787 Airplane Characteristics For Airport Planning
PRELIMINARY INFORMATION787Airplane Characteristics forAirport PlanningBoeing Commercial AirplanesD6-58331APRIL 2006 i
PRELIMINARY INFORMATION787 AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNINGLIST OF ACTIVE PAGESPageDateOriginal1 to 110April 2006Updated75 to 96October 2006PageDateD6-58331iiOCTOBER 2006PageDate
PRELIMINARY INFORMATIONTABLE OF CONTENTSSECTIONTITLEPAGE1.01.11.21.3SCOPE AND INTRODUCTIONScopeIntroductionA Brief Description of the 787 Family of Airplanes12342.02.12.22.32.42.52.62.7AIRPLANE DESCRIPTIONGeneral CharacteristicsGeneral DimensionsGround ClearancesInterior ArrangementsCabin Cross-SectionsLower Cargo CompartmentsDoor Clearances5689101315163.03.13.23.33.4AIRPLANE PERFORMANCEGeneral InformationPayload/Range for Long-Range CruiseF.A.R. Takeoff Runway Length RequirementsF.A.R. Landing Runway Length Requirements21222325334.04.14.24.34.44.54.6GROUND MANEUVERINGGeneral InformationTurning RadiiClearance RadiiVisibility from Cockpit in Static PositionRunway and Taxiway Turn PathsRunway Holding Bay373839404142475.05.15.25.35.45.55.65.7TERMINAL SERVICINGAirplane Servicing Arrangement - Typical TurnaroundTerminal Operations - Turnaround StationTerminal Operations - En Route StationGround Servicing ConnectionsEngine Start RequirementsConditioned Air Flow RequirementsGround Towing Requirements4951525354565760D6-58331APRIL 2006 iii
PRELIMINARY INFORMATIONTABLE OF CONTENTS (CONTINUED)SECTIONTITLEPAGE6.06.16.2JET ENGINE WAKE AND NOISE DATAJet Engine Exhaust Velocities and TemperaturesAirport and Community AVEMENT DATAGeneral InformationLanding Gear FootprintMaximum Pavement LoadsLanding Gear Loading on PavementFlexible Pavement Requirements - U.S. Army Corps ofEngineers Method (S-77-1)Flexible Pavement Requirements - LCN MethodRigid Pavement Requirements Portland Cement Association Design MethodRigid Pavement Requirements - LCN ConversionRigid Pavement Requirements - FAA MethodACN/PCN Reporting System - Flexible and Rigid Pavements8.0FUTURE 787 DERIVATIVE AIRPLANES979.0SCALED 787 DRAWINGS997.67.7D6-58331ivAPRIL 2006828486889193
PRELIMINARY INFORMATION1.0 SCOPE AND INTRODUCTION1.1Scope1.2Introduction1.3A Brief Description of the 787 Family of AirplanesD6-58331APRIL 20061
PRELIMINARY INFORMATION1.0SCOPE AND INTRODUCTION1.1 ScopeThis document provides, in a standardized format, airplane characteristics data for general airportplanning. Since operational practices vary among airlines, specific data should be coordinated withthe using airlines prior to facility design. Boeing Commercial Airplanes should be contacted for anyadditional information required.Content of the document reflects the results of a coordinated effort by representatives from thefollowing organizations:zAerospace Industries AssociationzAirports Council International - North AmericazAir Transport Association of AmericazInternational Air Transport AssociationThe airport planner may also want to consider the information presented in the "Commercial AircraftDesign Characteristics – Trends and Growth Projections," available from the US AIA, 1250 Eye St.,Washington DC 20005, for long-range planning needs. This document is updated periodically andrepresents the coordinated efforts of the following organizations regarding future aircraft growthtrends:zInternational Coordinating Council of Aerospace Industries AssociationszAirports Council International - North American and World OrganizationszAir Transport Association of AmericazInternational Air Transport AssociationD6-583312APRIL 2006
