serviceinformationletter - pilatus pc-12

Honeywell International Inc.21111 N. 19th AvenuePhoenix, Arizona 85027-2708U.S.A.CAGE: 55939Telephone: 800-601-3099 (Toll Free U.S.A./Canada)Telephone: 602-365-3099 (International Direct)

Website: www.myaerospace.com

SERVICE INFORMATION LETTERNZ-2000/NZ-2010/FMZ-2000/PRIMUS Apex/PRIMUS Epic/NG Flight Management System (FMS):NZ-2000/2010 and FMZ-2000/IC-615/IC-800/IC-810/IC-1080; Reduction of Navigation DatabaseProcedures Content due to FMS Lateral Navigation (LNAV) Display/Guidance Issues

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THIS DOCUMENT CONTAINS INFORMATION THAT IS THE JOINT PROPERTY OF HONEYWELLINTERNATIONAL INC., AND GENERAL ELECTRIC, PARTNERS OF CFE COMPANY. THIS DOCUMENTMAY NOT, IN WHOLE OR IN PART, BE DUPLICATED OR DISCLOSED OR USED FOR MANUFACTURE OFTHE PART DISCLOSED HEREIN, WITHOUT THE PRIOR WRITTEN PERMISSION OF THE OWNER.

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9 Nov 2010Revision 24, 22 Jun 2018 of 52

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

SERVICE INFORMATION LETTER

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This document and the information contained herein (“the Materials”) are the proprietary data ofHoneywell. These Materials are provided for the exclusive use of Honeywell-authorized Service Centers;Honeywell-authorized repair facilities; owners of a Honeywell aerospace product that is the subject ofthese Materials (“Honeywell Product”) that have entered into a written agreement with Honeywell relatingto the repair or maintenance of Honeywell Product; and direct recipients of Materials from Honeywell viahttps://myaerospace.honeywell.com/wps/portal/ that own a Honeywell Product. The terms and conditions ofthis Honeywell Materials License Agreement (“License Agreement”) govern your use of these Materials, exceptto the extent that any terms and conditions of another applicable agreement with Honeywell regarding themaintenance or repair of a Honeywell Product and that is the subject of the Materials conflict with the termsand conditions of this License Agreement, in which case the terms and conditions of the other agreement willgovern. However, this License Agreement will govern in the event of a conflict between these terms andconditions and those of a purchase order or acknowledgement. Your access or use of the Materials representsyour acceptance of the terms of this License Agreement.

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Copyright - Notice

Copyright 2010, 2018 Honeywell International Inc. All rights reserved.

Honeywell is a registered trademark of Honeywell International Inc.

All other marks are owned by their respective companies.THIS IS THE SB FOSI - DATE: 20170130




Transmittal InformationPublication Number D201011000003

SummaryThis revision is a FULL replacement. This revision includes the changes that follow:• Changed the content and format to agree with Honeywell processes in effect at the time of the release of

this revision.• Added Revision 23 and 24 in Service Information Letter Revision and Item Data, Table 2.• Added PN EB7030191-00111 thru -00115 to Leonardo AW139 in Table 3 and Table 4.• Added Gulfstream G500/G600 with PN EB60001034-00102 in Table 3.• Added PN EB7036889-00212 to Dassault PRIMUS Epic F2000 in Table 3.• Added E-1 model numbers to Embraer in Table 3.• Added Embraer E-1 170/175/190/195/Lineage 1000 and PN PS60002067-0306 (Load 27.1) in Table 3.• Deleted PN EB7036889-00112 for Dassault Primus EPIC F900 in Table 3. Revision bars are not used.• Deleted PN PS7027709-00124 and PN PS7027709-00126 for Embraer 170 in Table 3. Revision bars

are not used.• Delete PN PS7027709-00215 thru -00216 for Embraer 190 in Table 3. Revision bars are not used.• Delete PN EB7031236-00320 for Gulfstream G550 in Table 3. Revision bars are not used.• Added PN EB7038683-00106 to Gulfstream G650/G650ER in Table 3.• Delete PN EB7037248-00103 for Pilatus PC-12NG in Table 3. Revision bars are not used.• Changed Step (16)(a) for Item P in Summary Anomalies.• Added Step (19) for Item S in Summary Anomalies.• Changed the content in Table 4.• Added approximate number of procedures removed as 100 to item S in Table 4.• Added Dassault F8X with PN EB60001546-00109 and PN EB60001546-00111 in Table 3 and Table 4.• Added Leonardo AW139 with PN EB7030191-00109 in Table 4.• Added PN EB7031847-00115 to Cessna Sovereign in Table 4.• Added Embraer Aircraft to Table 4.• Deleted Dassault PRIMUS Epic F900 with PN EB7036889-00112 and Dassault PRIMUS Epic F900 with

PN EB7036889-00116 in Table 4. Revision bars are not used.• Deleted Embraer 170 with PN PS7027709-00124 and Embraer 170 with PN PS7027709-00126 in Table

4. Revision bars are not used.• Deleted Gulfstream G350/450 with PN EB7031236-00410, PN EB7031236-00409, -00414, PN

EB7031236-00415, and PN EB7031236-00418 in Table 4. Revision bars are not used.• Deleted Gulfstream 550 with PN EB7031236-00416, PN EB7031236-00315, -00501, PN

EB7031236-00316, PN EB7031236-00320, and PN EB7031236-00322 in Table 4. Revision bars are not used.

