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

2.7.4 Door Clearances: Model 777-200, -300, Main Entry Door No 4, or No 5.................................................................................................. 2-26 2.7.5 Door Clearances: Model 777-300, Cargo Door Locations .................. 2-27 2.7.6 Door Clearances: Model 777-200, -300, Forward Cargo Door ........... 2-28 2.7.7 Door Clearances: Model 777-200, -300, Aft Cargo Door ................... 2-29 2.7.8 Door Clearances: Model 777-200, -300, Bulk Cargo Door ................. 2-30 3.0 AIRPLANE PERFORMANCE ............................................................................ 3-31 3.1 GENERAL INFORMATION ......................................................................... 3-31 3.2 PAYLOAD/RANGE FOR 0.84 MACH CRUISE ......................................... 3-32 3.2.1 Payload/Range for 0.84 Mach Cruise: Model 777-200 (Baseline Airplane) .............................................................................. 3-32 3.2.2 Payload/Range for 0.84 Mach Cruise: Model 777-200 (High Gross Weight Airplane) ....................................................................... 3-33 3.2.3 Payload/Range for 0.84 Mach Cruise: Model 777-300 (Typical 90K Engine) ......................................................................................... 3-34 3.2.4 Payload/Range for 0.84 Mach Cruise: Model 777-300 (Typical 98K Engine) ......................................................................................... 3-35 3.3 F.A.R. TAKEOFF RUNWAY LENGTH REQUIREMENTS ....................... 3-36 3.3.1 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 777-200 (Baseline Airplane)..................................................... 3-36 3.3.2 F.A.R. Takeoff Runway Length Requirements - Standard Day + 27°F (STD + 15°C): Model 777-200 (Baseline Airplane) ................... 3-37 3.3.3 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 777-200 (High Gross Weight Airplane) ................................... 3-38 3.3.4 F.A.R. Takeoff Runway Length Requirements - Standard Day + 27°F (STD + 15°C): Model 777-200 (High Gross Weight Airplane) .............................................................................................. 3-39 3.3.5 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 777-300 (Typical 90K Engine) ................................................. 3-40 3.3.6 F.A.R. Takeoff Runway Length Requirements - Standard Day + 27°F (STD + 15°C): Model 777-300 (Typical 90K Engine) ............... 3-41 3.3.7 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 777-300 (Typical 98K Engine) ................................................. 3-42 D6-58329 REV E December 2024 v Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 3.3.8 F.A.R. Takeoff Runway Length Requirements - Standard Day + 27°F (STD + 15°C): Model 777-300 (Typical 98K Engine) ............... 3-43 3.4 F.A.R. LANDING RUNWAY LENGTH REQUIREMENTS ...................... 3-44 3.4.1 F.A.R. Landing Runway Length Requirements: Model 777-200 ........ 3-44 3.4.2 F.A.R. Landing Runway Length Requirements: Model 777-300 ........ 3-45 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 777-200 ................................... 4-3 4.2.2 Turning Radii – No Slip Angle: Model 777-300 ................................... 4-4 4.3 CLEARANCE RADII: MODEL 777-200, -300 .............................................. 4-5 4.4 VISIBILITY FROM COCKPIT IN STATIC POSITION: MODEL 777-200, -300 .................................................................................................... 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 777-200, -300 ................................................ 4-7 4.5.2 Runway and Taxiway Turn Paths - Runway-to-Taxiway, 90 Degrees: Model 777-200, -300 .............................................................. 4-8 4.5.3 Runway and Taxiway Turn Paths - Taxiway-to-Taxiway, 90 Degrees, Nose Gear Tracks Centerline: Model 777-200, -300 .............. 4-9 4.5.4 Runway and Taxiway Turn Paths - Taxiway-to-Taxiway, 90 Degrees, Cockpit Tracks Centerline: Model 777-200, -300 ................ 4-10 4.5.5 Runway and Taxiway Turn Paths - Taxiway-to-Taxiway, 90 Degrees, Judgmental Oversteering: Model 777-200, -300 .................. 