STC SA5777NM

FAA DRS lists SA5777NM as Current · Reissued, held by Spoilers Inc, for Beechcraft 58, Beechcraft 58A, and Beechcraft G58, and 4 more aircraft configurations. Recorded change: Installation of Spoilers, Inc., Model SP10000 hydraulic actuated wing spoiler system. Snapshot dated June 30, 2026.

FAA-listed holder

Spoilers Inc

Aircraft configurations

FAA revision date

July 9, 2013

FAA status

Current · Reissued

Recorded modification

What the FAA record covers

SA5777NM identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.

Applicability

Aircraft named in FAA DRS

Named aircraft: Beechcraft 58, Beechcraft 58A, and Beechcraft G58, and 4 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Beechcraft 583A16 Beechcraft 58A3A16 Beechcraft G583A16 Hawker Beechcraft 58PA23CE Hawker Beechcraft 58PAA23CE Hawker Beechcraft 58TCA23CE Hawker Beechcraft 58TCAA23CE

Buyer checks

Confirm before sourcing

SR09150RCFlight controlsRevised Apr 15, 2011

Installation of Cyclic Force Trim System in accordance with Premier Aviation, Inc. MDL F00-15000, Rev C, dated December 24, 1996, or later FAA approved revision.

FAA holder: Bell Helicopter Textron Inc.

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SA09628AC-DFlight controlsRevised Mar 21, 2011

1. Installation of S-TEC 01298 or 01304 Digital Flight Control System (DFCS), in according with Master Data List 921128, Rev. 11, dated 3-16-11 or later FAA Approved revisions of the above data.

FAA holder: S-TEC Corporation

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SA02933CHFlight controlsRevised Feb 25, 2011

Installation of the Cessna 182D cowling (upper cowling P/N 0752031-27, lower cowling P/N 0752031-28) with cowl flaps and cowl flap mechanism in accordance with Tom P. O Reilly s Installation Manual, Rev. Orig., Dated 11/7/2008, FAA approved on 2/25/2011 or later FAA approved revision.

FAA holder: O'Reilly Tom Paul

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SA1421SOFlight controlsRevised Feb 10, 2011

Installation of 40:1 gear ratio wing flap transmissions and related changes in accordance with Colemill Enterprises, Inc., Installation Instructions dated February 16, 1983, or later FAA approved revision. This modification provides and equivalent means of compliance with paragraphs (a)1, (a)2, and (a)4 of AD 82-27-13 and restores the 40 (full) flap travel.

FAA holder: Mike Jones Aircraft Sales Inc.

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What the FAA record covers

Aircraft named in FAA DRS

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Related flight controls STCs

Installation of Cyclic Force Trim System in accordance with Premier Aviation, Inc. MDL F00-15000, Rev C, dated December 24, 1996, or later FAA approved revision.

1. Installation of S-TEC 01298 or 01304 Digital Flight Control System (DFCS), in according with Master Data List 921128, Rev. 11, dated 3-16-11 or later FAA Approved revisions of the above data.

Installation of the Cessna 182D cowling (upper cowling P/N 0752031-27, lower cowling P/N 0752031-28) with cowl flaps and cowl flap mechanism in accordance with Tom P. O Reilly s Installation Manual, Rev. Orig., Dated 11/7/2008, FAA approved on 2/25/2011 or later FAA approved revision.