• Deleted Gulfstream G500/550, PN EB7031236-00317 in Table 4. Revision bars are not used.• Added PN EB7038683-0106 to Gulfstream G650/G650ER in Table 4.• Deleted Pilatus PC-12NG, PN EB7037248-00103 in Table 4. Revision bars are not used.• Added Gulfstream G500/G600 with PN EB60001034-00102 in Table 4.




• Added Cessna Citation Bravo/Encore/Excel/XLS, PN 7017000-94816,-95816,-98805, -99805, -98827,-98853, -99853, Dassault F900C/EX, PN 7017300-4XX27 in Table 4.

• Changed the content in Action.

Revision History

This service information letter has had twenty-four revisions as shown in Table 1.

Table 1. Revision History

Revision Number Revision Date0 9 Nov 2010

1 2 Feb 2011

2 24 May 2011

3 1 Jul 2011

4 26 Sep 2011

5 17 Nov 2011

6 9 Dec 2011

7 17 Jan 2012

8 17 May 2012

9 14 Sep 2012

10 11 Mar 2013

11 23 Apr 2013

12 29 May 2013

13 28 Feb 2014

14 14 Mar 2014

15 27 Feb 2015

16 28 Apr 2015

17 2 Jul 2015

18 13 Jul 2015

19 15 Sep 2015

20 14 Dec 2015

21 7 Nov 2016

22 18 Apr 2017

23 25 Apr 2017

24 22 Jun 2018




Table 2 identifies the revision of the service information letter when the specified item data was added.

Table 2. Service Information Letter Revision and Item Data

RevisionReason forRevision Item Issue

SILRevisionAdded Comments

A Procedures containing a coursechange of 180 degrees or more.

-

B Procedures containing right turnarcs.

-

C Standard instrument departures(SID) / standard terminal arrivalroutes (STAR) combinations.

-

- Initial release.

D Final approach overshoot. -

1 Minor formattingchanges.

E FMS/LNAV loss of turn directionon SID or approach.

2

F Missed approach activation. 2

2 Added Items E,F, and G. Minorformatting changesand updated Table4. G FLY XXX OR AS ASSIGNED

heading legs.2 Superseded SIL,

Publication NumberD201012000014.

3 Minor formattingchanges andupdated Table 4.

4 Updated Table 4.

5 Added Item H. H Procedure turns less than 10nautical miles (NM) (18.5 km).

5

6 Added Item I. I Continuous 360 degree turn. 6

7 Minor formattingchanges andupdated Table 4.

8 Minor formattingchanges, updatedItem D and Table 4.

Added Item J. J Direct leg early sequencing. 99

Added Item K. K Course to fix (CF) flight planlegs.

9




Table 2. Service Information Letter Revision and Item Data (Cont)



10 Updated Table 4- to add Item Land the affectedaircraft. ChangedNote 1 and addedNote 2.

L Direct leg back to previouswaypoint

10

M Altitude leg sequence 11 Superseded SIL,Publication NumberD201212000036.

11 Added Items M andN.

N First leg of missed approach is aradius to fix leg

11 Superseded SIL,Publication NumberD201109000024.

12 Minor formattingchanges, updatedTable 3.

13 Added Item O. O SID or missed approach withsignificant turns before and afteran altitude leg

13

14 Minor formattingchanges, updatedItem O and Table 4.

15 Added Item P. P Tear drop followed by 270degree turn

15

16 Added Item Q. Q SID procedures with largecourse change and altitude legs

16

17 Minor formattingchanges andupdated Table 3and Table 4.

18 Updated Table 3and Table 4.

19 Added Item R andupdated Table 4.

R Next waypoint behind issue. 19

20 Updated Table 4.






Table 2. Service Information Letter Revision and Item Data (Cont)




24 Updated Item Pand added Item S.Updated Table 4.

S Missed Approach Point Prior toRunway Threshold

24




Blank Page




1. General Information

A. Effectivity

(1) This service information letter is applicable to the equipment Table 3 identified in

Table 3. Effectivity Configuration Data

Equipment Model or Aircraft Identification Part Number and/or LoadNZ-2000/NZ-2010/FMZ-2000/PRIMUSApex/PRIMUS Epic FMS: NZ-2000/2010 andFMZ-2000/IC-615/IC-800/IC-810/IC-1080