PRELIMINARY INFORMATION1.2 IntroductionThis document conforms to NAS 3601. It provides characteristics of the Boeing Model 787 airplanefor airport planners and operators, airlines, architectural and engineering consultant organizations,and other interested industry agencies. Airplane changes and available options may alter modelcharacteristics; the data presented herein reflect typical airplanes in each model category.For additional information contact:Boeing Commercial AirplanesP.O. Box 3707Seattle, Washington 98124-2207U.S.A.Attention: Manager, Airport TechnologyMail Code 67-KRD6-58331APRIL 20063
PRELIMINARY INFORMATION1.3 A Brief Description of the 787 Family of AirplanesThe 787 is a family of twin-engine airplanes, very fuel efficient and with exceptional environmentalperformance. The 787 airplanes are being developed by an International team of aerospacecompanies, led by Boeing at its Everett Facility near Seattle, Washington. Using a suite of newtechnologies, as much as 50 percent of the primary structure will be composite materials.787-8The 787-8 is the first airplane in the 787 family of twin-engine airplanes and is designed for mediumto long range flights. The 787-8 can carry 210 to 250 passengers in a three-class configuration andup to 375 passengers in a single-class configuration.787 EnginesGeneral Electric and Rolls-Royce have been selected to develop engines using advanced enginetechnology for increased efficiency for the 787 airplane.Cargo HandlingThe lower lobe cargo compartments can accommodate a variety of containers and pallets now usedin narrow-body and wide-body airplanes.Ground ServicingThe 787 has ground service connections compatible with existing ground service equipment, and nospecial equipment is necessary.D6-583314APRIL 2006
PRELIMINARY INFORMATION2.0 AIRPLANE DESCRIPTION2.1General Characteristics2.2General Dimensions2.3Ground Clearances2.4Interior Arrangements2.5Cabin Cross Sections2.6Lower Cargo Compartments2.7Door ClearancesD6-58331APRIL 20065
PRELIMINARY INFORMATION2.0 AIRPLANE DESCRIPTION2.1 General CharacteristicsMaximum Design Taxi Weight (MTW). Maximum weight for ground maneuver as limited byaircraft strength and airworthiness requirements. (It includes weight of taxi and run-up fuel.)Maximum Design Takeoff Weight (MTOW). Maximum weight for takeoff as limited by aircraftstrength and airworthiness requirements. (This is the maximum weight at start of the takeoff run.)Maximum Design Landing Weight (MLW). Maximum weight for landing as limited by aircraftstrength and airworthiness requirements.Maximum Design Zero Fuel Weight (MZFW). Maximum weight allowed before usable fuel andother specified usable agents must be loaded in defined sections of the aircraft as limited by strengthand airworthiness requirements.Spec Operating Empty Weight (OEW). Weight of structure, powerplant, furnishing systems,unusable fuel and other unusable propulsion agents, and other items of equipment that are consideredan integral part of a particular airplane configuration. Also included are certain standard items,personnel, equipment, and supplies necessary for full operations, excluding usable fuel and payload.Maximum Structural Payload. Maximum design zero fuel weight minus operational empty weight.Maximum Seating Capacity. The maximum number of passengers specifically certificated oranticipated for certification.Maximum Cargo Volume. The maximum space available for cargo.Usable Fuel. Fuel available for aircraft propulsion.D6-583316 APRIL 2006
