F2000 - AFM SUP10 REV01 - 20100712

Part 0 PAGE 1 / 4

F2000 Airplane

Flight Manual

SUPPLEMENT 10 FLIGHT DYNAMICS HEAD UP GUIDANCE SYSTEM HGS 2850

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SUPPLEMENT No 10 TO THE EASA APPROVED FLIGHT MANUAL CONCERNING

FLIGHT DYNAMICS HEAD UP GUIDANCE SYSTEM HGS 2850

US REGISTERED A/C Serial No : Registration No : This supplement must be attached to the DTM537 Airplane Flight Manual approved by the DGAC on November 30, 1994. The information contained in this supplement, supplements that of sections 1 thru 5. The limitations, procedures and performance information which do not appear in this supplement remain these of sections 1 thru 5.

SECTIONS OF AIRPLANE FLIGHT MANUAL PARTS OF SUPPLEMENT - Section 1 : LIMITATIONS.......................................................................... Part 1, 1A, 1B, 1C and 1D - Section 2 : EMERGENCY PROCEDURES ....................................................................... No change - Section 3 : ABNORMAL PROCEDURES......................................................................Part 2 and 2A - Section 4 : NORMAL PROCEDURES....................................................... Part 3, 3A, 3B, 3C and 3D - Section 5 : PERFORMANCE ............................................................................................ No change - Annexes :......................................................................................................................... No change

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LIST OF REVISIONS

Parts changes Revision

and Date Title and

Approval reference Added Revised Removed

Original 29-jul-1997

FLIGHT DYNAMICS HEAD UP GUIDANCE SYSTEM HGS 2850 Software 1800-0040-001

Approved by DGAC.

First issue of Supplement 10.

Supplement 13 original (approved by DGAC on May 18, 1998), Supplement 19 original (approved by DGAC on November 15, 1999), Supplement 30A (approved by DGAC on June 20, 2003) and Supplement 31A (approved by DGAC on June 20, 2003) are merged into Supplement 10 revision 1.

Revsion 1 12-jul-2010

New page layout. Approved under DOA EASA.21.J.051

authority under change reference M3346.

Part 0 Issue 1 Part 1 Issue 1 Part 1A Issue 1 Part 1B Issue 1 Part 1C Issue 1 Part 1D Issue 1 Part 2 Issue 1 Part 2A Issue 1 Part 3 Issue 1 Part 3A Issue 1 Part 3B Issue 1 Part 3C Issue 1 Part 3D Issue 1

All pages.

Part 0 PAGE 3 / 4

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LIST OF EFFECTIVE PARTS

Reference Issue Special applicability

Part 0 Issue 1 US registered A/C Part 1 Issue 1 US registered A/C with M58B Part 1A Issue 1 US registered A/C with M58C, M1612 and M1437 Part 1B Issue 1 US registered A/C with M58D, M1612 and M1437

Part 1C Issue 1 US registered A/C with M2012 (SB F2000-157), M1612 and M1437

Part 1D Issue 1 US registered A/C with M2066 (SB F2000-157), M1612 and M1437

Part 2 Issue 1 US registered A/C with M58B Part 2A Issue 1 US registered A/C without M58B Part 3 Issue 1 US registered A/C with M58B Part 3A Issue 1 US registered A/C with M58C, M1612 and M1437 Part 3B Issue 1 US registered A/C with M58D, M1612 and M1437

Part 3C Issue 1 US registered A/C with M2012 (SB F2000-157), M1612 and M1437

Part 3D Issue 1 US registered A/C with M2066 (SB F2000-157), M1612 and M1437

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INTENTIONALLY LEFT BLANK

Part 1 PAGE 1 / 2

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Limitations (Software 1800-0040-001) Issue 1

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LIMITATIONS

GENERAL - HGS is approved as a supplementary flight display only. - PFD must be used as a primary source of flight and guidance information for all phases of flight.

