F2000 - AFM SUP12 REV03 - 20100712

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    Part 0

    PAGE 1 / 2

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    Table of contents Issue 1

    DTM537

    EASA APPROVED

    SUPPLEMENT No 12 TO THE EASA APPROVED AIRPLANE FLIGHT MANUAL

    CONCERNING OPERATION OF

    AIRPLANE EQUIPPED WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    AFTER INCORPORATION OF MODIFICATION M1141.

    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.

    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

    PAGE 2 / 2

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    Table of contents

    F2000Airplane

    Flight Manual

    DTM537

    EASA APPROVED

    p

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    LIST OF REVISIONS

    Parts changesRevisionand Date

    Titleand

    Approval reference Added Revised Removed

    Original

    27-may-1998

    Airplane equipped with one EGPWSwithout terrain display

    Approved by DGAC

    First Issue of supplement 12.

    Revision 1

    02-mar-2000

    Approved by DGAC Pages 2, 3, 3A**, 3B,3C***, 7 and 7A*.

    Revision 2

    17-oct-2000

    Approved by DGAC Pages 1 and 2.

    Revision 3

    12-jul-2010

    New page layout.

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

    Part 0 Issue 1

    Part 1 Issue 1

    Part 1A Issue 1

    Part 1B Issue 1

    Part 1C Issue 1

    Part 2 Issue 1

    Part 2A Issue 1

    All pages.

    * US registered A/C with M1605.

    ** A/C with GLOBAL FMS.

    *** US registered A/C with M1605 and GLOBAL FMS.

    LIST OF EFFECTIVE PARTS

    Reference Issue Special applicability

    Part 0 Issue 1

    Part 1 Issue 1

    Part 1A Issue 1 A/C with GLOBAL FMS

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

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

    Part 2 Issue 1

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

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    Part 1

    PAGE 1 / 2

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    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 TAAand Terrain Clearance Floor TCF functions) must be INHIBITED by selecting the TERR INHIBITswitch when within 15 NM of take-off, approach or landing at an airport for which any of thefollowing 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.

    - The use of Terrain Awareness Alerting TAA function is prohibited during QFE operations.

    - 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.

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    Part 1

    PAGE 2 / 2

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    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 TAA and

    Terrain Clearance Floor TCF 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 function.

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    Part 1A

    PAGE 1 / 2

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

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

    DTM537

    A/C with GLOBAL 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 TAAand Terrain Clearance Floor TCF functions) must be INHIBITED by selecting the TERR INHIBITswitch when within 15 NM of take-off, approach or landing at an airport for which any of thefollowing 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 made

    obstructions.

    - The use of Terrain Awareness Alerting TAA function is prohibited during QFE operations.

    - 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.

    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 theflight.

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    Part 1A

    PAGE 2 / 2

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

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

    F2000Airplane

    Flight Manual

    DTM537

    EASA APPROVED

    A/C with GLOBAL FMS

    p

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    EMERGENCY PROCEDURES

    For ditching or other off airports landings, the Enhanced modes (Terrain Awareness Alerting TAA andTerrain Clearance Floor TCF 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 function.

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    Part 1B

    PAGE 1 / 2

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

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

    DTM537

    US registered A/C with M1605

    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 TAAand Terrain Clearance Floor TCF functions) must be INHIBITED by selecting the TERR INHIBITswitch when within 15 NM of take-off, approach or landing at an airport for which any of thefollowing 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 made

    obstructions.

    - The use of Terrain Awareness Alerting TAA function is prohibited during QFE operations.

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

    - 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.

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    Part 1B

    PAGE 2 / 2

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

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

    F2000Airplane

    Flight Manual

    DTM537

    EASA APPROVED

    US registered A/C with M1605

    p

    y

    EMERGENCY PROCEDURES

    For ditching or other off airports landings, the Enhanced modes (Terrain Awareness Alerting TAA andTerrain Clearance Floor TCF 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 function.

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    Part 1C

    PAGE 1 / 2

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    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

    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 TAAand Terrain Clearance Floor TCF functions) must be INHIBITED by selecting the TERR INHIBITswitch when within 15 NM of take-off, approach or landing at an airport for which any of thefollowing 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 made

    obstructions.

    - The use of Terrain Awareness Alerting TAA function is prohibited during QFE operations.

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

    - 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.

    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 theflight.

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    Part 1C

    PAGE 2 / 2

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    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

    EMERGENCY PROCEDURES

    For ditching or other off airports landings, the Enhanced modes (Terrain Awareness Alerting TAA andTerrain Clearance Floor TCF 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 function.

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    Part 2

    PAGE 1 / 6

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    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.

    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

    PAGE 2 / 6

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    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 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 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

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    Part 2

    PAGE 3 / 6

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    Normal procedures Issue 1

    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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    Part 2

    PAGE 4 / 6

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    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 annunciation in PFD.

    WINDSHEAR voice warning:

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

    Level the wings.

    Pull up to stall warning onset.

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

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

    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

    PAGE 5 / 6

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    Normal procedures Issue 1

    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):

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

    Level the wings.

    Execute a positive pull up.

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

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

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

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

    Maintain best rate of climb until terrain clearance is assured.

    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

    PAGE 6 / 6

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    Normal procedures

    F2000Airplane

    Flight Manual

    DTM537

    EASA APPROVED

    p

    y

    INTENTIONALLY LEFT BLANK

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    Part 2A

    PAGE 1 / 6

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    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), 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.

    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

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    Normal procedures (US registered A/C with M1605)

    F2000Airplane

    Flight Manual

    DTM537

    EASA APPROVED

    US registered A/C with M1605

    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 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 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

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    Part 2A

    PAGE 3 / 6

    F2000Airplane

    Flight Manual

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

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

    DTM537

    US registered A/C with M1605

    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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    Part 2A

    PAGE 4 / 6

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    Normal procedures (US registered A/C with M1605)

    F2000Airplane

    Flight Manual

    DTM537

    EASA APPROVED

    US registered A/C with M1605

    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 annunciation in PFD.

    WINDSHEAR voice warning:

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

    Level the wings.

    Pull up to stall warning onset.

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

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

    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

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

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

    DTM537

    US registered A/C with M1605

    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:

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

    Level the wings.

    Execute a positive pull up.

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

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

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

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

    Maintain best rate of climb until terrain clearance is assured.

    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

    PAGE 6 / 6

    Issue 1

    SUPPLEMENT 12A/C WITH ONE EGPWS WITHOUT TERRAIN DISPLAY

    Normal procedures (US registered A/C with M1605)

    F2000Airplane

    Flight Manual

    p

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    INTENTIONALLY LEFT BLANK