Transcription of GENERAL AIRPLANE DIMENSIONS - MD-11
1 19 FT 9 IN.( m)35 FT 0 IN.( m)170 FT 6 IN. ( m) **26 FT 10 IN.( m)75 FT 10 IN.( m) GENERAL AIRPLANE DIMENSIONSMODEL MD-11 SCALE05m010 20FT*SP AN AT WING TIP DIMENSION POINT= 165 FT 7 IN. ( ) WITH FUEL**MAXIMUM SP AN WITH FUEL/NOMINAL SP AN WITHOUT FUEL= 169 FT 10 IN. ( )1030 148 FT 8 IN. ( m)136 FT 6 IN. ( m)*59 FT 2 IN ( m)79 FT 6 IN.( m)WINGTIP DIMENSION POINT44 FT 1 IN.( m)80 FT 9 IN. ( m)192 FT 5 IN. ( m)99 FT 4 IN.( m)9 FT 7 IN.( m)27 FT 10 IN.( m)202 FT 2 IN. ( m) WITH CF6-80C2D1F ENGINES200 FT 11 IN. ( m) WITH PW4460 VERTICAL CLEARANCEMIN CLEARANCECRITICAL WT AND CGMAX CLEARANCECRITICAL WT AND CGABCDEFGHIJKLMNOPRSTUVWX28 7 27 1 15 97 415 89 215 78 108 1015 429 557 67 103 29 810 812 423 432 737 315 810 315 228 617 58 916 1110 316 39 99 916 330 958 108 54 510 511 713 425 733 638 217 111 416 * = GE CF6 80C2 D1FH = STANDARD CENTER CARGO DOORV = FREIGHTERI = COMBI CENTER CARGO DOORX = COMBI MAIN DECK DOOR GROUND CLEARANCES model IN.
2 ( cm) IN. ( cm) ABCDFGXI/HJWKLPOMNRSTUWINGLET DETAIL MAXIMUM AND MINIMUM CLEARANCES OF INDIVIDUAL LOCATIONSARE GIVEN FOR COMBINATIONS OF AIRPLANE LOADING/UNLOADING ACTIVITIES THAT PRODUCE THE GREATEST VARIATION AT EACH ROLL ANGLE AND LEVEL GROUND WERE ASSUMED FOR ANALYSIS. IT IS RECOMMENDED THAT APPROXIMATELY 3 INCHES ( m) BE ALLOWEDFOR VERTICAL EXCURSIONS DUE TO VARYING STRUT AND TIRE INFLATIONS,PAVEMENT UNEVENNESS, ETC.*VE
