What it approves
Wing truss reinforcement, front spar, and change of hinge points for landing gear idler arm.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA 1123 WE This certificate issued to: Fred J. Miller Part 3 of the CIViI Air Hequlalind. effective November 13, 1945.
Original Product - Type bertificates Lumber A-777 Mak. Beech Muled: 35 and 35R Jescriplin /ype Jesin thunge: Wing Truss Reinforcement, Front Spar, and Change of Hinge Points for Landing Gear Idler Arm per Miller Aircraft FAA Sealed Drawing List No. 1423 dated July 25, 1967, revised April 2, 1976 or later FAA approved revision.
Jimilulum andfunditin: When this change in type design has been accomplished the requirements specified in Airworthiness Directive 63-25-1, (a) shall remain applicable except that the inspection interval may be extended to - not to exceed - 1000 hours' time in service.
Jule sf upfilicution: September 10, 1966 I ute rissued:
Jule of issuance May 26, 1967 Jule unended: August 8, 1967, June 6, 196i FEDERAL AVIATION By directi SON 11 1976 инявтив., гопатите TOMINIS RATION Aerbichief, Aircraft Engineering Division 47 FAA FORM 8110-2 (10-68)
ADs that name this STC · 0
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