STC SR00283SE
FAA DRS lists SR00283SE as Current · Reissued, held by Croman Corporation, for Sikorsky Aircraft S-61L and Sikorsky Aircraft S-61N. Recorded change: Removal of a 50 inch section from the forward fuselage between stations 110 and 160 and reinstallation of forward cabin with associated fabricated parts. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Removal of a 50 inch section from the forward fuselage between stations 110 and 160 and reinstallation of forward cabin with associated fabricated parts.
SR00283SE 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: Sikorsky Aircraft S-61L and Sikorsky Aircraft S-61N. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Sikorsky Aircraft S-61L and Sikorsky Aircraft S-61N model, serial range, and configuration?
- 02Which layout, materials, flammability evidence, and weight changes apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related cabin and interiors STCs
Modifies the aircraft to install new seats and new entertainment system in all classes. Installs new in-seat power outlets in first and business class. The modification changes the passenger capacity to 10F/49B/216Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00565, dated January 19, 2000, or later FAA approved revisions.
FAA holder: United Airlines Inc
The modification will remove one row (six seat places) of B/E Aerospace TSO C-39b seats in the forward area of economy class on our B737-200 series aircraft. When removed, the forward five rows of economy seats aft of the class divider will be relocated, increasing the seat pitch from 31 to 35 inches. The final seat configuration count will be 8F/95Y. The installation is in accordance with DAS-1-WE Approved United Air Lines Master Document List No. 00566 dated January 30, 2000, or later FAA approved revisions.
FAA holder: United Airlines Inc