STC SA00900AT
FAA DRS lists SA00900AT as Current · Reissued, held by Erik van Veenen, for Maule Aerospace Technology M-7-235, Maule Aerospace Technology M-7-235A, and Maule Aerospace Technology M-7-420A. Recorded change: Increase in aircraft gross weight to 3,265 pounds. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Increase in aircraft gross weight to 3,265 pounds.
SA00900AT 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: Maule Aerospace Technology M-7-235, Maule Aerospace Technology M-7-235A, and Maule Aerospace Technology M-7-420A. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Maule Aerospace Technology M-7-235 and Maule Aerospace Technology M-7-235A, and 1 more aircraft configuration model, serial range, and configuration?
- 02Which limits, loading assumptions, performance data, and supplements apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related aircraft performance STCs
Increase in take-off Gross Weight to10,200 pounds and landing weight to9800 pounds. Extension of Aft. C.G. limits to +120.5 at 10,200 pounds.
FAA holder: Staggerwing Museum Foundation Inc.
Increase in take-off weight to9800 pounds, and increase in landing weight to 9400 pounds, when P&W R-985-AN14B, or -AN4, -AN10 (modified per P&W Special Instruction No. 15F-45), or-AN1M1 (with NAR-9N-19 carburetor) modified per P&W Special Inst. No 15F-45 is installed.
FAA holder: Staggerwing Museum Foundation Inc.
Increase in take-off weight to 9800 pounds, and increase in landing weight to 9400 pounds, when P&W R-985-AN14B;-AN4 (modified per P&W Special Instruction No. 15F-45) or -AN10 (modified per P&W Special Instruction No. 15F-45) or -AN-1M1(with the Stromberg NAR-9B-19 carburetor with 2-3/4 inch venturi) is installed.
FAA holder: Staggerwing Museum Foundation Inc.
Increase in takeoff weight to10,200 lbs. and landing weight to9,800 lbs. and extension of aft C.G. limit to (+120.5) at 10,200 lbs. (Model may also be designated as Conrad 10,200.).
FAA holder: Staggerwing Museum Foundation Inc.