f2000 - afm sup12a original - 20100712
TRANSCRIPT
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
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Part 1
PAGE 1 / 2
F2000Airplane
Flight Manual
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 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.
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Part 1
PAGE 2 / 2
Issue 1
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 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.
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Part 1A
PAGE 1 / 2
F2000Airplane
Flight Manual
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 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 made
obstructions.
- 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.
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.
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Part 1A
PAGE 2 / 2
Issue 1
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 andDisplay TAAD 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 1B
PAGE 1 / 2
F2000Airplane
Flight Manual
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 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 made
obstructions.
- 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) 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 1C
PAGE 1 / 2
F2000Airplane
Flight Manual
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 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 made
obstructions.
- 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) 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 the
flight.
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Part 1C
PAGE 2 / 2
Issue 1
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 andDisplay TAAD 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 2
PAGE 1 / 6
F2000Airplane
Flight Manual
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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.
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.
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Part 2
PAGE 2 / 6
Issue 1
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 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
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Part 2
PAGE 3 / 6
F2000Airplane
Flight Manual
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 12AA/C WITH ONE EGPWS AND A 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 12AA/C WITH ONE EGPWS AND A 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 12AA/C WITH ONE EGPWS AND A 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 12AA/C WITH ONE EGPWS AND A 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.
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.
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Part 2A
PAGE 2 / 6
Issue 1
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 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
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Part 2A
PAGE 3 / 6
F2000Airplane
Flight Manual
SUPPLEMENT 12AA/C WITH ONE EGPWS AND A 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 12AA/C WITH ONE EGPWS AND A 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 12AA/C WITH ONE EGPWS AND A 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 12AA/C WITH ONE EGPWS AND A TERRAIN DISPLAY
Normal procedures (US registered A/C with M1605)
F2000Airplane
Flight Manual
p
y
INTENTIONALLY LEFT BLANK