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F2000Airplane

Flight Manual

SUPPLEMENT 5OPERATION WITH ONE MARK V GPWS

Table of contents Issue 1

DTM537

EASA APPROVED

SUPPLEMENT No 5 TO THE EASA APPROVED AIRPLANE FLIGHT MANUAL

CONCERNING OPERATION

WITH ONE MARK V GPWS

AFTER INCORPORATION OF MODIFICATION M66 or M923 or M1169 or M784B

Serial No :

Registration No :

This supplement must be attached to the DTM537 Airplane Flight Manual approved by the DGAC onNovember 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 ofsections 1 thru 5.SECTIONS OF AIRPLANE FLIGHT MANUAL PARTS OF SUPPLEMENT

- Section 1 : LIMITATIONS.................................................................................................. No change

- Section 2 : EMERGENCY PROCEDURES ....................................................................... No change

- Section 3 : ABNORMAL PROCEDURES.......................................................................... No change

- Section 4 : NORMAL PROCEDURES.......................................................................................Part 1- Section 5 : PERFORMANCE ............................................................................................ No change

- Annexes :......................................................................................................................... No change

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Issue 1

SUPPLEMENT 5OPERATION WITH ONE MARK V GPWS

Table of contents

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

p

y

LIST OF REVISIONS

Parts changesRevisionand Date

Titleand

Approval reference Added Revised Removed

Original

12-may-1995

Operation with one MARK V GPWS

Approved by DGAC.

First Issue of supplement 5.

Revision 1

07-mar-1996

Approved by DGAC. Pages 2, 4 and 10.

Revision 2

18-nov-1996

Approved by DGAC. Pages 1 and 2.

Revision 3

30-dec-1996

Approved by DGAC. Pages 1 and 2.

Revision 4

16-jun-1999

Approved by DGAC. Pages 1, 2, 3, 4, 5 and6.

Pages 7, 8, 9, 10, 11and 12.

Revision 5

12-jul-2010

New page layout.

Approved under DOA EASA.21.J.051authority under change referenceM3346.

Part 0 Issue 1

Part 1 Issue 1

All pages.

LIST OF EFFECTIVE PARTS

Reference Issue Special applicability

Part 0 Issue 1

Part 1 Issue 1

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F2000Airplane

Flight Manual

SUPPLEMENT 5OPERATION WITH ONE MARK V GPWS

Normal procedures Issue 1

DTM537

EASA APPROVED

ON GROUND

- Prior to every flight:

Perform a short system self test:TESTpushbutton............................................................................................................. Pushed

Lights............................................................................................................................ Checked

IN FLIGHT

NOTE

When any of the GPWS alert lights are illuminated, the TCAS is placed in TA ONLY mode whichinhibits all TCAS aural messages.

APPROACH

NOTE

If landing is expected with flaps 20, or below, set the GPWS FLAPS ORIDE switch to on positionin order to inhibit the TOO LOW FLAPS warning.

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SUPPLEMENT 5OPERATION WITH ONE MARK V GPWS

Normal procedures

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

p

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GROUND PROXIMITY WARNINGS SYSTEM - ALERTS

WARNINGSMODESVOICES LIGHTS

MODE 1 Excessive descent rate

SINKRATE

WHOOP WHOOP

PULL UP

PULL UP

MODE 2 Excessive terrain closure rate

TERRAIN TERRAIN

WHOOP WHOOP

PULL UP

PULL UP

MODE 3 Altitude loss after take-off DONT SINK PULL UP

MODE 4 Unsafe terrain clearance TOO LOW TERRAINTOO LOW GEAR

TOO LOW FLAPS

PULL UP

MODE 5 Excessive glideslope deviation GLIDESLOPEBELOW

GS

MODE 6 CalloutsVersus configuration(see Part 1 page 3) *

WINDSHEAR (PFD)MODE 7 Windshear

WINDSHEAR WINDSHEAR (PFD)

* Depending on call-out menu selected.

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F2000Airplane

Flight Manual

SUPPLEMENT 5OPERATION WITH ONE MARK V GPWS

Normal procedures Issue 1

DTM537

EASA APPROVED

GROUND PROXIMITY WARNINGS - MODES 1 TO 4

PULL UP light on with associated voice warning:

SINK RATE or TERRAIN TERRAIN or DON'T SINK or TOO LOW GEAR or TOO LOWFLAPS or TOO LOW TERRAIN.

Adjust the flight path / configuration until the PULL UP light goes out and the voice warning stops.

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 0Landing gear..................................................................................................................................Up

Slat-flap handle................................................................................. 20 FLAPS + SLATS maximum

Maintain best rate of climb until terrain clearance is assured.

GROUND PROXIMITY WARNINGS - MODE 5

BELOW GS light on.

GLIDESLOPE voice warning.

Initiate corrective action to fly the airplane back to the glideslope axis

or

Inhibit the warning (GS INHIBIT pushbutton) in case of visual approach.

ADVISORY CALLOUTS - MODE 6

- EXCESSIVE BANK ANGLE.

- MINIMUMS / APPROACHING MINIMUMS.

- HEIGHT.

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SUPPLEMENT 5OPERATION WITH ONE MARK V GPWS

Normal procedures

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

p

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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