STC SA410EA-D

Federal Aviation Agency Sepplemental Cope Cerafrate e Number: 41051-D This certifiente, coma l American Airlines, Inc.

633 Third Avenue New York, New York Part 25 of the Federal triation Regulations.

41.22 Make: Lockheed Model: 188A-08 Description of Type Design Change:

Relocate flight data recorder installation to aft fuselage area according to Engineering Change Orders E.00900D, (1-13-67), E.00900F (4-17-67), E.00900G (10-9-57), E.00900H (1-26-68), and Dravings listed in E.00900.

This approval should not be incorported into any aircraft of this specific model on which other approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the aircraft. This modification is eligible only on aircraft which have been modified in accordance with SIC SA407EA-D.

Iate fappliculin: July 14, 1967 Date Reissued:

Date of Issuance: July 21, 1967 Tate umental: January 26, 1968 MATION AGENEA By dincti I. C. Kèene (Sigmature Coordinator - DASIFA (Title :

Ans alteration ng 51,000, or imprisonment not exceeding 3 vears, a bath

FAA FORM 8110-2 11-051 0052-657-6000

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and Z1P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and Z1P code) Exent of Authority (if licensing agreement) :

Signature of grantor (2n ink) :

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