2011 honeywell operators conference fmz/nz2000...

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Rev March 24, 2011

2011 Honeywell Operators ConferenceFMZ/NZ2000 V6.1 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 informationHONEYWELL 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 for any purpose without prior written permission of Honeywell International pu pose ou p o e pe ss o o o ey e e a o aInc. All Rights Reserved.


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Why FMS 6.1?Why FMS 6.1?

• Several time-saving features/functions added• Improved safety features that lower pilot workload• Improved safety features that lower pilot workload• Ability to fly WAAS-LPV approaches into airports that don’t have ILS

(less diversions and use of alternates)• Potential for RNP SAAAR certification and LOA which opens upPotential for RNP SAAAR certification and LOA which opens up

special approaches at airports at high terrain or high congestion locations

• Required for future growth option of FANS 1/A Oceanic CPDLCq g p• Required for future mandates such as PM-CPDLC in Europe


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Product Certification Status by Platform

Name Description TSO Status TSO date STC DateDuncan Aviation –complete 8/3/2010;

Challenger 601 FMS 6.1 NZ aircraft; TSO & STC for NZ-2000TSO Complete June 2010

p ;Available to all Svc Ctrs

Hawker 800XP FMS 6.1 NZ aircraft; TSO & STC for NZ-2000TSO Complete June 2010

HBC/Std Aero in work – April 2011,; Available to all Svc Ctrs

Falcon 900B FMS 6.1 NZ aircraft; TSO & STC for NZ-2000TSO Complete June 2010

Duncan Aviation –complete 12/17/2011 Available to all Svc Ctrs

Gulfstream IVFMS 6.1 NZ aircraft, TSO & STC for FMZ-2000 TSO In work Aug 2011

Gulfstream Svc Ctrs –Aug 2011Gulfstream IV 2000 TSO In-work Aug 2011 Aug 2011

Gulfstream V FMS 6.1 IAC aircraft, TSO & STC for IC-800TSO In Work June 2011

Gulfstream Svc Ctrs –June 2011

Dassault – June 2011, Available to all Svc

Falcon 900EX/C FMS 6.1 IAC aircraft, TSO & STC for IC-800 TSO In-work June 2011 Ctrs

Citation X TSO & STC for FMZ-2000 IAC version 6.1 TSO In-work4Q/1Q 2011

Citation Svc Ctrs2Q2011Rolled into Batch 3; BAS 2011; Authorized


Bombardier GEX/5000/XRS TSO & STC for FMZ-2000 IAC version 6.1 See Batch 3 2011BAS 2011; Authorized BAS Svc Ctrs

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NZ-2000/FMZ v6.1 Feature OverviewNZ 2000/FMZ v6.1 Feature Overview

• Hardware Upgrade to CD820 (not required)• FANS 1/A Datalink (optional)• FANS 1/A Datalink (optional)• SBAS (WAAS, EGNOS & MSAS LPV)• RNP Annunciations• Circling Approaches• Circling Approaches• Multi RNAV or LOC Approaches per Runway• TACAN Approaches (if TACAN receiver equipped)

V t t Fi l A h (A ti t V t P t)• Vectors to Final Approach (Activate Vectors Prompt)• Augmented LOC Preview• VNAV Temp Compensation & Calculator

A t H ldi t Altit d S i• Auto Holding to Altitude Sequencing• En route Holding Patterns• Improve Crossload Time


• Auto LNAV armed for TOGA

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Honeywell FMZ System

Flight Management System Product Line

Honeywell FMZ System

IC-615 / -800C 6 5 / 800

IC b d FMS ( h d ith th t )IC-based FMS (shared processor with other systems)

G-V, Citation X, Global Express/XRS/5000, Falcon 900EX/C, L382


IC-800 A/C will get an IAC & Display/EFS Upgrade

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Honeywell NZ-2000 System

Flight Management System Product Line

Honeywell NZ 2000 System

NZ2000NZ2000

Separate NZ2000 Nav Computer

Falcon 900B, Citation Excel / Ultra, Bravo, Primus Epic® CDS/R platforms, Challenger 601-3A/R, Hawker 800XP, Citation III/VI/VII, Gulfstream IV/IV SP


,

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MCDU CD-820 UpgradeMCDU CD 820 Upgrade

• Required upgrade for FANS 1/A optional functionality

• Compatible with variety of graphical services: g p– AFIS®

– OneView™

– Airshow™

– JetMap™


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FANS 1/A – Future Air Navigation Option


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Sample CPDLC Datalink Message TypesSample CPDLC Datalink Message Types

• Uplink Message types (not inclusive)– Pre-departure clearances– Tactical route changes (direct to)– Vertical changes (altitude

change)change)– Lateral offset– Report requests

D li k M t ( t• Downlink Message types (not inclusive)– Emergency reports– Position reports– Accept/Reject/Standby response– Free text– Altitude, direct, speed, lateral

offset requests.


