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Engine and powerplant

STC SA02717AT

FAA DRS lists SA02717AT as Current · Issued, held by AvPower, for Cessna Aircraft TR182. Recorded change: Conversion of Cessna Model TR182 to Model R182 by removal of Cessna installed turbocharger and related systems, and replacement of engine model Lycoming O-540-L3C5D with O-540-J3C5D. Conversion in accordance with AvPower Master Parts List AP1010-4 dated June 4, 2003 or later FAA approved revision. This is a one time STC valid for Cessna Aircraft Model TR182 Serial Number R18201980 only. Snapshot dated June 30, 2026.

FAA-listed holder
AvPower
Aircraft configurations
1
FAA revision date
FAA status
Current · Issued

Recorded modification

What the FAA record covers

Conversion of Cessna Model TR182 to Model R182 by removal of Cessna installed turbocharger and related systems, and replacement of engine model Lycoming O-540-L3C5D with O-540-J3C5D. Conversion in accordance with AvPower Master Parts List AP1010-4 dated June 4, 2003 or later FAA approved revision. This is a one time STC valid for Cessna Aircraft Model TR182 Serial Number R18201980 only.

SA02717AT 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: Cessna Aircraft TR182. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Cessna Aircraft TR1823A13

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Cessna Aircraft TR182 model, serial range, and configuration?
  2. 02Which powerplant configuration, limits, instruments, and maintenance data apply?
  3. 03Who can legally supply the design data, kit, instructions, and ICAs?
  4. 04What parts, labor, conformity, and return-to-service work are excluded?

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.

View record