# TCDS G14EU: Societe C.A.R.M.A.M.

- Type: Type certificate data sheet
- Status: Current
- Holder: Societe C.A.R.M.A.M.
- Revision: 1
- Revised: March 1, 2012
- Product: Aircraft, Glider
- Certification basis: Part 21
- Registered aircraft: 2, by the registry models matched to it (OpenAirDocs)
- Data sheet PDF: https://openairdocs.org/files/sha256/b9/b6/b9b6c8848748e9da5a627b9da9fb3408871165d6c1214a646301299a856de07d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5983742F8618E9D5862579B300723B46.0001
- Page: https://openairdocs.org/tcds/G14EU

## Models (1)

As the data sheet lists them.

- M-200

## 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. 1 1 
 
DEPARTMENT OF TRANSPORATION 
FEDERAL AVIATION ADMINISTRATION 
 
G14EU 
Revision 1 
C.A.R.M.A.M 
M-200 
March 1, 2012 
 
TYPE CERTIFICATE DATA SHEET NO.  G14EU 
 
This data sheet which is a part of type certificate No.  G14EU 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 Societe C.A.R.M.A.M. 
  Aerodrome de Moulins-Avermes 
  MOULINS, Allier 
  France 
 
Type Certificate Ownership Record 
 
  (1)   This TC was considered not valid by the state of design on January 6, 2009, and has been replaced by 
European Aviation Safety Agency (EASA) Specific Airworthiness Specification (SAS) number 
EASA.SAS.A.007,  issued January 6, 2009.  Only standard airworthiness certificates issued prior to 
March 1, 2012 are valid. 
 
(2)   Future unsafe conditions existing in the aircraft may result in the revocation of the airworthiness 
certificates of the aircraft if there is no entity to comply with 14 CFR § 21.99(a), “Required design 
changes.” 
(3)   Replacement parts may not be available in the future. 
 
Model "M-200" Approved June 19, 1967 
 
 Airspeed limits (IAS) Glide or dive 121 kts. 
  Airbrakes extended 121 kts. 
  Airplane tow 81 kts. 
  Auto-winch tow 65 kts. 
 
 C.G. range From (+7.6") to (+14.2") 
 
 Datum Wing leading edge 
 
 Leveling means Pins on left side of fuselage at Stations 5 and 9 
 
 Maximum weight 1255 lbs. 
 
 No. of seats 2 (1 at -26.4) (1 at -6.7) 
 
 Control surface 
 Movements Elevator Up 32° Down 18° 
  Elevator tab Up 25° Down 25° 
  Rudder Right 38° Left 38° 
  Ailerons Up 25° Down 25° 
 
 Serial Nos. eligible Only those ai rcraft serials holding a standard airworthiness certificate issued prior to 
March 1, 2012 are eligible. 
 
 Certification Basis FAR 21.29 and AIR 2054 French Glider Requirements dated April 15, 1965 (these  
  requirements are equi valent to FAR 21.23)

G14EU 2 
  Type Certificate No. G14EU issued June 19, 1967 
  Date of Application for Type Certificate:  September 20, 1966. 
 
 Import requirements None elig ible after March 1, 2012.  
 
  Previous to this date: 
 
  A U.S. Airworthiness Certificate may be issued on the basis of a Certificate of  
  Airworthiness for Export signed by a repr esentative of the Secretariat General a  
  l'Aviation Civile containing the following statement:   
  "The glider covered by this certificate ha s been examined and found to comply with  
  French Government glider airworthine ss requirements AIR 2054 dated April 15, 1965,  
  and conforms to Type Certificate No. G14EU. 
 
 Equipment The basic required equipm ent 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 g lider at the time of original certification and all times  
 thereafter. 
 
NOTE 2. The following placard must be in stalled in full view of the pilot: 
 
 "Night Flying is Prohibited" 
 
 
 
...END...
```

## ADs (2, in force first)

- [AD 75-23-02](https://openairdocs.org/ad/75-23-02): Aileron Spars · Aer-Pegaso M-100 S and M-200. Effective Nov 14, 1975
- [AD 69-24-01](https://openairdocs.org/ad/69-24-01): Horizontal Stabilizer · Aer-Pegaso M-100 S and M-200. Effective Nov 23, 1969

## Registered aircraft by registry model (OpenAirDocs)

- [Carmam S A M-200](https://openairdocs.org/model/carmam-s-a-m-200): 2 aircraft (registry code 1981008)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.