777-200LR / -300ER / -Freighter Airplane Characteristics for Airport Planning

2.7.6 Door Clearances: Model 777F, Cargo Door Locations ....................... 2-24 2.7.7 Door Clearances: Model 777-200LR, -300ER, 777F, Forward Cargo Door ........................................................................................... 2-25 2.7.8 Door Clearances: Model 777-200LR, -300ER, Small Aft Cargo Door...................................................................................................... 2-26 2.7.9 Door Clearances: Model 777-200LR, -300ER, 777F, Bulk Cargo Door...................................................................................................... 2-27 3.0 AIRPLANE PERFORMANCE .............................................................................. 3-1 3.1 GENERAL INFORMATION ........................................................................... 3-1 3.2 PAYLOAD/RANGE FOR LONG RANGE CRUISE FOR 0.84 MACH CRUISE ............................................................................................................ 3-2 3.2.1 Payload/Range for 0.84 Mach Cruise: Model 777-200LR (GE90- 100 Series Engines) ................................................................................ 3-2 3.2.2 Payload/Range for 0.84 Mach Cruise: Model 777-300ER (GE90- 115BL Engines) ..................................................................................... 3-3 3.2.3 Payload/Range for 0.84 Mach Cruise: Model 777F (GE90-100 Series Engines) ....................................................................................... 3-4 3.3 F.A.R. TAKEOFF RUNWAY LENGTH REQUIREMENTS ......................... 3-5 3.3.1 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 777-200LR (GE90-100B1L Engines)......................................... 3-5 3.3.2 F.A.R. Takeoff Runway Length Requirements - Standard Day + 27°F (STD + 15°C): Model 777-200LR (GE90-110B1L Engines) ....... 3-6 3.3.3 F.A.R. Takeoff Runway Length Requirements - Standard Day + 49°F (STD + 27°C): Model 777-200LR (GE90-110B1L Engines) ....... 3-7 3.3.4 F.A.R. Takeoff Runway Length Requirements - Standard Day + 59°F (STD + 33°C): Model 777-200LR (GE90-110B1L Engines) ....... 3-8 3.3.5 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 777-200LR (GE90-115BL Engines)........................................... 3-9 3.3.6 F.A.R. Takeoff Runway Length Requirements - Standard Day + 27°F (STD + 15°C): Model 777-200LR (GE90-115BL Engines) ....... 3-10 3.3.7 F.A.R. Takeoff Runway Length Requirements - Standard Day + 49°F (STD + 27°C): Model 777-200LR (GE90-115BL Engines) ....... 3-11 3.3.8 F.A.R. Takeoff Runway Length Requirements - Standard Day + 59°F (STD + 33°C): Model 777-200LR (GE90-115BL Engines) ....... 3-12 D6-58329-2 REV G December 2024 v Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 3.3.9 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 777-300ER (GE90-115BL Engines)......................................... 3-13 3.3.10 F.A.R. Takeoff Runway Length Requirements - Standard Day + 27°F (STD + 15°C): Model 777-300ER (GE90-115BL Engines) ....... 3-14 3.3.11 F.A.R. Takeoff Runway Length Requirements - Standard Day + 49°F (STD + 27°C): Model 777-300ER (GE90-115BL Engines) ....... 3-15 3.3.12 F.A.R. Takeoff Runway Length Requirements - Standard Day + 59°F (STD + 33°C): Model 777-300ER (GE90-115BL Engines) ....... 3-16 3.3.13 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 777F (GE90-110B1L Engines) ................................................. 3-17 3.3.14 F.A.R. Takeoff Runway Length Requirements - Standard Day + 27°F (STD + 15°C): Model 777F (GE90-110B1L Engines) ............... 3-18 3.3.15 F.A.R. Takeoff Runway Length Requirements - Standard Day + 49°F (STD + 27°C): Model 777F (GE90-110B1L Engines) ............... 3-19 3.3.16 F.A.R. Takeoff Runway Length Requirements - Standard Day + 59°F (STD + 33°C): Model 777F (GE90-110B1L Engines) ............... 3-20 3.3.17 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 777F (GE90-115BL Engines) ................................................... 3-21 3.3.18 F.A.R. Takeoff Runway Length Requirements - Standard Day + 27°F (STD + 15°C): Model 777F (GE90-115BL Engines) ................. 3-22 3.3.19 F.A.R. Takeoff Runway Length Requirements - Standard Day + 49°F (STD + 27°C): Model 777F (GE90-115BL Engines) ................. 3-23 3.3.20 F.A.R. Takeoff Runway Length Requirements - Standard Day + 59°F (STD + 33°C): Model 777F (GE90-115BL Engines) ................. 