4-11 4.6 RUNWAY HOLDING BAY: MODEL 777-200, -300 .................................. 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 5.2 TERMINAL OPERATIONS - TURNAROUND STATION .......................... 5-4 5.2.1 Terminal Operations - Turnaround Station: Model 777-200 ................. 5-4 5.2.2 Terminal Operations - Turnaround Station: Model 777-300 ................. 5-5 5.3 TERMINAL OPERATIONS - EN ROUTE STATION ................................... 5-6 5.3.1 Terminal Operations - En Route Station: Model 777-200 ..................... 5-6 5.3.2 Terminal Operations - En Route Station: Model 777-300 ..................... 5-7 5.4 GROUND SERVICING CONNECTIONS ...................................................... 5-8 5.4.1 Ground Service Connections: Model 777-200 ....................................... 5-8 5.4.2 Ground Service Connections: Model 777-300 ....................................... 5-9 D6-58329 REV E December 2024 vi Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 5.4.3 Ground Service Connections and Capacities: Model 777- 200, -300 .............................................................................................. 5-10 5.5 ENGINE STARTING PNEUMATIC REQUIREMENTS ............................ 5-11 5.5.1 Engine Start Pneumatic Requirements - Sea Level: Model 777-200, -300 (Pratt & Whitney Engines) ........................................... 5-11 5.5.2 Engine Start Pneumatic Requirements - Sea Level: Model 777-200, -300 (General Electric Engines)............................................ 5-12 5.5.3 Engine Start Pneumatic Requirements - Sea Level: Model 777- 200, -300 (Rolls-Royce Engines) ......................................................... 5-13 5.6 GROUND PNEUMATIC POWER REQUIREMENTS ................................ 5-14 5.6.1 Ground Conditioned Air Requirements – Heating, Pull-Up: Model 777-200 ................................................................................................ 5-14 5.6.2 Ground Conditioned Air Requirements – Cooling, Pull-Down: Model 777-200 ..................................................................................... 5-15 5.6.3 Ground Conditioned Air Requirements – Heating, Pull-Up: Model 777-300 ................................................................................................ 5-16 5.6.4 Ground Conditioned Air Requirements – Cooling, Pull-Down: Model 777-300 ..................................................................................... 5-17 5.7 CONDITIONED AIR REQUIREMENTS ..................................................... 5-18 5.7.1 Conditioned Air Flow Requirements - Steady State Airflow: Model 777-200, -300 ............................................................................ 5-18 5.7.2 Air Conditioning Gauge Pressure Requirements - Steady State Airflow: Model 777-200, -300 ............................................................. 5-19 5.7.3 Conditioned Air Flow Requirements - Steady State BTU’s: Model 777-200, -300 ....................................................................................... 5-20 5.8 GROUND TOWING REQUIREMENTS ...................................................... 5-21 5.8.1 Ground Towing Requirements - English Units: Model 777- 200, -300 .............................................................................................. 5-21 5.8.2 Ground Towing Requirements - Metric Units: Model 777- 200, -300 .............................................................................................. 5-22 6.0 JET ENGINE WAKE AND NOISE DATA .......................................................... 6-1 6.1 JET ENGINE EXHAUST VELOCITIES AND TEMPERATURES .............. 6-1 6.1.1 Jet Engine Exhaust Velocity Contours – Idle Thrust: Model 777- 200 .......................................................................................................... 6-2 6.1.2 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / 0% Slope / Single Engine / MLW: Model 777-200 ..................................... 6-3 6.1.3 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / 0% Slope / Both Engines / MTW: Model 777-200 ...................................... 6-4 6.1.4 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / 1% Slope / Both Engines / MTW: Model 777-200 ...................................... 