Grob G 103a Twin II
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Original source: Transferred from en.wikipedia; transfer was stated to be made by User:Undead_warrior. Author Original uploader was Dhaluza at en.wikipedia Permission (Reusing this file) CC-BY-3.0; Released under the GNU Free Documentation License.
Author: Original uploader was Dhaluza at en.wikipedia Permission (Reusing this file) CC-BY-3.0; Released under the GNU Free Documentation License.

The G103 Twin II (originally designated the G 118) is a high performance two-seater sailplane made by Grob Aircraft. The aircraft is of T-tail configuration and is fitted with a non retractable undercarriage and upper surface airbrakes. Of glass fibre construction it is designed for training high performance and simple aerobatic flying.

Made by Grob Aircraft.

Empty Weight Lb
869
Wing Area Sqm
17.8
Lists
*List of gliders
Aspect Ratio
17
Glide Ratio
ca. 36.5
Span In
5
Gross Weight Lb
1280
Sink Rate Ms
ca. 0.64
Number Built
549
Crew
Two
Empty Weight Kg
395
Gross Weight Kg
580
Height In
1
Sink Rate Ftmin
126
Manufacturer
Max Speed Mph
160
Max Speed Kmh
250
Height Ft
5
Span Ft
57
National Origin
Germany
Wing Area Sqft
191
Met Or Eng
met
Span M
18
Length Ft
26
Height M
2
Length In
10
Length M
8
Category

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