PFTL 101BE-10.0处理器卡件
北纬在西经50°以东和东经70°以西是可接受的。除东经120°和东经165°之间的45°外，可在南纬70°运行。必须使用符合AC 20-130A、AC 91-49和AC 120-33标准的WGS-84坐标参考基准。卫星导航数据仅基于美国运营的全球定位系统（GPS）。5.基于FMS的仪表进近必须按照从FMS-6000数据库中检索的经批准的仪表进程程序完成。仪表进近必须在进近模式下进行，并且GPS完整性监测（RAIM）必须在最终进近修复时可用。未授权使用FMS完成ILS、LOC、LOC-BC、LDA和SDF进近。当适用的操作规则要求备降机场时，必须通过基于GPS导航以外的进近为其提供服务，飞机必须具有能够使用该导航辅助的操作设备，并且所需的导航辅助必须可操作。如果VHF导航接收机调谐到参考设施，则可以飞行从导航数据库检索到的具有RNVxxx进近名称的基于FMS的进近。6.如果FMS接收到足够的可用传感器输入，则已证明其能够并已证明符合：根据AC 20-130A的标准，VFR/IFR航路RNAV运行的精度规范。根据AC 20-130A，当与柯林斯故障检测和排除软件、双柯林斯FMS-6000飞行管理系统和双GPS-4000A接收机或单台FMS-6000航班管理系统和/或柯林斯GPS-4000A接收器一起在经批准的单GPS导航路线上运行时，海洋和偏远空域的GPS主要导航手段。这不构成运营批准。注：对于单一飞行管理系统的操作，操作程序和性能数据必须参考飞机飞行手册。第1页，共1页P/N 140-590032-005TC12（第2期）11月8日，2005临时变更P/N 140-590032-005TC12（第2期）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-航空电子限制以下附加信息适用于第19页的飞行管理系统：P-RNAV，前提是FMS接收到足够的可用传感器输入，根据JAA临时指导材料第10号传单，它已被证明能够并已被证明符合欧洲P-RNAV空域运行的精度规范，前提是以下设备可操作：数量描述2.CDU-6200控制显示器第一单元。DBU-4100数据库第二单元。VIR-432/NAV-4000/NAV-4500导航接收器（列出的任何2个）2.DME-442/DME-4000 DME收发器（列出的任意2个）2.GPS-4000A全球定位系统这不构成操作批准。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。修订了欧洲P-RNAV空域运行所需的运行设备安装。从第2节-限制第19页中删除并销毁2005年1月7日的现有临时变更12第1页，共1页。将本临时变更12（第2期）第1页（共1页）插入第2节“限制”中的第19页。第1页，共1页P/N 140-590032-005TC15 2005年12月15日临时更改P/N 140-599032-005TC5受影响的出版物：受影响的飞机序列号：更改描述：填写说明：第2节-限制航空电子限制自动驾驶在旋转高度预选器控制时不要按下垂直模式飞行指引按钮（FLC、VNAV或VS）。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飞机的最新版本。Hawker 800XP 258541、258556、258567及更高版本。自动驾驶飞行指引仪限制。将本临时变更第1页（共1页）插入第2节-限制，Hawker 800XP Pro Line 21飞机飞行手册第19页第2节限制FAA批准的修订版A1:2002年11月13日根据AC 90-96和AC 20-130A在欧洲B-RNAV/RNP-5空域运行。
North latitude is acceptable East of 50° West longitude and West of 70° East longitude.Operation to 70° South latitude is acceptable except for the 45° between 120° East and 165° East longitude.The WGS-84 coordinate reference datum in accordance with the criteria of AC 20-130A, AC 91-49, and AC 120-33 must be used. Satellite navigation data is based upon use of only the Global Positioning System (GPS) operated by the United States. 5. FMS-based Instrument approaches must be accomplished in accordance with approved instrument approach procedures that are retrieved from the FMS-6000 data base.Instrument approaches must be conducted in the approach mode and GPS integrity monitoring (RAIM) must be available at the Final Approach Fix.Accomplishment of ILS, LOC, LOC-BC, LDA and SDF approaches are not authorized utilizing the FMS.When an alternate airport is required by the applicable operating rules, it must be served by an approach based on other than GPS navigation, the airplane must have operational equipment capable of using that navigation aid, and the required navigation aid must be operational.FMS based approaches that are retrieved from the navigation database with an approach name of RNVxxx may be flown provided the VHF navigation receiver is tuned to the reference facility. 6. 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:VFR/IFR enroute RNAV operation in accordance with the criteria of AC 20-130A.GPS primary means of navigation in oceanic and remote airspace in accordance with AC 20-130A, when used in conjunction with the Collins Fault Detection and Exclusion software, dual Collins FMS-6000 Flight Management Systems and dual GPS-4000A receivers or a single FMS-6000 Flight Management System and/or Collins GPS-4000A receiver when operating on routes approved for single GPS navigation. This does not constitute an operational approval. NOTE: With single Flight Management System operation, cross reference must be made to the Airplane Flight Manual for operating procedures and performance data. Page 1 of 1 P/N 140-590032-0005TC12 (Issue 2) November 8, 2005 TEMPORARY CHANGE P/N 140-590032-0005TC12 (Issue 2) PUBLICATION AFFECTED: AIRPLANE SERIAL NUMBERS AFFECTED: DESCRIPTION OF CHANGE: FILING INSTRUCTIONS: SECTION 2 - LIMITATIONS AVIONICS LIMITATIONS The following additional information applies to the Flight Management System on Page 19: P-RNAV 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 Operation in European P-RNAV airspace in accordance with JAA Temporary Guidance Material, Leaflet No. 10, provided the following equipment is operational: Quantity Description 2 .CDU-6200 Control Display Unit 1 .DBU-4100 Data Base Unit 2 .VIR-432 / NAV-4000 / NAV-4500 Navigation Receiver (any 2 of the listed) 2 .DME-442 / DME-4000 DME Transceiver (any 2 of the listed) 2 .GPS-4000A Global Positioning System This does not constitute an operational approval. 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. Revised the required operational equipment installation for operations in European P-RNAV airspace. Remove and destroy existing Temporary Change 12 Page 1 of 1 dated January 7, 2005 from Section 2 - LIMITATIONS Page 19. Insert this Temporary Change 12 (Issue 2) Page 1 of 1 to face page 19 in Section 2 - LIMITATIONS. Page 1 of 1 P/N 140-590032-0005TC15 December 15, 2005 TEMPORARY CHANGE P/N 140-590032-0005TC15 PUBLICATION AFFECTED: AIRPLANE SERIAL NUMBERS AFFECTED: DESCRIPTION OF CHANGE: FILING INSTRUCTIONS: SECTION 2 - LIMITATIONS AVIONICS LIMITATIONS Autopilot Do not push a vertical mode Flight Director button (FLC, VNAV or VS) while the altitude preselector control is being rotated. FAA Approved Airplane Flight Manual, P/N 140-590032-0005, Dated Nov 30, 2001, or latest revision for Hawker 800XP airplanes equipped with Pro Line 21 avionics. Hawker 800XP 258541, 258556, 258567 and After. Autopilot Flight Director Limitation. Insert this Temporary Change Page 1 of 1 to face Page 19 in Section 2 - LIMITATIONS, Hawker 800XP Pro Line 21 Airplane Flight Manual Page 19 Section - 2 LIMITATIONS FAA Approved Revision A1: Nov 13, 2002Operation in European B-RNAV/RNP-5 airspace in accordance with AC 90-96 and AC 20- 130A.