CAUTION

The HUD display will be lost in the event of a LH engine failure or LH generator failure, (GEN 1 light on ), if the slats are retracted when, or after, the failure occurs, unless an alternate power source has been selected.

- The pilot’s sun visor must be stowed during approaches and take-off. - FMS waypoint is for situational awareness and is not to be used for navigation.

TAKE-OFF - Use of ILS symbology is not authorized:

- Do not select the ILS frequency.

APPROACH - Use of HGS is not authorized for ILS approaches: the combiner must be stowed. - For NDB approaches, HUD may be used to supplement the EFIS: navigation aids must be

displayed in the EFIS.

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Limitations (Software 1800-0040-001)

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Part 1A PAGE 1 / 2

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LIMITATIONS

CAUTION

If airplane is equipped with avionics COLLINS V6.0 (M1502) or V6.1 (M1649): Speed bugs are not displayed in the HUD for take-off. - Use of HUD is prohibited when VNAV is coupled with AP/FD, the combiner must be stowed. - If airplane is equipped with an E-GPWS (M1500), GND PROX Caution annunciation and PULL UP Warning annunciation are not displayed in the HUD.

GENERAL - The pilot’s sun-visor must be stowed during approaches and take-off. - FMS waypoint is for situational awareness and is not to be used for guidance. - The altitude display must be in feets.

TAKE-OFF WITH ILS SYMBOLOGY DISPLAYED - The ILS symbology has been found unsuitable for use as guidance or as a situational display for

low visibility take-offs. - Do not use the ILS symbology for maneuvering the airplane during take-off operations.

NON ILS APPROACH - For non instrument approaches, HUD may be used to supplement the EFIS: navigation aids must

be displayed in the EFIS.

CAT II / CAT III MANUAL APPROACH The highest wind values used for statistical analysis of simulation data and supported by flight evaluation for low visibility landings predicated on use of the HUD are listed below: - Maximum headwind component................................................................................................. 25 kt - Maximum tailwind component.................................................................................................... 10 kt - Maximum crosswind component................................................................................................ 15 kt

GENERAL - Minimum height for AP disconnection during Manual Cat.II / Cat.III .......................................... 500 ft

CAT II - HUD 2 or HUD 3 capability must be displayed.

CAT III - HUD 3 capability must be displayed.

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LIMITATIONS

GENERAL - The pilot’s sun-visor must be stowed during approaches and take-off. - FMS waypoint is for situational awareness and is not to be used for guidance.









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LIMITATIONS

GENERAL - The pilot’s sun-visor must be stowed during approaches and take-off. - FMS waypoint is for situational awareness and is not to be used for guidance. - The altitude display must be in feets.









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LIMITATIONS

GENERAL - The pilot’s sun-visor must be stowed during approaches and take-off. - FMS waypoint is for situational awareness and is not to be used for guidance.









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Part 2 PAGE 1 / 2

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Abnormal procedures (Software 1800-0040-001) Issue 1

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ABNORMAL PROCEDURES

GENERAL In the event of excessive or unusual attitude the PFD has been found to offer a more complete and intuitive attitude reference for recovery.

AIRPLANE EQUIPPED WITH 3 IRS FPV miscompare annunciation

FPV comparison annunciation in the Head Up Display. On the copilot side, perform an AHS reversion.

If FPV annunciation is removed: Continue to use the HUD.

If FPV annunciation is not removed: Delete the previous reversion and make an AHS reversion on the pilot side.


If FPV annunciation is not removed: Delete the previous reversion and stow the combiner.

AIRPLANE EQUIPPED WITH 2 IRS AND 1 AHRS OR 1 IRS AND 2 AHRS FPV miscompare annunciation





FPV comparison annunciation in the Head Up Display. Stow the combiner.