6-5 6.1.5 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / 0% Slope / Single Engine / MTW: Model 777-200 ..................................... 6-6 D6-58329 REV E December 2024 vii Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 6.1.6 Jet Engine Exhaust Velocity Contours – Takeoff Thrust: Model 777-200 .................................................................................................. 6-7 6.1.7 Jet Engine Exhaust Velocity Contours – Idle Thrust: Model 777- 300 .......................................................................................................... 6-8 6.1.8 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / 0% Slope / Single Engine / MLW: Model 777-300 ..................................... 6-9 6.1.9 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / 0% Slope / Both Engines / MTW: Model 777-300 .................................... 6-10 6.1.10 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / 1% Slope / Both Engines / MTW: Model 777-300 .................................... 6-11 6.1.11 Jet Engine Exhaust Velocity Contours – Breakaway Thrust / 0% Slope / Single Engine / MTW: Model 777-300 ................................... 6-12 6.1.12 Jet Engine Exhaust Velocity Contours – Takeoff Thrust: Model 777-300 ................................................................................................ 6-13 6.1.13 Jet Engine Exhaust Temperature Contours – Idle/Breakaway Thrust: All Models ............................................................................... 6-14 6.1.14 Jet Engine Exhaust Temperature Contours – Takeoff Thrust: 777- 200 ........................................................................................................ 6-15 6.1.15 Jet Engine Exhaust Temperature Contours – Takeoff Thrust: 777- 300 ........................................................................................................ 6-16 6.1.16 Inlet Hazard Areas: All Models ........................................................... 6-17 6.2 AIRPORT AND COMMUNITY NOISE ....................................................... 6-18 7.0 PAVEMENT DATA .............................................................................................. 7-1 7.1 GENERAL INFORMATION ........................................................................... 7-1 7.2 LANDING GEAR FOOTPRINT: MODEL 777-200, -200ER, -300 ............... 7-5 7.3 MAXIMUM PAVEMENT LOADS: MODEL 777-200, -200ER, -300 .......... 7-6 7.4 LANDING GEAR LOADING ON PAVEMENT ........................................... 7-7 7.4.1 Landing Gear Loading on Pavement: Model 777-200 ........................... 7-7 7.4.2 Landing Gear Loading on Pavement: Model 777-200ER...................... 7-8 7.4.3 Landing Gear Loading on Pavement: Model 777-300 ........................... 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 777-200............................................ 7-11 7.5.2 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method (S-77-1): Model 777-200ER ...................................... 7-12 7.5.3 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method (S-77-1): Model 777-300............................................ 7-13 7.6 FLEXIBLE PAVEMENT REQUIREMENTS - LCN METHOD ................. 7-14 7.6.1 Flexible Pavement Requirements - LCN Method: Model 777-200 ..... 7-15 7.6.2 Flexible Pavement Requirements - LCN Method: Model 777-200ER ........................................................................................... 7-16 D6-58329 REV E December 2024 viii Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 7.6.3 Flexible Pavement Requirements - LCN Method: Model 777-300 ..... 7-17 7.7 RIGID PAVEMENT REQUIREMENTS - PORTLAND CEMENT ASSOCIATION DESIGN METHOD ............................................................ 7-18 7.7.1 Rigid Pavement Requirements - Portland Cement Association Design Method: Model 777-200 .......................................................... 7-19 7.7.2 Rigid Pavement Requirements - Portland Cement Association Design Method: Model 777-200ER ..................................................... 7-20 7.7.3 Rigid Pavement Requirements - Portland Cement Association Design Method: Model 777-300 .......................................................... 7-21 7.8 RIGID PAVEMENT REQUIREMENTS - LCN CONVERSION ................ 