757-200/ -300 Airplane Characteristics for Airport Planning

3.3.4 F.A.R. Takeoff Runway Length Requirements - Standard Day + 25°F (STD + 14°C): Model 757-200 (RB211-535E4 Engines) .................................................................................... 3-10 3.3.5 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 757-200 (RB211-535E4B Engines)........................ 3-11 3.3.6 F.A.R. Takeoff Runway Length Requirements - Standard Day + 25°F (STD + 14°C): Model 757-200 (RB211-535E4B Engines) .................................................................................... 3-12 3.3.7 F.A.R. Takeoff Runway Length Requirements - Standard Day: Model 757-200 (PW2037 Engines) ................................... 3-13 3.3.8 F.A.R. Takeoff Runway Length Requirements - Standard Day + 25°F (STD + 14°C): Model 757-200 (PW2037 Engines) .................................................................................... 3-14 3.3.9 F.A.R. Takeoff Runway Length Requirements – Standard Day: Model 757-200 (PW2040 Engines) ................................... 3-15 3.3.10 F.A.R. Takeoff Runway Length Requirements – Standard Day +25°F (STD + 14°C): Model 757-200 (PW2040 Engines) .................................................................................... 3-16 3.3.11 F.A.R. Takeoff Runway Length Requirements – Standard Day: Model 757-300 (RB211-535E4 Engines) .......................... 3-17 D6-58327 REV H December 2024 v Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 3.3.12 F.A.R. Takeoff Runway Length Requirements – Standard Day +25°F (STD + 14°C): Model 757-300 (RB211-535E4 Engines) .................................................................................... 3-18 3.3.13 J.A.R. Takeoff Runway Length Requirements – Standard Day - Wet Runway: Model 757-300 (RB211-535E4 Engines) .................................................................................... 3-19 3.3.14 J.A.R. Takeoff Runway Length Requirements – Standard Day – Wet Runway +25°F (STD + 14°C): Model 757-300 (RB211-535E4 Engines) ........................................................... 3-20 3.3.15 F.A.R. Takeoff Runway Length Requirements – Standard Day: Model 757-300 (RB211-535E4B Engines)........................ 3-21 3.3.16 F.A.R. Takeoff Runway Length Requirements – Standard Day +25°F (STD + 14°C): Model 757-300 (RB211-535E4B Engines) .................................................................................... 3-22 3.3.17 J.A.R. Takeoff Runway Length Requirements – Standard Day - Wet Runway: Model 757-300 (RB211-535E4B Engines) .................................................................................... 3-23 3.3.18 J.A.R. Takeoff Runway Length Requirements – Standard Day – Wet Runway +25°F (STD + 14°C): Model 757-300 (RB211-535E4B Engines) ......................................................... 3-24 3.3.19 F.A.R. Takeoff Runway Length Requirements – Standard Day: Model 757-300 (PW2040 Engines) ................................... 3-25 3.3.20 F.A.R. Takeoff Runway Length Requirements – Standard Day +28°F (STD + 16°C): Model 757-300 (PW2040 Engines) .................................................................................... 3-26 3.3.21 J.A.R. Takeoff Runway Length Requirements – Standard Day - Wet Runway: Model 757-300 (PW2040 Engines) ........... 3-27 3.3.22 J.A.R. Takeoff Runway Length Requirements – Standard Day – Wet Runway +28°F (STD + 16°C): Model 757-300 (PW2040 Engines) .................................................................... 3-28 3.3.23 F.A.R. Takeoff Runway Length Requirements – Standard Day: Model 757-300 (PW2043 Engines) ................................... 3-29 3.3.24 F.A.R. Takeoff Runway Length Requirements – Standard Day: +28°F (STD + 16°C): Model 757-300 (PW2043 Engines) .................................................................................... 3-30 3.3.25 J.A.R. Takeoff Runway Length Requirements – Standard Day - Wet Runway: Model 757-300 (PW2043 Engines) ........... 3-31 3.3.26 J.A.R. Takeoff Runway Length Requirements – Standard Day - Wet Runway +28°F (STD + 15°C): Model 757-300 (PW2043 Engines) .................................................................... 3-32 3.4 F.A.R. LANDING RUNWAY LENGTH REQUIREMENTS .................. 3-33 3.4.1 F.A.R. Landing Runway Length Requirements: Model 757- 200 (RB211-535C, -535E4, -535E4B Engines)......................... 