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Abnormal procedures (Software 1800-0040-002 or 1800-0040-003 or 9801-2060-103 or 9801-2060-004) Issue 1

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Applicable for airplane equipped with: - HGS 2850 software 1800-0040-002 after incorporation of M58C, M1612 and M1437, Or, - HGS 2850 software 1800-0040-003 after incorporation of M58D, M1612 and M1437, Or, - HGS 2850 software 9801-2060-103 after incorporation of M2010 (SB F2000-157), M1612 and

M1437, Or, - HGS 2850 software 9801-2060-004 after incorporation of M2066 (SB F2000-157), M1612 and

M1437.

ABNORMAL PROCEDURES

GENERAL In the event of excessive or unusual attitude the PFD has been found to offer a more complete and intuitive attitude reference for recovery.

WINDSHEAR Windshear caution

WINDSHEAR displayed amber in PFD and WINDSHEAR in HUD. See GPWS or TAWS Supplement procedure.

Windshear warning WINDSHEAR displayed red in PFD and WINDSHEAR in HUD. WINDSHEAR voice warning.

Go-Around pushbutton.......................................................................................................... Pressed Follow manually the HGS windshear guidance. Apply windshear procedures........................................ See GPWS or TAWS Supplement procedure




If FPV annunciation is not removed: Delete the previous reversion and make an AHS reversion on the pilot side.



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Abnormal procedures (Software 1800-0040-002 or 1800-0040-003 or 9801-2060-103 or 9801-2060-004)

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AIRPLANE EQUIPPED WITH 2 IRS AND 1 AHRS OR 1 IRS AND 2 AHRS FPV miscompare annunciation





FPV comparison annunciation in the Head Up Display. Stow the combiner.

MANUAL CAT II / III

PRIOR TO START THE APPROACH: If FPV annunciation is displayed:

Apply the procedures described on page 1 and page 2 of this Part.

FROM START THE APPROACH THROUGH TOUCHDOWN: If engine failure

or Loss of HUD symbology

or Approach warning (below 500 ft above runway)

or FPV annunciation:

Perform an immediate missed approach procedure if insufficient visual references to make an unaided visual landing.

NOTE

Do not make any sensor reversion below 500 ft. A valid FPV is needed to continue the approach below 500 ft.

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NORMAL PROCEDURES

GENERAL - Pilot has to deploy the combiner, adjust the symbology brightness and seat position. - The Scales On display format should be used for all flight phases.

APPROACH - No data entry required on HUD Control Panel except SLOPE if desired.

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Part 3A PAGE 1 / 6

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NORMAL PROCEDURES

CAUTION

If airplane is equipped with avionics COLLINS V6.0 (M1502) or V6.1 (M1649): - Speed bugs are not displayed in the HUD for take-off. - Use of the HUD is prohibited when VNAV is coupled with AP/FD, the combiner must be stowed. - If airplane is equipped with an E-GPWS (M1500), GNDPROX Caution annunciation and PULL UP Warning annunciation are not displayed in the HUD.

The HUD is approved for the following uses, with the PFD available as the primary source of flight and guidance information: - Visual take-off, - En Route (including Climb and Descent), - Visual approaches, - Non ILS approaches, - Monitoring automatic ILS approaches, except monitoring Cat. II approaches when COLLINS

avionics V6.1 is installed. Additionally, the HUD has been demonstrated to meet the airworthiness criteria of AC 120–29 and AC 120–28C for manual ILS approaches.

NOTE

In order to avoid a nuisance display caused by the speed error tape symbol, do not press the Go-Around pushbutton at take-off.

GENERAL - Pilot has to deploy the combiner, adjust the symbology brightness and seat position. - The scales On display format should be used for all flight phases, except ILS approaches.

The scales Off display format may be selected at pilot’s discretion during ILS approach.

VISUAL AND NON ILS APPROACH - No parameters entry required. - Reference Glide slope and Localizer track may be useful.

CAT I ILS APPROACH - The following parameters have to be entered in the Head Up Control panel:

- Localizer track, in true entered manually with an accuracy of 0.1 degree, if known, or by confirming the default value computed by the system.

- Runway elevation. - Reference glideslope.

