- Holder
- Ardelt Eugene M.
- Revision
- 0
- Revised
- July 29, 1943
- Status
- Current
- Product
- Aircraft · Glider
- Models
- 1
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 |
|---|---|---|
| EA-5 | Formerly University of Denver |
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
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
ARDELT, EUGENE M.
MODELS: Ardelt EA-5 Glider, 1 POIM
T.C. NUMBER: 14 (Approved 7/29/43)
Type Class III
Airspeed limits Glide or dive - 50 mph True Ind.
Auto-winch tow - 45 mph True Ind.
C.G. range (+26-3) to (+30.2)
Datum Leading edge of wing at root
leveling means
Maximum empty weight 375 1bs. (+38-29) +0 (+39.75)
Maximum weight 545 1bs.
NO - seats
Faggage
Control surface Elevator - Up 38 degrees - Down 38 degrees
HO CEILS - Up 15 degrees - Down 16 degrees
(See NOTE B) Rudder - Right 24 degrees - Left 24 degrees
Tab (elevator) Up 18 degrees - Down 18 degrees
(Measured in relation to the neutral and
deflected positions of the respective chord
Serial Nos. eligible 3 and up (See NOIE A and B)
Reguired equipment
Certification basis Glider Type Certificate No. 14 (CAR 5)
Production basis NOTE A and B)
Equipment:
A pius (+) or minus sign preceding the weight of an optional
indicates the net weight change between that item and the equivalent
required item.
Interior Equipment
401. Airspeed indicator 1 1b. (-24)
Miscellaneous (not listed above)
601. Wing tip skids 4 1bs. (*21)
Prior to original certification, each glider must satisfactorily
An inspection for workmanship, materials and conformity before
any covering or final finish
A final inspection of the completed glider.
A check of flight characteristics.
A glider of the model manufactured by other than Eugene !. Ardelt
(formerly University of Denver) eligible for an airworthiness
is submitted to the effect that the
glider was constructed in accordance with the approved Eugene M. Ardelt
(University of Denver) Construction Manual and
pati and my pass insection eved in NoT A Such glider must
weight report only required. The actual empty weight to be used
for certification shall not exceed 375 1bs. and the empty weight C.G
range is (+38.3) to (+39.75). Weight report shall include list of
equipment included in empty and must be submitted
for each glider with the original agent's report and each subsequent
report covering a change in equipment.
NOTE The follars bested it view of the hot: 'Minimum weight of pilot and ballast in cockpit
Pilot Weight (lbs.)
Full Down".
"Airplane tow prohibited."
"Cloud soaring prohibited."