Rapport D'enquête

Total Page:16

File Type:pdf, Size:1020Kb

Rapport D'enquête Parution : Décembre 2018 RAPPORT D’ENQUÊTE Incident grave survenu le 22 mai 2015 à Paris – Charles-de-Gaulle (95) au Boeing 777-F immatriculé F-GUOC exploité par Air France www.bea.aero @BEA_Aero Les enquêtes de sécurité Le BEA est l’autorité française d’enquêtes de sécurité de l’aviation civile. Ses enquêtes ont pour unique objectif l’amélioration de la sécurité aérienne et ne visent nullement la détermination des fautes ou responsabilités. Les enquêtes du BEA sont indépendantes, distinctes et sans préjudice de toute action judiciaire ou administrative visant à déterminer des fautes ou des responsabilités. 2 F-GUOC - 22 mai 2015 Table des matières LES ENQUÊTES DE SÉCURITÉ 2 SYNOPSIS 10 ORGANISATION DE L’ENQUETE 12 1 - RENSEIGNEMENTS DE BASE 13 1.1 Déroulement du vol 13 1.2 Tués et blessés 14 1.3 Dommages à l’aéronef 15 1.4 Autres dommages 15 1.5 Renseignements sur le personnel 15 1.5.1 Équipage de conduite 15 1.6 Renseignements sur l’aéronef 16 1.6.1 Cellule 16 1.6.2 Procédure d’insertion de données sur Boeing 777 (Air France) 16 1.6.3 Outil de calcul des performances (OPT) et procédures associées 20 1.6.4 Vitesses de référence calculées par le FMS 21 1.6.5 Message V SPEEDS UNAVAILABLE affiché au CDU du FMS 22 1.6.6 Optimisation de la configuration des volets au décollage 24 1.6.7 Procédure TAIL STRIKE 26 1.7 Renseignements météorologiques 26 1.8 Aides à la navigation 26 1.9 Télécommunications 26 1.10 Renseignements sur l’aérodrome 27 1.11 Enregistreurs de bord 27 1.12 Renseignements sur l’épave et sur l’impact 30 1.13 Renseignements médicaux et pathologiques 30 1.14 Incendie 30 1.15 Questions relatives à la survie des occupants 30 1.16 Essais et recherches 30 1.16.1 Simulations effectuées par Boeing 30 1.16.2 Séance de simulateur effectuée par le BEA 31 1.17 Renseignements sur les organismes et la gestion 33 1.17.1 Prise en compte du risque par Air France 33 1.17.2 Surveillance des opérations aériennes 34 1.17.3 Prise en compte du sujet des erreurs d’insertion par les autorités de l’aviation civile 37 3 F-GUOC - 22 mai 2015 1.18 Renseignements supplémentaires 48 1.18.1 Témoignages 48 1.18.2 OFP, « carton décollage » et ECD utilisés pour la préparation du vol de l’événement 55 1.18.3 Paramètres au décollage calculés par l’OPT à partir de la masse correcte et de la masse erronée 57 1.18.4 Incidents similaires sur Boeing 777-300 57 1.18.5 Étude publiée par le BEA en 2008 et intitulée “Utilisation de paramètres erronés au décollage” 58 1.18.6 Autres études internationales 60 1.18.7 Système LINTOP de calcul de performance 61 1.18.8 Fonctionnalité EFB de comparaison de la masse sur Boeing 777 61 1.18.9 Systèmes TOS et TOM d’Airbus 62 1.19 Techniques d’enquête utiles ou efficaces 62 2 - ANALYSE 63 2.1 Scénario 63 2.2 Analyse de l’événement 67 2.2.1 Performance des barrières opérationnelles dans l’événement 67 2.2.2 Mobilisation des ordres de grandeur 68 2.2.3 Compatibilité des procédures et interfaces avec l’environnement opérationnel 69 2.2.4 Vitesses de référence calculées par le FMS, message V SPEEDS UNAVAILABLE 71 2.2.5 Protection contre l’insertion de vitesses de décollage trop basses 73 2.2.6 Chronologie du décollage 73 2.2.7 Décision de poursuivre le vol 73 2.2.8 Conclusion sur l’événement 74 2.3 Gestion du risque par Air France 75 2.4 Prise en compte du risque