AIRPORT PLANNING MANUAL 2.4.2. Cargo Compartments Twocargo compartments located underfloor are available, one forward of the wing, and the other aft of the wing. The cargo compartments comply with the FAR-25/JAR-25/RBHA-25 “class C” compartment classifica- tion. The table below contains the capacity of the cargo compartment: Table 2.5 - Capacity of the Cargo Compartment CARGOCOMPARTMENT LOADING VOLUME [1] 3 3 FWD 1370 kg (3020 lb) 8.59 m (303.35 ft ) 3 3 AFT 1030 kg (2270 lb) 5.80 m (204.83 ft ) 3 3 Total 2400 kg (5290 lb) 14.39 m (508.18 ft ) 1. Standard configuration (loading and volume may vary according to optional equipment installed). The cargo compartments are provided with the following features: • Optional vertical nets; • Door net at each cargo door. 2.4.3. Cockpit Thecockpitisacoustically and thermally insulated for appearance and durability. It follows the worldwide trend of rounded edges to avoid harm to the flight crew. The cockpit is separated from the passenger cabin by a bulkhead provided with a lockable door. The cockpit door has a locking system, which can only be opened from the cockpit side, a peep hole and an escape mechanism on the cockpit side. EFFECTIVITY: ALL Section 2 Page 2-10 Oct 07/08 w-apm1346