- Holder
- Societe C.A.R.M.A.M.
- Revision
- 1
- Revised
- March 1, 2012
- Status
- Current
- Product
- Aircraft · Glider
- Certification basis
- Part 21
- Models
- 1
- Registered
- 2 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 1
| Model | Also known as | Note |
|---|---|---|
| M-200 |
Airworthiness directives · 2
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
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(1) This TC was considered not valid by the state of design on January 6, 2009, and has been replaced by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...