Airport Compatibility Brochure 737 MAX. March 2014 PRELIMINARY

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Airport Compatibility Brochure 737 MAX March 2014 BOEING is a trademark of Boeing Management Company. Copyright 2013 Boeing. All rights reserved. PRELIMINARY Specific airport compatibility questions concerning Boeing commercial aircraft should be forwarded to: Airport Compatibility Engineering (Seal Beach, CA) Voice: 1-562-797-1172 Fax: 1-562-797-1524 E-mail: airportcompatibility@boeing.com

Introduction This brochure provides airplane characteristics for the 737 MAX family models that have an impact on airport compatibility. This information is intended solely for airport planning purposes. All information for the 737 MAX is preliminary and may change during development and testing. More detailed data for these models will be found in the Airplane Characteristics for Airport Planning document (ACAP) to be published at a future date. The 737 MAX are derivative aircraft of the 737-700/800/900ER, respectively. The 737 MAX 8 is scheduled to enter into service in the third quarter of 2017 while 737 MAX 9 and 737 MAX 7 are planned to enter into service in 2018 and 2019, respectively. PRELIMINARY Slide 2

737 MAX 7 General Arrangement * Static ground line condition, all gears approximately 80% compressed PRELIMINARY Slide 3

737 MAX 8 General Arrangement * Static ground line condition, all gears approximately 80% compressed PRELIMINARY Slide 4

737 MAX 9 General Arrangement * Static ground line condition, all gears approximately 80% compressed PRELIMINARY Slide 5

Weight Comparisons with 737-700/800/900ER Characteristics Unit 737 MAX 7 737-700 with Winglet 737 MAX 8 737-800 with Winglet 737 MAX 9 737-900ER with Winglet Max Design Taxi Weight Max Design Takeoff Weight Max Design Landing Weight Max Design Zero Fuel Weight Max Design Fuel Capacity lb 160,000 155,000 181,700 174,700 195,200 188,200 kg 72,575 70,307 82,418 79,243 88,541 85,366 lb 159,500 154,500 181,200 174,200 194,700 187,700 kg 72,348 70,080 82,191 79,016 88,314 85,139 lb 135,500 129,200 152,800 146,300 163,900 157,300 kg 61,462 58,604 69,309 66,361 74,344 71,350 lb 128,600 121,700 145,400 138,300 156,500 149,300 kg 58,332 55,202 65,952 62,732 70,987 67,721 US gallon 6,853 6,875 6,853 6,875 6,853 6,875 liter 25,941 26,024 25,941 26,024 25,941 26,024 PRELIMINARY Slide 6

Size Comparisons with 737-700/800/900ER 737 MAX 7 Wing Span (ft-in/m) 117-10 / 35.92 737-700 with Winglet 737 MAX 8 117-5 / 35.79 117-10 / 35.92 737-800 with Winglet 737 MAX 9 117-5 / 35.79 117-10 / 35.92 737-900ER with Winglet - ICAO Code Letter C C C C C C - FAA Design Group III III III III III III Overall Length (ft-in/m) 110-4 / 33.63 110-4 / 33.63 129-6 / 39.47 129-6 / 39.47 138-2 / 42.11 - ICAO RFF Category 6 6 7 7 7 7 - FAA ARFF Index B B C C C C 117-5 / 35.79 138-2 / 42.11 PRELIMINARY Slide 7

737 MAX Ground Clearances Nose gear is lengthened by 8 inches, compared with 737NG. 737 MAX 7 737 MAX 8 737 MAX 9 Description Max. Min. Max. Min. Max. Min. ft-in m ft-in m ft-in m ft-in m ft-in m ft-in m A Top of Fuselage 18-11 5.77 18-6 5.64 18-11 5.77 18-6 5.64 19-0 5.79 18-7 5.66 B Entry Door No 1 9-11 3.02 9-1 2.77 10-1 3.07 9-2 2.79 10-1 3.07 9-2 2.79 C FWD Cargo Door 5-4 1.63 4-8 1.42 5-6 1.68 4-8 1.42 5-6 1.68 4-9 1.45 D Engine 1-11 0.58 1-5 0.43 1-11 0.58 1-5 0.43 1-11 0.58 1-5 0.43 E Top of Winglet 20-3 6.17 19-6 5.94 20-3 6.17 19-6 5.94 20-3 6.17 19-6 5.94 F Aft Cargo Door 5-5 1.65 4-6 1.37 5-4 1.63 4-5 1.35 5-4 1.63 4-4 1.32 G Entry Door No 2 9-8 2.95 8-4 2.54 9-6 2.90 8-3 2.51 9-5 2.87 8-3 2.51 H Stabilizer 17-10 5.44 15-10 4.83 17-7 5.36 15-9 4.80 17-6 5.33 15-9 4.80 J Vertical Tail 41-0 12.50 39-0 11.89 40-9 12.42 38-11 11.86 40-8 12.40 38-11 11.86 K Bottom of Winglet 10-9 3.28 10-0 3.05 10-9 3.28 10-0 3.05 10-9 3.28 10-0 3.05 Notes: 1. Clearances shown are preliminarily nominal values and subject to change during the aircraft configuration development. Numbers are rounded to nearest whole inch. 2. During routine servicing, the airplane remains relatively stable, pitch and elevation changes occur slowly. PRELIMINARY Slide 8

