F2000 - AFM SUP12C Original - 20100712

8/3/2019 F2000 - AFM SUP12C Original - 20100712

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Part 0

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F2000Airplane

Flight Manual

SUPPLEMENT 12CA/C WITH ONE EGPWS

Table of contents Issue 1

DTM537

EASA APPROVED

SUPPLEMENT No 12C TO THE EASA APPROVED AIRPLANE FLIGHT MANUAL

CONCERNING OPERATION OF

AIRPLANE EQUIPPED WITH ONE EGPWS

AFTER INCORPORATION OF MODIFICATION M1755 or SB F2000-216

(AND M1605 FOR US REGISTERED A/C)

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 M1755 or SB F2000-216 (and M1605 for USregistered A/C).

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 and 1C

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

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

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

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


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Part 0

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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 25 revision 1 (approved by DGAC on November 07,2001) and supplement 25A revision 1 (approved by DGAC onNovember 07, 2001) are merged into supplement 12C original.

First issue of Supplement 12C.

LIST OF EFFECTIVE PARTS

Reference Issue Special applicability

Part 0 Issue 1

Part 1 Issue 1 A/C with HONEYWELL FMS

Part 1A Issue 1 A/C with COLLINS FMS

Part 1B Issue 1 US registered A/C with M1605 and HONEYWELL FMS

Part 1C Issue 1 US registered A/C with M1605 and COLLINS FMS

Part 2 Issue 1

Part 2A Issue 1 US registered A/C with M1605


3/22

Part 1

PAGE 1 / 2

F2000Airplane

Flight Manual


Limitations, Emergency and Abnormal procedures(A/C with HONEYWELL FMS) Issue 1

DTM537

A/C with HONEYWELL 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 TERRAIN 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 GPSSTATUS 2/2 FMS page when setting QFE.

- Alerting algorithms take into account man made obstructions, but the EGPWS obstacle data baseonly 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 ADCselected on the coupled side:

- QNH or QFE must be set on the left side if ADC1 is selected on the coupled side

- QNH or QFE must be set on the right side if ADC2 is selected on the coupled side.

NOTE

The EGPWS does not take account of specific aircraft 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


Limitations, Emergency and Abnormal procedures(A/C with HONEYWELL FMS)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with HONEYWELL 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 TERRAIN INHIBIT switch.

ABNORMAL PROCEDURES

An amber GPWS annunciation is provided on PFD for failure of the Ground Proximity WarningSystem.

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

An amber TERR annunciation is provided on PFD for the loss of the Terrain Awareness Alertingand Display function.

An amber EGPWS annunciation is provided on PFD when the above three failure conditions arepresent.


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Part 1A

PAGE 1 / 2

F2000Airplane

Flight Manual


Limitations, Emergency and Abnormal procedures(A/C with COLLINS FMS) Issue 1

DTM537

A/C with COLLINS FMS

EASA APPROVED

LIMITATIONS





- for operation with QFE reference if both GPS's are not in NAVIGATION mode as in LRNSTATUS MFD page when setting QFE.



- For proper operation of Terrain Awareness Alerting (TAA), QNH or QFE must be set on the ADCselected on the coupled side:



NOTE



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Part 1A

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Issue 1


Limitations, Emergency and Abnormal procedures(A/C with COLLINS FMS)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with COLLINS FMS

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ABNORMAL PROCEDURES






7/22

Part 1B

PAGE 1 / 2

F2000Airplane

Flight Manual


Limitations, Emergency and Abnormal procedures(US registered A/C with M1605 and HONEYWELL FMS) Issue 1

DTM537

US registered A/C with M1605and 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.



- For proper operation of Terrain Awareness Alerting (TAA), QNH or QFE must be set on the ADCselected on the coupled side, in the event of an ADC failure en-route:



NOTE



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Part 1B

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Issue 1


Limitations, Emergency and Abnormal procedures(US registered A/C with M1605 and HONEYWELL FMS)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

US registered A/C with M1605and HONEYWELL FMS

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ABNORMAL PROCEDURES






9/22

Part 1C

PAGE 1 / 2

F2000Airplane

Flight Manual


Limitations, Emergency and Abnormal procedures(US registered A/C with M1605 and COLLINS FMS) Issue 1

DTM537

US registered A/C with M1605and COLLINS FMS

EASA APPROVED

LIMITATIONS





- for operation with QFE reference if both GPS's are not in NAVIGATION mode as in LRNSTATUS MFD page when setting QFE.



