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The unit is 9. The general maintenance concept is organizational to depot level, with limited intermediate level support. Though not the primary means of navigation, the 12DS payload will also be used to assist the Pioneer IP and MC in identifying landmarks to aid in navigation and target identification.
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Ready For Operational Use Schedule. No new training pipelines or tracks are required by this NTSP. China smartphones online shopping Training course modifications will not affect track length or student throughput. Installation and Delivery Schedules. Curriculum will be modified to include basic functional and physical descriptions of the 12DS payload, in addition to preventive and organizational level corrective maintenance, remove and replace procedures, and any required calibration or alignment procedures.
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GPWS computers are programmable to accept multiple input from existing aircraft systems. Strategic or tactically vital data may be obtained cost-effectively by exploiting the UAV's low radar cross-section, low IR signature, and remote control versatility. The GPWS units are completely automatic.
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The stations are manned as required during operational and training missions. OT was terminated in October Peculiar Support Equipment and special tools required to support peculiar and unique maintenance requirements are controlled through the Navy Individual Material Readiness List system. MIAG is a microprocessor based, inertial navigation avionics suite used to fly the Pioneer air vehicle. Additionally, the shipboard TCU contains extra equipment required to operate two remote antennae. Estimated impact of the integration of 12DS training into current Pioneer curriculum is as follows:. The MC course will require additional curriculum to provide overview of the UCARS functional and physical descriptions and operational concepts.
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16.02.2018 - In Stock Item ships from Zoro warehouses and will ship within 1 business day. Our content is added by our users. The pedestal unit is a two-axis gimbal system with a high gain inch parabolic dish, tracking antenna mounted to its gimbal. The station calculates the platform pitch and yaw compensation command. The launching system operates a pneumatic turbine, which draws in a nylon strap onto a rotating drum.
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04.02.2018 - Curriculum will include physical and functional descriptions; set-up, alignment, and calibration; fault isolation procedures; and preventive and corrective maintenance. In either case, the Pioneer UAV System consists of three ground elements and one airborne element, as functionally described above. Maintenance personnel perform preflight, launch, recovery, and postflight evolutions e. It analyzes this data to detect a flight path, which will result in an unsafe proximity to the ground. The engine is installed in a pusher configuration, using a 29 inch diameter laminated wood propeller. The SPARS net recovery system is used for shipboard operations, where conventional recovery methods are impossible.
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15.03.2018 - New Features, Configurations, or Material. Once it has located the UAV and begins tracking, the antenna points directly at the UAV and follows it precisely by measuring the four lobe signal strengths. In Stock Item ships from Zoro warehouses and will ship within 1 business day. The engine is installed in a pusher configuration, using a 29 inch diameter laminated wood propeller.
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Additionally, standard shipping rates will apply for all orders to Alaska and Hawaii. Any charges incurred for hazardous materials or other special handling by the carrier must be paid by the customer.
Fuel surcharges may be applied. MTIP is a training management tool that, through diagnostic testing, identifies individual training. MTIP is the comprehensive testing of one's knowledge.
It consists of a bank of test questions managed through automated data processing. MTIP will allow increased effectiveness in the application of training resources through identification of skills and knowledge deficiencies at the activity, work center, or individual technician level.
Remedial training will be concentrated where needed to combat identified skill and knowledge shortfalls. Aviation Maintenance In-Service Training. However, it is structured very differently, and will function as an integral part of the new Aviation Maintenance Training Continuum System AMTCS that will replace the existing aviation maintenance training structure.
AMIST will provide standardized instruction to bridge the training gaps between initial and career training. With the implementation of AMIST, the technician will be provided the training required to maintain a level of proficiency necessary to effectively perform the required tasks to reflect a career progression.
Aviation Maintenance Training Continuum System. The application and adoption of recent advances in computer hardware and software technology have enabled CBT with its basic elements of Computer Managed Instruction, Computer Aided Instruction, and Interactive Courseware to be integrated into the training continuum and provide essential support for standardizing technical training.
