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F2000Airplane

Flight Manual

SUPPLEMENT 21A/C WITH FMS (GNS-X/ES) MOD 1 OR MOD 2 OR MOD 3

Table of contents Issue 1

DTM537

EASA APPROVED

SUPPLEMENT No 21 TO THE EASA APPROVED FLIGHT MANUAL

CONCERNING

AIRPLANE EQUIPPED WITH FMS (GNSX/ES) MOD 1 OR MOD 2 OR MOD 3

Serial No :

Registration No :

This supplement must be attached to the DTM537 Airplane Flight Manual approved by the DGAC onNovember 30, 1994.

The information contained in this supplement, supplements that of sections 1 thru 5 and annexes.The limitations, procedures and performance information which do not appear in this supplementremain these of sections 1 thru 5 and annexes.

SECTIONS OF AIRPLANE FLIGHT MANUAL PARTS OF SUPPLEMENT

- Section 1 : LIMITATIONS..........................................................................................................Part 1

- Section 2 : EMERGENCY PROCEDURES ....................................................................... No change

- Section 3 : ABNORMAL PROCEDURES.......................................................................... No change

- Section 4 : NORMAL PROCEDURES............................................................................... No change

- Section 5 : PERFORMANCE ............................................................................................ No change

- Annexes :......................................................................................................................... No change

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SUPPLEMENT 21A/C WITH FMS (GNS-X/ES) MOD 1 OR MOD 2 OR MOD 3

Table of contents

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

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y

LIST OF REVISIONS

Parts changesRevisionand Date

Titleand

Approval reference Added Revised Removed

Original

17-oct-2000

Approved by DGAC. First issue of supplement 21.

Revision 1

12-jul-2010

New page layout.

Approved under DOA EASA.21.J.051authority under change referenceM3346.

Part 0 Issue 1

Part 1 Issue 1

All pages.

LIST OF EFFECTIVE PARTS

Reference Issue Special applicability

Part 0 Issue 1

Part 1 Issue 1

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F2000Airplane

Flight Manual

SUPPLEMENT 21A/C WITH FMS (GNS-X/ES) MOD 1 OR MOD 2 OR MOD 3

Limitations Issue 1

DTM537

EASA APPROVED

LIMITATIONS

GENERAL

The FMSs meet the accuracy criteria of AC 90.45A and AC 20.130A for en-route, terminal andapproach areas provided the FMS is not in DR and excepted when POS WARN (Position Warning)FMS message is displayed on the CDU.

The minimum navigation performance required by NAT MNPS regulations (French arrt ofNovember 5th, 1987 and FAR Part 91 Appendix C) are demonstrated provided that there are at least2 FMSs and 2 IRSs in NAV mode operating on board.

LIMITATIONS

GNS-X/ES navigation must be periodically verified during the flight, by:

- Reading the Quality Factor (QF or Q).

- Comparison with the other means of radio-navigation.

To monitor the FMS with VOR DME raw data, the VPU used for monitoring should not be in autotunemode.

FUEL, TIME prediction informations are provided for advisory purposes only and must not be used forflight plan purposes.

Use of following functions is not authorized:

- LHDG.

- Holding pattern.

- VNAV.

- SID and STAR procedures.

- Approach.

Manual VOR tuning through the CDU is prohibited.Use of bearing / distance on the CDU tune page is prohibited.

GPS

- FMS may only be used for supplemental navigation when at least one GPS is used as a sensor.

- FMS may not be used with only the GPS sensor in function.

- FMS may not be used in terminal areas, approach, landing or take-off if at least one GPS is usedas a sensor.

- The FMS position must be monitored by the crew using other approved navigation means if GPS isused as a sensor.

- The raw data only, calculated by the GPS may not be used for navigation.

NOTE

PFD: in VOR source, do not use the FMS distance if the airplane is equipped with FMS (GNS XES)MOD 1.

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SUPPLEMENT 21A/C WITH FMS (GNS-X/ES) MOD 1 OR MOD 2 OR MOD 3

Limitations

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

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INTENTIONALLY LEFT BLANK