Download - F2000 - AFM SUP12C Original - 20100712
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1/22
Part 0
PAGE 1 / 2
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
PAGE 2 / 2
Issue 1
SUPPLEMENT 12CA/C WITH ONE EGPWS
Table of contents
F2000Airplane
Flight Manual
DTM537
EASA APPROVED
p
y
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
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Part 1
PAGE 1 / 2
F2000Airplane
Flight Manual
SUPPLEMENT 12CA/C WITH ONE EGPWS
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
PAGE 2 / 2
Issue 1
SUPPLEMENT 12CA/C WITH ONE EGPWS
Limitations, Emergency and Abnormal procedures(A/C with HONEYWELL FMS)
F2000Airplane
Flight Manual
DTM537
EASA APPROVED
A/C with HONEYWELL FMS
p
y
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
SUPPLEMENT 12CA/C WITH ONE EGPWS
Limitations, Emergency and Abnormal procedures(A/C with COLLINS FMS) Issue 1
DTM537
A/C with COLLINS 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 LRNSTATUS MFD 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 1A
PAGE 2 / 2
Issue 1
SUPPLEMENT 12CA/C WITH ONE EGPWS
Limitations, Emergency and Abnormal procedures(A/C with COLLINS FMS)
F2000Airplane
Flight Manual
DTM537
EASA APPROVED
A/C with COLLINS FMS
p
y
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 1B
PAGE 1 / 2
F2000Airplane
Flight Manual
SUPPLEMENT 12CA/C WITH ONE EGPWS
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
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, in the event of an ADC failure en-route:
- 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 1B
PAGE 2 / 2
Issue 1
SUPPLEMENT 12CA/C WITH ONE EGPWS
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
p
y
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 1C
PAGE 1 / 2
F2000Airplane
Flight Manual
SUPPLEMENT 12CA/C WITH ONE EGPWS
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
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 LRNSTATUS MFD 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, in the event of an ADC failure en-route:
- 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 1C
PAGE 2 / 2
Issue 1
SUPPLEMENT 12CA/C WITH ONE EGPWS
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
p
y
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 2
PAGE 1 / 6
F2000Airplane
Flight Manual
SUPPLEMENT 12CA/C WITH ONE EGPWS
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
PAGE 2 / 6
Issue 1
SUPPLEMENT 12CA/C WITH ONE EGPWS
Normal procedures
F2000Airplane
Flight Manual
DTM537
EASA APPROVED
p
y
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
PAGE 3 / 6
F2000Airplane
Flight Manual
SUPPLEMENT 12CA/C WITH ONE EGPWS
Normal procedures Issue 1
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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Part 2
PAGE 4 / 6
Issue 1
SUPPLEMENT 12CA/C WITH ONE EGPWS
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 12CA/C WITH ONE EGPWS
Normal procedures Issue 1
DTM537
EASA APPROVED
TERRAIN CLEARANCE FLOOR
GNDPROX annunciation in PFD.
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.
GNDPROX annunciation in PFD.
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 annunciation in PFD.
TERRAIN AHEAD - PULL UP or OBSTACLE AHEAD - PULL UP voice warning(continuously):
Autopilot........................................................................................................................Disconnected
Level the wings.
Execute a positive pull up.
Power levers.....................................................................................................................TAKE-OFF
AIRBRAKES handle............................................................................................................Position 0Landing 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 12CA/C WITH ONE EGPWS
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 12CA/C WITH ONE EGPWS
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
SUPPLEMENT 12CA/C WITH ONE EGPWS
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
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
SUPPLEMENT 12CA/C WITH ONE EGPWS
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 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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Part 2A
PAGE 4 / 6
Issue 1
SUPPLEMENT 12CA/C WITH ONE EGPWS
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 12CA/C WITH ONE EGPWS
Normal procedures (US registered A/C with M1605) Issue 1
DTM537
US registered A/C with M1605
EASA APPROVED
TERRAIN CLEARANCE FLOOR
GNDPROX annunciation in PFD.
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.
GNDPROX annunciation in PFD.
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.
PULL UP annunciation in PFD.
TERRAIN TERRAIN - PULL UP or OBSTACLE OBSTACLE - PULL UP voice warning(continuously):
Autopilot........................................................................................................................Disconnected
Level the wings.
Execute a positive pull up.
Power levers.....................................................................................................................TAKE-OFF
AIRBRAKES handle............................................................................................................Position 0Landing 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 12CA/C WITH ONE EGPWS
Normal procedures (US registered A/C with M1605)
F2000Airplane
Flight Manual
p
y
INTENTIONALLY LEFT BLANK