# TCDS TC 2-583: American Eaglecraft Company

- Type: Type certificate data sheet
- Status: Current
- Holder: American Eaglecraft Company
- Revision: 0
- Product: Aircraft, Small Airplane
- Certification basis: CAR 4a
- Data sheet PDF: https://openairdocs.org/files/sha256/1b/78/1b785cec00700feff88ab4feef354f625efb5d573bcb60d9e491d78e08d25319
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A686B975F5B224DE8525672E00467C88.0001
- Page: https://openairdocs.org/tcds/TC%202-583

## Models (1)

As the data sheet lists them.

- American Eaglet A-31-1B

## What the data sheet says

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

```text
AMERICAN EAGLECRAFT COMPANY
MODELS: American Eaglet A-31-1B, 2 PO-CIM
T.C. NOMBER: 2-583 (Approved 7/3/46)
Engine  Continental A-50-8 or A-50-8F
Fuel  73 minimum octane aviation gasoline
Engine limits  For all operations, 1900 rpm (50 hp)
Airspeed limits  Level flight or climb - 100 mph True Ind.
Glide or dive - 120 mph True Ind.
Propeller limits  Static rpm at maximum permissible throttle
Not more than 1750, not less than

Not more than 76 in., not less
than 74.5 in.
C.G. range
(*12.4) (21.2 percent MAC) to
(+18.6) (31.8 percent MAC)
At 1100 1bs. maximum weight:
(+17.0) (29.1 percent MAC) to
(+18.6) (31.8 percent MAC)
(Straight line variation between forward
limits for intermediate weight)
Datum  Wing leading edge (with airplane level)
MAC  58.4 in I.E. of MAC at (0)
Leveling means  Top longeron on left side in cockpit
Maximum weight
NO -  seats  2 (front at (+15), rear at (+42))
Baggage
Fuel capacity
0i1 capacity  1 gallon (-38)
Control surface  Elevator  Up 18 degrees  Down 19 de
movements  Aileron  17 degrees  18 de
Right 48 degrees  Left 48 de
Stabilizer  Fixed
Serial Nos. eligible  1201 and up (See NOTE A)
Required equipment  Airloithloess Certificate only (CAR 04a)
Certification basis
Production basis  None (See NOTE A)
eligible for export as follows  in Chapter  XII of Manual of Procedure.  subject to inspection for equipment sp
Canada
- Landplane - eligible
skiplane -  eligible
All other countries except Australia and New Zeland.
Equipment:
Items included in required list under specifications pertinent to
individual models may not  be removed unless replaced by approved equiv
The effect  upon balance of all equipment changes must be computed
the aircraft operations record revived accordingly
Values in inches shown in parenthesis after  each item represent
horizontal arrs to the C.G. of  the item measured minus (-)
(+)  to the rear of  the datum.  A plus (+)  (-) sign preceding
weight of an optional item indicates the net weight change between tha
the equivalent required item.
Propeller and Propeller Accessories
Propeller (including hub)  Fahlin D371-48(76) 16 1bs. (-56) 0
other fixed pitch wood  propeller eligible for the engine
and power and which meets the static rpm and diameter
specified under "Propeller limits" on Page 1.
Engine  and  Engine Accessories
101.  Carburetor air heater  2 1bs.  1-38
Landing Gear
Goodyear Model 3-LNBM with
18x8-3 4-ply tires  26 1bs.  (+2)
Goodyear  Model I6NBD with
6.00-6 4-ply tires  25 1bs.  (+2)
202.  Tail wheel
Uniloy Model 3000-A1 with
Pirestone 6x2  solid tire  • 1DS.  1+20
Scott type 3000B-2  • 1bs.  1+20
Interior Equipment
401.  Cabin enclosure  (American Eaglecraft
Drawing D-27-02)  8 1bs.  (+29
Miscellaneous (not listed above)
600.  Miscellaneous items as noted in the
approved weight and balance report.
Each aircraft manufactured must, prior to original certificat
satisfactorily pass:
An inspection for workmanship,  materials and conformity to tr
pertinent technical data before any covering, metal
final finish is applied.  All woodwork may be varnished.
A final inspection of the completed aircraft.

(c) A check of the flight characteristics.
NOTE 1-  the rollowing permanent placard should be dispidyed on int
instrument panel in full view of the pilot
"INTENTIONAL ACROBATICS PROHIBITED.
SOLO FROM FRONT SEAT ONLY."
```

## ADs

None name its models.

## STCs approved under this data sheet (2)

- [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC
- [STC SA347NW](https://openairdocs.org/stc/SA347NW): Installation of a McCauley 1B90-CN7443 propeller on a Continental A-65-8F engine. Spach, Charles M.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.