- Holder
- Piper Aircraft Inc.
- Revision
- 0
- Revised
- August 19, 1942
- Status
- Current
- Product
- Aircraft · Glider
- 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 |
|---|---|---|
| TG-8 (Army TG-8; Navy XLNP-1) |
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 · 1
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODELS: Piper Glider TG-8 (Army TG-8, Navy XINP-1), 3 PCIM
I.C. NUMBER: GTC 10 (Approved 8/19/42)
Type Class II
Airspeed limits Glide or dive - 122 mph True Ind.
Airplane tow - 122 mph True Ind.
Spoilers open - 122 mph True Ind.
Auto-winch tow - Not authorized
C.G. range (+13.5) to (+22.5)
Datum Leading edge of wing
Leveling means Lugs at sliding window on left longeron
Maximum weight 1160 1p8 (+9), 1 at (+36), and pilot at (-26))
Number seats 3(1 at
(See NOTE
Maximum baggage 20 1b8. (+49)
Control surface Elevator Up 34 degrees Down 29 degrees
movement Aileron Up 18 degrees Down 18 degrees
Rudder Right 30 degrees Left 30 degrees
Stabilizer Up 2.5 degrees Down 4 degrees
Spoilers Up 50 degrees Down 0 degrees
Serial numbers eligible G-1 and up (See NOTE A)
Required equipment Items 101, 102 and 103
SPECIFICATIONS PERTINENT TO ALL MODELS:
Certification basis Glider Type Certificate No. 10 (CAR 5)
Production basis None (See NOTE A)
EQUIPMENT:
Ianding Gear
102. 8.00-4 (Hayes 841) wheels with tires
and expander tube brakes 32 1bs. (+3)
103. 6x2.00 steerable tail wheel (Scott
Aviation Corp. Model CST-12) with
solid tire 7 1bs. (+193)
Electrical Equipment
301- Battery - Reading 324LD (with box) 16 lbs. (+20)
302. Position lights 3 1bs. (+79)
Interior Equipment
Airspeed indicator 1 1b. (-44)
Extra instruments
Front instrument panel 1.5 1bs. (-44)
Middle instrument panel 2.5 1bs. 1+91
304. Parachutes
Front seat 20 1bs. (-26)
Middle seat 20 1bs. (+9)
Rear seat 20 1bs. (+36)
Each glider manufactured for civil use subsequent to 3/20/45 must,
prior to original certification, satisfactorily pass:
(a) An inspection for workmanship, materials and conformity refore any
covering or final finish is applied. All woodwork may be varnished.
(b) A final inspection of the completed glider.
(C) A check of flight characteristics.
NOTE 1. The following placards must be installed in full view of the pilot:
(1) isolo flight from front seat only.
Minimum weight pilot and chute 145 1bs."
(2) "2nd person must use middle seat."
(3) "Auto-winch tow prohibited."
(4) "Instrument flight prohibited."
NOTE 2. Army TG-8 gliders having serial numbers G-1 and up are eligible for
certification as J3 series airplanes under the provisions of the pertinent
and conformity with the approved Piper data. provided they are converted to J3 series airplanes Conversion procedure
is given in Safety Regulation Release No. 186.