7-22 7.8.1 Radius of Relative Stiffness (Reference: Portland Cement Association) ............................................................................ 7-23 7.8.2 Rigid Pavement Requirements - LCN Conversion: Model 777-200 ................................................................................................ 7-24 7.8.3 Rigid Pavement Requirements - LCN Conversion: Model 777-200ER ........................................................................................... 7-25 7.8.4 Rigid Pavement Requirements - LCN Conversion: Model 777-300 ................................................................................................ 7-26 7.9 RIGID PAVEMENT REQUIREMENTS - FAA DESIGN METHOD ......... 7-27 7.9.1 Rigid Pavement Requirements: Model 777-200, -200ER, -300 .......... 7-28 7.10 ACN/PCN REPORTING SYSTEM - FLEXIBLE AND RIGID PAVEMENTS ................................................................................................ 7-29 7.10.1 Aircraft Classification Number - Flexible Pavement: Model 777-200 ................................................................................................ 7-30 7.10.2 Aircraft Classification Number - Rigid Pavement: Model 777-200 .... 7-31 7.10.3 Aircraft Classification Number - Flexible Pavement: Model 777-200ER ........................................................................................... 7-32 7.10.4 Aircraft Classification Number - Rigid Pavement: Model 777-200ER ........................................................................................... 7-33 7.10.5 Aircraft Classification Number - Flexible Pavement: Model 777-300 ................................................................................................ 7-34 7.10.6 Aircraft Classification Number - Rigid Pavement: Model 777-300 .... 7-35 7.11 ACR/PCR REPORTING SYSTEM - FLEXIBLE AND RIGID PAVEMENTS ................................................................................................ 7-36 7.11.1 Aircraft Classification Rating - Flexible Pavement: Model 777- 200 ........................................................................................................ 7-37 7.11.2 Aircraft Classification Rating - Rigid Pavement: Model 777-200....... 7-38 7.11.3 Aircraft Classification Rating - Flexible Pavement: Model 777- 200ER ................................................................................................... 7-39 7.11.4 Aircraft Classification Rating - Rigid Pavement: Model 777- 200ER ................................................................................................... 7-40 7.11.5 Aircraft Classification Rating - Flexible Pavement: Model 777- 300 ........................................................................................................ 7-41 D6-58329 REV E December 2024 ix Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 7.11.6 Aircraft Classification Rating - Rigid Pavement: Model 777-300....... 7-42 8.0 FUTURE MODEL 777 DERIVATIVE AIRPLANES .......................................... 8-1 9.0 SCALED MODEL 777 DRAWINGS .................................................................... 9-1 9.1 MODEL 777-200 .............................................................................................. 9-2 9.1.1 Scaled Drawings – 1 IN. = 32 FT: Model 777-200................................ 9-2 9.1.2 Scaled Drawings – 1 IN. = 32 FT: Model 777-200................................ 9-3 9.1.3 Scaled Drawings – 1 IN. = 50 FT: Model 777-200................................ 9-4 9.1.4 Scaled Drawings – 1 IN. = 50 FT: Model 777-200................................ 9-5 9.1.5 Scaled Drawings – 1 IN. = 100 FT: Model 777-200.............................. 9-6 9.1.6 Scaled Drawings – 1 IN. = 100 FT: Model 777-200.............................. 9-7 9.1.7 Scaled Drawings – 1:500: Model 777-200............................................. 9-8 9.1.8 Scaled Drawings – 1:500: Model 777-200............................................. 9-9 9.2 MODEL 777-300 ............................................................................................ 9-10 9.2.1 Scaled Drawings – 1 IN. = 32 FT: Model 777-300.............................. 9-10 9.2.2 Scaled Drawings – 1 IN. = 32 FT: Model 777-300.............................. 