2018 GROB G120TP


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    Aircraft Summary


    General

    Year
    2018
    Manufacturer
    GROB
    Model
    G120TP
    Condition
    New
    Description
    GROB AIRCRAFT TRAINING CONCEPT Focusing on required training tasks on a single multi-purpose platform minimizes type conversions, yielding to quality improved pilot training at reduced overall training cost. Grob Aircraft’s new G 120TP Training Concept, based upon the versatile G 120TP basic training aircraft, addresses the latest trends and strategic shifts in modern military flight training; reduced demand for fast jet pilots, increased demand for transport/helicopter/UAS pilots, an increase on mission complexity - and in the same time pressures from reduced military budgets. The G 120TP training system starts with the Primary and Basic Flight Training phase incorporating ab initio flight training and screening on a ‘simplified’ G 120TP with Flex Power facilitating engine handling and limiting power envelope for beginner pilots. The side-by-side cockpit arrangement supports high efficiency training, specifically in early training stages. The Primary and Basic Flight Training phase is graduated by the students with the Wings Test. In the Streaming phase, the G 120TP platform can be operated further for all subsequent pilot class streams by downloading of flight training tasks from more expensive training platforms. By using a common platform, delayed ‘cross streaming’ is facilitated between the fighter and transport streams. Elimination of unnecessary transitions and earlier channelling of the pilots results in a streamlined pilot training, focussing on relevant core skill development. Furthermore, future demand shifts between the various streams can be easily bolstered by a common platform.

    Airframe

    Airframe Notes
    Operating speed range Max. operating speed VMO MSL up to 13,000 ft 235 KCAS Max. mach number MMO above 13,000 ft 0.45 Stall speed VS (MSL landing config., utility) 57 KCAS Take off and landing distances (MSL, ISA) Take off distance over 50 ft (MTOW, no wind, no slope, utility) 376 m Take off roll (MTOW, no wind, no slope) 222 m Landing distance over 50 ft (MLW, no wind, no slope) 455 m Landing roll (MLW, no wind, no slope) 176 m Cruise speeds, rate of climbs, sustaining g (ISA, MTOW) Max. cruise speed (MSL, MCP, utility) 205 KTAS Max. cruise speed (10,000 ft, ISA, MCP, utility) 226 KTAS Rate of climb (MSL, MP, aerobatic) 2855 ft/min Sustained g (MSL, MCP, 1400 kg aircraft weight) 3.0 g Range / Endurance (ISA, 30 min reserve fuel, utility) Range (5,000 ft, LRC speed) 640 NM Range (10,000 ft, LRC speed) 725 NM Endurance (10,000 ft, max endurance power) 5.4 hrs

    Engine

    Engine Notes
    Max. continuos power (MCP) 380 SHP Max. power (MP, 5 min limit) 456 SHP Flat rated versions on request


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