S.I.L. HONEYWELL-24-May-2011

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Honeywell International Inc.

21111 N. 19th Avenue

Phoenix, Arizona 85027-2708

U.S.A.

CAGE: 55939

Telephone: (800) 601-3099 (Toll Free U.S.A./Canada)

Telephone: (602) 365-3099 (International Direct)

Telephone: 00-800-601-30999 (EMEA Toll Free)Telephone: 420-234-625-500 (EMEA Direct)

Web site: www.myaerospace.com

SERVICE INFORMATION LETTERNZ-2000/FMZ-2000/PRIMUS Apex/PRIMUS EPIC Flight Management System (FMS): NZ-2000 and

FMZ-2000/IC-615/IC-800/IC-1080, PN 7018879-01001, -01002, -02003 Thru -02007, -02010, -02017,

-03008, -03012, -03014, -03016, -03018, -03020, -03022, -03024, -03026, -03028, -03030, -03032,

-03034, -10000, -11009, -11015, -11019, -11021, -11023, PN 7017000-21XXX, -94XXX, -95XXX,

-98XXX, -99XXX, PN 7017300-01XXX, -11XXX, -21XXX, -31XXX, -41XXX, -43XXX, -45XXX, -56XXX,

-61XXX, -63XXX, (1) AgustaWestland AW139, PN EB7030191-00105 (Phase 4), PN EB7030191-00107

(Phase 5), PN EB7030191-00108 (Phase 6), (2) Cessna Sovereign, PN EB7031847-00105 (Phase 3),

PN EB7031847-00106 (Phase 4), PN EB7031847-00108 (Phase 4.1), PN EB7031847-00109 (Phase

4.2), PN EB7031847-00111 (Phase 5), (3) Dassault PRIMUS EPIC F900, PN EB7036889-00112, PN

EB7036889-00115, PN EB7036889-00116, (4) Dassault PRIMUS EPIC F2000, PN EB7036889-00203, PN

EB7036889-00205, PN EB7036889-00206, (5) Dassault F7X, PN EB7034843-00101, PN EB7034843-00102,

(6) Embraer 170, PN PS7027709-00124 (Load 21.2), PN PS7027709-00126 (Load 21.4), PN

PS7027709-00127 (Load 23.1), PN PS7027709-00128 (Load 21.5), PN PS7027709-00129 (Load 23.2), (7)

Embraer 190, PN PS7027709-00214 (Load 23.1), PN PS7027709-00215 (Load 21.4), PN PS7027709-00216

(Load 21.5), PN PS7027709-00217 (Load 23.2), (8) Embraer 170/190, PN PS7027709-00303 (Load

25.1.0.1), (9) Gulfstream G350/450, PN EB7031236-00410 (Delta), PN EB7031236-00411 (Echo), PN

EB7031236-00409 (Foxtrot), PN EB7031236-00414 (Foxtrot), PN EB7031236-00412 (Golf), (10) Gulfstream

G500/550, PN EB7031236-00315 (Delta), PN EB7031236-00316 (Echo), PN EB7031236-00314 (Foxtrot),

PN EB7031236-00319 (Foxtrot), PN EB7031236-00320 (Foxtrot), PN EB7031236-00317 (Golf), (11)

Hawker 4000, PN EB7030192-00113 (Load 19), (12) Pilatus PC-12NG, PN EB7037248-00103 (Build 6.2),

PN EB7037248-00104 (Build 7.2), (13) Viking DHC6-400, PN EB7032889-00101 (Load 1.3); Reduction

of Navigation Database Procedures Content due to FMS Lateral Navigation (LNAV) Display/Guidance

Issues

Legal Notice

Export Control

This document contains technical data and is subject to U.S. export regulations. These commodities,

technology, or software were exported from the United States in accordance with the export administration

regulations. Diversion contrary to U.S. law is prohibited.

ECCN: 7E994, NLR Eligible.

