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Supplier: Accuris
Description: CATEGORY III INSTRUMENT LANDING SYSTEM
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Supplier: Accuris
Description: SITING CRITERIA FOR INSTRUMENT LANDING SYSTEMS
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Supplier: Accuris
Description: MINIMUM OPERATIONAL PERFORMANCE SPECIFICATION FOR COMBINED INSTRUMENT LANDING SYSTEM (ILS) AND MICROWAVE LANDING SYSTEM (MLS) AIRBORNE RECEIVING EQUIPMENT
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Supplier: Accuris
Description: CATEGORY I INSTRUMENT LANDING SYSTEM EQUIPMENT REQUIREMENTS
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Supplier: SAE International
Description: This SAE Aerospace Recommended Practice (ARP) provides guidance to prepare pilots to participate in simultaneous instrument landing system (ILS) precision runway monitor (PRM) approaches to closely-spaced parallel runways.
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Supplier: UE Systems, Inc.
Description: machine cuts 21 groves in an armature. The armature is spun 360° creating a click for each grove. With sensor contacting the armature, the instrument counts the clicks. An incorrect count is noted in a control panel. III. A paper mill monitors a critical valve. In only specific situations
- Air / Structure Borne: Yes
- Form Factor: Monitoring System
- Instrument Type: Acoustic Emission, Condition Monitor / Fault Detector, Flaw Detector, Leak Detector
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Supplier: ASTM International
Description: aircraft shall be inspected for performance while on a specified flight time, including takeoff and landing, and shall undergo instrument verification. In addition, this specification also provides for post flight acceptance testing, which shall include a review of all flight critical
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Supplier: SAE International
Description: (DME), instrument landing system (ILS), markers (MKR), very low frequency (VLF), inertial navigation systems (INS), inertial reference systems (IRS), global navigation satellite system (GNSS), global positioning system (GPS), low range radio altimeter
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Supplier: Diamond Aircraft
Description: propeller with unfeathering accumulator Composite airframe and safety seats (up to 26g protection) Lightning protection system Fire extinguisher 3 point inertia reel safety harness (all seats) Instrument lighting Overhead cabin lights
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Supplier: SAE International
Description: (PA), Select Call (SELCAL), Call Select (CALSEL), Satellite Communications (SATCOM). b Navigation : Very High Frequency Omnidirectional Range (VOR), Tactical Air Navigation (TACAN), Automatic Direction Finder (ADF), Distance Measuring Equipment (DME), Instrument Landing System
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Supplier: Cessna Aircraft Company
Description: Installed on center glare shield panel: LH and RH master caution/master warning lights LH and RH engine fire control switches Flight director/autopilot controller Electronic standby instrument system LH and RH display control units Installed on
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Supplier: Airbus Group
Description: 17,250 km Take-off run 2,880 m Landing run 2,030 m Maximum operating Speed M0.89 Ceiling 13,100 m Engines thrust 311 kN Aircraft weights and
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Supplier: Airbus Group
Description: 18,600 km Take-off run 2,670 m Landing run 1,860 m Maximum operating Speed M0.89 Ceiling 13,100 m Engines thrust 374 kN Aircraft weights and
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Supplier: Airbus Group
Description: 18,300 km Take-off run 3,180 m Landing run 1,960 m Maximum operating Speed M0.86 Ceiling 12,500 m Engines thrust 235 to 249 kN Aircraft
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Supplier: Cessna Aircraft Company
Description: Class A (TAWS-A) SiriusXM Satellite Radio Cabin Briefer Satellite phone system Domestic and International Internet XM Satellite Weather and Radio HF-9000 High Frequency Communications Installed on Instrument Panel (left to
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Supplier: Cessna Aircraft Company
Description: Standby Instrument System LH and RH Display Control Units Installed on Instrument Panel (left to right): Electrical Power Panel Left-Hand Primary Flight Display (PFD) Multifunction Display (MFD) Right-Hand Primary Flight Display (PFD
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Supplier: Cessna Aircraft Company
Description: System Landing-Gear Control Module RH Multifunction Display (MFD) RH Primary Flight Display (PFD) RH Digital Audio Control Panel Cockpit Voice Recorder Controller Database Loading Unit (DBU) Installed on Tilt Panel (left to
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Supplier: ASTM International
Description: , takeoff, climb, landing, balked landing, controllability and maneuverability, vibrations, and ground control and stability. For compliance of structure requirements, the following shall be considered: flight loads; control surface and system loads; horizontal stabilizing and
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Supplier: ASTM International
Description: , landing, balked landing, controllability and maneuverability, vibrations, and ground control and stability. For compliance of structure requirements, the following shall be considered: flight loads; control surface and system loads; horizontal stabilizing and balancing
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Supplier: ASTM International
Description: , takeoff, climb, landing, balked landing, controllability and maneuverability, vibrations, and ground control and stability. For compliance of structure requirements, the following shall be considered: flight loads; control surface and system loads; horizontal stabilizing and
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Supplier: Airbus Group
Description: systems to maintain full functionality, including the dual-duplex Automatic Flight Control System (AFCS), dual-engine full authority digital engine control (FADEC) with backup; five LCD electronic flight instruments; and two Vehicle Monitoring Displays, among other features.
