PFTL 101BE-20.0备件模块
t在设置起飞功率之前打开。在预期结冰条件下，应在飞行中连续使用发动机入口防冰。当不存在结冰条件时，在高于50°F（10°C）的环境条件下使用入口防冰的时间不得超过10秒。燃油限制以下燃油和添加剂经批准用于本发动机安装。燃料规格航空煤油符合以下规格的当前批准版本：英国DEF STAN 91-87（D.E.R.D.2453）DEF STAN 91-91（D.E.R.D.2494）美国ASTM D1655/JET A ASTM D1655/JET A-1 MIL-T-83133/JP8加拿大CAN/CGSB 3.23/JET A CAN/CGSA 3.23/JE A-1俄罗斯GOST 10227-86 TS-1 GOST 10227-86T-1 GOST 10227-86%RT中国GB 6537-94/No。3喷气燃料第14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飞机飞行手册航空广泛削减燃料，符合以下规范的当前批准版本：燃料添加剂防静电STADIS 450添加剂的使用浓度不得超过百万分之三（ppm）（按体积计）。SIGBOL添加剂TU38-101741-78的使用浓度不得超过0.0005体积%。防冰和生物杀灭添加剂用于防冰和预防性连续生物杀灭处理，DEF STAN 68-252、MIL-I-27686或MIL-I-85470的使用浓度不得超过0.15体积%。注意：不应将上述添加剂添加到符合规格DEF STAN 91-87、MIL-T-5624和MIL-T-83133的燃油中，因为这些燃油中已经存在这些添加剂。符合GOST 17477-86的TGF；TGF（M）转化为TU6-10-1457-79；符合GOST 8313-88；I（M）至TU 6-10-1458-79的浓度可不超过0.3体积%。Biobor JF的浓度可不超过百万分之135（重量），作为预防性生物杀灭处理。对于生物杀灭冲击处理，Biobor JF的使用浓度不超过270 ppm（重量），前提是随后在发动机启动前卸载（135 ppm是发动机运行的最大浓度）。抗腐蚀添加剂燃料可能含有符合DEF STAN 68-251或MIL-I-25017的添加剂，其浓度符合燃料规范的要求。注：符合规格的DEF STAN 91-87燃料已经包括HITEC E515。英国DEF STAN 91-88（D.E.R.D.2454）美国ASTM D1655/JET B MIL-T-5624/JP4 MIL-T-5624/JP5加拿大CAN/CGSB 3.22/JET B俄罗斯GOST 10227-86 T-2 Hawker 800XP Pro Line 21飞机飞行手册第15页第2节限制FAA批准修订A1：11月13日，2002最高燃油温度最高允许燃油温度为57°C。最低燃油温度为避免燃油冻结或超过发动机限制的可能性，应遵守以下环境空气和指示的燃油温度限制：燃油量当重力填充时，每个油箱的可用燃油容量如下：当燃油量指示器在水平飞行中读数为零时，油箱中剩余的任何燃油不应计入。压力加油后，每个机翼油箱的容量将减少2.4美制加仑（9.1升），腹侧油箱的容量减少3.6美制加仑（13.6升）。对于具有外部厕所服务设施的飞机，腹水箱的容量减少了4.8美制加仑（18.2升）。起飞时燃油最低燃油温度或环境空气温度飞行时最低燃油温度燃油冻结温度DEF STAN 91-91（D.E.R.D 2494）DEF STAN 91-87（D.E.R.D 2453）ASTM D1655/JJET A-1 MIL-GALLONS EQUIVALENT LITERS机翼油箱（任一侧）634 2400通风油箱233 882 Hawker 800XP Pro Line 21飞机飞行手册第16页第2节限制FAA批准的A1版：11月13日，2002燃料装载燃料箱可按任何顺序进行补充，前提是遵守了适当的加油说明，并且满足了以下飞行前燃料装载条件：1.机翼油箱中的燃料应在两个机翼油箱之间均匀分配。2.除非每个主翼油箱含有至少3450磅（1565千克）的燃油，否则不得在腹油箱中携带燃油。3.在使用前，腹水箱必须完全装满。对于其他航班，必须为空。如果MWS面板上的琥珀色FUEL信号器和车顶面板上的黄色REFUEL on信号器亮起，则不得启动压力加油起飞。禁止在加油电源开关打开的情况下飞行。
urned ON prior to setting takeoff power. Engine inlet anti-icing should be used in flight continuously during expected icing conditions. When icing conditions do not exist, the inlet anti-icing should not be used above 50° F (10° C) ambient conditions for more than 10 seconds. FUEL LIMITATIONS The following fuels and additives are approved for use with this engine installation. Fuel Specifications Aviation kerosene to the current approved issue of the following specifications: British DEF STAN 91-87 (D.E.R.D. 2453) DEF STAN 91-91 (D.E.R.D. 2494) American ASTM D1655/JET A ASTM D1655/JET A-1 MIL-T-83133/JP8 Canadian CAN/CGSB 3.23/JET A CAN/CGSB 3.23/JET A-1 Russian GOST 10227-86 TS-1 GOST 10227-86 T-1 GOST 10227-86 RT Chinese GB 6537-94/No. 3 JET FUEL Page 14 Section - 2 LIMITATIONS FAA Approved Revision A3: Mar 22, 2005 Hawker 800XP Pro Line 21 Airplane Flight Manual Aviation wide-cut fuel to the current approved issue of the following specifications: Fuel Additives Anti-static STADIS 450 additive may be used in concentrations not exceeding 3 parts per million (ppm) by volume. SIGBOL additive TU38-101741-78 may be used in concentrations not exceeding 0.0005% by volume. Anti-icing and biocidal additives For anti-icing and preventative continuous Biocidal treatment DEF STAN 