STC SA02115AK

FAA DRS lists SA02115AK as Current · Amended, held by F Atlee Dodge Aircraft Service, for New Piper Aircraft PA-18-150, New Piper Aircraft PA-18A-150, and New Piper Aircraft PA-18AS-150, and 6 more aircraft configurations. Recorded change: Fabrication and installation of 30.5 gallon wing fuel tank sight gages. Snapshot dated June 30, 2026.

FAA-listed holder

F Atlee Dodge Aircraft Service

Aircraft configurations

FAA revision date

January 20, 2004

FAA status

Current · Amended

Recorded modification

What the FAA record covers

SA02115AK 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: New Piper Aircraft PA-18-150, New Piper Aircraft PA-18A-150, and New Piper Aircraft PA-18AS-150, and 6 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

New Piper Aircraft PA-18-1501A2 New Piper Aircraft PA-18A-1501A2 New Piper Aircraft PA-18AS-1501A2 New Piper Aircraft PA-18S-1501A2 New Piper Aircraft PA-22-1501A6 New Piper Aircraft PA-22-1601A6 New Piper Aircraft PA-12A-780 New Piper Aircraft PA-12SA-780 New Piper Aircraft PA-14A-797

Buyer checks

Confirm before sourcing

SA2033NMFuel systemsRevised Dec 1, 2009

Installation of a auxiliary fuel system in the forward baggage compartment. (727-2M7).

FAA holder: Southeast Aero-Tek Inc

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ST00543ATFuel systemsRevised Dec 1, 2009

Increase in aircraft operating weights(Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45855 only).

FAA holder: Aircraft Modification Design Services

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ST00558ATFuel systemsRevised Dec 1, 2009

Increase in aircraft operating weights (Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45410 only).

FAA holder: Aircraft Modification Design Services

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ST00617ATFuel systemsRevised Dec 1, 2009

Increase in aircraft operating weights(maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs. (DC-8-51 s/n 45935 only).

FAA holder: Aircraft Modification Design Services

View record

What the FAA record covers

Aircraft named in FAA DRS

Confirm before sourcing

Related fuel systems STCs

Installation of a auxiliary fuel system in the forward baggage compartment. (727-2M7).

Increase in aircraft operating weights(Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45855 only).

Increase in aircraft operating weights (Maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs.) (DC-8-51 s/n 45410 only).

Increase in aircraft operating weights(maximum takeoff weight - 315,000 lbs., maximum landing weight - 217,000 lbs., maximum zero fuel weight - 203,000 lbs. (DC-8-51 s/n 45935 only).