Proprietary Information

9 Nov 2010

Revision 2, 24 May 2011 Page 1 of 17

Publication Number D201011000003 © Honeywell International Inc. Do not copy without express permission of Honeywell.



SERVICE INFORMATION LETTER

Honeywell – Confidential

THIS COPYRIGHTED WORK AND ALL INFORMATION ARE THE PROPERTY OF HONEYWELLINTERNATIONAL INC., CONTAIN TRADE SECRETS AND MAY NOT, IN WHOLE OR IN PART, BE USED,DUPLICATED, OR DISCLOSED FOR ANY PURPOSE WITHOUT PRIOR WRITTEN PERMISSION OFHONEYWELL INTERNATIONAL INC. ALL RIGHTS RESERVED.

Honeywell Materials License Agreement

The documents and information contained herein ("the Materials") are the proprietary data of HoneywellInternational Inc. and Honeywell Intellectual Properties Inc. (collectively "Honeywell"). These Materialsare provided for the exclusive use of Honeywell Service Centers; Honeywell-authorized repair facilities;operators of Honeywell aerospace products subject to an applicable product support agreement, their whollyowned-subsidiaries or a formally designated third party service provider; and direct recipients of Materials fromHoneywell’s Aerospace Technical Publication Distribution. The terms and conditions of this License Agreementgovern your use of these Materials, except to the extent that any terms and conditions of another applicableagreement with Honeywell regarding the operation, maintenance, or repair of Honeywell aerospace productsconflict with the terms and conditions of this License Agreement, in which case the terms and conditions of theother agreement will govern. However, this License Agreement will govern in the event of a conflict between itsterms and conditions and those of a purchase order or acknowledgement.

1. License Grant - If you are a party to an applicable product support agreement, a Honeywell Service Centeragreement, or an authorized repair facility agreement, Honeywell hereby grants you a limited, non-exclusivelicense to use these Materials to operate, maintain, or repair Honeywell aerospace products only in accordancewith that agreement.

If you are a direct recipient of these Materials from Honeywell’s Aerospace Technical Publication Distributionand are not a party to an agreement related to the operation, maintenance or repair of Honeywell aerospaceproducts, Honeywell hereby grants you a limited, non-exclusive license to use these Materials to maintain orrepair the subject Honeywell aerospace products only at the facility to which these Materials have been shipped("the Licensed Facility"). Transfer of the Materials to another facility owned by you is permitted only if theoriginal Licensed Facility retains no copies of the Materials and you provide prior written notice to Honeywell.

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expressly granted to you, including all rights in patents, copyrights, trademarks, and trade secrets. No licenseto use any Honeywell trademarks or patents is granted under this License Agreement.

3. Confidentiality - You acknowledge that these Materials contain information that is confidential and proprietaryto Honeywell. You agree to take all reasonable efforts to maintain the confidentiality of these Materials.

4. Assignment And Transfer - This License Agreement may be assigned to a formally designated servicedesignee or transferred to a subsequent owner or operator of an aircraft containing the subject Honeywellaerospace products. However, the recipient of any such assignment or transfer must assume all of yourobligations under this License Agreement. No assignment or transfer shall relieve any party of any obligationthat such party then has hereunder.

5. Copies of Materials - Unless you have the express written permission of Honeywell, you may not make orpermit making of copies of the Materials. Notwithstanding the foregoing, you may make copies of only portionsof the Material for your internal use. You agree to return the Materials and any copies thereof to Honeywellupon the request of Honeywell.

6. Term - This License Agreement is effective until terminated as set forth herein. This License Agreementwill terminate immediately, without notice from Honeywell, if you fail to comply with any provision of thisLicense Agreement or will terminate simultaneously with the termination or expiration of your applicableproduct support agreement, authorized repair facility agreement, or your formal designation as a third partyservice provider. Upon termination of this License Agreement, you will return these Materials to Honeywellwithout retaining any copies and will have one of your authorized officers certify that all Materials have beenreturned with no copies retained.