PRELIMINARY INFORMATIONENGINE MANUFACTURERCHARACTERISTICSUNITSMAX DESIGNGENERAL UNDS340,000340,000KILOGRAMS154,221154,221SPEC OPERATINGPOUNDS240,000240,000EMPTY WEIGHT (1)KILOGRAMS108,862108,862MAX 9TAXI WEIGHTMAX DESIGNTAKEOFF WEIGHTMAX DESIGNLANDING WEIGHTMAX DESIGN ZEROFUEL WEIGHTPAYLOADSEATINGCAPACITYMAX CARGO- LOWER DECKUSABLE FUELNOTES:ONE-CLASS375 ALL-ECONOMY SEATS; EXIT LIMIT 440 SEATSMIXED CLASS224 THREE-CLASS; 12 FIRST CLASS, 42 BUSINESS CLASS,170 ECONOMY CLASS (SEE SEC 2.4)CUBIC FEET4,826 (2)4,826 (2)CUBIC METERS136.7 (2)136.7 (2)US 38224,638KILOGRAMS101,894101,894(1) SPEC WEIGHT FOR TYPICAL ENGINE/WEIGHT CONFIGURATION SHOWNTYPICAL OPERATING EMPTY WEIGHT SHOWN. ACTUAL WEIGHT WILLDEPEND ON SPECIFIC AIRLINE CONFIGURATION.(2) 16 LD3 CONTAINERS IN FWD COMPARTMENT AT 158 CU FT (4.5 CU M) EACH ; 12 LD3CONTAINERS IN AFT COMPARTMENT; 402 CU FT (11.4 CU M) IN BULK CARGO COMPARTMENT.SEE SEC 2.6 FOR OTHER LOADING COMBINATIONS.2.1 GENERAL CHARACTERISTICSMODEL 787-8D6-58331APRIL 20067
PRELIMINARY INFORMATION2.2GENERAL DIMENSIONSMODEL 787-8D6-583318 APRIL 2006
PRELIMINARY INFORMATIONNOMINAL (1)FEET - INCHESMETERSA25 - 37.70B14 - 24.32C8 - 02.44D5 - 91.75E14 - 74.45F (GE ENGINES)2 - 50.74F (RR ENGINES)2 - 40.71G15 - 44.67H9 - 22.79J25 - 27.67K9 - 62.90L15 - 104.83M23 - 57.13N55 - 616.92NOTES:2.31.NOMINAL DIMENSIONS BASED ON A STATIC AIRPLANE.2.DURING ROUTINE SERVICING, THE AIRPLANE REMAINS RELATIVELY STABLE,PITCH AND ELEVATION CHANGES OCCURRING SLOWLY.GROUND CLEARANCESMODEL 787-8D6-58331APRIL 20069
PRELIMINARY INFORMATION2.4.1 INTERIOR ARRANGEMENTS – LONG-RANGE CONFIGURATIONSMODEL 787-8D6-5833110 APRIL 2006
A AAAAA APRELIMINARY INFORMATION2.4.2 INTERIOR ARRANGEMENTS – SHORT-TO-MEDIUM-TO-LONG RANGEMODEL 787-8D6-58331APRIL 200611
PRELIMINARY INFORMATION2.4.3 INTERIOR ARRANGEMENTS – SHORT-TO-MEDIUM RANGEMODEL 787-8D6-5833112 APRIL 2006
PRELIMINARY INFORMATION2.5.1 CABIN CROSS-SECTIONS – FIRST CLASS AND BUSINESS CLASS SEATSMODEL 787-8D6-58331APRIL 200613
PRELIMINARY INFORMATION2.5.2 CABIN CROSS-SECTIONS - ALTERNATE SEATING ARRANGEMENTSMODEL 787-8D6-5833114 APRIL 2006
PRELIMINARY INFORMATION2.6 LOWER CARGO COMPARTMENTS – CONTAINERS AND BULK CARGOMODEL 787-8D6-58331APRIL 200615
PRELIMINARY INFORMATIONDOOR NAMEDOOR LOCATIONDOOR CLEAR OPENING1MAIN ENTRY/SERVICE DOOR NO 1 (2)LEFT AND RIGHT42 IN x 72 IN (1.07 x 1.83 M)2MAIN ENTRY/SERVICE DOOR NO 2 (2)LEFT AND RIGHT42 IN x 72 IN (1.07 x 1.83 M)3EMERGENCY EXIT DOOR NO 3LEFT AND RIGHT36 IN x 74 IN (0.91 x 1.88 M)4MAIN ENTRY/SERVICE DOOR NO 4 (2)LEFT AND RIGHT42 IN x 72 IN (1.07 x 1.83 M)5FORWARD CARGO DOORRIGHT106 IN x 67 IN (2.69 x 1.70 M)6AFT CARGO DOORRIGHT106 IN x 67 IN (2.69 x 1.70 M)7BULK CARGO DOORLEFT40 IN x 45 IN (1.02 x 1.14 M)NOTES:(1)SEE SEC 2.3 FOR DOOR SILL HEIGHTS(2)ENTRY DOORS LEFT SIDE, SERVICE DOORS RIGHT SIDE2.7.1 DOOR LOCATIONS AND SIZES - PASSENGER AND CARGO DOORSMODEL 787-8D6-5833116 APRIL 2006
PRELIMINARY INFORMATION2.7.2 DOOR CLEARANCES – MAIN DECK ENTRY AND SERVICE DOORSMODEL 787-8D6-58331APRIL 200617
PRELIMINARY INFORMATION2.7.3 DOOR CLEARANCES – LOWER DECK CARGO DOORMODEL 787-8D6-5833118 APRIL 2006
PRELIMINARY INFORMATION2.7.4 DOOR CLEARANCES - BULK CARGO DOORMODEL 787-8D6-58331APRIL 200619
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PRELIMINARY INFORMATIONSECTION 3.0 – AIRPLANE PERFORMANCE(Pages 21 – 36)CURRENTLY UNDERGOING REVISIOND6-58331JUNE 200621 thru 36
PRELIMINARY INFORMATION4.0 GROUND MANEUVERING4.1General Information4.2Turning Radii4.3Clearance Radii4.4Visibility From Cockpit in Static Position4.5Runway and Taxiway Turn Paths4.6Runway Holding BayD6-58331APRIL 200637