3-33 D6-58327 REV H December 2024 vi Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 3.4.2 F.A.R. Landing Runway Length Requirements: Model 757- 200, -200PF (PW2037, PW2040 Engines)................................ 3-34 3.4.3 F.A.R. Landing Runway Length Requirements: Model 757- 300, (RB211-535E4, -535E4B Engines) ................................... 3-35 3.4.4 F.A.R. Landing Runway Length Requirements: Model 757- 300, (PW2040, PW2043 Engines) ............................................ 3-36 4.0 AIRPLANE PERFORMANCE .................................................................... 4-1 4.1 GENERAL INFORMATION .................................................................. 4-1 4.2 TURNING RADII .................................................................................. 4-2 4.2.1 Turning Radii – No Slip Angle: Model 757-200 ........................... 4-2 4.2.2 Turning Radii – No Slip Angle: Model 757-300 ........................... 4-3 4.3 CLEARANCE RADII: MODEL 757-200, -300 ....................................... 4-4 4.4 VISIBILITY FROM COCKPIT IN STATIC POSITION: MODEL 757-200, -300 ....................................................................................... 4-5 4.5 RUNWAY AND TAXIWAY TURN PATHS ............................................ 4-6 4.5.1 Runway and Taxiway Turn Paths - Runway-to-Taxiway, 90 Degrees Turn: Model 757-300 .................................................... 4-6 4.5.2 Runway and Taxiway Turn Paths - Runway-to-Taxiway, More Than 90 Degrees: Model 757-300 ..................................... 4-7 4.5.3 Runway and Taxiway Turn Paths - Taxiway-to-Taxiway, 90 Degrees, Nose Gear Tracks Centerline: Model 757-300 ............ 4-8 4.5.4 Runway and Taxiway Turn Paths - Taxiway-to-Taxiway, 90 Degrees, Cockpit Tracks Centerline: Model 757-300 .................. 4-9 4.6 RUNWAY HOLDING BAY: MODEL 757-300 ..................................... 4-10 5.0 TERMINAL SERVICING ............................................................................ 5-1 5.1 AIRPLANE SERVICING ARRANGEMENT - TYPICAL TURNAROUND .................................................................................... 5-2 5.1.1 Airplane Servicing Arrangement - Typical Turnaround: Model 757-200 ............................................................................ 5-2 5.1.2 Airplane Servicing Arrangement - Typical Turnaround: Model 757-200PF ....................................................................... 5-3 5.1.3 Airplane Servicing Arrangement - Typical Turnaround: Model 757-300 ............................................................................ 5-4 5.2 TERMINAL OPERATIONS - TURNAROUND STATION ...................... 5-5 5.2.1 Terminal Operations - Turnaround Station: Model 757-200 ........ 5-5 5.2.2 Terminal Operations - Turnaround Station: Model 757-200PF .................................................................................. 5-6 5.2.3 Terminal Operations - Turnaround Station: Model 757-300 ........ 5-7 5.3 TERMINAL OPERATIONS - EN ROUTE STATION ............................. 5-8 5.3.1 Terminal Operations - En Route Station: Model 757-200............ 5-8 5.3.2 Terminal Operations - En Route Station: Model 757-300............ 5-9 5.4 GROUND SERVICING CONNECTIONS ........................................... 5-10 D6-58327 REV H December 2024 vii Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 5.4.1 Ground Service Connections: Model 757-200 .......................... 5-10 5.4.2 Ground Service Connections: Model 757-300 .......................... 5-11 5.4.3 Ground Service Connections: Model 757-200,-300 .................. 5-12 5.5 ENGINE STARTING PNEUMATIC REQUIREMENTS ....................... 5-13 5.5.1 Engine Start Pneumatic Requirements - Sea Level: Model 757-200, -300 (Rolls Royce Engines) ....................................... 5-13 5.5.2 Engine Start Pneumatic Requirements - Sea Level: Model 757-200, -300 (Pratt & Whitney Engines).................................. 5-14 5.6 GROUND PNEUMATIC POWER REQUIREMENTS ......................... 5-15 5.6.1 Ground Pneumatic Power Requirements – Heating & Cooling: Model 757-200 ............................................................ 5-15 5.6.2 Ground Pneumatic Power Requirements Heating & Cooling: Model 757-300 .......................................................................... 