STC ST00203BO

Number ST00203BO This certificate issued to:

Learjet Incorporated 85-173 Bradley International Airport Windsor Locks, CT 06096 Part 25 of the Federal; Aviation Regulations.

Original Product - Type Certificate Number: T00003NY Make: Bombardier, Inc.

Model: BD-700-1A10, BD-700-1A11

Installation of Honeywell MK V EGPWS Software Upgrade and/or optional Runway Awareness and Advisory System (RAAS) in accordance with Bombardier Aerospace Business Aviation Services Master Document List (MDL) BAS67017015, Revision G, dated May 9, 2016, or later FAA approved revision.

1. Each approved configuration listed in the MDL is contingent on a previously approved installation of a Honeywell MK V EGPWS with software version and installation requirements as specified in the notes on the MDL.

(continued on Page 3 of 4)

Date of Application: April 28, 2004 Date reissued:

Date of Issuance: August 10, 2004 Date amended: May 13, 2005; May 9, 2007;

June 20, 2016

Signature Raymond Reinhardt

Acting Manager, Boston Aircraft Certification Office Title

FAA Form 8110-2 (5/14) Page 1 of 4

To (Name and address of transferee) Name:

Address (Number and Street, City, State, and ZIP Code):

From (Name and address of grantor) Name:

Address (Number and Street, City, State, and ZIP Code):

FAA Form 8110-2 (5/14) Page 2 of 4

Number ST00203BO June 20, 2016

Limitations and Conditions: (continued from Page 1 of 4)

2. Operation must be in accordance with Bombardier Aircraft Flight Manual Supplement (AFMS), appropriate to the configuration as indicated below, and must be carried in the aircraft during all flights. An AFMS is not needed for configurations not listed.

a. Document BAS67047012, at Revision B only, for the -2 configuration.

b. Document BAS67047012, Revision C, or later FAA approved revision for configurations -7 and -8.

3. Maintenance must be in accordance with Bombardier Instructions for Continued Airworthiness (ICA), appropriate to the configuration as indicated below, and must be made available to the operator at the time of the installation. An ICA is not needed for configurations not listed.

a. Document BAS67017015-IFCA-2, Revision NC, dated 2/1/07, or later FAA accepted revision for configuration -2.

b. Document BAS67017015-IFCA-4, Revision C, dated 4/25/16, or later FAA accepted revision for configuration -4.

c. Document BAS67017015-ICA-5, Revision A, dated 4/25/16, or later FAA accepted revision for configuration -5.

d. Document BAS67017015-ICA-6, Revision B, dated 4/25/16, or later FAA accepted revision for configuration -6.

e. Document BAS67017015-ICA-7, Revision B, dated 4/25/16, or later FAA accepted revision for configuration -7.

f. Document BAS67017015-ICA-8, Revision B, dated 4/25/16, or later FAA accepted revision for configuration -8.

4. 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, BD-700-1A11 aircraft is as follows:

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FAA Form 8110-2 (5/14) Page 3 of 4

Number ST00203BO June 20, 2016 Certification Basis: (continued from Page 3 of 4)

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 amendment application date, September 12, 2011, is based upon part 25 as amended by Amendment 25-134 as follows:

Regulations at the latest amendment 25-0 through 25-134 None Regulations at an intermediate amendment None Regulations at the amendment level in TCDS T00003NY

25.1, 25.1301, 25.1309(a), 25.1322(b)(c)(d), 25.1353(a)(d)(2), 25.1381(a)(1), 25.1431(a)(c),

25.1529, 25.1581(a)(2)(b)(d) ------------------------------------------------------------END-------------------------------------------------------

FAA Form 8110-2 (5/14) Page 4 of 4