- Holder
- K & L Soaring LLC
- Revision
- 10
- Revised
- November 29, 2010
- Status
- Current
- Product
- Aircraft · Glider
- Certification basis
- CAR 5
- Models
- 6
- Registered
- 35 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 6
| Model | Also known as | Note |
|---|---|---|
| SGS 1-23D | Formerly Schweizer Aircraft Corporation | |
| SGS 1-23F | Formerly Schweizer Aircraft Corporation | |
| SGS 1-23G | Formerly Schweizer Aircraft Corporation | |
| SGS 1-23H | Formerly Schweizer Aircraft Corporation | |
| SGS 1-23H-15 | Formerly Schweizer Aircraft Corporation | |
| SGS 1-23 | Formerly BOHICA, Ag Cat, then Schweizer Aircraft Corporation |
Airworthiness directives · 3
ADs whose products are models on this data sheet, matched by model and maker.
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
What the data sheet says
From the PDF’s text layer, line by line: tables lose their columns. The PDF is the record.
Page No. 1 2 3
Rev. No. 10 10 8
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
1G1
Revision 10
K & L Soaring, LLC
SGS 1-23
SGS 1-23D
SGS 1-23F
SGS 1-23G
SGS 1-23H
SGS 1-23H-15
November 29, 2010
GLIDER SPECIFICATION NO. 1G1
Type Certificate Holder K & L Soaring, LLC
5996 State Route 224
Cayuta, New York 14824
Type Certificate Holder Record Schweizer Aircraft Corporation
County Airport
Elmira, New York 14902
I - Model SGS 1-23, 1 PCLM, Approved November 22, 1949; Model SGS 1-23D, 1 PCLM, Approved June 1, 1953;
Models SGS 1-23F and SGS 1-23G, 1 PCLM, Approved June 12, 1958; Models SGS 1-23H and SGS 1- 23H-15, 1 PCLM,
Approved March 13, 1961.
Model SGS 1-23D same as SGS 1-23 Serial No. 12 and up except for increased maximum weight, wing, aileron, rudder and
other minor changes.
Models SGS 1-23F and SGS 1-23G same as SGS 1-23D, Serial No. 25 and up, except for increase in wing span, minor wing
detail construction, and incorporation of an enlarged vertical tail surface.
Model SGS 1-23H same as SGS 1-23G except for redesigned dive brakes and revised detachable wing tips. Model SGS 1-23H-
15 same as SGS 1-23H except for shorter wing tips to reduce wing span to 15 meters (49 ft. 2 in.). Wing tips: Dwg. 23H-467 for
SGS 1-23H and Dwg. 23D-472 for SGS 1-23H-15.
Type Class I
Airspeed limits Serial Nos. 1 through 11:
(See NOTE 2 for eligibility for increased glide and dive and spoiler speeds)
Glide or dive 110 mph True Ind.
Airplane tow 100 mph True Ind.
Auto-winch tow 70 mph True Ind.
Spoiler extended 110 mph True Ind.
Serial Nos. 12 and up:
Glide or dive 116 mph True Ind.
Airplane tow 100 mph True Ind.
Auto-winch tow 70 mph True Ind.
Spoiler extended 116 mph True Ind.
Serial Nos. 25 and up:
Glide or dive 119 mph True Ind.
Airplane tow 110 mph True Ind.
Auto-winch tow 68 mph True Ind.
Spoiler extended 119 mph True Ind.
Serial Nos. 45 and up:
Glide or dive 140 mph True Ind.
Airplane tow 110 mph True Ind.
Auto-winch tow 68 mph True Ind.
Dive brake extended 140 mph True Ind.
(terminal velocity)
C.G. range (+12.9) to (+16). Serial Nos. 25 and up: (+12.8) to (+16).
1G1 2
_____________________________________________________________________________________________________
Maximum weight Serial Nos. 1 through 11: 600 lbs. (See NOTE 2 for eligibility for increased weight).
Serial Nos. 12 and up: 660 lbs.
Serial Nos. 25 and up: 750 lbs.
No. of seats 1 at (-6.5 to -10.5 adjustable)
Baggage None
Control surface SGS 1-23:
movements Elevator 23° Up 23° Down
Rudder 30° Right 30° Left
Aileron 36° Up 18° Down
Spoilers 80° Up 0° Down
SGS 1-23D:
Elevator 25° Up 25° Down
Rudder 30° Right 30° Left
Aileron 36° Up 18° Down
Spoilers 80° Up 0° Down
SGS 1-23F, SGS 1-23G, SGS 1-23H, and SGS 1-23H-15:
Elevator 25° Up 25° Down
Rudder 28° Right 28° Left
Aileron 36° Up 18° Down
Spoilers 80° Up 0° Down
Serial Nos. eligible (SGS 1-23) 1 through 24.
(SGS 1-23D) 25 through 33, 35 and 36.
(SGS 1-23F) 34.
(SGS 1-23G) 37 and up.
(SGS1-23H and SGS 1-23H-15) 45 and up.
Required equipment Items 201(a) or (b ), 401, 402 (SGS 1-23H, SGS 1-23H-15).
Specifications Pertinent to All Models
Datum Wing leading edge at root.
Leveling means Upper surface of stabilizer be tween front and rear spar near fuselage.
Certification basis Glider Type Certificate No. 1G1 (CAR 5)
Production basis None
Equipment:
Landing Gear
201. Wheel
(a) 5.00 x 4, Schweizer Model 1B213, with 4-ply rating tire 7 lbs. (+19)
(b) 5.00 x 4, Schweizer Model 1B216, with 4-ply rating tire No weight change
202. Schweizer circumferential brake Neglect weight
Interior Equipment
401. Airspeed indicator Neglect weight
402. Shoulder harness installation accordi ng to Schweizer Aircraft 1.5 lbs. (+11)
Corporation Dwg. No. 23B-217
3 1G1
Miscellaneous (not listed above)
601. Double spoilers installed accordi ng to Schweizer Aircraft 1 lb. (+13)
Corporation Dwg. No. 23D-605 and 23D-606.
Under wing spoiler movement 0° up 80° down.
NOTE 1. Suitable placards to cover the various pilot weights and positions must be installed in full view of the pilot
as determined from the manufact urer's weight and balance report.
NOTE 2. Serial Nos. 1 through 11 also eligible at 660 lbs. maximum weight Neglect weight change
with the "Airspeed limits" indicated for Serial Nos. 12 and up, when
the elevator is reinforced in accordance with Schweizer Aircraft
Corporation's Drawing No. 23D804, change A.
...END...