3-24 3.4 F.A.R. LANDING RUNWAY LENGTH REQUIREMENTS ...................... 3-25 3.4.1 F.A.R. Landing Runway Length Requirements - Flaps 25: Model 777-200LR (GE90-110B1L Engines) .................................................. 3-25 3.4.2 F.A.R. Landing Runway Length Requirements - Flaps 30: Model 777-200LR (GE90-110B1L Engines) .................................................. 3-26 3.4.3 F.A.R. Landing Runway Length Requirements - Flaps 25: Model 777-200LR (GE90-115BL Engines) .................................................... 3-27 3.4.4 F.A.R. Landing Runway Length Requirements - Flaps 30: Model 777-200LR (GE90-115BL Engines) .................................................... 3-28 3.4.5 F.A.R. Landing Runway Length Requirements - Flaps 25: Model 777-300ER (GE90-115BL Engines) .................................................... 3-29 3.4.6 F.A.R. Landing Runway Length Requirements - Flaps 30: Model 777-300ER (GE90-115BL Engines) .................................................... 3-30 3.4.7 F.A.R. Landing Runway Length Requirements - Flaps 25: Model 777F (GE90-110B1L Engines) ............................................................ 3-31 3.4.8 F.A.R. Landing Runway Length Requirements - Flaps 30: Model 777F (GE90-110B1L Engines) ............................................................ 3-32 3.4.9 F.A.R. Landing Runway Length Requirements - Flaps 25: Model 777F (GE90-115BL Engines) .............................................................. 3-33 D6-58329-2 REV G December 2024 vi Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 3.4.10 F.A.R. Landing Runway Length Requirements - Flaps 30: Model 777F (GE90-115BL Engines) .............................................................. 3-34 4.0 GROUND MANEUVERING ................................................................................ 4-1 4.1 GENERAL INFORMATION ........................................................................... 4-1 4.2 TURNING RADII ............................................................................................ 4-3 4.2.1 Turning Radii – No Slip Angle: Model 777-200LR, 777F .................... 4-3 4.2.2 Turning Radii – No Slip Angle: Model 777-300ER .............................. 4-4 4.3 CLEARANCE RADII: MODEL 777-200LR, -300ER, 777F .......................... 4-5 4.4 VISIBILITY FROM COCKPIT IN STATIC POSITION: MODEL 777- 200LR, -300ER, 777F....................................................................................... 4-6 4.5 RUNWAY AND TAXIWAY TURN PATHS ................................................. 4-7 4.5.1 Runway and Taxiway Turn Paths - Runway-to-Taxiway, More Than 90 Degrees: Model 777-200LR, -300ER, 777F ............................ 4-7 4.5.2 Runway and Taxiway Turn Paths - Runway-to-Taxiway, 90 Degrees: Model 777-200LR, -300ER, 777F .......................................... 4-8 4.5.3 Runway and Taxiway Turn Paths - Taxiway-to-Taxiway, 90 Degrees, Nose Gear Tracks Centerline: Model 777-200LR, - 300ER, 777F .......................................................................................... 4-9 4.5.4 Runway and Taxiway Turn Paths - Taxiway-to-Taxiway, 90 Degrees, Cockpit Tracks Centerline: Model 777-200LR, -300ER, 777F...................................................................................................... 4-10 4.5.5 Runway and Taxiway Turn Paths - Taxiway-to-Taxiway, 90 Degrees, Judgmental Oversteering: Model 777-200LR, -300ER, 777F...................................................................................................... 4-11 4.6 RUNWAY HOLDING BAY: MODEL 777-200LR, -300ER, 777F ............. 4-12 5.0 TERMINAL SERVICING ..................................................................................... 5-1 5.1 AIRPLANE SERVICING ARRANGEMENT - TYPICAL TURNAROUND .............................................................................................. 5-2 5.1.1 Airplane Servicing Arrangement - Typical Turnaround: Model 777-200 / -200ER / -200LR ................................................................... 5-2 5.1.2 Airplane Servicing Arrangement - Typical Turnaround: Model 777-300 / -300ER ................................................................................... 5-3 5.1.3 Airplane Servicing Arrangement - Typical Turnaround: Model 777F........................................................................................................ 5-4 5.2 TERMINAL OPERATIONS - TURNAROUND STATION .......................... 