STC SA4208NM-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA4208NM-D Certificate This certificate issued to: Hollingsead International SURRENDERED 2226 Goodyear Avenue on - 6-19-09 Ventura, California 93003 Part 25 of the Federal Aviation Regulations.

Original Product Type Cerlificate Number 4A25 Make: McDonnell Dougias Model: DC-8-71, DC-8-73F Description of Type Design Change: Interior reconfiguration of the McDonnell Douglas model DC-8-71, S/N 46099 airplane in accordance with Lucas Aviation Inc. Master Drawing List, R10-2, Revision D, dated 15 June 1992, or later FAA approved revisions.

Interior reconfiguration of the McDonnell Douglas model DC-8-73F Series airplanes in accordance with GCS EO 25-056 (DHL-Design Inspection Report No. EM 872) dated July 16, 1987, or later FAA approved revisions.

Limitations and Conditions: If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. See Limitations and Conditions: on page 3.

SEE SHEET 3.

Date of Application: May 22, 1990 Date Reissued: April 12, 1995; August 19, 1996;

April 1, 1998; August 1, 2005; May 7, 2007 Date of Issuance: June 16, 1992 Date Amended: August 19, 1996 By Direction of the Administrator Calta K. Woo (Signature) TOMANISTRATD Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA4208NM-D Limitations and Conditions: (continued) This approval should not be incorporated on any certificated product of this model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated modifications will not introduce any adverse effect upon the airworthiness of the certificated product. A copy of this STC must be included in the permanent records of the modified aircraft. All of the above interior furnishings meet the flammability requirements of FAR 25.853(a) Amendment 25-15.

With the Cargo Loading System (2151T100) installed and with the securing eyes on the side mountings, the loads limit values specified in the DC-8-73, -73F Weight, and Balance Manual No. MDC-V0294 must be observed.

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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):

* U.S. GPO 1987-763-289 Page 2 of 2