F2000 - AFM SUP01 REV04 - 20100712
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Transcript of F2000 - AFM SUP01 REV04 - 20100712
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8/3/2019 F2000 - AFM SUP01 REV04 - 20100712
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Part 0
PAGE 1 / 2
F2000Airplane
Flight Manual
SUPPLEMENT 1A/C WITH ONE COLLINS TCAS II
Table of contents Issue 1
DTM537
EASA APPROVED
SUPPLEMENT No 1 TO THE EASA APPROVED FLIGHT MANUAL
CONCERNING
THE OPERATION OF AIRPLANE EQUIPPED WITH ONE COLLINS TCAS II
AFTER INCORPORATION OF MODIFICATION M85 or M927B or M785B.
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 ..........................................................................................................Part 1
- Section 2: EMERGENCY PROCEDURES................................................................................Part 1
- Section 3: ABNORMAL PROCEDURES...................................................................................Part 1
- Section 4: NORMAL PROCEDURES........................................................................................Part 2
- Section 5: PERFORMANCE ............................................................................................. No change- Annexes:...........................................................................................................................No change
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Part 0
PAGE 2 / 2
Issue 1
SUPPLEMENT 1A/C WITH ONE COLLINS TCAS II
Table of contents
F2000Airplane
Flight Manual
DTM537
EASA APPROVED
p
y
LIST OF REVISIONS
Parts changesRevisionand Date
Titleand
Approval reference Added Revised Removed
Original
14-feb-1995
Approved by DGAC First Issue of supplement 1.
Revision 1
07-mar-1996
Approved by DGAC Pages 2, 4, 5 and 6.
Revision 2
07-oct-1996
Approved by DGAC Pages 1 and 2.
Revision 3
30-dec-1996
Approved by DGAC Pages 1 and 2.
Revision 4
12-jul-2010
New page layout.
Approved under DOA EASA.21.J.051authority under change referenceM3346.
Part 0 Issue 1
Part 1 Issue 1
Part 2 Issue 1
All pages
LIST OF EFFECTIVE PARTS
Reference Issue Special applicability
Part 0 Issue 1
Part 1 Issue 1
Part 2 Issue 1
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Part 1
PAGE 1 / 2
F2000Airplane
Flight Manual
SUPPLEMENT 1A/C WITH ONE COLLINS TCAS II
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 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 Checked
If the RA FAIL message is still in view :
TCAS .........................................................................................................................RTU : ST BY
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Part 1
PAGE 2 / 2
Issue 1
SUPPLEMENT 1A/C WITH ONE COLLINS TCAS II
Limitations, Emergency and Abnormal procedures
F2000Airplane
Flight Manual
DTM537
EASA APPROVED
p
y
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
SUPPLEMENT 1A/C WITH ONE COLLINS TCAS II
Normal procedures Issue 1
DTM537
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 do
so, 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):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
SUPPLEMENT 1A/C WITH ONE COLLINS TCAS II
Normal procedures
F2000Airplane
Flight Manual
DTM537
EASA APPROVED
p
y
PREFLIGHT CHECK
ATC transponder ......................................................................................................ST BY then ALT
TCAS....................................................................................................................................... AUTO
TEST 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 2,500 ft:
TCAS .............................................................................................................................. TA ONLY
AFTER LANDING
ATC .........................................................................................................................................ST BY