Honeywell 1553 - Manual

Honeywell 1553

Honeywell 1553 – Manual, read for free online in PDF format. We hope this helps you resolve any issues you may have. If you have further questions, please contact us through the contact form.

1 Page 1
2 Page 2
3 Page 3
4 Page 4
5 Page 5
6 Page 6
7 Page 7
8 Page 8
9 Page 9
10 Page 10
11 Page 11
12 Page 12
13 Page 13
14 Page 14
15 Page 15
16 Page 16
17 Page 17
18 Page 18
19 Page 19
20 Page 20
21 Page 21
22 Page 22
23 Page 23
24 Page 24
25 Page 25
26 Page 26
27 Page 27
28 Page 28
29 Page 29
30 Page 30
31 Page 31
32 Page 32
33 Page 33
34 Page 34
35 Page 35
36 Page 36
37 Page 37
38 Page 38
39 Page 39
40 Page 40
41 Page 41
42 Page 42
43 Page 43
44 Page 44
45 Page 45
46 Page 46
47 Page 47
48 Page 48
49 Page 49
50 Page 50
51 Page 51
52 Page 52
53 Page 53
54 Page 54
55 Page 55
56 Page 56
57 Page 57
58 Page 58
59 Page 59
60 Page 60
61 Page 61
62 Page 62
63 Page 63
64 Page 64
65 Page 65
66 Page 66
67 Page 67
68 Page 68
69 Page 69
70 Page 70
71 Page 71
72 Page 72
73 Page 73
74 Page 74
75 Page 75
76 Page 76
77 Page 77
78 Page 78
79 Page 79
80 Page 80
81 Page 81
82 Page 82
83 Page 83
84 Page 84
85 Page 85
86 Page 86
87 Page 87
88 Page 88
89 Page 89
90 Page 90
91 Page 91
92 Page 92
93 Page 93
94 Page 94
95 Page 95
96 Page 96
97 Page 97
98 Page 98
99 Page 99
100 Page 100
101 Page 101
102 Page 102
103 Page 103
104 Page 104
105 Page 105
106 Page 106
107 Page 107
108 Page 108
109 Page 109
110 Page 110
111 Page 111
112 Page 112
113 Page 113
114 Page 114
115 Page 115
116 Page 116
117 Page 117
118 Page 118
119 Page 119
120 Page 120
121 Page 121
122 Page 122
123 Page 123
124 Page 124
125 Page 125
126 Page 126
127 Page 127
128 Page 128
129 Page 129
130 Page 130
131 Page 131
132 Page 132
133 Page 133
134 Page 134
135 Page 135
136 Page 136
137 Page 137
138 Page 138
139 Page 139
140 Page 140
141 Page 141
142 Page 142
143 Page 143
144 Page 144
145 Page 145
146 Page 146
147 Page 147
148 Page 148
149 Page 149
150 Page 150
151 Page 151
152 Page 152
153 Page 153
154 Page 154
155 Page 155
156 Page 156
157 Page 157
158 Page 158
159 Page 159
160 Page 160
161 Page 161
162 Page 162
163 Page 163
164 Page 164
165 Page 165
166 Page 166
167 Page 167
168 Page 168
169 Page 169
170 Page 170
171 Page 171
172 Page 172
173 Page 173
174 Page 174
175 Page 175
176 Page 176
177 Page 177
178 Page 178
179 Page 179
180 Page 180
181 Page 181
182 Page 182
183 Page 183
184 Page 184
185 Page 185
186 Page 186
187 Page 187
188 Page 188
189 Page 189
190 Page 190
191 Page 191
192 Page 192
193 Page 193
194 Page 194
195 Page 195
196 Page 196
197 Page 197
198 Page 198
199 Page 199
200 Page 200
201 Page 201
202 Page 202
203 Page 203
204 Page 204
205 Page 205
206 Page 206
207 Page 207
208 Page 208
209 Page 209
210 Page 210
211 Page 211
212 Page 212
213 Page 213
214 Page 214
215 Page 215
216 Page 216
217 Page 217
218 Page 218
219 Page 219
220 Page 220
221 Page 221
222 Page 222
223 Page 223
224 Page 224
225 Page 225
226 Page 226
227 Page 227
228 Page 228
229 Page 229
230 Page 230
231 Page 231
232 Page 232
233 Page 233
234 Page 234
235 Page 235
236 Page 236
237 Page 237
238 Page 238
239 Page 239
240 Page 240
241 Page 241
242 Page 242
243 Page 243
244 Page 244
245 Page 245
246 Page 246
247 Page 247
248 Page 248
249 Page 249
250 Page 250
251 Page 251
252 Page 252
253 Page 253
254 Page 254
255 Page 255
256 Page 256
257 Page 257
258 Page 258
259 Page 259
260 Page 260
261 Page 261
262 Page 262
263 Page 263
264 Page 264
265 Page 265
266 Page 266
267 Page 267
268 Page 268
269 Page 269
270 Page 270
271 Page 271
272 Page 272
273 Page 273
274 Page 274
275 Page 275
276 Page 276
277 Page 277
278 Page 278
279 Page 279
280 Page 280
281 Page 281
282 Page 282
283 Page 283
284 Page 284
285 Page 285
286 Page 286
287 Page 287
288 Page 288
289 Page 289
290 Page 290
291 Page 291
292 Page 292
293 Page 293
294 Page 294
295 Page 295
296 Page 296
297 Page 297
298 Page 298
299 Page 299
300 Page 300
301 Page 301
302 Page 302
303 Page 303
304 Page 304
305 Page 305
306 Page 306
307 Page 307
308 Page 308
309 Page 309
310 Page 310
311 Page 311
312 Page 312
313 Page 313
314 Page 314
315 Page 315
316 Page 316
317 Page 317
318 Page 318
319 Page 319
320 Page 320
321 Page 321
322 Page 322
323 Page 323
324 Page 324
325 Page 325
326 Page 326
Page: / 326