5-5 5.2.1 Terminal Operations - Turnaround Station: Model 777-200LR ............ 5-5 5.2.2 Terminal Operations - Turnaround Station: Model 777-300ER ............ 5-6 5.2.3 Terminal Operations - Turnaround Station: Model 777F ...................... 5-7 5.3 TERMINAL OPERATIONS - EN ROUTE STATION ................................... 5-8 5.3.1 Terminal Operations - En Route Station: Model 777-200 / -200ER / -200LR ................................................................................................. 5-8 5.3.2 Terminal Operations - En Route Station: Model 777-300 / -300ER ..... 5-9 D6-58329-2 REV G December 2024 vii Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 5.4 GROUND SERVICING CONNECTIONS .................................................... 5-10 5.4.1 Ground Service Connections: Model 777-200LR................................ 5-10 5.4.2 Ground Service Connections: Model 777-300ER................................ 5-11 5.4.3 Ground Service Connections: Model 777F .......................................... 5-12 5.4.4 Ground Service Connections and Capacities: Model 777- 200LR, -300ER, 777F .......................................................................... 5-13 5.5 ENGINE STARTING PNEUMATIC REQUIREMENTS ............................ 5-14 5.5.1 Engine Start Pneumatic Requirements - Sea Level: Model 777- 200LR, -300ER .................................................................................... 5-14 5.6 GROUND PNEUMATIC POWER REQUIREMENTS ................................ 5-15 5.6.1 Ground Pneumatic Power Requirements – Heating, Pull-Up: Model 777-200LR ................................................................................ 5-15 5.6.2 Ground Pneumatic Power Requirements – Cooling, Pull-Down: Model 777-200LR ................................................................................ 5-16 5.6.3 Ground Conditioned Air Requirements – Heating, Pull-Up: Model 777-300ER ........................................................................................... 5-17 5.6.4 Ground Conditioned Air Requirements – Cooling, Pull-Down: Model 777-300ER ................................................................................ 5-18 5.6.5 Ground Conditioned Air Requirements – Heating, Pull-Up: Model 777F .......................................................................................... 5-19 5.6.6 Ground Conditioned Air Requirements – Cooling, Pull-Down: Model 777F .......................................................................................... 5-20 5.7 CONDITIONED AIR REQUIREMENTS ..................................................... 5-21 5.7.1 Total Ground Cart Flow – Ground Cart Supply Temperature: Model 777F .......................................................................................... 5-21 5.7.2 Conditioned Air Flow Requirements - Steady State Airflow: Model 777-200LR, -300ER ................................................................. 5-22 5.7.3 Conditioned Air Flow Requirements - Steady State Airflow: Model 777F .......................................................................................... 5-23 5.7.4 Air Conditioning Gauge Pressure Requirements - Steady State Airflow: Model 777-200LR, -300ER ................................................... 5-24 5.7.5 Conditioned Air Flow Requirements - Steady State BTU’s: Model 777-200LR, -300ER ............................................................................. 5-25 5.7.6 Conditioned Air Flow Requirements - Steady State BTU’s: Model 777F .......................................................................................... 5-26 5.7.7 Conditioned Air Flow Requirements - Steady State BTU’s: Model 777F .......................................................................................... 5-27 5.8 GROUND TOWING REQUIREMENTS ...................................................... 5-28 5.8.1 Ground Towing Requirements - English and Metric Units: Model 777F .......................................................................................... 5-28 6.0 JET ENGINE WAKE AND NOISE DATA .......................................................... 6-1 6.1 JET ENGINE EXHAUST VELOCITIES AND TEMPERATURES .............. 