PN 7018879-01001, -01002, -02003 thru -02007,-02010, -02017, -03008, -03012, -03014, -03016,-03018, -03020, -03022, -03024, -03026, -03028,-03030, -03032, -03034, -03036, -03036 (MOD A),-03038, -03040, -03042, -03044, -10000, -11009,-11015, -11019, -11021, -11023, -11024, -11025PN 7017000-21XXX, -94XXX, -95XXX, -98XXX,-99XXX,PN 7017300-01XXX, -11XXX, -21XXX, -31XXX,-41XXX, -43XXX, -45XXX, -56XXX, -56026, -56027,-6100X, -61010, -61013, -63XXX

Leonardo AW139 PN EB7030191-00105 (Phase 4),PN EB7030191-00107 (Phase 5),PN EB7030191-00108 (Phase 6),PN EB7030191-00109 (Phase 6),PN EB7030191-00110 (Phase 7),PN EB7030191-00111 (Phase 7),PN EB7030191-00112 (Phase 7),PN EB7030191-00114 (Phase 7),PN EB7030191-00115 (Phase 7)

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),PN EB7031847-00114 (Phase 5.2),PN EB7031847-00115 (Phase 5.3)

Dassault PRIMUS Epic F900 PN EB7036889-00114 (EASy II),PN EB7036889-00116,PN EB7036889-00117,PN EB7036889-00118,PN EB7036889-00120

Dassault PRIMUS Epic F2000 PN EB7036889-00203,PN EB7036889-00205,PN EB7036889-00206,PN EB7036889-00207,PN EB7036889-00208,PN EB7036889-00209,PN EB7036889-00212




Table 3. Effectivity Configuration Data (Cont)

Equipment Model or Aircraft Identification Part Number and/or LoadDassault F7X PN EB7034843-00103,

PN EB7034843-00102,PN EB7034843-00104,PN EB7034843-00107,PN EB7034843-00108

Dassault F8X PN EB60001546-00109,PN EB60001546-00111

Embraer E-1 170 PN PS7027709-00127 (Load 23.1),PN PS7027709-00128 (Load 21.5),PN PS7027709-00129 (Load 23.2)

Embraer E-1 190 PN PS7027709-00214 (Load 23.1),PN PS7027709-00217 (Load 23.2)

Embraer E-1 170/175/190/195/Lineage 1000 PN PS7027709-00303 (Load 25.1.0.1),PN PS7027709-00302 (Load 25.2),PN PS7027709-00304 (Load 25.3),PN PS7027709-00305 (Load 25.4),PN PS7027709-00309 (Load 25.5.0.1),PN PS7027709-00310 (Load 25.6),PN PS60002067-0306 (Load 27.1)

Gulfstream G350/450 PN EB7031236-00411 (Echo),PN EB7031236-00417 (ASC910),PN EB7031236-00420 (ASC 911),PN EB7031236-00421 (ASC 912)

Gulfstream G500/G600 PN EB60001034-00102

Gulfstream G550 PN EB7031236-00321 (ASC910),PN EB7031236-00323 (ASC 911),PN EB7031236-00325 (ASC 912)

Gulfstream G650/G650ER PN EB7038683-00103 (ASC901),PN EB7038683-00104 (ASC902),PN EB7038683-00106 (ASC902A)

Hawker 4000 PN EB7030192-001XX (Load 19),PN EB60000578-0114 (Load 20)

Pilatus PC-12NG PN EB7037248-00104 (Build 7.2),PN EB7037428-00105 (Build 8),PN EB7037428-00106 (Build 8.3.3),PN EB60000487-00108 (Build 8.6),PN EB60000487-00111 (Build 8.8)

Viking DHC6-400 PN EB7032889-00101 (Load 1.3),PN EB60002734-0104 (Load 4.4)




B. Applicability

(1) This service information letter is only applicable to equipment received from OriginalEquipment Manufacturers or equipment received from in-service aircraft. Aircrafttail number should be provided, as applicable. This service information letter is notapplicable to excess equipment and equipment removed from parked or dismantledaircraft.

C. Reason

CAUTION: SOME STANDARD INSTRUMENT DEPARTURES, STANDARD TERMINALARRIVAL ROUTES, TRANSITIONS, AND APPROACHES ARE NOT INTHE DATABASE DUE TO LIMITATIONS OF THE FMS. ADDITIONALPROCEDURES HAVE BEEN REMOVED TO ADDRESS THE ANOMALIESDISCUSSED IN THIS SERVICE INFORMATION LETTER. THE FLIGHTCREW SHOULD TAKE EXTRA CAUTION TO VERIFY DATABASE CONTENTDURING PREFLIGHT PLANNING.

CAUTION: WHEN FLYING ANY PROCEDURES USING THE FMS, THE FLIGHT CREWSHOULD MONITOR AIRCRAFT GUIDANCE TO ENSURE TURN DIRECTIONIS CONSISTENT WITH THE PUBLISHED PROCEDURE.

(1) The purpose of this service information letter is to advise all affected operators listedon Page 1 of this service information letter of anomalies that may occur with certainterminal area procedures and Honeywell's action to prevent them from occurring. Onlytop level system part numbers listed in the part number field of this service informationletter 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 aircraftshould utilize the NZ-2000 hardware part number.