Table of Contents:

  • Page 2 – Proprietary notice on title page applies; SHEET; Copyright
  • Page 3 – REVISION STATUS OF SHEETS INDEX; REVISIONS
  • Page 4 – THIS PAGE INTENTIONALLY LEFT BLANK
  • Page 5 – SHEET 5; TABLE OF CONTENTS
  • Page 6 – SHEET 6
  • Page 7 – SHEET 7
  • Page 8 – SHEET 8
  • Page 9 – SHEET 9
  • Page 11 – SECTION I
  • Page 12 – SECTION I – GENERAL INFORMATION
  • Page 13 – How To Us e This Document
  • Page 14 – Reference D o cuments
  • Page 15 – Description of Equipment
  • Page 16 – Sensor Systems
  • Page 17 – FIGURE 1-1 MK VI/MK VIII EGPWS SMART CABLE
  • Page 18 – Technical C h aracteristics; Configuration Module
  • Page 19 – Installation Kits and Accessories
  • Page 20 – Accessorie s not Supplied
  • Page 22 – STACO; STACO
  • Page 23 – TERR DISPLAY
  • Page 24 – Tools Requ i red
  • Page 25 – License Re q uirements
  • Page 27 – SECTION II
  • Page 28 – SECTION II - INSTALLATION
  • Page 29 – NOTE; Unpacking a nd Inspecting the Equipment
  • Page 31 – Configurati o n Module Installation
  • Page 32 – CONFIGURATION MODULE ASSEMBLY
  • Page 33 – INSTALLATION ASSEMBLY SEQUENCE
  • Page 34 – MK VI/MK VIII EGPWS CONFIGURATION MODULE
  • Page 40 – Cable Length
  • Page 41 – Glideslope Canceled
  • Page 42 – TERRAIN inhibit
  • Page 43 – TERR FAIL; PULLUP; The above picture is an example of lamp location and
  • Page 45 – MK VI/MK VIII EGPWS MOUNTING TRAY
  • Page 47 – SECTION III
  • Page 48 – SECTION III – SYSTEM PLANNING
  • Page 51 – Appendix E Section 5.2 groups; System Wir i ng/ Electrical Interfaces; Pin
  • Page 52 – Section 7
  • Page 53 – Output discretes are intended to operate with +28
  • Page 54 – Appendix E
  • Page 56 – Table
  • Page 57 – Category 2 – Air Data Input Select
  • Page 59 – EGPWS MK VI / MK VIII; Vendor Model
  • Page 61 – Vendor PN
  • Page 62 – Air Data Input Select
  • Page 63 – Category 3 – Position Input Select
  • Page 65 – GND
  • Page 66 – Lo; Position
  • Page 67 – Category 4 – Altitude Callouts
  • Page 68 – Category 5 – Audio Menu Select; registered aircraft are required to use Alternate Audio Menu.
  • Page 69 – Category 6 – Terrain Display Select; availability
  • Page 70 – Terrain Dis p lay Configuration Group; Display Input Control Group; Fault Designation: DISPLAY BUS 1
  • Page 71 – Channel; Appendix E Table
  • Page 72 – oneyw; RR; EGPW; connecti
  • Page 73 – Hon; TERR INHIB; No co
  • Page 74 – IN; EG
  • Page 75 – CH DS
  • Page 76 – Integr
  • Page 78 – Honeywell
  • Page 79 – Ho
  • Page 82 – ckwe
  • Page 83 – Co
  • Page 87 – Unive
  • Page 88 – Category 7 – Options Select Group #1
  • Page 90 – Using Appendix E
  • Page 91 – Category 8 – Radio Altitude Input Select; Radio Altitude; Radio Altimeter Indicator; DH out
  • Page 94 – Category 9 – Navigation Inputs Select
  • Page 95 – ILS Receiver; Backcourse
  • Page 98 – Category 1 0 – Attitude Input Select; Vertical Gyro; Roll Synchro; EGPWS MK
  • Page 100 – Category 1 1 – Heading Input Select; Directional Gyro; Heading Synchro; Heading; 6 VAC Reference; Heading Ref; Mag Hdg Validity
  • Page 102 – Category 1 2 – Windshear Input Select; Category 12 defines the Windshear interface.
  • Page 103 – Category 1 3 – Input / Output Discrete Type Select; False
  • Page 108 – On ground self-test is inhibited if Steep Approach is
  • Page 109 – Output discretes are intended to
