# TCDS GTC 7: Corcoran Stanley R.

- Type: Type certificate data sheet
- Status: Current
- Holder: Corcoran Stanley R.
- Revision: 0
- Revised: April 23, 1942
- Product: Aircraft, Glider
- Certification basis: CAR 5
- Data sheet PDF: https://openairdocs.org/files/sha256/b3/7a/b37ae715b9e42819825254610def79c164f0ce3b865232f0e995d48f1db8a0c8
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8601D47118F1398285256732004DE886.0001
- Page: https://openairdocs.org/tcds/GTC%207

## Models (1)

As the data sheet lists them.

- B Glider

## What the data sheet says

This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.

```text
CORCORAN, STANLEY R.
MODELS: Concoran (Pormerly Frankfort) Glider B (Army XIG-1, IG-1A, TG-1C, 2 PCLM
I-C. NUMBER: GTC 7 (Approved 4/23/42)
Type  Class I (See NOTE 2 (C) airplane tow - 80 mph:
Airspeed limits  Glide or dive - 80 mph;
(T.I.A.S.)  auto-winch tow - 55 mph; spoilers open - 60 mph
C. G.  range  (+1501) to (+2209)  (See NOTE 2(b) and (d)
Datum  Wing leading edge of root
Leveling means  Level top longeron in forward cockpit for weighing

Maximum weight  830 1bs.  (See NOTE 2)
No. seats  2 (1 at (+26.6) and pilot at (-19.4)
Baggage
Control Surface
Left 32 degrees
90 degrees  0 degrees
available
Serial Nos. eligible  B-2-3 and up per NOTE  A and all AAP Nos. (See also
Required equipment  Items 101, 102 and 103
Specifications Pertinent  to All Models:
Certification basis  Type Certificate No. 7 (CAR 5)
Production basis  None (See NOTE A)
EQUIPMENT:
Landing Gear
Wheel  (General C-1569) with 14h 6-ply
11.0 1bs.  (+19)
Interior Equipment
101.  Airspeed indicator  Airspeed pitot  • 105  1bs.
202.  Extra instruments
Front cockpit  1.0 1bs.  -31
Rear cockpit  2.5 1bs.  (+19
Miscell. neous (maristed above)  Mud guard  1.5 1bs.  (+19)
Prior to original certification, each glider manufactured for civil
use must satisfactorily pass:
covering, metal priming or  finish is applied.  All woodwork
may be varnished.
inspection of the completed glider.
Check of flight characteristics.
and balance report including list of equipment included
in the certificated weight empty must be submitted for each aircraft
with original inspector's report and each subsequent report covering
change in equipment.  The following placard,  as determined by the weight
report, must be installed in full view of the pilot:
Solo - Use Front Seat Only - Minimum Weight,
Dual - Front Seat - Minimum Weight,
Occupant and Parachute
- Rear Seat - Maximum Weight,
Occupant and Parachute
Serial Nos. B-2-1 is eligible for certification for a maximum
Serial Nos. B-1-1, B-1-4 to B-1-8, inclusive, and B-1-10 to B-1-12,
inclusive, are eligible for certification with small fin and
stabilizer, large rudder and elevator,  elevator control system
bungee and no spoilers with the folloving restrictions:
Maximum weight
C.G. range
Serial Nos. B-1-2, B-1-3 and B-2-2 are eligible for certification as
Class II gliders in accordance with the  provisions set forth in
with the following placard:
Airplane tow
Auto-wing tow  55 mph True Ind.
Inverted flying prohibited.
The above gliders may be certificated as Class I gliders when revised
(revisions necessary  to D-nose section and to accommodate balanced
alleron), balanced type aileron, and balance weights in the
elevators, are installed.
Serial Nos. B-2-23 and up are eligible for certification vith the
following restrictions:
Maximum weight
(+16-2) to (+21-6)
```

## ADs

None name its models.

## STCs approved under this data sheet (1)

- [STC SA4503NM](https://openairdocs.org/stc/SA4503NM): Remove original cloth covering and install Ceconite covering. Ceconite Division of Poly-Fiber Inc.

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