STC SA2319NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2319NM This certificate issued to: JAKE E. BRYANT 3325 LAKESHORE DRIVE ANCHORAGE, ALASKA 99503 Purt 3 of the CIVII AIR Regulations:

Original Product - Type Certificate Number: 1A6 Make: PIPER Model: PA-22-150 Description of Type Design Change:

Installation of Piper PA-14 wings, modification of lift struts, lengthening of the fuselage, and installation of Piper PA-18 empennage to an aircraft with STC #SA45RM (conversion from tricycle landing gear) and STC #SAllRM (installation of Cleveland wheel & brake kit) installed. All information and descriptive data pertaining to this modification are contained in STC Project file #A34-5.

Data pertaining to this modification are considered inadequate to permit duplication on other aircraft. This STC pertains to aircraft (S/N 22-4229; R/N N6949B) only.

FAA Approved Airplane Flight Manual Supplement dated December 20, 1985, or later FAA approved revision is required.

Date of Application: February 18, 1983 Date Reissued:

Date of Issuance: December 22, 1985 Date Amended:

FEDERAL AVIATION Layton O. Curtis By Direction of the Administrator DAYTON O. CURTIS (Signature)

TOMINISTRATO ANCHORAGE AIRCRAFT CERTIFICATION OFFICE

NORTHWEST MOUNTAIN REGION (Title) 47 FAA FOR 8110-2 (10-68)

Jake E. Bryant 3325 Lakeshore Drive Anchorage, Alaska 99503 LIMITATIONS: (Normal Category Only) The following limitations must be observed in the operation of this airplane:

C.G. Range (inches aft of wing leading edge):

(+17.5) to (+24.0) @ 1935 1bs.

(+12.0) to (+24.0) @ 1490 lbs.

(+11.5) to (+24.0) @ 1240 lbs. or less Maximum Weight: 1935 lbs. (takeoff and landing) Maximum Baggage: 100 1bs. @ (+67.0) Engine: Avco Lycoming 0-320-A2B (150 HP @ 2700 RPM) Engine Limits: For all operations 2700 RPM.

Fuel: 80/87 Minimum Aviation Gasoline Propeller: Sensenich M74DM Maximum Diameter 74.0 inches Minimum Diameter 72.5 inches Static Limits: Maximum 2480 RPM Minimum 2290 RPM Fuel Capacity: 17.5 U.S. Gallons in each wing tank @ 23.0

35.0 U.S. Gallons total fuel @ 23.0 Flaps (3 positions): Full Up = O degrees Intermediate = 18 degrees Full Down = 40 degrees Airspeed Limits (True Indicated Airspeed):

Flaps Extended 87 MPH Maneuvering 99 MPH Max. Structural Cruise 110 MPH Never Exceed 138 MPH IV. PROCEDURES: No Change III. PERFORMANCE: No Change

FAA APPROVED Make: December 20, 1985 Page 3 of 3