# STC ST00107SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Altair Holdings Limited, United States
- Description: Increase in the maximum taxi and flight weights up to 183,000 and182,500 lbs.
- Applied: June 2, 1994
- Status date: August 11, 1994
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/09/81/0981285718123c4031a26abfcea3e1a8b942b26f1cb8fe0477e3748aa59605f0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C47BC3C56C8D4E7B85256CC2006A7055.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00107SE

## ADs that name it (0)

None.

## Approved models (1)

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

## 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: ST00107SE This certificate issued to: Altair Holdings Ltd.

Certifies that the change in the type design for the following produot with the limitations and conditions therefor as specified hereon meets the airworthiness requirement's of Part 4b of the Civil Air Regulations.

Original Product -Type Certificate Number: A3WE Make: Boeing Model: 727-200 Description of Type Design Change:

Increase in the maximum taxi and flight weights up to 183,000 and 182,500 Ibs., for Boeing 727-200 airplanes in accordance with FAA Approved Altair Holdings Ltd., Drawing Number 2101, Revision A, dated July 21, 1994, or later FAA-approved revisions.

Approval of this change in type design applies to the above model aircraft 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 that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate and FAA Approved Drawing Number 2101, Revision A, must be maintained as part of the permanent records for the modified aircraft. The airplane must be operated in accordance with Altair Holding Ltd., FAA Approved Flight Manual Supplement No. 5, to Boeing Document Number D6-8728.

Date of Application: June 2, 1994 Date Reissued:

Date of Issuance: August 11, 1994 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Monale kulu (Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

47.

## Every issue (1)

- August 11, 1994: Issued, Current. [certificate](https://openairdocs.org/files/sha256/09/81/0981285718123c4031a26abfcea3e1a8b942b26f1cb8fe0477e3748aa59605f0)

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