par la DSAC 76 2.5 Gestion du risque par les autorités de l’aviation civile 77 3 - CONCLUSION 80 3.1 Faits établis par l’enquête 80 3.2 Causes et facteurs contributifs 81 4 F-GUOC - 22 mai 2015 4 - ACTIONS DE SÉCURITÉ ENTREPRISES ET RECOMMANDATIONS DE SECURITE 83 4.1 Actions de sécurité entreprises depuis l’incident grave 83 4.1.1 Actions prises par Air France 83 4.1.2 Actions prises par la DGAC 84 4.1.3 Actions prises par l’AESA 84 4.2 Recommandations de sécurité 91 4.2.1 Homogénéité des données de masses manipulées 91 4.2.2 Procédures opérationnelles 92 4.2.3 Poursuite du vol après la survenue d’un incident grave 92 4.2.4 Protections contre l’insertion de vitesses erronées sur Boeing 777 93 4.2.5 Gestion du risque par les autorités de l’aviation civile 93 ANNEXES 98 5 F-GUOC - 22 mai 2015 Glossaire AESA Agence Européenne de la Sécurité Aérienne AFM Aircraft Flight Manual (Manuel de vol) AMC Acceptable Means of Compliance (Moyens acceptables de mise en conformité) AP AutoPilot (Pilote automatique) ARMS Aviation Risk Management Solutions ARO Authority Requirement for Air Operations (Exigences applicables aux autorités en matière d’opérations aériennes) ASDA Acceleration Stop Distance Available (Longueur utilisable pour l’accélération arrêt) ASR Air Safety Report (Compte rendu de sécurité des vols) ATSB Australian Transport Safety Bureau (Organisme d’enquête de sécurité de l’Australie) BST Bureau de la Sécurité des Transports (Organisme d’enquête de sécurité du Canada) CAP Circulation Aérienne Publique CAS Calibrated Air Speed (Vitesse Conventionnelle) CASIA Civil Aviation Safety Investigation Authorities (Autorités d’enquête de sécurité de l’aviation civile) CDB Commandant de Bord CDU Control Display Unit (Tableaux de commande et d’affichage) CRM Crew Resource Management (Gestion des ressources de l’équipage) CTA Certificat de Transporteur Aérien CVR Cockpit Voice Recorder (Enregistreur phonique) DAC Directions de l’Aviation Civile DCS Direction du Contrôle de la Sécurité DGAC Direction Générale de l’Aviation Civile DSAC Direction de la Sécurité de l’Aviation Civile DSB Dutch Safety Board (Organisme d’enquête des Pays-Bas) DO Direction des Opérations (Air France) DOW Dry Operating Weight (Masse à vide en ordre d’exploitation) ECD État de Charge Définitif 6 F-GUOC - 22 mai 2015 ECR European Central Repository (Base de données européenne des événements de sécurité d’aviation civile) EFB Electronic Flight Bag (Système de documentation électronique) EICAS Engine Indication and Crew Alerting System (Système d’affichage des paramètres moteurs et des alarmes sur les deux écrans centraux du poste de pilotage) EUROCAE EURopean Organisation for Civil Aviation Equipment (Organisation européenne pour l’équipement de l’aviation civile) FAA Federal Aviation Administration (Agence américaine en charge de l’aviation civile) FCOM Flight Crew Operations Manual (Manuel d’exploitation des équipages) FCTM Flight Crew Training Manual (Manuel de formation des équipages) FDM Flight Data Monitoring (Programme de collecte de données de vol) FDR Flight Data Recorder (Enregistreur de paramètres) FL Flight Level (Niveau de vol) FMC Flight Management Computer (Calculateur de gestion de vol) FMS Flight Management System (Système de gestion du vol) FOB Fuel On Board (Quantité de carburant embarqué) FOI Flight Operation Inspector (Inspecteur en vol) FORDEC Faits Options