STC ST00299BO

United States of America Department of Transportation Federal Aviation Administration $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&¶VVXSSRUWLQJGRFXPHQWDWLRQ GUDZLQJVLQVWUXFWLRQV SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  683(56('(635(9,286(',7,21 3DJHRIBBB Supplemental Type Certificate Number:

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ST00299BO Learjet, Inc.

One Learjet Way Wichita, KS 67209 25 the Federal Aviation Regulations T00003NY Bombardier, Inc.

BD-700-1A10, BD-700-1A11 Installation of a Honeywell DU-875 or DU-875AF Liquid Crystal Display (LCD) based Display System including two Cursor Control Devices (CCDs) in accordance with Learjet, Inc. Master Document List (MDL), Document Number BAS67010045, Revision F, dated November 02, 2017, or later FAA approved revision. See Limitations and Conditions 1.

(continued on Page 3 of 4) November 12, 2009 November 02, 2011;

September 08, 2014; June 07, 2018 March 18, 2010 September 23, 2011; July 17, 2014;

November 03, 2017; May 17, 2019;

September 15, 2020 Keith Johnston ODA administrator ODA-501508-CE Learjet Inc.

Wichita, Kansas 4 Original signed by Keith Johnston

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate $Q\DOWHUDWLRQRIWKLVFHUWLILFDWHLVSXQLVKDEOHE\DILQHRIQRWH[FHHGLQJRULPSULVRQPHQWQRWH[FHHGLQJ\HDUVRUERWK7KLVFHUWLILFDWHPD\EHWUDQVIHUUHGRUPDGH DYDLODEOHWRWKLUGSHUVRQVE\OLFHQVLQJDJUHHPHQWVLQDFFRUGDQFHZLWK&)53RVVHVVLRQRIWKLV6XSSOHPHQWDO7\SH&HUWLILFDWH 67& GRFXPHQWE\SHUVRQVRWKHUWKDQ WKH67&KROGHUGRHVQRWFRQVWLWXWHULJKWVWRWKHGHVLJQGDWDQRUWRDOWHUDQDLUFUDIWDLUFUDIWHQJLQHRUSURSHOOHU7KH67&’s supporting documentation (drawings, instructions, SURSHOOHUPXVWSURYLGHWKDWSHUVRQZLWKZULWWHQSHUPLVVLRQDFFHSWDEOHWRWKH)$$ 5HI&)5  )$$)RUP  683(56('(635(9,286(',7,21 3DJHRIBBB

Date oI transfer:

ST00299BO 4

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1. Applicable LCDs for each configurations are identified in MDL Document Number BAS67040028, Revision Y, FAA approved on September 15, 2020, or later FAA approved revision.

2. Operation must be in accordance with Learjet, Inc. Aircraft Flight Manual Supplement (AFMS) as follows:

MDL -1 Configuration: Document Number BAS67040028, Revision B, FAA approved on May 22, 2012.

MDL -2 Configuration: Document Number BAS67040028, Revision D, FAA approved on July 17, 2014, or later FAA approved revision.

MDL -3 Configuration with P/N K9321062A11 only with Rev 00 and/or Rev 01:

Document Number BAS67047021, Revision NC, FAA approved on October 31, 2017, or later FAA approved revision.

MDL -3 Configuration with P/N K9321062A11:

Document Number BAS67045008, Revision NC, FAA approved on May 17, 2019, or later FAA approved revision.

The AFMS must be carried in the aircraft during all flights.

3. Maintenance must be in accordance with Learjet, Inc. Instructions for Continued Airworthiness (ICA) as follows:

MDL -1 Configuration: Document Number BAS67010045-ICA-1, Revision B, dated August 03, 2011, or later FAA accepted revision.

MDL -2 Configuration: Document Number BAS67010045-ICA-2, Revision NC, dated October 21, 2013, or later FAA accepted revision.

MDL -3 Configuration with P/N K9321062A11 only with Rev 00 and/or Rev 01:

Document Number BAS67010045-ICA-3, Revision A, dated September 21. 2017, or later FAA accepted revision.

MDL -3 Configuration with P/N K9321062A11:

Document Number BAS67010045-ICA-3, Revision B, dated February 27, 2019, or later FAA accepted revision.

The ICA must be made available to the operator at the time of installation.

(continued on Page 4 of 4)

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4. MFD Video functionality (fixed video image) has not been certified/is not approved by this STC.

5. Compatibility of this design with previously approved modifications must be determined by the installer.

Certification Basis:

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the Bombardier, Inc. BD-700- 1A10 and BD-700-1A11 aircraft is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown on TCDS T00003NY.

b. The modification certification basis for parts changed or affected by the change since the reference application date, November 12, 2009, is based upon part 25 as amended by Amendment 25-122 as follows (MDL -1 Configuration, MDL -2 Configuration, MDL -3 Configuration):

Regulations at the latest amendment 25-0 through 25-122

25.1, 25.29, 25.301 - 25.307, 25.341, 25.561, 25.601 - 25.605, 25.609, 25.619, 25.625,

25.672, 25.699, 25.703, 25.729, 25.771, 25.777, 25.841, 25.1303, 25.1316, 25.1317, 25.1321,

25.1322, 25.1326, 25.1331, 25.1333, 25.1337, 25.1351, 25.1381, 25.1441, 25.1501, 25.1529,

25.1545, 25.1549, 25.1551, 25.1555, 25.1581 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS T00003NY

25.207, 25.613, 25.677, 25.773, 25.783, 25.869, 25.1141, 25.1301, 25.1305, 25.1309,

25.1323, 25.1329, 25.1335, 25.1353, 25.1431

c. The modification certification basis, beyond paragraph b., for parts changed or affected by the change since the amendment application date, December 05, 2016, is based upon part 25 as amended by Amendment 25-143 as follows (MDL -3 Configuration only):

Regulations at the latest amendment 25-0 through 25-143

25.1302 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS T00003NY

25.1357(a)(c) ------------------------------------------------------------END------------------------------------------------------- ST00299BO