Honeywell SPZ-8000 User manual

Honeywell
CommercialFlightSystemsGroup
Businessand Commuter AviationSystemsDivision
HoneywellInc.
BOX 29000
Phoenix,Arizona85038
SPZ-8000 Digital Automatic Flight
Control System
Gulfstream IV
System
Maintenance Manual
Volume I—System and Component Description,
and System Operation
22-14-00
TITLE PAGE T-1
PRINTED IN U.S./L PUB. NO, Al 5-1146-38 REVISED 15 APRIL 1993
1JUNE 1987

PROPRIETARY NOTICE
This document and the information disclosed herein are proprietary data of Honeywell Inc. Neither
this document nor the information contained herein shall be used, reproduced, or disclosed
to others without the written authorization of Honeywell Inc., except to the extent required for
installation or maintenance of recipient’s equipment.
NOTICE -FREEDOM OF INFORMATION ACT (5 USC 552) AND
DISCLOSURE OF CONFIDENTIAL INFORMATION GENERALLY (18 USC 1905)
This document is being furnished in confidence by Honeywell Inc. The information disclosed herein
falls within exemption (b) (4) of 5USC 552 and the prohibitions of 18 USC 1905.
S93
LASEREF and PR!MIJS are registered trademarks of Honeywe/f Inc.
COLORCAL, COLORARAR, and LASERTRAK are additional trademarks of Honeywell Inc.
CopyrigtM 1993 Honeywell Inc.
All Rights Reserved REVISED 15 APRIL 1993
1JUNE 1987

Honeywell’s Continuous Quality
READER COMMENTS
Date
Process
Received
(Mail or FAX this form to [602] 436-4100)
Honeywell welcomes all comments and recommendations to improve future editions of this publication.
Your Name Company/Airline
State Country Zip
Telephone No. FAX Date
Honeywell Pub. No. ATA No.
Manual Title
COMMENTS/RECOMMENDATIONS:
LOCAL REPRODUCTION ENCOURAGED
(If returning by mail, please tape closed; Postal regulations prohibit use of staples.)

FOLD FOLD
----------------------------------------------------------------------------------------------------------------------------------------------------------------
From:
Place StampHere
Honeywell
Commercial Flight Systems Group
Business and Commuter Aviation
Systems Division
Logistics Quality Administrator
MS AV2CC85C3
P.O. Box 29000
Phoenix, AZ 85038-9000
----------------------------------------------------------------------------------------------------------------------------------------------------------------
FOLD FOLD

Date
REPORT OF POSSIBLE DATA ERROR
(Mail or FAX this form to [602] 436-4100)
Your Name Company/Airline
Received
Address
State Country Zip
Telephone No. FAX Date
Honeywell Pub. No. ATA No.
Manual Title
PAGE
NO. PARA-
GRAPH FIGURE
NO. TABLE NO. PROBLEM
I
HONEYWELL REPLY-
APPROVAL
LOCAL REPRODUCTION ENCOURAGED
(If returning by mail, please tape closed; Postal regulations prohibit use of staples.)

FOLD FOLD
-----------------------------------------------------------------------------------------------------------------------------------------------------------------
From:
Place Stamp Here
Honeywell
Commercial Flight Systems Group
Business and Commuter Aviation
Systems Division
Logistics Quality Administrator
MS AV2CC85C3
P.O. Box 29000
Phoenix, AZ 85038-9000
---------------------------------------------------------------------------------------------------------------------------------------------------------------
FOLD FOLD

RECORD OF REVISIONS - VOLUME I
For each revision, put the revised pages in your manual and discard the
superseded pages. Write the revision number and date, date put in manual, and
the incorporator’s initials in the applicable columns on the Record of Revisions.
The initials HI show Honeywell Inc. is the incorporator.
Revision Revision Insertion
Number Date Date By Revision Revision Insertion
Number Date Date By
01
02
03
04
05
06
Feb 1/88
Mar 1/89
Ott 1/89
Mar 15/91
Aua 15/91
Ai)r 15/93
Mar 1/88
ADr 15/89
~
ADr 15/91
Nov 1/91
Jul 1/93
HI
HI
HI
HI
HI
HI
22-14-00
Page RR-1/RR-2
Aug 15/91
Use 01 disclosure of information on this page is subject to the restrictions on the title page of this document.

