What it approves
Installation of a Contental engine, Hartzell propeller, and associated systems
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SAI103N4 This certificate issued to: Aircraft Specialties, InC.
Certifies that the change in the type design for the fellaving preduct with the limitations and conditions thereforas specifudhoreen meets the airworthinessnequirements of Purt 3 ofthe Civil Air Regulations, dated May 15, 1956.
Original Product - Type bertificate Number: 3A15 Make: Beech Model: E33 Description of Type Design Change: Installation of a Continental 10-520-BA engine, Hartzell PHC-A3VF-2B/V8433-4R propeller, and associated systems in accordance with Aircraft Specialties, Inc. photographs 1 through 4.
timilaliensand bonditiona:Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Beech E33, Serial Number CD-1132 only. A copy of the Certificate and FAA Approved Airplane Flight Manual Supplement shall be maintained as part of the permanent records for the modified aircraft.
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT TO BEECH E33; SERIAL NO. CD-1132; REGISTRATION NO. N66EE
FAA APPROVED AIRPLANE FLIGHT MANUAL The information in this document is FAA approved material which, together with the appropriate basic CAA/FAA Approved Airplane Flight Manual, is applicable and must be carried in the basic manual when the airplane is modified by the installation of a Continental 10-520-BA engine and a Hartzell PHC-A3VF-2B/V8433-4R propeller, STC SA1103NW.
The information in this document supersedes the basic manual only where covered in the items contained in this supplement. For Limitations, Procedures and Performance not contained in this supplement, consult the basic manual.
1. LIMITATIONS Engine Continental 10-520-BA Fuel: 100/130 minimum grade aviation gasoline Engine Limits: Takeoff (1 min) 2700 rpm (285 Hp) @ sea level Maximum continuous power: 2600 rpm full throttle Propeller and Propeller Limits: Hartzell PHC-A3VF-2B/V8433-4R Diameter: 80" maximum; 78⅖" minimum Pitch: 10.8 ‡ .2° Low; 32.0° High Powerplant Instrument Markings: Tachometer: 2700 rpm (red line) Cylinder Head Thermocouple: 460°F (red line) Oil Temperature Gauge: 240°F (red line) Oil Pressure Gauge: Minimum - 10 psi (red line) Maximum - 80 psi (red line) Normal - 30 to 60 psi (green arc)
NOISE CERTIFICATION PROCEDURE Compliance with FAR 36, Appendix F, was shown with the tollowing procedures:
Level flyover at 1000 feet AGL at 2600 engine rpm and full throttle manifold This noise level reday as well as a -4.4 dB(A) credit resulting from aircraft takeoff and climb characteristics.
PROCEDURES No change
PERFORMANCE Performance with the above engine and propeller combination installed is equal to or better than the data in the FAA Approved Flight Manual.
FAA APPROVED: naila C kroeder Acting Chiet, Seattle Area Aircraft Certification Office Make: _ November 19, 1980 AMENDED DATE: February 4, 1981
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Hawker Beechcraft Corporation | E33 | 3A15 |