AIRPORT PLANNING MANUAL Maximum Payload It is the difference between the MZFW and the BOW. Maximum Seating Capacity It is the maximum number of passengers specifically certified or anticipated for certification. Maximum Cargo Volume It is the maximum space available for cargo. Usable Fuel Fuel available for the aircraft propulsion. Table 2.1 - Aircraft General Characteristics EFFECTIVITY: ONACFT 170:00001-00006 00030-00044 00048-00058 00060-00065 OR PRE-MOD SB 170-53-0080 [1] AIRCRAFT MODELS DESIGN WEIGHTS STD LR, SU or SE MRW 36150 kg (79697 lb) 37360 kg (82365 lb) MTOW 35990 kg (79344 lb) 37200 kg (82012 lb) MLW 32800 kg (72311 lb) BOW[2] 20700 kg (45636 lb) MZFW 29600 kg (65257 lb) Maximum Payload [2] 9100 kg (20062 lb) MOW-MinimumOperating Weight 21800 kg (48060 lb) 70 passengers (SE) Maximum Seating Capacity 78 passengers 76 passengers (SU) 78 passengers (LR) [3] 3 3 Maximum Cargo Volume 14.39 m (508.18 ft ) Usable 9428 kg (20785 lb) Fuel [4] 11625  (3071 gal.) 1. Applicable for standard models. For further information, refer to AFM and AOM. 2. Standard configuration (weights may vary according to optional equipment installed or interior layouts). 3. Standard configuration (volume may vary according to optional equipment installed). 4. Adopted fuel density of 0.811 kg/ (6.77 lb/gal.). Table 2.2 - Aircraft General Characteristics EFFECTIVITY: ONACFT 170:00059-00059 00066-99999 OR POST-MOD SB 170-53-0080 [1] AIRCRAFT MODELS DESIGN WEIGHTS STD LR, SU or SE MRW 36150 kg (79697 lb) 37360 kg (82365 lb) MTOW 35990 kg (79344 lb) 37200 kg (82012 lb) 1. Applicable for standard models. For further information, refer to AFM and AOM. EFFECTIVITY: ALL Section 2 Page 2-2 Oct 06/11 w-apm1346