Honeywell ~~~${~~’
LIST OF EFFECTIVE PAGES
Original . . 0. . Jun 1/87
Revision . . 1. . Feb 1/88
Revision . . 2. . Mar 1/89
Revision . . 3. . Ott 1/89
SUBHEADING AND PAGE REVISION
Title
T-1 m
T-2 ■
Record of Revisions
RR-1/RR-2
List of Effective Pages
LEP-1 ■
LEP-2 ●
LEP-3 8
LEP-4 ■
LEP-5 ■
LEP-6 m
LEP-7 ■
LEP-8 m
Table of Contents
TC-1 ■
TC-2 ■
TC-3 ■
TC-4 ■
TC-5 ■
TC-6 ■
TC-7 ■
TC-8 ■
TC-9 ■
TC-10 ■
TC-11 ■
TC-12 ■
TC-13 ■
TC-14 ■
TC-15 ■
TC-16 ■
TC-17 ■
TC-17 ■
TC-18 ■
6
6
5
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
Revision .. 4 .. Mar 15/91
Revision .. 5 .. Aug 15/91
Revision .. 6 .. Apr 15/93
SUBHEADING AND PAGE
TC-20
TC-21
TC-23/TC-24
Introduction
INTRO-1
INTRO-2
INTRO-3
INTRO-4
INTRO-5
INTRO-6
INTRO-7
INTRO-8
INTRO-9
INTRO-10
INTRo-11/INTRo-12
System Description
;
3
4
4.1/4.2
F 5/6
F 7/8
9
10
11
12
13
14
15
16
17
18
18.1
18.2
■
■
■
■
■
■
■
■
■
■
■
■
■
■
■
■
■
■
■
■
m
■
■
■
■
●
■
REVISION
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
5
6
6
6
5
:
5
6
5
6
6
6
■indicates changed, added, or deleted page.
F indicates right foldout page with blank back. 22-14-00
Page LEP-1
Apr 15/93
Useor disclosure of information on this page issubject to the restrictions on the title page of this document.

Honeywell
SUBHEADING AND PAGE REVISION
System Description (cent)
18.3
18.4
18.5/18.6
19
20
21
22
23
24
25
26
27/28
F 29/30
Component Description
101
102
103
104
105
106
107
108
109
110
111/112
F 113/114
115
116
117
118
119/120
F 121/122
123
124
125
126
127
128
128.1
128.2
128.3
128.4
128.5
128.6
128.7
128.8
128.9
128.10
128.11
■6
■6
■6
■6
■:
5
5
5
5
5
5
5
96
■:
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
■6
5
5
=6
■6
■6
■6
■6
■6
86
■6
■6
■6
■6
■6
●6
;;WW$JANCE
GULFSTREAMIV
SUBHEADING AND PAGE
128.12
128.13/128.14
129
130
131
132
133
134
135/136
F 137/138
139
140
141
142
143
144
145
146
147
148
149
150
151/152
153/154
155
156
157
158
159
160
161
162
163
164
165
166
166/1/166.2
F 167/168
F 169/170
171
172
173
174
175
176
177
178
179
180
181
182
■
■
■
■
8
■
m
■
■
■
■
REVISION
6
6
5
5
5
;
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
2
5
5
6
6
6
6
5
5
5
5
5
5
6
5
5
5
5
5
6
5
5
5
5
5
5
6
6
22-14-00
Page LEP-2
Apr 15/93
Useor disclosure of information on this page issubject tothe restrictionson the title page of this document.