It is a performance-based, standardized, level-progressive, documentable, training management and evaluation program. It identifies and prioritizes task inventories by MOS through a front-end analysis process that identifies task, skill, and knowledge requirements of each MOS.
Test Sets, Tools, and Test Equipment. As a result of the Human Systems Integration testing during OT it was recommended that the light panel be removed in the final configuration.
Schedule of Events a. Installation and Delivery Schedules. Ready For Operational Use Schedule. Time Required to Install at Operational Sites. Specific activity schedules are shown in element IV.
Annual Incremental and Cumulative Billets. Existing training activity instructor and support personnel billet levels are adequate to support GPWS training. No additional billets are required.
Student billets are chargeable to the type aircraft for which the student receives overall training. The currently planned chargeable student billets will not change due to the GPWS.
They are contained in the specific aircraft NTSP. Existing Training Phased Out Note: For information on student throughputs refer to: Allied Signal Avionics, Inc. Cubic Defense Systems, Inc.
Training Hardware Training Devices. Date required indicates the date when GPWS information will be incorporated into these manuals. Refresher training is concentrated where needed to improve identified skill and knowledge shortfalls.
Aviation Maintenance In-Service Training. However, it is structured very differently, and will function as an integral part of the new Aviation Maintenance Training Continuum System AMTCS that will replace the existing aviation maintenance training structure.
AMIST will provide standardized instruction to bridge the training gaps between initial and career training. With implementation of AMIST, technicians will be provided the training required to maintain a level of proficiency necessary to effectively perform the required tasks to reflect career progression.
AMIST will begin when funding becomes available. Aviation Maintenance Training Continuum System. The application and adoption of recent advances in computer hardware and software technology will enable CBT, with its basic elements of Computer Managed Instruction, Computer Aided Instruction, and Interactive Courseware, to be integrated into the training continuum and provide essential support for standardizing technical training.
It is a performance-based, standardized, level-progressive, documentable, training management and evaluation program. It identifies and prioritizes task inventories by MOS through a front-end analysis process that identifies task, skill, and knowledge requirements of each MOS.
The Pioneer was purchased off-the-shelf, conforming to a Milestone IIIA decision and categorized as a non-development item. The technical manuals listed below were used as a baseline for proposing changes associated with the ECPs described in Appendices A through C.
PUI will provide updates to these technical manuals on electronic media for later incorporation by the government. These changes will identify changes to the system description, theory of operation, operating procedures, menu descriptions, maintenance procedures, and illustrated parts breakdown areas of the Pioneer Technical Manuals.
New illustration files will be provided in a Windows Metafile Format WMF and delivered separately from the text files. Test Sets, Tools, and Test Equipment. Existing test equipment in the Navy and Marine Corps inventory will be used when applicable.
Peculiar Support Equipment and special tools required to support peculiar and unique maintenance requirements are controlled through the Navy Individual Material Readiness List system.
Initial supply support was provided by the contractor and included acquisition, distribution, provisioning, and inventory replenishment of system components, spares, repair parts, and consumable supplies necessary to maintain the Pioneer UAV in a high state of readiness.
Class IX - Repair Parts. Spare parts requirements are generated by the Pioneer Item Manager Code 3. Squadrons submit their repairable assets to the Navy Supply Support System.
Installation and Delivery Schedules. Ready For Operational Use Schedule. Time Required to Install at Operational Sites. The External Pilot Simulator has been delivered to all Pioneer activities.
All equipment utilized is Training Equipment, and is described in the TRPPM as equipment designed for operational purposes which is the subject of instruction, or which is used by the instructor or student as an element of the process of teaching or learning.
Training Equipment has, or had as its prime or initial purpose for existence some function other than that of training personnel. MIAG fielding is currently awaiting resolution of Pioneer system software issues and final testing.
