Transcription of STL 945.7136/97
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STL 945.7136/97
STL and systemsbriefingfor pilotsTHIS BROCHURE IS PROVIDEDFOR INFORMATION PURPOSES ONLYAND ITS CONTENTSWILL NOT BE MUST NOT BE USED AS AN OFFICIAL TECHNICAL DATA OR OPERATIONAL PROCEDURES,PLEASE REFER TO THERELEVANT AIRBUS DOCUMENTATIONI ssue September 1998 STL deck power flight flight instrument management and centralized fault display system1 STL paxMax. 11in145180390220 STL weights (kg)Operation JetA320-111A320-211A320-212A320-214A320- 231A320-232A320-233A321-111A321-112A321- 131A321-211A321-231 CFMCFMCFMCFMCFMIAEIAEIAECFMIAECFMCFMCFMC FMIAEIAEIAECFMCFMIAECFMIAECFM56-5B5 CFM56-5B6 CFM565A4 CFM56-5A5 CFM56-5B7V2522-A5V2524-A5V2527-M-A5 CFM56-5-B6/5B7V2524-A5/V2527-M-A5 CFM56-5-A1 CFM56-5A1/5A3 CFM56-5A3 CFM56-5B4V2500-A1V2527-A5V2527E-A5 CFM56-5B1 CFM56-5B2V2530-A5 CFM56-5B3V2533-A564 000(options :68 000 or70 000)75 50068 00073 500(options : from68 000 up to77 000)83 000(options :78 000 or85 000)89 00061 00062 50063 00064 50073 500(option :74 500)75 00057 00058 00059 00060 500(option :61 000)69 500(option.)
STL 945.7136/97 A319/A320/A321 general 1.3 A319-100 A320-100 A320-200 A321-100 Span Length Height Fuselage Diameter Track Max. pax Max. FL 34.10m 111ft 10in
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