PRELIMINARY INFORMATION4.0 GROUND MANEUVERING4.1 General InformationThis section provides airplane turning capability and maneuvering characteristics.For ease of presentation, these data have been determined from the theoretical limits imposed by thegeometry of the aircraft, and where noted, provide for a normal allowance for tire slippage. As such,they reflect the turning capability of the aircraft in favorable operating circumstances. These datashould be used only as guidelines for the method of determination of such parameters and for themaneuvering characteristics of this aircraft.In the ground operating mode, varying airline practices may demand that more conservative turningprocedures be adopted to avoid excessive tire wear and reduce possible maintenance problems.Airline operating procedures will vary in the level of performance over a wide range of operatingcircumstances throughout the world. Variations from standard aircraft operating patterns may benecessary to satisfy physical constraints within the maneuvering area, such as adverse grades, limitedarea, or high risk of jet blast damage. For these reasons, ground maneuvering requirements shouldbe coordinated with the using airlines prior to layout planning.Section 4.2 shows turning radii for various nose gear steering angles. Radii for the main and nosegears are measured from the turn center to the outside of the tire.Section 4.3 provides data on minimum width of pavement required for 180o turn.Section 4.4 shows the pilot’s visibility from the cockpit and the limits of ambinocular vision throughthe windows. Ambinocular vision is defined as the total field of vision seen simultaneously by botheyes.Section 4.5 shows approximate wheel paths of a 787 on runway to taxiway, and taxiway to taxiwayturns.Section 4.6 illustrates a typical runway holding bay configuration.D6-5833138APRIL 2006
PRELIMINARY INFORMATIONNOTES: * ACTUAL OPERATING TURNING RADII MAY BE GREATER THAN SHOWN.* CONSULT WITH AIRLINE FOR SPECIFIC OPERATING PROCEDURESTEERINGANGLE(DEG)R-1R-2R-3R-4R-5R-6INNER GEAROUTER GEARNOSE GEARWING 11.033.84.2.1 TURNING RADII - NO SLIP ANGLEMODEL 787-8D6-58331APRIL 200639
PRELIMINARY XYAR3FTMFTMFTM74.822.834.910.6138.342.24.3 CLEARANCE RADIIMODEL 787-8D6-5833140APRIL .335.1
PRELIMINARY INFORMATION4.4 VISIBILITY FROM COCKPIT IN STATIC POSITIONMODEL 787-8D6-58331APRIL 200641
PRELIMINARY INFORMATION4.5.1 RUNWAY AND TAXIWAY TURNPATHS - RUNWAY-TO-TAXIWAY,MORE THAN 90-DEGREE TURNMODEL 787-8D6-5833142APRIL 2006
PRELIMINARY INFORMATION4.5.2 RUNWAY AND TAXIWAY TURNPATHS - RUNWAY-TO-TAXIWAY, 90-DEGREE TURNMODEL 787-8D6-58331APRIL 200643
PRELIMINARY INFORMATION4.5.3 RUNWAY AND TAXIWAY TURNPATHS - TAXIWAY-TO-TAXIWAY,90-DEGREE TURN, NOSE GEAR TRACKS CENTERLINEMODEL 787-8D6-5833144APRIL 2006
PRELIMINARY INFORMATION4.5.4 RUNWAY AND TAXIWAY TURNPATHS - TAXIWAY-TO-TAXIWAY,90-DEGREE TURN, COCKPIT TRACKS CENTERLINEMODEL 787-8D6-58331APRIL 200645
PRELIMINARY INFORMATION4.5.5 RUNWAY AND TAXIWAY TURNPATHS - TAXIWAY-TO-TAXIWAY,90-DEGREE TURN, JUDGMENTAL OVERSTEERINGMODEL 787-8D6-5833146APRIL 2006
PRELIMINARY INFORMATION4.6 RUNWAY HOLDING BAYMODEL 787-8D6-58331APRIL 200647
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PRELIMINARY INFORMATION5.0 TERMINAL SERVICING5.1Airplane Servicing Arrangement - Typical Turnaround5.2Terminal Operations - Turnaround Station5.3Terminal Operations - En Route Station5.4Ground Servicing Connections5.5Engine Starting Pneumatic Requirements5.6Ground Pneumatic Power Requirements5.7Conditioned Air Requirements5.8Ground Towing RequirementsD6-58331APRIL 2006 49
