F2000 - AFM SUP12D Original - 20100712

8/3/2019 F2000 - AFM SUP12D Original - 20100712

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Part 0

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F2000Airplane

Flight Manual

SUPPLEMENT 12DA/C WITH ONE EGPWS AND A TERRAIN DISPLAY

Table of contents Issue 1

DTM537

EASA APPROVED

SUPPLEMENT No 12D TO THE EASA APPROVED AIRPLANE FLIGHT MANUAL

CONCERNING OPERATION OF

AIRPLANE EQUIPPED WITH ONE EGPWS AND A TERRAIN DISPLAY

AFTER INCORPORATION OF MODIFICATION M1757

or SB F2000-169 revision 1 and subsequent or SB F2000-216 revision 1 and subsequent

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 M1757 or SB F2000-169 revision 1 andsubsequent or SB F2000-216 revision 1 and subsequent.

The information contained herein supplements the information of the basic Airplane Flight Manual; forlimitations, procedures and performance information not contained in this supplement, consult thebasic Airplane Flight Manual.

SECTIONS OF AIRPLANE FLIGHT MANUAL PARTS OF SUPPLEMENT

- Section 1 : LIMITATIONS....................................................................Part 1, 1A, 1B, 1C, 1D and 1E

- Section 2 : EMERGENCY PROCEDURES ......................................... Part 1, 1A, 1B, 1C, 1D and 1E

- Section 3 : ABNORMAL PROCEDURES............................................ Part 1, 1A, 1B, 1C, 1D and 1E- Section 4 : NORMAL PROCEDURES..............................................................Part 2, 2A, 2B and 2C

- 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

12-jul-2010

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

Supplement 29 revision 1 (approved by DGAC on June 03, 2004)and supplement 29A revision 1 (approved by DGAC on June 03,2004) are merged into supplement 12D original.

First issue of Supplement 12D.

LIST OF EFFECTIVE PARTS

Reference Issue Special applicability

Part 0 Issue 1

Part 1 Issue 1 A/C with UNS.1C FMS

Part 1A Issue 1 A/C with HONEYWELL FMS

Part 1B Issue 1 A/C with GLOBAL FMS

Part 1C Issue 1 A/C with UNS.1C FMS and (with M1605 or US registered A/C)

Part 1D Issue 1A/C with HONEYWELL FMSand (with M1605 or US registered A/C)

Part 1E Issue 1 A/C with GLOBAL FMS and (with M1605 or US registered A/C)

Part 2 Issue 1 A/C with UNS.1C FMS or HONEYWELL FMS

Part 2A Issue 1 A/C with GLOBAL FMS

Part 2B Issue 1A/C with (UNS.1C FMS or HONEYWELL FMS)and (with M1605 or US registered A/C)

Part 2C Issue 1 A/C with GLOBAL FMS and (with M1605 or US registered A/C)


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Part 1

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F2000Airplane

Flight Manual

SUPPLEMENT 12DA/C WITH ONE EGPWS AND A TERRAIN DISPLAYLimitations, Emergency and Abnormal procedures

(A/C with UNS.1C FMS) Issue 1

DTM537

A/C with UNS.1C FMS

EASA APPROVED

LIMITATIONS

EGPWS SYSTEM OPERATION

- Pilots are authorized to deviate from their current Air Traffic Control ATC clearance to the extendnecessary to comply with an EGPWS warning.

- In order to avoid giving unwanted alerts, the Enhanced modes (Terrain Awareness Alerting andDisplay TAAD and Terrain Clearance Floor TCF and Runway Field Clearance Floor RFCFfunctions) must be INHIBITED by selecting the TERR INHIBIT switch:

- When within 15 NM of take-off, approach or landing at an airport that is not included in the airportdatabase.

- For operation with QFE reference if both GPS's are not in NAVIGATION mode as in GPS 1/4FMS page when setting QFE.

- Alerting algorithms take into account man made obstructions, but the EGPWS obstacle databaseonly covers a few areas in the world.