68-252, MIL-I-27686 or MIL-I-85470 may be used in concentrations not exceeding 0.15% by volume. NOTE: The above additives should not be added to fuel to specification DEF STAN 91-87, MIL-T-5624 and MIL-T-83133 as they are already present in these fuels. TGF to GOST 17477-86; TGF(M) to TU 6-10-1457-79; I to GOST 8313-88; I(M) to TU 6-10-1458-79 may be used in concentrations not exceeding 0.3% by volume. Biobor JF may be used at concentrations not exceeding 135 parts per million by weight, as preventative biocidal treatment. For biocidal shock treatment, Biobor JF may be used at concentrations not exceeding 270 ppm by weight, provided it is subsequently off-loaded prior to engine start (135 ppm is the maximum concentration for engine operation). Anti-corrosive Additive Fuels may contain additives complying with DEF STAN 68-251 or MIL-I-25017 at concentrations permitted by the fuel specification. NOTE: Fuel to specification DEF STAN 91-87 already includes HITEC E515. British DEF STAN 91-88 (D.E.R.D. 2454) American ASTM D1655/JET B MIL-T-5624/JP4 MIL-T-5624/JP5 Canadian CAN/CGSB 3.22/JET B Russian GOST 10227-86 T-2 Hawker 800XP Pro Line 21 Airplane Flight Manual Page 15 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002 Maximum Fuel Temperature The maximum permissible fuel temperature is 57° C. Minimum Fuel Temperature To avoid the possibility of fuel freezing or exceeding engine limitations, the following ambient air and indicated fuel temperature limitations should be observed: Fuel Quantity The usable fuel capacity of each tank when gravity filled is as follows: Credit shall not be taken for any fuel remaining in the tanks when the fuel quantity indicators read zero in level flight. After pressure refueling, the contents of each wing tank will be 2.4 US Gallons (9.1 Liters) less and the contents of the ventral tank will be 3.6 US Gallons (13.6 Liters) less. The contents of the ventral tank are reduced by 4.8 US Gallons (18.2 Liters) for airplanes which have an external toilet servicing facility. FUEL MINIMUM FUEL OR AMBIENT AIR TEMP AT TAKEOFF MINIMUM FUEL TEMP IN FLIGHT FUEL FREEZING TEMP DEF STAN 91-91 (D.E.R.D 2494) DEF STAN 91-87 (D.E.R.D 2453) ASTM D1655/JET A-1 MIL- GALLONS EQUIVALENT LITERS Wing tank (either side) 634 2400 Ventral tank 233 882 Hawker 800XP Pro Line 21 Airplane Flight Manual Page 16 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002 Fuel Loading Fuel tanks may be replenished in any sequence provided that the appropriate refueling instructions are observed and that the following preflight fuel loading conditions are achieved: 1. Fuel contained in the wing tanks shall be equally disposed between the two wing tanks. 2. Fuel must not be carried in the ventral tank unless each main wing tank contains at least 3450 lb (1565 kg) of fuel. 3. Before flights on which it is to be utilized, the ventral tank must be filled completely. For other flights it must be empty. Pressure Refueling Takeoff must not be initiated if the amber FUEL annunciator on the MWS panel and the amber REFUEL ON annunciator on the roof panel are illuminated. Flight with the Refuel Power Switch ON is prohibited.
