Airport Compatibility

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1 747X Quiet Longer Range Family Airport Compatibility April, 2002 Specific airport compatibility questions concerning commercial aircraft should be forwarded to: Airport Technology Boeing (Seattle, WA) Voice , Fax AO-0017 C PW/CG

2 Introduction This brochure provides airport compatibility data for the 747X Quiet Longer Range Family. This information is intended solely for airport planning purposes. All information in this brochure is preliminary and may change during development and testing. The XQLR is the latest derivative of the 747 family of airplanes and is being developed in both passenger and freighter versions. Based upon the ER, the XQLR has a higher gross weight, 921,000 lb (417,759 Kg) MTOW, to increase the range by 300 nmi. The XQLR Freighter improves upon the Freighter with an additional 700 nmi and is more environmentally friendly. To improve performance the XQLR will incorporate changes to the wing, including raked wingtips and trailing edge wedge. These improvements include lower noise, reduced fuel burn, more range, and faster cruise speed (Mach.86). The raked wingtip will increase the 747 s wingspan from today s 213 ft (64.9 meters) to 225 ft 3 inches (68.7 meters). The X Quiet Longer Range will see noise reductions of 20 percent on takeoff and 40 percent on approach, compared to today s s. The XQLR is expected enter into service in early WD CF/PW

3 General Airplane Characteristics XQLR CHARACTERISTICS UNITS TODAY'S XQLR XQLRF(FREIGHTER) MAX DESIGN POUNDS 877, , ,000 TAXI WEIGHT KILOGRAMS 397, , ,666 MAX DESIGN POUNDS 875, , ,000 TAKEOFF WEIGHT KILOGRAMS 396, , ,759 MAX DESIGN POUNDS 652, , ,000 LANDING WEIGHT KILOGRAMS 295, , ,093 MAX DESIGN ZERO POUNDS 555, , ,000 FUEL WEIGHT KILOGRAMS 251, , ,052 SPEC OPERATING POUNDS 398,800 (1) 411,000 (2) 364,300 EMPTY WEIGHT KILOGRAMS 180, , ,244 MAX STRUCTURAL POUNDS 156, , ,700 PAYLOAD KILOGRAMS 70,851 65, ,808 SEATING TWO-CLASS 524 = 42 FIRST ECONOMY 524 = 42 FIRST ECONOMY ---- CAPACITY THREE-CLASS 416 = 23 FC + 78 BC EC 416 = 23 FC + 78 BC EC ---- MAX CARGO CUBIC FEET 6,025 (3) 5,599 / 4,837 (4)/(5) 27,467 (6) CUBIC METERS / MAXIMUM FUEL CAPACITY US GALLONS 57,065 (7) 65,705 (8) 53,765 LITERS 216, , ,523 Notes: (1) SPEC OPERATING EMPTY WEIGHT FOR BASELINE CONFIGURATION OF 400 PASSENGER ARRANGEMENT AND STANDARD ITEM ALLOWANCES; ROLLS ROYCE ENGINES. CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS. (2) SPEC WEIGHT FOR BASELINE CONFIGURATION OF 416 PASSENGERS, EXPANDED TAIL TANK AND ONE BODY FUEL TANK / TWO BODY FUEL TANK (GE ENGINES). CONSULT WITH AIRLINE FOR SPECIFIC WEIGHTS AND CONFIGURATIONS (3) MAX CARGO LOWER DECK CONTAINERS (30) LD-1'S; or 5,332 CU FT - (5) PALLETS, (14) ld-1's + 1 PALLET BULK CARGO (4) FWD CARGO - (14) LD1's/ 2422 CU FT TOTAL AFT CARGO - (14) LD1'S/ 2422 CU FT TOTAL BULK CARGO CU FT (449 CU FT WITH 2 OPTIONAL CONTAINERS) (5) FWD CARGO - (4) 96" x 125" PALLETS / 1660 CU FT TOTAL AFT CARGO - (14) LD1'S / 2422 CU FT TOTAL BULK CARGO CU FT (449 CU FT WITH 2 OPTIONAL CONTAINERS) (6) MAIN DECK - 21,347 CU FT (30 PALLETS, 96IN. X 125 IN); (LOWER DECK - 5,600 CU FT (32 LD-1 CONTAINERS); BULK CARGO CU FT (7) OPTIONAL TAIL FUEL OF 3,300 US GAL (8) 5,500 USG (EXPANDED TAIL FUEL) AND TWO AUXILIARY BODY FUEL TANKS IN FWD LOWER CARGO HOLD; FUEL CAPACITY WITH ONE BODY TANK IS 60,495 US GAL (228,990L) 797-WT DD/PW

