Tittel: | SPZ-700 AP/FD INSTRUMENT SYSTEM MAINTENANCE MANUAL FOR De HAVILLAND DHC-7 ATA 22-13-00 : (SKOLEBOK) Type AD-300D Attitude Director Indicator: Component, Maintenace Manual with illustrated parts list |
Materialtype: | Manual/Sivil |
Signatur: | 22-D-5 |
Utgitt: | Phoenix, Arizona : SPERRY FLIGHT SYSTEMS AVIONICS DIVISION, 1985 |
Klassenummer: | Perm |
Serie: | PUB. NO. ; 15-1146-04 |
Emneord: | Autopilot / Flight Director / Maintenance / Manual / SPZ-700 |
Materialbetegnelse: | Perm |
Note: | Published 1 September 1977, Revised 15 February 1985
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Innhold: | TABLE OF CONTENTS: Section 14 comes before the general contents in this issue Section 1: Description and Operation: 1. General 2. Functional Description 3. System Modes of Operation 4. System Performance/Operating Limits 5. Interface Data Section 2: Component Description: 1. General 2. Indicators: 2.A. Barometric Altitude Indicator 2.B. HZ-444/HZ-454 Attitude Director Indicator 2.C. RD-445 Horizontal Situation Indicator 2.D. Rh-445 Radio Magnetic Indicator 2.E. RD-500/RD-500A Horizontal Situation Indicator 2.F. RA-215/RA-315 Radio Altimeter Indicator 3. Selectors and Controller: 3.A. Autopilot Controller 3.B. Mode Selector 3.C. Altitude Alert Controller 3.D. Instrument Remote Controller (Optional Equipment) 3.E. CM-200 Comparator Monitor (Optional Equipment) 4. Sensors: 4.A. Accelerometer 4.B. VG-14 or VG-14A Vertical Gyro 4.C. C-14A Directional Gyro, Cs-412 Dual Remote Compensator, and FX-220 Flux Valve 4.D. AT-221 Antenna and R/T-221 Receiver/Transmitter 5. Computers: 5.A. Air Data Computer 5.B. Autopilot Computer 5.C. Flight Director Computer 6. Servos and Actuators: 6.A. Servo Drive and Bracket 6.B. Trim Servo Motor and Drive Assembly 6.C. Trim Servo Sprocket and Bracket 6.D. Linear Actuator Section 3: Ground Check (To be supplied) Section 4: Troubleshooting 1. General 2. Troubleshooting Section 5: Reinstallation and Adjustment: 1. General 2. Equipment and Materials 3. Procedure: 3.A. Autopilot Computer 3.B. Autopilot Controller 3.C. Mode Selector 3.D. HZ-444 or HZ-454 Attitude Director Indicator 3.E. Air Data Computer 3.F. Barometric Altitude Indicator 3.G. C14A Gyrosyn Compass 3.H. Dual Remot Compensator 3.I. Flux Valve 3.J. Flight Director Computer 3.K. RH-445 Radio Magnetic Indicator 3.L. RA-215 or RA-315 Radio Altimeter Indicator 3.M. RD-445 Horizontal Situation Indicator 3.N. RD-500 or RD-500A Horizontal Situation Indicator (Optional Equipment) 3.O. R/T-221 Receiver/Transmitter 3.P. Drum and Bracket Assembly 3.Q. Servo Drive Assembly 3.R. VG-14 or VG-14A Vertical Gyro 3.S. AT-221 Antenna 3.T. Linear Actuator 3.U. Altitude Alert Controller 3.V. Trim Servo Sprocket and Bracket Assembly 3.W. Trim Servo Drive Assembly 3.X. Accelerometer 3.Y Instrument Remote Controller (Optional Equipment) 3. CM-200 Comparator Monitor (Optional Equipment) Section 6: Shipping and Storage Instructions |
Eier: | Norsk Luftfartsmuseum |
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