STC ST00167MC

Number ST00167MC Plotkin ODA-501296-CE Administrator

(Title)

FAA FORM 8110-2(10-68) PAGE 1 of 3 PAGES This certificate, issued to The Boeing Company 6001 S. Air Depot Blvd Oklahoma City, OK 73135

Part 25 of the Federal Aviation Regulations.

(See Page 3 of 3 Continuation Sheet)

Original Product--Type Certificate Number: A20WE Make: Boeing Model: 747-2G4B Description of Type Design Change: Installation of VHF-2100E VHF Communications Transceivers in accordance with Boeing Master Drawing List document number D519-61268, Revision B, dated 2019-01-25 or later FAA approved revisions.

Limitations and Conditions: (See Page 3 of 3 Continuation Sheets)

1. This STC shall not be incorporated in any aircraft of this specific model on which other approved modifications are incorporated, unless the installer determines that the interrelationship between this change and any of those previously incorporated approved modification will not introduce any adverse effect upon the airworthiness of the airplane.

2. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP Code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP Code)

Signature of grantor (In ink):

Number ST00167MC

Certification Basis (continued from page 1):

1. As defined in Type Certificate Data Sheet No. A20WE and STC SA2119CE-D.

2. Compliance to later amendment levels has been found to the following regulations:

14 CFR Part 25.1309 [25-41] 14 CFR Part 25.1316 [25-134] 14 CFR Part 25.1317 [25-122] Limitations and Conditions (continued from page 1):

3. This STC approval is for the existing configuration as defined by the approved drawing list and later FAA approved minor change which have been reviewed and approved by the appropriate ODA- 501296-CE staff members.

4. Follow on Installation of this STC modification must be accomplished at a Boeing FAA Repair Station utilizing Boeing Planning Paper as Installation Instructions or at non-Boeing repair stations with installation instructions documentation. FAA approved changes to this STC may be installed at locations other than a Boeing FAA Repair Station if the changes are prepared in the form of kit engineering and include adequate installation instructions

5. Instructions for Continued Airworthiness as documented in the Boeing Document D519-61271, Revision New or later FAA accepted revision is required.

February 5, 2019 END