- Holder
- Wood Steven K. and Russell G. Williams
- Revision
- 1
- Revised
- March 6, 1984
- Status
- Current
- Product
- Aircraft · Small Airplane
- 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 |
|---|---|---|
| Eaglet 230 | Formerly American |
Airworthiness directives · 0
ADs whose products are models on this data sheet, matched by model and maker.
No ADs matched this data sheet’s models
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
STCs approved under this data sheet · 2
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
Rev No. 1
Reformatted 3/94.
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
ATC-380
Revision 1
AMERICAN
Eaglet 230
March 6, 1984
TYPE CERTIFICATE DATA SHEET NO. ATC-380
This data sheet which is a part of type certificate No. ATC-380 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: Steven K. Wood and Russell G. Williams
Grand Junction, Colorado
I - Model Eaglet 230
Engine Szekely SR-3L (See NOTE 1)
Engine limits 30 hp
Propeller Wood
Propeller limits Not available (fixed pitch)
Airspeed limits Not available
C.G. range Not available
Maximum weight 867 lbs. (See NOTE 1)
Number of seats 2
Maximum baggage None
Fuel capacity 8 1/2 gallons
Oil capacity 5 quarts
Serial Nos. eligible 1007, 1013, 1034 and up manufactured prior to 11-30-36 eligible. Approval expired as
of that date due to sale to Victor H. Roos, Kansas City, MO.
Certification basis Bulletin 7-A, in effect January 1, 1931.
NOTE 1. Eligible with Szekely SR-3L converted to SR-3-35 35 hp engine, provided the
conversion is made by either aircraft or engine manufacturer or competent factory
representative. Maximum weight after this conversion is 900 lbs.
NOTE 2. Airworthiness certificate must include the following unless it has been satisfactorily
demonstrated to an inspector of Civil Aeronautics that such notation is unnecessary:
"INTENTIONAL ACROBATICS PROHIBITED."
'
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