5-16 5.7 CONDITIONED AIR REQUIREMENTS.............................................. 5-17 5.7.1 Conditioned Air Flow Requirements - Steady State Airflow: Model 757-200 .......................................................................... 5-17 5.7.2 Conditioned Air Flow Requirements - Steady State Airflow: Model 757-300 .......................................................................... 5-18 5.8 GROUND TOWING REQUIREMENTS .............................................. 5-19 5.8.1 Ground Towing Requirements - English Units: Model 757-200, -300............................................................................ 5-19 5.8.2 Ground Towing Requirements - Metric Units: Model 757-200, -300............................................................................ 5-20 6.0 JET ENGINE WAKE AND NOISE DATA ................................................... 6-1 6.1 JET ENGINE EXHAUST VELOCITIES AND TEMPERATURES ......... 6-1 6.1.1 Predicted Jet Engine Exhaust Velocity Contours – Idle Thrust: Model 757-200, -300 ....................................................... 6-2 6.1.2 Predicted Jet Engine Exhaust Velocity Contours - Breakaway Thrust: Model 757-200, -300 .................................... 6-3 6.1.3 Predicted Jet Engine Exhaust Velocity Contours - Takeoff Thrust: Model 757-200, -300 ....................................................... 6-4 6.1.4 Predicted Jet Engine Exhaust Temperature Contours - Idle Thrust: Model 757-200, -300 ....................................................... 6-5 6.1.5 Predicted Jet Engine Exhaust Temperature Contours – Breakaway Thrust: Model 757-200, -300 .................................... 6-6 6.1.6 Predicted Jet Engine Exhaust Temperature Contours – Takeoff Thrust: Model 757-200, -300 .......................................... 6-7 6.2 AIRPORT AND COMMUNITY NOISE .................................................. 6-8 7.0 PAVEMENT DATA .................................................................................... 7-1 7.1 GENERAL INFORMATION .................................................................. 7-1 7.2 LANDING GEAR FOOTPRINT: MODEL 757-200, -200PF, -300 ......... 7-5 7.3 MAXIMUM PAVEMENT LOADS: MODEL 757-200, 300...................... 7-6 D6-58327 REV H December 2024 viii Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 7.4 LANDING GEAR LOADING ON PAVEMENT ...................................... 7-7 7.4.1 Landing Gear Loading on Pavement: Model 757-200, - 200PF ......................................................................................... 7-7 7.4.2 Landing Gear Loading on Pavement: Model 757-300 ................. 7-8 7.5 FLEXIBLE PAVEMENT REQUIREMENTS - U.S. ARMY CORPS OF ENGINEERS METHOD S-77-1 ...................................................... 7-9 7.5.1 Flexible Pavement Requirements - U.S. Army Corps of Engineers Design Method (S-77-1): Model 757-200, - 200PF, -300 .............................................................................. 7-10 7.6 FLEXIBLE PAVEMENT REQUIREMENTS - LCN CONVERSION ..... 7-11 7.6.1 Flexible Pavement Requirements - LCN Method: Model 757-200, -200PF ....................................................................... 7-12 7.6.2 Flexible Pavement Requirements - LCN Method: Model 757-300 ..................................................................................... 7-13 7.7 RIGID PAVEMENT REQUIREMENTS - PORTLAND CEMENT ASSOCIATION DESIGN METHOD .................................................... 7-14 7.7.1 Rigid Pavement Requirements - Portland Cement Association Design Method: Model 757-200, -200PF ............... 7-15 7.7.2 Rigid Pavement Requirements - Portland Cement Association Design Method: Model 757-300 ............................. 7-16 7.8 RIGID PAVEMENT REQUIREMENTS - LCN CONVERSION............ 7-17 7.8.1 Radius of Relative Stiffness (Reference: Portland Cement Association) .............................................................................. 7-18 7.8.2 Rigid Pavement Requirements - LCN Conversion: Model 757-200, -200PF, 300 ............................................................... 7-19 7.9 RIGID PAVEMENT REQUIREMENTS - FAA DESIGN METHOD ...... 7-20 7.9.1 Rigid Pavement Requirements – FAA Method: Model 757- 200, -200PF, 300 ...................................................................... 