PRELIMINARY INFORMATION5.0 TERMINAL SERVICINGDuring turnaround at the terminal, certain services must be performed on the aircraft, usually withina given time, to meet flight schedules. This section shows service vehicle arrangements, schedules,locations of service points, and typical service requirements. The data presented in this sectionreflect ideal conditions for a single airplane. Service requirements may vary according to airplanecondition and airline procedure.Section 5.1 shows typical arrangements of ground support equipment during turnaround. As noted,if the auxiliary power unit (APU) is used, the electrical, air start, and air-conditioning servicevehicles would not be required. Passenger loading bridges or portable passenger stairs could be usedto load or unload passengers.Sections 5.2 and 5.3 show typical service times at the terminal. These charts give typical schedulesfor performing service on the airplane within a given time. Service times could be rearranged to suitavailability of personnel, airplane configuration, and degree of service required.Section 5.4 shows the locations of ground service connections in graphic and in tabular forms.Typical capacities and service requirements are shown in the tables. Services with requirements thatvary with conditions are described in subsequent sections.Section 5.5 shows minimum electrical ground power requirements for engine start. The curves arebased on 120-second and 180-second start times depending on the ground power unit.Section 5.6 shows air conditioning requirements for heating and cooling (pull-down and pull-up)using ground conditioned air. The curves show airflow requirements to heat or cool the airplanewithin a given time at ambient conditions.Section 5.7 shows air conditioning requirements for heating and cooling to maintain a constant cabinair temperature using low pressure conditioned air. This conditioned air is supplied through an 8-in(20.3 cm) ground air connection (GAC) directly to the passenger cabin, bypassing the air cyclemachines.Section 5.8 shows ground towing requirements for various ground surface conditions.D6-5833150 APRIL 2006
PRELIMINARY INFORMATION5.1. AIRPLANE SERVICING ARRANGEMENT - TYPICAL TURNAROUNDMODEL 787-8D6-58331APRIL 2006 51
PRELIMINARY INFORMATIONDATA TO BE PROVIDEDAT A LATER DATE5.2.1 TERMINAL OPERATIONS - TURNAROUND STATIONMODEL 787-8D6-5833152 APRIL 2006
PRELIMINARY INFORMATIONDATA TO BE PROVIDEDAT A LATER DATE5.3.1 TERMINAL OPERATIONS - EN ROUTE STATIONMODEL 787-8D6-58331APRIL 2006 53
PRELIMINARY INFORMATION5.4. GROUND SERVICING CONNECTIONSMODEL 787-8D6-5833154 APRIL 2006
PRELIMINARY INFORMATIONSYSTEMMODELDISTANCE AFTOF NOSEDISTANCE FROM AIRPLANECENTERLINELH SIDERH SIDEMAX HTABOVEGROUNDFTMFTMFTMFTMCONDITIONED AIRTWO 8-IN (20.3 CM) PORTS787-87121.620.620.661.8ELECTRICALTWO LOCATIONS WITH TWOCONNECTIONS EACH90 KVA , 200/115 V AC 400 HZ,787-8247.351.5--82.49930.251.5--72.1POTABLE WATERONE SERVICE CONNECTION787-86319.230.9--61.8FUELONE UNDERWING PRESSURECONNECTOR WITH TWO 00TOTAL CAPACITY 33,528 US GAL(126,903 LITERS)LAVATORYBOTH FORWARD AND AFT TOILETSARE SERVICED THROUGH ONESERVICE PANEL9.52.95.4.2 GROUND SERVICING CONNECTIONS AND CAPACITIESMODEL 787-8D6-58331APRIL 2006 55
PRELIMINARY INFORMATION5.5 ENGINE START REQUIREMENTSMODEL 787-8D6-5833156 APRIL 2006
PRELIMINARY INFORMATIONDATA TO BE PROVIDEDAT A LATER DATE5.6.1 CONDITIONED AIR FLOW REQUIREMENTS – HEATINGMODEL 787-8D6-58331APRIL 2006 57
