKB on F900 and

F2000 (same as F7X) SmartRunwayTM (RAAS)

( ti f F7X)

EASy II Option 5 Paperless Terminal Charts

EASy II Option 6XM W th


(option for F7X) XM Weather* Certification under discussion.

Basic EASy IIFMS v7.1 and Feature Improvements

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Basic EASy IIas c Sy

FMS v7.1 Enhancements: System Improvements: RF Legs Automated Holding to

Altitude (HA) Sequencing

Takeoff Mode (A/T arm on ground)

2nd Electronic Checklist Suffix-Type Approaches

include APPROACH annunciationBaro VNAV Temperature

Improved TOLD Features Quick Access to TAWS

settingsS Baro VNAV Temperature

Compensation Temp Comp Calculator LNAV on Go-Around

Minimums Set VOR CDI Course Set DME in tenths in ranges

greater than 10NM LNAV on Go-Around greater than 10NM Backup Tuning Directly to

NAV / COM Radios (follow-on cert for F900; included for


cert for F900; included for F7X & F2000)

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Automated HA sequencingAutomated HA sequencing

Issue HA legs are most common during SIDs where a holding pattern is

required to reach an altitude constraint. Currently the pilot has to perform a manual operation during a

procedure that contains an HA leg in order for FMS to sequence outprocedure that contains an HA leg in order for FMS to sequence out of holding and on to the next leg after altitude is reached.

Solution HA (Holding to Altitude) legs are handled in a manner similar to VA HA (Holding to Altitude) legs are handled in a manner similar to VA

legs If the aircraft has a current altitude that complies with the HA leg

altitude constraint, the holding pattern will be deleted automatically , g p yby the FMS resulting in a VA leg

An HA leg will sequence when the aircraft has achieved the HA altitude constraint


FMS will perform an immediate exit of the holding pattern

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Benefits: HA leg Auto SequencingBenefits: HA leg Auto Sequencing Implementation of this feature will enhance the automatic leg

sequencing ability of the FMS.


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Suffix-Type ApproachesSuffix Type Approaches

Multiple approaches with the same guidance (RNAV, LOC, t ) t th t t d ith l h b ti letc.) to the same runway are annotated with an alphabetical

suffix beginning at the end of the alphabet and working backwards for subsequent proceduresTh lti l t dd d t th i ti d t b These multiple types were added to the navigation database as they are defined and the FMS will provide these approaches for selection by the pilot

Previous application did not include correct coding so APPROACH annunciation did not appear Subsequently, various features such as Approach CDI scaling and

VGP wont activate with suffix-based approaches


Several approaches of same type can be available for same runway

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Suffix-Type ApproachesSuffix Type Approaches

APPROACH annunciation on PDU will now appearon PDU will now appear when suffix-type approach is activated

Localizer-based approaches are unaffected

See Honeywell SIL D200908000037


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Baro VNAV Temperature CompensationBaro VNAV Temperature Compensation

Old way was to manually compensate for each critical i t d i h d i d h ( d twaypoint during approach and missed approach (mandatory

in Canada)


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Baro VNAV Temperature CompensationBaro VNAV Temperature Compensation

When Temp Comp is activated by the pilot, all alt constraints i th d t h d i d hin the departure, approach, and missed approach are compensated

Purpose of this is to raise the alt constraint in cold weather

When the air is cold, it is condensed and the altimeter ,reading will be higher than the true altitude

Conversely in hot weather the uncompensated altitude willConversely, in hot weather, the uncompensated altitude will bring the aircraft higher then the published alt constraint


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Manual Baro VNAV Correction CapabilityManual Baro VNAV Correction Capability

FMS provides means for crew to calculate temp-crew to calculate tempcomp altitude to use as min altitude for approach

TEMP COMP selection is on the Landing Config tab of the FMWthe FMW FMS already knows elevation