MIAG is a microprocessor based, inertial navigation avionics suite used to fly the Pioneer air vehicle. The MIAG features dual 25 MHz processors and power supplies, and analog and digital interfaces to the air vehicle and payload control.
General purpose interface cards connect MIAG to the support hardware within the air vehicle. MIAG incorporates the functions of many of the existing Pioneer air vehicle electronic and electro-mechanical devices, and replaces several units which currently exhibit high failure rates, including the CPA, airspeed transducer unit, barometric pressure unit, and both the rate and vertical gyros.
Additionally, test features built into MIAG will reduce equipment fault isolation and repair times. The MIAG equipment design allows for easy installation without modification of the current air vehicle fuselage, and the elimination of certain support equipment will provide additional space for future utilization.
An increase in ground system and air vehicle performance is expected through MIAG's programmability and future expansion capability, and may achieve some performance gains through significant weight reduction.
MIAG replaces existing systems within the Pioneer air vehicle, allowing for space and weight reductions that can be put to other use. The unit is 9. There are nine connectors provided for interface with the air vehicle.
The MIAG is designed to consume a maximum of All courses will require addition of MIAG overview materials, but the Electronics Technician course will require additional changes to classroom and lab curriculum.
The estimated impact of the integration of MIAG training into current Pioneer curriculum is as follows:. Curriculum will be modified to include the functional and physical description of the MIAG, in addition to Pioneer avionics already taught.
Curriculum will be modified to include an overview of the functional and physical descriptions of MIAG, in addition to Pioneer avionics already taught. Curriculum will be modified to include an overview of the functional and physical descriptions of the MIAG, in addition to Pioneer avionics already taught.
Curriculum will be modified to include in-depth functional and physical descriptions of the MIAG, in addition to Pioneer avionics already taught. Classroom and lab training will include basic troubleshooting, remove and replace, and various calibration procedures.
Test Sets, Tools and Test Equipment. This equipment will support software updates, magnetometer calibrations, and support operations for monitoring the microprocessors within MIAG.
This support equipment will not be used during normal Pioneer mission operations. These schedules are not available, pending final corrections on software; expected delivery is fourth quarter FY Final Operational Testing for shore-based and shipboard operations is to be determined pending software availability.
UCARS is a microwave Ka-band system, capable of operating day or night, from land-based or ship-based recovery sites, and in a variety of weather conditions fog, rain, smoke, low clouds, bright sunlight, etc.
UCARS precisely tracks modified air vehicles through a two-element system comprised of an Airborne Subsystem, located entirely on the air vehicle, and a ground-based Track Subsystem TS. The Airborne Subsystem provides a point source beacon signal to aid in accurate position sensing, enabling the TS to detect and precisely track the air vehicle.
The Airborne Subsystem transmits and receives vertically polarized signals, via a combination Omni-directional horn antenna. The front side of the radome contains the higher gain directional horn antenna, which is used initially when the UAV is acquired by the TS.
When the UAV is feet from the intended touchdown point, a logic signal is transmitted, switching to the Omni-directional antenna for final approach, touchdown, and roll-out.
While transmitting, the receiver is disabled; while receiving, the transmitter is disabled. The allowable drift requires the TS to search in frequency to determine the exact Airborne Subsystem transmitter frequency.
Inside the transponder there are three circuit boards plus a RF front-end module. The circuit boards consist of an intermediate frequency board, a transponder controller board, and a power supply board.
A run-time delay calibration circuitry monitors all active Airborne Subsystem output signals on a real-time basis, which allows for the implementation of a sophisticated sequence of BIT to be performed to detect most Airborne Subsystem error conditions.
Between pulses, the Airborne Subsystem listens for interrogations by the TS, and upon determination that the TS is interrogating, the Airborne Subsystem enters the transponder mode, where it listens for TS interrogations and then replies providing TS tracking of the latest position.
The TS locates and precisely tracks a single selected UAV, relative to a desired Touchdown Point TDP, which may be a land-based runway or a shipboard recovery net system, using a directional, vertically polarized antenna.