NOTE: For PRIMUS Apex and Dassault EASy aircraft, the top level system partnumber can be obtained from the system configuration tab. Dassault EASysystem configuration tab shown in Figure 1.




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

NOTE: For FMZ2000 systems, the software version may be used in conjunctionwith Table 4. The software version is indicated by SW on the NAV IDENTpage (push the buttons NAV, NEXT, then the line select key next to IDENT).Refer to Figure 2.

Figure 2. (Sheet 1 of 1) NAV IDENT Page

NOTE: For all multi-function control display unit (MCDU) equipped aircraft, the toplevel system part number can be obtained from the system configurationpage on the multi-function display (MFD). Hawker 4000 example shownin Figure 3.




Figure 3. (Sheet 1 of 1) Hawker 4000 Example

(3) Problem(a) 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 Athru K (refer to Paragraph 1.E.(1) thru Paragraph 1.E.(11)). The data providedin the aircraft matrix table (refer to Table 4 in Paragraph 1.E.(19)) is effective in2012 navigation database Cycle 05. Actual number of removed procedureswill vary each cycle.NOTE: The majority of procedures that have been removed from the

database are conventional short range navigation (e.g. VOR,VOR/DME, NDB, ILS) and may be flown using the short rangenavigation receivers on the aircraft.

(b) Honeywell will continue to evaluate procedures each navigation databasecycle to ensure that only problematic procedures are removed. A navigationdatabase process is in place to ensure that all anomalies listed in this serviceinformation letter are addressed by removing affected procedures.NOTE: This service information letter has been revised to include the FLY

XXX OR AS ASSIGNED heading leg issue previously addressed inService Information Letter, Publication Number D201012000014.Service Information Letter, Publication Number D201012000014,has been superseded by this service information letter and shouldno longer be used in reference to this anomaly.

D. References

(1) To find, see, and download Honeywell Technical Publications, go towww.myaerospace.com.

(2) The document(s) that follow(s) is/are related to this service information letter. Unlessspecified differently, you can use subsequent revisions.• Database Services Bulletin, DSB201505001, R0




• Instruction manual (IM), ATA Number 20-00-03 (Publication NumberA09-1100-004), Revision 8, Standard Repair Procedures for Honeywell AvionicsEquipment Instruction Manual

• Component Maintenance Manual (CMM), ATA Number 22-11-96 (PublicationNumber A09-6112-002), Revision 8, IC-500/HG-200 Display Guidance Computerand IC-600/IC-615/IC-1080 Integrated Avionics Computer.

E. 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. Thisexcludes holding patterns and procedure turns, which are flown correctly:• Last leg of a procedure contains a course change of 180 degrees or

greater.• 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 4): KGPI SKOTT 2 SID RWY02 – LNAVincorrect turn to FCA as indicated by red arrow. When common waypointbecomes the active leg, map display and lateral guidance are incorrect. Referto Figure 4.

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




(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 arctermination

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

NOTE: Many procedures containing right turn arcs have been removedfrom the database.

(b) Example of Item B (refer to Figure 5): RJBB MAYAH STAR entered in flightplan, LNAV guidance is incorrect and opposite of course indication on MFD.

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




(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 6): KDVT 1 departure and KTUS DINGO 5arrival entered in flight plan.

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




(4) Item D

(a) Final approach overshoot/incorrect turn:

• STAR, approach transition and approach contain common waypoint.

NOTE: Only problematic approach transitions are removed from thenavigation database.

(b) Example 1 of Item D (refer to Figure 7): RJBB ILS 6R – ALLAN waypoint iscommon to arrival, approach transition, and approach. FMS overflies ALLAN,the common waypoint.

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

(c) Example 2 of Item D (refer to Figure 8): RJNA ILS 34 - EXPOH waypointis common to arrival, approach transition and approach. FMS overfliesEXPOH, the common waypoint, turns a full 360 degrees, overflies EXPOHand continues the approach.




Figure 8. (Sheet 1 of 1) Example 2 of Item D




(5) Item E

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

• 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 altitudeconstraint prior to sequencing the *ALT waypoint.

(b) Example of Item E (refer to Figure 9): MCDU displays the correct left turn toPXR, FMS may turn right if aircraft is above 4,000 feet prior to sequencing*ALT07 waypoint.

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




(6) Item F

(a) Missed approach activation:


• 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 willchange the turn direction displayed on the MCDU.

(b) Example of Item F (refer to Figure 10): UATG RWY14 - missed approach isactivated - FMS incorrectly changes the turn direction to left on the MCDU,LNAV makes an incorrect left turn.

Figure 10. (Sheet 1 of 1) Example of Item F




(7) Item G

(a) FLY XXX OR AS ASSIGNED heading legs:


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

• FMS will turn in direction of least course change.

NOTE: Previously addressed in Service Information Letter, PublicationNumber D201012000014 (superseded). Procedures, which containheading legs with a course change of 160 degrees or greater havebeen removed from the navigation database beginning in 2011,Cycle 06.

