GrobTurboprops · Bavaria, Germany, Tussenhausen-Mattsies
2023 New Grob Aircraft G 120TP Turboprop
- Price
- On request
- Year
- 2023
- Total time
- 1 hours
- Location
- Germany
Specifications
General
- Registration
- TBA
- Total time
- 1
- Seats
- 2
- Condition
- New
- Type
- Turboprop Aircraft
- Sale
- aircraft for sale
Description
- Power availability appropriate to the phase of training
- Power can be physically limited to 312 SHP for ab initio training phase (Flex Power).
- All composite airframe
- lightweight, corrosion and fatigue free, easy repair.
- Operation
- VFR day/night, IFR, non-icing conditions
Description
Main Features At A Glance
Thoroughbred basic trainer aircraft optimized for the demanding military training environment.
Full aerobatic & military training capability (+6 / -4 g).
Excellent handling qualities and simple single lever ‘turbine-like’ power plant operation.
Proven dependability and supportability of the Rolls-Royce M250-B17F turbine engine.
456 SHP for take-off and 380 SHP for maximum cruise provides excellent power-to-weight ratios and with instantaneous excess power during normal operations.
5-blade, constant speed MT-Propeller.
Only aircraft in its class certified to latest FAR 23 crashworthiness requirements.
Most spacious side-by-side seating in its class.
Student pilot can be seated either in the LH or RH pilot seat, both with individual throttle levers.
Robust retractable landing gear optimized for rough training environment.
Furnished with latest state-of-the-art avionics (analogue/digital) allowing seamless transition to modern training platforms.
Primary flight display (PFD) in digital flight deck variant features tapes display or round dial display being unique for this class of trainer aircraft.
VFR day / night and IFR operations in non-icing conditions.
Available safety features include traffic advisory system (TAS), digital flight data and cockpit voice recorder
(FDR & CVR) and mission debriefing system (MDS).
Unbeatable low total life-cycle cost to its fibre reinforced composite airframe, requiring less maintenance effort.
High service life of the airframe of minimum 15,000 flight hours (aerobatic).
Technical Specification
Engine
Make/Model – Rolls-Royce M250-B17F turbine engine
Max. continuous power (MCP) – 380 SHP
Max. power (MP, 5 min limit) – 456 SHP
Flat rated versions on request
Performance
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) – 2,855 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
- Weights
- Max. take-off weight (MTOW, utility) – 1,515 kg (3,340 lb)
- Max. take-off weight (MTOW, aerobatic) – 1,440 kg (3,175 lb)
- Max. landing weight (MLW) – 1,515 kg (3,340 lb)
- Max. usable fuel capacity – 275 kg (606 lbs)
- Max. baggage weight – 50 kg (110 lb)
- Miscellaneous
- Max. load factors aerobatic – +6/-4G
- Max. operating altitude 25.000 ft
- Avionics
- The unique and state of the art open architecture mission simulation system of the G 120TP allows the training of student pilots from initial all the way through basic flight training.