7-21 7.10 ACN/PCN REPORTING SYSTEM - FLEXIBLE AND RIGID PAVEMENTS ..................................................................................... 7-22 7.10.1 Aircraft Classification Number - Flexible Pavement: Model 757-200, -200PF ...................................................................... 7-23 7.10.2 Aircraft Classification Number - Rigid Pavement: Model 757-200, -200PF .............................................................. 7-24 7.10.3 Aircraft Classification Number - Flexible Pavement: Model 757-300 ..................................................................................... 7-25 7.10.4 Aircraft Classification Number – Rigid Pavement: Model 757-300 ..................................................................................... 7-26 7.11 ACR/PCR REPORTING SYSTEM – FLEXIBLE AND RIGID PAVEMENTS ..................................................................................... 7-27 7.11.1 Aircraft Classification Rating - Flexible Pavement: Model 757-200, -200PF ................................................................. 7-28 D6-58327 REV H December 2024 ix Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 7.11.2 Aircraft Classification Rating - Rigid Pavement: Model 757- 200, -200PF .................................................................. 7-29 7.11.3 Aircraft Classification Rating - Flexible Pavement: Model 757-300 ..................................................................................... 7-30 7.11.4 Aircraft Classification Rating - Rigid Pavement: Model 757- 300 ............................................................................................ 7-31 8.0 FUTURE MODEL 757 DERIVATIVE AIRPLANES .................................. 8-32 9.0 SCALED MODEL 757 DRAWINGS ........................................................... 9-1 9.1 MODEL 757-200 .................................................................................. 9-1 9.1.1 Scaled Drawings – 1 IN. = 32 FT: Model 757-200 ...................... 9-1 9.1.2 Scaled Drawings – 1 IN. = 32 FT: Model 757-200 ...................... 9-2 9.1.3 Scaled Drawings – 1 IN. = 50 FT: Model 757-200 ...................... 9-3 9.1.4 Scaled Drawings – 1 IN. = 50 FT: Model 757-200 ...................... 9-4 9.1.5 Scaled Drawings – 1 IN. = 100 FT: Model 757-200 .................... 9-5 9.1.6 Scaled Drawings – 1 IN. = 100 FT: Model 757-200 .................... 9-6 9.1.7 Scaled Drawings – 1:500: Model 757-200 .................................. 9-7 9.1.8 Scaled Drawings – 1:500: Model 757-200 .................................. 9-8 9.1.9 Scaled Drawings – 1:1000: Model 757-200 ................................ 9-9 9.1.10 Scaled Drawings – 1:1000: Model 757-200 .............................. 9-10 9.2 MODEL 757-200 ................................................................................ 9-11 9.2.1 Scaled Drawings – 1 IN. = 32 FT: Model 757-200PF ................ 9-11 9.2.2 Scaled Drawings – 1 IN. = 32 FT: Model 757-200PF ................ 9-12 9.2.3 Scaled Drawings – 1 IN. = 50 FT: Model 757-200PF ................ 9-13 9.2.4 Scaled Drawings – 1 IN. = 50 FT: Model 757-200PF ................ 9-14 9.2.5 Scaled Drawings – 1 IN. = 100 FT: Model 757-200PF .............. 9-15 9.2.6 Scaled Drawings – 1 IN. = 100 FT: Model 757-200PF .............. 9-16 9.2.7 Scaled Drawings – 1:500: Model 757-200PF ............................ 9-17 9.2.8 Scaled Drawings – 1:500: Model 757-200PF ............................ 9-18 9.2.9 Scaled Drawings – 1:1000: Model 757-200PF .......................... 9-19 9.2.10 Scaled Drawings – 1:1000: Model 757-200PF .......................... 9-20 9.3 MODEL 757-300 ................................................................................ 9-21 9.3.1 Scaled Drawings – 1 IN. = 32 FT: Model 757-300 .................... 9-21 9.3.2 Scaled Drawings – 1 IN. = 32 FT: Model 757-300 .................... 9-22 9.3.3 Scaled Drawings – 1 IN. = 50 FT: Model 757-300 .................... 9-23 9.3.4 Scaled Drawings – 1 IN. = 50 FT: Model 757-300 .................... 9-24 9.3.5 Scaled Drawings – 1 IN. = 100 FT: Model 757-300 .................. 9-25 9.3.6 Scaled Drawings – 1 IN. = 100 FT: Model 757-300 .................. 9-26 9.3.7 Scaled Drawings – 1:500: Model 757-300 ................................ 9-27 9.3.8 Scaled Drawings – 1:500: Model 757-300 ................................ 