- Sperry Marine Navipilot 4000 User Manual
- Sperry Marine Naviknot Manual
- Sperry Marine Navipilot 4000
NORTHROP GRUMMAN • Online, all the time with Mobile Packet Data Service (MPDS) • Miui-M Voice • Global Voice Distress • Single-channel system • Simple installation because of • Compact, convenient, cost- • Global coverage, 78° north to Global Maritime Connectivity Sperry Marine The Sperry Marine NaviCom F 77 maritime communications terminal offers high-speed and cost-effective voice and data communication based on either the MPDS (Mobile Packet Data Service) protocol with constant online access or a 64 kbps ISDN With MPDS you are only charged for the amount of data sent, not for the time the channel remains open, making it the most economic and convenient solution for e- mail, small- and medium-size transfer, LANs, VPNs and Internet. ISDN services provide a high-capacity channel with a constant data stream and are usually preferable for uploading or downloading large files. The tracking antenna is 880 mm high, has a diameter of just 840 mm and weighs only 27 kg. It is line replaceable and features a bottom hatch for easy service and maintenance access. The antenna can be placed up to 70 meters from the transceiver. The NaviCom F 77 transceiver provides a constant two-way link to Inmarsat satellites offering Inmarsat Fleet MPDS accompanied by user-friendly software, which enables simple configuration from a The Sperry Marine NaviCom F 77 transceiver and antenna provide the hub for online communication all the time via desktop phones, payphones, DECT phones Connected to an IP router, the NaviCom F 77 terminal can integrate the vessel 24 hours a day with onshore management systems via the Web, including e-mail and Internet services. The NaviCom F 77 operates through the established network of Inmarsat and GPS satellites with interconnection to the international fax and packet switched data networks, offering fast and reliable transfer
Sperry Autopilot Manual Spz 400. Home Sperry Marine Navipilot 4000 Manual Sperry Marine Navipilot 4000 Manual Sperry NaviPilot 4000 Autopilot Series If searched for a book Sperry autopilot navipilot 4000 user manual in pdf format, then you have come on to the right site. We present the full option of this ebook in DjVu, ePub, txt, doc, PDF formats. Installation manual Sperry Autopilot Navipilot 4000 User Manual. Navipilot 4000 installation manual Sperry Marine Navipilot 4000 - WNL Marine Electronics B.V Sperry Marine Navipilot 4000. The installation is made far more simple and fast. Manual Manual cooler Download Sperry navipilot 4000 installation manual.pdf Download Kawasaki 1100 zxi jet. With the introduction of theNAVIPILOT 4000 Self-Tuning Adaptive Heading Control System, Sperry Marine continues its traditional philosophy of designing autopilots with the aim of increasing profit by reducing running costs. The innovative NAVIPILOT 4000 is the first. Necessity to load Sperry navipilot 4000 installation manual pdf, then you've come to the faithful site. We own Sperry navipilot 4000 installation manual PDF, txt, doc, ePub, DjVu forms. We will be pleased if you come back us again. Sperry NaviPilot 4000 Autopilot Series. Sperry Marine s expanded NAVIPILOT 4000 Series of self-tuning adaptive.
Sperry Marine Navipilot 4000 User Manual
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Sperry Marine Naviknot Manual
Sperry Marine Navipilot 4000
TM 1-1510-218-10 3C-46 (3) Program Mode. The preset channels and frequencies are set using the program mode. Pressing and holding the CHAN switch for 2 seconds will place the unit into the program mode. A –P- and a channel number will be shown in the active display, and a frequency or dashes will be shown in the standby display. Immediately after entering the program mode the channel number will begin to flash, indicating that rotating the tuning knobs will change the channel number. Momentarily pressing the transfer switch will cause the channel number to stop flashing and cause the frequency to begin flashing, indicating that rotating the tuning knobs will change the frequency. Momentarily pressing the CHAN switch will return the unit to the frequency mode. The standby frequency will return to what it was prior to entering the program mode. The unit will automatically return to the frequency mode if no front panel activity takes place for 20 seconds. d. Modes of Operation.The ADF receiver mode of operation is selected by a momentary push button switch placarded MODE. The operating mode changes from ADF to ANT to ADF/BFO to ANT/BFOwith each press of the mode switch. (1) Antenna Mode (ANT). When the ADF receiver is in the ANT mode, audio will be present in the speaker or headphone (if the respective number 1 or 2 ADF receiver audio switch is on), and the RMI indicator needle that is being used will be parked at the 90° relative position. (2) Automatic Direction Finder (ADF) Mode. When the ADF receiver is in the ADF mode of operation, the RMI needle or HSI bearing pointer that is being used will indicate the relative bearing to the station. (3) Beat Frequency Oscillator (BFO) Mode. The BFO is used to hear audio when the tuned station is a keyed continuous wave (CW) station. The BFO may be used either in the ANT or ADF mode. e. ADF Receiver Control Unit (KFS-564A) Operation.(1) Turn On Procedure. 1. Avionics Master Switch (overhead control panel, Figure 2-15) – ON. 2. OFF / VOL / PUSH Knob – Turn clockwise out of detent, then press to turn off automatic squelch circuit. Continue turning knob clockwise until background noise is heard in headphones or speaker, ensuring that the receiver is operating, then set audio volume to desired level. Press knob again to return unit to automatic squelch control. (2) ADF Operating Procedure. 1. Number 1 or Number 2 ADF Receiver Audio Monitor Switch (audio control panel, Figure 3C-1) – ON. 2. Mode Switch – Set operating mode as required. 3. Tuning Knobs – Set desired frequency or channel. 4. VOL Control – As required. 5. RMI Switch – As required. 3C-24. AUTOMATIC FLIGHT CONTROL SYSTEM (SPZ-4000). a. Description.The automatic flight control system is an integrated autopilot/flight director/air data system. When the autopilot is engaged and coupled to the commands of the flight director, the flight control system will control the aircraft using the same commands which are displayed on the attitude director indicator by the flight director command cue. When the autopilot is engaged and uncoupled from the flight director commands, manual pitch and roll commands may be inserted using the Touch Control Steering (TCS) on the control wheels or the pitch wheel and turn knob on the autopilot control panel. When the autopilot is coupled, the flight director command cue indications on the attitude director indicator provide a means of monitoring the performance of the autopilot. When the autopilot is not engaged, the same modes of operation are available for flight director only. The pilot maneuvers the aircraft to satisfy the flight director commands, as does the autopilot when it is engaged. b. Air Data Computer.A digital air data computer located in the forward avionics compartment provides the altitude information for the pilot's altimeter, altitude alerter, and transponder. The computer also provides altitude and airspeed hold function data to the flight control computers. The air data computer is powered through a 2-ampere circuit breaker, placarded AIR DATAENCODER, on the overhead circuit breaker panel, Figure 2-16. All air