6-1 D6-58329-2 REV G December 2024 viii Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 6.1.1 Jet Engine Exhaust Velocity Contours – Idle Thrust: Model 777- 200LR ..................................................................................................... 6-2 6.1.2 Jet Engine Exhaust Velocity Contours - Breakaway Thrust / Single Engine / MTW / 0% Slope: Model 777-200LR .......................... 6-3 6.1.3 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / Single Engine / MLW / 0% Slope: Model 777-200LR .......................... 6-4 6.1.4 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / Both Engines / MTW / 1% Slope: Model 777-200LR ................................... 6-5 6.1.5 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / Both Engines / MTW / 0% Slope: Model 777-200LR ................................... 6-6 6.1.6 Jet Engine Exhaust Velocity Contours – Takeoff Thrust: Model 777-200LR ............................................................................................. 6-7 6.1.7 Jet Engine Exhaust Velocity Contours – Idle Thrust: Model 777- 300ER ..................................................................................................... 6-8 6.1.8 Jet Engine Exhaust Velocity Contours – BreakawayThrust / Single Engine / 0% Slope / MTW: Model 777-300ER .......................... 6-9 6.1.9 Jet Engine Exhaust Velocity Contours – BreakawayThrust / Single Engine / 0% Slope / MLW: Model 777-300ER ........................ 6-10 6.1.10 Jet Engine Exhaust Velocity Contours – BreakawayThrust / Both Engines / 0% Slope / MTW: Model 777-300ER ................................. 6-11 6.1.11 Jet Engine Exhaust Velocity Contours – BreakawayThrust / Both Engines / 1% Slope / MTW: Model 777-300ER ................................. 6-12 6.1.12 Jet Engine Exhaust Velocity Contours – Takeoff Thrust: Model 777-300ER ........................................................................................... 6-13 6.1.13 Inlet Hazard Areas: All Models ........................................................... 6-14 6.2 AIRPORT AND COMMUNITY NOISE ....................................................... 6-15 7.0 PAVEMENT DATA .............................................................................................. 7-1 7.1 GENERAL INFORMATION ........................................................................... 7-1 7.2 LANDING GEAR FOOTPRINT: MODEL 777-200LR, -300ER, 777F ......... 7-5 7.3 MAXIMUM PAVEMENT LOADS: MODEL 777-200LR, -300ER, 777F 7-6 7.4 LANDING GEAR LOADING ON PAVEMENT ........................................... 7-7 7.4.1 Landing Gear Loading on Pavement: Model 777-200LR...................... 7-7 7.4.2 Landing Gear Loading on Pavement: Model 777-300ER...................... 7-8 7.4.3 Landing Gear Loading on Pavement: Model 777F ................................ 7-9 7.5 FLEXIBLE PAVEMENT REQUIREMENTS - U.S. ARMY CORPS OF ENGINEERS METHOD S-77-1 .................................................................... 7-10 7.5.1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method (S-77-1): Model 777-200LR, 777F ............................ 7-11 7.5.2 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method (S-77-1): Model 777-300ER ...................................... 7-12 7.6 FLEXIBLE PAVEMENT REQUIREMENTS - LCN CONVERSION ......... 7-13 D6-58329-2 REV G December 2024 ix Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 7.6.1 Flexible Pavement Requirements - LCN Method: Model 777- 200LR, 777F ........................................................................................ 7-14 7.6.2 Flexible Pavement Requirements - LCN Method: Model 777- 300ER ................................................................................................... 7-15 7.7 RIGID PAVEMENT REQUIREMENTS - PORTLAND CEMENT ASSOCIATION DESIGN METHOD ............................................................ 7-16 7.7.1 Rigid Pavement Requirements - Portland Cement Association Design Method: Model 777-200LR, 777F ........................................... 7-17 7.7.2 Rigid Pavement Requirements - Portland Cement Association Design Method: Model 777-300ER ..................................................... 7-18 7.8 RIGID PAVEMENT REQUIREMENTS - LCN CONVERSION ................ 7-19 7.8.1 Radius of Relative Stiffness (Reference: Portland Cement Association).......................................................................................... 7-20 7.8.2 Rigid Pavement Requirements - LCN Conversion: Model 777-200LR, 777F ................................................................................. 