PFTL 101BER-10.0机器人模块卡件
140-590032-005TC16（第2期）2006年3月2日第2节-防冰限制阅读以下信息，以代替第9页“结冰概述”中的现有信息：当室外空气温度（OAT）、地面和起飞时，SAT温度为10°C或以下，并且存在任何形式的可见水分（例如，云、能见度为1英里（1600米）或以下的雾、雨、雪、雨夹雪和冰晶）。在坡道、滑行道或跑道上运行时，地面和起飞时的OAT为10qC或以下时，也存在结冰情况，因为发动机可能会吸入表面雪、冰、积水或泥浆，或发动机、短舱或发动机传感器探头结冰。阅读以下信息代替第9页“机身结冰”中的现有信息：禁止在机翼、控制表面、发动机进气口或其他关键表面上附着霜、冰、雪或泥浆的情况下进行机身结冰起飞，但以下区域除外：只要深度不超过1/8英寸（3 mm），则允许在油箱总面积上的机翼下侧结霜。如果该区域出现霜冻，WAT限制起飞重量必须减少1000磅（454千克），并且必须使用比实际重量高1000磅（452千克）的重量获得净飞行路径参考和第四段爬升梯度。机身上的霜是允许的，前提是该层足够薄，能够区分表面特征，例如下面的油漆线或标记，但所有通风口、探头和端口必须没有霜。当外部空气温度低于50°F（10°C）或无法确定机翼燃油温度高于32°F（0°C）时，必须对机翼前缘和机翼上表面进行目视和触觉（手动）检查，以确保机翼无霜、冰、雪或雪泥；存在可见湿气（雨、毛毛雨、雨夹雪、雪、雾等）；或机翼上有水；或露点与外部空气温度之差为5°F（3°C）或更低；或大气条件有利于结霜。第9页第2节限制FAA批准的修订版A3:2005年3月22日Hawker 800XP Pro Line 21飞机飞行手册防冰限制当地面和起飞期间的外部空气温度（OAT）或飞行中的总空气温度（TAT）为10°C或以下时，存在一般结冰条件，并且存在任何形式的可见水分（例如云、能见度为1英里（1600米）或以下的雾、雨、雪、雨夹雪和冰晶）。当地面和起飞的OAT为10°C或以下时，当在坡道、滑行道或跑道上运行时，也会出现结冰情况，因为发动机可能会吸入表面雪、冰、积水或泥浆，或发动机、短舱或发动机传感器探头结冰。机身结冰飞机起飞前必须没有雪、冰和霜，以下区域除外：如果深度不超过0.125英寸（3.175毫米），则允许在油箱总面积上的机翼下侧结冰。如果该区域出现霜冻，WAT限制起飞重量必须减少1000磅（454千克），并且必须使用比实际重量高1000磅（452千克）的重量获得净飞行路径参考和第四段爬升梯度。机身上的霜是允许的，前提是该层足够薄，能够区分表面特征，例如下面的油漆线或标记，但所有通风口、探头和端口必须没有霜。机翼/尾翼防冰系统只能使用TKS80、R328除冰液或符合规格DTD 406B的除冰液。注：指示满的油箱可提供至少85分钟的充注和保护。发动机结冰-参见本节发动机限制。第10页第2节限制FAA批准的修订版A3:2005年3月22日Hawker 800XP Pro Line 21飞机飞行手册严重结冰条件限制警告：严重结冰可能由飞机认证以外的环境条件造成。在冻雨、冻雨或混合结冰条件（过冷液态水和冰晶）下飞行可能会导致受保护表面上的积冰超过防冰系统的能力，或可能导致受保护的表面后部结冰。这些冰可能不会使用防冰系统脱落，并可能严重降低飞机的性能和可控性。在飞行过程中，超过飞机认证的严重结冰条件应通过以下视觉提示确定。如果存在一个或多个此类视觉提示，请立即向空中交通管制部门请求优先处理，以促进路线或高度变化
140-590032-0005TC16 (Issue 2) March 2, 2006 SECTION 2 - LIMITATIONS ICE PROTECTION LIMITATIONS Read the following information in place of the existing information under Icing General on Page 9: Icing General Icing conditions exist when Outside Air Temperature (OAT), on the ground and during takeoff, is 10° C SAT or below and visible moisture in any form is present (e.g. clouds, fog with visibility of 1 mile (1600 meters) or less, rain, snow, sleet and ice crystals). Icing conditions also exist when the OAT, on the ground and for takeoff, is 10qC or below when operating on ramps, taxiways, or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on the engines, nacelles or engine sensor probes. Read the following information in place of the existing information under Airframe Icing on Page 9: Airframe Icing Takeoff is prohibited with frost, ice, snow or slush adhering to the wings, control surfaces, engine inlets or other critical surfaces, with the exception of the following areas:Frost is allowable on the underside of the wings over the general area of the fuel tanks provided that the depth does not exceed 1/8 inch (3 mm). If frost is present in this region, the WAT limited take-off weight must be reduced by 1000 lb (454 kg) and the net flight path reference and fourth segment climb gradients must be obtained using a weight 1000 lb (454 kg) higher than the actual weight.Frost is allowable on the fuselage provided the layer is thin enough to distinguish the surface features such as paint lines or markings underneath, but all vents, probes and ports must be clear of frost. A visual and tactile (hand on surface) check of the wing leading edges and the wing upper surface must be performed