STC SA01965WI

SA01965WI Avcon Industries, Inc.

714 N. Oliver, Hangar M Newton, KS 67114 PT 23 Federal Aviation Regulations A24CE Textron Aviation (Beechcraft) 200, 200C, A200, A200C, B200, B200C, B200GT, B200CGT, 300, B300, B300C Installation of Wing Tip Hard Point Provisions. Required data:

1. FAA Approved Master Data List, No. 05601000, Rev. IR, signed 5/5/2021, or later FAA Approved revisions.

Compatability of this design change with previously approved modifications must be determined by the installer.

May 20, 2020 May 6, 2021 Grant Youngdahl Program Manager Wichita ACO Branch 5

SA01965WI 5

SA01965WI Certification Basis (continued from page 1):

In accordance with 14 CFR 21.101 and 21.115, and the procedures specified in FAA Order 8110-48 and FAA AC 21.101, the certification basis for this modification is as follows:

1. The type certification basis for areas not changed or not affected by this modification remain as specified in the applicable TCDS.

2. The certification basis for areas changed or affected by this modification since the date of application, May 20, 2020, was determined to be:

Model 200 Series (includes 200/A200/B200 series) In accordance with FAR Part 23, effective February 1, 1965, as amended by Amendments 23.1 through (Model 200 series) 23.9 and 23-11:

FAR Amdt

23.143(a) 23-14

23.145(d) 23-14

23.153 23-14

23.161(c)(3) 23-14

23.173(a) 23-14

23.175 23-14

23.1305(n) 23-26

23.1529 23-26

A200CT and B200 series only:

FAR Amdt

23.951(c) 23-15

23.997(d) 23-15

B200 Series only:

FAR Amdt

23.1325(e) 23-20

23.1545(a) 23-23

Model 200 and B200 series aircraft approved for 35,000 feet:

FAR Amdt

25.831(d) 25-41

25.929 25-41

25.1419 25-41

FAA Special Conditions 23-47-CE-5 issued October 30, 1972, Amendment 1 dated December 18, 1973, and Amendment 2 dated January 12, 1979; SFAR 27 through Amendment 27-4; and FAR Part 36 through Amendment 36-10.

SA01965WI Certification Basis (continued from page 3):

Model 300:

SFAR 41C, effective September 13, 1982, see NOTE 7 or 11:

FAR Part 23, effective February 1, 1965, through Amendment 23-9; Amendment 23-11:

FAR Amdt

23.143(a) 23-14

23.145(d) 23-14

23.153 23-14

23.161(c)(3) 23-14

23.173(a) 23-14

23.175 23-14

23.427 23-14

23.441 23-14

23.445 23-14

23.951(c) 23-15

23.967 23-26

23.997(d) 23-15

23.1305(n) 23-26

23.1529 23-26

23.1545(a) 23-23

25.929 25-0

25.1419 25-23

25.831(d) 25-41

Special Conditions No. 23-47-CE-5, including Amendments 1, 2, 3, dated November 15, 1982, and 4 dated October 17, 1986:

FAR Part 36, through Amendment 36-10, and SFAR 27, through Amendment 27-4.

Compliance with ice protection has been demonstrated in accordance with FAR 25.1419 when ice protection equipment is installed in accordance with the Equipment List.

SA01965WI Certification Basis (continued from page 4):

Model B300/B300C:

FAR Part 23, effective February 1, 1965, as amended by Amendments 23-1 through 23-34; FAR Part 36 effective December 1, 1969, as amended by Amendment 36-1 through 36-15; SFAR 27 effective February 1, 1974, as amended by Amendments 27-1 through 27-5 and Exemption No. 5077 from compliance with Section 23.207(c).

Special Conditions 23-ACE-48A effective August 13, 1990, apply to Electronic Flight Instrument System (EFIS) equipped airplanes. FAR Part 23, Sections 23.201, 23.203 and 23.205 through amendment 23-45 (S/N FN-1 & On only).

Effective January 20, 1994, FAR 23.1457 as amended by Amendment 23-35.

Exemption 5599 from compliance with FAR 23.53(c)(1), for use of ground minimum control speed (Vmcg) for determination of takeoff decision speed (V1) (Serials FL-111 and after, FM-9 and after, FN-2 and after, or prior airplanes modified by Beech Kit No. 130-3004).

Exemption 6405 from compliance with FAR 23.807(d)(1)(i) to allow a single emergency exit, in addition to the cabin door.

Compliance with ice protection has been demonstrated in accordance with FAR 23.1419 when ice protection equipment is installed in accordance with the Equipment List.

Equivalent Safety Findings: FAR 23.781(b) for shape of the propeller control knob; FAR 23.1305(g) for use of fuel low pressure warning annunciators in lieu of the fuel pressure indicators; FAR 23.1321(d) for the basic "T" instrument panel arrangement. Does Not Apply to Pro Line 21 Equipped Aircraft

NOTE FOR ALL MODELS: Additional requirements are found in FAA TCDS A24CE, Rev. 124, or later FAA approved revision, and may depend on specific serial number aircraft.

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