9 Nov 2010

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7. Remedies - Honeywell reserves the right to pursue all available remedies and damages resulting from abreach of this License Agreement.

8. Limitation of Liability - Honeywell does not make any representation regarding the use or sufficiency of theMaterials. THERE ARE NO OTHER WARRANTIES, WHETHER WRITTEN OR ORAL, EXPRESS, IMPLIEDOR STATUTORY, INCLUDING, BUT NOT LIMITED TO, (i) WARRANTIES ARISING FROM COURSE OFPERFORMANCE, DEALING, USAGE, OR TRADE, WHICH ARE HEREBY EXPRESSLY DISCLAIMED, OR (ii)WARRANTIES AGAINST INFRINGEMENT OF INTELLECTUAL PROPERTY RIGHTS OF THIRD PARTIES,EVEN IF HONEYWELL HAS BEEN ADVISED OF ANY SUCH INFRINGEMENT. IN NO EVENT WILLHONEYWELL BE LIABLE FOR ANY INCIDENTAL DAMAGES, CONSEQUENTIAL DAMAGES, SPECIALDAMAGES, INDIRECT DAMAGES, LOSS OF PROFITS, LOSS OF REVENUES, OR LOSS OF USE,EVEN IF INFORMED OF THE POSSIBILITY OF SUCH DAMAGES. TO THE EXTENT PERMITTED BYAPPLICABLE LAW, THESE LIMITATIONS AND EXCLUSIONS WILL APPLY REGARDLESS OF WHETHERLIABILITY ARISES FROM BREACH OF CONTRACT, WARRANTY, TORT (INCLUDING BUT NOT LIMITEDTO NEGLIGENCE), BY OPERATION OF LAW, OR OTHERWISE.

9. Controlling Law - This License shall be governed and construed in accordance with the laws of the State ofNew York without regard to the conflicts of laws provisions thereof. This license sets forth the entire agreementbetween you and Honeywell and may only be modified by a writing duly executed by the duly authorizedrepresentatives of the parties.

Copyright - Notice

Copyright 2010, 2011 Honeywell International Inc. All rights reserved.

Honeywell, PRIMUS Apex, and PRIMUS EPIC are registered trademarks of Honeywell International Inc.

All other marks are owned by their respective companies.THIS IS THE SB FOSI - DATE: 20101101

9 Nov 2010






Transmittal Information

Publication Number D201011000003

Summary

This revision is a FULL replacement. This revision includes the changes that follow:

• Added additional aircraft types and associated equipment part numbers to the title of this SIL.

• Added the data that this SIL supersedes SIL, Publication Number D201012000014.

• Added additional procedures and associated examples that could cause anomalies.

• Identified the approximate number of procedures that are removed from the 2011, Cycle 06 database

for each aircraft and anomaly.

Because of the large number of changes, revision bars are not used.

Revision History

This service information letter (SIL) has had two revision(s) as shown in Table 1.

Table 1. Revision History

Revision Number Revision Date

0 9 Nov 2010

1 2 Feb 2011

2 24 May 2011

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1. General Information

A. Purpose

CAUTION: SOME STANDARD INSTRUMENT DEPARTURES (SID)S, STANDARDTERMINAL ARRIVAL ROUTES (STAR)S, TRANSITIONS, AND APPROACHES

ARE NOT IN THE DATABASE DUE TO LIMITATIONS OF THE FMS.

ADDITIONAL PROCEDURES HAVE BEEN REMOVED TO ADDRESS THE

ANOMALIES DISCUSSED IN THIS SIL. THE FLIGHT CREW SHOULD TAKE

EXTRA CAUTION TO VERIFY DATABASE CONTENT DURING PREFLIGHT

PLANNING.

(1) The purpose of this SIL is to advise all affected operators listed on Page 1 of this SIL

of anomalies that may occur with certain terminal area procedures and Honeywell’s

action to prevent them from occurring. Only top level system part numbers listed in the

part number field of this SIL are affected by these issues.

