# STC SA2044NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Ancra International LLC, United States
- Description: Installation of cargo conveyor restraint systems. (737-200F3P)
- Applied: January 11, 1984
- Status date: March 29, 2012
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE), [TCDS A3WE](https://openairdocs.org/tcds/A3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/2b/de/2bde136fd3a46949b44c61830e9ec8a0c898e7964acc282939a6918a73e42e6a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7A19F9956E02DFCA862579E9005DEB35.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2044NM

## ADs that name it (0)

None.

## Approved models (4)

- The Boeing Company 727-200 Series ([TCDS A3WE](https://openairdocs.org/tcds/A3WE))
- The Boeing Company 727-200F Series ([TCDS A3WE](https://openairdocs.org/tcds/A3WE))
- The Boeing Company 727C Series ([TCDS A3WE](https://openairdocs.org/tcds/A3WE))
- The Boeing Company 737-200C Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

Number SA2044NM

Ancra International LLC 875 W . 8th Street Azusa, California 91702 This Certificate issued to

Part 25 of the Federal Aviation Regulations.

A3W E

Boeing

737-200C, -200F, -200CF3P Description of Type Design Change:

Installation of Cargo Conveyor Restraint System in accordance with FAA approved ANCRA Drawing List DL 80200, Revision “A”, dated February 7, 1984, or later FAA approved revision.

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

Date reissued : January 30, 1992; October 8, 1996; March 29, 2012

Date amended : June 20, 1984

( Signature) Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office

(Title) Date of application : January 11, 1984

Date of issuance : May 25, 1984

Number (STC No.)

## Every issue (2)

- March 29, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/2b/de/2bde136fd3a46949b44c61830e9ec8a0c898e7964acc282939a6918a73e42e6a)
- October 8, 1996: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/08/d5/08d57e5709d2e39e1d52d31496f67ce0325c5a42d746793a46d519082496fa8f)

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