7-21 7.8.3 Rigid Pavement Requirements - LCN Conversion: Model 777- 300ER ................................................................................................... 7-22 7.9 RIGID PAVEMENT REQUIREMENTS - FAA DESIGN METHOD ......... 7-23 7.9.1 Rigid Pavement Requirements: Model 777-200LR, -300ER, 777F .... 7-24 7.10 ACN/PCN REPORTING SYSTEM - FLEXIBLE AND RIGID PAVEMENTS ................................................................................................ 7-25 7.10.1 Aircraft Classification Number - Flexible Pavement: Model 777-200LR ........................................................................................... 7-26 7.10.2 Aircraft Classification Number - Rigid Pavement: Model 777-200LR ........................................................................................... 7-27 7.10.3 Aircraft Classification Number - Flexible Pavement: Model 777-300ER ........................................................................................... 7-28 7.10.4 Aircraft Classification Number - Rigid Pavement: Model 777-300ER ........................................................................................... 7-29 7.10.5 Aircraft Classification Number - Flexible Pavement: Model 777F ..... 7-30 7.10.6 Aircraft Classification Number - Rigid Pavement: Model 777F ......... 7-31 7.11 ACR/PCR REPORTING SYSTEM - FLEXIBLE AND RIGID PAVEMENTS ................................................................................................ 7-32 7.11.1 Aircraft Classification Rating - Flexible Pavement: Model 777- 200LR ................................................................................................... 7-33 7.11.2 Aircraft Classification Rating - Rigid Pavement: Model 777- 200LR ................................................................................................... 7-34 7.11.3 Aircraft Classification Rating - Flexible Pavement: Model 777- 300ER ................................................................................................... 7-35 7.11.4 Aircraft Classification Rating - Rigid Pavement: Model 777- 300ER ................................................................................................... 7-36 7.11.5 Aircraft Classification Rating - Flexible Pavement: Model 777F ....... 7-37 7.11.6 Aircraft Classification Rating - Rigid Pavement: Model 777F ............ 7-38 D6-58329-2 REV G December 2024 x Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 8.0 FUTURE 777 DERIVATIVE AIRPLANES.......................................................... 8-1 9.0 SCALED 777 DRAWINGS ................................................................................... 9-1 9.1 MODEL 777-200LR ......................................................................................... 9-2 9.1.1 Scaled Drawings – 1:500: Model 777-200LR ....................................... 9-2 9.1.2 Scaled Drawings – 1:500: Model 777-200LR ....................................... 9-3 9.2 MODEL 777-300ER ......................................................................................... 9-4 9.2.1 Scaled Drawings – 1:500: Model 777-300ER ....................................... 9-4 9.2.2 Scaled Drawings – 1:500: Model 777-300ER ....................................... 9-5 9.3 MODEL 777 FREIGHTER .............................................................................. 9-6 9.3.1 Scaled Drawings – 1:500: Model 777F .................................................. 9-6 9.3.2 Scaled Drawings – 1:500: Model 777F .................................................. 9-7 D6-58329-2 REV G December 2024 1-1 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 1.0 SCOPE AND INTRODUCTION 1.1 SCOPE This document provides, in a standardized format, airplane characteristics data for general airport planning. Since operational practices vary among airlines, specific data should be coordinated with the using airlines prior to facility design. Boeing Commercial Airplanes should be contacted for any additional information required. Content of the document reflects the results of a coordinated effort by representatives from the following organizations: • Aerospace Industries Association • Airports Council International - North America • International Industry Working Group • International Air Transport Association The airport planner may also want to consider the information presented in the "Commercial Aircraft Design Characteristics – Trends and Growth Projections," for long range planning needs and can be accessed via the following web site: www.boeing.com/airports The document is updated periodically and represents the coordinated efforts of the following organizations regarding future aircraft growth trends: • International Civil Aviation Organization • International Coordinating Council of Aerospace Industries Associations • Airports Council International - North American and World Organizations • International Industry Working Group • International Air Transport Association 1.2 INTRODUCTION This document conforms to NAS 3601. It provides characteristics of the Boeing Model 777-200LR, 777-300ER and 777-Freighter airplanes for airport planners and operators, airlines, architectural and engineering consultant organizations, and other interested industry agencies. Airplane changes and available options may alter model characteristics. The data presented herein reflect typical airplanes in each model category. Data used is generic in scope and not customer-specific. D6-58329-2 REV G December 2024 1-2 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. For additional information contact: Boeing Commercial Airplanes 2201 Seal Beach Blvd. M/C: 110-SB02 Seal Beach, CA 90740-1515 U.S.A. Attention: Manager, Airport Compatibility Engineering Phone: 562-797-1172 Email: AirportCompatibility@boeing.com 1.3 A BRIEF DESCRIPTION OF THE 777 FAMILY OF AIRPLANES 777-200/-200ER Airplane The 777-200/-200ER is a twin-engine airplane designed for medium to long range flights. It is powered by advanced high bypass ratio engines. Characteristics unique to the 777 include: • Two-crew cockpit with digital avionics • Circular cross-section • Lightweight aluminum and composite alloys • Structural carbon brakes • Six-wheel main landing gears • Main gear aft axle steering • High bypass ratio engines • Fly-by-wire system 777-200LR Airplane The 777-200LR is a derivative of the 777-200 airplane and is equipped with raked wingtips to provide additional cruise altitude and range. It is powered by high bypass ratio engines that develop higher thrusts than those used in the 777-200/-200ER airplanes. The 777- 200LR has an identical fuselage as the 777-200/-200ER but has a wider wingspan due to raked wingtips. D6-58329-2 REV G December 2024 1-3 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 777-300 Airplane The 777-300 is a second-generation derivative of the 777-200. Two body sections are added to the fuselage to provide additional passenger seating and cargo capacity. 777-300ER Airplane The 777-300ER is a derivative of the 777-300 airplane and is equipped with raked wingtips for additional cruise altitude and range. It is powered by high bypass ratio engines that develop higher thrusts than those used in the 777-200/-200ER/-300 airplanes. The 777- 300ER has an identical fuselage as the 777-300, but has a wider wingspan due to the raked wingtips. 777-Freighter Airplane The 777-Freighter, newest member of the 777 Family of airplanes, is based on the 777- 200LR Worldliner (Longer Range) passenger airplane. The 777-Freighter will fly farther than any other freighter, providing more capacity than any other twin-engine freighter, and will meet QC2 noise standards for maximum accessibility to noise-sensitive airports. The 777-Freighter will share the 777 Family’s advanced features of a state-of-the-art flight deck, fly-by-wire design and an advanced wing design, including raked wing tips. The 777- Freighter is powered by the world’s most powerful commercial jet engine, General Electric’s GE90-110B1L. The 777-Freighter is designed to integrate smoothly with existing cargo operations and facilitate interlining with 747 freighter fleets. Cargo operators will be able to easily transfer 10-foot-high pallets between the two models via the large main deck cargo door. Main Gear Aft Axle Steering The main gear axle steering is automatically engaged based on the nose gear steering angle. This allows for less tire scrubbing and easier maneuvering into gates with limited parking clearances. High Bypass Ratio Engines The 777 airplane is powered by two high bypass ratio engines. The following table shows the available engine options: ENGINE MANUFACTURER ENGINE MODEL ENGINE THRUST MAX TAXI WEIGHT (LB) 77-200LR 777-300ER 777F GENERAL ELECTRIC GE90-110B 110,000 LB 768,000 - - GE90-110B1 