What it approves
Installation of Hoskins High Intensity Position Light system. A supplemental condenser discharge (strobe) lighting system. Consists of red/green/white wing tip and tail position lights, with or without white, top and bottom fuselage lights, plus a power supply.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Part 3 of the Civil Air Regulations and FS-100 Message 271930.
Description of Type Design Change: (1) Installation of Hoskins High Intensity Position Light system. A supplemental condenser discharge (strobe) lighting system. Consists of red/green/white wing tip and tail position lights, with or without white, top and bottom fuselage lights, plus a power supply.
Data required: (1) Hoskins High Intensity Position Light System Installation Manual, Part IV and Specification Sheets, as amended, dated December 1, 1965; (2) Hoskins High Intensity Position Light System Installation Manual and Specification Sheet as amended February 1, 1965 (Cessna 310J S/N 310J0025 only); (3) Hoskins High Intensity Position Light System Installation Manual and Specification Sheet dated March 31, 1965.
Limitations and Conditions: The approval of this change in type design applied basically to aircraft models listed above only. This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft..
BF Goodrich Aerospace Lighting Systems Division 3445 South 5th Street Phoenix, AZ 85040 3A10 and 3A25 Cessna Make :
310-A thru –K, 320, 320-A thru –D, 320-1 Model :
Date reissued : October 17, 1974, April 1, 1990, September 25, 1995, January 31, 1996, September 30, 2011
( Signature) Melvin Taylor Manager, Atlanta Aircraft Certification Office
( Title) Date of application : December 2, 1965
Date of issuance : February 4, 1966
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 16
| Make | Model | Data sheet |
|---|---|---|
| Cessna Aircraft Company | 310A | 3A10 |
| Cessna Aircraft Company | 310B | 3A10 |
| Cessna Aircraft Company | 310C | 3A10 |