PFTL 101BE-2.0机器人备件
燃油系统管理1.在飞行期间，包括起飞和着陆期间，两个机翼油箱之间的燃油量差异不得超过500磅（227千克）。2.当机翼油箱中的燃油油位降至每侧3300磅（1497千克）时，腹侧油箱中携带的燃油应转移到机翼油箱中。3.对于腹侧油箱中有燃油的着陆，需要进行超重着陆程序和检查。电气限制电池限制起飞前主飞机电池（B1和B2）的最大电池电量不得超过20安培。发电机限制最大连续发动机发电机负载：300 AMPS注：允许最大400 AMPS的瞬时偏移最多持续2分钟。主发动机起动机占空比在地面上，允许的最大起动机工作时间为30秒。在中止启动后，在再次尝试启动之前，必须允许至少1分钟的冷却时间。在进行第三次尝试之前，还需要1分钟。该循环可以在另外的30分钟后重复。断路器的操作如果在飞行过程中，系统故障伴随着断路器操作，则除非在适当的紧急或异常程序中有规定，否则不得尝试重置断路器，或者如果认为有必要继续安全飞行，断路器可重置一次。Hawker 800XP Pro Line 21飞机飞行手册第17页第2节限制FAA批准的修订版A1:2002年11月13日航空电子限制概述1.以下文件必须始终携带在飞机上：Hawker 800XP飞行员指南P/N 523-7800409，第1版，2001年5月31日或更高版本。Collins FMS-6000 Hawker 800XP飞行员指南飞行管理系统，P/N 523-780705，2001年4月17日第1版或更高版本。Mk V增强型近地警告系统飞行员指南，P/N 060-4241-0000，D版，2000年3月或更高版本。这些出版物包含柯林斯Pro Line 21航空电子设备、FMS-6000、TCAS II和EGPWS装置的说明和操作，必须可供使用。2.飞行员和副驾驶的空气数据计算机必须能在起飞时运行。3.AHRS 1和2必须可用于起飞。高频无线电1。当ADF用于进近时，禁止使用高频无线电。2.高频无线电传输期间不得使用燃油量指示。电子备用仪表系统（ESIS）1.ESIS空速带上的红色空速警告不提供相关的声音警告。2.在仅参考ESIS的操作过程中，不得超过备用VMO/MMO指示，因为ESIS高度和空速指示未针对静态误差进行校正。飞行管理系统1.IFR航路和终端导航被禁止，除非飞行员参考当前批准的数据验证数据库的货币或每个选定航路点和助航设备的准确性。2.在用作导航工具之前，在以下条件下，必须检查FMS位置的准确性：在FMS沿经批准的RNAV航路导航期间，在到达每个航路航路点时或之前。在请求离航航路之前，以及在FMS导航离开批准的RNAV航路期间，每隔一小时进行一次。在IFR运行期间的每个强制报告点之前，不受雷达监视控制。3.航位推算期间，FMS不得用于导航。霍克800XP Pro Line 21飞机飞行手册第18页第2节限制FAA批准版本A1：2002年11月13日4。所有FMS导航操作均在美国国家空域系统内批准，纬度以北纬60°和南纬60°为界。北纬70°的作业可在西经75°以东和西经120°以西进行。操作至80°
Fuel System Management 1. During flight, including takeoff and landing, the difference in fuel quantity between the two wing tanks must not exceed 500 lb (227 kg). 2. Fuel carried in the ventral fuel tank shall be transferred into the wing tanks when the fuel level in the wing tanks has fallen to 3300 lb (1497 kg) per side. 3. Overweight landing procedure and inspection is required for any landing with fuel in the ventral tank. ELECTRICAL LIMITATIONS Battery Limitations Maximum battery charge on the main airplane batteries (B1 and B2) immediately before takeoff shall not be greater than 20 AMPS. Generator Limitations Maximum continuous engine generator load: 300 AMPS NOTE: Transient excursions, up to a maximum of 400 AMPS, are permitted for a maximum of 2 minutes. Main Engine Starter Duty Cycle On the ground, the maximum permitted starter operating time is 30 seconds. After an aborted start, a minimum of 1 minute cooling time must be allowed before making another attempt to start. A further 1 minute is required before making a third attempt. The cycle may be repeated after a further period of 30 minutes. Operation of Electrical Circuit Breakers If, during flight, a systems failure is accompanied by a circuit breaker operation, no attempt must be made to reset the circuit breaker unless specified in the appropriate Emergency or Abnormal procedure or, if deemed necessary for the continuation of safe flight, a circuit breaker may be reset once. Hawker 800XP Pro Line 21 Airplane Flight Manual Page 17 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002 AVIONICS LIMITATIONS General 1. The following documents must be carried onboard the airplane at all times:Collins Pro Line 21 Avionics System for the Hawker 800XP Pilot’s Guide P/N 523-0780409, 1st Edition dated May 31, 2001 or later revision.Collins FMS-6000 Flight Management System for the Hawker 800XP Pilot’s Guide, P/N 523-0780705, 1st Edition dated April 17, 2001 or later revision.Mk V Enhanced Ground Proximity Warning System Pilot Guide, P/N 060-4241-0000, Rev D, dated March 2000 or later revision. These publications contain the description and operation of the Collins Pro Line 21 avionics, the FMS-6000, TCAS II and EGPWS installations and must be available for use. 2. The pilot’s and copilot’s Air Data Computers must be operative for takeoff. 3. AHRS 1 and 2 must be operative for takeoff. HF Radio 1. When the ADF is being used for approaches, the use of the HF radio is prohibited. 2. Fuel quantity indications are not to be used during HF radio transmissions. Electronic Standby Instrument System (ESIS) 1. The red airspeed warning on the ESIS airspeed tape does not provide an associated aural warning. 2. During operations solely with references to the ESIS, the standby VMO/MMO indication must not be exceeded, as the ESIS altitude and airspeed indications are not corrected for static error. Flight Management System 1. IFR enroute and terminal navigation is prohibited unless the pilot verifies either the currency of the database or the accuracy of each selected waypoint and navaid by reference to current approved data. 2. The FMS position must be checked for accuracy prior to use as a means of navigation and under the following conditions:At or prior to arrival at each enroute waypoint during FMS navigation along approved RNAV routes.Prior to requesting off-airway routing and at hourly intervals thereafter during FMS navigation off approved RNAV routes.Prior to each compulsory reporting point during IFR operation when not under radar surveillance control. 3. During periods of dead reckoning, the FMS shall not be used for navigation. Hawker 800XP Pro Line 21 Airplane Flight Manual Page 18 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002 4. All FMS navigation operations are approved within the U.S. National Airspace System and latitudes bounded by 60° North latitude and 60° South latitude at any longitude.Operation to 70° North latitude is acceptable East of 75° West longitude and West of 120° West longitude.Operation to 80°
