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关于FPPM简述?

 zhanghe1011 2019-09-06

愿你经历再多,都不忘初心;

愿你难过再多,都不忘微笑;

愿你能披荆斩棘,做到自己想要做到的事

FPPM是指波音飞行计划与性能手册,此手册中包含了完整的航空器运行性能数据,其中包含放行数据和飞行中的数据,这些数据根据不同的构型、发动机型号。

 


这个手册根据不同的机型、构型来划分。
This Flight Planning and Performance Manual has been prepared by Boeing Commercial Airplanes, Commercial Aviation  Services. The purpose of this manual is to provide a complete operational performance data reference including dispatch and inflight performance data applicable to a specific airframe, engine rating, and regulatory agency as identified on the cover page  of the document.

本飞行计划和性能手册由波音商用飞机、商用航空服务公司编写。本手册的目的是提供一个完整的运行性能数据参考,包括适用于特定机身、发动机额定和监管机构的调度和飞行性能数据,如文件封面所示。

This manual is suitable for use for any airplane configuration that meets the criteria identified on the cover page of the document.

本手册适用于任何符合文件封面所列标准的飞机配置。

Owners/operators are solely responsible for ensuring the performance documentation they are using is complete and matches the current configuration identified on the cover page of the document. This includes the accuracy and validity of all information furnished by the owner/operator or any other party.

在FPPM手册的所有者/运行人只负责确保他们正在使用的性能文档是完整的,并且与文档封面上标识的当前配置相匹配。这包括所有者/运行者或任何其他方面提供的所有资料的准确性和有效性。

The manual is periodically revised to incorporate pertinent flight planning and performance information. Items of a more critical nature will be incorporated in Flight Planning and Performance Manual Bulletins and will be distributed in a timely manner.

手册定期修订,纳入有关飞行计划和性能信息。更为关键的项目将列入飞行计划和性能手册公报,并将及时分发。

 In all cases, such revisions and changes must remain compatible with the approved AFM with which the operator must comply. In the event of conflict with the AFM, the AFM shall supersede.
This manual assumes the user is familiar with basic jet airplane performance and regulatory requirements common to airplanes of this type.

在所有情况下,这些修订和变更必须与经批准的AFM保持一致,操作员必须遵守AFM。如与AFM发生冲突,AFM应予以取代。本手册假定用户熟悉这类飞机的基本喷气式飞机性能和常见的法规要求。

 
一、基本内容?
在FPPM手册中基本包含四个内容:
1)起飞落地 take off and landing
This chapter contains data to determine takeoff and landing performance limitations, based on engine bleed effects for normal air conditioning operation and antiice off, i.e., two packs at normal flow, one pack bleed from each engine.

在这一章节,包含了起飞和落地的性能限制,这些数据基于发动机空调引气、防冰关,两个组件正常流量,每个组件引气来自每个发动机。

The data is presented in simplified form and is therefore conservative. In the event of any conflict between data presented in this section and those contained in the approved Airplane Flight Manual, the Flight Manual shall always take precedence.

数据以简化的形式表示,因此是保守的。本节所列数据与经批准的飞机飞行手册所载数据发生冲突时,应始终以飞行手册为准。

 

起飞限重是场长限重、爬升限重、障碍物限重、胎速限制、刹车能量限制和结构限制的最小值。

The maximum brake release weight is the least of the field length, climb, obstacle, tire speed, brake energy and structural limit weights.

在起飞和落地这个章节中,主要内容都是起飞的场长限制、爬升限制、刹车能量等数据和表格,还有一个备用的减推力(24K、22K)的起飞性能数据限制、推力设定、起飞速度、配平设定等的性能数据。

 


 
2)飞行计划?
This chapter contains flight planning data to determine trip fuel/time, reserve fuel and enroute terrain clearance capability. The data includes engine bleed effects for normal air conditioning operation, i.e. two packs at normal flow, one pack bleeding each engine.

本章包含飞行计划数据,以确定行程燃料/时间,储备燃料和途中越障能力。数据包括正常空调运行时的发动机引气,即正常流量下两组,每台发动机一组引气。

在这章节可以查找到一些很关键的数据,例如,地面运行耗油、APU耗油、复飞、下降、爬升耗油数据:

 


 
同时也可以看到飘降、ETOPS运行的飞行计划数据:
 


 
3)航路运行数据
This chapter contains inflight data for use as general reference in airplane performance monitoring, flight planning studies and as a supplement to information provided in the Operations Manual。

本章载有飞行数据,作为飞机性能监测、飞行计划研究的一般参考,并作为《操作手册》所载资料的补充,且包括双发动机和单发动机不工作时的数据。在这一章节包含巡航、航路爬升、下降、盘旋等待,以及当单发失效时不同速度下的高度、巡航、油耗等数据,其中还包含备降时的耗油。

 


4)非标准构型数据

此章节主要包括非标准构型的一些数据,例如起落架放下时的起飞、着陆、越障、飘降等等性能数据,也包含一发失效且起落架不能收起时的相关数据。

除此之外,还有一个备用EEC模式:
This section contains performance data for airplane operation with the Electronic Engine Control (EEC) in alternate mode (ALTN & EEC switch illuminated) for applicable thrust ratings. The data includes engine bleed effects for normal air conditioning operation i.e., two packs on at normal flow, all engines operating.Operation with derated and/or assumed temperature reduced takeoff thrust is not permitted with the EEC in the alternate mode.

本节包含电子发动机控制(EEC)在备用模式(ALTN和EEC开关照明)下飞机运行的性能数据,用于适用的推力额定值。数据包括正常空调运行时的发动机引气效果。,在正常流量下打开两个包,所有引擎都在工作。在备用模式下,不允许在降低和/或假设温度下降低起飞推力的情况下运行。

To Be Continued.......

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