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NOTE

- If an approach is interrupted after Glide Slope capture, the Go-Around pushbutton should be used in order to allow the display of the Flight Director when selecting other modes. - If during an approach the Go-Around pushbutton is inadvertently pressed, the pilot has to deselect and select again the ILS frequency then arm APPR mode in order to recover the whole CAT. III symbology.

GO-AROUND - If a touch and go is performed after an ILS approach, pilot must select GA in order to retrieve the

GA symbology.

NOTE

If the GA is not selected after a Touch and Go, the Flight Director in the HUD is not displayed after a selection of other modes.

CAT II MANUAL APPROACH Manual Cat II operations are predicated on the use of ILS facilities with performance and integrity equivalent to, or better than, a United States Type II ILS (i.e. ICAO Facility Performance Category II or Category III). The Head Up system has been demonstrated to meet the airworthiness and performance criteria of Advisory Circular 120-29, Appendix 1, for use in Cat II manual approaches with : - HUD 2 or HUD 3 annunciation displayed. - The following equipments installed and operative.

- Head Up System including: - HGS computer, - HGS overhead unit, - HGS combiner, - HGS control panel.

- 2 PFD (Primary Flight Displays), one on each side. - 1 IRS (Inertial Reference Sensor) displayed on the left side. - 1 independent IRS displayed on the right side. - 2 ILS receivers one displayed on the left side, the other on the right side. - 2 radio-altimeters displayed on both sides. - 2 ADC (Air Data Computer) one on each side. - Stand-by horizon. - 2 operating engines. - 2 independent hydraulic systems. - 2 independent electrical power sources. - Windshields wipers at each pilot station.

Airplane configuration - Landing configuration (40° SLATS + FLAPS).

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Minimum crew - 2 pilots with qualification according to operational rules.

NOTE

Compliance with the certification standards does not constitute an approval to conduct Cat II operations. Such authorization must be obtained by the Operator from the appropriate authorities.

CAT III MANUAL APPROACH Manual Cat III operations are predicated on the use of ILS facilities with performance and integrity equivalent to, or better than, a United States Type III ILS (i.e. ICAO Facility Performance Cat III). The Head Up system has been demonstrated to meet the Fail Passive landing systems airworthiness and performance criteria of Advisory Circular 120-28C, Appendix 1, for use in Cat III manual approaches with : - HUD 3 annunciation displayed. - The following equipments installed and operative.


- 2 PFD (Primary Flight Displays), one on each side. - 1 IRS (Inertial Reference Sensor) displayed on the left side. - 1 independent IRS displayed on the right side. - 2 ILS receivers one displayed on the left side, the other on the right side. - 2 radio-altimeters, one on each side. - 1 GPWS (Ground Proximity Warning System) or E-GPWS with radio-altitude call out. - 2 ADC (Air Data Computer) one on each side. - Stand-by horizon. - 2 operating engines. - 2 independent hydraulic systems. - 2 independent electrical power sources. - Windshields wipers for each pilot station.

The Head Up system has been shown to meet the airworthiness and performance criteria of AC 120-28C for fail passive Cat IIIA operations demonstrated to the following conditions. - Maximum demonstrated winds :

- Headwind component ......................................................................................................... 30 kt - Tailwind component............................................................................................................ 10 kt - Crosswind component ........................................................................................................ 18 kt

- Demonstrated runway elevation (by simulation of DENVER airport) ...................................... 5,431 ft - Demonstrated minimum visual segment 600 ft at 50 ft above TDZ. Airplane configuration - Landing configuration (40° SLATS + FLAPS).

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Minimum crew - 2 pilots with qualification according to operational rules.

NOTE

Compliance with the certification standards does not constitute an approval to conduct Cat III operations. Such authorization must be obtained by the Operator from the appropriate authorities.

CAT II / III MANUAL APPROACH A successful and safe approach depends essentially on the pilot accurate following of the HUD Flight Director and approach speed, and on the copilot careful monitoring of primary deviations.