- Navigation must not be predicated upon the use of Terrain Awareness Display.The Terrain Awareness Display is intended to serve as a situational tool only.

- For proper operation of Terrain Awareness Alerting (TAA):

- QNH or QFE must be set on the left side if ADC1 is operative.

- QNH or QFE must be set on right side if ADC1 is not operative, or after a reversion from ADC1 toADC2.

NOTE

The EGPWS does not take account of specific airplane configuration and climb performance and aPULL UP maneuver, for certain situations may not ensure terrain clearance.


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Part 1

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Issue 1


(A/C with UNS.1C FMS)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with UNS.1C FMS

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EMERGENCY PROCEDURES

To avoid unwanted alerts when ditching or other off airports landings, the Enhanced modes (TerrainAwareness Alerting and Display TAAD and Terrain Clearance Floor TCF and Runway Field

Clearance Floor RFCF functions) should be INHIBITED by selecting the TERR INHIBIT switch.

ABNORMAL PROCEDURES

- An amber GPWS annunciation is provided for failure of the Ground Proximity Warning System.

- An amber W/S annunciation is provided for failure of the Windshear Detection function.

- An amber TERR annunciation is provided for the loss of the Terrain Awareness Alerting andDisplay function.


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Part 1A

PAGE 1 / 2

F2000Airplane

Flight Manual


(A/C with HONEYWELL FMS) Issue 1

DTM537

A/C with HONEYWELL FMS

EASA APPROVED

LIMITATIONS





- For operation with QFE reference if both GPS's are not in NAVIGATION mode as in GPSSTATUS 2/2 FMS page when setting QFE.






NOTE



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Part 1A

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Issue 1


(A/C with HONEYWELL FMS)

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Flight Manual

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EASA APPROVED

A/C with HONEYWELL FMS

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ABNORMAL PROCEDURES





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Part 1B

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F2000Airplane

Flight Manual


(A/C with GLOBAL FMS) Issue 1

DTM537

A/C with GLOBAL FMS

EASA APPROVED

LIMITATIONS



- In order to avoid giving unwanted alerts, the Enhanced modes (Terrain Awareness Alerting andDisplay TAAD and Terrain Clearance Floor TCF and Runway Field Clearance Floor RFCFfunctions) must be INHIBITED by selecting the TERR INHIBIT switch when within15 NM of take-off,approach or landing at an airport that is not included in the airport data base.



- The use of Terrain Awareness Alerting and Display TAAD function is prohibited during QFEoperations.


- QNH must be set on the left side if ADC1 is operative.

- QNH must be set on right side if ADC1 is not operative, or after a reversion from ADC1 to ADC2.

NOTEThe EGPWS does not take account of specific airplane configuration and climb performance and aPULL UP maneuver, for certain situations may not ensure terrain clearance.

CAUTION

- When the FMS is in IRS, the pilot must deselect the terrain function.- When the FMS is in DR mode, the pilot must deselect the terrain function for the rest of theflight.


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Part 1B

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Issue 1


(A/C with GLOBAL FMS)

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DTM537

EASA APPROVED

A/C with GLOBAL FMS

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ABNORMAL PROCEDURES





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Part 1C

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F2000Airplane

Flight Manual


(A/C with UNS.1C FMS and (with M1605 or US registered A/C)) Issue 1

DTM537

A/C with UNS.1C FMSand (with M1605 or US registered A/C)

EASA APPROVED

LIMITATIONS





- For operation with QFE reference if both GPS's are not in NAVIGATION mode as in GPS 1/4FMS page when setting QFE.



