PFTL 101BE-5.0 ABB卡件
退出结冰条件：机身上大量积冰，通常无法观察到积冰的区域。保护区机翼后部积冰。由于自动驾驶仪可能会掩盖指示操纵特性不利变化的触觉提示，当存在上述任何视觉提示时，或当飞机处于结冰状态时遇到异常的横向配平要求或自动驾驶仪配平警告时，禁止使用自动驾驶仪。第11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飞机飞行手册发动机限制发动机类型2联合信号TFE731-5BR-1H涡扇发动机。发动机限制*这些条件显示在标牌上。注：1.初始最大起飞推力由飞行员在起飞时选择。当自动性能储备（APR）系统运行时，如果另一台发动机在起飞过程中发生故障，将在一台发动机上自动获得最大起飞推力。最大APR推力的五分钟限制必须包括APR运行前初始最大起飞推力下的运行时间。APR运行期间超过的任何正常起飞限制必须记录在技术日志中。2.这不是正常的巡航设置。条件%RPM最大ITT°C时间限制N1 N2启动或重新启动*---978 996超过996无限制10秒5秒起飞*100 100.8 978 1006 1016 5分钟5秒2秒最大起飞推力*（APR运行）（见注释1）100 100.8 996 1006 1015分钟5秒钟2秒初始最大起飞推力（APR不运行）最大持续秒数*100 100.8 968无限制（见注释2）最大超速*103 103----最高127°C至最高30000 ft的5秒。最高瞬时温度高于30000 ft的140°C。最低149°C（2分钟）（启动）。最低-40°C（起飞）30°C起飞和最大连续爬升。38磅/平方英寸（262 kPa）至46磅/平方英尺（317.2 kPa）空载25磅/平方米（172.4 kPa）最低瞬时最大值。55磅/平方英寸（379.2千帕）（3分钟）油压温度第12页第2节限制FAA批准的A3版：2005年3月22日霍克800XP Pro Line 21飞机飞行手册批准的发动机机油发动机机油消耗任何飞行期间发动机的最大允许机油消耗率为0.01美国加仑（0.036升）/小时。不得在发动机燃油计算机不工作的情况下启动发动机燃油计算机飞行。发动机同步器起飞时，发动机同步开关必须选择OFF。自动性能储备（APR）自动性能储备系统必须为起飞准备就绪，但机组人员培训除外，无需准备就绪。发动机仪表标记红色指示。已超过最大或最小限值。黄色指示在短时间内或特殊情况下允许的小心操作-请参阅个别限制。绿色或白色指示正常操作。未完成霍尼韦尔服务公告72-3597或72-3662的飞机已完成霍尼韦尔服务公报72-3597和72-3662 Aeroshell/Royco涡轮机油500美孚254 Aeroshell/Royco涡轮机油560埃克森2197 BP涡轮机油2197 BP汽轮机油2197英国石油涡轮机油2380 Castrol 5000埃克森/埃索2380涡轮机油埃克森2197美孚喷气机油II美孚254注：发动机机油在该柱中可以混合。注意：此列中的发动机机油可以混合。不要将这些油与任何其他油混合。第13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飞机飞行手动推力反向器任一推力反向器的部署仅限于地面操作。在飞机落地之前，不得选择推力反向操纵杆。禁止在反推装置展开的情况下启动发动机。不得使用反向推力向后滑行。除非在紧急情况下，否则不得在低于50 KIAS的速度下选择超过反向怠速的推力。在非铺装路面上作业时，不得超过反向空转推力，紧急情况除外。如果已知反推系统不工作或不可用，则必须禁用并锁定在前推力位置。发动机防冰系统发动机防冰开关可在任何发动机转速下选择ON（接通）。如果起飞期间需要发动机防冰，建议
exit the icing conditions:Extensive ice accumulation on the airframe in areas not normally observed to collect ice.Accumulation of ice on the wing aft of the protected area. Since the autopilot may mask tactile cues that indicate adverse changes in handling characteristics, use of the autopilot is prohibited when any of the visual cues specified above exist, or when unusual lateral trim requirements or autopilot trim warnings are encountered while the airplane is in icing conditions. Page 11 Section - 2 LIMITATIONS FAA Approved Revision A3: Mar 22, 2005 Hawker 800XP Pro Line 21 Airplane Flight Manual ENGINE LIMITATIONS Engine Type Two Allied Signal TFE731-5BR-1H turbofan engines. Engine Limitations * These conditions appear on placards. NOTES: 1. Initial maximum take-off thrust is selected by the pilot on takeoff. When the Automatic Performance Reserve (APR) System is operative, maximum take-off (APR) thrust will be obtained automatically on one engine if the other engine fails during takeoff. The five minute limit of maximum APR thrust must include the duration of operation at initial maximum take-off thrust prior to the operation of APR. Any normal takeoff limitations exceeded during APR operation must be recorded in the technical log. 2. This is not a normal cruise setting. CONDITION % RPM MAX ITT °C TIME LIMIT N1 N2 Start or Relight * ---- ---- 978 996 over 996 Unrestricted 10 Seconds 5 Seconds Takeoff * 100 100.8 978 1006 1016 5 Minutes 5 Seconds 2 Seconds Maximum Take-off Thrust * (APR Operating) (see NOTE 1) 100 100.8 996 1006 1016 5 Minutes 5 Seconds 2 Seconds Initial Maximum Take-off Thrust (APR Not Operating) 100 100.8 978 1006 1016 5 Minutes 5 Seconds 2 Seconds Maximum Continuous * 100 100.8 968 Unrestricted (see NOTE 2) Maximum Overspeed * 103 103 ---- 5 Seconds Maximum . 