AIRPORT PLANNING MANUAL Table 2.2 - Aircraft General Characteristics (Continued) EFFECTIVITY: ONACFT 170:00059-00059 00066-99999 [1] AIRCRAFT MODELS DESIGN WEIGHTS STD LR, SU or SE MLW[2] 32800 kg (72311 lb) BOW[3] 20700 kg (45636 lb) MZFW 30140 kg (66447 lb) Maximum 9640 kg (21252 lb) Payload [3] MOW-MinimumOperating Weight 21800 kg (48060 lb) 70 passengers (SE) Maximum Seating Capacity 78 passengers 76 passengers (SU) 78 passengers (LR) [4] 3 3 Maximum Cargo Volume 14.39 m (508.18 ft ) Usable 9428 kg (20785 lb) Fuel [5] 11625  (3071 gal.) 1. Applicable for standard models. For further information, refer to AFM and AOM. 2. For aircraft POST-MOD. S.B. 170-00-0003, consider MLW = 33300 kg (73414 lb). 3. Standard configuration (weights may vary according to optional equipment installed or interior layouts). 4. Standard configuration (volume may vary according to optional equipment installed). 5. Adopted fuel density of 0.811 kg/ (6.77 lb/gal.). 2.2. GENERALAIRCRAFTDIMENSIONS 2.2.1. External Dimensions • Span over winglets - 26.00 m (85 ft 4 in.) • Height (maximum) - 9.85 m (32 ft 3 in.) • Overall length - 29.90 m (98 ft 1 in.) 2.2.2. Wing 2 2 • Reference area - 72.72 m (783 ft ) • Reference aspect ratio - 8.6 2.2.3. Fuselage • Total Length - 29.90 m (98 ft 1 in.) • Length of pressurized section - 22.74 m (74 ft 7 in.) 2.2.4. Horizontal Tail • Span - 10.00 m (32 ft 9 in) 2 2 2 • Area - 23.25 m (250 ft 37 in ) 2.2.5. Vertical Tail 2 2 2 • Reference area - 16.20 m (174 ft 55 in ) EFFECTIVITY: ALL Section 2 Page 2-3 Oct 07/08 w-apm1346