# TCDS G3IN: Elliotts of Newbury Ltd.

- Type: Type certificate data sheet
- Status: Current
- Holder: Elliotts of Newbury Ltd.
- Revision: 0
- Revised: April 1, 1963
- Product: Aircraft, Glider
- Certification basis: CAR 10
- Data sheet PDF: https://openairdocs.org/files/sha256/da/ac/daac75621cf4df04f4f35fd28e133c65663ef29a9313bb4d0a94564ee1c45b6e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/817DCC05927D771185256720004DAB15.0001
- Page: https://openairdocs.org/tcds/G3IN

## Models (1)

As the data sheet lists them.

- EON 460 Series 1

## 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. - - 
 
DEPARTMENT OF TRANSPORTATION 
FEDERAL AVIATION ADMINISTRATION 
 
G3IN 
ELLIOTTS 
EON 460 
Series 1 
April 1, 1963 
 
TYPE CERTIFICATE DATA SHEET NO. G3IN 
 
This data sheet which is a part of type  certificate No.  G3IN prescribes conditi ons and limitations under which the product for  
which the type certificate was issued meets the airworthiness requirements of the Civil Air Regulations. 
 
Type Certificate Holder Elliotts of Newbury Ltd. 
   Newbury, Berkshire, 
   England 
 
I - Model EON 460 Series 1, approved February 25, 1963 
 
 Airspeed limits Glide or dive  118 knots (136 m.p.h.) 
 (indicated airspeed) Airpla ne tow  82 knots (94 m.p.h.) 
   Auto-winch tow  65 knots (75 m.p.h.) 
   Maximum speed in rough air  74 knots (85 m.p.h.) 
   Airbrakes extended  118 knots (136 m.p.h.) 
 
 C.G. range  (-1.5) to (+2.8) 
 
 Datum  Centre line of wing main spar 
 
 Leveling means Straight e dge across mainplane joint 
   pins at main and rear spar joints 
 
 Maximum weight 630 lb. 
 
 No. of seats  1 (-22.5) 
 
 Baggage  None 
 
 Control surface movements Elevator Up 22° Down 22° 
   Elevator trim tab Up 10° Down 30° 
   Rudder Right 25° Left 25° 
   Aileron Up 28° Down 12 1/2° 
   Airbrakes 5.75" above  and below wing surfaces 
 
 Serial Nos. eligible The United Kingdom Certificate of Airworthiness for export endorsed as noted below 
   under "Certification basis" must be s ubmitted for each individual glider for which 
   application for certification is made.

G31N 2 
 
 Certification basis CAR 10.  Type Certif icate No.  G3IN, issued February 25, 1963 
   Application for Type Cer tificate dated November 14, 1961. 
 
   Each glider and any replacement parts manufactured in the United Kingdom must be 
   clearly labeled as imported. 
 
   A U.S. Airworthiness Certificate may be issued on the basis of a United Kingdom 
   Certificate of Airworthiness signed by a representative of the Ministry of Aviation, 
   containing the following statement:  "The  glider covered by this certificate has been 
   examined and found to comply with British Civil Airworthiness Requirements for 
   gliders current on 1st January 1960 and confor ms to T.C. G3IN."  This certification is 
   equivalent to CAR 5 effective February 15, 1956. 
 
 Equipment:  The basic required equipment as prescr ibed in the applicable airworthiness regulations 
   (see Certification basis) must be in stalled in the glider for certification. 
 
 
NOTE 1: Current weight and balance re port including list of equipment included in certificated empty weight, must 
  be in each glider at the time of original certification. 
 
NOTE 2: The following placards must be in stalled in full view of the pilot: 
 
  (a) "Flight in cloud perm issible only when altimeter and turn and bank indicators of an approved type are 
   installed." 
 
  (b) "Maneuvers permitted - Tight turn s, stall turns, inside loops, spins." 
 
  (c) "Night flyi ng is prohibited." 
 
  (d) "When flying in rough air the speed is not to exceed 74 knots IAS." 
 
 
 
...END...
```

## ADs

None name its models.

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