Boeing 777 fcom manual

In all cases, such revisions and changes must remain compatible with the approved AFM with which the operator must comply. This manual is written under the assumption that the user has had previous multi—engine jet aircraft experience and is familiar with basic jet airplane systems and basic pilot techniques common to airplanes of this type.

Therefore, the manual does not contain basic flight information that is considered prerequisite training. It also contains lists of abbreviations, a record of revisions, bulletins, and a list of effective pages.

All operating procedures are based on a thorough analysis of crew activity required to operate the airplane, and reflect the latest knowledge and experience available. Volume 2 — Chapters 1 through 15 contain general airplane and systems information.

These chapters are generally subdivided into sections covering controls and indicators and systems descriptions. The page number is divided into three fields; chapter, section, and page. An example of a page number for the hydraulics chapter follows: chapter 13, section 20, page 3. The customer document number is composed of the general FCOM number, DW—, and is followed by the customer identification. Note: An operating procedure, technique, etc.

Information contained in notes may also be safety related. The Boeing Company keeps a list of each airplane configuration as it is built and modified through the Service Bulletin process. The FCOM does not reflect customer originated modifications without special contract provisions. Special Note This FCOM contains information which has been included at the request of your airline for airplanes covered by this manual.

This information may differ from Boeing recommended information. By including this information in the manual, Boeing is providing a publishing service only and such inclusion does not imply that The Boeing Company in any way endorses or approves such information. The technical accuracy and validity of all such airline originated information, and its effect, if any, on other portions of this manual, is the sole responsibility of the airline.

The following rules are used to express airplane effectivities: 1. Airplane effectivies are listed by tail numbers in alpha-numeric order.

A range of airplanes is defined by a dash, e. A comma in the effectivity range indicates a break in the range, e. Airplane effectivities apply only to the paragraph, illustration, operational note, procedural step, etc. Note: After engine shutdown, all remaining fuel can be used for the operating engine.

Resume normal fuel management procedures. The next equivalently indented step Note: After engine shutdown When airplane effectivities are stated immediately below a checklist, the entire : checklist applies to the listed airplanes only.

Some abbreviations may also appear in lowercase letters. Abbreviations having very limited use are explained in the chapter where they are used. This revision reflects the most current information available to The Boeing Company 45 days prior to the subject revision date. Most of the panel pages in sections 1. There are no technical changes on those pages unless a revision bar appears on the page. General information below explains the use of revision bars to identify new or revised information.

Highlights in the Revision Highlights section explain the revision bar changes in this revision. Revision Record No. Revision Date Date Filed No. Revision Date 29 June 11, 30 December 10, 31 June 16, 32 December 15, 33 June 15, 34 December 14, Date Filed General The Boeing Company issues flight crew operations manual revisions to provide new or revised procedures and information. Formal revisions also incorporate appropriate information from previously issued flight crew operations manual bulletins.

The revision date is the approximate date the manual is mailed to the customer. Use the information on the new Revision Record and List of Effective Pages to verify the manual content. Pages containing revised technical material have revision bars associated with the changed text or illustration. Highlights in the Revision Highlights section provide descriptions of the changes identified by the revision bars.

Editorial revisions for example, spelling corrections may have revision bars with no associated highlight. Remove corresponding old pages and replace or add new pages. Be careful when inserting changes not to throw away pages from the manual that are not replaced. Using the List of Effective Pages 0. After the revision has been filed into the manuals, the revision number, revision date and the date the revision was filed should be recorded in the Revision Record table above by the person that filed the revision.

Revision Highlights This section 0. Throughout the manual, airplane effectivity may be updated to reflect coverage as listed on the Preface - Model Identification page, or to show service bulletin airplane effectivity.

Highlights for these airplane effectivity updates are not supplied. Occasionally, because the editors rearrange the database markers, or mark items with configuration information due to the addition of new database content, some customers may receive revision bars on content that appears to be unchanged. Pages may also be republished without revision bars due to slight changes in the flow of the document.

Chapter 0 - Preface Section 2 - Introduction General 0. Section 6 - Bulletin Record 0. Doors SP. Navaid Inhibit SP. Takeoff Field Corrections PD. Takeoff Speeds PD. Section 14 - Text Takeoff PD. Section 24 - Text Takeoff PD. Section 34 - Text Takeoff PD. Entry Door 1. Overwing Emergency Exit Door 1. No longer applicable to fleet configuration. Section 40 - Systems Description Lighting Systems 1. Master Brightness Control System 1. No technical change. Cabin Signs 1.

Passenger Airplane 1. Portable Oxygen Bottles 1. Crew Rest Smoke Detection System 1. Entrance Enclosure Control Panel 1. Entry Doors 1. Overwing Escape Slide 1. Emergency Exit Operation 1. Bleed Air System 2. Anti—Ice Indications 3. Directory Page [Typical] 5.

Category Numbers Page [Typical] 5. Oil Quantity Indications 7. Compact Engine Indications 7. APU Controls 7. Non—Normal Flight Control Synoptic 9. Information from the remarks section is already included in chapter Video Surveillance Typical FMC Position Update Takeoff and Climb Manual entries are allowed. Calculated Step Climb Reference Navigation Data Page Section 20 - System Description Introduction These non-technical editorial changes result in some revision bars being displayed on some pages without a respecitive highlight, even though the text or content has not been revised.

Takeoff Configuration Warnings Crew Alertness Monitor Added inhibits previously omitted. Introduction Altitude Voice Annunciations During Approach Alerts Inhibited During Takeoff The text may be unchanged from previous revisions.

Alerts Inhibited During Landing The transmitted information may be of interest to only specific Operators or may apply to all Operators of this model airplane. Each bulletin will vary. Bulletins are dated and numbered sequentially. Each bulletin identifies airplanes affected by the bulletin.

When appropriate, the next formal Flight Crew Operations Manual revision will include an updated bulletin record page to reflect current bulletin status.

All bulletins previously cancelled are no longer listed in the Bulletin Record. The person filing a new or revised bulletin should amend the Bulletin Record as instructed in the Administrative Information section of the bulletin. The following changes have taken place since index dated June 15, Bulletin No. Discard bulletin SIA R Added corrective action information. Information in this bulletin is recommended by The Boeing Company, but may not be FAA approved at the time of writing.

EgyptAir Boeing aircraft cockpit fire. AT Cairo Airport. On 29 th Aircraft General Information. Boeing publishes a recommended all- engine normal takeoff procedure in the. MD, and DC models. Jul 3, An overweight landing is defined as a landing made at a gross weight in excess of the maximum design. A pilot may consider making an overweight landing when a situation arises that requires the airplane to return to the takeoff airport or divert to another airport soon Apr 27, Oct 18, Boeing Upper Crew Rest Compartment.

Flight Crew Operating Manual. Flight Crew Training Manual. Universal Time Coordinate. Jan 3, The landing distance is measured from the point at which the main landing gear of the aircraft is 50 feet. Photo: The Boeing Company. Sep 5, Make and Model: Boeing H. Place of Occurrence: Dubai International Airport. State of Flight crew operations manual. Flight crew training manual. Flight director.

Flight hours. Flight management system. Mar 17, Typical manual set. Does not include maintenance logs. Nov 12, User's Manual. November Ultimate Legal Stuff. This manual was developed for use only with the QualityWings Simulations. The shares a Boeing aircraft configured for landing is ob- tained using a structured overset grid process and the