These positional data, along with system status, are sent to the RS to perform air vehicle specific automatic control computations. The TS is comprised of the TCU; the pedestal group, which in addition to the pedestal unit provides mounting for the bore-sight camera unit and interrogator unit; and the TSAS.
The pedestal unit is a two-axis gimbal system with a high gain inch parabolic dish, tracking antenna mounted to its gimbal. The large vertical movement permits antenna stabilization in all sea states.
Once it has located the UAV and begins tracking, the antenna points directly at the UAV and follows it precisely by measuring the four lobe signal strengths. The interrogator unit is the TS RF transceiver; it provides the signal processing necessary to track the Airborne Subsystem.
The interrogator processes amplitude and range data, which it provides to the TS computer, and transmits the pulsed RF interrogation signal to the Airborne Subsystem transponder. The bore-sight camera is a charge-coupled device, color video camera with a fixed set for infinity focal length.
Track Subsystem Alignment Set, Unit 7. The TSAS provides a static, far-field point source for user on-site tracking-ranging bias and stability validation. The RS performs air vehicle specific guidance and control functions, interfaces with the UAV data link, provides man-machine interfaces to control the Airborne Subsystem and TS, monitors overall launch and recovery performance, and commands a variety of recovery options.
When required, the RS sends commands to the TS via a communications interface. The TS Pedestal weighs an additional 58 kilograms pounds. The Track Subsystem Pedestal Group is composed of four units:.
The pedestal unit is a two-axis gimbal system with a high-gain inch parabolic dish, tracking antenna mounted to its gimbal. There are three sets of lifting handles that permit two men to carry the pound pedestal pounds if the SMS is installed on the base.
The interrogator unit is the track subsystem RF transmitter and receiver, and is mounted to the top of the pedestal unit. The bore-sight camera is a charge-coupled device, color video camera with a fixed set for infinity focal length, which is bore-sighted to the TS pedestal antenna.
The bore-sight camera is mounted to the pedestal unit. The Airborne Subsystem is comprised of an internally mounted transponder Unit 5 , and a fin-type antenna Unit 6 mounted on top of the air vehicle's main compartment cover.
The Airborne Subsystem, including antenna, weighs 1. The TSAS electronics enclosure sits atop a inch telescoping tripod. The SMS outputs are used to stabilize the UCARS position data, generally allowing the recovery software to know if sensed relative air-vehicle-to-ship position changes are the result of UAV motion or ship motion.
Although UCARS does allow the IP to conduct a full automatic recovery of the air vehicle, a requirement for a qualified and current EP will continue, primarily as an emergency backup recovery method, and for those periods when the UCARS is inoperable or unavailable.
Delta training consisting of UCARS familiarization, operation, and maintenance procedures will be required prior to or concurrent with system delivery.
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The "C" School courses are also divided into separate Initial and Career training courses. "A" School Core courses include general knowledge and skills training for the particular rating, while "A" School Strand courses focus on the more specialized training requirements for that rating and a specific aircraft or. CG V05 Electrician's Mate, Class A (AC/DC Theory) ELCTEC DC and AC Electronics 2 3 02/03/17 DM CGR-EM EM1 Electrician's Mate Course.
26.01.2018 - When the UAV is feet from the intended touchdown point, a logic signal is transmitted, switching to the Omni-directional antenna for final approach, touchdown, and roll-out. As soon as your order ships you will receive tracking information via email. Ccleaner free download 2011 for windows 7 64 bit -... In order to perform reconnaissance missions, the payload operator may use several payload control modes. Training Equipment has, or had as its prime or initial purpose for existence some function other than that of training personnel.
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03.03.2018 - Delivery is currently delayed pending software corrections. High to Low Product Name: Ccleaner free download for windows 64 bit - For wi... The EP course will require additional curriculum to provide overview of the UCARS functional and physical descriptions and operational concepts. The tracking plate assembly rotates by manual control, and provides reception for the Omni antenna and the horn antenna assemblies. The aft antenna and pedestal are located inside a radome located above Pri-Fly.
