STC ST00381SE

Supplemental type certificate · Honeywell International Inc

Holder
Honeywell International Inc · United States
Status
Current · Reissued
Status date
December 21, 2021
Applied
September 30, 1996
Product
Aircraft · Large Airplane
Certification basis
Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 21, Part 25, Part 121
Data sheet
TCDSA2NM

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of enhanced ground proximity warning system

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

ST00381SE Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 25 the Federal Aviation Regulations A2NM Boeing 757-200 series Installation of the Enhanced Ground Proximity Warning System as defined in Master Drawing 960-2227-003, Revision V, dated December 5, 2000, or later FAA-approved revisions.

Approval of this change in type design applies to the above model aircraft equipped with either a flight management system (FMS), which meets AC90-45A, or an EGPWS with a global positioning system (GPS) based navigation system or an EGPWS equipped with an internal GPS and a GPS antenna as defined in the above Master Drawing. U.S. registered aircraft that operate under FAR part 121 may not incorporate the Honeywell "alternate" glideslope cancel feature and any aircraft imported into the U.S with the intent to operate under FAR part 121 must remove this feature prior to operation. This approval should not be extended to other aircraft 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 the aircraft. A copy of this Certificate and FAA Approved Airplane Flight Manual Supplement must be maintained as part of the permanent records for the modified aircraft. A system self-test shall be performed per the production ground test procedures as specified in the applicable Installation number of the above Master Drawing. The self-test intervals shall be performed at intervals not to exceed 4500 flight hours, or 18 months, whichever comes first.

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.

September 30, 1996 December 21, 2021 November 5, 1996 5/30/1997; 9/6/2000; 1/18/2001 For Acting Manager, Seattle ACO Branch 2

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

ST00381SE 2

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
The Boeing Company757-200A2NM

Every issue · 3

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
December 21, 2021Reissued, currentCertificate
December 21, 2021Reissued, earlier issueCertificate
January 18, 2001Amended, earlier issueCertificate