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Windows Área de trabalho Earth Alerts 2025.1.10 Earth Alerts2025.1.10 Earth Alertsé um aplicativo de software projetado para manter os usuários informados sobre desastres naturais em todo o mundo. Ele monitora vários eventos ambientais, incluindo terremotos, furacões, tsunamis e vulcões. Através de dados em tempo real de fontes oficiais, Earth Alerts fornece atualizações oportunas, ajudando os usuários a se manterem cientes de possíveis ameaças próximas à sua localização ou em qualquer região que eles escolham monitorar.A interface é fácil de usar, tornando fácil a navegação e a personalização das notificações. Os usuários podem selecionar alertas específicos, filtrar por localização e ajustar como recebem as atualizações. Essa personalização garante informações relevantes e sob medida que atendem às necessidades pessoais ou profissionais sem sobrecarregar os usuários com notificações excessivas.Earth Alertsintegra uma variedade de fontes, incluindo o U.S. Geological Survey e o National Weather Service. Esta extensa rede permite que o software ofereça dados abrangentes e precisos sobre condições atuais e riscos potenciais. Além disso, mapas visuais, imagens de radar e satélite aprimoram a experiência fornecendo uma visão clara do status e desenvolvimento de cada evento.Earth Alertsé particularmente útil para qualquer pessoa vivendo em áreas propensas a desastres, viajantes frequentes ou equipes de resposta a emergências. Com Earth Alerts, os usuários obtêm informações valiosas que melhoram a preparação e a consciência situacional, ajudando-os a permanecer seguros diante de eventos naturais imprevisíveis.Principais Características:Alertas em Tempo Real: Receba notificações instantâneas para vários eventos naturais, incluindo furacões, terremotos, tsunamis e erupções vulcânicas.Rastreamento do Tempo: Acesse previsões meteorológicas atualizadas e alertas de tempo severo para locais em todo o mundo.Relatórios Detalhados: Veja dados abrangentes sobre eventos naturais em andamento, incluindo detalhes de tempestades, magnitude de terremotos e riscos de inundações.Imagens de Satélite: Acesse imagens de satélite e mapas de radar que oferecem uma visão visual dos eventos naturais ativos.Notificações Personalizáveis: Defina preferências de localização para receber alertas específicos para áreas de interesse.Dados Históricos: Revise dados de eventos passados para entender a frequência e tendências de impacto de diferentes desastres naturais.Monitoramento de Eventos Múltiplos: Acompanhe múltiplos eventos naturais simultaneamente, garantindo cobertura abrangente e conscientização.Interface Amigável: Navegue por uma interface clara e organizada com fácil acesso a alertas atuais e dados de eventos. Alertas da Terra desastres naturais dados em tempo real Programa disponível em outras línguas Download Earth Alerts Télécharger Earth Alerts Herunterladen Earth Alerts Scaricare Earth Alerts ダウンロード Earth Alerts Descargar Earth Alerts Avaliações dos usuários Classificação do

N) Propeller manufacturer : mt-Propeller o) Propeller designation : MTV-6-A-C-F/CF 187-129... Page 44 Operating Limitations DA 42 AFM CAUTION If the coolant or gearbox oil level is low, the reason must be determined and the problem must be corrected by authorized personnel. v) Maximum restart altitude 6000 ft w) Restart airspeed 80 to 120 KIAS Page 2 - 8 Rev. Page 45: Engine Instrument Markings DA 42 AFM Operating Limitations 2.5 ENGINE INSTRUMENT MARKINGS Engine instrument markings and their color code significance are shown in the table below: