F2000 - AFM SUP01A Original - 20100712

8/3/2019 F2000 - AFM SUP01A Original - 20100712

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F2000Airplane

Flight Manual

SUPPLEMENT 1AA/C WITH ONE COLLINS TCAS II CHANGE 7

Table of contents Issue 1

DTM537

EASA APPROVED

SUPPLEMENT No 1A TO THE EASA APPROVED FLIGHT MANUAL

CONCERNING

THE OPERATION OF AIRPLANE EQUIPPED WITH ONE COLLINS TCAS II Change 7

AFTER INCORPORATION OF MODIFICATION M1861 (TCAS 94)

OR SERVICE BULLETIN F2000-191 (TCAS 94) OR M1874 (TCAS 4000)OR M1996 (TCAS 4000) OR M2054 (TCAS 4000) OR M2133 (TCAS 4000)

OR M2145 (TCAS 4000) OR M2195 (TCAS 4000)

These equipments are compliant with ACAS II performance level

Serial No :

Registration No :

This supplement must be attached to the DTM537 Airplane Flight Manual approved by the DGAC onNovember 30, 1994, when the airplanes incorporates M1861 or SB F2000-191 or M1874 or M1996 orM2054 or M2133 or M2145 or M2195.

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 ..........................................................................................................Part 1

- Section 2: EMERGENCY PROCEDURES................................................................................Part 1

- Section 3: ABNORMAL PROCEDURES...................................................................................Part 1

- Section 4: NORMAL PROCEDURES............................................................................Part 2 and 2A

- Section 5: PERFORMANCE ............................................................................................. No change

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


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Table of contents

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

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LIST OF REVISIONS

Parts changesRevisionand Date

Titleand

Approval reference Added Revised Removed

Original

12-jul-2010

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

Supplement 20 revision 5 (approved by DGAC on April 20, 2000) ismoved in Supplement 1A original.

First issue of Supplement 1A.

LIST OF EFFECTIVE PARTS

Reference Issue Special applicabilityPart 0 Issue 1

Part 1 Issue 1

Part 2 Issue 1 A/C with RTU 4020

Part 2A Issue 1 A/C with RTU 4220


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Part 1

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F2000Airplane

Flight Manual


Limitations, Emergency and Abnormal procedures Issue 1

DTM537

EASA APPROVED

LIMITATIONS

TCAS II SYSTEM OPERATION LIMITATIONS

Pilots are authorized to deviate from their current ATC clearance to the extent necessary to complywith a TCAS II resolution advisory (RA).

Following a TCAS II "clear of conflict" advisory, the pilot should expeditiously return to the applicableATC clearance unless otherwise directed by ATC.

EMERGENCY PROCEDURES

In the event of an engine failure:

TCAS .............................................................................................................................. TA ONLY

ABNORMAL PROCEDURES

MODE S TRANSPONDER FAILURE

Change in ATC color code (green to cyan).

ATC1 / ATC2 selection ............................................................................................... 1 to 2 or 2 to 1

TCAS II SYSTEM FAILURE

Yellow TCAS FAIL message on both PFD and

Yellow TCAS FAIL or TD FAIL message on both MFD.

ATC1 / ATC2 selection ............................................................................................... 1 to 2 or 2 to 1

If the message is still in view :

TCAS ........................................................................................RTU : AUTO or TA/RA Checked

If the message remains still in view :

TCAS......................................................................................................................RTU : ST BY

LOSS OF RESOLUTION ADVISORIES INFORMATION

Yellow RA FAIL message on both PFD and MFD.

TCAS............................................................................................RTU : AUTO or TA/RA Checked

If the RA FAIL message is still in view :

TCAS .........................................................................................................................RTU : ST BY


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Issue 1


Limitations, Emergency and Abnormal procedures

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

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LOSS OF VERTICAL SPEED INFORMATION

VS flag instead of the scale on PFD.RA FAIL message.

Operate with the other VSI indicator without flag.


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Part 2

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F2000Airplane

Flight Manual


Normal procedures (A/C with RTU 4020) Issue 1

DTM537

A/C with RTU 4020

EASA APPROVED

NORMAL PROCEDURES

TCAS II OPERATION

General information- The INCREASE CLIMB RA is de-activated when the slat-flap handle is in the 40 FLAPS +SLATS

position; in this case the CLIMB RA remains annunciated for advisory only.

- Compliance with a TCAS II resolution (RA) is necessary unless the pilot considers it unsafe to doso, or unless the pilot has better information about the cause of the RA and can maintain safeseparation from a nearby airplane, obvious TCAS II system failure, etc.

