# STC SA02252LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: IKHANA Group Inc., United States
- Description: Increase the maximum takeoff weight to 12,5000 lb.
- Applied: October 12, 2005
- Status date: November 18, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A9EA](https://openairdocs.org/tcds/A9EA)
- Certificate PDF: https://openairdocs.org/files/sha256/1c/27/1c271467d2dd78c6af15e05f7aceef1c93ecc070ba33f98b23f13bd5a8b2f87c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/149621CED9934CB3862586B6004C9CC2.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02252LA

## ADs that name it (0)

None.

## Approved models (1)

- Viking Air Limited DHC-6-200 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA))

## 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.

FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 1 of 3

Number: SA02252LA IKHANA Group, LLC 37260 Sky Canyon Drive, Hangar 20 Murrieta, California 92563 Part 23*of the Federal Aviation Regulations. *Certification basis set forth in Type Certificate Data Sheet A9EA

Original Product Make: Viking Air Limited Type Certificate Number: A9EA Model: DHC-6-200,

Description of Type Design Change: Increase the maximum takeoff weight to 12,500 of the Viking Air Limited Model DHC-6-200 airplane, in accordance with R. W. Martin Drawing List No. ER218- 2000, Revision D, dated August 5, 2010, or later FAA approved revision. Maintain and operate the airplane according to Master Data List No. ER218-2010, Revision B, dated October 15, 2010, or later FAA approved revision.

Limitations and Conditions: The approval of this modication applies to the above noted airplane series only. This approval should not be extended to other specific airplanes of this model series on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. 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. *Continued on Page 3.

Date of Application: October 12, 2005 Date Reissued: May 13, 2014; November 18, 2020

Date of Issuance: August 31, 2009 Date Amended: December 1, 2010

Title: Manager, Technical & Administrative Support Section Los Angeles ACO Branch

FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 2 of 3

Number: SA02252LA

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02252LA

* Limitation and Conditions Change (Continued)

Note: The modification has been substantiated to be a non-acoustic change per 14 CFR § 21.93(b).

A copy of this STC must be included in the permanent records of each airplane modified in accordance with this STC.

…………………………………………………END………………………………………………

FAA Form 8110-2 (4/20) Page 3 of 3

## Every issue (4)

- November 18, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/1c/27/1c271467d2dd78c6af15e05f7aceef1c93ecc070ba33f98b23f13bd5a8b2f87c)
- May 13, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/5c/70/5c7013f06cc78243bed6e606c75f552ed2e2f463bd7b90f611551c5503072de5)
- December 1, 2010: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/6d/eb/6deb10fcace779add42e1ba2ac87ce2bd7e6b2594e48113cef334974b9bea090)
- August 31, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/78/e5/78e558dee1c63545ba24dcbdc1e8f932495f1860fdd5bbd58e98975780feba47)

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