(2) The top level system part number can be obtained from the system configuration pageon all PRIMUS Apex and PRIMUS EPIC aircraft. NZ-2000/FMZ-2000 equipped aircraft

should utilize the NZ-2000 hardware part number.

NOTE: For PRIMUS Apex and Dassault EASy aircraft, the top level system part

number can be obtained from the system configuration tab. Dassault EASy

system configuration tab shown in Figure 1.

Figure 1. (Sheet 1 of 1) Dassault EASy System Configuration tab

NOTE: For all multi-function control display unit (MCDU) equipped aircraft, the toplevel system part number can be obtained from the system configuration

page on the multi-function display (MFD). Hawker 4000 example shown in

Figure 2.

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Figure 2. (Sheet 1 of 1) Hawker 4000 Example

B. Background

(1) Honeywell recently discovered software anomalies in which the FMS LNAV function

may incorrectly fly published terminal area procedures. As a result, Honeywell is

removing procedures from the navigation database for Items A thru G (refer to

Paragraph 1.D.(1) thru Paragraph 1.D.(7)). The data provided in the aircraft matrix

table (refer to Table 2 in Paragraph 1.D.(8)) is effective in 2011 navigation database

Cycle 06. Actual number of removed procedures will vary each cycle.

(2) Honeywell will continue to evaluate procedures each navigation database cycle to

ensure that only problematic procedures are removed. A navigation database process

is in place to ensure that all anomalies listed in this SIL are addressed by removing

affected procedures.

NOTE: This SIL has been revised to include the FLY XXX OR AS ASSIGNED

heading leg issue previously addressed in SIL, Publication Number

D201012000014. SIL, Publication Number D201012000014, has been

superseded by this SIL and should no longer be used in reference to

this anomaly.

C. References

(1) To find, see, and download Honeywell Technical Publications, go to

www.myaerospace.com.

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(2) The document(s) that follow(s) is/are related to this SIL. Unless specified differently,

you can use subsequent revisions.

• SIL, Publication Number D201012000014, NZ-2000/FMZ-2000, PRIMUS Apex,

PRIMUS EPIC Flight Management Systems (FMS)s: (1) all NZ-2000/FMZ-2000

Software Prior to NZ6.1 and NZ6.1, PN 7018879-03034, Only, (2) all PRIMUS

Apex PC-12/47E, Build 6.2 Software, PN EB7037248-00103, and Build 7.2, PN

EB7037248-00104, and Viking DHC6-400, PN EB7032889-00101, (3) all PRIMUS

EPIC FMS Software Prior to VAR14ZL and Dassault EASy, PN EB7036889-00112,

PN EB7036889-00115, PN EB7036889-00116, PN EB7036889-00203, PN

EB7036889-00205, PN EB7036889-00206, PN EB7034843-00101, PN

EB7034843-00102; Terminal Area Procedures Using Heading Legs FLY XXX OR

AS ASSIGNED, Revision 1.

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D. Summary Anomalies

NOTE: For each item, all conditions must be met for anomaly to occur.

(1) Item A

(a) Procedures containing a course change of 180 degrees or more. This

excludes holding patterns and procedure turns, which are flown correctly:

• Last leg of a procedure contains a course change of 180 degrees orgreater.

• Last leg has a turn direction specified in the navigation database.

• Last waypoint common in connecting procedures.

(b) Example of Item A (refer to Figure 3): KGPI SKOTT 2 SID RWY02 – LNAV

incorrect turn to FCA as indicated by red arrow. When common waypoint

becomes the active leg, map display and lateral guidance are incorrect.

Refer to Figure 3.

Figure 3. (Sheet 1 of 1) Example of Item A

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(2) Item B

(a) Procedures containing right turn arcs:

• A right turn direction arc leg terminates a procedure (for example, STAR).• First leg of following procedure (for example, approach) begins with arc

termination.

• When arc becomes the active leg, lateral guidance is incorrect.

NOTE: Many procedures containing right turn arcs have been removed

from the database.

