SGS-1-34 Schweizer   


Click on an image to see a full size photograph
General Details
Manufacturer: Schweizer
Plane Name:

SGS-1-34

Classified as: Unclassified
Country Of Origin: U S A
Designer: Ernest Schweizer
No. of Seats 1
No. Built 93
   
Performance:
L/DMax: 34 88 kph / 48 kt / 55 mph
   
MinSink: 0.64 m/s / 2.1 fps / 1.24 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.
15 49.2 14.03 151 250 550 131 290 381 840 27.15 5.56 0 0
Aspect ratio: 16
Airfoil: Wortmann FX 61-163
Structure: all metal
Engine:

Comment:
On handling suitable for the low time pilot. It featured full terminal-velocity speed-limiting dive brakes, in-flight adjustable rudder pedals and a two-way adjustable seat. Originally offered only with a fixed gear, a retractable version was added. The prototype first flew in 1969. At least one example has been substantially modified οΎ– a storm damaged 1-34 was rebuilt by Bob Park with a V-tail and provision for 105 kg./ 230 lb. Water ballast in the wings. ATC.


           

Your Comments:
Another 1-34 on the web, with narratives - 125 - Posted by: JR. (02/Mar/2002) Reply
www.martialartsacademy.org/zr.htm - 126 - Posted by: JR. (02/Mar/2002) Reply
web page for N7595 SGS-1-34 S/N 45 - 91 - Posted by: xcnick (24/Oct/2001) Reply
   RE: web
        web page for N7595 SGS-1-34 S/N 45 - 91_92 - Posted by: xcnick (24/Oct/2001) Reply

Sailplanedirectory.com Copyright 2006 Activate Media. Glider data contains information Copyright www.ssa.org.