SGM 2-37 Schweizer   


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General Details
Manufacturer: Schweizer
Plane Name:

SGM 2-37

Classified as: Unclassified
Country Of Origin: U S A
Designer: Leslie Schweizer
No. of Seats 2
No. Built 12
   
Performance:
L/DMax: 28
   
MinSink: 0.96 m/s / 3.16 fps / 1.87 kt
   


 

Specifications:
Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
/sq.m
lb.
/sq.ft
kg lb.
18.14 59.5 18.18 195.7 544 1200 213 470 757 1670 41.64 8.99 0 0
Aspect ratio: 17.9
Airfoil: Wortmann Fx 61-163
Structure: all metal
Engine: 83 kW/ 112 bhp Lycoming 0-235-L2C

Comment:
The SGM 2-37 self-launching motorglider, which first flew in 1982, has the capacity to operate as a towplane for other gliders. 9 (known as the TG-7A) are operated as trainers at the U.S. Air Force Academy. The aircraft is without flaps but has balanced upper/lower surface dive brakes. ATC


           

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