# STC SA884CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc
- Description: Installation of a solar T-62T-39 auxiliary tower unit.
- Status date: December 1, 2016
- Data sheets: A3EU
- Certificate PDF: https://openairdocs.org/files/sha256/c3/7a/c37a05f40d03f634a3bd2cf845d9ddea812b326be97ddf3bd2e75a402014a34d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/24C404CA84397A078625814800502A88.0001
- Page: https://openairdocs.org/stc/SA884CE

## ADs that name it

None.

## Approved models (1)

- Raytheon Aircraft Company BH.125 Series 600A (TCDS A3EU)

## 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 (5/14) Page 1 of

Part of the

Signature

Title SA884CE Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 Civil Air Regulations.

4b Installation of a Solar T-62T-39 Auxiliary Power Unit. Data Required:

1. Drawings called out in Beech STC List No. 125-001119, Revision "H", for auxiliary power unit installation; and

2. FAA approved Airplane Flight Manual Supplement for Beechcraft Hawker BH-125-Series 600A airplanes, Beech P/N 131117 dated December 6, 1972.

Hawker Siddeley BH125-600A

(see continuation sheet 3 of 3) April 15, 1996; March 26, 2007;

December 1, 2016 August 1974; June 14, 1974;

September 25, 1974; January 5, 1976 May 19, 1972 December 6, 1972 A3EU Mark Fuller STC ODA administrator ODA-100129-CE

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of

Date of Issuance: December 6, 1972 Date Reissued: December 1, 2016

This approval should not be extended to other specific airplanes of this model 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 airplane. Parts manufactured under this STC may have been produced without an FAA approved quality control procedure. Prior to installation, such parts must be inspected for conformity and airworthiness in accordance with FARs 21 and 43. 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.

-- END -- SA884CE 3

## Every issue (2)

- December 1, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c3/7a/c37a05f40d03f634a3bd2cf845d9ddea812b326be97ddf3bd2e75a402014a34d)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/9e/3a/9e3a55aec8cc334f162d32f18f2f39a3cf715a97e1313ecffbdc764c567ba348)

---
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.