#: locale=en
## Action
### URL
LinkBehaviour_1B1290BB_0B3C_657D_41A2_275561ECE78B.source = http://www.starbasela.org/
LinkBehaviour_E371DA5E_FAE2_0338_41B2_8F1AC59FFA07.source = http://www.starbasela.org/360/A10/
LinkBehaviour_E3B9F53A_FA26_0178_41E5_BE411D8F8D4E.source = http://www.starbasela.org/360/B1/
LinkBehaviour_21A9213C_334C_4182_41A8_FD9774032238.source = http://www.starbasela.org/360/B29/
LinkBehaviour_EA085D4A_FA22_0118_41C4_E64BD7CB3E32.source = http://www.starbasela.org/360/B52/
LinkBehaviour_045648AE_0AFC_A517_418F_46BF8398BCBC.source = http://www.starbasela.org/360/C130/
LinkBehaviour_0545DCD6_0AE4_9D37_417A_0166D1A58498.source = http://www.starbasela.org/360/C17/
LinkBehaviour_1FF896A3_0662_0308_414A_4E4207FC4264.source = http://www.starbasela.org/360/C5/
LinkBehaviour_05449590_0AE4_6F0B_4181_C178F47373C1.source = http://www.starbasela.org/360/CV22/
LinkBehaviour_E26DA1F3_FA26_0108_41C1_D7DC0BE3CB14.source = http://www.starbasela.org/360/F15/
LinkBehaviour_E39F0E98_FA26_0338_41D0_111C256A7049.source = http://www.starbasela.org/360/F16/
LinkBehaviour_759EC8DA_4279_D9A6_41B9_86EB0167CA60.source = http://www.starbasela.org/360/F22/
LinkBehaviour_E286C3D4_FA22_0108_41C5_F3B37A782769.source = http://www.starbasela.org/360/F35/
LinkBehaviour_1BCECD09_0B27_9F1D_4190_6F1634274858.source = http://www.starbasela.org/360/HH60/
LinkBehaviour_E1966935_FADE_0108_41EB_496F3B2829E7.source = http://www.starbasela.org/360/KC10/
LinkBehaviour_E08BB16B_FAE2_0118_41E3_020D227FB217.source = http://www.starbasela.org/360/KC135/
LinkBehaviour_16EED80B_0BED_E51D_41A1_8A50D676A461.source = http://www.starbasela.org/360/MQ9/
LinkBehaviour_2038DC9B_3344_4086_41AD_3E7854F08D4F.source = http://www.starbasela.org/360/Thunderbirds/
WebFrame_22F9EEFF_0C1A_2293_4165_411D4444EFEA_mobile.url = https://www.google.com/maps/embed?pb=!1m18!1m12!1m3!1d14377.55330038866!2d-73.99492968084243!3d40.75084469078082!2m3!1f0!2f0!3f0!3m2!1i1024!2i768!4f13.1!3m3!1m2!1s0x89c259a9f775f259%3A0x999668d0d7c3fd7d!2s400+5th+Ave%2C+New+York%2C+NY+10018!5e0!3m2!1ses!2sus!4v1467271743182" width="600" height="450" frameborder="0" style="border:0" allowfullscreen>
## Media
### Title
video_5C62225A_4C29_A191_41D1_ABB37A7D13C6.label = B17_Flying_Fortress
video_43D5C41B_4C29_A197_41C4_7CF5015B7991.label = P51_Mustang
panorama_14A98558_0F4F_8555_41A9_D411D17D8C70.label = cargo_back
panorama_14A85714_0F4D_86DD_41AD_85DD10A6ABC7.label = cargo_front
panorama_14A8AFF5_0F4A_855F_41A8_1C0F2AFCE7BB.label = copilot
panorama_14A88950_0F4E_8D55_41A6_5C225ADA886D.label = folded rotors
panorama_14A8D4D3_0F4E_9B5B_41A1_53B59D2FED28.label = folded rotors 2
panorama_14A8807B_0F4E_FB4B_4191_589FC892126B.label = front
panorama_14A83234_0F4A_9EDD_419C_5BD0C1748626.label = front cabin
panorama_14A88BB0_0F4E_8DD6_41A7_8F146BBD5C95.label = left front
panorama_14A840DF_0F4F_9B4B_41A8_AECD8F15CC3A.label = left rear
panorama_14A8A483_0F4D_7BBB_41AD_1299F65EC3DC.label = pilot
panorama_14A99C44_0F4F_8ABD_4174_CA9F322968C3.label = rear
panorama_14A2CA28_0F4F_8EF5_418D_341149AF5A49.label = right front
panorama_12E06EDB_0F4F_874B_4191_9CFE22092621.label = right rear
### Video
videolevel_A7170625_BFE4_106F_41D5_A7BE9954BFC7.url = media/video_43D5C41B_4C29_A197_41C4_7CF5015B7991_en.mp4
videolevel_A7170625_BFE4_106F_41D5_A7BE9954BFC7.posterURL = media/video_43D5C41B_4C29_A197_41C4_7CF5015B7991_poster_en.jpg
videolevel_A717B65D_BFE4_10DF_41D9_076112D6F41F.url = media/video_5C62225A_4C29_A191_41D1_ABB37A7D13C6_en.mp4