Risques Décision Exécution Contrôles ft Feet (Pieds) GM Guidance Material (Document d’orientation) GPS Global Positioning System (Système de positionnement par satellite) GW / GR WT Gross Weight (Masse brute totale au départ) kt Knot (Nœud) LEF Livret d’Entraînement et de Formation LINTOP Lido Integrated Takeoff Performance Tool (Système de calcul de performance au décollage de Lido) LOSA Line Operations Safety Audit (Audit de sécurité des opérations en ligne) MCT Manuel de Contrôle Technique MEP Mise en Place MMS Minimum Maneuvering Speed (Vitesse minimale de manœuvre) MOPS Minimum Operational Performance Standards (Spécifications de performances opérationnelles minimales) 7 F-GUOC - 22 mai 2015 MTOW Maximum Take-Off Weight (Masse maximale au décollage) NASA National Aeronautics and Space Administration (Agence aéronautique et spatiale américaine) NOTAM Notice To AirMen (Avis aux navigants aériens) NPA Notice of Proposed Amendment (Avis de proposition de modification de réglement) NTSB National Transportation Safety Board (Organisme d’enquête de sécurité des USA) OFP Operational Flight Plan (Plan de vol exploitation) OPL Officier Pilote de Ligne OPT On-board Performance Tool (Outil de calcul des performances) ORO Organisation Requirement for Air Operators (Exigences applicables aux organismes pour les opérations aériennes) OSV Officier de Sécurité des Vols OBWBS On-Board Weight and Balance Systems (Systèmes de pesée autonomes) PA Pilote Automatique PF Pilot Flying (Pilote aux commandes) PFD Primary Flight Display (Écran de vol primaire) PIA Preliminary Impact Assessment (Analyse préliminaire d’impact) PLD PayLoad (Charge utile) PLI Pitch Limit Indicator (Indicateur de limite d’assiette) PNS Programme National de Sécurité PNT Personnel Navigant Technique PM Pilot Monitoring (Pilote non en fonction) PPV Préparation du Plan de Vol QAR Quick Access Recorder (Enregistreur de paramètres à déchargement rapide) RMT Rule Making Task (Tâche réglementaire) QRH Quick Reference Handbook QT Qualification de Type SGS Système de Gestion de la Sécurité SIB Safety Information Bulletin (Bulletin d’information de sécurité) SRM Safety Risk Management (Processus de gestion des risques de sécurité de l’AESA) 8 F-GUOC - 22 mai 2015 TAIC Transport Accident Investigation Commission (Organisme d’enquête de sécurité de Nouvelle-Zélande) TODA Take-Off Distance Available (Distance utilisable au décollage) TOGA Take-Off Go-Around (Décollage / Remise des gaz) TORA Take-Off Runway Available (Longueur de roulement au décollage utilisable) TOM Take-Off Monitoring (Système de surveillance du décollage) TOS Take-Off Securing (Système de détection d’erreurs d’insertion au décollage) TOW Take-Off Weight (Masse au décollage) TOPMS Take-Off Performance Monitoring System (Système de surveillance des performances au décollage) TRE Type Rating Examiner (Examinateur de qualification de type) TSP Tail Strike Protection (Protection contre le toucher de queue) UTC Coordinated Universal Time (Temps universel coordonné) VR Vitesse de Rotation WG Working Group (Groupe de travail) ZFW Zero Fuel Weight (Masse sans carburant) 9 F-GUOC - 22 mai 2015 n° codé : BEA2015-0225 Synopsis Heure À 10 h 25(1) (1)Sauf précision contraire, les Exploitant Air France heures figurant Nature du vol Vol cargo dans ce rapport sont exprimées en Personnes à bord CDB (PM) ; OPL (PF) ; Deux OPL de renfort heure en UTC.