Stand-by horizon.................................................................................................................. Checked Both radio-altimeters............................................................................................................... Tested Both altimeters..................................................................................................................... Checked DH ............................................................................................................................Set on both side On the SPEED / BARO / HEIGHT control panel:

Approach speed................................................................................................ Computed and set

NOTE

Certified Cat III Approach Speed equal to VREF + 1/2 headwind component + gust. The result being limited to VREF + 20 kt.

ILS frequency....................................................................................................... Select on both side Nav source .................................................................................................. VOR / LOC on both side Course (MAGNETIC) ................................................................................................Set on both side On HGS control panel:

Loc track (TRUE) default value confirmed, or Exact value, if known.................................................................................................................Set Runway elevation......................................................................................................................Set

NOTE

If QFE setting is used, runway elevation must be set to zero.

GS slope (between 2.5° and 3°) ................................................................................................Set On the Flight Guidance Control Panel:

APP mode............................................................................................................................Armed FD:

On left side................................................................................................................................ON On right side..............................................................................................................................ON

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NOTE

As long as radio-altimeter is not displayed on EFIS or HUD autopilot must be engaged for interception and tracking of ILS.

The glide slope beam must be captured not later than 1,000 ft above the runway.

AT 1,000 FT ABOVE THE RUNWAY: Landing configuration........................................................................................................... Checked AP.................................................................................................................................Disconnected Airplane trimmed on the three axes ..................................................................................... Checked (yaw axis should be carefully trimmed) ILS beam tracking...............................................................................................................Stabilized Approach speed..................................................................................................................Stabilized Altimeters and radio-altimeters ...................................................................................Cross-checked On HUD and PFD’s:

HUD 2 or HUD 3 green annunciations...................................................... Checked and called out

FROM 1,000 FT AND DOWN: Pilot follows precisely the HUD Flight Director and maintains the approach speed. Below 200 ft (radio-altimeter), he also monitors outside and must be prepared to initiate a go-around procedure, Copilot monitors instrument panel and calls out any deficiencies.

AT DH: Landing or go-around according to visual references....................................... Called out by the pilot

NOTE

If not called out at DH, pilot decision must be requested by the copilot.

For Cat III approaches only:

AT FLARE HEIGHT (FLARE DISPLAYED ON PFD): Flare..........................................................................................................Called out by the copilot

AT IDLE HEIGHT (IDLE DISPLAYED IN HUD AND PFD): Idle ............................................................................................................Called out by the copilot Power levers ..................................................................................................Reduced by the pilot

LANDING: Performed by the pilot following precisely the HUD Flight Director until the touchdown (to insure precise touchdown position), then using visual reference to maintain the airplane on the centerline while braking.

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GO-AROUND: GA pushbutton..................................................................................................... Pushed by the pilot Apply normal go-around procedure and establish go-around attitude using:

The HUD in normal case, The PFD if HUD symbology is off or unusable, The stand-by horizon if ATT flag or PITCH or ROLL comparator is displayed.

DEFICIENCIES: - The following must be called out by the copilot:

- Approach warning, - Expanded Loc deviation above one dot, - GS deviation above one dot (if radio altitude above 100 ft), - Airspeed 10 kt higher or 5 kt lower than approach speed, - Bank angle in excess of 10°, - Pitch attitude below -2.5° or above +7.5°, - Rate of descent in excess of 1,000 ft/mn, - Flag in view, - Warning on the warning panel.

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NORMAL PROCEDURES

The HUD is approved for the following uses, with the PFD available as the primary source of flight and guidance information: - Visual take-off, - En Route (including Climb and Descent), - Visual approaches, - Non ILS approaches, - Monitoring automatic ILS approaches. Additionally, the HUD has been demonstrated to meet the airworthiness criteria of AC 120–29 and AC 120–28C for manual ILS approaches.

NOTE

In order to avoid a nuisance display caused by the speed error tape symbol, do not press the Go-Around pushbutton at take-off.