9-28 9.3.9 Scaled Drawings – 1:1000: Model 757-300 .............................. 9-29 D6-58327 REV H December 2024 x Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 9.3.10 Scaled Drawings – 1:1000: Model 757-300 .............................. 9-30 D6-58327 REV H 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 • Air Transport Association of America • International Air Transport Association The airport planner may also want to consider the information presented in the "CTOL Transport Aircraft, 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 and represents the coordinated efforts of the following organizations regarding future aircraft growth trends: • International Coordinating Council of Aerospace Industries Associations • Airports Council International - North America • Air Transport Association of America • International Air Transport Association 1.2 INTRODUCTION This document conforms to NAS 3601. It provides characteristics of the Boeing Model 757 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. D6-58327 REV H 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 Operations Engineering Email: AirportCompatibility@boeing.com D6-58327 REV H December 2024 1-3 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 1.3 A BRIEF DESCRIPTION OF THE MODEL 757 AIRPLANE The 757 is a twin-engine, new technology jet airplane designed for low fuel burn and short-to-medium range operations. This airplane uses new aerodynamics, materials, structures, and systems to fill market requirement that cannot be efficiently provided by existing equipment or derivatives. The 757 is a low-noise airplane powered by either Rolls-Royce RB211- 535C, -535E4, or -535E4B, or the Pratt & Whitney PW2037, PW2040, or PW2043 engines. These are high-bypass-ratio engines which are efficient, reliable, and easy to maintain. The following table shows the available engine options ENGINE MANUFACTURER ENGINE MODEL ENGINE THRUST AIRPLANE MODEL PRATT & WHITNEY PW2037 37,200 LB 757-200, -200PF PW 2040 41,700 LB 757-200,-200PF, -300 PW 2043 43,850 LB 757-300 ROLLS ROYCE RB211-535C 37,400 LB 757-200 RB211-535E4 40,100 LB 757-200,-300 RB211-535E4B 43,100 LB 757-200,-300 757-200 The 757-200 family of airplanes consists of passenger and package freighter versions. The passenger version is available in two configurations: • The basic configuration (overwing-exit) has three LH and RH passenger doors and two LH and RH overwing exit doors. • An optional configuration (four-door) has the same three LH and RH passenger doors but with LH and RH exit door aft of the wing, in lieu of the overwing exit doors. In the passenger configuration, the 757-200 can typically carry 186 passengers in a six-abreast, mixed class configuration over a 2,900-nautical-mile range with full load. High gross options can increase the range to about 3,900 nautical miles. High-density seating arrangements can accommodate as many as 239 passengers in an all-economy configuration. The 757-200 can be equipped for Extended Range Operations (EROPS) to allow extended overwater operations. Changes include a backup hydraulic motor- generator set and an auxiliary fan for equipment cooling. D6-58327 REV H December 2024 1-4 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 757-200PF The Package Freighter (757-200PF) airplane is designed to carry an all-cargo payload. Main-deck cargo is either in cargo containers or pallets and are loaded through a large cargo door forward of left wing. The -200PF has no windows or passenger doors in the fuselage. A crew entry door is provided forward of the main deck cargo door. 757-300 The 757-300 is a second-generation derivative of the 757-200 airplane. Two body extensions are added to the airplane fuselage to provide additional seating and cargo capacity. The 757-300 can typically seat 243 passengers in a dual-class arrangement or 279 passengers in an all-economy configuration. The EROPS option has been incorporated in the 757-300. The 757 has ground service connections compatible with existing ground support equipment and no special equipment is required. D6-58327 REV H December 2024 2-5 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 Pay load. 