  • Page 111 – GPWS
  • Page 112 – Display; FIGURE 3.15-2 Example of Terrain Display Interface; Figure 3.15-3 Example of Terrain Display switch with relay
  • Page 113 – Category 1 4 – Audio Output Level
  • Page 114 – Category 1 5 - 17 – Undefined Input Selects
  • Page 115 – SECTION IV
  • Page 116 – SECTION IV – CONFIGURATION MODULE PROGRAMMING AND
  • Page 117 – SECTION IV – Config Module Programming And Regional TDB Loading; Harness Ch e ckout and Power Check
  • Page 119 – Configurati o n Module Programming
  • Page 120 – Configuration update failed, please try again
  • Page 121 – CONFIGURATION MODULE:
  • Page 122 – Configurati o n Module Reprogramming
  • Page 125 – Verification of the Terrain Database Version
  • Page 126 – SYSTEM CONFIGURATION
  • Page 127 – SECTION V
  • Page 128 – SECTION V – CERTIFICATION; Certificatio n Procedure
  • Page 129 – Use the Event Marker, F9 key, to identify events during tests.
  • Page 130 – SECTION VI
  • Page 131 – SECTION VI - MK VI GPWS to MK VI/VIII EGPWS Signal Mapping; Connector Pin-Out Sorted By Pin Number (USE FOR REFERENCE ONLY)
  • Page 134 – NEW CONNECTOR
  • Page 137 – APPENDIX A - Customer Worksheet
  • Page 139 – MK VI / MK VIII EGPWS; ENHANCED GROUND PROXIMITY WARNING SYSTEM; CUSTOMER INTERFACE WORK SHEET; DATE:; Interface; CURRENT GPWS INSTALLATION:; SYSTEM
  • Page 140 – AIRCRAFT SYSTEMS INFORMATION:; DG; MSL
  • Page 141 – APPENDIX B - Sample Wiring Diagrams
  • Page 145 – APPENDIX C
  • Page 146 – APPENDIX C – WinVIEWS Operation Instructions; RS-232 COMMUNICATION WITH THE EGPWS
  • Page 147 – Windows Virtual Interface to the Enhanced Warning System; Normal Operation for Ground Testing the EGPWS:
  • Page 148 – The format for the WinVIEWS command file is:
  • Page 149 – APPENDIX D
  • Page 150 – APPENDIX D - Vendor Contact Information
  • Page 152 – West Coast Specialties
  • Page 153 – APPENDIX E
  • Page 154 – Table of Contents; APPENDIX E - INTERFACE DESCRIPTION DOCUMENT
  • Page 155 – AIRCRAFT APPLICATION DATA
  • Page 156 – Discrete Word (273) – Bendix Weather Radar Vertical Profile Mode
  • Page 157 – OUTPUT DATA DEFINITION
  • Page 158 – CONNECTOR INTERFACE
  • Page 159 – APPENDIX E - Interface Description Document
  • Page 160 – MECHANICAL; Amp Part Number
  • Page 161 – and
  • Page 164 – ELECTRICAL; The heater blanket turns on at temperatures
  • Page 165 – Localizer Deviation or Low Level Glideslope Validity
  • Page 170 – +28 VDC Discrete Characteristics; Output to Config Module; INTERFACE OF EGPWS OUTPUTS TO CONFIGURATION MODULE
  • Page 171 – Output
  • Page 172 – Front Panel Test Interface
  • Page 173 – Front Panel Status Indicators
  • Page 174 – AIRCRAFT APPLICATION DATA
  • Page 175 – Table 5.2: Category ID Selection Procedure; Signal Selection; Ident No
  • Page 177 – Selection Tables
  • Page 179 – Description
  • Page 180 – Temperature Probe only.; Configuration Data; Derive Baro Altitude Rate
  • Page 195 – ALERT/WARNING CONDITION
  • Page 198 – Configuration
  • Page 200 – KC Picture Bus
  • Page 201 – No Display, TAD and TCF enabled
  • Page 202 – Display Configuration Group 6; Display Input Control Group 1
  • Page 203 – Display Configuration Group 1
  • Page 204 – Collins ProLine II, 5x6
  • Page 205 – Display Configuration Group 3
  • Page 206 – Display Configuration Group 4; Display Input Control Group 2
