Supplemental type certificate · FAA Aviation System Standards AVN-300

Holder
FAA Aviation System Standards AVN-300 · United States
Status
Current · Amended
Status date
June 3, 1998
Applied
October 3, 1997
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDS3A16

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of antennas and various carry-on systems.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Hnitrd &tKu of SUstrita Bepartment of ^transportation —.federal Stoation administration Supplemental "Cjipe Certificate SA2138SW-AC Aviation System Standards Flight Inspection Maintenance Division, AVN-300 6500 S. MacArthur Boulevard Oklahoma City, OK 73169 CAM 3 jJ'jAj,, Civil Aviation

• 3A16

•• Beech Aircraft Corporation '• 58 -M - — * ----- j-.-Installation of antennas on Beech Model 58 and installation of the following carry-on systems: 1. Radio Frequency Interference System, FAA Model Ho. ADFBE58; 2. Navigational Aids Signal Evaluator, Raytheon Service Co. Model ANM-400, P/N WT104TS; 3. Southwest Region FAA Model No. SW-400; 4. Airborne Technologies Model AT-921; 5. Spectrum Analyzer, Marconi Radio Test Set, Model No.

2947; and 6. Spectrum Analyzer, Hewlett-Packard RF Test Set, Model Ho. 8920A. This alteration installs communications and navigation antennas on the Model 58 for use in locating Radio Frequency Interference and for troubleshooting Navigational Aids facilities.

This alteration is to be made in accordance with FAA Data List BE-58-1, dated October 7, 1997., or later approved revisions.

-&n*£*&lfft&.-a*ujfa-ri«6&en4.. The following FAA Approved Flight Manual Supplement is required; Airplane Flight Manual Supplement for the Beech Aircraft Corporation Model 58 with HASE/RFI Provisions Installed, dated October 29, 1997, or later FAA approved revisions.

Compatibility of this alteration with previously approved alterations is to be determined by the installer.

: October 3, 1997 October 29, 1997 'Crtfr «•**««/.• 'a& „ „*,*£,/-• June 3, 1998

•" /(Signalute) DAS Coordinator ( Title)

This ceitifitatr may bf transfftred tn actGtdana with FAR 21-47.

f AA fom. a I 10-2 (10-68)

INSTRUCTIONS. The iransfcr endorsement below may be used lo notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Cmifkaie.

The FAA will reissue the rrrlificdlc in the name of list- transferee and forward It to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Cerliiicate Number to (Name of transferee) (Address of transferee) (Number anil jlrttt) (City, Klalt, and ZIP radii from (Name of grantor) (Print or type) (Address of grantor) ' and tl'til) (City, Slau. aid <JI*rodij Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

C FAA AC 69-9536

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Beechcraft Corporation583A16