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Engine and powerplant

STC SA11854CH

FAA DRS lists SA11854CH as Current · Issued, held by Dakota Cub Aircraft Inc., for FS 2003 Corp PA-12, FS 2003 Corp PA-12S, and FS 2002 Corp PA-14, and 34 more aircraft configurations. Recorded change: Installation of modified exhaust system in lieu of original components. Snapshot dated June 30, 2026.

FAA-listed holder
Dakota Cub Aircraft Inc.
Aircraft configurations
37
FAA revision date
FAA status
Current · Issued

Recorded modification

What the FAA record covers

SA11854CH 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: FS 2003 Corp PA-12, FS 2003 Corp PA-12S, and FS 2002 Corp PA-14, and 34 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

FS 2003 Corp PA-12A-780FS 2003 Corp PA-12SA-780FS 2002 Corp PA-14A-797Piper Aircraft PA-161A1Piper Aircraft PA-16S1A1Piper Aircraft PA-181A2Piper Aircraft PA-18S1A2Piper Aircraft PA-18-105 (Special)1A2Piper Aircraft PA-18S-105 (Special)1A2Piper Aircraft PA-18A1A2Piper Aircraft PA-18-125 (Army L-21A)1A2Piper Aircraft PA-18S-1251A2Piper Aircraft PA-18AS-1251A2Piper Aircraft PA-18-1351A2Piper Aircraft PA-18A-1351A2Piper Aircraft PA-18S-1351A2Piper Aircraft PA-18AS-1351A2Piper Aircraft PA-18-1501A2Piper Aircraft PA-18A-1501A2Piper Aircraft PA-18S-1501A2Piper Aircraft PA-18AS-1501A2Piper Aircraft PA-19 (Army L-18C)1A2Piper Aircraft PA-19S1A2Piper Aircraft PA-201A4Piper Aircraft PA-20-1151A4Piper Aircraft PA-20-1351A4Piper Aircraft PA-20S1A4Piper Aircraft PA-20S-1151A4Piper Aircraft PA-20S-1351A4Piper Aircraft PA-221A6Piper Aircraft PA-22-1081A6Piper Aircraft PA-22-1351A6Piper Aircraft PA-22S-1351A6Piper Aircraft PA-22-1501A6Piper Aircraft PA-22S-1501A6Piper Aircraft PA-22-1601A6Piper Aircraft PA-22S-1601A6

Buyer checks

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Related engine and powerplant STCs

SA493CHEngine and powerplant

Increase in maximum gross weight from 3600 lbs. to 3700 lbs. with installation of Continental I0-550-B engine in accordance with D'Shannon Products Installation Instruction 71-20-00, dated 10/20/88, or later FAA-approved revision; and installation of Cooling Air Baffles in accordance with D'Shannon Products Installation Instruction DSP1M95-2, dated 6/1/95, FAA-approved 6/21/95 or later FAA Approved revisions.

FAA holder: D'Shannon Products Ltd.

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