9-11 9.2.3 Scaled Drawings – 1 IN. = 50 FT: Model 777-300.............................. 9-12 9.2.4 Scaled Drawings – 1 IN. = 50 FT: Model 777-300.............................. 9-13 9.2.5 Scaled Drawings – 1 IN. = 100 FT: Model 777-300............................ 9-14 9.2.6 Scaled Drawings – 1 IN. = 100 FT: Model 777-300............................ 9-15 9.2.7 Scaled Drawings – 1:500: Model 777-300........................................... 9-16 9.2.8 Scaled Drawings – 1:500: Model 777-300........................................... 9-17 D6-58329 REV E 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: http://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 family of 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. For additional information contact: D6-58329 REV E December 2024 1-2 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 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 MODEL 777 FAMILY OF AIRPLANES 777-200 Airplane The 777-200 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 777-300 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. 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 D6-58329 REV E December 2024 1-3 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 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 (LBS) 777-200/-200ER 777-300 GENERAL ELECTRIC GE 90-B3/-B4 74,500 LB 537,000 GE 90-B5 76,400 LB 537,000 GE 90-B1 84,100 LB 634,000 GE 90-B4 84,700 LB 634,000 GE 90-92B 90,500 LB 662,000 GE 90-98B 98,000 LB 662,000 PRATT & WHITNEY PW 4073/4073A 73,500 LB 537,000 PW 4077 77,200 LB 537,000 PW 4082 82,200 LB 634,000 PW 4084 84,600 LB 634,000 PW 4090 90,500 LB 662,000 PW 4098 98,000 LB 662,000 ROLLS ROYCE TRENT 870/871 71,200 LB 537,000 TRENT 877 74,900 LB 537,000 TRENT 882 82,200 LB 634,000 TRENT 884 84,300 LB 634,000 TRENT 890 90,000 LB 662,000 TRENT 898 98,000 LB 662,000 D6-58329 REV E 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 Landing Weight (MLW). Maximum weight for landing as limited by aircraft strength and airworthiness requirements. 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.) 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 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. Maximum 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 REV E December 2024 2-2 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.1 General Characteristics: Model 777-200 (General Electric Engines) CHARACTERISTICS UNITS BASELINE AIRPLANE HIGH GROSS WEIGHT OPTION MAX DESIGN TAXI WEIGHT POUNDS 508,000 517,000 537,000 582,000 592,000 634,500 KILOGRAMS 230,424 234,507 243,579 263,990 268,526 287,804 MAX DESIGN TAKEOFF WEIGHT POUNDS 506,000 515,000 535,000 580,000 590,000 632,500 KILOGRAMS 229,517 233,600 242,671 263,083 267,619 286,897 MAX DESIGN LANDING WEIGHT POUNDS 441,000 445,000 445,000 460,000 460,000 460,000 KILOGRAMS 200,034 201,848 201,848 208,652 208,652 208,652 MAX DESIGN ZERO FUEL WEIGHT POUNDS 420,000 420,000 420,000 430,000 430,000 430,000 KILOGRAMS 190,508 190,508 190,508 195,044 195,044 195,044 SPEC OPERATING EMPTY WEIGHT (1) POUNDS 298,900 298,900 299,550 304,500 304,500 304,500 KILOGRAMS 135,578 135,578 135,873 138,118 138,118 138,118 MAX STRUCTURAL PAYLOAD (1) POUNDS 121,100 121,100 120,450 125,550 125,550 125,550 KILOGRAMS 54,930 54,930 54,635 56,948 56,948 56,948 SEATING CAPACITY (1) TWO-CLASS 375 - 30 FIRST + 345 ECONOMY THREE-CLASS 305 - 24 FIRST + 54 BUSINESS + 227 ECONOMY MAX CARGO - LOWER DECK CUBIC FEET 5,656 (2) 5,656 (2) 5,656 (2) 5,656 (2) 5,656 (2) 5,656 (2) CUBIC METERS 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) USABLE FUEL U.S. GALLONS 31,000 31,000 31,000 45,220 45,220 45,220 LITERS 117,347 117,347 117,347 117,347 117,347 117,347 POUNDS 207,700 207,700 207,700 207,700 207,700 207,700 KILOGRAMS 94,230 94,230 94,230 94,230 94,230 94,230 NOTES: 1. SPEC WEIGHT FOR BASELINE CONFIGURATION OF 375 PASSENGERS. CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS. 2. 