Honeywell
SUBHEADING AND PAGE REVISION
Component Description (cent)
183
184
185
186
187
188
189
190
191
192
193
194
195
196
196.1
196.2
196.3
196.4
196.5/196.6
197
198
198.1
198.2
198.3/198.4
198.4.1/198.4.2
F 198.5/198.6
F 198.7/198.8
198.9
198.10
198.11
198.12
198.13
198.14
198.15
198.16
198.17/198.18
F 198.19/198.20
198.21
198.22
198.23
198.24
198.25
198.26
198.27
198.28
198.29
198.30
198.31/198.32
F 198.33/198.34
198.35
■
9
■
9
m
8
■
■
■
5
:
5
5
:
:
6
i
5
2
6
!?
6
5
5
5
5
5
6
5
5
5
5
5
5
5
:
5
5
5
5
5
5
5
5
5
5
5
5
5
5
6
5
MAINTENANCE
MANUAL
GULFSTREAMIV
SUBHEADING AND PAGE REVISION
198.36
198.37
198.38
198.39
198.40
198.41
198.42
198.43
198.44
198.45
198.46
198.47
198.48
198.49
198.50
198.51
198.52
198.53/198.54
F 198.55/198.56
198.57
198.58
198.59/198.60
F 198.61/198.62
198.63
198.64
198.65/198.66
F 198.67/198.68
F 198.69/198.70
198.71
198.72
198.73
198.74
F 198.75/198.76
198.77
198.78
198.79
198.80
F 198.81/198.82
198.83
198.84
198.85
198.86
198.87
198.88
198.89
198.90
198.91
198.92
198.93
198.94
198.95
5
5
5
5
5
5
5
5
5
;
5
5
■:
5
5
■6
5
5
5
5
5
5
5
:
5
5
5
5
;
5
5
5
5
5
5
5
5
5
5
■6
5
5
5
5
5
■6
22-li-oo
Page LEP-3
Apr 15/93
Use or disclosure of information on this page is subject to the restrictions on the title page of this document,

Honeywell
SUBHEADING AND PAGE REVISION
Component Description (cent)
198.96 -
198.97/198.98
F 198.99/198.100
198.101
198.102
198.103
198.104
198.105
198.106
198.107
198.108
198.109
198.110
198.111
198.112
198.113
198.114
198.115
198.116
198.117
198.118
198.119
198.120
198.121
198.122
F 198.123/198.124
F 198.125/198.126
198.127
198.128
198.129
198.130
198.131
198.132
198.133/198.134
F 198.135/198.136
198.137
198.138
198.139
198.140
198.141
198.142
198.143
198.144
198.145
198.146
198.147
198.148
F 198.149/198.150
198.151
198.152
5
5
5
5
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
:
6
5
5
5
5
6
5
5
5
5
6
6
6
5
5
5
5
5
5
5
5
:
5
MAINTENANCE
MANUAL
GULFSTREAMIV
SUBHEADING AND PAGE
198.153
198.154
198.155
198.156
198.157
198.158
198.159
198.160
198.161
198.162
198.163
198.164
198.165
198.166
198.167
198.168
198.169
198.170
198.171
198.172
198.173
198.174
198.175
198.176
198.177
198.178
198.179
198.180
198.181
198.182
198.183
198.184
198.185
198.186
198.187
198.188
198.189
198.190
198.191
198.192
198.193
198.194
198.195
198.196
198.197
198.198
198.199
198.200
198.201
198.202
198.203
■
■
m
■
m
■
■
■
■
■
■
m
m
■
●
■
■
9
■
■
●
■
■
■
■
■
■
9
■
■
●
■
#
■
■
■
■
■
■
■
■
■
■
■
REVISION
:
6
5
5
5
5
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
6
22-14-00
Page LEP-4
Apr 15/93
Use or disclosure of informationon this page is subject to the restrictions onthe title page of this document,