(b) Example of Item B (refer to Figure 4): RJBB MAYAH STAR entered in flight

plan, LNAV guidance is incorrect and opposite of course indication on MFD.

Figure 4. (Sheet 1 of 1) Example of Item B

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(3) Item C

(a) SID/STAR combinations:

• SID/STAR combinations, which contain common waypoints betweendeparture, arrival, and/or approach segments.

• Course change to common waypoint is 180 degrees or greater.

(b) Example of Item C (refer to Figure 5): KDVT 1 departure and KTUS DINGO 5

arrival entered in flight plan.

Figure 5. (Sheet 1 of 1) Example of Item C

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(4) Item D

(a) Final approach overshoot:

• STAR, approach transition and approach contain common waypoint.NOTE: Only problematic approach transitions are removed from the

navigation database.

(b) Example of Item D (refer to Figure 6): RJBB ILS 6R – ALLAN waypoint is

common to arrival, approach transition, and approach. FMS overflies ALLAN,

the common waypoint.

Figure 6. (Sheet 1 of 1) Example of Item D

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(5) Item E

(a) FMS/LNAV loss of turn direction on SID:

• Procedures with course change of 180 degrees or greater.

• Altitude terminating leg (displayed on MCDU as *ALT) precedescourse/direct to a fix leg (CF/DF).

• Aircraft has reached an altitude which is above the specified altitude

constraint prior to sequencing the *ALT waypoint.

(b) Example of Item E (refer to Figure 7): MCDU displays the correct left turn

to PXR, FMS may turn right if aircraft is above 4,000 feet (1,219 m) prior

to sequencing *ALT07 waypoint.

Figure 7. (Sheet 1 of 1) Example of Item E

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(6) Item F

(a) Missed approach activation:

• Procedures with course change of 180 degrees or greater.• Any of the following combinations: track/course/direct to a fix leg

(TF/CF/DF) preceding a CF/DF in a missed approach procedure.

• If missed approach is activated by the pilot on the MCDU, the FMS will

change the turn direction displayed on the MCDU.

(b) Example of Item F (refer to Figure 8): UATG RWY14 - missed approach is

activated - FMS incorrectly changes the turn direction to left on the MCDU,

LNAV makes an incorrect left turn.

Figure 8. (Sheet 1 of 1) Example of Item F

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(7) Item G

(a) FLY XXX OR AS ASSIGNED heading legs:

• Procedures with course change of 180 degrees or greater.

• Heading leg turn direction from database not followed by LNAV.

• FMS will turn in direction of least course change.

NOTE: Previously addressed in SIL, Publication Number D201012000014

(superseded). Procedures, which contain heading legs with a

course change of 160 degrees or greater have been removed from

the navigation database beginning in 2011, Cycle 06.

(b) Example of Item F (refer to Figure 9): UATG RWY14 – right turn heading leg

to 322 degrees, FMS incorrectly turns left.

Figure 9. (Sheet 1 of 1) Example of Item G

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(8) Aircraft Matrix Table

(a) Refer to Table 2 to identify the approximate number of procedures removed

from the database cross referenced to the anomaly and aircraft type.

Table 2. Aircraft Matrix Table

Item A B C D E F G

Approximate Number of Procedures Removed

NOTE: Data displayed for 2011, Cycle 06 and will vary each

cycle 470 400 200 600 325 375 530

Aircraft X indicates database removal for item

AgustaWestland AW139, PN EB7030191-00105 (Phase 4) X X X

AgustaWestland AW139, PN EB7030191-00107 (Phase 5) X X X X X X X

AgustaWestland AW139, PN EB7030191-00108 (Phase 6) X X X X X X XCessna Sovereign, PN EB7031847-00105 (Phase 3) X X X