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 D6-58329 REV E December 2024 2-3 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.2 General Characteristics: Model 777-200 (Pratt & Whitney Engines) CHARACTERISTICS UNITS BASELINE AIRPLANE HIGH GROSS WEIGHT OPTION MAX DESIGN TAXI WEIGHT POUNDS 508,000 517,000 537,000 582,000 592,000 634,500 KILOGRAMS 230,424 234,507 243,579 263,990 268,526 287,804 MAX DESIGN TAKEOFF WEIGHT POUNDS 506,000 515,000 535,000 580,000 590,000 632,500 KILOGRAMS 229,517 233,600 242,671 263,083 267,619 286,897 MAX DESIGN LANDING WEIGHT POUNDS 441,000 445,000 445,000 450,000 455,000 455,000 KILOGRAMS 200,034 201,848 201,848 204,116 206,384 206,384 MAX DESIGN ZERO FUEL WEIGHT POUNDS 420,000 420,000 420,000 430,000 430,000 430,000 KILOGRAMS 190,508 190,508 190,508 195,044 195,044 195,044 SPEC OPERATING EMPTY WEIGHT (1) POUNDS 296,600 296,600 297,250 302,200 302,200 302,200 KILOGRAMS 134,535 134,535 134,830 137,075 137,075 137,075 MAX STRUCTURAL PAYLOAD POUNDS 123,400 123,400 122,750 127,800 127,800 127,800 KILOGRAMS 55,973 55,973 55,678 57,969 57,969 57,969 SEATING CAPACITY (1) TWO-CLASS 375 - 30 FIRST + 345 ECONOMY THREE-CLASS 305 - 24 FIRST + 54 BUSINESS + 227 ECONOMY MAX CARGO - LOWER DECK CUBIC FEET 5,656 (2) 5,656 (2) 5,656 (2) 5,656 (2) 5,656 (2) 5,656 (2) CUBIC METERS 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) USABLE FUEL U.S. GALLONS 31,000 31,000 31,000 45,220 45,220 45,220 LITERS 117,347 117,347 117,347 171,176 171,176 171,176 POUNDS 207,700 207,700 207,700 302,974 302,974 302,974 KILOGRAMS 94,230 94,230 94,230 137,454 137,454 137,454 NOTES: 1. SPEC WEIGHT FOR BASELINE CONFIGURATION OF 375 PASSENGERS. CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS. 2. 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 D6-58329 REV E December 2024 2-4 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.3 General Characteristics: Model 777-200 (Rolls-Royce Engines) CHARACTERISTICS UNITS BASELINE AIRPLANE HIGH GROSS WEIGHT MAX DESIGN TAXI WEIGHT POUNDS 508,000 517,000 537,000 582,000 592,000 634,500 KILOGRAMS 230,424 234,507 243,579 263,990 268,526 287,804 MAX DESIGN TAKEOFF WEIGHT POUNDS 506,000 515,000 535,000 580,000 590,000 632,500 KILOGRAMS 229,517 233,600 242,671 263,083 267,619 286,897 MAX DESIGN LANDING WEIGHT POUNDS 441,000 445,000 445,000 450,000 455,000 455,000 KILOGRAMS 200,034 201,848 201,848 204,116 206,384 206,384 MAX DESIGN ZERO FUEL WEIGHT POUNDS 420,000 420,000 420,000 430,000 430,000 430,000 KILOGRAMS 190,508 190,508 190,508 195,044 195,044 195,044 SPEC OPERATING EMPTY WEIGHT (1) POUNDS 293,400 293,400 294,050 299,000 299,000 299,000 KILOGRAMS 133,084 133,084 133,378 135,624 135,624 135,624 MAX STRUCTURAL PAYLOAD (1) POUNDS 126,600 126,600 125,950 131,000 131,000 131,000 KILOGRAMS 57,424 57,424 57,129 59,420 59,420 59,420 SEATING CAPACITY (1) TWO-CLASS 375 - 30 FIRST + 345 ECONOMY THREE-CLASS 305 - 24 FIRST + 54 BUSINESS + 227 ECONOMY MAX CARGO - LOWER DECK CUBIC FEET 5,656 (2) 5,656 (2) 5,656 (2) 5,656 (2) 5,656 (2) 5,656 (2) CUBIC METERS 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) 160.3 (2) USABLE FUEL U.S. GALLONS 31,000 31,000 31,000 45,220 45,220 45,220 LITERS 117,347 117,347 117,347 117,347 117,347 117,347 POUNDS 207,700 207,700 207,700 207,700 207,700 207,700 KILOGRAMS 94,230 94,230 94,230 94,230 94,230 94,230 NOTES: 1. SPEC WEIGHT FOR BASELINE CONFIGURATION OF 375 PASSENGERS. CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS. 2. 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 D6-58329 REV E December 2024 2-5 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.4 General Characteristics: Model 777-300 (General Electric Engines) CHARACTERISTICS UNITS BASELINE AIRPLANE MAX DESIGN TAXI WEIGHT POUNDS 582,000 592,000 634,500 662,000 KILOGRAMS 263,990 268,526 287,804 300,278 MAX DESIGN TAKEOFF WEIGHT POUNDS 580,000 590,000 632,500 660,000 KILOGRAMS 263,083 267,619 286,897 299,370 MAX DESIGN LANDING WEIGHT POUNDS 524,000 524,000 524,000 524,000 KILOGRAMS 237,682 237,682 237,682 237,682 MAX DESIGN ZERO FUEL WEIGHT POUNDS 495,000 495,000 495,000 495,000 KILOGRAMS 224,528 224,528 224,528 224,528 SPEC OPERATING EMPTY WEIGHT (1) POUNDS 353,800 353,800 353,800 353,800 KILOGRAMS 160,480 160,480 160,480 160,480 MAX STRUCTURAL PAYLOAD POUNDS 141,200 141,200 141,200 141,200 KILOGRAMS 64,047 64,047 64,047 64,047 SEATING CAPACITY (1) TWO-CLASS 451 - 40 FIRST + 411 ECONOMY THREE-CLASS 368 - 30 FIRST + 84 BUSINESS + 254 ECONOMY MAX CARGO - LOWER DECK CUBIC FEET 7,552 (2) 7,552 (2) 7,552 (2) 7,552 (2) CUBIC METERS 213.9 (2) 213.9 (2) 213.9 (2) 213.9 (2) USABLE FUEL