videolevel_A717B65D_BFE4_10DF_41D9_076112D6F41F.posterURL = media/video_5C62225A_4C29_A191_41D1_ABB37A7D13C6_poster_en.jpg
### Video Subtitles
## Popup
### Body
htmlText_A6CF4C8C_BE7C_103D_41D9_933B4F26A96D.html = AN/AAQ-27 Forward Looking Infrared (FLIR) - a passive optical imaging sensor that uses IR (thermal) detectors to detect RF heat energy.
AN/APQ-186 Multi-Mode Radar (MMR) – provides real-time, forward looking, multipurpose radar sensor for piloting and navigating the aircraft in day, night, and adverse weather conditions.
Aerial Refuel Probe Manual Drive Unit - allows for extension and retraction of the probe when hydraulic system no. 3 is unavailable.
Aerial Refueling Retractable Probe (ARRP) - allows refueling of all fuel cells while in forward flight
Aircraft Battery - provides 24 VDC power. At 80% charge (19.2 ampere-hour) it provides sufficient power for pressure refueling of the aircraft, a three-minute prestart period, and two APU start cycles, with 18% capacity remaining. In flight, at 80% charge, the Battery provides 20 minutes of emergency power for flight essential equipment in the event of total primary DC power failure.
Aircraft Tow Bar - Towing may be accomplished using a tow bar with a tow tractor or using a spotting dolly. A spotting dolly is typically used aboard ship to facilitate moving aircraft in a confined space. The aircraft Nose Landing Gear (NLG) axle ends are hollow to facilitate connection of towing equipment.
Airdrop Line - provides attachment for breakaway and non-breakaway airdrop anchors. The Anchor Line can be used for parachute static lines or airdrop of containers.
Blade Fold/Wing Stow Control Panel - during any BFWS automated process, the fold/stow push-button switch is pressed and held until the process is completed.
Bottom Anti-Collision Light - provide visibility in all modes of flight and assist in the prevention of aircraft collisions.
Cabin Dome Light (4 total) - provide general purpose interior lighting to the passenger compartment cabin area. Each light contains a white and green NVIS lens.
Cabin Environmental Distribution Ducting – diffuses conditioned air across the cabin.
Call/Tail Numbers – Each aircraft has a call or “tail” number to designate that specific aircraft.
USAF – United States Air Force
0028 – Aircraft Specific call/tail number
Chaffe/Flare Dispenser - capable of launching a "threat specific" response. 5 modes: automatic, semi-automatic, bypass, jettison, and standby.
Circuit Break Panel No. 1 - contain Circuit Breakers, Feeder Buses, and Electro-Magnetic Interference (EMI) filters.
Countermeasures Dispensing System Safety Switch - provides an accessible safety device for a technician to disable the dispense capability of the Countermeasures Dispensing System.
Cycling Control Stick - provides a load path from the Cyclic Grip Assembly to the Cyclic Control mechanical components for transmission of pitch and roll commands.
Deice Boots - The outboard, center, and inboard wing deice boots are neoprene pneumatic boots capable of being inflated from 15 - 22 PSIG maximum. Deice boot inflation is sequential, starting with the outboard wing deice boots moving to the center deice boots then to the inboard deice boots. The inflation duration of the wing deice boots is 5 seconds. After 5 seconds, there is a 15 second air evacuation period in which a vacuum deflates the boots to return it to its original more aerodynamic shape.
