F2000 - AFM SUP11 REV04 - 20100712

Part 0 PAGE 1 / 4

F2000 Airplane

Flight Manual

SUPPLEMENT 11 FLIGHT DYNAMICS HEAD UP GUIDANCE SYSTEM HGS 2850

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SUPPLEMENT No 11 TO THE EASA APPROVED FLIGHT MANUAL CONCERNING

FLIGHT DYNAMICS HEAD UP GUIDANCE SYSTEM HGS 2850

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 - 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 16-dec-1997

Flight Dynamics Head up Guidance System HGS 2850 Software 1800-0040-002

Approved by DGAC.

First Issue of supplement 11.

Revision 1 04-sep-1998

Approved by DGAC. Pages 2 and 3.

Revision 2 08-jan-1999

Approved by DGAC. Pages 2 and 3.

Revision 2 08-jan-1999

Approved by DGAC. Pages 2, 11 and 16.

Supplement 07 original (approved by DGAC on August 30, 1996), Supplement 18 revision 1 (approved by DGAC on November 07, 2001), Supplement 30 (approved by DGAC on June 20, 2003) and Supplement 31 (approved by DGAC on June 20, 2003) are merged into Supplement 11 revision 4.

Revision 4 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 3 Issue 1 Part 3A Issue 1 Part 3B Issue 1 Part 3C Issue 1 Part 3D Issue 1

All pages

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LIST OF EFFECTIVE PARTS

Reference Issue Special applicability

Part 0 Issue 1 Part 1 Issue 1 A/C with M58B Part 1A Issue 1 A/C with M58C Part 1B Issue 1 A/C with M58D Part 1C Issue 1 A/C with M2012 or SB F2000-157 Part 1D Issue 1 A/C with M2066 or SB F2000-157 Part 2 Issue 1 A/C with M58C or M58D or M2012 or M2066 or SB F2000-157 Part 3 Issue 1 A/C with M58B Part 3A Issue 1 A/C with M58C Part 3B Issue 1 A/C with M58D Part 3C Issue 1 A/C with M2012 or SB F2000-157 Part 3D Issue 1 A/C with M2066 or SB F2000-157

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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 - In case of excessive attitude or doubt, revert to PFD.

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

- Do not select the ILS frequency.

APPROACH - Manual Category 2 approaches are not authorized. Autopilot must be engaged. - The pilot’s sun-visor must be stowed during approaches and take-off. - For ILS approaches, APPR Mode has to be selected in order to have ILS symbology displayed. - If a touch and go is performed after an ILS approach, pilot must select GA in order to retrieve the

GA symbology. - For non precision approaches, HUD may be used to supplement the EFIS: navigation aids must be

displayed in the EFIS.

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Issue 1


Limitations (Software 1800-0040-001)

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LIMITATIONS

The HUD is approved for the following use: - Visual take-off, - En Route (included Climb and Descent), - Visual approaches (included Steep Approaches), - Non precision approaches, - Automatic approaches Cat I, - Automatic approaches Cat II (Monitoring) with Avionics V5.1 (M1253) and V6.0 (M1502), - Manual approaches Cat I Cat II and Cat III.

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.

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


CAT II / CAT III MANUAL APPROACH The Head Up system is certified for use in Cat II / III manual approaches within the following limits:

GENERAL - Minimum height for AP disconnection ....................................................................................... 500 ft - Maximum headwind component................................................................................................. 25 kt - Maximum tailwind component.................................................................................................... 10 kt - Maximum crosswind component................................................................................................ 15 kt

CAT II: - Runway equipped with Cat II ILS system.

- Minimum Decision Height (DH) ............................................................................................. 100 ft - Minimum Runway Visual Range (RVR)..................................................................1,000 ft / 300 m

- HUD 2 or HUD 3 capability must be displayed.

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CAT III: - Runway equipped with Cat III ILS system.

- Minimum Decision Height (DH) ............................................................................................... 50 ft - Minimum Runway Visual Range (RVR).....................................................................600 ft / 180 m

- HUD 3 capability must be displayed.

NOTE

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

MINIMUM EQUIPMENT LIST The following equipments should be in proper operating condition: - 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. - 2 radio-altimeters for CAT III. - 1 radio-altimeter displayed on both side for CAT II. - 1 GPWS (Ground Protection Warning System) with radio altitude call out (required for

CAT III only). - 2 ADC (Air Data Computer). - Stand-by horizon.

AIRPLANE CONFIGURATION - 2 operating engines. - Landing configuration (40° SLATS + FLAPS).

MINIMUM CREW - 2 pilots with qualification according to operational rules.