Recommended publications
  • Cessna 182P ©2010 Axenty Aviation LLC Cessna 182P ©2010 Axenty Aviation LLC V SPEEDS (KIAS) EXTERIOR INSPECTION FLOODED START EXTERIOR INSPECTION Vso
    Cessna 182P ©2010 Axenty Aviation LLC Cessna 182P ©2010 Axenty Aviation LLC V SPEEDS (KIAS) EXTERIOR INSPECTION FLOODED START EXTERIOR INSPECTION Vso..........................................48 Aft Fuselage (CONT.) Master....................................ON Vs............................................53 Baggage Door..............LOCKED Throttle....................FULL OPEN Vr.......................................50-60 Fuselage.........................CHECK Stall Warning...................CLEAR Mixture................IDLE CUT OFF Vx (sea level)..........................59 Empennage Tie Down.....................REMOVE Ignition.........................ENGAGE Vx (10,000 ft.).........................63 Horiz. Stabilizer..............CHECK Leading Edge.................CHECK *When engine fires advance Vy (sea level)..........................80 Elevator..........................CHECK Left Aileron.....................CHECK mixture, retard throttle* Vy (10,000 ft.).........................73 Tail Tie-Down..............REMOVE Left Flap........................CHECK Vfe (10°)................................140 Trim Tab.........................CHECK COLD WEATHER START Vfe (10°-40°)...........................95 Rudder............................CHECK PRE-ENGINE START Vno........................................141 Antennas........................CHECK Prime.........................6-8 TIMES Vne........................................176 Horiz. Stabilizer..............CHECK Preflight...................COMPLETE Mixture......................FULL RICH
    [Show full text]
  • Guidance for the Implementation of Fdm Precursors
    EUROPEAN OPERATORS FLIGHT DATA MONITORING WORKING GROUP B SAFETY PROMOTION Good Practice document GUIDANCE FOR THE IMPLEMENTATION OF FDM PRECURSORS June 2019 Rev 02 Guidance for the Implementation of FDM Precursors | Rev 02 Contents Table of Revisions .............................................................................................................................5 Introduction ......................................................................................................................................6 Occurrence Reporting and FDM interaction ............................................................................................ 6 Precursor Description ................................................................................................................................ 6 Methodology for Flight Data Monitoring ................................................................................................. 9 Runway Excursions (RE) ..................................................................................................................11 RE01 – Incorrect Performance Calculation ............................................................................................. 12 RE02 – Inappropriate Aircraft Configuration .......................................................................................... 14 RE03 – Monitor CG Position .................................................................................................................... 16 RE04 – Reduced Elevator Authority .......................................................................................................
    [Show full text]
  • Gemini Series PFD
    Gemini Series PFD Installation/User Manual 8300-083 Rev D Table of Contents Table of Contents ............................................................................................................................... 2 Document Revision Level & Notes ................................................................................................................ 4 Instrument Installation ................................................................................................................................... 5 Mounting Considerations................................................................................................................ 5 Wiring Considerations ..................................................................................................................... 5 Pitot and Static Connections .......................................................................................................... 5 RFI/EMI Considerations .................................................................................................................. 6 Getting Acquainted With Your Gemini PFD................................................................................................. 7 Gemini PFD Display........................................................................................................................... 7 Using the Touch Screen.................................................................................................................... 8 Info Page Display...............................................................................................................................
    [Show full text]
  • Flight Deck Solutions, Technologies and Services Moving the Industry Forward Garmin Innovation Brings Full Integration to Business Flight Operations and Support
    FLIGHT DECK SOLUTIONS, TECHNOLOGIES AND SERVICES MOVING THE INDUSTRY FORWARD GARMIN INNOVATION BRINGS FULL INTEGRATION TO BUSINESS FLIGHT OPERATIONS AND SUPPORT From web-based flight planning, fleet scheduling and tracking services to integrated flight display technology, head-up displays, advanced RNP navigation, onboard weather radar, Data Comm datalinks and much more — Garmin offers an unrivaled range of options to help make flying as smooth, safe, seamless and reliable as it can possibly be. Whether you operate a business jet, turboprop or hard-working helicopter, you can look to Garmin for industry-leading solutions scaled to fit your needs and your cockpit. The fact is, no other leading avionics manufacturer offers such breadth of capability — or such versatile configurability — in its lineup of flight deck solutions for aircraft manufacturers and aftermarket upgrades. When it comes to bringing out the best in your aircraft, Garmin innovation makes all the difference. CREATING A VIRTUAL REVOLUTION IN GLASS FLIGHT DECK SOLUTIONS By presenting key aircraft performance, navigation, weather, terrain routings and so on. The map function is designed to interface with a and traffic information, in context, on large high-resolution color variety of sensor inputs, so it’s easy to overlay weather, lightning, traffic, displays, today’s Garmin glass systems bring a whole new level of terrain, towers, powerlines and other avoidance system advisories, as clarity and simplicity to flight. The screens offer wide viewing angles, desired. These display inputs are selectable, allowing the pilot to add advanced backlighting and crystal-sharp readability, even in bright or deselect overlays to “build at will” the map view he or she prefers for sunlight.