110,000 LB 768,000 - - GE90- 110B1L 110,000 LB - - 768,800 GE90-115B1 115,300 LB 768,000 777,000 - D6-58329-2 REV G December 2024 1-4 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. Document Applicability This document contains data specific to the 777-200LR, 777-300ER and 777-Freighter. Data for the 777-200, 777-200ER, and 777-300 airplanes are contained in document D6-58329. D6-58329-2 REV G December 2024 2-1 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.0 AIRPLANE DESCRIPTION 2.1 GENERAL CHARACTERISTICS Maximum Design Taxi Weight (MTW). Maximum weight for ground maneuver as limited by aircraft 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 aircraft strength 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 aircraft strength and airworthiness requirements. Maximum Design Zero Fuel Weight (MZFW). Maximum weight allowed before usable fuel and other specified usable agents must be loaded in defined sections of the aircraft as limited by strength and airworthiness requirements. Operating Empty Weight (OEW). Weight of structure, powerplant, furnishing systems, unusable fuel and other unusable propulsion agents, and other items of equipment that are considered an 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 or anticipated for certification. Maximum Cargo Volume. The maximum space available for cargo. Usable Fuel. Fuel available for aircraft propulsion. D6-58329-2 REV G December 2024 2-2 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.1 General Characteristics: Model 777-200LR, -300ER, 777F CHARACTERISTICS UNITS 777-200LR 777-300ER 777-F MAX DESIGN TAXI WEIGHT POUNDS 768,000 777,000 768,800 KILOGRAMS 348,358 352,441 348,721 MAX DESIGN TAKEOFF WEIGHT POUNDS 766,000 775,000 766,800 KILOGRAMS 347,451 351,534 347,814 MAX DESIGN LANDING WEIGHT POUNDS 492,000 554,000 575,000 KILOGRAMS 223,167 251,290 260,815 MAX DESIGN ZERO FUEL WEIGHT POUNDS 461,000 524,000 547,000 KILOGRAMS 209,106 237,682 248,115 TYPICAL SEATING CAPACITY TWO CLASS 279 (3) 339 (5) N/A THREE CLASS 301 (4) 370 (6) N/A MAX CARGO --LOWER DECK CUBIC FEET 5,656 (1) 7,552 (1) 22,371 (2) CUBIC METERS 160.1 (1) 213.8 (1) 633.4 (2) USABLE FUEL U.S. GALLONS 47,890 47,890 47,890 LITERS 181,283 181,283 181,283 POUNDS 320,863 320,863 320,863 KILOGRAMS 145,570 145,570 145,570 NOTES: 1. FWD CARGO = 18 LD3'S AT 158 CU FT EACH. AFT CARGO = 14 LD3'S AT 158 CU FT EACH. BULK CARGO = 600 CU FT 2. INCLUDES MAIN DECK, FORWARD LOWER LOBE, AND AFT LOWER LOBE 3. 42 FIRST CLASS AND 237 ECONOMY CLASS 4. 16 FIRST CLASS, 58 BUSINESS CLASS AND 227 ECONOMY CLASS 5. 56 FIRST CLASS AND 283 ECONOMY CLASS 6. 12 FIRST CLASS, 42 BUSINESS CLASS AND 316 ECONOMY CLASS D6-58329-2 REV G December 2024 2-3 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.2 GENERAL DIMENSIONS 2.2.1 General Dimensions: Model 777-200LR D6-58329-2 REV G December 2024 2-4 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.2.2 General Dimensions: Model 777-300ER D6-58329-2 REV G December 2024 2-5 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.2.3 General Dimensions: Model 777F D6-58329-2 REV G December 2024 2-6 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.3 GROUND CLEARANCES 2.3.1 Ground Clearances: Model 777-200LR Dimension MINIMUM* MAXIMUM* FT - IN M FT - IN M A 27 - 5 8.36 28 - 7 8.70 B 15 - 5 4.69 16 - 7 5.06 C 9 - 2 2.79 10 - 2 3.11 D 15 - 11 4.85 16 - 10 5.11 E 2 - 4 0.70 2 - 10 0.88 F 16 - 10 5.14 17 - 5 5.30 G (LARGE/SMALL DOOR) 10 - 6 3.19 11 - 9 3.58 H 11 - 2 3.40 11 - 10 3.61 J 17 - 5 5.31 18 - 1 5.52 K 60 - 8 18.48 61 - 6 18.75 L 23 - 6 7.16 24 - 7 7.49 M 26 - 2 8.06 27 - 5 8.34 NOTES: VERTICAL CLEARANCES SHOWN OCCUR DURING MAXIMUM VARIATIONS OF AIRPLANE ATTITUDE. COMBINATIONS OF AIRPLANE LOADING AND UNLOADING ACTIVITIES THAT PRODUCE THE GREATEST POSSIBLE VARIATIONS IN ATTITUDE WERE USED TO ESTABLISH THE VARIATIONS SHOWN. DURING ROUTINE SERVICING, THE AIRPLANE REMAINS RELATIVELY STABLE, PITCH AND ELEVATION CHANGES OCCURRING SLOWLY. * NOMINAL DIMENSIONS D6-58329-2 REV G December 2024 2-7 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.3.2 Ground Clearances: Model 777-300ER Dimension MINIMUM* MAXIMUM* FT - IN M FT - IN M A 27 - 9 8.46 28 - 10 8.78 B 15 - 9 4.80 16 - 10 5.13 C 9 - 5 2.88 10 - 6 3.19 D 16 - 2 4.92 17 - 1 5.20 E 2 - 5 0.73 3 - 3 0.99 F 16 - 9 5.11 17 - 5 5.32 G (LARGE/SMALL DOOR) 10 - 6 3.19 11 - 9 3.58 H 10 - 11 3.32 12 - 4 3.76 J 17 - 0 5.19 18 - 7 5.66 K 59 - 10 18.24 