(b) Example of Item G (refer to Figure 11): UATG RWY14 – right turn heading legto 322 degrees, FMS incorrectly turns left.

Figure 11. (Sheet 1 of 1) Example of Item G




(8) Item H

(a) Procedure turns less than 10 NM (18.5 km):

• Procedure turns less than 10 NM (18.5 km)

• Speeds greater than 200 knots (370 kph) groundspeed

• FMS commands a turn that will result in an airspace violation as theaircraft will fly outside of the airspace boundary

• For PN 7017300-61010, the FMS may command a turn opposite thepublished procedure if flown above 250 knots (463 kph) groundspeed.

• Only the affected transitions are removed, not the entire procedure.

(b) Example of Item H:

1 The ACTIVE FLT PLAN screen in Figure 12 shows the CYZR RWY14,BAC14.ZR approach. Note the P next to DURPO indicating aprocedure turn.

Figure 12. (Sheet 1 of 1) Procedure Turn Shown for DURPO

2 In Figure 13 (For PN 7017300-61010 only), the FMS approximatetrack based on approximate speed shows the aircraft outside ofboundary or turning the wrong direction.




Figure 13. (Sheet 1 of 1) For PN 7017300-61010 Only: Approximate Aircraft Track, Boundary LimitCircled in Yellow

3 In Figure 14, colored lines show the approximate aircraft track atdifferent speeds. The boundary limit circled in yellow




Figure 14. (Sheet 1 of 1) Approximate Aircraft Track at Different Speeds, Boundary Limit Circled inYellow




(9) Item I

(a) Continuous 360 degree turn:• Procedure containing DF-AF (direct to a fix leg – arc to a fix leg)

combinations

• FMS may command a continuous 360 degree turn (left or right) with noattempt to return to the published procedure.

(b) Example of Item I (refer to Figure 15): LICT, MEGAN1F STAR, FMSsequences LOPKO and D221S at the same time, aircraft turns opposite of theprocedure and will fly a continuous 360 degree turn.

Figure 15. (Sheet 1 of 1) Example of Item I

(10) Item J

(a) Direct leg early sequencing:• Course changes greater than 180 degrees• Small radius of course reversal• SID and missed approach procedures (MAP)

• FMS may command turn in wrong direction.

(b) Example 1 of Item J (refer to Figure 16): ZYYJ KAN01D SID, FMS sequencesthe YNJ leg early, and turns right (see red line) to KANVU as there is aspecified right turn to KANVU.




Figure 16. (Sheet 1 of 1) Example 1 of Item J

(c) Example 2 of Item J (refer to Figure 17): EDMA KPT7F SID, FMS sequencesMA034 and immediately MA035 resulting in the FMS calculating a shortestcourse change to AUG in a right turn.

Figure 17. (Sheet 1 of 1) Example 2 of Item J




(11) Item K

(a) Course to fix (CF) flight plan legs:

• Approach transition selection may result in early sequence of previous leg

• Flight plan leg prior to CF leg has course change of 180 degrees or greater

• FMS may command turn in wrong direction.

NOTE: The problematic approach transitions are removed from thenavigation database.

(b) Example of Item K (refer to Figure 18): EGSS ABBOT1C STAR, ABBOTapproach transition, FMS sequences LAPRA and immediately sequencesABBOT. The FMS turns to the course of the next leg and results in the flightpath referenced in red.

Figure 18. (Sheet 1 of 1) Example of Item K

(12) Item L

(a) Direct leg back to previous waypoint:

• Procedure with a direct-to a fix leg (DF) back to the previous waypoint.

• Any of the following combinations for the two waypoints: track/course/directto a fix (TF/CF/DF) preceding a DF with a defined turn direction in aterminal area procedure.

• FMS will remove the second DF leg of the procedure and may command aturn in the wrong direction.

(b) Refer to Figure 19: ZLIC LUV13D SID, FMS is expected to show two MNBwaypoints.




Figure 19. (Sheet 1 of 1) Expected Delay

(c) Example 1 of Item L (refer to Figure 20): ZLIC LUV13D SID, FMS removesthe second MNB (and the corresponding right turn direction) as is shown onthe MCDU and commands a left turn to D099O.

Figure 20. (Sheet 1 of 1) Example 1 of Item L




(13) Item M

(a) Altitude leg sequence:

• Procedure with a altitude leg (fix to an altitude [FA] / climb to / proceed toaltitude X / turn X when altitude Y has been reached / and others) followedby a direct to a fix leg (DF).

• DF leg results in a 180 degree or greater turn.

• FMS may drop the DF leg once the FA has sequenced and command aturn in the incorrect direction to the subsequent waypoint.

NOTE: Previously addressed in SIL, Publication Number D201212000036(superseded). Procedures have been removed from the navigationdatabase beginning in 2013, Cycle 05.