& temp


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Manual Baro VNAV Correction CapabilityManual Baro VNAV Correction Capability

When activated, compensated altitudes arecompensated altitudes are shown in white & T Comp is shown in waypoint list

Use LNAV/VNAV as beforeUse LNAV/VNAV as before Chart limitation is no longer

applicable


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Temp Comp CalculatorTemp Comp Calculator

Enter an altitude in the Altitude box using the MKBAltitude box using the MKB or use the CCD knob

The Temp Comp Altitude is The Temp Comp Altitude is displayed

Th f th Altit d The range of the Altitude field is TDZE to 2,250

To close the Temp Comp Calculator, select the X

-


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Improved TOLD FeaturesImproved TOLD Features

Gust factor Failures Failures


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Take Off Mode EnhancementsTake Off Mode Enhancements

FD Guidance for all takeoff and go around phasesand go around phases

Same behavior with or without engine failure

TO mode selectable on TO mode selectable on ground

A/T can be armed on groundground Auto-engagement after

takeoff at 400 ft AGL if no engine failuree g e a u e

A/T stays on during go-around and goes to full power automatically EASy II


p y EASy II

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2nd Electronic Checklist2nd Electronic Checklist

For F900EX/F2000EX EASy Increased availability Synchronized to 1st checklist Already standard on F7Xy


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Back-up Tuning Directly to NAV and COM RadiosBack up Tuning Directly to NAV and COM Radios

Backup tuning of VHF1/2 is il bl i LH RH MKB iavailable using LH or RH MKB via

dedicated bus Used in case of failure of NIM or

ASCB bASCB bus

St 3


Step 3F900EX EASy / F2000EX

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Back-up Tuning Directly to NAV and COM RadiosBack up Tuning Directly to NAV and COM Radios

Backup tuning of VHF1/2 is il bl i LH RH MKBavailable using LH or RH MKB

via dedicated bus Used in case of failure of NIM or

ASCB bASCB bus

F7X & EAS IIF7X & EASy IIF900EX / F2000EX EASy


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Minimums SetMinimums Set

Mandatory entry

CAS message appears when gear is lowered if mins are not setmins are not set


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Tools TabTools Tab

Tools tab with calculator and Timer/Alarm functions


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QFE/QNH Calculator (Takeoff & Landing)QFE/QNH Calculator (Takeoff & Landing)


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VOR CDI Course SetVOR CDI Course Set

New setting of VOR CDI Course


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DME in tenths > 9 9 nmDME in tenths 9.9 nm


EASy II Options

SmartView SVS

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SmartView SVSSmartView SVS

Current PDU PDU with SmartView


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EASy II PDU vs SmartView PDUEASy II PDU vs SmartView PDU

EASy II Basic EASy II SVS (optional)


y

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SmartViewSmartView

Synthetic Vision (SV) Display / SmartView is aDisplay / SmartView is a Synthetic Vision Systems that overlays conformal HUD symbology on 3D y gyterrain driven by the Honeywell EGPWS terrain DB

Field of view in straight & level flight:g Vertical = 38 (2) Lateral = 33.7 (2)


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SmartViewSmartView

Increases pilot situational awareness by providing info on the surrounding terrain

Reduces runway incursions by providing info on departure/arrival runway (i.e. runway numbering)y ( y g)

Precise energy management information provided via the flight path marker and acceleration chevronchevron

Reduces potential loss of control by clearly indicating the pilot any unusual attitudes via specific symbologysymbology

Make training easier because of the information displayed is very intuitive and easy to use


SmartViewTM with On-side Radar

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INAV Field of ViewINAV Field of View

Field of View displayed on the SmartView isthe SmartView is depicted on INAV as two lines representing the lateral limits of the rendered terrain Near end of the field of view

lines represent nearest terrain visible on the SV display

Far end of the field of view lines represent the SV PDU view depthview depth


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How to turn off SmartViewHow to turn off SmartView