U.S. GALLONS 44,700 44,700 44,700 44,700 LITERS 169,207 169,207 169,207 169,207 POUNDS 299,490 299,490 299,490 299,490 KILOGRAMS 135,873 135,873 135,873 135,873 NOTES: 1. SPEC WEIGHT FOR BASELINE CONFIGURATION OF 451 PASSENGERS. CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS. 2. FWD CARGO = 24 LD3'S AT 158 CU FT EACH. AFT CARGO = 20 LD3'S AT 158 CU FT EACH. BULK CARGO = 600 CU FT D6-58329 REV E December 2024 2-6 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.5 General Characteristics: Model 777-300 (Pratt & Whitney Engines) CHARACTERISTICS UNITS BASELINE AIRPLANE MAX DESIGN TAXI WEIGHT POUNDS 582,000 592,000 634,500 662,000 KILOGRAMS 263,990 268,526 287,804 300,278 MAX DESIGN TAKEOFF WEIGHT POUNDS 580,000 590,000 632,500 660,000 KILOGRAMS 263,083 267,619 286,897 299,370 MAX DESIGN LANDING WEIGHT POUNDS 524,000 524,000 524,000 524,000 KILOGRAMS 237,682 237,682 237,682 237,682 MAX DESIGN ZERO FUEL WEIGHT POUNDS 495,000 495,000 495,000 495,000 KILOGRAMS 224,528 224,528 224,528 224,528 SPEC OPERATING EMPTY WEIGHT (1) POUNDS 351,700 351,700 351,700 351,700 KILOGRAMS 159,528 159,528 159,528 159,528 MAX STRUCTURAL PAYLOAD POUNDS 143,300 143,300 143,300 143,300 KILOGRAMS 64,999 64,999 64,999 64,999 SEATING CAPACITY (1) TWO-CLASS 451 - 40 FIRST + 411 ECONOMY THREE-CLASS 368 - 30 FIRST + 84 BUSINESS + 254 ECONOMY MAX CARGO - LOWER DECK CUBIC FEET 7,552 (2) 7,552 (2) 7,552 (2) 7,552 (2) CUBIC METERS 213.9 (2) 213.9 (2) 213.9 (2) 213.9 (2) USABLE FUEL U.S. GALLONS 44,700 44,700 44,700 44,700 LITERS 169,207 169,207 169,207 169,207 POUNDS 299,490 299,490 299,490 299,490 KILOGRAMS 135,873 135,873 135,873 135,873 NOTES: 1. SPEC WEIGHT FOR BASELINE CONFIGURATION OF 451 PASSENGERS. CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS. 2. FWD CARGO = 24 LD3'S AT 158 CU FT EACH. AFT CARGO = 20 LD3'S AT 158 CU FT EACH. BULK CARGO = 600 CU FT D6-58329 REV E December 2024 2-7 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.6 General Characteristics: Model 777-300 (Rolls-Royce Engines) CHARACTERISTICS UNITS BASELINE AIRPLANE MAX DESIGN TAXI WEIGHT POUNDS 582,000 592,000 634,500 662,000 KILOGRAMS 263,990 268,526 287,804 300,278 MAX DESIGN TAKEOFF WEIGHT POUNDS 580,000 590,000 632,500 660,000 KILOGRAMS 263,083 267,619 286,897 299,370 MAX DESIGN LANDING WEIGHT POUNDS 524,000 524,000 524,000 524,000 KILOGRAMS 237,682 237,682 237,682 237,682 MAX DESIGN ZERO FUEL WEIGHT POUNDS 495,000 495,000 495,000 495,000 KILOGRAMS 224,528 224,528 224,528 224,528 SPEC OPERATING EMPTY WEIGHT (1) POUNDS 347,800 347,800 347,800 347,800 KILOGRAMS 157,759 157,759 157,759 157,759 MAX STRUCTURAL PAYLOAD POUNDS 147,200 147,200 147,200 147,200 KILOGRAMS 66,768 66,768 66,768 66,768 SEATING CAPACITY (1) TWO-CLASS 451 - 40 FIRST + 411 ECONOMY THREE-CLASS 368 - 30 FIRST + 84 BUSINESS + 254 ECONOMY MAX CARGO - LOWER DECK CUBIC FEET 7,552 (2) 7,552 (2) 7,552 (2) 7,552 (2) CUBIC METERS 213.9 (2) 213.9 (2) 213.9 (2) 213.9 (2) USABLE FUEL U.S. GALLONS 44,700 44,700 44,700 44,700 LITERS 169,207 169,207 169,207 169,207 POUNDS 299,490 299,490 299,490 299,490 KILOGRAMS 135,873 135,873 135,873 135,873 NOTES: 1. SPEC WEIGHT FOR BASELINE CONFIGURATION OF 451 PASSENGERS. CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS. 2. FWD CARGO = 24 LD3'S AT 158 CU FT EACH. AFT CARGO = 20 LD3'S AT 158 CU FT EACH. BULK CARGO = 600 CU FT D6-58329 REV E December 2024 2-8 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.2 GENERAL DIMENSIONS 2.2.1 General Dimensions: Model 777-200 D6-58329 REV E December 2024 2-9 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.2.2 General Dimensions: Model 777-300 D6-58329 REV E December 2024 2-10 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.3 GROUND CLEARANCES 2.3.1 Ground Clearances: Model 777-200 Dimension MINIMUM* MAXIMUM* FT - IN M FT - IN M A 27 -6 8.39 28 - 6 8.68 B 15 - 5 4.71 16 - 5 5.00 C 9 - 3 2.81 10 - 0 3.05 D 16 - 0 4.88 16 - 7 5.07 E (PW) 3 - 2 0.96 3 - 5 1.04 E (GE) 2 - 10 0.85 3 - 1 0.93 E (RR) 3 - 7 1.09 3 - 10 1.17 F 16 - 10 5.14 17 - 4 5.28 G(LARGE DOOR) 10 - 7 3.23 11 - 2 3.41 G(SMALL DOOR) 10 - 6 3.22 11 - 2 3.40 H 10 - 7 3.23 11 - 5 3.48 J 17 - 4 5.28 18 - 2 5.54 K 60 - 5 18.42 61 - 6 18.76 L 23 - 6 7.16 24 - 6 7.49 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 REV E December 2024 2-11 