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F2000Airplane
Flight Manual
SUPPLEMENT 21AA/C WITH FMS (GNS-X/ES) MOD 4
Table of contents Issue 1
DTM537
EASA APPROVED
SUPPLEMENT No 21A TO THE EASA APPROVED FLIGHT MANUAL
CONCERNING
AIRPLANE EQUIPPED WITH FMS (GNSX/ES) MOD 4
AFTER INCORPORATION OF MODIFICATION M885
Serial No :
Registration No :
This supplement must be attached to the DTM537 Airplane Flight
Manual approved by the DGAC onNovember 30, 1994, when the airplane
incorporates M885.
The information contained in this supplement, supplements that
of sections 1 thru 5 and annexes.The limitations, procedures and
performance information which do not appear in this
supplementremain these of sections 1 thru 5 and annexes.
SECTIONS OF AIRPLANE FLIGHT MANUAL PARTS OF SUPPLEMENT
- Section 1 :
LIMITATIONS..........................................................................................................Part
1
- Section 2 : EMERGENCY PROCEDURES
.......................................................................
No change
- Section 3 : ABNORMAL
PROCEDURES..........................................................................
No change
- Section 4 : NORMAL
PROCEDURES...............................................................................
No change
- Section 5 : PERFORMANCE
............................................................................................
No change- Annexes
:.........................................................................................................................
No change
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SUPPLEMENT 21AA/C WITH FMS (GNS-X/ES) MOD 4
Table of contents
F2000Airplane
Flight Manual
DTM537
EASA APPROVED
p
y
LIST OF REVISIONS
Parts changesRevisionand Date
Titleand
Approval reference Added Revised Removed
Original
17-oct-2000
Approved by DGAC. First issue of supplement 21A.
Revision 1
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 21AA/C WITH FMS (GNS-X/ES) MOD 4
Limitations Issue 1
DTM537
EASA APPROVED
LIMITATIONS
GENERAL
The FMSs meet the accuracy criteria of AC 90.45A for en-route,
terminal and approach areasprovided the FMS is not in DR and
excepted when POS WARN (Position Warning) FMS message isdisplayed
on the CDU.
The minimum navigation performance required by NAT MNPS
regulations (French arrt ofNovember 5th, 1987 and FAR Part 91
Appendix C) are demonstrated provided that there are at least2 FMSs
and 2 IRSs in NAV mode operating on board.
LIMITATIONS
GNS-X/ES navigation must be periodically verified during the
flight, by:
- Reading the Quality Factor (QF or Q).
- Comparison with the other means of radio-navigation.
To monitor the FMS with VOR DME raw data, the VPU used for
monitoring should not be in autotunemode.
FUEL, TIME prediction informations are provided for advisory
purposes only and must not be used forflight plan purposes.
Use of following functions is not authorized:
- Holding pattern.
- VNAV.
- SID and STAR procedures.
- Approach.
Manual VOR tuning through the CDU is prohibited.
FMS must not be used for navigation above 75 North and below 75
South latitudes.GPS
- The GPS is not approved as a primary mean of navigation.
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SUPPLEMENT 21AA/C WITH FMS (GNS-X/ES) MOD 4
Limitations
F2000Airplane
Flight Manual
DTM537
EASA APPROVED
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INTENTIONALLY LEFT BLANK
