F2000 - AFM SUP12A Original - 20100712

8/3/2019 F2000 - AFM SUP12A Original - 20100712

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Part 0

PAGE 1 / 2

F2000Airplane

Flight Manual

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

Table of contents Issue 1

DTM537

EASA APPROVED

SUPPLEMENT No 12A TO THE EASA APPROVED AIRPLANE FLIGHT MANUAL

CONCERNING OPERATION OF

AIRPLANE EQUIPPED WITH ONE EGPWS AND A TERRAIN DISPLAY

AFTER INCORPORATION OF MODIFICATIONS M1141 AND M1501.

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 M1141 and M1501.

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



Part 1

PAGE 1 / 2

F2000Airplane

Flight Manual


Limitations, Emergency and Abnormal procedures Issue 1

DTM537

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 functions) must be INHIBITED by selecting theTERR INHIBIT switch when within 15 NM of take-off, approach or landing at an airport for whichany of the following conditions apply:

- The airport has no approved instrument approach procedure.

- The longest runway is less than 3,500 ft in length.

- The EGPWS database, and alerting algorithms currently do not account for man madeobstructions.

- 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.

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

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

- QNH must be set on 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.

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.



Part 1

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Issue 1


Limitations, Emergency and Abnormal procedures

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

p

y

EMERGENCY PROCEDURES

For ditching or other off airports landings, the Enhanced modes (Terrain Awareness Alerting and

Display TAAD and Terrain Clearance Floor TCF functions) should be INHIBITED by selecting theTERR 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 function.



Part 1A

PAGE 1 / 2

F2000Airplane

Flight Manual


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

DTM537

A/C with GLOBAL FMS

EASA APPROVED

LIMITATIONS






- The EGPWS database, and alerting algorithms currently do not account for man made

obstructions.



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



NOTE


CAUTION

- When the FMS is in IRS only 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 the

flight.



Part 1A

PAGE 2 / 2

Issue 1


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

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with GLOBAL FMS

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y


For ditching or other off airports landings, the Enhanced modes (Terrain Awareness Alerting andDisplay TAAD and Terrain Clearance Floor TCF functions) should be INHIBITED by selecting the

TERR INHIBIT switch.

ABNORMAL PROCEDURES






Part 1B

PAGE 1 / 2

F2000Airplane

Flight Manual


Limitations, Emergency and Abnormal procedures (US registered A/Cwith M1605) Issue 1

DTM537

US registered A/C with M1605

EASA APPROVED

LIMITATIONS







obstructions.



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



NOTE




Part 1C

PAGE 1 / 2

F2000Airplane

Flight Manual


Limitations, Emergency and Abnormal procedures (US registered A/Cwith M1605 and GLOBAL FMS) Issue 1

DTM537

US registered A/C with M1605and GLOBAL FMS

EASA APPROVED

LIMITATIONS







obstructions.



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



NOTE


CAUTION

- When the FMS is in IRS only 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 the

flight.



Part 1C

PAGE 2 / 2

Issue 1


Limitations, Emergency and Abnormal procedures (US registered A/Cwith M1605 and GLOBAL FMS)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

US registered A/C with M1605and GLOBAL FMS

p

y


For ditching or other off airports landings, the Enhanced modes (Terrain Awareness Alerting andDisplay TAAD and Terrain Clearance Floor TCF functions) should be INHIBITED by selecting the

TERR INHIBIT switch.

ABNORMAL PROCEDURES






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), WINDSHEARDETECTION and TERRAIN CLEARANCE FLOOR will not be available but the enhanced features ofterrain awareness alerting, 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 O’RIDE switch to”on” position in order to inhibit the TOO LOW FLAPS warning.



Part 2

PAGE 2 / 6

Issue 1


Normal procedures

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

p

y

GROUND PROXIMITY WARNINGS SYSTEM - ALERTS

WARNINGSMODESVOICES 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 DON’T 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 Callouts Versus configuration(see Part 2 page 3)

WINDSHEAR (PFD)MODE 7

Windshear WINDSHEAR WINDSHEAR (PFD)

ENHANCED MODES

TCF Terrain Clearance Floor TOW LOW TERRAIN GNDPROX

TERRAIN AHEAD GNDPROX

TAA Terrain Awareness Alerting TERRAIN AHEAD

PULL UPPULL UP



Part 2

PAGE 3 / 6

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.



Part 2

PAGE 4 / 6

Issue 1


Normal procedures

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

p

y

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



Part 2

PAGE 5 / 6

F2000Airplane

Flight Manual



DTM537

EASA APPROVED

TERRAIN CLEARANCE FLOOR

GNDPROX light on.

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 baro-altitude(QNH) and a terrain database to predict potential conflicts between the airplane flight path and theterrain.

GNDPROX light on.

TERRAIN 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 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.



Part 2

PAGE 6 / 6

Issue 1


Normal procedures

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

p

y

INTENTIONALLY LEFT BLANK



Part 2A

PAGE 1 / 6

F2000Airplane

Flight Manual


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

DTM537


EASA APPROVED

SYSTEM ACTIVATION

NOTE

After losing all radio altimeters, the basic GPWS MODES (MODES 1 to 6), WINDSHEARDETECTION and TERRAIN CLEARANCE FLOOR will not be available but the enhanced features ofterrain awareness alerting, 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 O’RIDE switch to”on” position in order to inhibit the TOO LOW FLAPS warning.



Part 2A

PAGE 2 / 6

Issue 1


Normal procedures (US registered A/C with M1605)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED


p

y

GROUND PROXIMITY WARNINGS SYSTEM - ALERTS

WARNINGSMODESVOICES 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 DON’T 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 Callouts Versus configuration(see Part 2A page 3)

WINDSHEAR (PFD)MODE 7

Windshear WINDSHEAR WINDSHEAR (PFD)

ENHANCED MODES

TCF Terrain Clearance Floor TOW LOW TERRAIN GNDPROX

CAUTION TERRAIN GNDPROX

TAA Terrain Awareness Alerting TERRAIN TERRAIN

PULL UPPULL UP



Part 2A

PAGE 3 / 6

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.


Level the wings.




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


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.



Part 2A

PAGE 4 / 6

Issue 1



F2000Airplane

Flight Manual

DTM537

EASA APPROVED


p

y

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



Part 2A

PAGE 5 / 6

F2000Airplane

Flight Manual



DTM537


EASA APPROVED

TERRAIN CLEARANCE FLOOR

GNDPROX light on.

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 baro-altitude(QNH) and a terrain database to predict potential conflicts between the airplane flight path and theterrain.

GNDPROX light on.

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

PULL UP light on.

TERRAIN TERRAIN - PULL UP voice warning:


Level the wings.




Landing 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.



Part 2A

PAGE 6 / 6

Issue 1



F2000Airplane

Flight Manual

p

y

INTENTIONALLY LEFT BLANK

F2000 - AFM SUP12A Original - 20100712

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