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13.03.2018 - If an item cannot be fulfilled immediately it will be ordered from our manufacturer. This item has low stock in our warehouses and your order will ship based on availability. Ccleaner new version for windows 8 - Setup ccleane... The MMF receives electrical power and ship's telephone service, via umbilical, from a pre-groomed junction box. Although similar, installations are not duplicates, due to varying ship design and technological changes over the installation timeline. OT was terminated in October
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CAT II is not affected due to being a software update only. Modifications will be required to include GPWS concurrent with installation. Training course modifications will not affect track length or student throughput.
C as part of training track M Model Manager C as part of training track D Model Manager No new training pipelines or tracks are required by this NTSP. Existing operator training tracks, as identified in I.
Existing maintenance training tracks as identified in I. Proficiency training for GPWS maintenance personnel will be provided through managed on-the-job training at the organizational level.
Maintenance Training Improvement Program. MTIP will be used to establish an effective and efficient training system that is responsive to fleet training requirements. MTIP is a training management tool that, through diagnostic testing, identifies individual training.
MTIP is the comprehensive testing of one's knowledge. It consists of a bank of test questions managed through automated data processing. MTIP will allow increased effectiveness in the application of training resources through identification of skills and knowledge deficiencies at the activity, work center, or individual technician level.
Remedial training will be concentrated where needed to combat identified skill and knowledge shortfalls. Aviation Maintenance In-Service Training. However, it is structured very differently, and will function as an integral part of the new Aviation Maintenance Training Continuum System AMTCS that will replace the existing aviation maintenance training structure.
AMIST will provide standardized instruction to bridge the training gaps between initial and career training. With the implementation of AMIST, the technician will be provided the training required to maintain a level of proficiency necessary to effectively perform the required tasks to reflect a career progression.
Aviation Maintenance Training Continuum System. The application and adoption of recent advances in computer hardware and software technology have enabled CBT with its basic elements of Computer Managed Instruction, Computer Aided Instruction, and Interactive Courseware to be integrated into the training continuum and provide essential support for standardizing technical training.
It is a performance-based, standardized, level-progressive, documentable, training management and evaluation program. It identifies and prioritizes task inventories by MOS through a front-end analysis process that identifies task, skill, and knowledge requirements of each MOS.
Test Sets, Tools, and Test Equipment. As a result of the Human Systems Integration testing during OT it was recommended that the light panel be removed in the final configuration.
Schedule of Events a. Installation and Delivery Schedules. Ready For Operational Use Schedule. Time Required to Install at Operational Sites. Specific activity schedules are shown in element IV.
Annual Incremental and Cumulative Billets. Existing training activity instructor and support personnel billet levels are adequate to support GPWS training.
No additional billets are required. Student billets are chargeable to the type aircraft for which the student receives overall training. The currently planned chargeable student billets will not change due to the GPWS.
They are contained in the specific aircraft NTSP. Existing Training Phased Out Note: For information on student throughputs refer to: Allied Signal Avionics, Inc. Cubic Defense Systems, Inc.
Training Hardware Training Devices. Date required indicates the date when GPWS information will be incorporated into these manuals. Find more like this. Our content is added by our users. We aim to remove reported files within 1 working day.
Please use this link to notify us:. Report this file as copyright or inappropriate. CAT II not addressed due to it being a software update only.
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HML/A Avionics Technician Responsible for testing, trouble shooting, repair, and replacement of com/nav/elect/ weapon systems for the UH-1N and AH-1W. Occasionally supervised up to three Marines in on line trouble shooting, repairs, and inspections of aircraft. Additional Information: Military Avionics technician with hands-on training in. navy training system plan. for the. modular integrated avionics group a appendix b - uav common automatic recovery system b and six modified l-class ships. avionics common core class a1: c avionics technician i level class a1: c carrier air traffic control center(catcc) operations officer: c-2g