DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION A8CE Revision 2 Mitchel Waco RPT March 23, 1978 TYPE CERTIFICATE DATA SHEET NO. A8CE This data sheet which is part of type certificate No. A8CE prescribes conditions and limitations under which the product for which the type certificate was issued meets the airworthiness requirements of the Federal Aviation Regulations. Type Certificate Holder: Dean W. Mitchel 18330 West Burleigh Brookfield, Wisconsin 53005

I - Model Waco RPT (Restricted Category) Approved July 13, 1965 Engine: Kinner R-56 Fuel: 73 minimum octane aviation gasoline Engine limits: For all operations, 1850 r.p.m. (160 hp.) Propeller: Sensenich 90HA-90, including hub 53 lb. (-38) Airspeed limits: (CAS) Never exceed 145 m.p.h. (126 knots) Maneuvering 115 m.p.h. (100 knots) C.G. range: (+37.0) to (+40.5) at 1975 lb. (+34.0) to (+42.0) at 1875 lb. or less. Straight line variation between points given. Empty weight C.G. range: None Datum: Front face of firewall Leveling means: First fuselage longeron below cockpit opening on left side. Maximum weight: 1975 lb. No. seats: 2 (+48.5 and +95.2) Maximum baggage: None Fuel capacity: 31 gal. (+10.3) Oil capacity: 12 qt. (+3.8) Control surface movements: Aileron Up 34° Down 21° Elevator Up 26° Down 20° Rudder Left 27° Right 27° Serial Nos. eligible: 6000 only. Certification basis: Part 8 of the Civil Air Regulations as amended to October 11, 1950. Type Certificate No. A8CE issued July 13, 1965. Application for Type Certificate dated November 6, 1963. Production basis: None. No aircraft may be produced under this approval. Equipment: The basic required equipment as prescribed in the applicable airworthiness regulations must be installed in the aircraft for certification.

NOTES NOTE 1. Current weight and balance report together with list of equipment included in certificated empty weight and loading instructions when necessary must be provided for each aircraft at the time of original certification. - END -