Draft ICAO Circular on NLA.pdf - Airports Council International

More documents

Recommendations

Info

Aeroplane Dimensions A380-800 <strong>ICAO</strong> Version 4.1 — 15 March 2004 A-2 Code F Code E B747- Advanced* C5 An 124 A340-600 B747- 400ER B777- 300ER Maximum wing tip height at OEW 8.3 m ~5.7 m 4.0 m Unknown 7.8 m 7.3 m 7.5 m Cockpit view at OEW: - Cockpit height - Cockpit cut-off angle - Obscured segment 7.2 m 20° Max.19.8 m 8.7 m 18.4° 25.8 m 8.2 m unknown unknown 8.3 m unknown unknown 5.7 m 20° 15.7 m 8.7 m 18.4° 25.8 m 5.9 m 21° 14.6 m Taxi camera Yes No No No Yes No Yes Pilot-to-nose landing gear distance 2.1 m 2.3 m 5.0 m 2.4 m 4.3 m 2.3 m 3.6 m Pilot-to-main landing gear distance 31.8 m 28.4 m 29.9 m** 27.2 m 25.3 m 37.4 m 26.4 m 34.2 m ~ symbol indicates “approximate” * B747-Advanced is a proposed aircraft (not yet launched) and, therefore, the specifications are subject to change. ** Freighter version values provided where appropriate *** Highest door at OEW # For aircraft with large winglets (significant wing and winglet deflection with full fuel) ## For aircraft without winglets, reference frequently made to “jig” span, i.e. the span as measured in the manufacturing jig (straight wing without 1G droop). Landing gear geometry A380-800 Weights MRW MTOW MLW Landing gear dimensions Table 3: Landing gear geometry 562 t 602 t** 560 t 600 t** 386 t 427 t** Code F Code E B747- Advanced* C5 An 124 A340-600 B747- 400ER B777- 300ER 4232 t 437 t** 381 t 405 t 369 t 414 t 341 t 422 t 435 t** 379.6 t 398 t 368 t 296 t 333 t** 288.4 t 330 t 256 t 413 t 340 t 296 t 302 t** 251 t Wheel track 12.5 m 11.0 m 7.9 m 6.3 m 10.7 m 11.0 m 11.0 m Outer main gear wheel span 14.3 m 12.7 m 11.4 m 8.0 m 12.6 m 12.6 m 12.9 m Wheelbase 29.7 m 26.1 m 27.6 m** 22.2 m 22.9 m 33.1 m 24.1 m 30.6 m Main gear steering system*** Yes Yes Yes Yes No Yes Yes
Landing gear geometry A380-800 ACN - Flexible FA FB FC FD ACN - Rigid RA RB RC RD 63 66** 69 73** 83 87** 111 116** 55 58** 68 72** 89 94** 110 117** A-3 Code F Code E B747- Advanced* C5 An 124 A340-600 B747- 400ER B777- 300ER 63 65** 29 51 70 61 62 71 72** 33 60 75 69 69 88 90** 40 77 89 85 86 111 114** 56 107 119 108 117 61 62** 29 35 62 59 64 71 72** 34 48 72 69 82 83 85** 44 73 84 81 105 94 97** 55 100 98 92 127 Discussions on the value of alpha factor is ongoing. Aircraft footprints and ACN curves are available in Section 7 of the respective “Airplane Characteristics for Airport Planning” document in the manufacturers Web site (Appendix B). * B747-Advanced is a proposed aircraft (not yet launched) and, therefore, the specifications are subject to change. ** Freighter version values provided where appropriate. *** There are two types of main landing gear steering system – post steering with all wheels steered (747, C5 and An 124), aft-axle steering (aft two wheels out of 6-wheel gear, e.g. A380-800 and 777). The effect of main gear steering system on turn center location is shown in the Section 4.3 of the respective “Airplane Characteristics for Airport Planning” document in the manufacturer Web site (Appendix B). Table 4: Minimum pavement width required for U-turn (in ascending order) Code Aircraft U-turn width Wheelbase Track (to outside tire edge) E 747-400 152' (46.3 m) 79.0' (24.1 m) 41.3' (12.6 m) D MD11 161 (49) 81.2 (24.7) 41.2 (12.6) F 747-Adv 163' (49.7) 85.6 (26.1) 41.3 (12.6) <strong>ICAO</strong> Version 4.1 — 15 March 2004
Page 1 and 2:
NLACircularVersion
Page 3 and 4:
- iii - 4.1.4 Taxiway and shoulders
Page 5 and 6:
- v - The Circular
Page 7 and 8: ICAO Version 4.1
Page 11 and 12: f) wake turbulence; g) selection of
Page 13 and 14: d) wake turbulence. ICAO</s
Page 57: Wing span Outer main gear wheel spa
Page 61 and 62: Maximum passenger and fuel carrying
Page 63 and 64: OFZ/runway width and other OPS/AIR
Page 69: ICAO Version 4.1
show all

Draft ICAO Circular on NLA.pdf - Airports Council International

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?