What it approves
Structural reinforcement of wing root area to increase strength and durability.
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: SA1795NM This certificate issued to: Dennis Childers Part 8 of the CIVil Air Regulations:
Original Product - Type Certificate Number: ATWE Make S. L. Industries Model: Callair B-l and B-TA Description of Type Design Change: . Structural reinforcement of the wing spar root web to obviate spar replacement in accordance with ASW-190.25 letter dated January 21, 1983.
Limitatuneandtonditina: Approval of this change in type design applies to the above model Callair B-1 and B-1A only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other That be for is ne as are of no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate previously approved modifications, including changes in type design, will introduce must be maintained as part of the permanent records for the modified aircraft.
Tate s/ upplication: November 29, 1982 Gut missued:
Date of Issuance: June 27, 1983 Date Amended:
FEDERAL AVIATION By Direction of the Administrator HEltera ( Signature ) PAINISTER DE Manager, Seattle Aircraft Certification Office (Title) 47 FAA FORM 8110-2 (10-68)
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