FlightGlobal.com
Home
Premium
Archive
Video
Images
Forum
Atlas
Blogs
Jobs
Shop
RSS
Email Newsletters
You are in:
Home
Aviation History
1969
1969 - 0471.PDF
a 9 10 fl* 13 14 IS l« 17 18 19 DO Douglas DC-10-30 Intercontinental Accommodation Standard mixed-class configuration total 270 seats) I Crew and passenger door and Type A exits 32in • 76in Underfloor galley (occupies 1,350 cu ft) Twin lifts between galley and main deck Food and beverage trolley Food trolley loading pack Galley attendants' folding seats Emergency ladder Passenger entry door 42in 76in (up and over type) three per side First-class seating (six abreast. 38in pitch) Forward cargo hold, volume 1,390 cu ft (containerised 960 cu ft; half- . containers shown) Forward hold door (electrically powered) 70m - 66in (single entry for galley servicing and cargo loading) Coach-class seating (eight-abreast. 34in pitch) Overhead luggage lockers Cabin attendant's seat (at each vestibule) Lavatory (two in the first-class section) Rear cargo hold 1,590 cu ft (con tainerised 1.280 cu ft). Electrically powered door 70in - 66in Bulk cargo hold (door 44in 48in) volume 870 cu ft Cabin windows (I lin I6in) Lavatory (five for tourist-class section) Structure: Fuselage St Afterbody tail-cone of multiple frames and stringers, upper frames aligned with fin-spars. Engine maintenance platforms incor porated 52 Pressure bulkhead 53 Transverse and circumferential skin breaks with finger-style doubters 54 Centre-section fuselage main frames (wing/fusetage junction) built up from forged alloy and rolled sections. Plain sheet skin stabilised by multiple longitudinal intercostals 55 "I" section transverse floor beams 56 Forged alloy floor beams over under-carriage bay 57 Sheer-web beams supporting the floor pressure panel 58 Undercarriage-bay pressure bulk head 59 Keel box spanning main under carriage bay opening SfO Vertical tie beam—machine forg ing SI I Centre-undercarriage bay 512 Shear-webs over centre-wing fuel tank support pressure floor 513 Titanium frame between wing rear spar and fuselage frames also carries main undercarriage side brace 514 Wing/fuselage titanium "T" sec tion longeron V^ SIS SI* SI7 SI9 S20 S2I Centre-section from beam Extruded frames and stringers Sandwich construction floor panels carry seat tracks "I" section beams reduced depth over galley Unpressurised nosewheel bay Windscreen: twin flat front panels of five-ply glass vinyl laminated: single-curve clear-view windows: and two double-curve side win dows Front pressure bulkhead Fin and Rudder S22 Fin torsion box. Four spars, multi ple ribs, integrally stiffened skins. Single-piece forged ring spars (aluminium alloy 7075-T73) around air inlet are oversized for growth engines Fin leading-edge and tip remov able (light-alloy skin/rib) Fin/rudder shrouds (light alloy bonded) Two-piece double-hinged rudder (single spar and ribs, aluminium sheet skin panels with bonded scalloped doubier, glass-fibre rein forced plastic trailing-edge) MB I S23 S24 S25 continued on page 410
Sign up to
Flight Digital Magazine
Flight Print Magazine
Airline Business Magazine
E-newsletters
RSS
Events
