What it approves
Installation of a Continental O-470-R engine, Hartzell HC-82XF-1B/8433-O propeller and Cessna 60 amp alternator (P/N C611501-0102)
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: SA82ANW This certificate issued to: Tim Heneghan Purt 3 of the CiVi1 Air Pugelations:
Original Product - Type Certificate Number: 5A6 Make: Cessna Model: 180 Hartzell HC-82XF-1B/8433-0 propeller and Cessna 60 amp alternator (P/N C611501- Description of Type Design Change: Installation of a Continental 0-470-R engine, 0102) in accordance with Tim Heneghan photographs 1 through 5.
Limitations and Conditions: Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Cessna 180, Serial Number 30309 only. A copy of this Certificate and Addendum No. SA824NW shall be maintained as part of the permanent records for the modified aircraft.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) August 16, 1979 Number SAB2ANW Supplemental Type Certificate ADDENDUM NO. SA824NW The conditions and limitations of Type Certificate Data Sheet Number 5A6 apply except where superseded by the following:
Supplemental Type Certificate Data Sheet, which is part of STC SA824NW, prescribes the conditions and limitations under which the product for which the STC was issued meets the airworthiness requirements of the Federal Aviation Regulations.
Supplemental Type Certificate HOLDER: Tim Heneghan CESSNA MODEL 180, 4PCL-SM, (NORMAL CATEGORY) AS MODIFIED BY SIC SA824NW Engine: Continental 0-470-R Fuel: 80/87 octane minimum grade aviation gasoline Engine Limits: For all operations, 2600 rpm (230 Hp) Propeller and Hartzell HC-82XF-1B/8433-0 Propeller Limits: Diameter: 841 maximum; 8.20 minimum Pitch Setting: Low; 28.0° High Propeller Governor: See Data Sheet 5A6 Powerplant Instrument Markings: Oil Tempere ure to 2255 - normal operating range Yellow Arc 30 to 60 psi - normal operating range Red Line 10 psi minimum, 100 psi maximum Tachometer:
Green Arc 500 to 2600 rpm - normal operating range Red Line 2600 rpm - maximum Fuel Flow:
Green Arc 0 to 25 gph - normal operating range Red Line 18.5 psi maximum at sea level F - normal operating range C. G. Range: See Data Sheet 5A6 Maximum Weight: 2550 pounds Serial Number Eligible: 30309 only
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PAGE 30F 3 PAGES C FAA AC 73-2651
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 |
|---|---|---|
| Cessna Aircraft Company | 180 | 5A6 |