PRELIMINARY INFORMATIONDATA TO BE PROVIDEDAT A LATER DATE5.6.2 CONDITIONED AIR FLOW REQUIREMENTS – COOLINGMODEL 787-8D6-5833158 APRIL 2006
PRELIMINARY INFORMATION5.7.1 CONDITIONED AIR FLOW REQUIREMENTS – STEADY STATEMODEL 787-8D6-58331APRIL 2006 59
PRELIMINARY INFORMATIONDATA TO BE PROVIDEDAT A LATER DATE5.8.1 GROUND TOWING REQUIREMENTS - ENGLISH UNITSMODEL 787-8D6-5833160 APRIL 2006
PRELIMINARY INFORMATIONDATA TO BE PROVIDEDAT A LATER DATE5.8.2 GROUND TOWING REQUIREMENTS - METRIC UNITSMODEL 787-8D6-58331APRIL 2006 61
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PRELIMINARY INFORMATION6.0JET ENGINE WAKE AND NOISE DATA6.1Jet Engine Exhaust Velocities and Temperatures6.2Airport and Community NoiseD6-58331APRIL 200663
PRELIMINARY INFORMATION6.0 JET ENGINE WAKE AND NOISE DATA6.1 Jet Engine Exhaust Velocities and TemperaturesThis section shows exhaust velocity and temperature contours aft of the 787-8 airplane. Thecontours were calculated from a standard computer analysis using three-dimensional viscous flowequation
PRELIMINARY INFORMATION D6-58331 APRIL 2006 3 1.2 Introduction This document conforms to NAS 3601. It provides characteristics of the Boeing Model 787 airplane
787 Airplane Characteristics CHARACTERISTICS UNITS 787-8 787-9 787-10 Wing Span FT/M 197.3 / 60.1 197.3 / 60.1 197.3 / 60.1 ICAO Code Letter E E E FAA Design Group V V V . 777-8/-9/10X Airport Compatibility Key Characteristics Wingspan Code F Solution -Folding Wing Tip (FWT)
AIRPLANE CHARACTERISTICS FOR AIRPORT PLANNING HIGHLIGHTS Revision No. 20 - Jan 01/12 LOCATIONS CHG CODE DESCRIPTIONS OF CHANGE CHAPTER 2 Section 2-1 Subject 2-1-0 General Airplane Characteristics R Subject 2-1-1 General Airplane Characteristics Data R OEW AND PAYLOAD DELETED. WV054, WV055 AND WV056 ADDED USABLE VOLUME BASED ON LD3 UPDATED OEW .
Bruksanvisning för bilstereo . Bruksanvisning for bilstereo . Instrukcja obsługi samochodowego odtwarzacza stereo . Operating Instructions for Car Stereo . 610-104 . SV . Bruksanvisning i original
Cathay Pacific Headquarters Changi Airport Chiang Kai-Shek Airport Dragon Air Headquarters Hong Kong International Airport Incheon Airport KAL Cargo Terminal Ninoy Aquino Airport Savarnabhumi Airport Soejkarno-Hatta Airport TaeGu Airport Wuxi Shuofang Airport Incheon, South Korea Brisbane, Australia Hong Kong, China
that airport capacity expansion decisions need to take into account a multi-airport perspective in assessing the value and timeliness of such investments. Planning scenarios based on calibrated airport choice model are developed to evaluate the market size of each airport. Keywords: Airport choice, Multi-airport region, Airport planning 1.
787-8, will carry up to 223 pas-sengers 8,500 naut. mi. in a three-class configuration. The shorter-range version, the 787-3, will carry up to 296 passengers 3,500 naut. mi. in a two-class configuration. Assembly on the 787-8 will start in 2006, with first flight in 2007 and certifica-tion and entry into service in 2008. The 787-3 will enter .
787.21 Dysphagia, oral phase R13.11 Dysphagia, oral phase 787.22 Dysphagia, oropharyngeal phase R13.12 Dysphagia, oropharyngeal phase 787.23 Dysphagia, pharyngeal phase R13.13 Dysphagia, pharyngeal phase 787.24 Dysphagia, pharyngoesophageal phase R13.14 Dysphagia, pharyngoesophageal phase 787.29 Other dysphagia Cervical dysphagia Neurogenic .
2019-2020 Baldridge Excellence Framework (Education) . �ส าคัญของ Baldrige Excellence Framework (Education) �กณฑ์ Educational Performance Excellence (EdPEx) จากเกณฑ์ปี 2558-2561 ถึงฉบับปัจจุบัน 75 อภิธาน .