SmartView defaults to ON when aircraft is powered upwhen aircraft is powered up

To disable SmartView, de select the SV box fromde-select the SV box from the Data item in the PDU menu bar


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SmartView FeaturesSmartView Features

Advanced, performance-based HUD symbologybased HUD symbology

Flight path marker Conformal, color-coded

terrainterrain 3D terrain using EGPWS

databaseR D t ili Runway Detailing

Range Rings Grid Lines Runway Lead-In Line

(Extended Centerline)


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SmartView FeaturesSmartView Features

Water texturing Display of Obstacles Display of Obstacles Runway markings

centerline, runway numbering & realisticnumbering & realistic pavement

Unusual attitude de-clutter and fade outand fade-out


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Runway DetailingRunway Detailing

Runway Numbers and Centerline Display Displayed in white Runway numbers are displayed at both ends of runways Runway numbers that include letters are displayed with the letter

b l th bbelow the number Runway numbers approximate the appearance of actual runway

markingsR P t T t Runway Pavement Texture Displayed in dark gray Displayed such that motion is apparent when moving along the

runwayrunway


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Runway DetailingRunway Detailing

Runway detailing is only displayed on SmartViewdisplayed on SmartView when all of the following conditions are satisfied: Aircraft position is within 1 mile ofAircraft position is within 1 mile of

the runway Aircraft altitude is within 500 ft. of

the runway field elevation The difference between the

runway bearing and the aircraft viewpoint is 30 degrees or less

Th R d t ili f t The Runway detailing features fade into view as the aircraft approaches the runway


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Runway Outline & Extended CenterlineRunway Outline & Extended Centerline


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Runway Detailing (in flight)Runway Detailing (in flight)


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Runway Detailing (on ground)Runway Detailing (on ground)


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Range RingsRange Rings

Range ringsRange rings are positioned at Range rings are positioned at 3, 5, 10, 20, and 30 NM from the aircraft

Rings are labeled with gdistance from the aircraft to the left of the airspeed tape

Rings conform to the ground t d b hidd bcontour and can be hidden by

nearer, higher terrain Range rings declutter

automatically as at higherautomatically as at higher altitudes the closest ones (i.e. 3 or 5nm) are below the aircraft and not visible


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Grid LinesGrid Lines

Grid LinesDisplayed in black over the Displayed in black over the terrain depiction

Grid lines are very subtle in order to attract attention to them only when the pilot is looking at them

Depict approximate th/ th t/ t idnorth/south, east/west grid

Spaced at 0.4 nautical mile distances along both axesTranslate and rotate with the Translate and rotate with the terrain

Follow the contour of the terrain


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Range Rings & Grid LinesRange Rings & Grid Lines


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Runway Lead-in Line (Extended Centerline)Runway Lead in Line (Extended Centerline)


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Additional PDU SymbologyAdditional PDU Symbology

Additional alert annunciations (i e TCASannunciations (i.e., TCAS, EGPWS and excessive deviation) appear in the center of the PDU


SBAS (WAAS LPV)

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RNAV Approaches with LPV MinimumsRNAV Approaches with LPV Minimums

Conducted utilizing the LSBA (lateral) and VSBA (vertical) fli ht di t dflight director modes

Once the aircraft is up to 30 nm of the FAF, the EASy system computes the approach path/deviation using high integrity angular deviations provided directly from the SBAS/WAAS capable GNSSU This is indicated by the green LPV active annunciator


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CDI MenuCDI Menu

Selections & indications are similar to ILSsimilar to ILS

Approach is armed with APP button

Annunciations are Annunciations are consistent with HUD symbology


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LPV Annunciations on the PDU 1LPV Annunciations on the PDU

