What it approves
Installation of engine exhaust tail pipe extension.
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.
Number SH1138CE This certificate issued to
Part 6 of the Civil Air Regulations dated January 15, 1951, including Amendments 6-1 through 6-8 except CAR 6.604(c). Additional CAR’s and FAR’s as noted on TC Data Sheet Number 4H12.
Description of Type Design Change: Installation of engine exhaust tail pipe extension in accordance with Kinzie Drawing List Number 3-269-3-10-75, Revision B, dated January 22, 1988, or later FAA approved revision.
Limitations and Conditions: Eligible only on Schweizer Aircraft Corporation Models 269B and 269C having Hughes P/N 269A4593 or 269A8241, or 269A4593 (modified per Hughes Service Information Notice N-110), muffler installed. Compatibility of this modification with other previously approved modifications must be determined by the installer. Parts manufactured under this STC may have been produced without an FAA approved quality control procedure. Prior to installation, such parts must be inspected for conformity and airworthiness in accordance with FAR’s 21 and 43. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
Kinzie Industries, Inc.
115 Cheesman St.
Erie, CO 80516 4H12 Make : Schweizer Aircraft Corporation Model : 269B, 269C
Date of application : March 10, 1975
Date of issuance : May 23, 1975
Date reissued : February 2, 2010
Date amended : 11/6/85; 1/27/88 Rev. 2
( Signature) Lance T. Gant, Manager Rotorcraft Certification Office, Southwest Region
( Title)
FAA Form 8110-2-1(10-69) Page 2 of 3
FAA Form 8110-2-1(10-69) Page 3 of 3
Number SH868SW Date of Issuance: December 18, 1967 Date Amended: January 16, 1969
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.