STC SA6030NM

FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA6030NM This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: Cessna Citation A22CE Model: 560 Description of Type Design Change:

Installation of Honeywell/Racal Aeronautical Satellite Communications (SATCOM) MCS-3000/MCS-6000 systems in accordance with FAA Approved Honeywell Master Data List, Specification No. ML4077689, Revision B, or later FAA approved revision of this specification.

FAA approved Honeywell. Airplane Flight Manual Supplement, Specification No. 1050-0766, Revision N/C, or later FAA approved revision is required for this modification.

1) 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.

2) The High Gain Antenna (HPA) ins tallation shall be periodically inspected in accordance with the high gain antenna inspection requirements listed in Honeywell Specification No. 1050-0772, Revision A or later FAA approved revision.

3) The approval of this change in ty pe in type design applies only to Cessna Model 560 airplanes. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effects upon the airworthiness of the aircraft.

Date of Application: September 25, 1992 Date Reissued: January 20, 2009, March 9, 2020 Date of Issuance: June 2, 1993 Date Amended: November 14, 1997 By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA6030NM

FAA Form 8110-2 (5/14) Page 3 of 3 Limitations and Conditions: (continued) Note 1: Maximum Weight S/N 560-0001 through -0259 S/N 560-0260 and on Takeoff 15,620 lb. 16,020 lb.

Landing 15,200 lb. 15,200 lb.

Note 2: Noise Characteristics This modification was determined not to increase the noise level and was not considered an “acoustical change” as defined in

21.93(b), Amendment 21-73 of the Federal Aviation Regulations.

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