1. LSBA & VSBA Mode

2

3Annunciators

2. Approach (APP) annunciation

4

3. LPV Status Field Display and WAAS Approach Identifierpp

4. Vertical Deviation Indicator & Scale

5. Lateral Deviation

5

5. Lateral Deviation Pointer & Scale

6. CDI Course Pointer Nav Source 6


Nav Source annunciation

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LPV Approach SequenceLPV Approach Sequence

VSBA (vertical FD mode) is armed when:armed when: The APP button on the

guidance panel is pushed The VSBA mode arm criteria e S ode a c te a

have been met


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LPV Approach SequenceLPV Approach Sequence

VSBA (vertical FD mode) is captured when:captured when: The VSBA mode is armed

and The VSBA pointer moves e S po te o es

towards the center of the scale


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LPV-Specific PDU AnnunciationsLPV Specific PDU Annunciations

WAAS Approach ID (W07A)Displayed in the upper right of Displayed in the upper right of the attitude sphere

Also known as the Reference Path Identifier

Indicates the particular LPV approach that is loaded in the FMS

Must be cross referenced to the Approach ID displayed on the approach chart


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LPV Lateral Deviation PointerLPV Lateral Deviation Pointer

PF Indications:Cyan = Armed FD lateral Cyan = Armed FD lateral mode is LSBA

Magenta = Active FD lateral mode is LSBA

White = Any other condition PNF Indications:

Cyan = Armed FD lateralCyan Armed FD lateral mode is LSBA and LPV WAAS identifiers are same on both sides

Magenta = Active FD lateral mode is LSBA and LPV WAAS identifiers are same on both sides


both sides White = Any other condition

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CDI MenuCDI Menu


RNP Required Navigation Performance andSAAAR (RNP AR) Authorization

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RNP Approach Category SelectionRNP Approach Category Selection

The approach is selected using the STAR/APP tabusing the STAR/APP tab

RNP value can be changed or modified using the Landing Data tab (shownLanding Data tab (shown here)

The RNP value will automatically default to theautomatically default to the lowest available setting in the nav database


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RNP Approach Category SelectionRNP Approach Category Selection

NOTE: If the active flight plan contains a LOC-basedplan contains a LOC based approach, RNP, LPV and LNAV/VGP selections will be grayed outg y


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RNP Approach Symbology 1RNP Approach Symbology

1. VGP Mode APPVGP

2

3Annunciator

2. Terminal (TERM) or Approach (APP)

RNP ( 0.10)3

pp ( )Annunciation

3. RNP Status Field4. Vertical Deviation

4

54. Vertical Deviation Scale and Indicator

5. Lateral Deviation Scale and TSE Indicator

5

6RNP 0.1and TSE Indicator

6. Current Leg Value


NOTE: Display symbology may not represent actual aircraft software

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RNP Approach SymbologyRNP Approach Symbology

RNP Status (RNP X.XX) is green when: APP

VGP

green when: EPU from displayed FMS is

valid RNP lateral dev is displayed

RNP ( 0.10)

ate a de s d sp ayedand not amber

FMS vertical dev is valid No UNABLE RNP condition Both FD are valid and

displayed RNP is

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Lateral Deviation Indicator and Scale

APP

VGP

Scale When FMS is selected as Nav

source and RNP approach is selected in FMS, lateral

RNP ( 0.10)

selected in FMS, lateral deviation scale appears at top of HSI

Scale represents active RNP value

RNP 0.3 approach scaling will be 0.3nm full left dot and full right dot RNP

0.1



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Lateral deviation pointer = triangle APP

VGP

triangle EPU indicator = horizontal

line EPU indicator is limited to

RNP ( 0.10)

EPU indicator is limited to scale limits

Combined indicator shows Total System Error (TSE)Total System Error (TSE) Means of monitoring EPU and

lateral dev and reflects available margin during RNP

RNP 0.1a a ab e a g du g

approach



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TSE indicator changes color APP

VGP

color White = LNAV not armed or

engaged and EPU

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Scale is removed:If RNP value or deviation is If RNP value or deviation is invalid