4 General Arrangement X Quiet Longer Range 225 ft 3 in (68.7 m) 72 ft 2 in (22.0 m) 63 ft 5 in (19.3 m) 12 ft 7 in (3.8 m) 36 ft 1 in (11.0 m) 231 ft 10 in (70.7 m) 797-CO CF

5 Interior Arrangement XQLR Tri-Class Seating, Long-Range Rules In-flight overhead crew rest 8 bunks and 2 seats 40 business 23 first 61-in pitch 38 business 39-in pitch 315 economy 32-in pitch 416 passengers XQLR same size as current LO CF

6 Payload-Range Capability 747XQLR General Electric Engines / CF6-80C2B1F 875,000 lb MTOW 398,800 lb OEW 7,260 nmi Design Range ER / CF6-80C2B5F 910,000 lb MTOW 405,300 lb OEW 7,500 nmi Design Range XQLR / CF6-80C2B10F 910,000 lb MTOW 409,400 lb OEW 7,875 nmi Design Range Payload 1000 lb Passengers XQLR / CF6-80C2B10 F 910,000 lb MTOW 409,400 lb OEW 7,715 nmi Design Range XQLR / CF6-80C2B10F 921,000 lb MTOW 411,000 lb OEW 8,000 nmi Design Range 60 1 Body Tank & Extended Tail Tank 62,575 2 Body Tanks & Extended Tail Tank 65,785 Fuel Capacity (US Gallons) 40 1 Body Tank 60, Body Tank 60,275 57,065 Typical Mission Rules Standard Day Nominal Fuel Burn Mach lb / Passenger 6.7 lb / US Gallon Range ~ 1000 nmi 797-PR whp/PW

7 Payload 1000 lb Passengers Payload-Range Capability 747XQLR Pratt & Whitney Engines / PW ,000 lb MTOW 399,600 lb OEW 7,325 nmi Design Range ER / PW ,000 lb MTOW 406,100 lb OEW 7,575 nmi Design Range XQLR / PW ,000 lb MTOW 409,200 lb OEW 7,920 nmi Design Range XQLR / PW ,000 lb MTOW 409,200 lb OEW 7,780 nmi Design Range XQLR / PW ,000 lb MTOW 410,800 lb OEW 8,050 nmi Design Range Body Tank & Extended Tail Tank 62,795 1 Body Tank 60,495 2 Body Tanks & Extended Tail Tank 66,005 Fuel Capacity (US Gallons) 20 1 Body Tanks 60,495 57,285 Typical Mission Rules Standard Day Nominal Fuel Burn Mach lb / Passenger 6.7 lb / US Gallon Range ~ 1000 nmi 797-PR whp/PW

8 Payload-Range Capability 747XQLR Freighter 300 (120) (100) Cargo density 9 lb per ft kg per m 3 8 lb per ft kg per m F 875K MTOW 610K MZFW ERF 910K MTOW 611K MZFW (80) Payload, 1,000 lb (60) (1,000 kg) lb per ft kg per m XQLRF 910K MTOW 611K MZFW (40) 100 (20) 50 Fuel capacity, U.S. gal (L) 53,765 (203,504) (0) (0) (5) (10) (15) GE engines Typical mission rules Range, 1,000 nmi (1,000 km) Nominal fuel burn 85% annual winds 6.7 lb per U.S. gal fuel density 797-PR whp

9 Takeoff Field Length (1,000 ft) Field Length Range XQLR XQLR / PW4062 MTOW 921,000 lb OEW 411, ,800 lb 416 Passengers 65,758 66,005 USG Fuel Capacity / 2 Body Tanks XQLR / PW4062 MTOW 910,000 lb OEW 409, ,200 lb 416 Passengers 62,575 62,795 USG Fuel Capacity / 1 Body Tank 5,000 ft Field Elevation Sea Level Field Elevation Flaps 20 Takeoff Zero Wind & Slope ISA + 15 C Takeoff Temp Typical Mission Rules Standard Day Cruise Temp Nominal Fuel Burn 210 lb/pax 6.7 lb/usg Fuel Density 4 1,000 2,000 3,000 4,000 5,000 6,000 7,000 8,000 9,000 Range (nmi) 797-AO whp

10 Takeoff Field Length (1,000 ft) Field Length Range XQLR XQLR / CF6-80C2B10F MTOW 921,000 lb OEW 411,000 lb 416 Passengers 65,758 65,785 USG Fuel Capacity / 2 Body Tanks XQLR / CF6-80C2B10F MTOW 910,000 lb OEW 409,400 lb 416 Passengers 62,575 USG Fuel Capacity / 1 Body Tank 5,000 ft Field Elevation Sea Level Field Elevation Flaps 20 Takeoff Zero Wind & Slope ISA + 15 C Takeoff Temp Typical Mission Rules Standard Day Cruise Temp Nominal Fuel Burn 210 lb/pax 6.7 lb/usg Fuel Density 4 1,000 2,000 3,000 4,000 5,000 6,000 7,000 8,000 9,000 Range (nmi) 797-AO whp