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LIMITATIONS

The HUD is approved for the following use: - Visual take-off. - En Route (included Climb and Descent). - Visual approaches (included Steep Approaches). - Non precision approaches. - Automatic approaches Cat. I. - Automatic approaches Cat. II (monitoring). - Manual approaches Cat. I Cat. II and Cat. III.

GENERAL - The pilot’s sun-visor must be stowed during approaches and take-off.



CAT II / CAT III MANUAL APPROACH The Head Up guidance system is certified for use in Cat II / III manual approaches within the following limits:


CAT II - Runway equipped with Cat II ILS system.



CAT III - Runway equipped with Cat III ILS system.



NOTE

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

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- 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. - 2 radio-altimeters. - 1 GPWS (Ground Protection Warning System) with radio altitude call out (required for CAT III only). - 2 ADC (Air Data Computer). - Stand-by horizon.



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LIMITATIONS

The HGS is approved for the following use: - Visual take-off. - En Route (included Climb and Descent). - Visual approaches (included Steep Approaches). - Non precision approaches. - Automatic approaches Cat. I. - Automatic approaches Cat. II (monitoring) with avionics V5.1 (M1253). - Manual approaches Cat. I Cat. II and Cat. III.












NOTE


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- 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. - 2 radio-altimeters for Cat III. - 1 radio-altimeter displayed on both side for Cat. II. - 1 GPWS (Ground Protection Warning System) with radio altitude call out (required for CAT III only). - 2 ADC (Air Data Computer). - Stand-by horizon.



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LIMITATIONS

The HGS is approved for the following use: - Visual take-off. - En Route (included Climb and Descent). - Visual approaches (included Steep Approaches). - Non precision approaches. - Automatic approaches Cat. I. - Automatic approaches Cat. II (monitoring). - Manual approaches Cat. I Cat. II and Cat. III.












NOTE


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- 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. - 2 radio-altimeters. - 1 GPWS (Ground Protection Warning System) with radio altitude call out (required for CAT III only). - 2 ADC (Air Data Computer). - Stand-by horizon.



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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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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. Monitor wind direction and intensity evolution in comparison with tower wind. Maintain or let the airspeed increase (consider a go around).

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

Go-Around pushbutton.......................................................................................................... Pressed Follow manually the HGS windshear guidance. Power levers.....................................................................................................................TAKE-OFF AIRBRAKES handle............................................................................................................Position 0 Slat-flap handle................................................................................. 20° FLAPS + SLATS maximum At pilot's discretion according to airplane height and vertical speed.

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

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.

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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. On the copilot side, perform an AHS reversion.


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

AIRPLANE EQUIPPED WITH 2 IRS FPV miscompare annunciation

FPV comparison annunciation in the Head Up Display.

If the pilot can clearly identify the faulty IRS: Perform an IRS reversion on appropriate side. Continue to use the HUD provided cross-check between flight path symbol position and basic flight data is performed.

If the pilot cannot identify the faulty IRS: Stow the combiner.

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MANUAL CAT II / III

ABOVE 500 FT ABOVE RUNWAY: If FPV annunciation is displayed, apply the procedures described on page 1 and page 2 of this Part.

BETWEEN 500 FT ABOVE RUNWAY AND DH: If engine failure

or Loss of HUD symbology

or Approach warning

or FPV annunciation:

Perform an immediate missed approach procedure if insufficient visual references.

BELOW DH: If loss of HUD symbology

or Approach warning

or FPV annunciation:

Perform an immediate missed approach procedure, except if airplane position and attitudes certainly allow a safe landing.

NOTE

Do not make any sensor reversion below 500 ft.

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

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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, except ILS approaches. The

Scales Off format may be selected at pilot’s discretion during the approach..

APPROACH - Approach parameters have to be entered in the Head Up Control panel:

- Localizer track, in true with an accuracy of 0.1 degree. - Runway elevation - Reference glideslope

NOTE

For visual or non precision approaches, the localizer track can be set equal to runway track in true (1.0 degree accuracy).

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Normal procedures (Software 1800-0040-001)

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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, except ILS approaches.

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

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 AND NON PRECISION 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.

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.

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CAT II / III 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............................................................................................................................ OFF

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.

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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.

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.

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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



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.





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.

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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 FD:


NOTE



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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 / 4

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NORMAL PROCEDURES







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.


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.

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NOTE



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


NOTE






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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






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NORMAL PROCEDURES








GA symbology.


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.



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NOTE



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


NOTE







NOTE


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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 4 / 4

Issue 1



F2000 Airplane

Flight Manual

DTM537

EASA APPROVED


DAS

SAU

LT A

VIAT

ION

Pro

prie

tary

Dat

a


F2000 - AFM SUP11 REV04 - 20100712

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Transcript of F2000 - AFM SUP11 REV04 - 20100712