Indi- Yellow Green Yellow cation arc/bar arc/bar arc/bar arc/bar arc/bar lower caution normal caution upper prohibited range... Page 46: Warning, Caution And Advisory Alerts Operating Limitations DA 42 AFM 2.6 WARNING, CAUTION AND ADVISORY ALERTS 2.6.1 WARNING, CAUTION AND ADVISORY ALERTS ON THE G1000 NOTE The alerts described in the following are displayed on the Garmin G1000. Section 7.10 includes a detailed description of the alerts. Page 47 DA 42 AFM Operating Limitations Warning alerts Meaning / Cause (red) L/R ENG FIRE Left / Right engine fire detected. L/R STARTER Left / Right engine starter is engaged. DOOR OPEN Front and/or rear canopy and/or baggage door are/is not closed and locked. Page 48 Operating Limitations DA 42 AFM Color and significance of the caution alerts on the G1000 Caution-alerts Meaning / Cause (amber) * A fault has occurred in the left / right engine ECU A (one reset of minor faults is possible) Page 49: Other Warning Alerts DA 42 AFM Operating Limitations Color and significance of the advisory alerts on the G1000 advisory alerts Meaning / Cause (white) L/R GLOW ON Left / Right engine glow plug active. L/R FUEL XFER Fuel transfer from auxiliary to main tank is in progress. Page 50: Mass (Weight) Operating Limitations DA 42 AFM 2.7 MASS (WEIGHT) Value Mass (Weight) Minimum flight mass 1250 kg 2756 lb Maximum take-off mass MÄM 42-088 not carried out 1700 kg 3748 lb MÄM 42-088 carried out 1785 kg 3935 lb Maximum zero fuel mass... Page 51: Center Of Gravity DA 42 AFM Operating Limitations 2.8 CENTER OF GRAVITY Datum Plane The Datum Plane (DP) is a plane which is normal to the airplane’s longitudinal axis and in front of the airplane as seen from the direction of flight. The airplane’s longitudinal axis is parallel with the floor of the nose baggage compartment. Page 52: Approved Maneuvers Operating Limitations DA 42 AFM 2.9 APPROVED MANEUVERS The airplane is certified in the Normal Category in accordance with JAR-23. Approved maneuvers 1) all normal flight maneuvers; 2) stalling (with the exception of dynamic stalling); and 3) Lazy Eights, Chandelles, as well as steep turns and similar maneuvers, in which an angle

Hiểm liên quan đến sạt lở đất.Hoạt động tại các địa điểm ở Hoa Kỳ mà người sử dụng đã chọn: động đất, cháy rừng, thời tiết tại địa phương bao gồm cảnh báo thời tiết NWS/nguy hiểm, tình trạng hiện tại, dự báo và ảnh vệ tinh/rada.Tích hợp Google Earth để cung cấp hình ảnh các hiện tượng động đất, sóng thần, bão nhiệt đới, cháy rừng và thời tiết khắc nghiệt.Cảnh báo hình ảnh và âm thanh trên máy tính Windows.Gửi email: Thông tin về bất kỳ loại hiện tượng tự nhiên nào được theo dõi bởi Earth Alerts đều có thể được thiết lập tự động ngay khi có cảnh báo; các tin nhắn email chứa bản báo cáo và hình ảnh cảnh báo tương tự như được hiển thị trong màn hình ứng dụng Earth Alerts.Điện thoại di động: Tin nhắn SMS/MMS chứa thông tin cảnh báo tổng quan với hình ảnh liên quan (chỉ dành cho điện thoại kích hoạt MMS) có thể được gửi tự động tới thiết bị di động của bạn. Những thông báo này bao gồm các hiện tượng tự nhiên nghiêm trọng nhất bao gồm động đất, sóng thần, núi lửa,…Yêu cầu hệ thốngPhần mềmTrong quá trình cài đặt Earth Alerts, bạn sẽ được thông báo tự động để download/cài đặt .NET Framework 3.5 nếu nó chưa có trên hệ điều hành Windows của bạn. Tuy nhiên, nếu quá trình cài đặt Earth Alerts thất bại và/hoặc nó không thông báo cho bạn về .NET Framework 3.5, bạn có thể download trực tiếp từ đây.Phần cứngBộ vi xử lý: Pentium III trở lên.Độ phân giải màn hình: 1024 x 768 trở lên.Ổ đĩa cứng trống: 5 MB.Kết nối Internet băng thông rộng.