Hone~elI
SUBHEADING AND PAGE REVISION
Component Description (cent)
198.204
198.205
198.206
198.207
198.208
198.209/198.210
System Operation
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
■
■
■
■
■
●
■
●
■
■
m
■
■
■
9
■
9
■
■
■
■
■
6
6
6
6
6
6
5
5
5
5
5
6
5
5
:
5
6
5
5
5
6
5
6
5
5
5
5
6
5
6
6
6
5
5
6
6
6
6
6
5
5
5
:
5
5
6
MAINTENANCE
MANUAL
GULFSTREAMIV
SUBHEADING AND PAGE
243
244
245
246
247
248
249
250
251
252
253
254
255
256
257
258
259
260
261
262
263
264
265
266
F 267/268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
289
290
291
292
293
294
■
■
■
■
■
●
m
REVISION
5
5
6
6
5
:
6
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
6
5
z
5
5
z
5
5
5
:
5
5
6
5
5
5
5
5
5
5
5
22-14-00
Page LEP-5
Apr 15/93
Use or disclosure of information on this page is subject to the restrictions onthe title page of this document.

SUBHEADING AND PAGE
Honeywell
System Operation (cent)
295
296
297
298
298.1
298.2
298.3
298.4
298.5
298.6
298.7
298.8
298.9
298.10
298.11
298.12
298.13
298.14
298.15
298.16
298.17
298.18
298.19
298.20
298.21
298.22
298.23
298.24
298.25
298.26
298.27
298.28
298.29
298.30
298.31
298.32
298.33
298.34
298.35
298.36
298.36.1
298.36.2
298.36.3
298.36.4
298.36.5
298.36.6
298.36.7
298.36.8
298.36.0
298.36.10
REVISION
i
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
5
2
5
5
:
5
5
5
5
5
5
5
5
:
5
5
5
5
■6
●6
●6
●6
●6
m6
m6
m6
■
■:
MAINTENANCE
MANUAL
GULFSTREAMIV
SUBHEADING AND PAGE
298.36.11 ■
298.36.12 ■
298.36.13 ■
298.36.14 ■
298.36.15 ■
298.36.16
298.36.17/298.36.18 :
298.37
298.38
298.39
298.40
298.41
298.42
298.43
298.44
298.45
298.46
298.47
298.48
298.49/298.50
F 298.51/298.52
F 298.53/298.54
F 298.55/298.56
F 298.57/298.58
298.59
298.60
298.61
298.62
298.63
298.64
298.65
298.66
298.67
298.68
298.69
298.70
298.71
298.72
298.73
298.74
298.75/298.76
F 298.77/298.78
F 298.79/2-98.80
298.81
298.82
298.83
298.84
298.85
298.86
298.87
298.88
■
■
■
■
■
■
■
■
■
■
■
■
■
■
■
■
REVISION
6
6
6
6
6
6
6
5
6
6
5
5
5
6
5
:
6
5
5
5
5
5
:
5
6
5
6
5
5
5
5
6
6
5
6
6
5
5
5
6
5
5
6
5
5
:
6
6
22-14-00
Page LEP-6
Apr 15/93
Use or disclosure of information on this page is subject to the restrictions on the title page of this document.