If EPU value is invalid If FMS nav source (CDI) is

RNP (0.10)

If FMS nav source (CDI) is not selected for display



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Scale is amber:If winglet extends past 2 dots If winglet extends past 2 dots deviation



ADM Auto Descent Mode

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Auto-Descent Mode (ADM)Auto Descent Mode (ADM)

Safety feature that activates automatically in the eventautomatically in the event of cabin depressurization at high altitudes

Safeguard for incapacitated crewAutopilot guides aircraft to Autopilot guides aircraft to safe altitude at maximum velocity

Peace of mind for business jets operating at high altitudes


altitudes

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ADM implementationADM implementation

Activated when: Autopilot is engaged Aircraft is above 30,000 Cabin altitude is 9,700 or greater

Action: Aircraft turns 90 left Autothrottle will autoengage if required and reduce thrust to IDLE Descend at speed 10 kts less than Vmo/Mmo 15,000 is placed in altitude preselect, p p ADM is annunciated in the center of the FMA panel Upon reaching 15,000 maintains 250 kts


ADM remains active until autopilot is disengaged

SmartRunwayIncludes RAAS (Runway Awareness & Advisory System)y )

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www EGPWS Com SmartRunway/RAAS Infowww.EGPWS.Com SmartRunway/RAAS Info


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RAAS Inhibit - FMWRAAS Inhibit FMW


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RAAS Inhibit - SensorsRAAS Inhibit Sensors

RAAS Inhibit


ADS-B Out

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ADS-B OutADS B Out

Mandate Nov. 2010 Hudson Bay Area FL350-FL400Bay Area FL350 FL400

Mandate Dec. 2013 Australia above FL290


XM Graphical Weather

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XM Uplink WeatherXM Uplink Weather

If the optional Uplink Weather capability (XM) isWeather capability (XM) is installed, it can be used to receive the broadcast and display graphical weather p y g pinformation on the MFD using the optional XM antenna and receiver

This information is available only over the U.S.y


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Enables strategic route planning around weatherplanning around weather conditions

Potential fuel savings by routing around severerouting around severe weather conditions and optimizing cruising altitudes by referencing y gwinds aloft data

Improved cabin comfort


Weather is at least 8 min. old

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XM is a streaming commercial weather datacommercial weather data source (broadcast)

Information is automatically Information is automatically updated and stored until requested by the pilot for displaydisplay

Use the drop down WX menu to select eachmenu to select each product overlay


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XM Data available for display includes:display includes: NEXRAD (precipitation

return) Satellite imagerySate te age y Winds Aloft Storm tops LightningLightning Clear Air Turbulence Echo Tops TFRsTFRs Airmets Sigmets & CONUS


CONUS

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The Legend can also be selected for display byselected for display by checking the box next to the Legend menu selection


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NEXRAD DisplayNEXRAD Display

NEXRAD (next generation radar) is a network of Doppler d t d b th N ti l W th S iradars operated by the National Weather Service

NEXRAD data has a minimum display range of 10 nm in North Up and 5 nm in Heading Up mode


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The WX menu at the top of the INAV display is thethe INAV display is the pilots primary interface for the XM products

Select WX from the top menu

Select the WX XMTM from the drop down menu

Highlight and check the box next to the NEXRAD prompt ( h h )


(as shown here)

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A graphical depiction of NEXRAD weather will beNEXRAD weather will be shown on the INAV Map

Use the scroll knob to Use the scroll knob to change the range ring on the display

The time stamp of the uplinked NEXRAD image is displayed in the right sidedisplayed in the right side of the display


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Satellite DisplaySatellite Display

Clouds below 5000 feet are not displayednot displayed

This image has a minimum display range of 50 nm indisplay range of 50 nm in North Up and 25 nm in Heading Up Mode

Color of clouds is dependent upon altitude

Here the Satellite legend has been turned on and is in flight level (FL)


in flight level (FL)