  • Page 207 – Display Configuration Group 5
  • Page 208 – Display Configuration Group 7
  • Page 209 – Display Configuration Group 8; Software Level 14 required for integrated display and popup.
  • Page 210 – Display Configuration Group 9
  • Page 211 – Display Configuration Group 10
  • Page 212 – Display Configuration Group 11; Display Input Control Group 3
  • Page 213 – Display Configuration Group 12
  • Page 214 – Display Configuration Group 13
  • Page 215 – KC Picture Bus without presentation of Geometric Altitude
  • Page 216 – KC Picture Bus with Soft Keys
  • Page 218 – Display Configuration Group 2; Display Input Control Group 244
  • Page 219 – Display Configuration Group 241
  • Page 220 – Honeywell Primus 1000 with binary Peaks Elevations and Cyan; Display Input Control Group 248
  • Page 221 – Honeywell Primus 1000 with binary Peaks Elevations
  • Page 222 – MK VIII Only; Display Input Control Group 253
  • Page 223 – Collins Pro Line 21 (Integrated) with overlay Peaks Elevations
  • Page 225 – dual SCI range
  • Page 226 – Display Input Control Group 249
  • Page 228 – If all the conditions indicated for the amber “TERR” above are FALSE.
  • Page 229 – Honeywell/Bendix EFIS 10, EFS 86 Radar system; Display Input Control Group 246
  • Page 230 – Collins FDS 255/2000 with selection controlled by the EGPWS
  • Page 232 – Peaks Elevations; Display Input Control Group 250
  • Page 233 – If bit 17 = 1 then display white “TERRAIN OFF” message on PFD and MFD.
  • Page 234 – Honeywell Primus EPIC CDS/R, with binary Peaks Elevations
  • Page 238 – Collins FDS 255/2000 with selection controlled by the display
  • Page 240 – Honeywell SPZ8000 older style; Display Input Control Group 255
  • Page 244 – In this category, only the following signals are defined:
  • Page 249 – KN40 Nav Source
  • Page 254 – compatible with Inertial Vertical Speed.
  • Page 257 – In this category, only the following signals are to be defined:
  • Page 259 – Lamp Format
  • Page 270 – CONFIGURABLE INPUT DATA DEFINITION; Data Item
  • Page 276 – 7 ARINC 547 Localizer Deviation with Discrete Valid; Transmission System Interconnect.
  • Page 277 – DISCRETE DATA
  • Page 278 – UNCORRECTED BAROMETRIC ALTITUDE
  • Page 280 – SENSOR STATUS – GPS
  • Page 281 – CONTROL WORD – MFD
  • Page 282 – DISCRETE WORD – MFD
  • Page 283 – RANGE – MG
  • Page 284 – KEY PRESS DATA; Source: KCPB Display; CONTROL WORD 1 – WXR
  • Page 285 – Discrete Word
  • Page 288 – LONGITUDINAL ACCELERATION
  • Page 289 – DISCRETE WORD – FWC & GP
  • Page 290 – Body Pitch Rate
  • Page 292 – STATIC AIR TEMPERATURE
  • Page 297 – Inputs; The Level 6 audio information specifies the voice issued when; Analog Radio Altitude Validity Flags
  • Page 301 – 2 Barometric Altitude Validity Discrete
  • Page 303 – OUTPUT DATA DEFINITION; inputs to display systems and flight recorders.
  • Page 312 – NOTE: Text code for degree sign is non-standard ASCII for 40
  • Page 313 – Provides equipment identification for maintenance reporting.
  • Page 316 – INOP & Warning Annunciation in Same
  • Page 317 – System Configuration Status; Glideslope Inhibit input discrete activated
  • Page 318 – System Level Event; Latitude Invalid
  • Page 319 – CONNECTOR; Terrain Awareness and TCF Inhibit Discrete (Ground)
  • Page 324 – DEFINITIONS; Acronym
Loading the manual