    [Show full text]
  • GSW-8 Flight Instruments
    GSW-8 Flight Instruments READING ASSIGNMENT PHAK Chapter 8 – Flight Instruments Study Questions 1. In addition to being able to read and interpret flight instruments, a pilot must also be able to a) build replacement flight instruments from spare parts. b) detect changes in altitude, airspeed, and heading using only body signals. c) recognize errors and malfunctions of these instruments during preflight inspection and in the air. Pitot-Static System 2. Impact air pressure is taken from the ___________________________________ , and ___________________________________ air pressure is usually taken from vents mounted flush with the fuselage. 3. A change in airspeed will affect the air pressure in which line of the pitot-static system? a) Static air pressure in the static line. b) Impact air pressure in the pitot line. c) Air pressure in both lines will change. 4. A change in altitude will affect the air pressure in which line of the pitot-static system? a) Static air pressure in the static line. b) Impact air pressure in the pitot line. GSW-8 c) Air pressure in both lines will change. 5. During preflight inspection, if a pilot notices a blocked or partially blocked static vent, how should it be ? resolved? a) The pilot should blow forcefully on the vent hole until the clog dislodges. b) A certificated mechanic should be notified so that he or she can remove the blockage. c) The clog will likely remove itself during slipping flight. 6. Which flight instrument uses impact pressure from the pitot line? ___________________________________________________________________________________ 7. Why do many planes have more than one static port? a) Multiple ports allow air pressure to equalize from one side of the airplane to the other.
    [Show full text]
  • Operations Circular 3 of 2011
    GOVERNMENT OF INDIA CIVIL AVIATION DEPARTMENT OFFICE OF DIRECTOR GENERAL OF CIVIL AVIATION NEW DELHI OPERATIONS CIRCULAR 3 OF 2011 AV. 22024/8/2010-FSD 21st April 2011 Subject: OPERATIONS OF AIRCRAFT AT ALTITUDES ABOVE 25,000 FEET MSL AND/OR MACH NUMBERS (MMO) GREATER THAN .75 1. PURPOSE. This circular is issued to guide pilots, particularly those who are transitioning from aircraft of lower performance capability to complex, high-performance aircraft that are capable of operating at high altitudes and high airspeeds. It is essential to have knowledge of the special physiological, engine and aerodynamic considerations involved in these operations. 2. BACKGROUND. A series of safety recommendations have required that, among other things, a minimum training curriculum be established for use at pilot schools covering pilots initial transition onto general aviation turbojet airplanes. Aerodynamics and physiological aspects of high-performance aircraft operating at high altitudes were among the subjects recommended for inclusion in this training curriculum. These recommendations were the result of a review of a series of fatal accidents which were believed to involve a lack of flightcrew knowledge and proficiency in general aviation turbojet airplanes capable of operating in a high-altitude environment. Although the near total destruction of physical evidence and the absence of installed flight recorders had prevented authorities to accurately determine the circumstances which led to these accidents, the concern that a lack of flightcrew knowledge and proficiency in the subject matter of this circular was involved in either the initial loss of control or the inability to regain control of the aircraft, or both.
    [Show full text]
  • Ac 25-15 11/20/89
    Advisory us. Departmenf of Tronsportafion Federal Aviation Circular Administration Subject: APPROVAL OF FLIGHT MANAGEMENT Date: 11/20/89 AC No: 25-15 SYSTEMS IN TRANSPORT CATEGORY Initiated by: ANM-110 Change: AIRPLANES 1. PURPOSE. This advisory circular (AC) provides guidance material for the airworthiness approval of flight management systems (FMS} in transport category airplanes. Like all AC material, this AC is not mandatory and does not constitute a regulation. It is issued for guidance purposes and to outline a method of compliance with the rules. In lieu of following this method without deviation, the applicant may elect to follow an alternate method, provided the alternate method is also found by the Federal Aviation Administration (FAA} to be an acceptable means of complying with the requirements of Part 25. Because the method of compliance presented in this AC is not mandatory, the terms II sha11" and "must II used herein apply on1y to an applicant who chooses to follow this particular method without deviation. 2. RELATED DOCUMENTS. a. Related Federal Aviation Regulations {FAR}. Portions of Part 25 and a portion of Part 121, as presently written, can be applied for the design, substantiation, and certification of FMS for transport category airplanes. Sections which prescribe requirements for these types of systems include: § 25.101 Performance: General. § 25 .103 Stalling speed. § 25.105 Takeoff. § 25.107 Takeoff speeds. § 25.109 Accelerate-stop distance. § 25.111 Takeoff path. § 25.113 Takeoff distance and takeoff run. § 25.115 Takeoff flight path. § 25.117 Climb: general. § 25.119 Landing climb: All-engines-operating. § 25.121 Climb: One-engine-inoperative.
