F2000 - AFM SUP22C REV02 - 20100712

8/3/2019 F2000 - AFM SUP22C REV02 - 20100712

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F2000Airplane

Flight Manual

SUPPLEMENT 22CA/C WITH FMS UNS-1C SOFTWARE 601.2

Table of contents Issue 1

DTM537

EASA APPROVED

SUPPLEMENT No 22C TO THE EASA APPROVED FLIGHT MANUAL

CONCERNING

AIRPLANE EQUIPPED WITH FMS UNS-1C SOFTWARE 601.2

AFTER INCORPORATION OF SERVICE BULLETIN F2000-91 OR M1277

Serial No :

Registration No :

This supplement must be attached to the DTM537 Airplane Flight Manual approved by the DGAC onNovember 30, 1994, when the airplane incorporates SB F2000-91 or M1277.

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 and 1A

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

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

- Section 4 : NORMAL PROCEDURES.......................................................................................Part 2

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

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Issue 1


Table of contents

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

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LIST OF REVISIONS

Parts changesRevisionand Date

Titleand

Approval reference Added Revised Removed

Original

17-oct-2000

Approved by DGAC. First issue of supplement 22C.

Original

26-nov-2001

Approved by DGAC. Pages 1, 2, 3A and4A.

Revision 2

12-jul-2010

New page layout.

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

M3346.

Part 0 Issue 1

Part 1 Issue 1

Part 1A Issue 1

Part 2 Issue 1

All pages.

LIST OF EFFECTIVE PARTS

Reference Issue Special applicability

Part 0 Issue 1

Part 1 Issue 1

Part 1A Issue 1 A/C with M2081

Part 2 Issue 1

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Part 1

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F2000Airplane

Flight Manual


Limitations Issue 1

DTM537

EASA APPROVED

LIMITATIONS

GENERAL

The FMS’s comply with AC 20-130A and in particular meet the accuracy criteria of AC 20-130A foren-route, terminal areas provided the FMS is not in Dead Reckoning (DR in PFD) and there is noPOS annunciation on any CDU pages, and satisfy the accuracy criteria of AC 20-129.

The minimum navigation performance required by NAT MNPS regulations (French “arrêté” ofNovember 5th, 1987 and FAR Part 91 Appendix C) are demonstrated provided that there are at least2 FMS’s and 2 IRS’s in NAV mode operating on board or 2 GPS or 1 IRS in NAV mode operating onboard and 1 GPS.

Dual UNS-1C GPS system operating Software Control Number (SCN) 601.2 with internal GPS sensorSCN 10.2, or later approved software versions, as installed has been found to comply with therequirements for GPS primary means of navigation in oceanic and remote airspace as defined byFAA Order 8110.60 when used in conjunction with the 10751 SCN 11.2, or later approved predictionprogram.

The here-above statement is valid if there is no FMS and/or GPS related failure message/label onPFD and CDU.

This does not constitute an operational approval.

LIMITATIONS

UNS-1C navigation must be periodically verified during the flight by:

- Reading the Quality Factor (QF or Q).

- Comparison with the other means of navigation.

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

Use of Command Heading (CMD HDG) in a configuration where Attitude and Heading sensor n°1 isan AHRS is not authorized.

APPROACH

Use of the FMS during approach is forbidden:

- Except for published RNAV procedures, a transcription of published VOR, VOR/DME, GPS overlayor ADF approach procedures.

- If the navaids specified in the procedures are not available and displayed on the EFIS and activelymonitored by the crew.

- If the APPR annunciation in the PFD is not green before FAF.

- If POS or DR annunciation is illuminated in the PFD or APPR is illuminated red in the PFD.

CAUTION

For the approach procedure where the MAP (Missed Approach Point) is located after therunway threshold, use of VNAV is forbidden. After passing the FAF (Final Approach Fix),approach must be made in Vertical Speed mode down to the MDA (Minimum DescentAltitude). The computation of the vertical speed must be done by the crew.

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Issue 1


Limitations

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

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CAUTION

Altitude constraints on FAF and MAP are automatically displayed on PFD. Modification ofthese constraints and addition of altitude constraints on other waypoints should not beattempted:

- Modification or addition of constraints done by the crew before the activation of APPROACHwill be suppressed by the system when APPROACH is activated.- After APPROACH is activated, modification or addition of constraints result in loss of FMSAPPROACH.

VNAV

Observing the Minimum Safe Altitude and obstacles clearances remains a crew responsibility.

Transition VNAV En Route / VNAV in Approach are not authorized.

The VNAV page should not be used for reference during approach phase: altitudes and path anglesare all displayed on NAV page.

GPS

GPS is not approved as a primary means of navigation for continental en-route, approach andterminal operations.

Use of the FMS during approach is forbidden for non precision GPS procedures (GPS Stand aloneApproaches).

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Part 1A

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F2000Airplane

Flight Manual


Limitations (A/C with M2081) Issue 1

DTM537

A/C with M2081

EASA APPROVED

LIMITATIONS

GENERAL

The FMS’s comply with AC 20-130A and in particular meet the accuracy criteria of AC 20-130A foren-route, terminal areas provided the FMS is not in Dead Reckoning (DR in PFD) and there is noPOS annunciation on any CDU pages, and satisfy the accuracy criteria of AC 20-129.

The minimum navigation performance required by NAT MNPS regulations (French “arrêté” ofNovember 5th, 1987 and FAR Part 91 Appendix C) are demonstrated provided that there are at least2 FMS’s and 2 IRS’s in NAV mode operating on board or 2 GPS or 1 IRS in NAV mode operating onboard and 1 GPS.

