PFTL 101B-10.0机器人模块
禁止在执行复飞程序时使用VNAV。5.如果FMS接收到足够的可用传感器输入，已证明其能够并已证明符合AC 20-129标准的VNAV操作精度规范。此类VNAV进近必须使用飞行指引仪或自动驾驶仪进行飞行。6.如果报告的表面温度低于适用RNAV进近程序图中规定的Baro VNAV最低温度限制，则不允许向DA提供VNAV进近指导。注：进近过程中的气压VNAV制导，包括进近过渡、最后进近航段和复飞程序，不进行温度补偿。在未补偿的最低IFR高度下运行不会为低于ISA的温度提供预期的地形和障碍物净空。第21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EGPWS 1。导航不得基于TAD的使用。地形显示仅用作态势感知工具，可能无法提供仅基于地形回避机动的精度和/或保真度。2.飞行员有权在遵守EGPWS警告所需的范围内偏离其当前的空中交通管制（ATC）许可。3.为了避免发出不必要的警报，当在EGPWS机场数据库中未包含的机场起飞、进近或着陆15海里范围内时，必须通过选择TERR INHIB开关灯来禁止地形感知警报。关于已安装的EGPWS地形数据库中包含的机场，请参阅霍尼韦尔文件060-4326-000。4.当FMS在DR模式下运行时，必须通过选择TERR INHIB（地形抑制）开关灯来禁止地形感知警报。注意：地形数据库、显示器和警报算法目前解释了北美和欧洲有限的编目人为障碍物。如果特定障碍物的数据库中没有障碍物数据，则该障碍物的障碍物感知警报不可用。TCAS II飞行员有权在遵守TCAS决议咨询所需的范围内偏离其当前的ATC许可。如果ATC要求禁用应答机高度报告，则必须关闭TCAS II。第22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飞机飞行手册空速限制最大运行速度VMO 280 KIAS（油箱未空，襟翼0°）VMO 335 KIAS，在29000英尺的最大工作马赫数MMO.80 IMN MMO.73 IMN时，每680英尺减少1节，至310 KIAS，马赫数微调系统失效/不工作且自动驾驶脱离。注：除根据《飞行员操作手册》（POM）第5节第2小节进行飞行员培训或例行试飞外，任何飞行状态（爬升、巡航或下降）均不得故意超过上述最大运行速度和运行马赫数。如果无意中超过了限值，应尽快将速度降低至或低于限值。
4. Use of VNAV while conducting a missed approach procedure is prohibited. 5. Provided the FMS is receiving adequate usable sensor inputs, it has been demonstrated capable of and has been shown to meet the accuracy specifications of VNAV operation in accordance with the criteria of AC 20-129. Such VNAV approaches must be flown utilizing either the flight director or autopilot. 6. VNAV approach guidance to a DA is not authorized if the reported surface temperature is below the Baro-VNAV minimum temperature limitation specified on the applicable RNAV approach procedure chart. NOTE: Barometric VNAV guidance during approach including the approach transition, final approach segment and the missed approach procedure is not temperature compensated. Operating at uncompensated minimum IFR altitudes will not provide expected terrain and obstacle clearance for temperatures below ISA. Page 21 Section - 2 LIMITATIONS FAA Approved Revision A3: Mar 22, 2005 Hawker 800XP Pro Line 21 Airplane Flight Manual EGPWS 1. Navigation must not be predicated upon the use of the TAD. The Terrain Display is intended to serve as a situational awareness tool only and may not provide the accuracy and/or fidelity on which to solely base terrain avoidance maneuvering. 2. Pilots are authorized to deviate from their current air traffic control (ATC) clearance to the extent necessary to comply with an EGPWS warning. 3. In order to avoid giving unwanted alerts, the Terrain Awareness alerting must be inhibited by selecting the TERR INHIB switchlight when within 15 nautical miles of takeoff, approach or landing at an airport not contained in the EGPWS Airport Database. Refer to Honeywell document 060-4326-000 for airports contained in the installed EGPWS Terrain Database. 4. When the FMS is operating in the DR mode, the Terrain Awareness alerting must be inhibited by selecting the TERR INHIB switchlight. NOTE: The terrain database, displays and alerting algorithms currently account for limited cataloged human-made obstructions in North America and Europe. If obstacle data is not in the database for a particular obstacle, the Obstacle Awareness alerting is not available for that obstacle. TCAS II Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a TCAS resolution advisory. If ATC requires the transponder altitude reporting to be disabled, TCAS II must be turned off. Page 22 Section - 2 LIMITATIONS FAA Approved Revision A3: Mar 22, 2005 Hawker 800XP Pro Line 21 Airplane Flight Manual AIRSPEED LIMITATIONS Maximum Operating Speed VMO 280 KIAS (Ventral fuel tank not empty, Flaps 0°) VMO 335 KIAS (Ventral fuel tank empty, Flaps 0°) Sea Level to 12,000 ft, reducing by 1 kt per 680 ft to 310 KIAS at 29,000 ft. Maximum Operating Mach Number MMO.0.80 IMN MMO.0.73 IMN with Mach Trim System Fail/ Inoperative and Autopilot disengaged. NOTE: The maximum operating speeds and operating Mach numbers as given above shall not be deliberately exceeded in any regime of flight (climb, cruise or descent) except for the purpose of pilot training or routine test flights in accordance with Section 5, Sub-section 2 of the Pilot’s Operating Manual (POM). If the limits are inadvertently exceeded, speed shall be reduced to or below the limiting values as quickly as possible.