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Supplier: Embraer S.A.
Description: EICAS formats ENGINE INDICATON & CREW ALERTING SYSTEM (EICAS) is used to monitor: system indications engine & APU information cabin pressurization information fuel information flap/speed brake settings landing gear trim positions Airlines
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Supplier: Embraer S.A.
Description: EICAS formats ENGINE INDICATON & CREW ALERTING SYSTEM (EICAS) is used to monitor: system indications engine & APU information cabin pressurization information fuel information flap/speed brake settings landing gear trim positions Airlines
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Supplier: Embraer S.A.
Description: EICAS formats ENGINE INDICATON & CREW ALERTING SYSTEM (EICAS) is used to monitor: system indications engine & APU information cabin pressurization information fuel information flap/speed brake settings landing gear trim positions Airlines
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Supplier: Embraer S.A.
Description: EICAS formats ENGINE INDICATON & CREW ALERTING SYSTEM (EICAS) is used to monitor: system indications engine & APU information cabin pressurization information fuel information flap/speed brake settings landing gear trim positions Airlines
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Supplier: Beechcraft Corporation
Description: the intensity and level of targets, and turbulence detection to help avoid severe weather. This system is designed to interface with the Primary Flight Display (PFD), Multi-Function Flight Display (MFD) and the Electronic Flight Instrument System (EFIS). Threat Awareness The
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Supplier: Gulfstream Aerospace
Description: vision. Gulfstream also was a technology leader in creating Synthetic Vision-Primary Flight Display. The advanced monitoring system blends three-dimensional color images of terrain, obstacles and runways with instrument readings on the pilot’s display unit, a combination that creates a
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Supplier: Beechcraft Corporation
Description: Electronic Flight Instrument System (EFIS) Engine Indication System (EIS) Air Data System (ADS) Dual Attitude Heading Reference System (AHRS) Automatic Flight Guidance System (AFGS) Flight Management System (WXR) Dual Navigation and
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Supplier: Gulfstream Aerospace
Description: with the Gulfstream Broadband Multilink high-speed data system, two multichannel satellite communications systems or a wireless local network that provides onboard printing, additional Internet access and phone service. Dual media servers, high-definition video source equipment and a
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Supplier: Beechcraft Corporation
Description: The Primary Flight Display (PFD) replaces many traditional cockpit instruments ensuring that all flight-critical information is displayed at the pilot’s fingertips. The Class-B Terrain Awareness and Warning System (TAWS) will alert pilots of potentially hazardous obstacles and
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Supplier: Instrumented Sensor Technology
Description: now available in tri-axial version referred to as the SnapShock-PLUS/3D (SSP/3D)acceleration data logger / impact & transportation data recorder. Each instrument measures and records the peak acceleration levels to which it is exposed along with shock duration and velocity change, and the
- Application: General Lab and Industrial, Vehicular
- Connection to Host: USB, Other
- Sensor Inputs: Accelerometer
- User Interface: None
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Supplier: ValueTronics International, Inc.
Description: . Courseware feature The innovative Courseware feature sets up an education ecosystem by combining powerful PC Course Editor software with the TBS1000B-EDU instruments and a Courseware landing page. The new feature gives educators the ability to create lab descriptions and instructions
- Bandwidth: 200 MHz
- Number of Input Channels: 2 (# channels)
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Supplier: ValueTronics International, Inc.
Description: two different signal frequencies simultaneously. Courseware feature The innovative Courseware feature sets up an education ecosystem by combining powerful PC Course Editor software with the TBS1000B-EDU instruments and a Courseware landing page. The new feature gives educators
- Bandwidth: 100 MHz
- Number of Input Channels: 2 (# channels)
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Supplier: ValueTronics International, Inc.
Description: different signal frequencies simultaneously. Courseware feature The innovative Courseware feature sets up an education ecosystem by combining powerful PC Course Editor software with the TBS1000B-EDU instruments and a Courseware landing page. The new feature gives educators the ability
- Bandwidth: 70 MHz
- Number of Input Channels: 2 (# channels)
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Supplier: ValueTronics International, Inc.
Description: combining powerful PC Course Editor software with the TBS1000B-EDU instruments and a Courseware landing page. The new feature gives educators the ability to create lab descriptions and instructions and then upload the material directly onto a TBS1000-EDU oscilloscope. Existing labs can
- Bandwidth: 200 MHz
- Number of Input Channels: 2 (# channels)
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Small-scale Turbo Compressors for More Efficient Take-off/Landing and Cruise of Future Aircraft
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