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Aircraft performance

STC SA02267LA

FAA DRS lists SA02267LA as Current · Reissued, held by IKHANA Group Inc., for Viking Air DHC-6-300 and Viking Air DHC-6-400. Recorded change: Approves the Viking Air Limited DHC-6-300 and DHC-6-400 landplanes to take off and land at a maximum weight of 14,000 pounds and DHC-6-300 and DHC-6-400 floatplanes to take off and land at a maximum weight of 13,600 pounds. Snapshot dated June 30, 2026.

FAA-listed holder
IKHANA Group Inc.
Aircraft configurations
2
FAA revision date
FAA status
Current · Reissued

Recorded modification

What the FAA record covers

Approves the Viking Air Limited DHC-6-300 and DHC-6-400 landplanes to take off and land at a maximum weight of 14,000 pounds and DHC-6-300 and DHC-6-400 floatplanes to take off and land at a maximum weight of 13,600 pounds.

SA02267LA 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: Viking Air DHC-6-300 and Viking Air DHC-6-400. Confirm the approved model list, serial effectivity, configuration, and certificate revision.

Viking Air DHC-6-300A9EAViking Air DHC-6-400A9EA

Buyer checks

Confirm before sourcing

  1. 01Does it cover the exact Viking Air DHC-6-300 and Viking Air DHC-6-400 model, serial range, and configuration?
  2. 02Which limits, loading assumptions, performance data, and supplements 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 aircraft performance STCs

ST00779LAAircraft performance

Installation of side vertical restraints in accordance with approved Master Drawing List SIE 37-703, Revision A, dated May 25, 1999, or later FAA approved revisions. Structural Integrity Engineering FAA Approved Airplane Flight Manual Supplement, SIE 37-607 dated May 26, 1999, or later FAA approved revisions and Weight and Balance Supplement, SIE 37-608, dated February 9, 1999, or later FAA approved revisions, are required as part of this modification.

FAA holder: Structural Integrity Engineering

View record