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l9 - r".1 60° rf'1 500 High Capacity 1" flan-Hm...

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Unformatted text preview: r" .1: 60° \ rf' '1 . 500 High Capacity 1" flan-Hm 400 Seats 300 Existing .- Widebfldies ' Lang Flange 209- 'Iflfl-fiflfl seats " Internatinnal 100 70-100 Seats 30-55 Seats Range ~ 1000 nmi . . -_ 957; ASMfi’I/eeasts Will Define :fFi'rs’t'ifiut" Fleet Expansion Malawi} fiat Mil??? MSW} Existing 4- Retirement: Ownership Indirect costs Overhead Administrative Non-flying assets Fixed cost Crew . Fuel Variable cost Fees Ops support 451'me The Interior Design . . . ...... . mmrmw mum-in um “Study" 5"" optimum\ . | ! "I'r' Fuselage Mum no: passenger ~ft3 “at ~« I w:- [UH-"'41!“- Il|'|.|" Ill'li - - '- "l I '. 'i !'I 1“ IE- illil'li '|"-| I Two Basic Objectives: 1. Reduce airplane acquisition, operational, and maintenance costs. 2. Preserve product differentiation for each airline. f .' I/J H H 5 NR; \ I”i. /e Airfane is Assembled as a "Frozen Tub'e'i r' i. .' -_. m 1m m J is imim to: all. customm 1 (mm m bins. Imam "mm it!!! May Aitlin'g‘finlque Features Are Installed I. \ _at'a "Finlshing Center" .a-“H 4r -._ Hf _ _ I .e' . --- I ll' m i f ' --/ ' H“ ' ‘ StandaKIzatIon Results" In Savings by the Manufacturer _'l'hat Can be Passed to the Airline I I "One build fits all” . ”I I No unique engineering required. ‘I, I No out-of-posltion Installations. I No special checkout or test procedures. I Support system costs can be minimiled . I Consistent products developed as basellne I for all airplanes. . I “One pass" revision scenario for all services. I Standardization IIIIIII taeilllate common industry problemalvlng. ' r‘ ...
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