    [Show full text]
  • CZAW Sportcruiser
    CZAW Sport Cruiser © 2012 Axenty Aviation LLC http://axenty.com CZAW Sport Cruiser © 2012 Axenty Aviation LLC http://axenty.com V - SPEEDS (KIAS) EXTERIOR INSPECTION BEFORE ENGINE START RUNUP Vso..........................................32 Left Wing Preflight Inspection..COMPLETE Canopy……CLOSED & LOCKED Vs............................................39 Flaps………………………CHECK Passenger Briefing..COMPLETE Brakes………………………….SET Vr............................................43 Ailerons……………………CHECK Safety Harness............SECURE Power…………………..2500 RPM Vx……………………………....60 Leading Edge…………….CHECK Controls……FREE & CORRECT UNTIL OIL PRESSURE Vy……………..........................65 Pitot Tube…………………CHECK Canopy…………..………CLEAN REACHES 50°C Vfe...........................................75 Static Port…………………CHECK Power…………………..4000 RPM Vno........................................108 Fuel Quantity.....................CHECK ENGINE START Ignition………..CHECK L/R/BOTH Vne........................................138 Fuel Filler Cap................SECURE MAX. DROP 300 RPM Va (1320 lbs)...........................88 Fuel Sump.........................CHECK Brakes……………………….SET MAX. DIFFERENTIAL 120 RPM Va (1025 lbs)………………….84 Main Wheel.......................CHECK Fuel Selector….FULLEST TANK Carb Heat……….........…..CHECK Best Glide……………………...60 Fuel Tank Vent..................CHECK Throttle................................IDLE Oil Temperature…………..CHECK Maximum Crosswind…………10 Choke………………….FULL ON Oil Pressure……………….CHECK Maximum Headwind………….23 Nose (HOT START – NO CHOKE)
    [Show full text]
  • Bordgeräte Flight Instruments
    Bordgeräte flight instruments Vorwort Flugüberwachungsinstrumente müssen einen sicheren Flug gewährleisten und dem Piloten die Möglichkeit geben, die Leistungen seines Flug- zeuges optimal auszunutzen. In Bezug auf Messgenauigkeit, Unempfind- lichkeit gegen störende Einflüsse (Vibrationen, Beschleunigungen, Temperaturschwankungen usw.) und Betriebssicherheit werden sehr hohe Anforderungen gestellt. Die Firma Gebr. Winter besitzt langjährige Erfahrung auf dem Gebiet der Bordgeräteherstellung und -entwick- lung. Dank sehr gut eingerichteter Prüfräume, Werkstätten für Feinmechanik und einem Stab erfahrener Spezialisten zeichnen sich Winter- Bordgeräte durch hohe Präzision und Zuverlässigkeit aus. Auf guten Service bei Nachprüfung und Überholung der Geräte wird sehr großen Wert gelegt. Der vorliegende Katalog soll einen Überblick über unser Bord- geräte-Programm geben. Wenn Sie weitergehende Informationen wünschen oder irgendwelche Probleme in Bezug auf Bord­ geräte haben, Preface wenden Sie Flight instru- sich bitte ments must an uns. ensure a safe Wir stellen flight and afford unsere the pilot the oppor- Erfahrung tunity of exploiting gerne in the capabilities of his Ihre Dienste. aircraft to the full. The requirement placed on instruments of this nature as regards measuring accuracy, insensitivity to outside influences (vibration, acceleration, fluctuations in temperature, etc.) and operational reliability are stringent in the extreme. Gebr. Winter has accumulated many years’ experience in manufacturing and developing flight instruments. Thanks to optimally equipped test facilities, instrument workshops and a staff of experienced specialists, Winter instruments have become a byword for high precision and reliability. Maximum emphasis is placed on dependable service in the after-sales inspection and overhaul of the instruments. This catalogue will give you an overview of the range of flight instruments we produce.