VISUAL TAKE-OFF WITH ILS SYMBOLOGY DISPLAYED If the pilot wants to display the ILS symbology, he should apply the procedure :

Tune the ILS frequency on pilot's side, Select the inbound course of the localizer, On HCP, validate or enter the localizer track value, After alignment on the runway axis adjust if necessary the localizer track value (allow 30 seconds for symbology stabilization).

NOTE

The location and movement of the ILS symbology may vary from the true runway centerline. The ILS symbology has been found unsuitable for use as guidance or as a situational display for low visibility take-offs.

VISUAL AND NON ILS APPROACH - No parameters entry required. - Reference Glide slope and localizer track may be useful.

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NOTE

If an approach is interrupted after Glide Slope capture, the Go-Around pushbutton should be used in order to allow the display of the Flight Director when selecting other modes.


GA symbology.

NOTE

If the GA is not selected after a Touch and Go, the Flight Director in the HUD is not displayed after a selection of other modes.



- 2 PFD (Primary Flight Displays), one on each side. - 1 IRS (Inertial Reference Sensor) displayed on the left side. - 1 independent IRS displayed on the right side. - 2 ILS receivers one displayed on the left side, the other on the right side. - 2 radio-altimeters displayed on both sides. - 2 ADC (Air Data Computer) one on each side. - Stand-by horizon. - 2 operating engines. - 2 independent hydraulic systems.

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- 2 independent electrical power sources. - Windshields wipers at each pilot station.

Airplane configuration - Landing configuration (40° SLATS + FLAPS). Minimum crew - 2 pilots with qualification according to operational rules.

NOTE







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- Demonstrated runway elevation (by simulation of DENVER airport) ...................................... 5,431 ft - Demonstrated minimum visual segment 600 ft at 50 ft above TDZ. Airplane configuration - Landing configuration (40° SLATS + FLAPS). Minimum crew - 2 pilots with qualification according to operational rules.

NOTE



Stand-by horizon.................................................................................................................. Checked Both radio-altimeters............................................................................................................... Tested Both altimeters..................................................................................................................... Checked DH ............................................................................................................................Set on both side On the SPEED / BARO / HEIGHT control panel:


NOTE

Certified Cat II and Cat III Approach Speed equal to VREF + 1/2 headwind component + gust. The result being limited to VREF + 20 kt.



NOTE



APP mode............................................................................................................................Armed

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FD: On left side................................................................................................................................ON On right side..............................................................................................................................ON

NOTE







NOTE


AT FLARE HEIGHT (FLARE DISPLAYED ON PFD): Flare .............................................................................................................Called out by the copilot

AT IDLE HEIGHT (IDLE DISPLAYED IN HUD AND PFD): Idle................................................................................................................Called out by the copilot Power levers......................................................................................................Reduced by the pilot

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Part 3C PAGE 1 / 6

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Flight Manual



DTM537


EASA APPROVED

DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a

NORMAL PROCEDURES

The HGS is approved for the following uses, with the PFD available as the primary source of flight and guidance information: - Visual take-off, - En Route (including Climb and Descent), - Visual approaches, - Non ILS approaches, - Monitoring automatic ILS approaches. Additionally, the HUD has been demonstrated to meet the airworthiness criteria of AC 120–29 and AC 120–28C for manual ILS approaches.







NOTE

If during an approach the Go-Around pushbutton is inadvertently pressed, the pilot has to deselect and select again the ILS frequency then arm APPR mode in order to recover the whole CAT. III symbology.


GA symbology.