Dual UNS-1C GPS system operating Software Control Number (SCN) 601.2 with internal GPS sensorSCN 10.2, or later approved software versions, as installed has been found to comply with therequirements for GPS primary means of navigation in oceanic and remote airspace as defined byFAA Order 8110.60 when used in conjunction with the 10751 SCN 11.2, or later approved predictionprogram.

The here-above statement is valid if there is no FMS and/or GPS related failure message/label onPFD and CDU.

This does not constitute an operational approval.

LIMITATIONS

UNS-1C navigation must be periodically verified during the flight by:

- Reading the Quality Factor (QF or Q).

- Comparison with the other means of navigation.

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

Use of Command Heading (CMD HDG) in a configuration where Attitude and Heading sensor n°1 isan AHRS is not authorized.

FMS Vspeeds database A12540 are representative of Airplane Flight Manual performance charts upto Revision 9. These database take into account performance charts for take-off and landing below10,000 ft.

FMS Vspeeds database must be disregarded if Airplane Flight Manual performance charts areupdated through a revision upper than revision 9.

CAUTION

Vspeed prediction information are provided for advisory purposes only. In case ofdiscrepancy between the advanced performance mode database and the data calculated fromthe airplane documentation, the latter applies.

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Part 1A

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Issue 1


Limitations (A/C with M2081)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with M2081

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APPROACH

Use of the FMS during approach is forbidden:

- Except for published RNAV procedures, a transcription of published VOR, VOR/DME, GPS overlayor ADF approach procedures.

- If the navaids specified in the procedures are not available and displayed on the EFIS and activelymonitored by the crew.

- If the APPR annunciation in the PFD is not green before FAF.

- If POS or DR annunciation is illuminated in the PFD or APPR is illuminated red in the PFD.

CAUTION

For the approach procedure where the MAP (Missed Approach Point) is located after therunway threshold, use of VNAV is forbidden. After passing the FAF (Final Approach Fix),approach must be made in Vertical Speed mode down to the MDA (Minimum DescentAltitude). The computation of the vertical speed must be done by the crew.

CAUTION

Altitude constraints on FAF and MAP are automatically displayed on PFD. Modification ofthese constraints and addition of altitude constraints on other waypoints should not beattempted:- Modification or addition of constraints done by the crew before the activation of APPROACHwill be suppressed by the system when APPROACH is activated.- After APPROACH is activated, modification or addition of constraints result in loss of FMSAPPROACH.

VNAV

Observing the Minimum Safe Altitude and obstacles clearances remains a crew responsibility.

Transition VNAV En Route / VNAV in Approach are not authorized.

The VNAV page should not be used for reference during approach phase: altitudes and path anglesare all displayed on NAV page.

GPS

GPS is not approved as a primary means of navigation for continental en-route, approach andterminal operations.

Use of the FMS during approach is forbidden for non precision GPS procedures (GPS Stand alone

Approaches).

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Part 2

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F2000Airplane

Flight Manual


Normal procedures Issue 1

DTM537

EASA APPROVED

NORMAL PROCEDURES

GENERAL

If remote/oceanic operations are based on GPS only, check FDE availability before flight.Check waypoints and altitude constraints using published charts (SID, STAR, APP, GA).

Constantly check the trajectory compare to the published procedure by displaying on the EFIS thenavaids provided for in the procedure.

APPROACH

- Engage LNAV mode.

- Press ARM APPR on the CDU at 50 NM of the destination airport.

- Press ACT APPR on the CDU or wait for automatic activation 2 NM before the FAF.

- Check APPR annunciation is illuminated green on PFD to inform the crew that the system isconfigured properly to conduct (non precision) approach using FMS for navigation.

VNAV

- In order to engage the VNAV mode, select the NAV SOURCE FMS on the coupled side.

- Check altimeter setting on the coupled side (the FMS uses the altitude information given on thePFD on the coupled side).

- Engage VNAV mode.

NOTE

If a message FPA CHANGE is not read on the CDU before a TOD (Top of Descent), the VNAV doesnot engage.

- LNAV and VNAV En Route can be used until level off at the altitude of the FAF.(or until 10 NM before FAF).Then deselect VNAV.

- Switch for example in ALT or VS mode.

- For approach, decrease ASEL to MDA.

- Upon passing the FAF, engage VNAV.

HOLDING PATTERN

CAUTION

The FMS does not always take into account the published maximum Holding Pattern speed.

- Adapt and stabilize the airplane speed 0.5 minute prior the airplane overflies the fix for the firsttime.

- Check that the FMS message HIGH GND SPD FOR HOLDING is out when passing the entry point.

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Issue 1


Normal procedures

F2000Airplane

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DTM537

EASA APPROVED

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GO-AROUND

- Activate the go-around procedure by depressing the GO AROUND pushbutton on the controlcolumn (the MISSED APPROACH procedure is then automatically set in the FMS).

- Reselect the NAV SOURCE FMS.

- Select ASEL at the required altitude.- Engage LNAV and VNAV as needed.

NOTE

The MSSD APPR line select on the CDU does not activate the go-around procedure. It is used toenter the missed approach procedure into the FMS. It has no action on the horizontal and verticalmodes.

The ASEL must be increased up to the go-around altitude.

CROSSFILL (XFILL)The XFILL function allows crossfill of initialization, routes and fuel data. Notably the Pseudo-Vortac,Holding Pattern, Direct To, LNAV, VNAV page parameters are not crossfilled.

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F2000 - AFM SUP22C REV02 - 20100712