Honeywell PRIMUS 1000 Manual

PRIMUS 1000
Integrated Avionics System
Pilot's Manual for the
Embraer 145
AD-52817@

Printed inU.S.A.Pub.No.A28--1146--112--00 August1997
Business and CommuterAviation Systems
Honeywell Inc.
Box 29000
Phoenix,Arizona 85038--9000
PRIMUSr1000Integrated
AvionicsSystem
forthe
Embraer Model145
Pilot’sManual

ASSOCIATE
MEMBER
Member ofGAMA
GeneralAviation
Manufacturer’sAssociation
E
PRIMUSisatrademarkofHoneywell Inc.
E1997 Honeywell Inc.
PROPRIETARYNOTICE
Thisdocumentand the information disclosed herein are proprietary
data ofHoneywell Inc.Neitherthisdocumentnorthe information
contained hereinshall be used,reproduced,ordisclosed to others
without thewritten authorizationofHoneywellInc., excepttotheextent
required forinstallation ormaintenance ofrecipient’sequipment.
NOTICE-- FREEDOMOFINFORMATIONACT(5USC552)AND
DISCLOSUREOFCONFIDENTIALINFORMATIONGENERALLY
(18 USC1905)
Thisdocumentisbeing furnished inconfidence byHoneywell Inc.The
informationdisclosedhereinfallswithinexemption(b)(4)of5USC552
and the prohibitionsof18 USC1905.
S97

PRIMUSr1000 Integrated Avionics System
Record ofRevisions
A28--1146--112--00 RR--1/(RR--2 blank)
Record ofRevisions
Upon receiptofarevision,insert the latestrevised pagesand dispose
ofsuperseded pages.Enter revision numberand date,insertion date,
and the incorporator’sinitialson the Record ofRevisions.The typed
initialsHIare used when Honeywell Inc.isthe incorporator.
Revision
NumberRevision DateInsertion DateBy

PRIMUSr1000 Integrated Avionics System
Record ofTemporaryRevisions
A28--1146--112--00 RTR--1/(RTR--2 blank)
Record ofTemporaryRevisions
Upon receiptofatemporaryrevision,insert the yellowtemporary
revision pagesaccording tothe filing instructionson each page.Then,
enterthe temporaryrevision number,issue date,and insertion date on
thispage.
Temporary
Revision
No. IssueDate
Datethe
Temporary
Revision Was
Incorporated
byaRegular
Revision
Insertion of
Temporary
Revision,
Date/By
Removalof
Temporary
Revision,
Date/By

PRIMUSr1000 Integrated Avionics System
A28--1146--112--00 ListofEffectivePages
LEP--1
ListofEffective Pages
Original0. . . . Aug 1997
Subheading and PageRevision Subheading and PageRevision
TitlePage 0
Record ofRevisions
RR--1/RR--2 0
Record ofTemporaryRevisions
RTR--1/RTR--2 0
ListofEffectivePages
LEP--1 0
LEP--2 0
LEP--3 0
LEP--4 0
LEP--5/LEP--6 0
Table ofContents
TC--1 0
TC--2 0
TC--3 0
TC--4 0
TC--5 0
TC--6 0
TC--7 0
TC--8 0
TC--9 0
TC--10 0
TC--11 0
TC--12 0
Introduction
1--1 0
1--2 0
1--3/1--4 0
F1--5/1--6 0
SystemDescription
2--1 0
2--2 0
2--3 0
2--4 0
2--5 0
2--6 0
2--7 0
2--8 0
2--9 0
2--10 0
F2--11/2--12 0
ElectronicDisplaySystem(EDS)
3--1/3--2 0
F3--3/3--4 0
3--5 0
3--6 0
3--7 0
3--8 0
ElectronicFlight InstrumentSystem
(EFIS)4--1/4--2 0
F4--3/4--4 0
4--5 0
4--6 0
4--7 0
4--8 0
4--9 0
4--10 0
4--11 0
4--12 0
4--13 0
4--14 0
4--15 0
4--16 0
4--17 0
4--18 0
4--19 0
4--20 0
Findicatesright foldoutpage with blankback.
Hindicates changed,added ordeleted pages.
Findicatesright foldoutpage withablankback.