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. D6-58327 REV H December 2024 2-6 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.1 General Characteristics: Model 757-200 (RB211- 535C, -535E4, -535E4B Engines) CHARACTERISTICS UNITS 757-200 MAX DESIGN TAXI WEIGHT POUNDS 221,000 231,000 241,000 251,000 256,000 KILOGRAMS 100,243 104,779 109,315 113,851 116,119 MAX DESIGN TAKEOFF WEIGHT POUNDS 220,000 230,000 240,000 250,000 255,000(1) KILOGRAMS 99,790 104,326 108,862 113,398 115,666(1) MAX DESIGN LANDING WEIGHT POUNDS 198,000 198,000 198,000 198,000 210,000 KILOGRAMS 89,811 89,811 89,811 89,811 95,254 MAX DESIGN ZERO FUEL WEIGHT POUNDS 184,000 184,000 184,000 184,000 188,000 KILOGRAMS 83,461 83,461 83,461 83,461 85,275 SPEC OPERATING EMPTY WEIGHT POUNDS 134,090 125,110 132,280 136,940 136,940 KILOGRAMS 60,822 56,748 60,001 62,114 62,114 MAX STRUCTURAL PAYLOAD POUNDS 49,910 58,890 51,720 47,060 47,060 KILOGRAMS 22,638 26,712 23,459 21,346 21,346 SEATING CAPACITY TWO-CLASS 186 - 16 FIRST + 170 ECONOMY ONE-CLASS FAA EXIT LIMIT: 224 (2), 239(3) MAX CARGO - LOWER DECK (4) CUBIC FEET 1,790 1,790 1,790 1,790 1,790 CUBIC METERS 51 51 51 51 51 USABLE FUEL U.S. GALLONS 11,276 11,276 11,276 11,276 11,276 LITERS 42,684 42,684 42,684 42,684 42,684 POUNDS 75,549 75,549 75,549 75,549 75,549 KILOGRAMS 34,275 34,275 34,275 34,275 34,275 NOTES: WEIGHTS SHOWN ARE FOR TYPICAL AS-DELIVERED OR AS-OFFERRED CONFIGURATIONS. CONSULT WITH AIRLINE FOR ACTUAL WEIGHTS. 1. 255,500 LB (115,892 KG) FOR AIRPORT ALTITUDES BELOW 1,500 FT. 2. OVERWING-EXIT CONFIGURATION AIRPLANE. 3. FOUR-DOOR CONFIGURATION AIRPLANE. 4. VOLUME IS REDUCED BY 100 CU FT (3 CU M) WITH TELESCOPING BAGGAGE SYSTEM. D6-58327 REV H December 2024 2-7 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.2 General Characteristics: Model 757-200 (PW2037, PW2040 Engines) CHARACTERISTICS UNITS 757-200 MAX DESIGN TAXI WEIGHT POUNDS 221,000 231,000 241,000 251,000 256,000 KILOGRAMS 100,243 104,779 109,315 113,851 116,119 MAX DESIGN TAKEOFF WEIGHT POUNDS 220,000 230,000 240,000 250,000 255,000(1) KILOGRAMS 99,790 104,326 108,862 113,398 115,666(1) MAX DESIGN LANDING WEIGHT POUNDS 198,000 198,000 198,000 198,000 210,000 KILOGRAMS 89,811 89,811 89,811 89,811 95,254 MAX DESIGN ZERO FUEL WEIGHT POUNDS 184,000 184,000 184,000 184,000 188,000 KILOGRAMS 83,461 83,461 83,461 83,461 85,275 SPEC OPERATING EMPTY WEIGHT POUNDS 128,380 130,850 130,860 130,875 130,875 KILOGRAMS 58,232 59,352 59,357 59,363 59,363 MAX STRUCTURAL PAYLOAD POUNDS 55,620 53,140 53,140 53,125 53,125 KILOGRAMS 25,228 24,103 24,103 24,097 24,097 SEATING CAPACITY TWO-CLASS 186 - 16 FIRST + 170 ECONOMY ONE-CLASS FAA EXIT LIMIT: 224 (2), 239(3) MAX CARGO - LOWER DECK (4) CUBIC FEET 1,790 1,790 1,790 1,790 1,790 CUBIC METERS 51 51 51 51 51 USABLE FUEL U.S. GALLONS 11,276 11,276 11,276 11,276 11,276 LITERS 42,684 42,684 42,684 42,684 42,684 POUNDS 75,549 75,549 75,549 75,549 75,549 KILOGRAMS 34,275 34,275 34,275 34,275 34,275 NOTES: WEIGHTS SHOWN ARE FOR TYPICAL AS-DELIVERED OR AS-OFFERRED CONFIGURATIONS. CONSULT WITH AIRLINE FOR ACTUAL WEIGHTS. 1. 255,500 LB (115,900 KG) FOR AIRPORT ALTITUDES BELOW 1,500 FT. 2. OVERWING-EXIT CONFIGURATION AIRPLANE. 3. FOUR-DOOR CONFIGURATION AIRPLANE. 4. VOLUME IS REDUCED BY 100 CU FT (3 CU M) WITH TELESCOPING BAGGAGE SYSTEM. D6-58327 REV H December 2024 2-8 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.3 General Characteristics: Model 757-200PF CHARACTERISTICS UNITS 757-200PF MAX DESIGN TAXI WEIGHT POUNDS 251,000 256,000 KILOGRAMS 113,851 116,119 MAX DESIGN TAKEOFF WEIGHT POUNDS 250,000 255,000(1) KILOGRAMS 113,398 116,666(1) MAX DESIGN LANDING WEIGHT POUNDS 210,000 210,000 KILOGRAMS 92,254 92,254 MAX DESIGN ZERO FUEL WEIGHT POUNDS 200,000 200,000 KILOGRAMS 90,718 90,718 SPEC OPERATING EMPTY WEIGHT POUNDS 114,000 114,000 KILOGRAMS 51,709 51,709 MAX STRUCTURAL PAYLOAD POUNDS 86,000 86,000 KILOGRAMS 39,008 39,008 MAX CARGO LOWER DECK (2) CUBIC FEET 1,830 1,830 CUBIC METERS 52 52 MAX CARGO - MAIN DECK (3) CUBIC FEET 6,600 6,600 CUBIC METERS 187 187 USABLE FUEL U.S. GALLONS 11,276 11,276 LITERS 42,684 42,684 POUNDS 75,549 75,549 KILOGRAMS 34,275 34,275 NOTES: WEIGHTS SHOWN ARE FOR TYPICAL AS-DELIVERED OR AS-OFFERRED CONFIGURATIONS. CONSULT WITH AIRLINE FOR ACTUAL WEIGHTS. 1. 255,500 LB (115,900 KG) FOR AIRPORT ALTITUDES BELOW 1,500 FT. 2. VOLUME IS REDUCED BY 100 CU FT (3 CU M) WITH TELESCOPING BAGGAGE SYSTEM. 3. 