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 1-425-237-0126, Fax 1-425-237-0860 E-mail: AirportTechnology@Boeing.com 797-AO-0017 C 3-27-2-PW/CG
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 747-400XQLR is the latest derivative of the 747 family of airplanes and is being developed in both passenger and freighter versions. Based upon the 747-400ER, the 747-400XQLR has a higher gross weight, 921,000 lb (417,759 Kg) MTOW, to increase the range by 300 nmi. The 747-400XQLR Freighter improves upon the 747-400 Freighter with an additional 700 nmi and is more environmentally friendly. To improve performance the 747-400XQLR will incorporate changes to the 747-400 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 747-400X Quiet Longer Range will see noise reductions of 20 percent on takeoff and 40 percent on approach, compared to today s 747-400s. The 747-400XQLR is expected enter into service in early 2004. 797-WD-0033 4-10-2-CF/PW
General Airplane Characteristics 747-400XQLR CHARACTERISTICS UNITS TODAY'S 747-400 747-400XQLR 747-400XQLRF(FREIGHTER) MAX DESIGN POUNDS 877,000 923,000 923,000 TAXI WEIGHT KILOGRAMS 397,801 418,666 418,666 MAX DESIGN POUNDS 875,000 921,000 921,000 TAKEOFF WEIGHT KILOGRAMS 396,893 417,759 417,759 MAX DESIGN POUNDS 652,000 652,000 666,000 LANDING WEIGHT KILOGRAMS 295,742 295,742 302,093 MAX DESIGN ZERO POUNDS 555,000 555,000 613,000 FUEL WEIGHT KILOGRAMS 251,744 251,744 278,052 SPEC OPERATING POUNDS 398,800 (1) 411,000 (2) 364,300 EMPTY WEIGHT KILOGRAMS 180,892 186,427 165,244 MAX STRUCTURAL POUNDS 156,200 144,000 248,700 PAYLOAD KILOGRAMS 70,851 65,317 112,808 SEATING TWO-CLASS 524 = 42 FIRST + 482 ECONOMY 524 = 42 FIRST + 482 ECONOMY ---- CAPACITY THREE-CLASS 416 = 23 FC + 78 BC + 315 EC 416 = 23 FC + 78 BC + 315 EC ---- MAX CARGO CUBIC FEET 6,025 (3) 5,599 / 4,837 (4)/(5) 27,467 (6) CUBIC METERS 149 158.5 / 137.0 778 MAXIMUM FUEL CAPACITY US GALLONS 57,065 (7) 65,705 (8) 53,765 LITERS 216,014 248,710 203,523 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 - 755 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 - 755 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 - 420 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-0008 4-16-02-DD/PW
General Arrangement 747-400X 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-0046 3-27-2-CF
Interior Arrangement 747-400XQLR 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 747-400XQLR same size as current 747-400 797-LO-0001 3-27-2-CF
180 160 140 Payload-Range Capability 747XQLR General Electric Engines 747-400 / CF6-80C2B1F 875,000 lb MTOW 398,800 lb OEW 7,260 nmi Design Range 747-400 ER / CF6-80C2B5F 910,000 lb MTOW 405,300 lb OEW 7,500 nmi Design Range 747-400 XQLR / CF6-80C2B10F 910,000 lb MTOW 409,400 lb OEW 7,875 nmi Design Range Payload 1000 lb 120 100 80 416 Passengers 747-400 XQLR / CF6-80C2B10 F 910,000 lb MTOW 409,400 lb OEW 7,715 nmi Design Range 747-400 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 60,275 20 1 Body Tank 60,275 57,065 Typical Mission Rules Standard Day Nominal Fuel Burn Mach 0.855 210 lb / Passenger 6.7 lb / US Gallon 0 5.0 5.5 6.0 6.5 7.0 7.5 8.0 8.5 9.0 9.5 10.0 Range ~ 1000 nmi 797-PR-0001 4-18-2-whp/PW
Payload 1000 lb 180 160 140 120 100 80 416 Passengers Payload-Range Capability 747XQLR Pratt & Whitney Engines 747-400 / PW4056 875,000 lb MTOW 399,600 lb OEW 7,325 nmi Design Range 747-400 ER / PW4062 910,000 lb MTOW 406,100 lb OEW 7,575 nmi Design Range 747-400 XQLR / PW4062 910,000 lb MTOW 409,200 lb OEW 7,920 nmi Design Range 747-400 XQLR / PW4062 910,000 lb MTOW 409,200 lb OEW 7,780 nmi Design Range 747-400 XQLR / PW4062 921,000 lb MTOW 410,800 lb OEW 8,050 nmi Design Range 60 40 1 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 0.855 210 lb / Passenger 6.7 lb / US Gallon 0 5.0 5.5 6.0 6.5 7.0 7.5 8.0 8.5 9.0 9.5 10.0 Range ~ 1000 nmi 797-PR-0002 4-18-2-whp/PW