Stopped: 6. Rudder ......neutral 7. Page 124 Emergency DA 42 AFM Procedures 3.9.7 EMERGENCY DESCENT 1. FLAPS ......UP 2. Page 125 Normal Operating DA 42 AFM Procedures CHAPTER 4A NORMAL OPERATING PROCEDURES Page 4A.1 INTRODUCTION ........4A-3 4A.2 AIRSPEEDS FOR NORMAL OPERATING PROCEDURES . Page 126 Normal Operating DA 42 AFM Procedures 4A.6.14 SHUT-DOWN ....... . 4A-37 4A.6.15 PARKING . Page 127: Introduction Normal Operating DA 42 AFM Procedures 4A.1 INTRODUCTION Chapter 4A contains checklists and describes procedures for the normal operation of the airplane. NOTE Readability of the G1000 PFD and MFD displays may be degraded when wearing polarized sunglasses. 4A.2 AIRSPEEDS FOR NORMAL OPERATING PROCEDURES... Page 128 NOTE is always less than v . For the DA 42 however, the actual value of v would be below the minimum safe speed. The minimum airspeed for best angle of climb was therefore raised... Page 129: Advisory Alerts On The G1000 Normal Operating DA 42 AFM Procedures 4A.3 ADVISORY ALERTS ON THE G1000 The G1000 provides the following advisory-alerts on the PFD in the alert area: 4A.3.1 ADVISORY / GENERAL White color coded text CHARACTERISTICS 4A.3.2 L/R GLOW ON L/R GLOW ON Left / Right engine glow plug active 4A.3.3 L/R FUEL XFER... Page 130: Flight Characteristics Procedures 4A.4 FLIGHT CHARACTERISTICS The DA 42 is to be flown with "the feet on the pedals“, meaning that coordinated flight in all phases and configurations shall be supported by dedicated use of the rudder and ailerons together. With the landing gear extended and at aft CG-locations, with flaps up and full power... Page 131: Daily Check Normal Operating DA 42 AFM Procedures 4A.5 DAILY CHECK Before the first flight of a day it must be ensured that the following functions are operable without failure. * On-condition check of the canopy, the side door and the baggage compartment doors for cracks and major scratches. Page 132 Normal Operating DA 42 AFM Procedures Center console: FUEL SELECTOR ..... check ON POWER Lever ......check condition, freedom of... Page 133 Normal Operating DA 42 AFM Procedures Check procedure: a) ELECT. MASTER ..... ON CAUTION When switching the ELECT. MASTER ON, the electrically driven hydraulic gear pump may activate itself for 5 to 20 seconds in order to restore the system pressure. Page 134 Normal Operating DA 42 AFM Procedures g) Control stick ......pull fully aft / hold at backstop h) FLAPS . Page 135 Normal Operating DA 42 AFM Procedures II. Walk-around check, visual inspection CAUTION A visual inspection means: examination for damage, cracks, delamination, excessive play, load transmission, correct attachment and general condition. In addition control surfaces should be checked for freedom of movement. Page 136 Normal Operating DA 42 AFM Procedures 2. Left engine nacelle:

Caution And Advisory Messages DA 42 AFM Airplane Description 7.10.3 WARNING, CAUTION AND ADVISORY MESSAGES Crew Alerting System (CAS) The G1000 Crew Alerting System (CAS) is designed to provide visual and aural alerts to the flight crew. Alerts are divided into three levels as follows:... Page 308 Airplane Description DA 42 AFM Alert levels Level Text Color Importance Audible Tone Warning May require Warning chime tone immediate w h i c h r e p e a t s corrective action without delay until acknowledged by the crew... Page 309 DA 42 AFM Airplane Description Warning alerts on the G1000 Warning alerts Meaning / Cause The annunciation is active when the engine coolant temperature L/R ENG TEMP is greater than 105 °C. The annunciation is active when the engine oil temperature is L/R OIL TEMP greater than 140 °C. Page 310 Airplane Description DA 42 AFM Warning alerts Meaning / Cause WARN This annunciation constitutes a RAIM position warning. The nav deviation bar is removed. Audible warning alerts Warning alerts Meaning / Cause A warning chime tone which repeats without delay is active... Page 311 DA 42 AFM Airplane Description Caution alerts on the G1000 Caution-alerts Meaning / Cause The annunciation is active when a fault in ECU A or ECU B has occurred. L/R ECU A FAIL In case of minor faults, the annunciation can be reset once by pressing the ECU TEST button for more than 2 seconds. Page 312 Airplane Description DA 42 AFM Annunciation advisory alerts on the G1000 Advisory alerts Meaning / Cause L/R GLOW ON The annunciation is active when the glow plugs are powered. L/R FUEL XFER The annunciation is active when fuel transfer from auxiliary to main tank is in progress. Page 313: Pitot-Static System 7.12 STALL WARNING SYSTEM The lift detector of the DA 42 is located on the front edge of the left wing below the wing chord line. It is supplied electrically and provides a stall warning, before the angle of attack becomes critical. Page 314: Garmin G1000 Integrated Avionics System Airplane Description DA 42 AFM 7.13 GARMIN G1000 INTEGRATED AVIONICS SYSTEM 7.13.1 GENERAL The Gamin G1000 is a fully integrated flight, engine, communication, navigation and surveillance instrumentation system. This Integrated Avionics System consists of a Primary Flight Display (PFD), a Multi-Function Display (MFD), an Audio Panel, an Attitude and Heading Reference System (AHRS), an Air Data Computer (ADC) and the sensors and computers to process flight and engine information for display to the pilot. Page 315: Primary Flight Display (Pfd) DA 42 AFM Airplane Description 7.13.2 PRIMARY FLIGHT DISPLAY (PFD) The Primary Flight Display (PFD; see figure below) typically displays airspeed, attitude, altitude, and heading information in a