Proprietary notice on title page applies

CAGE CODE: 97896

SCALE: NONE

SIZE: A

DWG NO: 060-4314-150

REV:

SHEET

1 OF

326

Airlines & Avionics Products
Honeywell Inc.
15001 N.E. 36th Street
Redmond, WA 98052

MK VI
MK VIII

Enhanced Ground Proximity Warning System

(Class A TAWS)

Installation Design Guide

Hardware/Software Part Numbers:

965-1180-020
965-1190-020
965-1210-020
965-1220-020

Release Date: July 14, 2003

"Loading the manual" means you need to wait until the file loads and becomes available for online reading. Some manuals are very large, and the time they take to appear depends on your internet speed.

Other Manuals for Honeywell 1553

Summary

Page 2 - Proprietary notice on title page applies; SHEET; Copyright

Honeywell MK VI MK VIII EGPWS Installation Design Guide Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 2 Copyright  2003 Honeywell, Inc. All rights reserved. This document and all information and expression contained herein are the prop...

Page 3 - REVISION STATUS OF SHEETS INDEX; REVISIONS

Honeywell MK VI MK VIII EGPWS Installation Design Guide Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 3 Typed names constitute approval signatures. Actual signatures are on file at Honeywell in Redmond, WA. DRAWN Larry Matter 14-JULY-03...

Page 4 - THIS PAGE INTENTIONALLY LEFT BLANK

Honeywell MK VI MK VIII EGPWS Installation Design Guide Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 4 THIS PAGE INTENTIONALLY LEFT BLANK

Other Honeywell Models