- For proper operation of Terrain Awareness Alerting (TAA), QNH or QFE must be set on the ADCselected on the coupled side, in the event of an ADC failure en-route:



NOTE



10/22

Part 1C

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Issue 1


Limitations, Emergency and Abnormal procedures(US registered A/C with M1605 and COLLINS FMS)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

US registered A/C with M1605and COLLINS FMS

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ABNORMAL PROCEDURES






11/22

Part 2

PAGE 1 / 6

F2000Airplane

Flight Manual


Normal procedures Issue 1

DTM537

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:

TERR............................................................................................................................... Selected

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

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 PFD

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)

WINDSHEARMODE 7 WindshearWINDSHEAR WINDSHEAR

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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Part 2

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F2000Airplane

Flight Manual



DTM537

EASA APPROVED

GROUND PROXIMITY WARNINGS - MODES 1 TO 4

GNDPROX annunciation in PFD with associated voice warning.

Adjust the flight path / configuration until the GNDPROX annunciation goes out and the voicewarning stops.

PULL UP annunciation in PFD.

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 annunciation in PFD.

GLIDESLOPE voice warning:

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

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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Issue 1


Normal procedures

F2000Airplane

Flight Manual

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


TOO LOW TERRAIN voice warning.Adjust the flight path / configuration until the warning 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.


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.


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


Level the wings.



AIRBRAKES handle............................................................................................................Position 0Landing 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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Part 2

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Issue 1


Normal procedures

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

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INTENTIONALLY LEFT BLANK


17/22

Part 2A

PAGE 1 / 6

F2000Airplane

Flight Manual


Normal procedures (US registered A/C with M1605) Issue 1

DTM537

US registered A/C with M1605

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:

TERR............................................................................................................................... Selected

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 2A

PAGE 2 / 6

Issue 1


Normal procedures (US registered A/C with M1605)

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 PFD

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)

WINDSHEARMODE 7 WindshearWINDSHEAR WINDSHEAR

ENHANCED MODES

RFCF Runway Field Clearance Floor TOO LOW TERRAIN GNDPROX

TCF Terrain Clearance Floor TOO LOW TERRAIN GNDPROX

CAUTION TERRAIN

CAUTION OBSTACLEGNDPROX

TERRAIN TERRAINPULL UP

TAA Terrain Awareness Alerting

OBSTACLE OBSTACLEPULL UP

PULL UP


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Part 2A

PAGE 3 / 6

F2000Airplane

Flight Manual



DTM537


EASA APPROVED

GROUND PROXIMITY WARNINGS - MODES 1 TO 4

GNDPROX annunciation in PFD with associated voice warning.

Adjust the flight path / configuration until the GNDPROX annunciation goes out and the voicewarning stops.


PULL UP voice warning.


Level the wings.




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


GROUND PROXIMITY WARNINGS - MODE 5


GLIDESLOPE voice warning:

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

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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Part 2A

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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).


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 2A

PAGE 5 / 6

F2000Airplane

Flight Manual



DTM537


EASA APPROVED

TERRAIN CLEARANCE FLOOR


TOO LOW TERRAIN voice warning.Adjust the flight path / configuration until the warning 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.


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

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


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


Level the wings.



AIRBRAKES handle............................................................................................................Position 0Landing gear..................................................................................................................................Up

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


NOTE

Only vertical maneuvers are recommended, unless operating in visual meteorological conditions(VMC), and / or the pilot determines, based on all available information, that turning in addition to thevertical escape maneuver is the safest course of action.


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Part 2A

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Issue 1



F2000Airplane

Flight Manual

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INTENTIONALLY LEFT BLANK

F2000 - AFM SUP12C Original - 20100712

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