Post on 06-Apr-2018
8/3/2019 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
y
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
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 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
y
INTENTIONALLY LEFT BLANK