# STC SA416EA-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: American Airlines Inc, United States
- Description: Installation of life rafts.
- Applied: January 19, 1967
- Status date: September 27, 1968
- Product: Aircraft, Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 4A30](https://openairdocs.org/tcds/4A30)
- Certificate PDF: https://openairdocs.org/files/sha256/2d/8d/2d8de43e2bb5f43f70a9b6f94dd02dfea88bccb91246416e4a9f926f1ee76bdc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6D37613AE781A97B86257DFC00537A86.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA416EA-D

## ADs that name it (0)

None.

## Approved models (1)

- AeroXin Industries Inc 30A ([TCDS 4A30](https://openairdocs.org/tcds/4A30))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

Federal Aviation Agency Supplemental Type Certificate Number: SA416EA-D This certificate issued to: American Airlines, INc.

633 Third Avenue New York, New York Certifies that the change in the type design for the following product with the limitations and conditions herefer as aperiend homon needs the rimeathines agreeats of Pent 251 of the talent treativa Rogulations.

Original Product - Type Tortificate Number: 4A30 Make: General Dynamics Model: 30 A Description of Type Design Change:

Installation of life rafts in accordance with the following American Airlines data:

1. Engineering Change Orders K.00874 dated 10/21/66, K.00874 Rev. A dated 2/3/67, K00874 Rev. B dated 5/28/68.

2. Engineering Change Orders K.00875 Rev. B dated dated 1/17/67, K.00875 Rev. C dated 8/27/68.

(See Attached Sheet) timilationsand bondilins: This STC approves only the structural aspects of the above installations. Compliance with FAR 25.1411(d) and (g), and 25.1415 has not been shown. Items 1, 2, 3, 4, and 5 above may be installed individually or concurrently.

This approval should not be incorporated in 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 direction.of.the N.. Hannon 9/27/68 g Naministrator UNITED STATES O W.P.Hannan ( Signature ) Coordinator DASIEA (Title)

**FAA FORM 8110-2 (1-66) 0052-657-6000**

Attachment to Supplemental Type Certificate #SA416FA-D Description of Type Design Change: (Contd):

3. Engineering Change Orders K.00877 Rev. A dated 1/6/67; K.00877 Rev. B dated 1/15/67 Rev. C dated 4/28/67, K.00877 Rev. D dated 9/18/67; K.00877 Rev. E dated 5/31/68, K.00877Rev. F dated 9/12/68.

4. Engineering Change Order K.00904 Rev. B dated 12/15/67; K.00904 Rev C dated 5/24/68.

5. Engineering Change Order K.00912 dated 1/16/67; K.00912 Rev. A dated 12/15/67; K.00912 Rev. B dated 5/24/68.

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 ZIP code) Exent of Authority (if licensing agreement) :

Signature of grantor (In ink) :

Page 2 of ?

## Every issue (1)

- September 27, 1968: Amended, Current. [certificate](https://openairdocs.org/files/sha256/2d/8d/2d8de43e2bb5f43f70a9b6f94dd02dfea88bccb91246416e4a9f926f1ee76bdc)

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