    [Show full text]
  • Airspeeds for Normal Operation (V Speeds (KIAS))
    NOTES Contents Normal Checklists.......................................................................1 Airspeeds for Normal Operation ...........................................1 Preflight Inspection.................................................................3 Preflight External Accessories ...........................................3 Preflight Fuel and Oil .........................................................3 Preflight Cabin ....................................................................4 Preflight Empennage ..........................................................5 Preflight Right Wing...........................................................5 Preflight Nose ......................................................................6 Preflight Left Wing .............................................................6 Before Starting Engine ...........................................................7 Starting Engine........................................................................7 Before Taxiing .........................................................................8 Taxiing......................................................................................8 Before Takeoff.........................................................................9 Normal Takeoff .....................................................................10 Short Field Takeoff ...............................................................10 Climb......................................................................................10 Cruise
    [Show full text]
  • Takeoff Safety Training Aid
    Training Aid U.S. Department of Transportation Federal Aviation Administration (This page intentionally left blank) TAKEOFF SAFETY TRAINING AID IMPORTANT - READ IF YOU DESIRE REVISION SERVICE, PLEASE FILL IN THE INFORMATION BELOW: COMPLETE ADDRESS (PLEASE TYPE OR PRINT) COMPANY NAME TITLE ADDRESS RETURN TO: BOEING COMMERCIAL AIRPLANE GROUP P.O. BOX 3707 SEATTLE, WASHINGTON 98124-2207 USA ATTN : MANAGER, AIRLINE SUPPORT CUSTOMER TR41NING AND FLIGHT OPERATIONS SUPPORT ORG. M-7661 MAIL STOP 2T-65 (This page intentionally left blank) t!! Office of the Administrator 800 IndependenceAve., S.W u.s.Defxfrtment Washington,D.C. 20591 of Transportation Federal Aviation Administration AUG13B92 Captain Chester L. Ekstrand Director, Flight Training Boeing Commercial Airplane Group P.O. BOX 3707, MS 2T-62 Seattle, WA 98124-2207 Dear Captain Ekstrand: It is a pleasure to recommend this “Takeoff Safety Training Aid” for use throughout the air carrier industry. This training tool is the culmination of a long, painstaking effort on the part of an industry/Government working group representing a broad segment of the U.S. and international air carrier community. In late 1990, the working group began studying specific cases of rejected takeoff (RTO) accidents and incidents and related human factors issues. Opportunities for making improvements to takeoff procedures and for increasing the levels of aircrew knowledge and skill were indicated. To test this hypothesis, the working group was expanded to include all major aircraft manufacturers, international carriers, and members of the academic community. The general consensus supports enhancing flight safety through widespread use of the material developed. I urge operators to adopt this material for use in qualification and recurring aircrew training programs.
    [Show full text]
  • Airplane Flying Handbook (FAA-H-8083-3B) Chapter 15
    Chapter 15 Transition to Jet-Powered Airplanes Introduction This chapter contains an overview of jet powered airplane operations. The information contained in this chapter is meant to be a useful preparation for, and a supplement to, formal and structured jet airplane qualification training. The intent of this chapter is to provide information on the major differences a pilot will encounter when transitioning to jet powered airplanes. In order to achieve this in a logical manner, the major differences between jet powered airplanes and piston powered airplanes have been approached by addressing two distinct areas: differences in technology, or how the airplane itself differs; and differences in pilot technique, or how the pilot addresses the technological differences through the application of different techniques. For airplane-specific information, a pilot should refer to the FAA-approved Airplane Flight Manual for that airplane. 15-1 Jet Engine Basics Although the propeller-driven airplane is not nearly as efficient as the jet, particularly at the higher altitudes and cruising A jet engine is a gas turbine engine. A jet engine develops speeds required in modern aviation, one of the few advantages thrust by accelerating a relatively small mass of air to very the propeller-driven airplane has over the jet is that maximum high velocity, as opposed to a propeller, which develops thrust is available almost at the start of the takeoff roll. Initial thrust by accelerating a much larger mass of air to a much thrust output of the jet engine on takeoff is relatively lower slower velocity. and does not reach peak efficiency until the higher speeds.
    [Show full text]