- For proper operation of Terrain Awareness Alerting (TAA), in the event of an ADC failure en-route:



NOTE



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Part 1C

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Issue 1


(A/C with UNS.1C FMS and (with M1605 or US registered A/C))

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with UNS.1C FMSand (with M1605 or US registered A/C)

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ABNORMAL PROCEDURES





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Part 1D

PAGE 1 / 2

F2000Airplane

Flight Manual


(A/C with HONEYWELL FMS and (with M1605 or US registered A/C)) Issue 1

DTM537

A/C with HONEYWELL FMSand (with M1605 or US registered A/C)

EASA APPROVED

LIMITATIONS





- For operation with QFE reference if both GPS's are not in NAVIGATION mode as in GPSSTATUS 2/2 FMS page when setting QFE.






NOTE



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Part 1D

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Issue 1


(A/C with HONEYWELL FMS and (with M1605 or US registered A/C))

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with HONEYWELL FMSand (with M1605 or US registered A/C)

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ABNORMAL PROCEDURES





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Part 1E

PAGE 1 / 2

F2000Airplane

Flight Manual


(A/C with GLOBAL FMS and (with M1605 or US registered A/C)) Issue 1

DTM537

A/C with GLOBAL FMSand (with M1605 or US registered A/C)

EASA APPROVED

LIMITATIONS



- In order to avoid giving unwanted alerts, the Enhanced modes (Terrain Awareness Alerting andDisplay TAAD and Terrain Clearance Floor TCF and Runway Field Clearance Floor RFCFfunctions) must be INHIBITED by selecting the TERR INHIBIT switch when within15 NM of take-off,approach or landing at an airport that is not included in the airport data base.



- The use of Terrain Awareness Alerting and Display TAAD function is prohibited during QFEoperations.


- QNH must be set on the left side if ADC1 is operative.

- QNH must be set on right side if ADC1 is not operative, or after a reversion from ADC1 to ADC2.

NOTEThe EGPWS does not take account of specific airplane configuration and climb performance and aPULL UP maneuver, for certain situations may not ensure terrain clearance.

CAUTION

- When the FMS is in IRS, the pilot must deselect the terrain function.- When the FMS is in DR mode, the pilot must deselect the terrain function for the rest of theflight.


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Part 1E

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Issue 1


(A/C with GLOBAL FMS and (with M1605 or US registered A/C))

F2000Airplane

Flight Manual

DTM537

EASA APPROVED


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ABNORMAL PROCEDURES





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Part 2

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F2000Airplane

Flight Manual


Normal procedures (A/C with UNS.1C FMS or HONEYWELL FMS) Issue 1

DTM537

A/C with UNS.1C FMS or HONEYWELL FMS

EASA APPROVED

SYSTEM ACTIVATION

NOTE

After losing all radio altimeters, the basic GPWS MODES (MODES 1 to 6),WINDSHEAR DETECTION and TERRAIN CLEARANCE FLOOR will not be available but theenhanced feature of Terrain Awareness Alerting (TAA) and the Runway Field Clearance Floor(RFCF), however, will be available.

ON GROUND

- Prior to every flight:

Perform a short system self test.

IN FLIGHT

NOTE

When any of the EGPWS alert lights are illuminated, the TCAS is placed in TA ONLY mode whichinhibits all TCAS aural messages.

To display the Terrain on MFD:

- On DCP:

RDR................................................................................................................................. Selected

- Then on glareshield:

TERR pushbutton............................................................................................................... Pushed

APPROACH

NOTE

If landing is expected with 20 FLAPS + SLATS, or below, set the EGPWS FLAPS ORIDE switch toon position in order to inhibit the TOO LOW FLAPS warning.


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Part 2

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Issue 1


Normal procedures (A/C with UNS.1C FMS or HONEYWELL FMS)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED


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GROUND PROXIMITY WARNINGS SYSTEM - ALERTS

Audio and visual alerts from the EGPWS are available independently of terrain display on the MFD.

