# STC ST00117SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Altair Holdings Limited, United States
- Description: For operation up to 197,700 lb maximum taxi weight, Increase in the maximum zero fuel weight to 155,000 lbs and increase in the maximum landing weight up to 164,000 lbs
- Applied: May 2, 1994
- Status date: June 6, 2001
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A3WE](https://openairdocs.org/tcds/A3WE)
- Certificate PDF: https://openairdocs.org/files/sha256/10/2c/102cb0b2838398445d2fa8de61162ec9ca8e3c50d82b48a7ff69397459d73d8f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D25D43036F384669862579AD006AA7A3.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST00117SE

## 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.

Where Hae Department at Campura-chard Arabin Againesation Supplemental Type Certificate Number: ST00117SE This certificate issued to: Altair Holdings Ltd.

Part 4b of the Civil Air Stegulationd (See Type Certification Data Sheet AWE for the complete certification basis), Original Product -Type Certificate Lumber AGWE Make: Boeing Model 727-200 Despite of tir Jane Slager Elange: For operation up to 197,700 lb. maximum taxi weight, increase in the maximum zero fuel weight to 155,000 lb., and increase in the maximum landing weight up to 164,000 lo., for Boeing 727-200 airplanes in accordance with FAA Approved Altair Holdings Ltd., Drawing Number 4102, dated June 20, 1894, or later FAA-approved revisions For operation up to 203,600 Ib. Maximum taxi weight. increase in the maximum zero fuel weight to 155,000 lb., and increase in the maximum landing weight up to 166,000 lb.. for Boeing 727-200 airplanes in accordance with FAA Aproved Altair Holdings Ltd., Drawing Number 4104, Revision B, dated June 1, 2001, or later FAA-approved Simulatoes and Sanditint- Approval of this change in type design applies to the above model aircratt 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 4102 or 4104, which ever is applicable, must be maintained as part of the permanent records for the modified aircraft. The airplane must be operated in accordance with Altair Holding Ltc., FAA Approved Flight Manual Supplement No. 4, or 10, whichever is applicable, la Boeing Document Number D6-8728

Date of Application: May 2 1994 Bate mosued?

Date of Issuance: - August 26, 1994 Date Amended: June 14, 1995; October 25, 1995; June June 6, 2001 воС: Sy duration gret 10-. 1 2] *EAST PA 102 Acting Manager, Seattle Aircraft Certification Office (Titie)

FAR FORS 1110-2110-63|

## Every issue (1)

- June 6, 2001: Amended, Current. [certificate](https://openairdocs.org/files/sha256/10/2c/102cb0b2838398445d2fa8de61162ec9ca8e3c50d82b48a7ff69397459d73d8f)

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