15 UNIT LOAD DEVICES (ULD) AT 440 CU FT (12.36 CU M) EACH. D6-58327 REV H December 2024 2-9 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.1.4 General Characteristics: Model 757-300 CHARACTERISTICS UNITS PW2040, PW 2043 ENGINES RB211-535E4, -535E4B ENGINES MAX DESIGN TAXI WEIGHT POUNDS 271,000 271,000 KILOGRAMS 122,923 122,923 MAX DESIGN TAKEOFF WEIGHT POUNDS 270,000 270,000 KILOGRAMS 122,449 122,449 MAX DESIGN LANDING WEIGHT POUNDS 224,000 224,000 KILOGRAMS 101,604 101,604 MAX DESIGN ZERO FUEL WEIGHT POUNDS 210,000 210,000 KILOGRAMS 95,254 95,254 SPEC OPERATING EMPTY WEIGHT (1) POUNDS 141,800 142,350 KILOGRAMS 64,319 64,568 MAX STRUCTURAL PAYLOAD POUNDS 68,200 67,650 KILOGRAMS 30,935 30,685 SEATING CAPACITY (1) TWO-CLASS 243 - 12 FIRST + 231 ECONOMY ONE-CLASS 279 ALL-ECONOMY MAX CARGO - LOWER DECK CUBIC FEET 2,382 (2) 2,382 (2) CUBIC METERS 67.5 (2) 67.5 (2) USABLE FUEL U.S. GALLONS 11,490 11,490 LITERS 43,494 43,494 POUNDS 76,983 79,983 KILOGRAMS 34,925 34,925 NOTES: 1. SPEC WEIGHT FOR BASELINE CONFIGURATION OF 243 PASSENGERS. CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS. 2. FWD CARGO = 1,070 CU FT (30.3 CU M). AFT CARGO = 1,312 CU FT (37.2 CU M). D6-58327 REV H December 2024 2-10 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.2 GENERAL DIMENSIONS 2.2.1 General Dimensions: Model 757-200, -200PF D6-58327 REV H December 2024 2-11 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.2.2 General Dimensions: Model 757-300 D6-58327 REV H December 2024 2-12 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.3 GROUND CLEARANCES 2.3.1 Ground Clearances: Model 757-200, 200PF Dimension MINIMUM MAXIMUM MODEL FT - IN M FT - IN M APPLICABILITY A 20 - 6 6.25 21 - 2 6.45 -200, -200PF B 7 - 4 2.24 8 - 0 2.44 -200, -200PF C 12 - 5 3.79 13 - 2 4.01 -200 D 8 - 1 2.46 8 - 9 2.67 -200, -200PF E 12 - 7 3.84 13 - 2 4.01 -200 F 12 - 9 3.89 13 - 3 4.04 -200 G 7 - 9 2.36 8 - 3 2.51 -200, -200PF H 8 - 6 2.59 9 - 1 2.77 -200 J 12 - 9 3.89 13 - 7 4.14 -200 K 44 - 3 13.49 45 - 1 13.74 -200, -200PF L 2 - 5 0.74 2 - 10 0.86 -200, -200PF M 15 - 4 4.67 16 - 1 4.90 -200, -200PF N 12 - 5 3.78 13 - 3 4.04 -200, -200PF O 18 - 7 5.66 19 - 8 5.99 -200, -200PF P 12 - 5 3.79 13 - 2 4.01 -200PF Q 12 - 6 3.81 13 - 2 4.01 -200PF 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. * NOMINAL DIMENSIONS D6-58327 REV H December 2024 2-13 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.3.2 Ground Clearances: Model 757-300 Dimension MINIMUM MAXIMUM FT - IN M FT - IN M A 20 - 7 6.27 21 - 4 6.50 B 7 - 5 2.26 8 - 2 2.49 C 12 - 5 3.79 13 - 2 4.01 D 8 - 0 2.44 8 - 9 2.67 E 12 - 7 3.84 13 - 2 4.01 F 12 - 11 3.94 13 - 4 4.06 G 7 - 6 2.29 7 - 10 2.39 J 13 - 0 3.96 13 - 4 4.06 K 44 - 6 13.56 44 - 9 13.64 L (RB211) 3 - 0 0.91 3 - 7 1.09 L (PW2043) 2 - 8 0.81 3 - 3 0.99 M 16 - 1 4.90 16 - 6 5.03 N (TAIL SKID) 9 - 0 2.74 9 - 4 2.85 O 18 - 10 5.74 19 - 1 5.82 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. * NOMINAL DIMENSIONS D6-58327 REV H December 2024 2-14 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4 INTERIOR ARRANGEMENTS 2.4.1 Interior Arrangements: Model 757-200, Overwing-Exit Airplane D6-58327 REV H December 2024 2-15 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.2 Interior Arrangements: Model 757-200, Four-Door Airplane D6-58327 REV H December 2024 2-16 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.3 Interior Arrangements: Model 757-200PF, Main Deck Cargo D6-58327 REV H December 2024 2-17 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.4.4 Interior Arrangements: Model 757-300 D6-58327 REV H December 2024 2-18 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.5 CABIN CROSS SECTIONS: MODEL 757-200, -300 D6-58327 REV H December 2024 2-19 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.6 LOWER CARGO COMPARTMENTS 2.6.1 Lower Cargo Compartments: Model 757-200, -300, Bulk Cargo Capacities D6-58327 REV H December 2024 2-20 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.6.2 Lower Cargo Compartments: Model 757-200, -300, Bulk Cargo Capacities • SYSTEM AVAILABLE IN EITHER OR BOTH CARGO COMPARTMENTS • FORWARD CARGO COMPARTMENT USES A THREE-MODULE SYSTEM AFT OF THE CARGO DOOR • AFT CARGO COMPARTMENT USES A TWO-MODULE SYSTEM FORWARD OF THE CARGO DOOR BULK CARGO CAPACITIES - TELESCOPING SYSTEM TOTAL(1) FWD COMPARTMENT AFT COMPARTMENT 3 MODULES ADD’L BULK 2 MODULES ADD’L BULK VOLUME CU FT 420 