The Aermacchi M-345 is a compact twin-seat shoulder-wing
monoplane trainer aircraft. It is based on the earlier S.211 and features structural and equipment improvements, underwing
hard points. Both the pilot and instructor, which are seated in a
tandem configuration, are provided with
Hands-On-Throttle-And-Stick (HOTAS) controls. Both crew are seated upon
Martin-Baker-built
Mk.IT16D 'zero-zero' ejection seats. The cockpit's internal dimensions have been increased to be broadly identical to those of the
BAE Systems Hawk. The displays and all light sources have been selected for compatibility with
night-vision goggles (NVG). The environmental control system cools the cockpit for ground operations in temperatures up to ISA +35 °C (95 °F); the presence of an On-Board Oxygen-Generation System (OBOGS) removes the need for
oxygen bottles. The M-345's glass cockpit features various avionics and last generation Human-Machine Interface. Displays include three identical 5 x 7in (125 x 180mm) colour Multi-Function
liquid-crystal Displays (MFD), a forward-mounted wide-angle
Head-Up Display (HUD), while the rear position is provided with a full-sized HUD repeater via a fourth dedicated multifunction display. The integrated avionics suite includes dual mission computers, embedded
Global Positioning System/
inertial navigation system and
Radar Altimeter (EGIR), two V/UHF radios, integrated central
Audio Warning,
IFF Transponder,
Traffic Alert System (TAS),
Traffic Collision Avoidance System (TCAS) and, optionally, a
digital moving map, stores management system, and an embedded simulation capability (Embedded Tactical Training System - ETTS - identical to that offered on the M-346). The latter is able to simulate a tactical scenario with threats and targets, presence of realistic Computer Generated Forces (CGF), on-board sensors (multimode Fore Control Radar, targeting pod and active/passive electronic countermeasures), weapons. Conventional
ailerons are
hydraulically boosted, with provisions for manual reversion, while both the
elevator and
rudder are mechanically actuated via pushrods, with three-axis electrical trimming. Secondary flight controls are simple
trailing edge flaps, which are electrically actuated, and a belly-mounted
air brake, which is electrically controlled and hydraulically actuated. The 207bar (3,000 lb/in2) hydraulic system is used to operate the
landing gear, wheel brakes, air brake and aileron boost; the electrical system is
DC with internal-
battery engine start. The M-345 is suited for a two level maintenance concept, organizational and intermediate, for aircraft, equipment and system, whilst an on-board
Health and Usage Monitoring System (HUMS) enables data collection and monitoring, contributing to the long life of the airframe and simplifying maintenance activities. ==Operational history==