STC SA1470NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1470NM This certificate issued to: Elton I. George Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meels the airworthiness reguirements of Purt 42 of the Civil Air Regulations:

Original Product - Type bentifcate Number: A -759 Make: Bellanca Model: TAC con are Duilange continental 0-200 A engine, a McCauley 1A101/GCM 6948 Installation of a six foot shorter span wing, two 6.5 propeller, a 3-inch propeller spacer, and a gross weight increase to 1317 pounds in accordance with Keefer Aircraft Engineering Report No. W-100.

Limilalionsandbindilions: Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Bellanca Model 7AC, Serial Number 7AC-664, only. A copy of this Certificate, and Addendum, shall be maintained as part of the permanent records for the modified aircraft.

Supplemental Type Certificate HOLDER: Elton I. George BELLANCA (AERONCA) 7AC (LANDPLANE - NORMAL CATEGORY) AS MODIFIED BY STC SA1470NM.

ENGINE: Continental 0-200-A ENGINE LIMITS: 100 hp @ 2750 rpm PROPELLER: McCauley 1A101/GCM 6948 PROPELLER LIMITS: 100 hp @ 2750 rpm STANDARD PITCH: 68" to 38" Maximum Diameter: 69" Minimum Diameter: 67" No rpm restrictions C. G. RANGE (+10.9) TO (+17.0) EMPTY WT. C.G. RANGE: None MAXIMUM WEIGHT: 1317 pounds NOTE 2: The following additional placard must be placed in full view of the pilots:

SPINS PROHIBITED VNE = 120 mph

SOLO FRONT SEAT ONLY MAX. WEIGHT 1317 LB.

C.G. (+10.9) to (+17.0)

47.