220 420 630 1,690 CU M 11.9 6.2 11.9 17.8 47.8 NOTE: 1. OPTIONAL THIRD CARGO DOOR REDUCES VOLUME BY 100 CU FT D6-58327 REV H December 2024 2-21 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7 DOOR CLEARANCES 2.7.1 Door Clearances: Model 757-200, -300, Passenger, Service and Cargo Door Locations DOOR NAME DISTANCE FROM NOSE (1) – 757-200 DISTANCE FROM NOSE (1) – 757-200 DOOR OPENING SIZE NO. 1 PASSENGER DOOR (LH) 16 FT 7 IN (5.05 M) 16 FT 7 IN (5.05 M) 33 BY 72 IN (0.84 BY 1.83 M) NO. 1 SERVICE DOOR (RH) 15 FT 8 IN (4.78 M) 15 FT 8 IN (4.78 M) 30 BY 65 IN (0.76 B7 1.65 M) NO. 2 PASSENGER DOOR (LH & RH) 45 FT 11 IN (13.99 M) 45 FT 11 IN (13.99 M) 33 BY 72 IN (0.84 BY 1.83 M) NO. 3 EXIT DOOR (LH & RH) (N/A) 121 FT 4 IN (35.99 M) 24 BY 44 IN (0.61 BY 1.18 M) NO. 4 PASSENGER DOOR (LH & RH) 125 FT 5 IN (38.23 M) 148 FT 9 IN (45.34 M) 30 BY 72 IN (0.76 BY 1.83 M) FWD CARGO DOOR (RH) 35 FT11 IN (10.95 M) 35 FT11 IN (10.95 M) 55 BY 42.5 IN (1.40 BY 1.08 M) AFT CARGO DOOR (RH) 104 FT 3 IN (31.78 M) 127 FT 7 IN (38.89 M) 55 BY 45 IN (1.40 BY 1.14 M) BULK CARGO DOOR (2) 117 FT 3 IN (35.74 M) (N/A) 48 BY 32 IN (1.22 BY 0.81 M) NOTES: 1. LONGITUDINAL DISTANCE FROM NOSE TO CENTER OF DOOR 2. EARLY PRODUCTION 757-200 AIRPLANES ONLY D6-58327 REV H December 2024 2-22 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.2 Door Clearances: Model 757-200, -300, Main Deck Door No 1 D6-58327 REV H December 2024 2-23 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.3 Door Clearances: Model 757-200, -300, Main Deck Door No 2 D6-58327 REV H December 2024 2-24 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.4 Door Clearances: Model 757-200, -300, Main Deck Door No 4 D6-58327 REV H December 2024 2-25 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.5 Door Clearances: Model 757-200, -300, Cargo Doors D6-58327 REV H December 2024 2-26 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 2.7.6 Door Clearances: Model 757-200PF, Main Deck Doors D6-58327 REV H December 2024 3-1 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 3.0 AIRPLANE PERFORMANCE 3.1 GENERAL INFORMATION The graphs in Section 3.2 provide information on operational empty weight (OEW) and payload, trip range, brake release gross weight, and fuel limits. To use this graph, if the trip range and zero fuel weight (OEW + payload) are known, the approximate brake release weight can be found, limited by fuel quantity. The graphs in Section 3.3 provide information on F.A.R. takeoff runway length requirements with typical engines at different pressure altitudes. Maximum takeoff weights shown on the graphs are the heaviest for the particular airplane models with the corresponding engines. Standard day temperatures for pressure altitudes shown on the F.A.R. takeoff graphs are given below: PRESSURE ALTITUDE STANDARD DAY TEMP FEET METERS °F °C 0 0 59.0 15.00 2,000 609 51.9 11.04 4,000 1,219 44.7 7.06 6,000 1,828 37.6 3.11 8,000 2,438 30.5 -0.85 Wet runway performance for the 757-300 airplane is shown in accordance with JAR-OPS 1 Subpart F, with wet runways defined in Paragraph 1.480(a)(10). Skid- resistant runways (grooved or PFC treated) per FAA or ICAO specifications exhibit runway length requirements that remove some or all of the length penalties associated with wet smooth (non-grooved) runways. Under predominantly wet conditions, the wet runway performance characteristics may be used to determine runway length requirements, if it is longer than the dry runway performance requirements. This is not required for the 757-200 airplanes. The graphs in Section 3.4 provides information on landing runway length requirements for different airplane weights and airport altitudes. The maximum landing weights shown are the heaviest for the particular airplane model. D6-58327 REV H December 2024 3-2 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 3.2 PAYLOAD/RANGE FOR LONG-RANGE CRUISE 3.2.1 Payload/Range for Long-Range Cruise: Model 757-200 (RB211- 535C Engines) D6-58327 REV H December 2024 3-3 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 3.2.2 Payload/Range for Long-Range Cruise: Model 757-200 (RB211-53E4, -535E4B Engines) D6-58327 REV H December 2024 3-4 Not Subject to EAR or ITAR. Copyright © 2024 Boeing. All Rights Reserved. 3.2.3 Payload/Range for Long-Range Cruise: Model 757-200, -200PF (PW2037, PW2040 Engines)