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Winds Aloft DisplayWinds Aloft Display

Winds Aloft Data is displayed based on altitudedisplayed based on altitude specified in the window (FL240)


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Winds Aloft DisplayWinds Aloft Display

To change the altitude of the displayed wind,the displayed wind, highlight the altitude box and use the CCD knob to adjust the flight level

Push Enter


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Storm TopsStorm Tops

Storm Tops data is displayed only when thedisplayed only when the cell height (altitude) is greater than or equal to 20,000 ft

Text for the Storm Tops height and speed is g pdisplayed relative to the direction of the cell (shown here at FL210 or 21,000)FL210021Kt

The white storm top direction arrow begins at


gthe location of the cell

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Lightning Strike OverlayLightning Strike Overlay

XM WX lightning function receives lightning strikereceives lightning strike information from remote, ground-based lightning sensors

Lightning has a minimum display range of 10 nm in p y g 0North Up and 5 nm in Heading Up Modes


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Turbulence (Turb) DisplayTurbulence (Turb) Display

Areas of reported turbulence are shown inturbulence are shown in different shades of blue which represent intensity


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Turbulence (Turb) DisplayTurbulence (Turb) Display

Turbulence data is displayed for the altitudedisplayed for the altitude specified in the window on the selection menu (in this example FL240)


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Echo Tops DisplayEcho Tops Display

Data is shown in shades of purple and gray


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TFR DisplayTFR Display

Temporary Flight Restrictions (TFRs) areRestrictions (TFRs) are broadcast with continuous updates over the Continental U.S.

This gives pilots information on continuously changing flight restricted areas


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The TFR is graphically represented by a magentarepresented by a magenta circle


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Move the cursor over the applicable TFR informationapplicable TFR information box and push Enter

Select Show Info Select Show Info


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The TFR Information Dialog box will be displayedbox will be displayed

This provides the type, min/max altitudes datemin/max altitudes, date created or modified and expiration

Select the X to close the window


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AIRMET DisplayAIRMET Display

This displays a graphical representation of AIRMETs (Ai M t l i l I f ti ) th di l(Airmens Meteorological Information) on the map display

When the cursor is placed on the AIRMET graphic for more than 1 second, the AIRMET type and expiration time is di l ddisplayed


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Graphics are displayed in different colorsdifferent colors

The AIRMET Legend can be overlaid on the INAV


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To obtain additional information on an AIRMET,information on an AIRMET, position the cursor over the AIRMET graphic on the display and push the Enter key on the MF Controller

Select Show InfoS S


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The AIRMET Show Info Dialog box is displayed andDialog box is displayed and shows valid times, summary and locations


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SIGMET DisplaySIGMET Display

SIGMETs (Significant Meteorological Information)Meteorological Information) are weather advisories that concern the safety of all aircraft Extreme Turbulence Severe Icing or Widespread IMC conditions

over due to dust, sand or volcanic ash


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When the cursor is placed on a SIGMET graphic for more th 1 d th t d i ti ti i di l dthan 1 second, the type and expiration time is displayed

SIGMET graphics are displayed in different colors (see legend)


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To get additional information on a particularinformation on a particular SIGMET, position the cursor in the SIGMET and push Enter

Select Show Info The SIGMET information

dialog box is displayedg p y Neighboring SIGMETs can

be selected using the cursor

Select the X to close the dialog box


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Update RatesUpdate Rates

Weather products are updated at predefined intervals: NEXRAD - 5 minutes TFRs 12 minutes AIRMETs 12 minutes SIGMETs 12 minutes Storm Tops 75 seconds Lightning (CONUS only) 5 minutes Winds Aloft 45 seconds Satellite Mosaic (cloud heights) 15 minutes CAT 1 hour CONUS 5 minutes Echo Tops and Storm Movement 7.5 minutes


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Question and AnswersQuestion and Answers

Q & AQ


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