What it approves
Delete righthand rudder tab and system; install rudder control system bungee and shut-off valve.
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.
This certificate issued to: Staggerwing Museum Foundation, Inc.
560 Old Shelbyville Hwy Tullahoma, TN 37388
Part * of the Civil Air Regulations. * CAR 03 effective 11/13/45 and 3.242 of CAR 3 effective 11/01/49 as amended by 3-14.
Original Product - Type Certificate Number : 765 Make : Beech Model : C-45G/H and TC-45G/H
(1) Delete right-hand rudder tab and system in accordance with Section III.F of Airline Training, Inc. Report No.
13001, Revision No. 1 dated 01/05/59.
(2) Installation of rudder control system bungee in accordance with ATI Report No. 13001, Revision No. 1 dated 01/05/59, and ATI Drawing No. 12032 dated 12/07/58.
(See Continuation Page 3 of 3.)
(1) Airline Training, Inc. Supplement dated 08/19/58 to CAA approved Beech C-45G, TC-45G, C-45H and TC- 45H Airplane Flight Manual dated 02/18/58, or Airline Training, Inc. CAA approved Airplane Flight Manual dated 10/16/58 for Beech C-45G, TC-45G, C-45H, and TC-45H required.
(2) When Airline Training, Inc. speed-up kit, STC SA4- 113, is installed, CAA approved Airline Training, Inc.
Airplane Flight Manual Supplement dated 08/20/58 as revised 11/14/56 is required.
(3) Airworthiness compatibility of this STC with all ot her major changes to the standard original model(s) shown above should be confirmed prior to installation of this STC.
(4) If the holder agrees to permit another person to use th is certificate to alter the product, the holder shall give the other person written evidence of that permission.
Date reissued : December 9, 1966; August 15, 1968;
February 26, 1990; October 6, 2006 Date amended : February 26, 1959
Original signed by Robert D. Adamson
( Signature) Robert D. Adamson Program Manager Wichita Aircraft Certification Office (Title) Date of application : July 14, 1958 Date of issuance : September 5, 1958
FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES
Number SA2-625
Date Issued: September 5, 1958 Date Amended: February 26, 1959 Date Reissued: December 9, 1966 Date Reissued: August 15, 1968 Date Reissued: February 26, 1990 Date Reissued: October 6, 2006
(3) Installation of Harding Devices Co. shut-off valve No. 24-125C as an alternative to manual shut-off valve which is shown on ATI Drawing No. B13090 in accordance with ATI Report No. 13001, Revision 1 dated 01/05/59, and installation instructions for Dwg. No. B13091 dated 08/18/58.
(4) Military surplus C-45G, TC-45G, C-45H, and TC-45H airplanes modified in accordance with Airline Training, Inc. Report 13001, together with data listed therein, and having the required and any optional equipment shown on Aircraft Spec. A-765 installed are eligible for original airworthiness certification.
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.