(b) Refer to Figure 21: RJBD, RWY15, VORDME15 missed approach, theexpected missed approach as shown on the MCDU.

Figure 21. (Sheet 1 of 1) MCDU Display of VORDME15 (RJBD) Missed Approach

(c) Example 1 of Item M (refer to Figure 22): RJBD, VORDME15 missedapproach. Blue line indicates approximate path of the aircraft with respect tothe published procedure. In this example the FMS reached the expectedaltitude of 4,000 feet just prior to turning back to the 270 radial. The *ALT05leg sequenced as well as the DF leg including the left turn (L in inverse video)to NKE. The FMS commands an incorrect turn towards the hold at NKE.

NOTE: In newer versions of EPIC software, LNAV may disconnect insteadof turning in the wrong direction. Example 1 only applies to EPICFMS certifications.




Figure 22. (Sheet 1 of 1) Example 1 of Item M

(d) Example 2 of Item M (refer to Figure 23): RJBD, VORDME15 missedapproach. The red line indicates approximate path of the aircraft with respectto the published procedure. In this example the FMS reached the expectedaltitude of 4,000 feet prior to turning back to the 270 radial. The *ALT05 leghas sequenced as well as the DF leg including the left turn (L in inverse video)to NKE and the FMS makes a tighter turn back towards the hold at NKE.

NOTE: Example 2 applies to all affected versions of NO and EPIC FMS.




Figure 23. (Sheet 1 of 1) Example 2 of Item M




(14) Item N

(a) First leg of missed approach is a radius to fix leg:

• Procedure with a radius to fix leg (RF) as the first leg of the missedapproach procedure.

• Missed approach is activated after the missed approach point.

NOTE: Previously addressed in SIL, Publication Number D201109000024(superseded). Procedures have been removed from the navigationdatabase beginning in 2011, Cycle 11.

(b) Refer to Figure 24: KTEB, RNAV (RNP) RWY19, missed approach. Themissed approach point is circled in red.

Figure 24. (Sheet 1 of 1) KTEB RNAV (RNP) RWY19 MAP

(c) Example of Item N (refer to Figure 25): missed approach is activated aftersequencing JAPIR, display shows the yellow line indicating a left turn althoughthe missed approach requires a right turn (reference the magenta line).




Figure 25. (Sheet 1 of 1) Example of Item N




(15) Item O

(a) SID or missed approach with significant turns before and after an altitude leg:

• Procedures with course change of 90 degrees or more prior to the altitude(displayed on MCDU as *ALT) leg

• Procedures with course change of 180 degrees or more after the *ALT leg

• Altitude terminating leg precedes direct to a fix leg (DF)

• Aircraft has reached an altitude which is just below the specified altitudeconstraint prior to sequencing the *ALT waypoint

• Aircraft reaches the specified altitude constraint prior to turning to theinbound course of the *ALT waypoint.

(b) Example of Item O (refer to Figure 26 and Figure 27): YBTL, RWY19 BOWLY3Departure – MCDU (Figure 26) displays the correct left turn to TL; FMS mayturn right to TL if aircraft reaches 2,000 feet immediately after the *ALT01becomes the TO waypoint and as the FMS commands a turn to the 105degree course to *ALT01 waypoint.

Figure 26. (Sheet 1 of 1) YBTL RWY19 BOWLY3 SID




Figure 27. (Sheet 1 of 1) FMS may Command Incorrect Right Turn (Red Arrow)

(16) Item P

(a) Tear drop followed by 270 degree turn:

• Procedures with leg combinations DF-DF-CI/VI and CA-DF-CI/VI

• DF-DF with turn flag direction-CI/VI with Turn Direction, and Distancebetween two DF legs is less than 1 NM

• CA-DF with turn flag direction-CI/VI with Turn Direction, and Distancebetween CA termination point and DF leg is less than 1 NM.

(b) Example of Item P: LICB, RWY 23 OBAXU 5A Departure. Refer to Figure 28.– Once the aircraft sequences the *ALT01 waypoint, there is a right turn flagwith a flyover back to the COM VOR. The FMS does not comply with this firstturn flag per the Lufthansa integrated dispatch operation (LIDO) chart as ittakes the shortest lateral distance and attempts to turn left to join the R327radial. Refer to red dotted line in Figure 29.




Figure 28. (Sheet 1 of 1) OBAX 5A Procedure Review




Figure 29. (Sheet 1 of 1) LIDO Chart Sample




(17) Item Q

(a) SID procedures and missed approaches with large course change and altitudelegs:

• Procedures with xA (CA, FA, VA) legs that have large course changes

• If aircraft reaches 2,000 ft before making a left turn, the direct to fix (DF)leg becomes active and the FMS turns right.

(b) Example of Item Q: Aircraft reaches the 2,000 ft before having turned left ofthe NN VOR towards 270 degree and sequences the *ALT leg early basedon altitude only. The direct to fix (DF) leg becomes active causing a right turnfrom the FMS and a right 360 is flown before proceeding to the NADI VOR (redline diagram). The leg combination in this case is CA-CA-DF with databaseturn directions encoded on both the CA-DF. Refer to Figure 30.

