PFTL 101B-2.0工业自动化卡件
这不构成运营批准。最低导航性能规范（MNPS）空域，当配备双柯林斯FMS-6000飞行管理系统和双柯林斯GPS-4000A GPS接收机，或在批准用于单GPS导航的航线上配备单FMS-6000航班管理系统和/或单GPS-4000A接收机时。这不构成运营批准。根据AC 20-129.7，航路、终端和进近VNAV操作过程中的VFR/IFR。禁止使用FMS在公布的终点外捕捉和跟踪DME弧。8.燃油管理参数仅供参考，不能替代主要燃油量指示。自动驾驶仪1。必须在当天的第一次飞行之前以及任何通电或维护活动之后对系统进行令人满意的飞行前检查。2.在自动驾驶仪操作期间，驾驶员必须坐在控制装置上，系好安全带和肩带。3.起飞和着陆时不得使用自动驾驶仪和偏航阻尼器。4.在正常飞行期间，不要手动超控自动驾驶仪。警告：在俯仰时超控自动驾驶仪不会取消自动驾驶仪自动配平。如果在自动驾驶仪接通的情况下对转向柱施加力，则自动配平将运行以对抗所施加的力。在飞行的任何阶段，这都可能导致严重的越野状况。5.自动驾驶系统运行的最大空速不得超过飞机指示的最大速度VMO/MMO。6.禁止在俯仰配平故障时操作自动驾驶系统。7.在非精密进近或I类精密进近操作期间，不得在地面上方200英尺以下使用自动驾驶仪或偏航阻尼器，或在所有其他操作期间，在地面上方600英尺以下使用。8.自动驾驶耦合进近的最大证明不利风力条件为17节侧风分量和11节顺风分量。9.必须以小于90°的截距角完成导航和定位器捕获。Hawker 800XP Pro Line 21飞机飞行手册第20页第2节限制FAA批准的修订版A1：2002年11月13日10。当与自动驾驶仪连接时，必须执行II类进近，限制如下：跑道可视范围（RVR）最小决断高度（DH）最小100英尺顺风17节顺风11节顺风17节自动驾驶仪必须在。仅80英尺双发动机运行11.在II类进近过程中，如果自动驾驶仪故障或在1000英尺AGL以下脱离，则必须停止II类进。允许手动飞行接近I类最小值。VNAV 1.使用VNAV系统时，气压高度表必须用作所有操作的主要高度参考。2.禁止对V-MDA进近使用VNAV制导，该进近包括最终进近定位和错过进近点之间的降压定位。3.使用VNAV进行飞行引导时，必须在MFD地图页面或CDU航段页面上显示VNAV高度。
This does not constitute an operational approval.Minimum Navigation Performance Specification (MNPS) airspace when equipped with dual Collins FMS-6000 Flight Management Systems and dual Collins GPS-4000A GPS receivers, or a single FMS-6000 Flight Management System and/or single GPS-4000A receiver on routes approved for single GPS navigation. This does not constitute an operational approval.VFR/IFR enroute, terminal and approach VNAV operation in accordance with AC 20-129. 7. Use of FMS to capture and track a DME arc outside the published end points is prohibited. 8. Fuel management parameters are advisory only and do not replace the primary fuel quantity indications. Autopilot 1. A satisfactory preflight check of the system must be performed before the first flight of the day and after any power up or maintenance activity. 2. During autopilot operations, a pilot must be seated at the controls with seat belt and shoulder harness fastened. 3. The autopilot and yaw damper must not be used for takeoff and landing. 4. Do not manually override the autopilot during normal flight. WARNING: OVERRIDING THE AUTOPILOT IN PITCH DOES NOT CANCEL THE AUTOPILOT AUTOMATIC TRIM. IF A FORCE IS APPLIED TO THE COLUMN WITH THE AUTOPILOT ENGAGED, THEN AUTOMATIC TRIM WILL RUN TO OPPOSE THE APPLIED FORCE. THIS CAN LEAD TO A SEVERE OUT-OFTRIM CONDITION DURING ANY PHASE OF FLIGHT. 5. Maximum airspeed for operation of the autopilot system must not exceed the airplane indicated maximum speed VMO/MMO. 6. Operation of the autopilot system with a pitch trim malfunction is prohibited. 7. Do not use the autopilot or yaw damper below 200 ft above terrain during non-precision or Category I precision approach operations, or 600 ft above terrain during all other operations. 8. The maximum demonstrated adverse wind conditions for autopilot coupled approaches are 17 knots crosswind component and 11 knots tailwind component. 9. Nav and localizer captures must be accomplished with an intercept angle of less than 90°. Hawker 800XP Pro Line 21 Airplane Flight Manual Page 20 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002 10. Category II approaches must be executed while coupled to the autopilot with the following limits: Runway Visual Range (RVR) 1200 ft minimum Decision Height (DH) 100 ft minimum Headwind 17 knots Tailwind 11 knots Crosswind 17 knots Autopilot must be disengaged at.80 ft Two engine operations only 11. During a Category II approach, if the autopilot malfunctions or disengages below 1000 ft AGL, the Category II approach must be discontinued. Hand flying the approach to Category I minimums is allowable. VNAV 1. When using the VNAV system, the barometric altimeters must be used as the primary altitude reference for all operations. 2. Use of VNAV guidance for a V-MDA approach that includes a step-down fix between the final approach fix and missed approach point is prohibited. 3. VNAV altitudes must be displayed on the MFD map page or CDU legs page when utilizing VNAV for flight guidance.