WARNINGSMODES

VOICES LIGHTS

GPWS MODES

SINKRATE GNDPROXMODE 1 Excessive descent rate

PULL UP PULL UP

TERRAIN TERRAIN GNDPROXMODE 2 Excessive terrain closure rate

PULL UP PULL UP

MODE 3 Altitude loss after take-off DONT SINK GNDPROX

TOO LOW TERRAIN GNDPROX

TOO LOW GEAR GNDPROXMODE 4 Unsafe terrain clearance

TOO LOW FLAPS GNDPROX

MODE 5 Excessive glideslope deviation GLIDESLOPE GNDPROX

MODE 6 CalloutsVersus configuration(see page 3)

WINDSHEAR (PFD)MODE 7 WindshearWINDSHEAR WINDSHEAR (PFD)

ENHANCED MODES

RFCF Runway Field Clearance Floor TOO LOW TERRAIN GNDPROX

TCF Terrain Clearance Floor TOO LOW TERRAIN GNDPROX

TERRAIN AHEAD

OBSTACLE AHEADGNDPROX

TERRAIN AHEADPULL UP

TAA Terrain Awareness Alerting

OBSTACLE AHEADPULL UP

PULL UP


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F2000Airplane

Flight Manual



DTM537


EASA APPROVED

GROUND PROXIMITY WARNINGS - MODES 1 TO 4

GNDPROX light on with associated voice warning.

Adjust the flight path / configuration until the GNDPROX light goes out and the voice warningstops.

PULL UP light on.

PULL UP voice warning.

Autopilot........................................................................................................................Disconnected

Level the wings.

Execute a positive pull up.

Power levers.....................................................................................................................TAKE-OFF

AIRBRAKES handle............................................................................................................Position 0

Landing gear..................................................................................................................................UpSlat-flap handle................................................................................. 20 FLAPS + SLATS maximum

Maintain best rate of climb until terrain clearance is assured.

GROUND PROXIMITY WARNINGS - MODE 5

GNDPROX light on.

GLIDESLOPE voice warning:

Initiate corrective action to fly the airplane back to the glideslope axis

or

Inhibit the warning in case of visual approach by pushing the G/S INHIBIT pushbutton.

ADVISORY CALLOUTS - MODE 6

- EXCESSIVE BANK ANGLE.

- MINIMUMS / APPROACHING MINIMUMS.

- HEIGHT.


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DTM537

EASA APPROVED


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WINDSHEAR - MODE 7

WINDSHEAR annunciation in PFD.

Monitor wind direction and intensity evolution in comparison with tower wind.Maintain or let the airspeed increase (consider a go-around).


WINDSHEAR voice warning:


Level the wings.

Pull up to stall warning onset.



Slat-flap handle................................................................................. 20 FLAPS + SLATS maximumAt pilot 's discretion according to airplane height and vertical speed:

Landing gear ..............................................................................................................................Up


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Part 2

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F2000Airplane

Flight Manual



DTM537


EASA APPROVED

TERRAIN CLEARANCE FLOOR

GNDPROX light on.

TOO LOW TERRAIN voice warning.Adjust the flight path / configuration until the GNDPROX light goes out and the voice warning

stops.

TERRAIN AWARENESS ALERTING

The TERRAIN AWARENESS ALERTING use airplane geographic position, airplane geometricaltitude (blended altitude of GPS, radio, runway calibrated altitudes and baro-corrected altitudeaccording to the flight phase), a terrain database and an obstacle database to predict potentialconflicts between the airplane flight path and the terrain or obstacle.

GNDPROX light on.

TERRAIN AHEAD or OBSTACLE AHEAD voice warning (each 7 seconds):

Adjust the flight path / configuration until the warning light goes out and the voice warning stops.

PULL UP light on.

TERRAIN AHEAD - PULL UP or OBSTACLE AHEAD - PULL UP voice warning(continuously):


Level the wings.




Landing gear..................................................................................................................................Up

Slat-flap handle................................................................................. 20 FLAPS + SLATS maximum


NOTE

For enhanced functions, in addition to climb, a turn maneuver can be performed if the crewconcludes turning is the safest way of action taking into account the airplane position.