Honeywell
SUBHEADING AND PAGE REVISION
System Operation (cent)
298.89
298.90 ■
298.91 ■
298.92
298.93
298.94
298.95
298.96
298.97
298.98
298.99
298.100
F 298.101/298.102
F 298.103/298.104 =
F 298.105/298.106 m
F 298.107/298.108 =
298.109
298.110 ■
298.111
298.112 9
298.112.1/298.112.2 ■
298.113
298.114
298.115 m
298.116 a
298.117 ■
298.118
298.119
298.120
298.121
298.122
298.123
298.124 ■
298.125
298.126
F 298.127/298.128
F 298.129/298.130
F 298.131/298.132
F 298.133/298.134
F 298.135/298.136
F 298.137/298.138 ■
F 298.139/298.140
F 298.141/298.142
298.143
298.144 ■
F 298.145/298.146 ■
F 298.147/298.148 ■
298.149 9
298.150
298.151 ■
5
6
6
5
5
5
5
5
5
5
5
5
5
6
6
6
:
5
6
6
5
:
6
6
5
5
5
5
5
:
5
5
5
5
i
5
6
5
5
;
6
6
6
5
6
MAINTENANCE
MANUAL
GULFSTREAMIV
SUBHEADING AND PAGE
298.152
F 298.153/298.154 ■
298.155 ■
298.156 ■
298.157
298.158
298.159
298.160
298.161/298.162 ■
F 298.163/298.164 ■
298.165 ■
298.166 ■
298.166.1/298.166.2 ■
298.167
298.168
298.169
298.170
298,171
298.172
298.173
298.174
298.175 ■
298.176
298.176.1/298.176.2 =
298.177
298.178
298.179 ■
298.180
298.181
298.182 ■
298.183
298.184
298.185
298.186
298.187/298.188
F 298.189/298.190 =
298.191/298.192
F 298.193/298.194 =
298.195
298.196
298.197/298.198 ■
F 298.199/298.200 ■
298.201
298.202 ■
298.203/298.204
F 298.205/298.206
F 298.207/298.208 ■
F 298.209.298.210
298.211 ■
298.212 ■
298.213 ■
REVISION
2
6
6
5
:
5
6
6
6
6
6
5
5
5
5
5
5
5
5
6
5
6
5
5
6
5
5
6
5
5
5
5
5
6
5
6
5
5
6
6
5
6
5
5
6
2
6
6
22-14-00
Page LEP-7
Apr 15/93
Use or disclosure of informationon this page is subject to the restrictions onthe title page of this document.

SUBHEADING AND PAGE
System Operation (cent)
298.214
298.214.1
298.214.2
298.214.3
298.214.4
298.214.5/298.214.6
298.215
298.216
298.217
298.218
298.219
298.220
298.221
298.222
298.223/198.224
REVISION SUBHEADING AND PAGE REVISION
96
■6
■6
■6
■6
86
5
■6
5
5
■6
5
5
■2
22-14-00
Page LEP-8
Apr 15/93
Use or disclosure of information on this page is subject to the restrictions on the title page of this document.

TABLE OF CONTENTS
Section
1
Subheading ~
VOLUME I
Svstem Descri~tion
General
;: System Description
A. LASEREF@ II Inertial Reference System (IRS)
B. ADZ-81O Air Data System
C. AA-300 Radio Altimeter System
D. EDZ-884 Electronic Display System (EDS)
E. DFZ-820 Dual Flight Guidance System
PRIMUS@ 800 Weather Radar System
;: PRIMUS@ 870 Weather Radar System
H. FMZ-800 Flight Management System
I. Engine Pressure Ratio System
J. VLF/Omega System (Optional)
[. LSZ-850 Lightning Sensor System (Optional)
. TCZ-91O Traffic Alert and Collision Avoidance
System (Optional)
~. MLZ-850 Microwave Landing System (Optional)
. Global Positioning System (Optional)
1
10
12
12
13
14
15
15
1:
18!!
18.4
18.5
18.5
3. Avionics Standard Communications Bus (ASCB) Description 19
Coml)onentDescription
General
;: LASEREF@ II Inertial Reference System (IRS)
A. Inertial Reference Unit
B. Mode Select Unit
Inertial System Display Unit (ISDU)
;: Optional LASERTRAKW Navigation Display Unit (NDU)
3. ADZ-81O Air Data System
4. AA-300 Radio Altimeter System
A. RT-300 Radio Altimeter Receiver Transmitter
B. AT-222 Radio Altimeter Antenna
Paragraph 5 is not applicable to this System.
:: EDZ-884 Electronic Display System
A. DU-880 Display Unit
B. SG-884 Symbol Generator
C. DC-884 Display Controller
D. DA-884 Data Acquisition Unit
E. DP-884 Dimmer Panel
101
101
102
102
116
124
128.4
130
140
140
144
145
146
146
156
172
198.10
198.22
22-14-00
Page TC-1
Apr 15/93
Use or disclosure of informationon this page is subject to the restrictions onthe title page of this document.