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.3.2 Ground Clearances: Model 777-300 Dimension MINIMUM MAXIMUM FT - IN M FT - IN M A 27 -6 8.39 28 - 6 8.68 B 15 - 5 4.71 16 - 5 5.00 C 9 - 3 2.81 10 - 0 3.05 D 16 - 0 4.88 16 - 7 5.07 E (PW) 3 - 2 0.96 3 - 5 1.04 E (GE) 2 - 10 0.85 3 - 1 0.93 E (RR) 3 - 7 1.09 3 - 10 1.17 F 16 - 10 5.14 17 - 4 5.28 G(LARGE DOOR) 10 - 7 3.23 11 - 2 3.41 G(SMALL DOOR) 10 - 6 3.22 11 - 2 3.40 H 10 - 7 3.23 11 - 5 3.48 J 17 - 4 5.28 18 - 2 5.54 K 60 - 5 18.42 61 - 6 18.76 L 23 - 6 7.16 24 - 6 7.49 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 REV E December 2024 2-12 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4 INTERIOR ARRANGEMENTS 2.4.1 Interior Arrangements: Model 737-200, Tri-Class Configuration D6-58329 REV E December 2024 2-13 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.2 Interior Arrangements: Model 777-200, Two- Class Configuration D6-58329 REV E December 2024 2-14 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.3 Interior Arrangements: Model 777-200, All-Economy Configuration D6-58329 REV E December 2024 2-15 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.4 Interior Arrangements: Model 777-300, Tri-Class Configuration D6-58329 REV E December 2024 2-16 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.5 Interior Arrangements: Model 777-300, Two-Class Configuration D6-58329 REV E December 2024 2-17 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.6 Typical Interior Arrangements: Model 777-300, All-Economy Configuration D6-58329 REV E December 2024 2-18 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.5 CABIN CROSS SECTIONS 2.5.1 Cabin Cross-Sections: Model 777-200, -300, First and Business Class Seats D6-58329 REV E December 2024 2-19 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.5.2 Cabin Cross-Sections: Model 777-200, -300, Business and Economy Class Seats D6-58329 REV E December 2024 2-20 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.6 LOWER CARGO COMPARTMENTS 2.6.1 Lower Cargo Compartments: Model 777-200, -300, Containers and Bulk Cargo MODEL 777-200 MODEL 777-300 CROSS SECTION D6-58329 REV E December 2024 2-21 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.6.2 Lower Cargo Compartments: Model 777-200, Optional Aft Large Cargo Door D6-58329 REV E December 2024 2-22 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.6.3 Lower Cargo Compartments: Model 777-300, Optional Aft Large Cargo Door D6-58329 REV E December 2024 2-23 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7 DOOR CLEARANCES 2.7.1 Door Clearances: Model 777-300, Main Entry Door Locations MODEL 777-200 MODEL 777-300 NOTES: 1. MODEL 777-200 - EIGHT PASSENGER DOORS, 4 ON EACH SIDE DOOR OPENING SIZE = 42 BY 74 IN (1.07 M BY 1.88 M) DOOR SIZE = 42 BY 74 IN (1.07 BY 1.88 M) 2. MODEL 777-300 - TEN PASSENGER DOORS, 5 ON EACH SIDE DOOR OPENING AND SIZE SAME AS IN 777-200. 3. DOORS ARE TRANSLATING TYPE A DOORS 4. SEE SECTION 2.3 FOR DOOR SILL HEIGHTS. D6-58329 REV E December 2024 2-24 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.2 Door Clearances: Model 777-200, -300, Main Entry Door No 1 D6-58329 REV E December 2024 2-25 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.3 Door Clearances: Model 777-200, -300, Main Entry Door No 2, No 3, and No 4 NOTES: 1. DOOR MOVES UPWARD 2 IN AND INWARD 0.4 IN TO CLEAR STOPS BEFORE OPENING OUTWARD 2. DOOR CAPABLE OF MOVING AN ADDITIONAL 3 IN VERTICALLY (OVERLIFT) TO PRECLUDE DAMAGE FROM CONTACT WITH LOADING BRIDGE. 3. DOOR NO 2 AND 3 ON 777-200, DOOR NO 2, 3, AND 4 ON 777-300 D6-58329 REV E December 2024 2-26 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.4 Door Clearances: Model 777-200, -300, Main Entry Door No 4, or No 5 NOTES: 1. DOOR MOVES UPWARD 2 IN AND INWARD 0.4 IN TO CLEAR STOPS BEFORE OPENING OUTWARD 2. DOOR CAPABLE OF MOVING AN ADDITIONAL 3 IN VERTICALLY (OVERLIFT) TO PRECLUDE DAMAGE FROM CONTACT WITH LOADING BRIDGE. 3. DOOR NO 4 ON 777-200, DOOR NO 5 ON 777-300 D6-58329 REV E December 2024 2-27 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.5 Door Clearances: Model 777-300, Cargo Door Locations MODEL 777-200 MODEL 777-300 D6-58329 REV E December 2024 2-28 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.6 Door Clearances: Model 777-200, -300, Forward Cargo Door