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DTM537

EASA APPROVED


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INTENTIONALLY LEFT BLANK


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Part 2A

PAGE 1 / 6

F2000Airplane

Flight Manual


Normal procedures (A/C with GLOBAL FMS) Issue 1

DTM537

A/C with GLOBAL FMS

EASA APPROVED

SYSTEM ACTIVATION

NOTE


ON GROUND



IN FLIGHT

NOTE



- On DCP:

RDR................................................................................................................................. Selected

- Then on glareshield:


APPROACH

NOTE



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Part 2A

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Issue 1


Normal procedures (A/C with GLOBAL FMS)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with GLOBAL FMS

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WARNINGSMODES

VOICES LIGHTS

GPWS MODES


PULL UP PULL UP


PULL UP PULL UP







WINDSHEAR (PFD)MODE 7 WindshearWINDSHEAR WINDSHEAR (PFD)

ENHANCED MODES



TERRAIN AHEAD

OBSTACLE AHEADGNDPROX

TERRAIN AHEADPULL UP

TAA Terrain Awareness Alerting

OBSTACLE AHEADPULL UP

PULL UP


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Part 2A

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F2000Airplane

Flight Manual



DTM537

A/C with GLOBAL FMS

EASA APPROVED




PULL UP light on.



Level the wings.







GNDPROX light on.



or





- HEIGHT.


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Part 2A

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Issue 1



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Flight Manual

DTM537

EASA APPROVED

A/C with GLOBAL FMS

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WINDSHEAR - MODE 7


Monitor wind direction and intensity evolution in comparison with tower wind.Maintain or let the airspeed increase (consider a go-around).




Level the wings.




Slat-flap handle................................................................................. 20 FLAPS + SLATS maximumAt pilot 's discretion according to airplane height and vertical speed:

Landing gear ..............................................................................................................................Up


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Part 2A

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F2000Airplane

Flight Manual



DTM537

A/C with GLOBAL FMS

EASA APPROVED


GNDPROX light on.


stops.


The TERRAIN AWARENESS ALERTING use airplane geographic position, airplane baro-correctedaltitude (QNH), a terrain database and an obstacle database to predict potential conflicts between theairplane flight path and the terrain or obstacle.

GNDPROX light on.

TERRAIN AHEAD or OBSTACLE AHEAD voice warning (each 7 seconds):


PULL UP light on.

TERRAIN AHEAD - PULL UP or OBSTACLE AHEAD - PULL UP voice warning(continuously):


Level the wings.




Landing gear..................................................................................................................................Up



NOTE



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Issue 1



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Flight Manual

DTM537

EASA APPROVED

A/C with GLOBAL FMS

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27/38

Part 2B

PAGE 1 / 6

F2000Airplane

Flight Manual


Normal procedures (A/C with (UNS.1C FMS or HONEYWELL FMS) and(with M1605 or US registered A/C)) Issue 1

DTM537

A/C with (UNS.1C FMS or HONEYWELL FMS)and (with M1605 or US registered A/C)

EASA APPROVED

SYSTEM ACTIVATION

NOTE


ON GROUND



IN FLIGHT

NOTE



- On DCP:

RDR................................................................................................................................. Selected- Then on glareshield:


APPROACH

NOTE



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Part 2B

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Issue 1


Normal procedures (A/C with (UNS.1C FMS or HONEYWELL FMS) and(with M1605 or US registered A/C))

F2000Airplane

Flight Manual

DTM537

EASA APPROVED


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WARNINGSMODES

VOICES LIGHTS

GPWS MODES


PULL UP PULL UP


PULL UP PULL UP







WINDSHEAR (PFD)

MODE 7 Windshear WINDSHEAR WINDSHEAR (PFD)

ENHANCED MODES



CAUTION TERRAIN

CAUTION OBSTACLEGNDPROX

TERRAIN TERRAINPULL UPTAA Terrain Awareness Alerting

OBSTACLE OBSTACLEPULL UP

PULL UP


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Part 2B

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F2000Airplane

Flight Manual



DTM537


EASA APPROVED




PULL UP light on.



Level the wings.