Payload-Range Capability 747XQLR Freighter 300 (120) (100) 250 200 Cargo density 9 lb per ft 3 144.2 kg per m 3 8 lb per ft 3 128.1 kg per m 3 747-400F 875K MTOW 610K MZFW 747-400ERF 910K MTOW 611K MZFW (80) Payload, 1,000 lb (60) (1,000 kg) 150 7 lb per ft 3 112.1 kg per m 3 747-400XQLRF 910K MTOW 611K MZFW (40) 100 (20) 50 Fuel capacity, U.S. gal (L) 53,765 (203,504) (0) 0 0 1 2 3 4 5 6 7 8 9 10 (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-0003 3-27-2-whp
Takeoff Field Length (1,000 ft) 18 16 14 12 10 8 6 Field Length Range 747-400XQLR 747-400XQLR / PW4062 MTOW 921,000 lb OEW 411,000 410,800 lb 416 Passengers 65,758 66,005 USG Fuel Capacity / 2 Body Tanks 747-400XQLR / PW4062 MTOW 910,000 lb OEW 409,400 409,200 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-0018 3-27-2-whp
Takeoff Field Length (1,000 ft) 18 16 14 12 10 8 6 Field Length Range 747-400XQLR 747-400XQLR / CF6-80C2B10F MTOW 921,000 lb OEW 411,000 lb 416 Passengers 65,758 65,785 USG Fuel Capacity / 2 Body Tanks 747-400XQLR / 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-0019 3-27-2-whp
Fillet Requirements 747-400XQLR* 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 747-400 family (except SP) 797-AO-0023 4-10-02-DD/PW
Fillet Requirements 747-400XQRL* 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 747-400 family (except SP) Nose gear tracking centerline to centerline 797-AO-0022 4-10-02-DD/PW
Nose/Body Gear Turn Ratios 747-400XQLR* Max 70 Nose gear Wing gear Turn center Body gear Max 13 Body gear angle (Deg) 13 0 13 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) 70 65 20 0 20 65 70 Nose gear angle (Deg) * Turn ratios are the same as 747-400 family (except SP) 797-AO-0021 4-10-02-DD/PW
Turning Radius Requirements 747-400XQLR 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) 40 163 165 96 91 61 61 142 146 117 112 156 152 60 182 184 106 102 81 81 154 158 125 120 187 183 80 201 202 119 115 101 101 167 171 136 132 219 216 100 220 222 133 130 121 121 182 185 148 145 254 251 120 240 241 149 146 141 141 197 200 162 159 290 287 140 259 260 166 163 161 161 213 216 178 175 327 324 160 279 280 183 181 181 181 230 233 194 191 364 362 (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 747-400X QLR 797-AO-0020 3-28-02-DD
Landing Gear Footprint 747-400XQLR* 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 747-400XQLR 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 2 15.8 Main Gear Tire Size Inches 50X20.0R22 (34PR) Main Gear PSI 225 Tire Pressure KG/CM 2 15.8 58 IN (1.47 M) TYP. * Foot print the same as 747-400 family (except SP) 797-AO-0024 4-10-02-DD/PW
Aircraft Classification Number 747-400XQLR Rigid and Flexible Pavement 110 Aircraft Classification Number (ACN) 100 90 80 70 60 50 40 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) 30 20 550 600 650 700 750 800 850 900 Aircraft Gross Weight (x 1,000 lb) 797-AO-0025 3-27-02-DD
The 747-400XQLR Is a Quiet Neighbor 747-400XQLR Noise Area Reduced by 40% Over 747-400 40% smaller area Base 747-400 875K MTOW 3.41 mi 2 747-200 833K MTOW 7.74 mi 2 747-400XQLR 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 0 20,000 (5,000) (10,000) Distance from brake release, ft (m) 85-dBA contour comparison; takeoff with cutback; ICAO B 797-NO-0055 5-16-2-SF/DD