Figure 30. (Sheet 1 of 1) NFFN Alpha RW02




(18) Item R

(a) Next Waypoint behind Issue:• Affects SIDs and approach procedures• Procedures with xF-CF waypoint combination and a turn direction on the

CF and course change of 135 degrees or more.• The location of the xF leg is not within a 45 degree window from the CF

leg inbound course.

• The cross track of xF leg onto the CF leg is more than 3.3 NM (6.11 km)based on 200 knots.

(b) Example of Item R: LIMC, RWY 35R, MMP 5S Departure – Issue is observedwhen the aircraft is on a radial from the VOR that is directly behind it and whenthe next waypoint in the procedure is more than 45 degrees from the previouswaypoint course. Refer to Figure 31.

Figure 31. (Sheet 1 of 1) LIMC SID MMP 5S RW 35R

(19) Item S

(a) Missed Approach Point Prior to Runway Threshold.

1 Approach procedures that meet the following criteria:• Non Circling and non-Localizer based Approaches• Missed Approach Point (MAP) is not beyond runway threshold

and is greater than 0.3 nm from runway threshold




• First missed approach leg is a fixed track/path (CF, FA, FC, FD,FM, or TF)

• Difference from the course into the MAP and the course into thefirst missed approach leg is greater than 10°.

(b) Example of Item S: NZMO RNAV (GNSS) RW 26. As shown by the red dottedline in Figure 32, the FMS will command the incorrect turn prior to the missedapproach being activated. The incorrect turn will be commanded until the FMSsequences the MAP and LNAV disengages (by design).

Figure 32. (Sheet 1 of 1) NZMO RNAV (GNSS) RW 26

(20) Aircraft Matrix TableRefer to Table 4 to identify the approximate number of procedures removed from thedatabase cross referenced to the anomaly and aircraft type.




Table 4. Aircraft Matrix Table - Items A Thru S

Item A B C D E F G H I J K L M N O P Q R S

ApproximateNumber ofProceduresRemoved 1

675 381 60 1387 138 824 452 110 31 313 1 2 13 6 157 5 70 105 100

Aircraft X indicates database removal for itemLeonardo AW139,PN EB7030191-00105 (Phase 4)

X X X X X X X X

Leonardo AW139,PN EB7030191-00107 (Phase 5)

X X X X X X X X X X X X




X X X X

Leonardo AW139,PN EB7030191-00110, 00111,00112, 00114,00115 (Phase 7)

X X X

Cessna Sovereign,PN EB7031847-00105 (Phase 3)

X X X X X X X X X X X X X



Cessna Sovereign,PN EB7031847-00108 (Phase4.1)


Cessna Sovereign,PN EB7031847-00109 (Phase4.2)



X X X X X X X X X X X X X X X X




Table 4. Aircraft Matrix Table - Items A Thru S (Cont)



675 381 60 1387 138 824 452 110 31 313 1 2 13 6 157 5 70 105 100

Aircraft X indicates database removal for itemCessna Sovereign,PN EB7031847-00114(Phase 5.2),PN EB7031847-00115 (Phase 5.3)

X X X X X X

Dassault PRIMUSEpic F900,PN EB7036889-00114 (EASy II)

X X X X X X X X X X

Dassault PRIMUSEpic F900,PN EB7036889-00117

X X X


X X X


X X X








X X X







675 381 60 1387 138 824 452 110 31 313 1 2 13 6 157 5 70 105 100

Aircraft X indicates database removal for itemDassault PRIMUSEpic F2000,PN EB7036889-00208

X X X


X X X

Dassault F7X,PN EB7034843-00103





X X X


X X X


X X X

Dassault F8X,PN EB60001546-00109, PNEB60001546-00111

X

Embraer 170,PN PS7027709-00127 (Load 23.1)












675 381 60 1387 138 824 452 110 31 313 1 2 13 6 157 5 70 105 100

Aircraft X indicates database removal for itemEmbraer 190,PN PS7027709-00214 (Load 23.1)








Embraer 170/190,PN PS7027709-00303 (Load25.1.0.1)

X X X X X X X X X X X X X X

Embraer 170/190,PN PS7027709-00304 (Load 25.3)

X X X


X X X X X X X X X

Embraer 170/190,PN PS7027709-00309 (Load25.5.0.1),PS7027709-00310 (Load 25.6)

X X X


X X X X X X

Embraer175/195, PNPS60002067-0306(Load 27.1)

X







675 381 60 1387 138 824 452 110 31 313 1 2 13 6 157 5 70 105 100

Aircraft X indicates database removal for itemGulfstreamG350/450,PN EB7031236-00411 (Echo)


GulfstreamG350/450,PN EB7031236-00417 (ASC 910)

X X X X X X


X X X


X X X

Gulfstream 550,PN EB7031236-00321 (ASC 910)

