STC SA03359NY

Number SA03359NY

FAA Form 8110-2 (7/19) Page 1 of 6 This certificate issued to:

Innovative Solutions & Support, Inc.

1500 District Avenue Burlington, MA 01803 Part 23 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A00002AC Make: Eclipse Aerospace Model: EA500 Description of Type Design Change:

Installation of Supplemental Type Certificate (STC) Configuration 1 or of STC Configuration 2:

STC Configuration 1: Innovative S olutions & Support, Inc. (IS&S) Autothrottles, Standby Display Unit and Flight Management System updates; see Limitations and Conditions 1.

STC Configuration 2: Expand the S peed Hold (SPD HOLD) Mode capability of STC Configuration 1 Autothrottles (during approach SPD HOLD no longer disabled with gear down or flaps landing) and add a Synthetic Vision System; see Limitations and Conditions 2.

(continued on Page 3 of 6)

Date of Application: April 15, 2011 Date reissued:

Date of Issuance: December 26, 2013 Date amended: January 22, 2 014;

August 03, 2020

Signature Kevin Dickert Manager, Boston ACO Branch Title

FAA Form 8110-2 (7/19) Page 2 of 6

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):

(Continuation Sheet) Number SA03359NY

FAA Form 8110-2 (7/19) Page 3 of 6 Limitations and Conditions: (continued from Page 1 of 6)

1. STC Configuration 1, installed in accordance with IS&S Master Data List (MDL) 1D-08905, Revision 6, dated January 16, 2014, or later FAA approved revision, prerequisites are as follows:

a. Installation of Flight Management System (FMS) in accordance with STC SA02946NY, issued on March 28, 2011, is a prerequisite to this modification.

b. Installation of NG 2.5 Provisions in accordance with Eclipse MB 500-31-003, issued on October 11, 2013, is a prerequisite to this modification.

c. Installation of Engine PW610F-A-FADEC Software version 0406 is a prerequisite to this modification.

d. Installation of Aircraft Computer System (ACS) Software Update to 5.5.06 in accordance with Eclipse MB 500-31-004, issued on September 20, 2013, is a prerequisite to this modification.

e. Installation of Byteflight Input/Output (BIO) Software Update to 6.0 in accordance with Eclipse SB 500-31-005, issued on September 20, 2013, is a prerequisite to this modification.

2. STC Configuration 2, installed in accordance with IS&S Master Data List (MDL) 1D-13947, Revision 1, dated July 22, 2020, or later FAA approved revision, prerequisites are as follows:

a. Installation of STC Configuration 1 is a prerequisite to this modification.

b. All Original Product models must be equipped as follows:

equipment 9K-07048-5 FPDS FMS FADEC ACS Byteflight Databus GPS PFD MFD hardware part number 9D-84098-3 9D-84100-3 9K-07048-5 FPDS PW610F-A 2536-6 none 9B-87010-7 software part number 7H-09938-25 7H-09939-21 7H-09938-25 0406 5.6.041 or 5.7.022 6.0 7H-10065-03 installed by Eclipse Aerospace MB 500-31- 021, Rev C MB 500-31- 021, Rev C MB 500-31- 021, Rev C MB 500- 76-001, Rev B 1MB 500-31- 012, Rev A;

2MB 500-31- 017, Rev B MB 500- 31-005, Rev B MB 500-31- 007, Rev J (continued on Page 4 of 6)

(Continuation Sheet) Number SA03359NY

FAA Form 8110-2 (7/19) Page 4 of 6 Limitations and Conditions: (continued from Page 3 of 6)

3. Operation must be in accordance with Innovative Solutions & Support Aircraft Flight Manual Supplement (AFMS):

STC Configuration 1: AFMS Document 1D-08291, Revision 6, FAA approved on December 26, 2013, or later FAA approved revision.

STC Configuration 2: AFMS Document 1D-13957, Revision IR, FAA approved on July 30, 2020, or later FAA approved revision.

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

4. Maintenance must be in accordance with Innovative Solutions & Support Instructions for Continued Airworthiness (ICA):

STC Configuration 1: ICA Document 1D-10186, Revision 5, dated December 18, 2013, or later FAA accepted revision.

STC Configuration 2: ICA Document 1D-13956, Revision 2, dated July 15, 2020, or later FAA accepted revision.

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

5. Compatibility of this design with previously approved modifications must be determined by the installer (refer to FAA Advisory Circular 20-188).

Certification Basis:

(continued on Page 5 of 6)

(Continuation Sheet) Number SA03359NY

FAA Form 8110-2 (7/19) Page 5 of 6 Certification Basis: (continued from Page 4 of 6) Certification Basis STC Configuration 1:

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 Eclipse Aerospace EA500 aircraft is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A00002AC.

b. The modification certification basis for parts changed or affected by the change since the reference application date, April 15, 2011, is based upon part 23 as amended by Amendment 23-62 as follows:

Regulations at the latest amendment 23-0 through 23-62

23.777, 23.1301, 23.1303, 23.1306, 23.1308, 23.1309, 23.1310, 23.1311, 23.1323, 23.1331,

23.1431, 23.1545, 23.1555, 23.1585, 23.1587 Regulations at an intermediate amendment level None Regulations at the amendment level in TCDS A00002AC None Special Condition 23-13-01-SC, Autothrottle Functions (continued on Page 6 of 6)

(Continuation Sheet) Number SA03359NY

FAA Form 8110-2 (7/19) Page 6 of 6 Certification Basis: (continued from Page 5 of 6) Certification Basis STC Configuration 2:

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 Eclipse Aerospace EA500 aircraft is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A00002AC.

b. The modification certification basis for parts changed or affected by the change since the amendment application date, March 05, 2020, corresponding to the reference amendment date August 03, 2020, is based upon part 23 as amended by Amendment 23-64 as follows:

Regulations at the latest amendment 23-0 through 23-64

23.1529, 23.2000, 23.2010, 23.2135(a)(2), 23.2150, 23.2250, 23.2405, 23.2500, 23.2505,

23.2510, 23.2600(a)(b), 23.2605, 23.2610, 23.2615, 23.2620(a)(1)(2)(5) Regulations at an intermediate amendment level None Regulations at the amendment level in TCDS A00002AC None Special Condition 23-13-01-SC, Autothrottle Functions ------------------------------------------------------------END-------------------------------------------------------