Dual Standby Flight Instrument (SFI)/ Traffic Alert and Collision Avoidance System (TCAS) Display –
provides a secondary integrated display of Airspeed, Altitude, Attitude, and Vertical Velocity.
Electric Rescue Hoist Assembly - can lift a capacity of 600 pounds at a continuously variable speed of 0 to 250 feet per minute (FPM) from a maximum distance of 250 feet below the aircraft.
Emergency Oxygen Bottle - provides a limited backup supply of breathing oxygen to the crew in the event of an On-Board Oxygen Generating System (OBOGS) failure. When the system is fully charged it will provide approximately 400 liters of oxygen (approximately 5 minutes of oxygen for four people) at 40 to 70 psi.
Engine Control Panel - a module that brings all of the engine controls, except the thrust control levers, to one central point.
Environmental Control Unit (ECU)- provides conditioned air (heating or cooling) to the aircraft air conditioning system.
Fire Door (2 per nacelle) - During normal operation, the Doors will remain open for cooling of the nacelles. When a fire is detected in a nacelle, the door actuators are signaled to close, shutting off airflow to the nacelle.
Fire Suppression Panel - provides emergency fuel shutoff and fire extinguishing control for aircraft engines and an indication of fire in the engine and/or wings
Flaperons (2 per wing) – During VTOL (vertical takeoff) operation these surfaces works as flaps to a max deflection of 73 degrees. During Airplane mode, these surfaces work as conventional ailerons providing deflection of 25 degrees up and 40 degrees down.
Flight Director Panel (FDP) - serves as the primary operator data entry interface for Flight Director and navigation systems control (automatic flight control system controls).
Flight Ready Configuration – when the wing is spread and locked, rotors are unlocked, nacelles are at 90 degrees, and all blades are unfolded/latched/not in pitch lock.
Ground Refuel/Defuel Panel (GRDP) - provides for all ground refuel and defuel modes, a basic display of fuel system status, total fuel quantity, indications of low oil levels, and a basic display of fuel system failures.
Hydraulic Fluid Level Monitor (HFLM) - monitors the hydraulic fluid level in each Hydraulic System 1, 2, or 3 Reservoir and converts it to quantity
Infrared Suppressor (IRS) - reduces aircraft infrared (IR) signature, deflects engine exhaust away from the fuselage, and provides a cooling air flow path for the nacelle. The IRS system reduces aircraft IR signature by mixing engine exhaust with upper compartment, engine compartment and outside air.
Infrared Suppressor (IRS) - reduces aircraft infrared (IR) signature, deflects engine exhaust away from the fuselage, and provides a cooling air flow path for the nacelle. The IRS system reduces aircraft IR signature by mixing engine exhaust with upper compartment, engine compartment and outside air.
Internal Escape Hatch Initiator Safety Pin – prevents inadvertent firing of the internal escape hatch initiator. If fired, the escape hatch would discharge outward.
Jettison Tube Assembly - provides an external path for the fuel being jettisoned. Fuel is dumped at approximately 800 lbs per minute.
Left Sponson Forward Fuel Cell - provides for storage and containment of fuel and inerting gas, partial self-sealing capabilities, and provides a structural support/mounting interface.
Main Cabin Door - used for normal ingress and egress for aircrew and passengers. The upper half of the door can also be used as an Escape Hatch in emergency situations for quick egress. In an Emergency situation, the Upper Main Cabin Door can be released by internal or external emergency release levers installed in the upper door.
Multifunction Displays (2 in front of each pilot) - provide multicolor displays of flight data, communications, navigation, and aircraft system status.
Nose Landing Gear (NLG) Down-Lockpin - activated by a pop-out handle on the right side of the aircraft nose. The Safety pin is installed to prevent inadvertent movement of the nose landing gear from the down and locked position.
Pendulum Weight Assembly - provides oscillatory force to reduce fixed system oscillatory loads. The assembly consists of the weight and an anti-ice boot.
Position Lights (Left=Red, Right=Green, Tail=White) - installed to determine the aircraft flight direction at night or during low visibility conditions.
