- Holder
- Pratt Read & Co. Inc.
- Revision
- 0
- Revised
- December 23, 1942
- Status
- Current
- Product
- Aircraft · Glider
- Certification basis
- CAR 5
- Models
- 1
- Registered
- 4 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 |
|---|---|---|
| PR-G1 (Army TG-32; Navy LNE-1) | Formerly Gould Aeronautical Division |
Airworthiness directives · 1
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.
STCs approved under this data sheet · 6
STC SA4503NMRemove original cloth covering and install Ceconite coveringSTC SA01734SEApplication of Stewart Systems synthetic fabric covering system to aircraft fuselage, wings, tail surfaces, control surfaces and related parts.STC SA4005NMPrecise Flight Inc. Pulselite Control SystemSTC SG10WEReplace existing fabric on wings, fuselage, empennage, and/or control surfaces with Ceconite103 material.STC SA4-840Fabric replaced with glass cloth on wings, fuselage, empennage and/or control surfaces.STC SG4-1411Ceconite 103 covering of glider.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
PRATI READ & COMPANY, INC.
MODELS: Pratt Read Glider PR-G1 (Army TG-32; Navy INE-1). 2 PCIM
I.C. NUMBER: GIC 12 (Approved 12/23/42)
Type
Airspeed limits Glide or dive - 99 mph True Ind.
Airplane tow - 90 mph True Ind.
Spoilers extended - 99 mph True Ind.
C.G. range (+1.3) to (+5.9)
Datum Centerline of main wing spar fitting at fuselage
Leveling means Front face of main wing fittings in cabin are
Maximum weight
No. seats 2 (-22) (See NOTE 1)
Eaggage
control surface Up 30 degrees Down 20 degrees
movement Elevator trim tab Up 40 degrees Down 35 degrees
Rudder 25 degrees Left 25 degree
Up 24 degrees Down 12 degree!
Spoilers Double flat plate type extending
5.5 inches above wing and 5.5
inches below wing.
serial numbers eligible 2 and up per NOTE A and all AAF and Navy numbers
Required equipment Items 200
SPECIFICATIONS PERTINENT TO ALL MODELS:
Certification basis Glider Type Certificate No. 12 (CAR 5)
Froduction basis None (See NOTE A)
EQUIPMENT:
200. 6.00-6 wheel (Goodyear L6MBM) with
7.00-6 4-ply H.D. tire and Frake
(wheel must be placarded for this
H.D. tire) 18 1bs. (*184)
201. Tail skid (Drawing No. 01-33909) 1 1b.
NOTE A. Each glider manufactured after 9/16/43, for civil use must, prior to
original certification,
An inspection for workmanship, materials and conformity before any
covering or final finish is applied. All woodwork may be varnished.
inspection of the completed glider.
A check of flight characteristics.
NOTE 1. The following placards must be installed in full view of the pilot:
Authorized Loadings
(a) Maximum weight of occupants and parachutes - 380 1bs.
(D) Minimum weight of occupants and parachutes - 190 1bs.
Ballast, if firmly secured, may be carried in the
seat when necessary.