- The pilot should not initiate evasive maneuvers using information from the traffic display only or ona traffic advisory (TA) only without visually sighting the traffic. These displays and advisories areintended only for assistance in visually locating the traffic and lack of flight path trends necessaryfor use in evasive maneuvering.However, while climbing or descending, modest change in vertical speed based on traffic display

information is not considered evasive maneuvering.RESOLUTION ADVISORY

In case of resolution advisories (RAs) or suddent reversion of RAs sense:Disconnect the autopilot.

Promptly and smoothly perform the evasive maneuver.

If the stall, GPWS or windshear occurs:

Immediately stop the evasive maneuver.

Perform the procedure corresponding to the warning in progress.

CAUTION

Once an RA has been issued, safe separation could be compromised if current vertical speedis changed, except as necessary to comply with the RA.This is because TCAS II - to TCAS II coordination may be in progress with the intruderairplane, and any change in vertical speed that does not comply with the RA may negate theeffectiveness of the other airplane's compliance with the RA.


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Part 2

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Issue 1


Normal procedures (A/C with RTU 4020)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with RTU 4020

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PREFLIGHT CHECK

ATC switch ............................................................................................................... ATC 1 or ATC 2

ATC mode ...................................................................................................................................ALT

TCAS....................................................................................................................................... AUTOTEST pushbutton (ATC or TCAS)................................................................................Pushed 1 sec.

Symbol................................................................................................................................Displayed

Voice callout TCAS SYSTEM TEST OK at the end of test..................................................... Verified

ATC transponder .....................................................................................................................ST BY

BEFORE TAKE-OFF

ATC transponder .........................................................................................................................ALT

MFD................................................................................................................ TCAS visual displayed

APPROACH

If a CLIMB message is issued:

Perform the GO-AROUND procedure (see 4-150-25).

If approach is performed on parallel runways separated by less than 1,200 ft:

TCAS .............................................................................................................................. TA ONLY

AFTER LANDING

ATC .........................................................................................................................................ST BY


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Part 2A

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F2000Airplane

Flight Manual


Normal procedures (A/C with RTU 4220) Issue 1

DTM537

A/C with RTU 4220

EASA APPROVED

NORMAL PROCEDURES

TCAS II OPERATION

General information- The INCREASE CLIMB RA is de-activated when the slat-flap handle is in the 40 FLAPS +SLATS

position; in this case the CLIMB RA remains annunciated for advisory only.

- Compliance with a TCAS II resolution (RA) is necessary unless the pilot considers it unsafe to doso, or unless the pilot has better information about the cause of the RA and can maintain safeseparation from a nearby airplane, obvious TCAS II system failure, etc.

- The pilot should not initiate evasive maneuvers using information from the traffic display only or ona traffic advisory (TA) only without visually sighting the traffic. These displays and advisories areintended only for assistance in visually locating the traffic and lack of flight path trends necessaryfor use in evasive maneuvering.However, while climbing or descending, modest change in vertical speed based on traffic display

information is not considered evasive maneuvering.RESOLUTION ADVISORY

In case of resolution advisories (RAs) or suddent reversion of RAs sense:Disconnect the autopilot.

Promptly and smoothly perform the evasive maneuver.

If the stall, GPWS or windshear occurs:

Immediately stop the evasive maneuver.

Perform the procedure corresponding to the warning in progress.

CAUTION

Once an RA has been issued, safe separation could be compromised if current vertical speedis changed, except as necessary to comply with the RA.This is because TCAS II - to TCAS II coordination may be in progress with the intruderairplane, and any change in vertical speed that does not comply with the RA may negate theeffectiveness of the other airplane's compliance with the RA.


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Part 2A

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Issue 1


Normal procedures (A/C with RTU 4220)

F2000Airplane

Flight Manual

DTM537

EASA APPROVED

A/C with RTU 4220

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PREFLIGHT CHECK

ATC ...........................................................................................................................ST BY then ON

ATC mode ALT.............................................................................................................................ON

TCAS.......................................................................................................................................TA/RATEST pushbutton (ATC or TCAS)................................................................................Pushed 1 sec.

Symbol................................................................................................................................Displayed

Voice callout TCAS SYSTEM TEST OK at the end of test..................................................... Verified

ATC transponder .....................................................................................................................ST BY

BEFORE TAKE-OFF

ATC transponder ..................................................................................................... ON and ALT ON

MFD................................................................................................................ TCAS visual displayed

APPROACH

If a CLIMB message is issued:

Perform the GO-AROUND procedure (see 4-150-25).

If approach is performed on parallel runways separated by less than 1,200 ft:

TCAS .............................................................................................................................. TA ONLY

AFTER LANDING

ATC .........................................................................................................................................ST BY

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F2000 - AFM SUP01A Original - 20100712