Section
2
TABLE OF CONTENTS (cent)
Subheading
VOLUME I
Comoonent Description (cent)
6. F. FC-880 Fault Warning Computer
G. MD-880 Checklist Module
7. DFZ-820 Dual Flight Guidance System
A. FZ-820 Flight Guidance Computer
B. GP-820 Flight Guidance Controller
PC-880 Turn Pitch Controller
:: SM-600 Dual Servo/SB-600 Bracket and
TM-260 Dual Trim Servo/TB-261 Bracket
8. PRIMUS@ 800 Weather Radar System
A. WR-800 Receiver Transmitter
B. WC-81O Weather Radar Controller
c. WA-800 Antenna Pedestal and FP-900 24-Inch
Flat-Plate Radiator
8.1 PRIMUS@ 870 Weather Radar System
A. WU-870 Antenna and Receiver Transmitter Unit
B. WC-874 Weather Radar Controller
9. FMZ-800 Flight Management System (FMS)
A. NZ-920 Navigation Computer
B. CD-81O Control Display Unit
C. DL-800 or DL-900 Data Loader
D. PZ-800 Performance Computer
E. SM-81O Servo-Autothrottle
10. Engine Pressure Ratio (EPR) System
11. Optional VLF/Omega System
A. OZ-800 Receiver Processor Unit (RPU)
B. AT-800 Antenna Coupler Unit (ACU) -
Teardrop H-Field
C. AT-801 Antenna Coupler Unit (ACU) -
Brick H-Field
D. AT-803 Antenna Coupler Unit (ACU) -
Blade E-Field
12. Optional LSZ-850 Lightning Sensor System
A. LP-850 Lightning Sensor Processor
LU-860 Lightning Sensor Controller
:: AT-850 Antenna
D. AT-855 Antenna
Paqe
198.24
198.36
198.38
198.38
198.50
198.58
198.64
198.72
198.72
198.78
198.84
198.88
198.88
198.92
198.102
198.102
198.128
198.138
198.142
198.152
198.154
198.160
198.160
198.166
198.168
198.170
198.172
198.172
198.176
198.180
198.182
LL-14-00
Page TC-2
Apr 15/93
Use or disclosure of information on this page is subject to the restrictions on the title page of this document.

Section
2
Paqe
TABLE OF CONTENTS (cent)
Subheading
VOLUME I
ComDonent Descrit)tion(Cent)
13. Optional TCZ-91O Traffic Alert and Collision 198.184
Avoidance System (TCAS)
A. RT-91O TCAS Computer 198.184
B. AT-91O Directional Antenna 198.189
c. Typical Bottom OmnidirectionalAntenna (Optional) 198.191
14. Optional MLZ-850 Microwave Landing System (MLS)
A. ML-850 Microwave Landing System Receiver
B. CM-850 Control/DisplayUnit
15. Optional Global Positioning System (GPS)
Global Positioning System Sensor Unit
System Operation
General
;: EDZ-884 Electronic Display System
A.
::
D.
E.
::
H.
I.
J.
K.
Display System Formats
EFIS/EICAS System Components
Primary Flight Display (PFD)
Navigation Display (ND) Formats
Engine (ENG) Display
Crew Alerting System (CAS) Display
System Page Displays
Compacted EICAS Display
EFIS/EICAS Reversionary Modes
Traffic Alert and Collision Avoidance System
(TCAS) Displays
Microwave Landing System (MLS)
3. DFZ-820 Dual Flight Guidance System
A. System Performance/OperatingLimits
198.192
198.192
198.196
198.204
198.204
201
201
202
202
202
206
223
261
277
292
298.22
298.27
298.36.1
298.36.12
298.37
298.37
B. Fiight Director/AutopilotF~nctional Description 298.43
4. FMZ-800 Flight Management System 298.149
A. General 298.149
B. NZ-920 Navigation Computer 298.152
c. PZ-800 Performance (Autothrottle)Computer 298.166
D. Target Speeds 298.211
22-14-00
Page TC-3
Apr 15/93
Use or disclosure of information on this page is subject to the restrictions on the title page of this document.
,,,

