# TCDS G10EU: Szybowcowy Zaklad Doswiadczalny

- Type: Type certificate data sheet
- Status: Current
- Holder: Szybowcowy Zaklad Doswiadczalny
- Revision: 0
- Revised: September 30, 1966
- Product: Aircraft, Glider
- Certification basis: Part 21
- Registered aircraft: 1, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/53/8e/538e68ec7a7dad788488be84010364c8edec45c1e580651b96e18b0c399bfa82
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EA0FE635EB1E515F852567200059514E.0001
- Page: https://openairdocs.org/tcds/G10EU

## Models (1)

As the data sheet lists them.

- SZD-24-4A Foka-4

## What the data sheet says

From the PDF's text layer, line by line; tables lose their columns. The PDF is the record.

```text
Page No. 1 2
Rev. No. - -
FEDERAL AVIATION AGENCY
G10EU
SZYBOWCOWY ZAKLAD
DOSWIADCZALNY
SZD-24-4A "Foka-4"
September 30, 1966
TYPE CERTIFICATE DATA SHEET NO.  G10EU
This data sheet which is a part of type certificate No.  G10EU prescribes conditions and limitations under which the product for
which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations.
Type Certificate Holder Szybowcowy Zaklad Doswiadczalny
325, Cieszynska
Bielsko-Biala, Poland.
I - Model SZD-24-4A, approved July 19, 1966
Airspeed limits (IAS) Glide or dive 140 knots (161 mph)
Airplane tow 91 knots (105 mph)
Auto-winch tow 65 knots (74 mph)
Spoilers extended 140 knots (161 mph)
C.G. range 9.5" to 13.5"
Datum Nose of wing root section
Leveling means Reference points on the front and rear fuselage
Maximum weight 849 lbs.
No. of seats 1
Control surface
Movements Elevator Up 23° Down 18°
Rudder Right 35° Left 35°
Aileron Up 34° Down 16°
Elevator trim tab Up 15° Down 45°
Serial Nos. eligible The Polish People's Republic Certificate of Airworthiness endorsed as noted below under
"Import Requirement" must be submitted for each individual glider for which application
for certification is made.
Certification basis FAR 21.29 and Section G of the Polish Civil Airworthiness Requirements dated
September 1, 1964.  (These requirements are equivalent to FAR 21.23)
Type Certificate G10EU issued July 19, 1966.
Date of Application for Type Certificate April 5, 1966.
Import requirement A U.S. Airworthiness Certificate may be issued on the basis of a Certificate of
Airworthiness signed by a representative of the Ministry of Transport Department of
Civil Aviation, containing the following statement:
"The glider covered by this certificate has been examined and found to comply fully with
Section G of the Polish Civil Airworthiness glider requirements dated September 1,
1964, and conforms to Type Certificate No. G10EU."

G10EU 2
Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations
(see Certification basis) must be installed in the glider for certification.
NOTE 1. Current weight and balance report including list of equipment included in certificated empty weight, and
loading instructions when necessary, must be in each glider at the time of original certification and at all
times thereafter.
...END...
```

## ADs (1, in force first)

- [AD 75-16-17](https://openairdocs.org/ad/75-16-17): Wing, Fuselage and Tailplane · Szybowcowy Zaklad Doswiadczalny SZD-24-4A Foka-4. Effective Jul 29, 1975

## Registered aircraft by registry model (OpenAirDocs)

- [Szybowcowy Zaklad Doswiadczaln SZD-24-4A "FOKA"-4](https://openairdocs.org/model/szybowcowy-zaklad-doswiadczaln-szd-24-4a-foka-4): 1 aircraft (registry code 8821004)

## STCs approved under this data sheet (2)

- [STC SG03715NY](https://openairdocs.org/stc/SG03715NY): Iunstallation and maintenance of Oratex 6000 Covering and Coating System. Lanitz-Prena Folien Factory GmbH
- [STC SG04702NY](https://openairdocs.org/stc/SG04702NY): Installation and maintenance of Oratex UL600 Covering and Coating System. Lanitz-Prena Folien Factory GmbH

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