What it approves
Replacement of the original engine oil screen with an external mounted full flow oil adapter & spin-on filter.
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: SE4314NM This certificate issued to: Allen E. Timberman Purt 13 of the CiViT Air Regulations: effective June 15, 1956, as amended by 13-1 through 13-5.
Original Product - Type Certificate Numben: E5CE Make: Continental Model: IO-520-A, D, E, F, J, K, and L terplion ye ughange adapter and spin on filter in accordance with FAA sealed Replacement of the original engine oil screen with an copies of Timberman Master Drawing List No. AT-2-I0-470-DL, revised March 30, 1988, and Installation Instructions No. AT-2-10-470-II, revised March 30, 1988, and Installation Instructions No. AT-2-10-470-II, revised March 30, 1988, or later FAA Approved revisions.
this change and any other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of these engines.
Date of Application: July 3, 1985 Juk missed: June 16, 1987; August 5, 1993 Date of Issuance: June 26, 1986 Jake mundul: September 21, 1988; August 5, 1993 FEDERAL AVIATION By Direction of the Administrator Manager, Special Certification Branch TOMINISTRATO Seattle Aircraft Certification Office (Title)
47.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SE4314NM Limitations and Conditions: (continued):
Supplemental Type Certificate HOLDER: Allen E. Timberman Limitations and Conditions: shown on Type Certificate Data Sheet No. E5CE for Continental Models I0-520-A, D, E, F, J, K, and L engines remain applicable.
The installation of an engine modified in accordance with this STC will require a determination by the installer that no interference is created with existing aircraft systems.
Engines equipped with the limberman spin-on oil filter must continue to be maintained in accordance with the original engine manufacturer's maintenance instructions, except as indicated on an FAA sealed copy of Timberman Maintenance Instructions No. AT-2-10-470-M1, dated May 5, 1986, or later FAA Approved revision, a copy of which must be added to the engine maintenance records.
This SIC covers the fabrication of all parts associated with this oil filter installation and also the physical modification of the engine models listed on this Certificate. Associated STC No. SA4320NM covers the use of these modified engines on specific airplane models, and also covers the mounting of the oil filter, filter base, and mounting plate on the firewalls of these airplanes.
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FAA FORM 8110-2-1 (10-69) PAGE 3 OF 3 PAGES FAN AC 92.03578
ADs that name this STC · 0
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