Power Distribution Panel (PDP) - contain Contactors, Current Sensors, Feeder Buses, and Terminal Boards to connect, route, and sense aircraft electrical power.
Proprotor Blades – when folded, green blade is on bottom, red blade is in the middle, and the white blade is on top. The proprotor blades are rotated by the hub and produce the lift and thrust that is necessary for flight. The blade structure also supports the centrifugal, torsional, and bending loads that are experienced during flight. The blades have 7 deice zones, a parting strip anti-ice zone, top and bottom tip lighting, and adjustable tip weights.
Proprotor Tip Lights (2 per blade) - show the outer circumference of the rotating proprotor blades during night operations. There are twelve Proprotor Tip Lights which consist of two Light Emitting Diode (LED) light assemblies installed at the tip of each Proprotor blade, one on the upper surface, the other on the lower. These lights provide either visible aviation green lighting or a NVG compatible IR lighting mode.
Pylon Conversion Actuator (PCA) - single telescoping ball screws (1 per nacelle), mounted between the nacelle and wingtip (left and right). The actuators provide control of nacelle rotation, permitting conversion from either helicopter or airplane modes.
Rear Escape Hatch & External Initiator – There are 7 total escape hatches with internal and external initiators to thrust open the hatches (the crew door is the only escape hatch without initiators). The external initiators are provided for use by rescue teams to access the fuselage from outside the aircraft.
Remote Frequency Indicator Selector (RFIS) - displays the active and standby radio information, including radio selected, COMM PLAN channel, preset/manually entered frequency or net, active/standby frequency, radio mode, and security status for the selected radio of the associated pilot.
Search/Landing Lights (1 per pilot) – retractable and rotatable lights that are illuminated during landing, taxing, and search operations in normal or NVG modes.
Shaft Driven Compressor (SDC) Insulated Ducting - double wall construction with an inner titanium pressure carrier and an outer insulation shroud made from a phenolic/fiberglass laminate with an inner layer of aluminum foil bonded to it. Provides air gap insulation with a touch temperature of less than 200 degrees F.
Shaft Driven Compressor (SDC)/Midwing Gearbox (MWGB) Oil Cooler Exhaust – SDC transforms ambient air into compressed air for use by the Environmental Control Unit (ECU) for air conditioning. The MWGB Oil Cooler is a multipurpose unit that contains four separate cores for cooling oil from the MWGB, SDC, utility hydraulic system NO. 3, and the Variable Frequency Generator NO. 4
Standby flight display (SFD) - provides for the independent backup of engine, fuel, and drive systems parameters.
Thrust Control lever (TCL) - provides the pilot/copilot with an interface to the mechanical thrust flight controls for transmission of power commands to the Flight Control Computers. They are interconnected (i.e. one moves, the other copies).
Top Anti-Collision Light - provide visibility in all modes of flight and assist in the prevention of aircraft collisions. The bottom anti-collision light is located on the belly of the aircraft.
Windshields - Anti-Ice heating elements are embedded in the Windshields and terminate on the inside surface with interface terminal strips where the aircraft wiring is connected.
Wing Stow Safety Flags (2 on each side of the fuselage) - allow a ground observer to have a visual indication of the lock/unlock status of the wing lockpins during the Wingstow operation.
Yaw Pedals
Power Steering Mode: provide steering actuator control of the nose landing gear.
Helicopter Mode: provide yaw control of the proprotors when weight-off-wheels is sensed.
Airplane Mode: provide rudder actuator control
Mauris aliquet neque quis libero consequat vestibulum. Donec lacinia consequat dolor viverra sagittis. Praesent consequat porttitor risus, eu condimentum nunc. Proin et velit ac sapien luctus efficitur egestas ac augue. Nunc dictum, augue eget eleifend interdum, quam libero imperdiet lectus, vel scelerisque turpis lectus vel ligula. Duis a porta sem. Maecenas sollicitudin nunc id risus fringilla, a pharetra orci iaculis. Aliquam turpis ligula, tincidunt sit amet consequat ac, imperdiet non dolor.