61 - 10 18.85 L 23 - 11 7.29 25 - 11 7.90 M 25 - 7 7.79 27 - 8 8.43 NOTES: VERTICAL CLEARANCES SHOWN OCCUR DURING MAXIMUM VARIATIONS OF AIRPLANE ATTITUDE. COMBINATIONS OF AIRPLANE LOADING AND UNLOADING ACTIVITIES THAT PRODUCE THE GREATEST POSSIBLE VARIATIONS IN ATTITUDE WERE USED TO ESTABLISH THE VARIATIONS SHOWN. DURING ROUTINE SERVICING, THE AIRPLANE REMAINS RELATIVELY STABLE, PITCH AND ELEVATION CHANGES OCCURRING SLOWLY. * NOMINAL DIMENSIONS ROUNDED TO NEAREST INCH AND NEAREST CENTIMETER D6-58329-2 REV G December 2024 2-8 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.3.3 Ground Clearances: Model 777 Freighter Dimension MINIMUM* MAXIMUM* FT - IN M FT - IN M A 27 - 9 8.46 28 - 10 8.78 B 15 - 3 4.65 16 - 10 5.13 C 9 - 5 2.88 10 - 6 3.19 E 2 - 7 0.79 3 - 3 0.99 G (LARGE/SMALL DOOR) 10 - 10 3.32 11 - 8 3.56 H 10 - 11 3.32 12 - 4 3.76 K 60 - 11 18.58 62 - 4 18.99 L 23 - 11 7.29 25 - 11 7.90 M 26 - 10 8.17 28 - 3 8.60 O 17 - 4 5.29 18 - 2 5.53 NOTES: VERTICAL CLEARANCES SHOWN OCCUR DURING MAXIMUM VARIATIONS OF AIRPLANE ATTITUDE. COMBINATIONS OF AIRPLANE LOADING AND UNLOADING ACTIVITIES THAT PRODUCE THE GREATEST POSSIBLE VARIATIONS IN ATTITUDE WERE USED TO ESTABLISH THE VARIATIONS SHOWN. DURING ROUTINE SERVICING, THE AIRPLANE REMAINS RELATIVELY STABLE, PITCH AND ELEVATION CHANGES OCCURRING SLOWLY. * NOMINAL DIMENSIONS ROUNDED TO NEAREST INCH AND NEAREST CENTIMETER D6-58329-2 REV G December 2024 2-9 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4 INTERIOR ARRANGEMENTS 2.4.1 Typical Interior Arrangements: Model 777-200LR, Typical Two- Class Configurations D6-58329-2 REV G December 2024 2-10 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.2 Typical Interior Arrangements: Model 777-200LR, Typical Three- Class Configurations D6-58329-2 REV G December 2024 2-11 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.3 Typical Interior Arrangements: Model 777-300ER, Typical Two- Class Configurations D6-58329-2 REV G December 2024 2-12 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.4 Typical Interior Arrangements: Model 777-300ER, Typical Three- Class Configurations D6-58329-2 REV G December 2024 2-13 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.5 CABIN CROSS SECTIONS 2.5.1 Cabin Cross-Sections: Model 777-200LR, -300ER, First & Business Class Seats D6-58329-2 REV G December 2024 2-14 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.5.2 Cabin Cross-Sections: Model 777-200LR, -300ER, Business and Economy Class Seats D6-58329-2 REV G December 2024 2-15 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.6 LOWER CARGO COMPARTMENTS 2.6.1 Lower Cargo Compartments: Model 777-200LR, -300ER, Containers and Bulk Cargo D6-58329-2 REV G December 2024 2-16 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.6.2 Lower Cargo Compartments: Model 777-200LR, 777F, Optional Aft Large Cargo Door D6-58329-2 REV G December 2024 2-17 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.6.3 Lower Cargo Compartments: Model 777-300ER, Optional Aft Large Cargo Door D6-58329-2 REV G December 2024 2-18 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.6.4 Main Deck Cargo: Model 777F D6-58329-2 REV G December 2024 2-19 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7 DOOR CLEARANCES 2.7.1 Door Clearances: Model 777-200LR, -300ER, 777F, Main Entry Door Locations D6-58329-2 REV G December 2024 2-20 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.2 Door Clearances: Model 777-200LR, -300ER, 777F, Main Entry Door No 1. D6-58329-2 REV G December 2024 2-21 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.3 Door Clearances: Model 777-200LR, -300ER, Main Entry Door No 2, and No 3. D6-58329-2 REV G December 2024 2-22 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.4 Door Clearances: Model 777-200LR, -300ER, Main Entry Door No 4, or No 5 D6-58329-2 REV G December 2024 2-23 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.5 Door Clearances: Model 777-200LR, -300ER, Cargo Door Locations D6-58329-2 REV G December 2024 2-24 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.6 Door Clearances: Model 777F, Cargo Door Locations D6-58329-2 REV G December 2024 2-25 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.7 Door Clearances: Model 777-200LR, -300ER, 777F, Forward Cargo Door D6-58329-2 REV G December 2024 2-26 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.8 Door Clearances: Model 777-200LR, -300ER, Small Aft Cargo Door