Honeywell SPZ-8000 Maintenance Manual page 20

Digital automatic flight control system for gulfstream iv
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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/Reinstallation and 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.

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