# STC SA02642LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: IKHANA Group Inc.
- Description: Installation of Pratt & Whitney Canada PT6A-27 engines rated at 620 SHP, Hartzell HC-B3TN-3D(Y)/T10282H(B)+0  propellers, and associated modifications
- Status date: September 11, 2020
- Data sheets: A9EA, A9EA
- Certificate PDF: https://openairdocs.org/files/sha256/41/da/41da9de09df988c627d82aeee759156ab011f244862062027df0576a8052dc1b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FEA4FB9CEAC74071862586EE005DAA58.0001
- Page: https://openairdocs.org/stc/SA02642LA

## ADs that name it

None.

## Approved models (2)

- Viking Air Limited DHC-6-100 (TCDS A9EA)
- Viking Air Limited DHC-6-200 (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.

SA02642LA IKHANA Group, LLC.

37260 Sky Canyon Drive, Hanger 20 Murrieta, California 92563 23 the Federal Aviation Regulation A9EA Viking Air Limited DHC-6-100 and DHC-6-200 Installation of Pratt & Whitney Canada PT6A-27 engines rated at 620 SHP, Hartzell HC-B3TN-3D (Y)/T10282H(B)+0 propellers, and associated modifications in accordance with KHANA Aircraft Services Drawing List ER218-2027, Revision B, dated May 30, 2017, or later FAA approved revision. Maintain and operate the airplane according to IKHANA Aircraft Services Master Data List ER218-2016, Revision NC, dated June 21, 2017, or later FAA approved revision.

(See Continuation Sheet Page 3 of 3Pages) September 27, 2016 September 11, 2020 June 29, 2017 Manager, Technical & Administrative Support Section Los Angeles ACO Branch 3

SA02642LA 3

SA02642LA The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

1) Installation of this STC does not allow increase in Max Gross Weight.

Notes: a) This modification has been substantiated to be a non-acoustic change per 14 CFR part 21.93 (b).

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

## Every issue (2)

- September 11, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/41/da/41da9de09df988c627d82aeee759156ab011f244862062027df0576a8052dc1b)
- June 29, 2017: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/1b/cd/1bcd665296e569118a6d94ee366d35138e8caa2208a40e01e0673d766e5dbdaf)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.