PFTL 101B 5KN 3BSE00418SR1机器人备件
机动速度VA 196 KIAS注：机动速度是指完全应用空气动力学控制不会导致飞机过载的速度。涉及失速附近迎角的机动应限于低于VA的速度。避免快速和大的交替控制输入，尤其是与俯仰、横滚或偏航的大变化（例如大滑移角）相结合，因为它们可能导致任何速度下的结构故障，包括低于VA的情况。机翼襟翼扩展/操作速度VFE/VFO。220 KIAS（15°襟翼）175 KIAS（25°襟翼）165 KIAS（45°襟翼）15°襟翼用于下降和保持的程序使用15°襟翼进行下降和保持程序使用的最大空速为220 KIAS。最大使用高度为15000英尺。结冰条件下不允许使用机翼襟翼。Hawker 800XP Pro Line 21飞机飞行手册第23页第2节限制FAA批准修订版A1:2002年11月13日空气制动器空气制动器（仅襟翼0°）无限制起落架扩展/操作速度VLE/VLO 220 KIAS鸟击速度在正常情况下，满足鸟击要求的最大允许空速为280 KIAS至8000 ft。在-10°C以下的温度下进行飞机地面浸泡后，挡风玻璃加热装置应在环境温度低于-10°C的情况下运行并选择开启至少5分钟，在环境温度高于-20°C的条件下起飞至少15分钟。如果未达到挡风玻璃加热操作的最短时间，或者在环境温度低于-10°C的情况下发生挡风玻璃加热故障，则最大允许空速为257 KIAS至8000 ft。Hawker 800XP Pro Line 21飞机飞行手册第24页第2节限制FAA批准的原始版本：11月30日，2001故意留空第1页，共2页，P/N 140-590032-005TC13 2005年3月14日临时变更P/N 140-599032-005TC3受影响的出版物：受影响的飞机序列号：变更说明：填写说明：第2节-限制其他限制阅读以下信息，作为第2节：挖沟后的补充，请勿打开主舱门。FAA批准的飞机飞行手册，P/N 140-590032-005，2001年11月30日，或配备Pro Line 21航空电子设备的Hawker 800XP飞机的更高版本。Hawker 800XP 258541、258556、258567及更高版本。增加挖沟信息和程序。将本临时变更第1页（共1页）插入第2节-限制中的第25页。Hawker 800XP Pro Line 21飞机飞行手册第25页第2节限制FAA批准修订版A1:2002年11月13日其他限制空气制动器在飞行中，当襟翼伸展到任何位置时，不得操作空气制动器。客舱紧急过载出口客舱内部紧急过载出口锁销（如已安装）必须在每次飞行前拆除并收起。仅当在海拔9000英尺以上的机场作业时，才应选择客舱高基准。机组座椅在起飞和着陆期间，两个机组座椅应锁定到位。安装和使用时，第三个机组成员座椅应锁定到位；不使用时，应将其折叠、存放或从飞机上取下。客舱间门当机组和乘客舱之间设有门时，应在起飞和着陆期间将其固定在打开位置。提升卸载提升卸载仅在飞机在地面上时使用。机动载荷系数限制操作仅限于正常飞行机动，不允许特技飞行。结构批准的最大加速度（即荷载系数）为2.0g（襟翼展开时）和2.73g（襟翼完全缩回时）。超过这些值的操作会导致结构永久变形，必须避免。最少飞行机组人员最少两名飞行员。
Maneuvering Speed VA 196 KIAS NOTE: Maneuvering speed is the speed below which full application of aerodynamic controls will not result in excessive airplane loads. Maneuvers involving angles of attack near the stall should be confined to speeds below VA. Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll or yaw (e.g. large slip angles) as they may result in structural failures at any speed, including below VA. Wing Flaps Extended/Operating Speed VFE/VFO.220 KIAS (Flaps 15°) 175 KIAS (Flaps 25°) 165 KIAS (Flaps 45°) Procedural Use of Flaps 15° for Descent and Holding The maximum airspeed for procedural use of flaps 15° for descent and holding is 220 KIAS. The maximum altitude for use is 15,000 ft. Such use of wing flaps is not permitted in icing conditions. Hawker 800XP Pro Line 21 Airplane Flight Manual Page 23 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002 Air Brakes Air Brakes (Flaps 0° Only) No Limit Landing Gear Extended/Operating Speed VLE/VLO 220 KIAS Bird Strike Speed Under normal conditions the maximum permissible airspeed to meet bird strike requirements is 280 KIAS up to 8000 ft. Following an airplane ground soak at temperatures below -10° C, the windscreen heat should be operative and selected ON for a minimum of 5 minutes prior to takeoff in ambient temperatures of below -10° C and for a minimum of 15 minutes prior to takeoff when ambient temperatures are below -20° C. If the minimum times for windscreen heat operation have not been achieved or in the case of windscreen heat failure followed by flight in ambient temperature below -10° C, the maximum permissible airspeed is 257 KIAS up to 8000 ft. Hawker 800XP Pro Line 21 Airplane Flight Manual Page 24 Section - 2 LIMITATIONS FAA Approved Original Issue: Nov 30, 2001 Intentionally left blank Page 1 of 2 P/N 140-590032-0005TC13 March 14, 2005 TEMPORARY CHANGE P/N 140-590032-0005TC13 PUBLICATION AFFECTED: AIRPLANE SERIAL NUMBERS AFFECTED: DESCRIPTION OF CHANGE: FILING INSTRUCTIONS: SECTION 2 - LIMITATIONS MISCELLANEOUS LIMITATIONS Read the following information as an addition to Section 2: Ditching After ditching, do not open the main cabin door. FAA Approved Airplane Flight Manual, P/N 140-590032-0005, Dated Nov 30, 2001, or later revision for Hawker 800XP airplanes equipped with Pro Line 21 avionics. Hawker 800XP 258541, 258556, 258567 and After. Addition of ditching information and procedures. Insert this Temporary Change Page 1 of 1 to face Page 25 in Section 2 - LIMITATIONS. Hawker 800XP Pro Line 21 Airplane Flight Manual Page 25 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002 MISCELLANEOUS LIMITATIONS Air Brakes In flight, the air brakes must not be operated when the flaps are extended to any position. Cabin Emergency Overwing Exit The internal cabin emergency overwing exit locking pin, if installed, must be removed and stowed before each flight. Cabin High Datum Cabin High Datum shall only be selected when operating into airfields greater than 9000 ft elevation. Crew Seats Both crew seats shall be locked in position during takeoff and landing. When installed and in use, the 3rd crew member seat shall be locked in position; when not in use, it shall be folded and stowed or removed from the airplane. Inter-compartment Door When a door is provided between the crew and passenger compartments, it shall be secured in the open position during takeoff and landing. Lift Dump Lift dump is to be used only when the airplane is on the ground. Maneuvering Load Factor Limitations Operation is limited to normal flying maneuvers and aerobatic maneuvers are not permitted. The maximum accelerations (i.e. load factors) for which the structure is approved are 2.0g with flaps extended and 2.73g with flaps fully retracted. Maneuvers exceeding these values can cause permanent distortion of the structure and must be avoided. Minimum Flight Crew The minimum crew is two pilots.
