STC SA8191NM-D

Supplemental type certificate · Learjet Inc.

Holder
Learjet Inc. · United States
Status
Current · Reissued
Status date
December 23, 2015
Applied
February 8, 2001
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA21EA

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of a Safe Flight Enhanced Autopower 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(10-68) SA8191NM-D

A21EA

Installation of a Safe Flight Enhanced Autopower System in accordance with FAA approved Master Document List DC22305001, revision C, dated August 07, 2001, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement, C1122 revision (-), dated August 8, 2001, or later FAA approved revision, and FAA accepted Instructions for Continued Airworthiness, TE-22305001-IFCA, revision C, or later FAA accepted revision, are required for the -1 configuration. FAA approved Airplane Flight Manual Supplement, C1122 revision A, dated December 5, 2003, or later FAA approved revision, and FAA accepted Instructions for Continued Airworthiness, TE-22305001-IFCA-2, revision B, or later FAA accepted revision, are required for the -2 configuration. FAA approved Airplane Flight Manual Supplement, BAS63040125 revision NC, dated April 26, 2007 or later FAA approved revision, and FAA accepted Instructions for Continued Airworthiness, TE-22305001-IFCA-3, revision A, or later FAA accepted revision, are required for the -3 configuration.

1.This approval should not be extended to 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, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

2. 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.

3. A copy of this certificate must be maintained as part of the permanent record for the modified aircraft.

4. The -3 Configuration requires a previous or concurrent installation of STC SA8191NM-D, -1 or -2 Configuration.

Learjet Inc.

One Learjet Way Wichita, Kansas 67209 Canadair / Bombardier, Inc.

CL-600-2B16 : February 8, 2001 : August 8, 2001

: November 17, 2005; October 16, 2006; December 23, 2015

: April 26, 2007; June 25, 2014

Original signed by Keith Johnston

(Signature) Keith Johnston ODA administrator ODA-501508-CE, Learjet Inc.

Wichita, Kansas (Title)

Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee)

(Address of transferee)

(Number and street)

(City, State, and Zip code) from (Name of grantor) (Print or type)

(Address of grantor)

(Number and street)

(City, State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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 · 3

MakeModelData sheet
Bombardier Inc.CL-600-2B16 (CL-601-3A)A21EA
Bombardier Inc.CL-600-2B16 (CL-601-3R)A21EA
Bombardier Inc.CL-600-2B16 (CL-604)A21EA

Every issue · 4

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

DateStatusFiles
December 23, 2015Reissued, currentCertificate
June 2, 2014Amended, earlier issueCertificate
October 16, 2006Reissued, earlier issueCertificate
November 17, 2005Reissued, earlier issueCertificate