# TCDS G1WE: Prue Irving O.

- Type: Type certificate data sheet
- Status: Current
- Holder: Prue Irving O.
- Revision: 0
- Revised: January 15, 1965
- Product: Aircraft, Glider
- Certification basis: Part 5, CAR 5
- Data sheet PDF: https://openairdocs.org/files/sha256/12/12/121234d4f812986d633f925d379568033d7786c52cd5e134998b617d08b61ee1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8A4BB7DE83B2AE2C85256720004F7DCD.0001
- Page: https://openairdocs.org/tcds/G1WE

## Models (1)

As the data sheet lists them.

- Prue Super Standard

## 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
G1WE
Prue
Prue Super Standard
January 15, 1965
TYPE CERTIFICATE DATA SHEET NO.  G1WE
Type Certificate Holder Irving O. Prue
12654 E. Avenue V-12
Pearblossom, California
I - Model Prue Super Standard (High Performance), Approved December 28, 1964
Type High Performance Sailplane
Airspeed limits Vne-Glide or Dive with or
  without dive brakes 120 MPH
Vta-Aircraft Tow 90 MPH
Vmax to Close Dive Brakes 100 MPH
Vtaw Auto-Winch Tow 77 MPH
Vp-Maneuvering 96 MPH
C.G. range F.S> 76.5 to F.S. 80.5
Maximum weight 725 lbs.
No. of seats One
Baggage None
Control surface movements Ailerons Up 24° Down 11°
Rudder Left 25° Right 25°
Elevator Up 25° Down 15°
Air Brake Out 90° Closed Flush
Serial Nos. eligible 1 through 499
Datum F.S.O (nose of Sailplane.  See Dwg. 1-1000 dated December 22, 1964)
M.A.C. 30.75 Ins.  (L.E. of M.A.C.  F.S.  69.7)
Leveling means Level attitude F.S. 68.5 plumb
Certification basis CAR 5 effective February 15, 1956, Amendment 5-1 effective May 3, 1962, and Basic
Glider Criteria Handbook, 1962.
Type Certificate No.  G1WE issued December 28, 1964.
Production basis None.  Prior to original certification an FAA representative must perform a detailed
inspection for workmanship, materials, and conformity with the approved technical data,
and a check of the flight characteristics.
Equipment: The basic equipment as prescribed in the applicable airworthiness regulations (See
Certification Basis) must be installed in the aircraft for certification.
NOTE 1. Ballast Wt. of 26 lbs. Max. may be installed at F.S. 24 for C.G. Control.

G1WE 2
NOTE 2. The following placards must be installed in full view of the pilot.
(a) Flight in air with visible moisture prohibited.
(b) Airspeed Limitations MPH
Vne-Dive 120
Dive Brakes Closing 100
Vta-Aero Tow 90
Vtaw-Auto-Winch Tow 77
Vp-Maneuvering 96
(c) Center of Gravity Limits - inches
Aft of Nose (Datum) 76.5 to 80.5
Level Attitude  Sta. 68.5 Plumb
(d) Weight Limits Pounds
Ballast at Sta. 24 26
Maximum Gross Wt. 725
NOTE 3. Glider is approved for day-VFR operation only.
NOTE 4. Day-VFR restriction and placard "Flight in air with visible moisture prohibited" may be removed provided
that the minimum equipment installation, and/or modifications required by the CAR's for IFR or
precipitation flight are accomplished and FAA approved.
...END...
```

## ADs

None name its models.

## Registered aircraft by registry model (OpenAirDocs)

- [Prue Irving O PRUE SUPER STANDARD](https://openairdocs.org/model/prue-irving-o-prue-super-standard): 0 aircraft (registry code 7340102)

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