Cessna Sovereign, PN EB7031847-00106 (Phase 4) X X X

Cessna Sovereign, PN EB7031847-00108 (Phase 4.1) X X X

Cessna Sovereign, PN EB7031847-00109 (Phase 4.2) X X X

Cessna Sovereign, PN EB7031847-00111 (Phase 5) X X X X X X X

Dassault PRIMUS EPIC F900, PN EB7036889-00112 X X X






Dassault F7X, PN EB7034843-00101 X X X

Dassault F7X, PN EB7034843-00102 X X X

Embraer 170, PN PS7027709-00124 (Load 21.2) X X X


Embraer 170, PN PS7027709-00127 (Load 23.1) X X X X X X X






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Table 2. Aircraft Matrix Table (Cont)

Item A B C D E F G

Approximate Number of Procedures Removed

NOTE: Data displayed for 2011, Cycle 06 and will vary each

cycle 470 400 200 600 325 375 530

Aircraft X indicates database removal for item


Embraer 170/190, PN PS7027709-00303 (Load 25.1.0.1) X X X X X

Gulfstream G350/450, PN EB7031236-00410 (Delta) X X X

Gulfstream G350/450, PN EB7031236-00411 (Echo) X X X

Gulfstream G350/450, PN EB7031236-00409 (Foxtrot) X X X X X X X


Gulfstream G350/450, PN EB7031236-00412 (Golf) X X X X X


Gulfstream G500/550, PN EB7031236-00315 (Delta) X X X

Gulfstream G500/550, PN EB7031236-00316 (Echo) X X X



Gulfstream G500/550, PN EB7031236-00317 (Golf) X X X X X

Hawker 4000, PN EB7030192-00113 (Load 19) X X X

Pilatus PC-12NG, PN EB7037248-00103 (Build 6.2) X X X X X X X

Pilatus PC-12NG, PN EB7037248-00104 (Build 7.2) X X X X X

Viking DHC6-400, PN EB7032889-00101 (Load 1.3) X X X X X X X

NZ-2000 and FMZ-2000/IC-615/IC-800/IC-1080, PN7018879-01001, -01002, -02003 thru -02007, -02010, -02017,-03008, -03012, -03014, -03016, -03018, -03020, -03022,-03024, -03026, -03028, -03030, -10000, -11009, -11015,-11019, -11021, -11023, PN 7017000-21XXX, -94XXX, -95XXX,-98XXX, -99XXX, PN 7017300-01XXX, -11XXX, -21XXX,-31XXX, -41XXX, -43XXX, -45XXX, -56XXX, -61XXX, -63XXX

X

PN 7018879-03032, -03034 X X X X

E. Action

(1) To prevent the problems from occurring, Honeywell is analyzing and removing

procedures from the navigation database that can cause incorrect guidance. As further

analysis is performed, additional procedures may be removed from the database.

(2) A list of removed procedures can be obtained at:

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• http://www.honeywellaes.com

• http://www.epicinds.com.

CAUTION: WHEN FLYING ANY PROCEDURES USING THE FMS, THE FLIGHT CREWSHOULD MONITOR AIRCRAFT GUIDANCE TO ENSURE TURN DIRECTION

IS CONSISTENT WITH THE PUBLISHED PROCEDURE.

(3) The flight crew should use the following procedures:

• Verify availability of procedures in the database when preflight planning.

• Compare and monitor the charted procedure with the active flight plan.

(4) If your aircraft is not included in the part number list or the aircraft top level operational

software part number has changed, please contact your navigation database account

service provider to verify you are receiving the correct database.

NOTE: The Honeywell navigation database information as indicated on the NAV

IDENT page of the FMS is subject to change.

(5) For more information regarding this SIL, contact the applicable Honeywell field service

engineer or the location identified below.

Honeywell

Global Customer Care Center

Telephone: (800) 601-3099 (Toll Free U.S.A./Canada)

Telephone: (602) 365-3099 (International Direct)

Telephone: 00-800-601-30999 (EMEA Toll Free)

Telephone: 420-234-625-500 (EMEA Direct)

9 Nov 2010

Revision 2 24 May 2011 Page 17

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S.I.L. HONEYWELL-24-May-2011