PRIMUSr1000 Integrated Avionics System
A28--1146--112--00
ListofEffectivePages
LEP--2
Subheading and PageRevision Subheading and PageRevision
ElectronicFlight InstrumentSystem
(EFIS) (cont)
4--21 0
4--22 0
4--23 0
4--24 0
4--25 0
4--26 0
F4--27/4--28 0
4--29 0
4--30 0
4--31 0
4--32 0
4--33 0
4--34 0
4--35 0
4--36 0
4--37 0
4--38 0
4--39 0
4--40 0
4--41 0
4--42 0
4--43 0
4--44 0
4--45 0
4--46 0
4--47 0
4--48 0
4--49 0
4--50 0
4--51 0
4--52 0
4--53 0
4--54 0
4--55 0
4--56 0
4--57 0
4--58 0
4--59 0
4--60 0
4--61 0
4--62 0
4--63 0
4--64 0
4--65 0
4--66 0
4--67 0
4--68 0
4--69 0
4--70 0
4--71 0
4--72 0
4--73 0
4--74 0
4--75 0
4--76 0
4--77 0
4--78 0
4--79 0
4--80 0
4--81 0
4--82 0
4--83 0
4--84 0
4--85 0
4--86 0
4--87 0
4--88 0
4--89 0
4--90 0
4--91 0
4--92 0
4--93 0
4--94 0
4--95 0
4--96 0
4--97 0
4--98 0
4--99 0
4--100 0
Engine Instrumentand CrewAlerting
System(EICAS)
5--1/5--2 0
F5--3/5--4 0
5--5 0
5--6 0
5--7 0
5--8 0
5--9 0
5--10 0
5--11 0
5--12 0
5--13 0
5--14 0

PRIMUSr1000 Integrated Avionics System
A28--1146--112--00 ListofEffectivePages
LEP--3
Subheading and PageRevision Subheading and PageRevision
Engine Instrumentand CrewAlerting
System(EICAS) (cont)
5--15 0
5--16 0
5--17 0
5--18 0
5--19 0
5--20 0
5--21 0
5--22 0
5--23 0
5--24 0
5--25 0
5--26 0
5--27 0
5--28 0
5--29 0
5--30 0
5--31 0
5--32 0
5--33 0
5--34 0
FlightGuidanceSystem
6--1 0
6--2 0
6--3 0
6--4 0
6--5 0
6--6 0
6--7/6--8 0
SystemLimits
7--1 0
7--2 0
7--3 0
7--4 0
7--5 0
7--6 0
7--7 0
7--8 0
ModesofOperation
8--1 0
8--2 0
8--3 0
8--4 0
8--5 0
8--6 0
8--7 0
8--8 0
8--9 0
8--10 0
8--11 0
8--12 0
8--13 0
8--14 0
8--15 0
8--16 0
8--17 0
8--18 0
8--19 0
8--20 0
8--21 0
8--22 0
8--23 0
8--24 0
8--25 0
8--26 0
8--27 0
8--28 0
8--29 0
8--30 0
8--31 0
8--32 0
8--33 0
8--34 0
8--35 0
8--36 0
8--37 0
8--38 0
8--39 0
8--40 0
8--41/8--42 0
Troubleshooting
9--1 0
9--2 0
9--3 0
9--4 0
9--5 0
9--6 0
9--7 0
9--8 0
9--9 0

PRIMUSr1000 Integrated Avionics System
A28--1146--112--00
ListofEffectivePages
LEP--4
Subheading and PageRevision Subheading and PageRevision
Troubleshooting (cont)
9--10 0
9--11 0
9--12 0
9--13/9--14 0
Honeywell ProductSupport
10--1 0
10--2 0
10--3 0
10--4 0
Abbreviations
11--1 0
11--2 0
11--3 0
11--4 0
11--5 0
11--6 0
AppendixA
A--1/A--2 0
FA--3/A--4 0
A--5 0
A--6 0
A--7 0
A--8 0
A--9 0
A--10 0
A--11/A--12 0
AppendixB
B--1 0
B--2 0
B--3 0
B--4 0
B--5 0
B--6 0
B--7 0
B--8 0
B--9 0
B--10 0
B--11 0
B--12 0
AppendixC
C--1/C--2 0
FC--3/C--4 0
C--5 0
C--6 0
C--7 0
C--8 0
C--9 0
C--10 0
C--11 0
C--12 0
C--13 0
C--14 0
C--15 0
C--16 0
C--17 0
C--18 0
C--19 0
C--20 0
C--21 0
C--22 0
C--23 0
C--24 0
C--25 0
C--26 0
C--27 0
C--28 0
C--29 0
C--30 0
C--31 0
C--32 0
C--33 0
C--34 0
C--35 0
C--36 0
C--37 0
C--38 0
IndexIndex--1 0
Index--2 0
Index--3 0
Index--4 0
Index--5 0
Index--6 0
Index--7 0
Index--8 0
Index--9 0
Index--10 0
Index--11 0

PRIMUSr1000 Integrated Avionics System
A28--1146--112--00 ListofEffectivePages
LEP--5/(LEP--6 blank)
Subheading and PageRevision Subheading and PageRevision
Index(cont)
Index--12 0
Index--13 0
Index--14 0
Index--15 0
Index--16 0
Index--17 0
Index--18 0
Index--19 0
Index--20 0
Index--21 0
Index--22 0
Index--23 0
Index--24 0