737 MAX 7 Interior Arrangement (typical) Dual Class - 126 Passengers 8 First Class 36 in. Pitch 118 Economy Class 31 in. Pitch 36 Seats at 32 in. Pitch Single Class 140 Passengers 32 in. Pitch 24 Seats at 31 in. Pitch PRELIMINARY Slide 9

737 MAX 8 Interior Arrangement (typical) Dual Class -162 Passengers 12 First Class - 36 in. Pitch 150 Economy Class 32 in. pitch Single Class -175 Passengers 32 in. Pitch 18 Seats at 31 in. Pitch PRELIMINARY Slide 10

737 MAX 9 Interior Arrangement (typical) Dual Class - 180 Passengers 12 First Class 36 in. Pitch 168 Economy Class 32 in. Pitch Single Class - 204 Passengers 30 in. Pitch PRELIMINARY Slide 11

737 MAX Cargo Compartments PRELIMINARY Slide 12

737 MAX Door Locations All 737 MAX 7 door locations remain the same as 737-700 with or without winglet. All 737 MAX 8 door locations remain the same as 737-800 with or without winglet. All 737 MAX 9 door locations remain the same as 737-900ER with or without winglet. Please refer to the following link to access the 737 Airplane Characteristics for Airport Planning (ACAP), Section 2.0 Airplane Description, for 737-700/800/900ER door locations: http://www.boeing.com/airports PRELIMINARY Slide 13

737 MAX Takeoff / Cruise / Landing Performance While the 737 MAX has its most improved performance in cruise, which will improve the payload range capability by a percentage, the 737 MAX may have slightly better performance in regards to field length limited takeoff and landing charts. Using the existing 737NG charts will be a conservative estimate. Please refer to the following link to access the 737 Airplane Characteristics for Airport Planning (ACAP), Section 3.0 Airplane Performance, for 737-700/800/900ER performance: http://www.boeing.com/airports Please consult with operating airlines for detailed airplane performance data. PRELIMINARY Slide 14

737 MAX Landing Gear Configuration 737 MAX 7 landing gear configuration remains the same as 737-700 with or without winglet. 737 MAX 8 landing gear configuration remains the same as 737-800 with or without winglet. 737 MAX 9 landing gear configuration remains the same as 737-900ER with or without winglet Maximum Design Taxi Weight Unit 737 MAX 7 737 MAX 8 737 MAX 9 lb 160,000 181,700 195,200 Kg 72,575 82,418 88,541 Nose Gear Tire Size In 27x7.75R15, 12PR 27x7.75R15, 12PR 27x7.75R15, 12PR Nose Gear Tire Pressure psi 185 185 185 kg/cm2 13.01 13.01 13.01 Main Gear Tire Size In H44.5X16.5R21, 30PR H44.5X16.5R21, 30PR H44.5X16.5R21, 32PR Main Gear Tire Pressure psi 184 213 230 kg/cm2 12.94 14.98 16.17 PRELIMINARY Slide 15

737 MAX Turning Capability 737 MAX 7 turning capability remains similar to 737-700 with or without winglet. 737 MAX 8 turning capability remains similar to 737-800 with or without winglet. 737 MAX 9 turning capability remains similar to 737-900ER with or without winglet Please refer to the following link to access the 737 Airplane Characteristics for Airport Planning (ACAP), Section 4.0 Ground Maneuvering, for 737-700/800/900ER turn capability: http://www.boeing.com/airports PRELIMINARY Slide 16

737 MAX Ground Servicing 737 MAX 7 ground servicing remains similar to 737-700 with or without winglet. 737 MAX 8 ground servicing remains similar to 737-800 with or without winglet. 737 MAX 9 ground servicing remains similar to 737-900ER with or without winglet Please refer to the following link to access the 737 Airplane Characteristics for Airport Planning (ACAP), Section 5.0 Terminal Servicing, for 737-700/800/900ER ground serving: http://www.boeing.com/airports PRELIMINARY Slide 17

737 MAX 7 Aircraft Classification Number (ACN) - Flexible Pavement PRELIMINARY Slide 18

737 MAX 7 Aircraft Classification Number (ACN) - Rigid Pavement PRELIMINARY Slide 19

737 MAX 8 Aircraft Classification Number (ACN) - Flexible Pavement PRELIMINARY Slide 20

737 MAX 8 Aircraft Classification Number (ACN) - Rigid Pavement PRELIMINARY Slide 21

737 MAX 9 Aircraft Classification Number (ACN) - Flexible Pavement PRELIMINARY Slide 22

737 MAX 9 Aircraft Classification Number (ACN) - Rigid Pavement PRELIMINARY Slide 23