# STC SA1730CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Sabreliner Aviation LLC, United States
- Description: Installation of Collins FMS-90 Flight Management System, Dual Collins DME-40 System and Second Collins 590A-301 Air Data System.
- Applied: March 19, 1982
- Status date: March 7, 2014
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A2WE](https://openairdocs.org/tcds/A2WE)
- Certificate PDF: https://openairdocs.org/files/sha256/0a/a7/0aa7216d7a6f117a983ff8d20e92a39c586e329d12c9558e2061f5861daa1c32
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F86F8F34127C3C9586257E62004DF821.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1730CE

## ADs that name it (0)

None.

## Approved models (1)

- Sabreliner Corporation NA-265-40 ([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 plus Amendments and Special Conditions listed on the Type Certificate Data Sheet SA1730CE Sabreliner Aviation, LLC 1390 Highway H Perryville, MO 63775 4b Civil Air Regulations dated December 31, 1953, 2 A2WE NA-265-40 Installation of Collins FMS-90 Flight Management System, Dual Collins DME-40 System and Second Collins 590A-301 Air Data System. Data required: (1a) Rockwell International Drawing No. 40E-098-0015, Rev. A, dated March 16, 1982, for Model NA-265-40, S/N 282-098 only; (1b) Rockwell International Drawing No. 40E-098-0015, Rev. C, dated October 4, 1982, for Model NA-265-40 series; (2a) Airplane Flight Manual Supplement, dated April 9, 1982, for Model NA-265-40, S/N 282-098 only; (2b) Airplane Flight Manual Supplement, dated May 31, 1983, for Model NA-265-40 series, or later FAA approved revisions of all documents.

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.

Rockwell International March 19, 1982 June 30, 1983; March 7, 2014 April 9, 1982 May 31, 1983 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)

SA1730CE 2

## Every issue (1)

- March 7, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0a/a7/0aa7216d7a6f117a983ff8d20e92a39c586e329d12c9558e2061f5861daa1c32)

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