# STC SA1242CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Sabreliner Aviation LLC, United States
- Description: Installation of Collins ADF-60A Automatic Direction Finding and Intercontinental Dynamics Corp. RAD/BAR with Voice Terrain Advisory Systems.
- Applied: June 28, 1976
- Status date: March 7, 2014
- Product: Aircraft, Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A2WE](https://openairdocs.org/tcds/A2WE)
- Certificate PDF: https://openairdocs.org/files/sha256/10/a3/10a32e9e53db68f85280fb6fa9ba1136c5cdd52b87578d858c6b8db4e87427d0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B3B5DF8D2DFAD55186257DD30075B269.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1242CE

## ADs that name it (0)

None.

## Approved models (1)

- Sabreliner Aviation LLC NA-265-60 ([TCDS A2WE](https://openairdocs.org/tcds/A2WE))

## 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 SA1242CE Sabreliner Aviation, LLC 1390 Highway H Perryville, MO 63775 4b Civil Air Regulations 2 A2WE NA-265-60 Installation of Collins ADF-60A Automatic Direction Finding and Intercontinental Dynamics Corp. RAD/BAR with Voice Terrain Advisory Systems. Data required: (1) FAA Approved Rockwell International Drawing No. 60S-103-0005, No Change, and (2) FAA Approved Airplane Flight Manual Supplement No. 59, or later FAA approved revisions.

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer 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. 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 FAR's 21 and 43.

Rockwell International June 28, 1976 June 30, 1983; March 7, 2014 July 2, 1976 Grant E. Youngdahl Program Manager Wichita Aircraft Certification Office

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

To (Name and address of transferee)

From (Name and address of grantor)

SA1242CE 2

## Every issue (1)

- March 7, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/10/a3/10a32e9e53db68f85280fb6fa9ba1136c5cdd52b87578d858c6b8db4e87427d0)

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