What it approves
Installation of Benz Part Number PCS-111A Continuity Sensor in the engine, tail rotor gearbox, intermediate gearbox, and main transmission chip detectors
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.
This Certificate issued to
Part 27 of the Federal Aviation Regulations.
Original Product Type Certificate Number : H3EU Make : Eurocopter Deutschland Model : BO-105C, BO-105S
Installation of Benz Part Number PCS-111A Continuity Sensor in the engine, tail rotor gearbox, intermediate gearbox, and main transmission chip detectors in accordance with Benz Airborne Systems, drawing list BAS-005-003-DL-001, dated July 30, 1993, or later FAA approved revision.
1. Rotorcraft Flight Manual Supplement dated July 30, 1992, or later FAA approved revision is required.
2. Compatibility of this modification with previously installed equipment must be determined by installer.
Meggitt, Orange County, Inc.
14600 Myford Road Irvine, CA 92606 Date reissued : 1/15/99; 10/13/00; 7/22 /13
Date amended : August 2, 1993 Revision 1
(Signature) Robert G. Mann Manager Boston Aircraft Certification Office
(Title)
Date of application : January 20, 1992
Date of issuance : July 30, 1992
Transfer the ownership of Supplemental Type Certificate Number
to (Name of transferee)
(Address of transferee) (Number and street)
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from (Name of grantor)(Print or type)
(Address of grantor) (Number & street)
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Signature of grantor (In ink):
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.