Part 3C PAGE 2 / 6

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F2000 Airplane

Flight Manual

DTM537

EASA APPROVED


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SAU

LT A

VIAT

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Pro

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Dat

a





NOTE


Part 3C PAGE 3 / 6

F2000 Airplane

Flight Manual



DTM537


EASA APPROVED

DAS

SAU

LT A

VIAT

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Pro

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Dat

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NOTE


Part 3C PAGE 4 / 6

Issue 1



F2000 Airplane

Flight Manual

DTM537

EASA APPROVED


DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a


Stand-by horizon.................................................................................................................. Checked Both radio-altimeters............................................................................................................... Tested Both altimeters.........................................................................................................Set and checked DH ............................................................................................................................Set on both side On the SPEED / BARO / HEIGHT control panel:


NOTE

Certified Cat III Approach Speed equal to VREF + 1/2 headwind component + gust. The result being limited to VREF + 20 kt.



NOTE



APP mode............................................................................................................................Armed FD:


NOTE



Part 3C PAGE 5 / 6

F2000 Airplane

Flight Manual



DTM537


EASA APPROVED

DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a





NOTE


For Cat III approaches only:

AT FLARE HEIGHT (FLARE DISPLAYED ON PFD): Flare..........................................................................................................Called out by the copilot

AT IDLE HEIGHT (IDLE DISPLAYED IN HUD AND PFD): Idle ............................................................................................................Called out by the copilot Power levers ..................................................................................................Reduced by the pilot




Part 3C PAGE 6 / 6

Issue 1



F2000 Airplane

Flight Manual

DTM537

EASA APPROVED


DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a



Part 3D PAGE 1 / 6

F2000 Airplane

Flight Manual



DTM537


EASA APPROVED

DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a

NORMAL PROCEDURES

The HGS is approved for the following uses, with the PFD available as the primary source of flight and guidance information: - Visual take-off, - En Route (including Climb and Descent), - Visual approaches, - Non ILS approaches, - Monitoring automatic ILS approaches. Additionally, the HUD has been demonstrated to meet the airworthiness criteria of AC 120–29 and AC 120–28C for manual ILS approaches.



VISUAL TAKE-OFF WITH ILS SYMBOLOGY DISPLAYED If the pilot wants to display the ILS symbology, he should apply the procedure :

Tune the ILS frequency on pilot's side, Select the inbound course of the localizer, On HCP, validate or enter the localizer track value, After alignment on the runway axis adjust if necessary the localizer track value (allow 30 seconds for symbology stabilization).

NOTE

The location and movement of the ILS symbology may vary from the true runway centerline. The ILS symbology has been found unsuitable for use as guidance or as a situational display for low visibility take-offs.





Part 3D PAGE 2 / 6

Issue 1



F2000 Airplane

Flight Manual

DTM537

EASA APPROVED


DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a


GA symbology.





NOTE


Part 3D PAGE 3 / 6

F2000 Airplane

Flight Manual



DTM537


EASA APPROVED

DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a







NOTE


Part 3D PAGE 4 / 6

Issue 1



F2000 Airplane

Flight Manual

DTM537

EASA APPROVED


DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a


Stand-by horizon.................................................................................................................. Checked Both radio-altimeters............................................................................................................... Tested Both altimeters.........................................................................................................Set and checked DH ............................................................................................................................Set on both side On the SPEED / BARO / HEIGHT control panel:


NOTE

Certified Cat II and Cat III Approach Speed equal to VREF + 1/2 headwind component + gust. The result being limited to VREF + 20 kt.



NOTE



APP mode............................................................................................................................Armed FD:


NOTE



Part 3D PAGE 5 / 6

F2000 Airplane

Flight Manual



DTM537


EASA APPROVED

DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a





NOTE


AT FLARE HEIGHT (FLARE DISPLAYED ON PFD): Flare .............................................................................................................Called out by the copilot

AT IDLE HEIGHT (IDLE DISPLAYED IN HUD AND PFD): Idle................................................................................................................Called out by the copilot Power levers......................................................................................................Reduced by the pilot




Part 3D PAGE 6 / 6

Issue 1



F2000 Airplane

Flight Manual

DTM537

EASA APPROVED


DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a



F2000 - AFM SUP10 REV01 - 20100712

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Transcript of F2000 - AFM SUP10 REV01 - 20100712