STC SA3319WE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA3319WE This certificate issued to: ROGERSON ATS Certificate

SURRENDERED 5/12/08 Part 4b of the CiVi 1 AiT dated December 1953. Amendment 4b-1 thru 4b-11; Special CAR No. SR-422B.

Anginal 99, 901g, 8503, un i o3 and FAR 21° Regulations&pec! a! ConditIons listed In Attachment A of FAA letter to Boeing set forth in FAA letter 1963 and SFAR 27 thru Amendment 1.

Make: Boeing Model: 727-30 Description of Type Design Change:

Installation of auxiliary fuselage fuel tanks (1600 gallons) in the forward and aft cargo compartments in accordance with FAA sealed Aircraft Tank Service So dated eume 25127.4 is Feel red for the Model 927-30 as part of this Summary Drawin, 4600, Revision E, or later FAA-Approved revisions, Aircraft Tank 727-30 FAA-Approved Airplane Flight Manual Supplement No.

is required for the Model 727-30 as part of this Installation.

(See page 3 of this STC.)

Date of Application: Apri1 5, 1976 Lute wissued: March 4, 1991 Date of Issuance: December 28, 1976 Date Amended:

FEDERAL AVIATION for Manager, Los Angeles Aircraft * MINISTRATO Certification Office (Title)

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 ) Extent of Authority (if licensing agreement):

Signature of grantor (In ink): -

(1) December 28, 1976 (R) March 4, 1991 Number SA3319WE Limitations and Conditions:

The approval of this change in type design requires verification of compliance to SFAR 27 through Amendment 1 and applies basically to the Model 727-30 airplane equipped with the 3-tank system. This approval should not be extended to other specific aircraft of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adver se effect upon the airworthiness of that aircraft. Further, this approval is not to be used in conjunction with a cabin Interior unless the additional floor loading in excess of that of the Aircraft Tank Service AFM Supplement is approved as an independent action.

47.

PAGE 3 OF 3 PAGES FAA AC 82-03578