q

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Features Transparent to Flight Crew

• ADS:Encoding/Decoding

Features Transparent to Flight Crew

• CPDLC:E di /D di– Encoding/Decoding

– Periodic report triggering– Event report

monitoring/triggeringE d ll ti

– Encoding/Decoding– Connection management (incl.

handoff)– Log management (capacity– Emergency mode cancellation

from ground– Downlink error messages

Log management (capacity handling)

– Uplinked route: pre-load Validity/compatibility checkingU li k d t l di i t FPLN• AFN:

– Encoding/Decoding– AFN handoff

– Uplinked route: loading into FPLN– Downlink request: Nav database

validity checking– Downlink reports:Downlink reports:

monitoring/triggering– Automatic ADS emergency mode

initiation (w/MAYDAY)D li k


– Downlink error messages

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ATC Comm (CPDLC)ATC Comm (CPDLC)

• CPDLC (Controller Pilot Data Link Communications) has been i l t d i t th i ti FANS f ti litimplemented into the existing FANS functionality

• CPDLC is also known as ATC Comm

• ATC Comm is an ATS (Air Traffic Services) application with which pilots and controllers exchange messages using a data linkwhich pilots and controllers exchange messages using a data link connection

ATC C i l d t f l i f ti d/• ATC Comm includes a set of clearance, information, and/or request messages which correspond to existing phraseology used in current ATC procedures


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ATC Comm (cont.)ATC Comm (cont.)

• ATC Comm is integrated into the FMS

• This integration provides the pilot with the capability to review uplinked flight plans and activate them directly into the active flight plan

• ATC Comm messages are comprised of one or more specific g p pmessage elements

• Each message element contains some or all of the following:Each message element contains some or all of the following:– Fixed Text– Variable Text– Free Text


– Free Text

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RNP Annunciations


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Possible Primus 2000 RNP Display on PFDPossible Primus 2000 RNP Display on PFD

Global Express (P2000) DisplayGlobal Express (P2000) Display


Annunciations will only appear on PFD if EDS is modified

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RNP on CDU PagesRNP on CDU Pages

Set RNP Page Progress Page 1


Ability to manually set RNP value

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SBAS (WAAS-LPV)


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LPV Selection on CDULPV Selection on CDU


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LPV and VGP Armed AnnunciationLPV and VGP Armed Annunciation

Arm with theAPPR button on Guidance panel



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LPV and VGP Active AnnunciationsLPV and VGP Active Annunciations



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SBAS Approach Failure AnnunciationsSBAS Approach Failure Annunciations



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Example LPV Annunciator PanelsExample LPV Annunciator Panels

• For aircraft that do not have EDS modified, additional annunciatorpanels are required

• Added to main instrument panel for pLPV indications

• White – armedWhite armed• Green – active• Amber - failure


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Additional 6.1 Features


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Automated Holding to Altitude sequencingAutomated Holding to Altitude sequencing

HA (H ldi t Altit d ) l h dl d i i il t 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 ltit d t i t th h ldi tt ill b d l t d t ti llaltitude constraint, the holding pattern will be deleted automatically

by the FMS resulting in a VA leg• An HA leg will sequence when the aircraft has achieved the HA

ltit d t i taltitude constraint• FMS will perform an immediate exit of the holding pattern upon

achieving the altitude constraint• Altitude is provided by the navigation database when defined for

SIDs, and missed approach procedures


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Benefits: HA leg Auto SequencingBenefits: HA leg Auto Sequencing

• Currently the pilot has to perform a manual operation during a procedure that contains an HA leg. Implementation of this feature will enhance the automatic leg sequencing ability of the FMS.


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Circling ApproachesCircling Approaches

• Circling Approaches already added to Nav DB – now they can be ll d d ti t dcalled up and activated

• There are four cases where requirements to circle occur:1. Approach not aligned with the runway 2. Circling patterns 3. Approach aligned with a runway, but not the one to land on4. Sidestep Manoeuvre

• Circling Approach procedures are specific for an airport and apply to all runways at that airport

• Flight profile for a circling approach will fly the aircraft to a minimum descent altitude

• Pilot will still have to manually heading-bug themselves around the circle but missed approach procedures will be enabled


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Vectors to Final (Activate Vectors Prompt)Vectors to Final (Activate Vectors Prompt)

• Vector operations are invoked when the selected navigation mode for the flight director transitions from LNAV to HDG modemode for the flight director transitions from LNAV to HDG mode– This operation may be desired during any phase of flight including

an en route vector operation, a vectored approach transition, or vectors to final approach procedure. Vectors to final (VTF) shall be activated when the flight director mode transitions from LNAV toactivated when the flight director mode transitions from LNAV to HDG.

• The FMS shall activate vector operations when the active flight director mode transitions from LNAV to HDG.director mode transitions from LNAV to HDG.

