Plane Details

SGS-1-34 Schweizer

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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 ﾖ 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