TABLE OF CONTENTS (cent)
Section Subheading
VOLUME II
4Ground Check
1. General
Equipment and Materials
:: Procedure
VOLUME 111
5Fault Isolation
General
;: Procedure
3. LASEREF@ II Inertial Reference System (IRS)
A. Self-Test
B. System Navigation Performance Determination
and Removal Criteria
Reject Criteria
k: Techniques to Improve Navigation Performance
4. AZ-81O Air Data System
A. DADC Functions
B. Altitude Preselect Operation
C. Angle of Attack (AOA) Operation
D. DADC Red X Failures
5. AA-300 Radio Altimeter System
A. Preflight Test
B. In-Flight Test
6. EDZ-884 Electronic Display System (EDS)
A. Trend and Limit Monitoring
B. Troubleshooting Display Unit Red “X’’ing
7. DFZ-820 Flight Guidance System
A. List of Flow Chart Figures
B. List of Tables
8. PRIMUS@ 870 Weather Radar System
9. FMZ-800 Flight Management System (FMS)
A. Airborne Logic
B. Runway Alignment
Estimated Time Enroute
k: Descent Time and Fuel Predictions
Paqe
301
301
301
301
401
401
401
402
402
402
402
403
413
413
413
422
422
425
425
425
426
426
438
439
439
439
460
461
461
461
462
463
22-14-00
Page TC-4
Apr 15/93
Use or disclosure of information on this page is subject to the restrictions on the title page of this document,

Section
5
TABLE OF CONTENTS (cent)
Subheading
VOLUME III
Fault Isolation (cent)
9. E. Stored Flight Plan Waypoints
Takeoff Vspeeds
:: V1 Selection
H. Speed/Altitude Entries
Wind/Temperature Model
:: Temperature Envelope
K. Autothrottle Disengages
Takeoff and Landing Weight
Fl: Level Off at 10,000 Feet for Airspeed Control
in G-IV Phase 11 Aircraft
N. CDU Blanking
o. Fuel Used
Flight Plan Collapse
~: EPR Bugs on Approach
Victor Airways
s: Data Loader Fault Codes
10. Engine Pressure Ratio Transmitter
Interconnects
System Schematics
Removal/Reinstallationand Ad.iustment
L
3.
4.
5.
6.
;:
9.
General
Equipment and Materials
Procedure for DU-880 Display Unit
Procedure for WC-810/874 Weather Radar Controller,
GP-820 Flight Guidance Controller, PC-880 Turn Pitch
Controller, DC-884 Display Controller, CD-81O Control
Display Unit, DL-800/900 Data Loader, or DP-884 Dimmer
Panel
Procedure for AZ-81O Digital Air Data Computer, FZ-820
Flight Guidance Computer, SG-884 Symbol Generator,
FC-880 Fault Warning Computer, DA-884 Data Acquisition
Unit, or PZ-800 Performance Computer
Procedure for RT-300 Radio Altimeter Receiver
Transmitter
Procedure for AT-222 Radio Altimeter Antennas
Procedure for WR-800 Weather Radar Receiver Transmitter
Procedure for WA-800 Weather Radar Antenna and FP-900
24-Inch Radiator Plate
10. Procedure for WU-870 Antenna and Receiver Transmitter
Unit
11. Procedure for SM-600 Dual Servo, TM-260 Dual Trim
Servo and Brackets, and SM-81O Servo
464
464
465
465
465
467
467
467
468
468
469
469
469
469
470
471
501
601
701
701
701
701
702
703
703
704
704
706
710
713
22-14-00
Page TC-5
Apr 15/93
Use or disclosure of informationon this page is subject to the restrictions on the title page of this document.