What it approves
Modifications consist of spar reinforcements.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
WE - 70- FEDERAL AVIATION AGENCY Form Approved, Budget Bureau No. 04-R015 INSTRUCTIONS - Submit in triplicate to local FAA Flight Standards Inspector. Copy will be Supplemental Type Certificate returned to applicant upon issuance.
1. NAME AND ADDRESS OF APPLICANT Supplemental Type Certificate APPLIED FOR:
AIRCRAFT TECHNICAL SERVICE,ING. AIRCRAFT ENGINE PROPELLER
ORIGINAL MODEL DESIGNATION 16021 Arminta Street Van Nuys, California NEW MODEL DESIGNATION (If desired) None
3. DESCRIPTION OF CHANGE Modifications consist of spar reinforcements per Aircraft Technical Services, Inc. FAA sealed Drawing Summary No. 756.
Limitation of Applicability: The approval of this change in type design applies to Model A-26B or A-26C aircraft only. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the inter-relationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.
• WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS? YES NO
b. WILL PARTS BE MANUFACTURED FOR SALE (Ref. CAB 1.55)? ] YES NO
5. SIGNATURE AND TITLE OF APPLICANT
SIGNATURE Date of Application: Prentient
6. To be completed by FAA NATURE AND LOCATION OF DATA The drawings listed on Drawing Summary No. 756, Change G, together with the substantiating data and Forms FAA-1600 are on file at Aircraft Technical Service, Inc. and at the Aircraft Engineering Division, FAA, Western Region Los Angeles, California Certification and Approval Basis: CAR Part 9, CAR 04 of November 9, 1945 and CAR 4b.270 (b).
Note: This change to the lower front spar cap is considered an approved modificatior within the meaning of Paragraph (d) of Airworthiness Directive 64-12-3 as ammended on AD Card 65-4. If both the lower front spar cap and the rear spar ORIGINAL TYPE CERTIFICATE NO. FAA APPROVAL amended on AD Card 65-4.
1-3-3 Original signed by Supplemental Type Certificate NO. Rocco L Lippis SA926WE Charles R. Hawks, Chief GNATURE Aircraft Engineering Division
DATE OF APPROVAL April 22, 1965 TITLE Form FAA-2417 (5-59) 3540
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.