11 Fillet Requirements XQLR* 45 Notes: Symmetrical thrust Mid CG Body gear steering inoperative No differential braking Before determining the size of intersection fillets, consult using airlines or airport authority regarding operating procedures and aircraft types expected to serve the airport Approximate path of outside edge of wing gear tires R = 100 ft (30m) Modified fillet Runway-to-taxiway centerline of turn R = 100 ft (30m) 75 ft (23m) 150 ft (45m) Nose gear tracking centerline to centerline * Fillet requirements are the same as the family (except SP) 797-AO DD/PW

12 Fillet Requirements XQRL* 75 ft (23m) Approximate path of outside edge of wing gear tires 75 ft (23m) Approximate 16 ft (5m) (both sides) R = 100 ft (30m) Runway-to-taxiway centerline of turn Notes: Symmetrical thrust Mid CG Body gear steering inoperative No differential braking Before determining the size of intersection fillets, consult using airlines or airport authority regarding operating procedures and aircraft types expected to serve the airport Approximate path of outside edge of wing gear tires 7 ft (2m) Modified fillet R = 100 ft (30m) Approximate path of nose gear 150 ft (45m) Approximate path of nose gear 150 ft (45m) Nose gear tracking beyond intersecting taxiway centerline (judgemental oversteering) * Fillet Requirements are the same as family (except SP) Nose gear tracking centerline to centerline 797-AO DD/PW

13 Nose/Body Gear Turn Ratios XQLR* Max 70 Nose gear Wing gear Turn center Body gear Max 13 Body gear angle (Deg) Gear nearest turn center Gear farthest from turn center Nose gear Body gear 0 (Deg) to 20 (Deg) 0 (Deg) 20 (Deg) to 70 (Deg) 0 (Deg) to 13 (Deg) Nose gear angle (Deg) * Turn ratios are the same as family (except SP) 797-AO DD/PW

14 Turning Radius Requirements XQLR NOTE: CONSULT AIRLINE FOR OPERATING PROCEDURES X RADIUS (FEET) Z (3) A (4) B (3) C (3) D E WING TIP NOSE GEAR WING GEAR TAIL TIP NOSE TURN RADIUS (FEET) MINIMUM WIDTH FOR 180 TURN (1) (2) (1) (2) (1) (2) (1) (2) (1) (2) (1) (2) (1) BODY GEAR STEERING INOPERATIVE (2) WITH BODY GEAR STEERING (3) MEASURED TO OUTSIDE TIRE FACES (4) WINGSPAN AT 225 FT 3 IN CLEARANCE RADII - ENGLISH UNITS MODEL X QLR 797-AO DD

15 Landing Gear Footprint XQLR* Not to Scale 78 FT 11.5 IN (24.07 M) 10 FT 1 IN (3.07 M) 36 IN (0.91 M) 40 FT 11 IN (12.5 M) 36 FT 1 IN (11.00 M) TYP. 12 FT 7 IN (3.84 M) 44 IN (1.12 M) TYP. BASELINE AIRPLANE Characteristics Units XQLR Max Design Pounds 923,000 Taxi Weight Kilograms 419,000 Nose Gear Tire Size Inches 49X17 (32PR) [49X19 (32PR) OPT] Nose Gear PSI 185 Tire Pressure KG/CM 2 13 Wing Gear Tire Size Inches 50X20.0R22 (34PR) Wing Gear PSI 225 Tire Pressure KG/CM Main Gear Tire Size Inches 50X20.0R22 (34PR) Main Gear PSI 225 Tire Pressure KG/CM IN (1.47 M) TYP. * Foot print the same as family (except SP) 797-AO DD/PW

16 Aircraft Classification Number XQLR Rigid and Flexible Pavement 110 Aircraft Classification Number (ACN) Flexible Rigid CODE A - CBR 15 (HIGH) CODE B - CBR 10 (M EDIUM ) CODE D - CBR 3 (ULTRA LOW) CODE C - CBR 6 (LOW) CODE D - K=75 (ULTRA LOW) CODE C - K=150 (LOW) CODE B - K=300 (M EDIUM ) CODE A - K=550 (HIGH) Aircraft Gross Weight (x 1,000 lb) 797-AO DD

17 The XQLR Is a Quiet Neighbor XQLR Noise Area Reduced by 40% Over % smaller area Base K MTOW 3.41 mi K MTOW 7.74 mi XQLR 875K MTOW 2.07 mi 2 5,000 (1,000) 40,000 (15,000) 60,000 Distance from centerline, ft (m) (1,000) 5, ,000 (5,000) (10,000) Distance from brake release, ft (m) 85-dBA contour comparison; takeoff with cutback; ICAO B 797-NO SF/DD

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