• When a vectored approach transition is selected, the FMS will create an approach that consists of an intercept leg leading in to the FAF, removing any legs that existed in the approach prior tothe FAF, removing any legs that existed in the approach prior to the FAF– Only the approach legs prior to the FAF are removed; the departure,

cruise, and arrival legs will still remain in the flight plan.


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Activate Vectors PromptActivate Vectors Prompt

BENEFIT: simplifies vectored approach (aligns the a/c with FAF)


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Activate Vectors PromptActivate Vectors Prompt


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Multiple Approaches to Same RunwayMultiple Approaches to Same Runway

• Multiple approaches with the same guidance (RNAV, LOC, etc.) to the same runway are annotated with an alphabetical suffix beginning at the end of the alphabet and working backwards for subsequent procedures

• These multiple types will be added to the navigation database as they are defined and the FMS will provide these approaches for selection by the pilot– Note: Most RNAV approach procedures will require RNP = 0.3

BENEFITS:• Several approaches of the same type can be available for the same

runway


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Multiple Approaches to Same RunwayMultiple Approaches to Same Runway


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Enroute Holding PatternsEnroute Holding Patterns • The FMS shall provide capability to utilize a database holding pattern in

place of a default hold definition at an enroute waypointIf th l t h ld t t i t th FMS ill fi t• If the crew selects a hold at an enroute waypoint, the FMS will first determine if there is a database defined hold at that particular waypoint

• If a hold exists, it will be entered into the flight plan as specified• If no database hold exists the default hold definition will be inserted into• If no database hold exists, the default hold definition will be inserted into

the flight plan• If multiple patterns exist for a particular fix, they will be displayed on a

page from which the desired pattern can be selectedpage from which the desired pattern can be selected


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Barometric VNAV Temp CompBarometric VNAV Temp Comp

• FMS will provide a means by which the crew may calculate a temperature compensated altitude to use as the minimum altitude for antemperature-compensated altitude to use as the minimum altitude for an approach

• When Temp Comp is activated by the pilot all alt constraints in the• When Temp Comp is activated by the pilot, all alt constraints in the departure, approach, and missed approach are compensated

• Purpose of this is to raise the alt constraint in cold weatherPurpose 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 less than the true altitude

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


Already active on Bombardier Global Express with Batch 2

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Temperature Compensation ActivationTemperature Compensation Activation

Set the desired temperature compensation configuration

Enter the landing (surface) temperature on the LAND/GA

INITp g

Enter an approach from the

INIT page

Verify the compensated altitudes on the TEMP COMPEnter an approach from the

into the Active Flight Planaltitudes on the TEMP COMP

page

Select the ACTIVATE prompt on the TEMP COMP page



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Manual Baro VNAV Correction CapabilityManual Baro VNAV Correction Capability

• Once temp comp is activated adjustedactivated, adjusted altitudes appear on active flight plan page in white

• All altitude constraints on approach and missed approach procedures areapproach procedures are recalculated and shown



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VNAV Temp Comp CalculatorVNAV Temp Comp Calculator

• Compensation correction to altitudes in flight plan are only for database altitudes which have not been modified by pilot

• Calculator can be used for minima that is not part of a published approach

• Using the Temp Comp g p pCalculator function, the pilot inputs an altitude value and views the ‘compensated’ altitude


New for all aircraft getting FMS v6.1

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VNAV Temp Comp CalculatorVNAV Temp Comp Calculator

• In this example, the landing p , ginit temp was set to -25°C

• Pilot entered altitude of 15000Pilot entered altitude of 15000 on Line 1L

• NOTE If the pilot modifies• NOTE - If the pilot modifies any waypoint altitude constraint, it will not be displayed on Temp Compdisplayed on Temp Comp page and will not be changed when Temp Comp is activated


New for all aircraft getting FMS v6.1

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VNAV Data PageVNAV Data Page

• Provides information on VNAV path• Provides information on VNAV path


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VA/VI Leg CombinationVA/VI Leg Combination

• Improve the guidance and sequencing for heading tosequencing for heading to altitude (VA) and heading to intercept (VI) leg combinations by using ground speed toby using ground speed to compute the turning point onto the course

• Reduces unnecessaryReduces unnecessary maneuvers

• FMS will re-compute the intersection when the leg Isintersection when the leg Is active

• Eliminates the ‘Honeywell head fake’ maneuver in LNAV


fake maneuver in LNAV

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Auto LNAV Arming for TOGAAuto LNAV Arming for TOGA

• When G/A or TOGA button is pushed, FD will automatically select NAV and course pointer on HSI will auto switch to FMSNAV and course pointer on HSI will auto switch to FMS

• AP/FD modes on go-around will be NAV ARMED & G/A (not PIT & G/A)& G/A)


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Question and AnswersQuestion and Answers

Q & AQ


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