STC SA01969SE

United States of America Department of Transportation – Federal Aviation Administration Supplemental Type Certificate Number SA01969SE This Certificate issued to: Mid-Continent Instruments and Avionics 9400 East 34th Street North Wichita, KS 67226 Part 23 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: See attached FAA-Approved Model List (AML) issued 17 January 2014 or later FAA-approved revisions for the list Make: of approved airplane models, applicable installation data Model: requirements, and specific limitations.

Description of Type Design Change: Installation of a Mid -Continent MD302 Standby Attitude Module in accordance with Master Data List AM0261 -DL02-00, specified on the attached FAA-Approved Model List (AML) issued 17 January 2014, or later FAA -approved revision. Altered aircraft must be maintained in accordance with t he Instructions fo r Continued Airworthiness (ICA) document AM0261-IC01-00, Revision “—”, dated 11 November 2013 or later FAA-accepted revision.

Limitations and Conditions: Approval of this change in type design applies to the aircraft listed on the AML only. This approval should not be applied to an eligible aircraft model on which other previously-approved modifications are incorporated unless it is determined by the installer that the relationship between this change and the other previously -approved modifications will introduce no adverse effect upon the airworthiness of the aircraft.

(Limitations and Conditions continued on Page 3 of 3)

Date of application: March 25, 2013 Date reissued:

Date of issuance: January 17, 2014 Date amended:

(Signature) ODA Administrator (Title)

United States of America Department of Transportation – Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA01969SE

The MD302 cannot be used as a primary display. For aircraft that require the pilot to hold a type rating, the candidate aircraft must be equipped with primary flight displays that include vertical tape displays of airspeed and altitude. This AML STC is only applicable to 14 CFR part 23 Class I, II, III, and IV aircraft as defined in Advisory Circular 23.1309- 1(). 14 CFR part 25, 27, and 29 aircraft are not authorized under this STC.

For airplanes with maximum gross weights of 6000 lbs or more (AC 23.1309- 1() Class II and IV aircraft), the primary display systems must consist of at least two displays of airspeed, altitude, and attitude. If the primary display system does not include two displays of airspeed, altitude, and attitude, the installer must obtain an independent approval addressing the system safety aspects of the applicable amendment of 14 CFR 23.1309, Equipment, Systems, and Installations.

A copy of this certificate and the FAA -approved AML must be maintained as part of the permanent records for the modified aircraft.

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.

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FAA Form 8110-2.1(10-69) Page 3 of 3