127° C up to 30,000 ft Maximum . 140° C above 30,000 ft Transient Maximum.149° C (2 minutes) Minimum (Starting) .-40° C Minimum (Takeoff) 30° C Takeoff and Maximum Continuous and Climb .38 lb/in2 (262 kPa) to 46 lb/in2 (317.2 kPa) Idle25 lb/in2 (172.4 kPa) minimum Transient Maximum.55 lb/in2 (379.2 kPa) (3 minutes) Temp Oil Press Oil Page 12 Section - 2 LIMITATIONS FAA Approved Revision A3: Mar 22, 2005 Hawker 800XP Pro Line 21 Airplane Flight Manual Approved Engine Oils Engine Oil Consumption The maximum permissible oil consumption rate of an engine during any flight is 0.01 U.S. gallons (0.036 liters) per hour. Engine Fuel Computer Flight must not be initiated with an engine fuel computer inoperative. Engine Synchronizer The ENG SYNC switch must be selected OFF for takeoff. Automatic Performance Reserve (APR) The Automatic Performance Reserve (APR) system must be armed for takeoff, except for crew training only, when it need not be armed. Engine Instrument Markings Red Indications .A maximum or minimum limit has been exceeded. Yellow IndicationsCautionary operations permissible for short duration or in special circumstances - refer to individual limitations. Green or White IndicationsNormal operations. Airplanes which have not accomplished Honeywell Service Bulletin 72-3597 or 72-3662 Airplanes which have accomplished Honeywell Service Bulletin 72-3597 or 72-3662 Aeroshell/Royco Turbine Oil 500 Mobil 254 Aeroshell/Royco Turbine Oil 560 Exxon 2197 BP Turbo Oil 2197 BP Turbo Oil 2197 BP Turbo Oil 2380 Castrol 5000 Exxon/Esso 2380 Turbo Oil Exxon 2197 Mobil Jet Oil II Mobil 254 NOTE: Engine oils in this column can be mixed. NOTE: Engine oils in this column can be mixed. Do not mix these oils with any other oils. Page 13 Section - 2 LIMITATIONS FAA Approved Revision A3: Mar 22, 2005 Hawker 800XP Pro Line 21 Airplane Flight Manual Thrust ReversersDeployment of either thrust reverser is restricted to ground operations only.The thrust reverse levers must not be selected until the airplane is on the ground.Engine starts with thrust reversers deployed are prohibited.Reverse thrust must not be used to taxi backwards.Thrust in excess of reverse idle must not be selected below speeds of 50 KIAS, except in an emergency.When operating on unpaved surfaces, reverse idle thrust must not be exceeded except in an emergency.If the thrust reverser system is known to be inoperative or unserviceable, it must be disabled and locked in the forward thrust position. Engine Ice Protection System The ENG ANTICE switches may be selected ON at any engine speed. If engine anti-icing is required during takeoff, it is recommended that they should be