___
cv-22 osprey
Mission
The CV-22 Osprey is a tiltrotor aircraft that combines the vertical takeoff, hover and vertical landing qualities of a helicopter with the long-range, fuel efficiency and speed characteristics of a turboprop aircraft. The mission of the CV-22 is to conduct long-range infiltration, exfiltration and resupply missions for special operations forces.
features
This versatile, self-deployable aircraft offers increased speed and range over other rotary-wing aircraft, enabling Air Force Special Operations Command aircrews to execute long-range special operations missions. The CV-22 can perform missions that normally would require both fixed-wing and rotary-wing aircraft. The CV-22 takes off vertically and, once airborne, the nacelles (engine and prop-rotor group) on each wing can rotate into a forward position.
The CV-22 is equipped with integrated threat countermeasures, terrain-following radar, forward-looking infrared sensor and other systems that allow it to operate in various austere conditions.
Background
The CV-22 is the Special Operation Forces variant of the U.S. Marine Corps MV-22 Osprey. The first two test aircraft were delivered to Edwards Air Force Base, California in September 2000. The 58th Special Operations Wing at Kirtland AFB, New Mexico began CV-22 aircrew training with the first two production aircraft in August 2006.
The first operational CV-22 was delivered to Air Force Special Operations Command in January 2007. Initial operational capability was achieved in 2009. A total of 54 CV-22 aircraft are scheduled to be delivered by the end of 2021.
General Characteristics
Primary function: Special operations forces long-range infiltration, exfiltration and resupply
Builders: Bell Helicopter Textron Inc., Amarillo, Texas; Boeing Company, Defense and Space Group, Helicopter Division, Philadelphia
Deployment date: 2006
Propulsion: Two Rolls-Royce Liberty AE1107C engines
Thrust: more than 6,200 shaft horsepower per engine
Length: 57’ 4”
Height: 22’ 1”
Wingspan: 83’ 10”
Weight: maximum gross 60,500 pounds (self-deployment); 57,000 pounds (STOL); 52,600 (VTOL)
Speed: maximum 280 knots
Ceiling: 25,000 feet (7,620 meters)
Range: combat radius of 500 nautical miles with one internal auxiliary fuel tank
Crew: four (pilot, copilot and two flight engineers)
Program of Record: 54 aircraft for the Air Force
Rotor diameter: 38 feet
Armament: one .50-caliber machine gun on ramp
Payload: 24 personnel (seated), 32 personnel (floor loaded) or 10,000 pounds of cargo
Unit cost: $90 million
john doe
licensed real estate salesperson
Tlf.: +11 111 111 111
jhondoe@realestate.com
www.loremipsum.com
location
address line 1
address line 2
Mauris aliquet neque quis libero consequat vestibulum. Donec lacinia consequat dolor viverra sagittis. Praesent consequat porttitor risus, eu condimentum nunc. Proin et velit ac sapien luctus efficitur egestas ac augue. Nunc dictum, augue eget eleifend interdum, quam libero imperdiet lectus, vel scelerisque turpis lectus vel ligula. Duis a porta sem. Maecenas sollicitudin nunc id risus fringilla, a pharetra orci iaculis. Aliquam turpis ligula, tincidunt sit amet consequat ac.
Lorem ipsum
dolor sit amet
consectetur adipiscing elit. Morbi bibendum pharetra lorem, accumsan san nulla.
Mauris aliquet neque quis libero consequat vestibulum. Donec lacinia consequat dolor viverra sagittis. Praesent consequat porttitor risus, eu condimentum nunc. Proin et velit ac sapien luctus efficitur egestas ac augue. Nunc dictum, augue eget eleifend interdum, quam libero imperdiet lectus, vel scelerisque turpis lectus vel ligula. Duis a porta sem. Maecenas sollicitudin nunc id risus fringilla, a pharetra orci iaculis. Aliquam turpis ligula, tincidunt sit amet consequat ac, imperdiet non dolor.
Integer gravida dui quis euismod placerat. Maecenas quis accumsan ipsum. Aliquam gravida velit at dolor mollis, quis luctus mauris vulputate. Proin condimentum id nunc sed sollicitudin.
Donec feugiat:
• Nisl nec mi sollicitudin facilisis
• Nam sed faucibus est.
• Ut eget lorem sed leo.
• Sollicitudin tempor sit amet non urna.
• Aliquam feugiat mauris sit amet.