X X X X X X


X X X


X X X

GulfstreamG500/G600,PN EB60001034-00102

X

GulfstreamG650/G650ER,PN EB7038683-0103 (ASC901),PN EB7038683-0104 (ASC902),PN EB7038683-0106 (ASC902A)

X X







675 381 60 1387 138 824 452 110 31 313 1 2 13 6 157 5 70 105 100

Aircraft X indicates database removal for itemHawker 4000,PN EB7030192-001XX (Load 19)


Hawker 4000,PN EB60000578-0114 (Load 20)

X X X X X X X X

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

X X X X X X X X X X X X X X

Pilatus PC-12NG,PN EB7037248-00105 (Build 8)

X X X X X X X

PilatusPC-12NG, PNEB7037248-00106(Build 8.3.3)

X X X X X X


X X X


X X X

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

X X X X X X X X X X X X X X X

Viking DHC6-400,PN EB60002734-0104 (Load 4.4)

X X X







675 381 60 1387 138 824 452 110 31 313 1 2 13 6 157 5 70 105 100

Aircraft X indicates database removal for itemNZ-2000/2010 andFMZ-2000/IC-615/IC -800/IC-810/IC-1080,PN 7018879-01001, -01002,-02003 thru-02007, -02010,-02017, -03008,-03014, -03016,-03018, -03020,-03022, -03024,-03026, -03028,-03030, -10000,-11009, -11015,-11019, -11021,-11023, PN7017000 -21XXX,-94XXX, -95XXX,-98XXX, -99XXX,PN 7017300-01XXX, -11XXX,-21XXX, -31XXX,-41XXX, -43XXX,-45XXX, -56XXX,-6100X, -63XXX(NZ4.X, 5.X, 6.0)


PN 7018879-03032, -03034(NZ6.1)

X X X X X X X X X X X X X X X

NZ-2010, PN7018879 -03036,-03036 MOD A,-03038 (NZ6.1)

X X X X X X X X X







675 381 60 1387 138 824 452 110 31 313 1 2 13 6 157 5 70 105 100

Aircraft X indicates database removal for itemNZ-2010,PN 7018879-11024, -11025-03040, -03042(NZ6.1)IC-810,PN 7017300-31554, -31564,-4XX25, -4XX26,-56026, -56027,(NZ6.1)

X X X X X

NZ-2010,PN 7018879-03044 (NZ6.1),IC-810,Bombardier GEX,PN 7017300-61013 (NZ6.1),Cessna CitationX, PN 7017300-31574,Cessna CitationBravo/ Encore/Excel/ XLS,PN 7017000-94816, -95816,-98805, -99805,-98827, -98853,-99853 (NZ6.1),DassaultF900C/EX,PN 7017300-4XX27 (NZ6.1)

X

IC-810,BombardierGEX Batch 3,PN 7017300-61010 (NZ6.1)

X X X X X X X X X

NOTE:1. Data displayed for 2018, Cycle 06 and will vary each cycle.




F. Action

(1) To prevent the problems from occurring, Honeywell is analyzing and removingprocedures from the navigation database that can cause incorrect guidance. As furtheranalysis is performed, additional procedures may be removed from the database. Todetermine the appropriate database for each aircraft configuration, reference oneof the following links to access the Database Services Bulletin (DSB201505001):ads.honeywell.com → Flight Info → Alerts/Notices or inds.epicinds.com → Flight Info→ Alerts/Notices.

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

(a) For aircraft equipped with charts/maps (EPIC Integrated Navigation DataService users):

1 Go to www.epicinds.com.

2 Select Flight Info (upper left side).

3 Select Content/Procedures.

4 Select the applicable navigation database that applies to the aircraft.

5 Select the spreadsheet under the Removed Procedures column onthe right side that is applicable to the aircraft navigation database.

(b) For all other aircraft:

1 Go to www.honeywellaes.com.

2 Select Flight Info (upper left side).

3 Select Content/Procedures.

4 Follow the instructions to determine the applicable navigationdatabase identifier (database identification [ID]).

5 Select the spreadsheet under the reports column on the right side thatis applicable to the navigation database ID.

CAUTION: WHEN FLYING ANY PROCEDURES USING THE FLIGHT MANAGEMENTSYSTEM, THE FLIGHT CREW SHOULD MONITOR AIRCRAFT GUIDANCETO ENSURE TURN DIRECTION IS CONSISTENT WITH THE PUBLISHEDPROCEDURE.

(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 operationalsoftware part number has changed, please contact your navigation database accountservice provider to verify you are receiving the correct database.

NOTE: The Honeywell navigation database information as indicated on the NAVIDENT page of the FMS is subject to change.




G. Contact Information

(1) The Honeywell Aerospace Technical Support (ATS) team can be contacted foradditional information on this SIL.

Honeywell Aerospace Technical SupportTelephone: 855-808-6500 (Toll Free U.S.A./Canada)Telephone: 602-365-6500 (International Direct)Option 1 for Avionics or Option 2 for Mechanical.E-mail: [email protected]



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