# STC SA3334WE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Air Medic LLC, United States
- Description: Installation of stretcher carrier, AM 2003.
- Applied: November 15, 1976
- Status date: August 21, 2003
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE)
- Certificate PDF: https://openairdocs.org/files/sha256/e9/60/e960c8c2a92789cffb1170b594af2f8962c5c6cd31753655e26a4f3aa3598603
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/236A09DBF0D674DE8625788E00516846.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3334WE

## ADs that name it (0)

None.

## Approved models (5)

- The Boeing Company 737-100 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-200 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-300 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-400 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))
- The Boeing Company 737-500 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))

## What the certificate says

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA3334WE This certificate issued to: AIR MEDIC, L.L.C.

7309 Clybourne Avenue, Unit 3 Sun Valley, California 91352 Part 25 of the Federal Aviation Pegulations.

Original Product Type Certificate Number: A16WE Moatin : The Boeing Company Model: 737-100, -200, -300, -400, -500 Series Description of Type Design Change: Installation of Stretcher Carrier, in accordance with FAA Sealed Air Medic Stretcher Carrier Master Drawing List AM-2001, Revision "Z", dated August 12, 1988, or later FAA approved revision, and utilization in accordance with Air Medic Operations Specifications AM 2017, is required as part of this installation.

Limitations and Conditions: The approval of this change in type design applies basically to the Boeing 737-100, -200, -300, -400, -500 Series only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between the change and those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.

Date of Application: November 15, 1976 Date Amended: April 28, 1989, January 14, 1993, Date of Issuance: February 8, 1977 August 21, 2003 (Signature) TOMINSTRATON Program Manager, Systems and Equipment Branch Los Angeles Aircraft Certification Office (Title)

## Every issue (1)

- August 21, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e9/60/e960c8c2a92789cffb1170b594af2f8962c5c6cd31753655e26a4f3aa3598603)

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