PFTL 101B 20.0KN 3BSE004203R1模块备件
前轮轮胎飞机必须安装机加工前轮轮胎。占用人数所载总人数不得超过17人，也不得超过提供经批准座位的人数。压力舱在起飞和着陆过程中，机舱不得加压。正常操作时的最大压差为8.55 lb/in2。注意：安全阀设置为在8.6至8.8 lb/in2（59.3至60.7 kPa）之间运行。方向舵偏置方向舵偏置开关必须打开，并且系统在每次起飞时都能工作。Hawker 800XP Pro Line 21飞机飞行手册第26页第2节限制FAA批准修订版A1:2002年11月13日吸烟当飞机以运输类别（乘客）运行时，禁止在厕所隔间吸烟。应在每个厕所内外提供总结该限制的标牌，且不得遮挡。系统仪表标记红色弧/红色径向最大或最小极限。黄色电弧。短时或特殊情况下允许的警戒范围-请参阅个别限制。天气雷达请勿在地面人员附近使用天气雷达。危险区域延伸至雷达盘前方2英尺。车轮制动器注意：如果任何车轮的易熔塞熔断，则必须在下次起飞前检查制动器并证明其可用。在飞机正常着陆或从被拒起飞停机后，应建立一个等待期，以确保刹车充分冷却，并处于可使用状态，以便再次被拒起飞（关键情况）。拒绝起飞后从拒绝起飞后以90 KIAS或更低的速度完成滑行至开始滑行起飞前所需的时间。单次拒绝起飞后25分钟两次或多次连续拒绝起飞后45分钟如果拒绝起飞的速度大于90 KIAS，则在下一次起飞前必须检查制动器并证明其可用。正常着陆后，从着陆完成滑行到起飞开始滑行所需的等待时间为5分钟，除非起飞重量超过表1中给出的值。当重量超过这些值时，必须允许30分钟。该表基于静止空气和不超过1/2%的下坡。表1下的注释中给出了更不利条件的修正。Hawker 800XP Pro Line 21飞机飞行手册第27页第2节限制FAA批准的修订版A1:2002年11月13日表1-车轮制动器等待期的起飞重量注释：1.在1-5节顺风中减去1500磅（680千克）。2.在6-10节顺风中减去3000磅（1360千克）。3.如果下坡坡度超过1/2%，减去250 lb（113 kg）。4.在阴影区域作业时，受爬升要求限制的起飞重量可能会受到更多限制。5.当现场气压高度低于海平面时，应使用适合海平面的性能。现场压力海拔英尺温度公告700-HF小型方形底座冰块继电器特点这些用于工业应用的小型继电器可从罗克韦尔自动化公司获得两极和四极版本。还有两种类型的插座。透明盖允许目视检查端子。插入式端子连接牢固，但易于安装或拆卸继电器。什么是新的颜色编码标签和线圈盖指示线圈电压类型：交流为橙色，直流为蓝色。使用手动超控按钮进行测试手动超控功能可改变触点状态，即使线圈未通电。此升级将所有具有（-1）选项的目录号更改为新的（-3）选项。增加触点额定值继电器现在额定值为12安培。顶部面板上的视觉接线图机械指示器插座每个触点配置有两种类型，一种与Allen-Bradley通用继电器配件（如浪涌抑制器和定时装置）兼容，另一种与传统开放式端子兼容。产品选择说明：三极选项不再可用。LED选项：为所选公告700-HF继电器类别添加后缀（-4）。否。除了240V交流装置外，添加（-4L）。
Nosewheel Tires The airplane must be installed with chined nosewheel tires. Number of Occupants The total number of persons carried shall not exceed 17 nor that for which approved seating accommodation is provided. Pressure Cabin The cabin shall not be pressurized during takeoff and landing. Maximum pressure differential for normal operations is 8.55 lb/in2. NOTE: The safety valve is set to operate between 8.6 to 8.8 lb/in2 (59.3 to 60.7 kPa). Rudder Bias The rudder bias switches must be ON and the systems operative during each takeoff. Hawker 800XP Pro Line 21 Airplane Flight Manual Page 26 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002 Smoking When the airplane is being operated in the Transport Category (Passenger), smoking in the toilet compartment is prohibited. Placards summarizing this limitation shall be provided inside and outside each toilet and shall not be obscured. System Gage Markings Red Arc/Red Radial Maximum or minimum limit. Yellow Arc . Cautionary range permissible for short duration or in special circumstances - refer to individual limitations. Weather Radar Do not use the weather radar in the vicinity of ground personnel. A hazardous area extends up to 2 feet in front of the radar dish. Wheel Brakes NOTE: If any of the wheels’ fusible plugs blow, the brakes must be inspected and certified serviceable before the next takeoff. After the airplane has made a normal landing or a stop from a rejected takeoff, a waiting period should be established to make sure the brakes are both sufficiently cool and in a serviceable condition for a further rejected takeoff (critical case). After Rejected Takeoff Required period from completion of taxi-in following a rejected takeoff from a speed of 90 KIAS or less, to before start of taxi-out for takeoff. After a single rejected takeoff25 minutes After two or more successive rejected takeoffs .45 minutes If the rejected takeoff is made from a speed greater than 90 KIAS, the brakes must be inspected and certified to be serviceable before the next takeoff. After Normal Landing The required waiting period from completion of taxi-in from landing to before start of taxi-out for takeoff is 5 minutes, except when the take-off weight exceeds the values given in Table 1. When the weight exceeds these values, a period of 30 minutes must be allowed. The table is based on still air and a downhill slope not exceeding 1/2%. Corrections for more adverse conditions are given in the NOTES below Table 1. Hawker 800XP Pro Line 21 Airplane Flight Manual Page 27 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002 Table 1 - Take-off Weights for Wheel Brakes Waiting Period NOTES: 1. In 1 - 5 knot tailwind subtract 1500 lb (680 kg). 2. In 6 - 10 knots tailwind subtract 3000 lb (1360 kg). 3. If the downhill slope exceeds 1/2%, subtract 250 lb (113 kg). 4. Take-off weight as limited by climb requirements may be more restrictive when operating in shaded areas. 5. Performance appropriate to sea level shall be used when the field pressure altitude is below sea level. Field Pressure Altitude ft Temperature Bulletin 700-HF Miniature Square Base Ice-Cube Relay Features These small relays—used in industrial applications—are available from Rockwell Automation in two- and four-pole versions. Two styles of sockets are available, as well. Clear cover Allows visual inspection of terminals. Plug-in terminals Secure connections, yet easy to install or remove relays. What’s New Color coding Tabs and coil covers indicate coil voltage type: orange for AC and blue for DC. Push-to-test with manual override Manual override feature enables changing contact state, even when coils are not energized. This upgrade changes all catalog numbers that had the (-1) option to the new (-3) option. Increased contact ratings Relays are now rated for 12 amps. VisualWiring diagram on top faceplateMechanical indicator Sockets Available in two styles for each contact configuration, one that is compatible with Allen-Bradley general purpose relay accessories such as surge suppressors and timing units and the second with traditional open style terminals. Product Selection Note: Three pole-option is no longer available. LED Option: Add suffix (-4) to the selected bulletin 700-HF relay Cat. No. except for the 240V AC units, add (-4L).
