What it approves
Modification involves fabrication and installation of new skins and doublers around the gearboxes and baggage door
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.
FAA FORM 8110-2(10-69) Sheet 1 of 3 Number SA01458WI
Barron Aviation, LLC 30530 Highway Y Perry, MO 63462 This certificate issued to:
Part 3 of the Civil Air Regulations and Part 23 of the Federal Aviation Regulations (See continuation sheet 3 of 3.)
Original Product Type Certificate Number: A-790
Make: Cessna
Model: 190, 195, 195A, 195B, LC-126A, LC-126B, LC-126C
This modification involves fabrication and installation of new skins and doublers around the gearboxes and baggage door in accordance with Barron Aviation Drawing and Document List, BA-311-DL, Revision 7, dated August 28, 2007, or later FAA approved revision.
1. Compatibility of this design change with previously approved modifications must be determined by the installer.
2. 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.
This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.
Date of application: January 20, 2006
Date of issuance: November 6, 2007 Date reissued:
Original signed by Dan Withers
( Signature) Dan Withers FAA Program Manager Wichita Aircraft Certification Office
( Title)
FAA FORM 8110-2(10-69) Sheet 3 of 3 Number SA01458WI
Date of issuance: November 6, 2007
Certification Basis (continued):
The certification basis for the Cessna aircraft models identified on Page 1 of this certificate is as follows:
a. The type certification basis for the Cessna aircraft models identified on Page 1 of this certificate is shown on TCDS A-790 for parts not changed or not affected by this change.
b. The type certification basis for the parts changed or affected by this change since the reference date of application, February 20, 2006, is shown on TCDS A-790. Additionally, the applicant has voluntarily complied with 14 CFR Part 23 as reflected below:
14 CFR Amendment 14 CFR Amendment
23.23 23-45 23.485 23-45
23.25 23-50 23.493 23-38
23.29 23-21 23.505 23-7
23.301 23-48 23.521 23-48
23.303 23-38 23.601 23-38
23.305 23-45 23.603 23-23
23.307 23-38 23.605 23-23
23.341 23-48 23.607 23-48
23.361 23-45 23.609 23-38
23.363 23-38 23.613 23-45
23.471 23-38 23.625 23-7
23.479 23-45 23.627 23-38
23.481 23-38 23.1529 23-26
23.483 23-38
…END…
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