to ensure the wing is free from frost, ice, snow or slush when the outside air temperature is less than 50° F (10° C) or if it cannot be ascertained that the wing fuel temperature is above 32° F (0° C) and;There is visible moisture (rain, drizzle, sleet, snow, fog, etc.) present; orWater is present on the wing; orThe difference between the dew point and the outside air temperature is 5° F (3° C) or less; orThe atmospheric conditions have been conducive to frost formation. Page 9 Section - 2 LIMITATIONS FAA Approved Revision A3: Mar 22, 2005 Hawker 800XP Pro Line 21 Airplane Flight Manual ICE PROTECTION LIMITATIONS Icing General Icing conditions exist when Outside Air Temperature (OAT) on the ground and during takeoff, or Total Air Temperature (TAT) in flight is 10° C or below, and visible moisture in any form is present (e.g. clouds, fog with visibility of 1 mile (1600 meters) or less, rain, snow, sleet and ice crystals). Icing conditions also exist when the OAT on the ground and for takeoff is 10° C or below when operating on ramps, taxiways, or runways where surface snow, ice, standing water or slush may be ingested by the engines or freeze on the engines, nacelles or engine sensor probes. Airframe Icing The airplane must be clear of snow, ice and frost before takeoff with the exception of the following areas:Frost is allowable on the underside of the wings over the general area of the fuel tanks provided that the depth does not exceed 0.125 inch (3.175 mm). If frost is present in this region, the WAT limited take-off weight must be reduced by 1000 lb (454 kg) and the net flight path reference and fourth segment climb gradients must be obtained using a weight 1000 lb (454 kg) higher than the actual weight.Frost is allowable on the fuselage provided the layer is thin enough to distinguish the surface features such as paint lines or markings underneath, but all vents, probes and ports must be clear of frost. Wing/Tail Antice System Only de-ice fluids TKS80, R328 or fluid to specification DTD 406B must be used. NOTE: A tank indicating FULL provides priming and protection for a period of at least 85 minutes. Engine Icing Refer to ENGINE LIMITATIONS - this section. Page 10 Section - 2 LIMITATIONS FAA Approved Revision A3: Mar 22, 2005 Hawker 800XP Pro Line 21 Airplane Flight Manual SEVERE ICING CONDITIONS LIMITATIONS WARNING: SEVERE ICING MAY RESULT FROM ENVIRONMENTAL CONDITIONS OUTSIDE OF THOSE FOR WHICH THE AIRPLANE IS CERTIFICATED. FLIGHT IN FREEZING RAIN, FREEZING DRIZZLE, OR MIXED ICING CONDITIONS (SUPERCOOLED LIQUID WATER AND ICE CRYSTALS) MAY RESULT IN ICE BUILD-UP ON PROTECTED SURFACES EXCEEDING THE CAPABILITY OF THE ICE PROTECTION SYSTEM, OR MAY RESULT IN ICE FORMING AFT OF THE PROTECTED SURFACES. THIS ICE MAY NOT BE SHED USING THE ICE PROTECTION SYSTEMS, AND MAY SERIOUSLY DEGRADE THE PERFORMANCE AND CONTROLLABILITY OF THE AIRPLANE. During flight, severe icing conditions that exceed those for which the airplane is certificated shall be determined by the following visual cues. If one or more of these visual cues exists, immediately request priority handling from Air Traffic Control to facilitate a route or an altitude change to