GNDPROX light on.



or





- HEIGHT.


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Issue 1



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Flight Manual

DTM537

EASA APPROVED


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WINDSHEAR - MODE 7


Monitor wind direction and intensity evolution in comparison with tower wind.

Maintain or let the airspeed increase (consider a go-around).




Level the wings.





At pilot 's discretion according to airplane height and vertical speed:

Landing gear ..............................................................................................................................Up


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Part 2B

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F2000Airplane

Flight Manual



DTM537


EASA APPROVED


GNDPROX light on.


stops.


The TERRAIN AWARENESS ALERTING use airplane geographic position, airplane geometricaltitude (blended altitude of GPS, radio, runway calibrated altitudes and baro-corrected altitudeaccording to the flight phase), a terrain database and an obstacle database to predict potentialconflicts between the airplane flight path and the terrain or obstacle.

GNDPROX light on.CAUTION TERRAIN or CAUTION OBSTACLE voice warning (each 7 seconds):


PULL UP light on.

TERRAIN TERRAIN - PULL UP or OBSTACLE OBSTACLE - PULL UP voice warning(continuously):


Level the wings.


Power levers.....................................................................................................................TAKE-OFFAIRBRAKES handle............................................................................................................Position 0

Landing gear..................................................................................................................................Up



NOTE



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Part 2B

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Flight Manual

DTM537

EASA APPROVED


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33/38

Part 2C

PAGE 1 / 6

F2000Airplane

Flight Manual


Normal procedures(A/C with GLOBAL FMS and (with M1605 or US registered A/C)) Issue 1

DTM537


EASA APPROVED

SYSTEM ACTIVATION

NOTE


ON GROUND



IN FLIGHT

NOTE



- On DCP:

RDR................................................................................................................................. Selected- Then on glareshield:


APPROACH

NOTE



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Part 2C

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Issue 1


Normal procedures(A/C with GLOBAL FMS and (with M1605 or US registered A/C))

F2000Airplane

Flight Manual

DTM537

EASA APPROVED


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WARNINGSMODES

VOICES LIGHTS

GPWS MODES


PULL UP PULL UP


PULL UP PULL UP







WINDSHEAR (PFD)

MODE 7 Windshear WINDSHEAR WINDSHEAR (PFD)

ENHANCED MODES



CAUTION TERRAIN

CAUTION OBSTACLEGNDPROX

TERRAIN TERRAINPULL UPTAA Terrain Awareness Alerting

OBSTACLE OBSTACLEPULL UP

PULL UP


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Part 2C

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F2000Airplane

Flight Manual



DTM537


EASA APPROVED




PULL UP light on.



Level the wings.







GNDPROX light on.



or





- HEIGHT.


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Issue 1



F2000Airplane

Flight Manual

DTM537

EASA APPROVED


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WINDSHEAR - MODE 7


Monitor wind direction and intensity evolution in comparison with tower wind.

Maintain or let the airspeed increase (consider a go-around).




Level the wings.





At pilot 's discretion according to airplane height and vertical speed:

Landing gear ..............................................................................................................................Up


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Part 2C

PAGE 5 / 6

F2000Airplane

Flight Manual



DTM537


EASA APPROVED


GNDPROX light on.


stops.


The TERRAIN AWARENESS ALERTING use airplane geographic position, airplane baro-correctedaltitude (QNH), a terrain database and an obstacle database to predict potential conflicts between theairplane flight path and the terrain or obstacle.

GNDPROX light on.

CAUTION TERRAIN or CAUTION OBSTACLE voice warning (each 7 seconds):


PULL UP light on.

TERRAIN TERRAIN - PULL UP or OBSTACLE OBSTACLE - PULL UP voice warning(continuously):


Level the wings.




Landing gear..................................................................................................................................Up



NOTE



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Part 2C

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Issue 1



F2000Airplane

Flight Manual

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F2000 - AFM SUP12D Original - 20100712

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Transcript of F2000 - AFM SUP12D Original - 20100712