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Grob 120TP

Grob 120TP

Training Turboprop Aircrafts
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Basic Information
Name
Grob 120TP
Designation
Grob 120TP
Alternate Designation
G 120TP
Equipment Type
Training Turboprop Aircrafts
Manufacturer
Grob Aerospace
Date of Introduction
2012
Description

The Grob 120TP, also referred to as G 120TP, is a side-by-side twin-seat, turboprop-powered military training and aerobatic aircraft capable of typical elementary, basic and advanced pilot training flights. This cost effective platform provides high performance, full Virtual Tactical Training capability including HOTAS, combined with high dispatch reliability. It features lightweight Martin Baker Mk 17 ejection seats and the Rolls-Royce Model 250-B17F turbine engine which is more powerful than the Lycoming engine on the G 120A aircraft. The G 120TP uses a five-blade propeller instead of the three-blade propeller used on the basic G120 aircraft. In September 2011, the Indonesian Air Force became the launch customer for the G 120TP ordering 18 aircraft with deliveries due to start in 2012.

Air & Air Defense Specifications
Crew 2
Max Speed 245.0 km/h
Range 1361.2 km
Service Ceiling 7620 m
Overview (Deagel)
Group Training Turboprop Aircrafts
Status Active
Also Known As G 120TP
Origin Switzerland
Contractor Grob Aerospace
Initial Operational Capability (IOC) August 2012
Total Production 18
Specifications (Deagel)
Crew 2
Number of Engines 1
Propeller Blades 5
G-load — Max Maneuvering Load Factor 6 g
G-load — Min Maneuvering Load Factor -4.00 g
Mass — Empty Weight 1,095 kilogram
Mass — Fuel Load 288 kilogram
Mass — Max Landing Weight 1,550 kilogram
Mass — Max Takeoff Weight 1,590 kilogram
Mass — Max Zero Fuel Weight 1,390 kilogram
Mass — Payload 295 kilogram
Performance — Ceiling 25,000 foot
Performance — Landing Run Distance 497 meter
Performance — Max Range 735 nautical mile
Performance — Take Off Run Distance 374 meter
Power — Max Power at TakeOff 456 shp
Speed — Climb Rate 2,772 fpm
Speed — Cruise Speed 237 KTAS
Speed — Stall Speed 58 KCAS
Speed — Top Speed at High Altitude 245 KCAS
Time — Flight Endurance 6 hour
Volume — Fuel Tank Capacity 360 liter
Gear (Deagel)
Item 1 Turboprop Engines: Model 250-B17F (1)
Variants
Variant 1 Grob 120A
Variant 2 Grob 120TP
Details
Country of Origin Switzerland
Sources

deagel.com: https://www.deagel.com/x/x/a002036

Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
—
Width
—
Height
—
Weight
1550 kg
Operators (1)
Indonesia
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