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Aircraft structures

STC SA605SW

FAA DRS lists SA605SW as Current 路 Reissued, held by Airline Fueling Inc., for Piper Aircraft PA-23-250 (Navy UO-1). Recorded change: Rear baggage door. Snapshot dated June 30, 2026.

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FAA-listed holder
Airline Fueling Inc.
Aircraft configurations
1
FAA revision date
FAA status
Current 路 Reissued

Recorded modification

What the FAA record covers

SA605SW 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: Piper Aircraft PA-23-250 (Navy UO-1). Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Piper Aircraft PA-23-250 (Navy UO-1)1A10

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SA6073NMAircraft structures

Installation of fatigue sensor and structural life extension of wing spar in accordance with FAA approved SIE Master Drawing List 91000, Revision A, dated September 23, 1993, or later FAA approved revision, and FAA approved Airplane Flight Manual Supplement Report No. SIE-12-601, Revision N/C, dated October 19, 1993 or later FAA approved Airplane Flight Manual Supplement, and Report No. SIE-12-602, Revision N/C, dated December 21, 1993, or later FAA approved Revision. (SIE-12-601 is for model C99 only, and SIE-12-602 is for the remaining models, 99, 99A, A99A, and B99.).

FAA holder: Structural Integrity Engineering

View record

FAA record reference

STC number
SA605SW
Product
Aircraft 路 Small Multi-Engine
Country
United States
Application date
February 8, 1966
Revision date
July 15, 2010
CFR references
Part 3, Part 21