STC SA3251NM
FAA DRS lists SA3251NM as Current · Issued, held by AvComp LLC, for Boeing Airplane Wichita Division IB75A, Boeing Airplane Wichita Division E75N1, and Boeing Airplane Wichita Division B75N1 (Navy N2S-3), and 7 more aircraft configurations. Recorded change: Installation of Speed Ring engine cowling. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of Speed Ring engine cowling.
SA3251NM 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: Boeing Airplane Wichita Division IB75A, Boeing Airplane Wichita Division E75N1, and Boeing Airplane Wichita Division B75N1 (Navy N2S-3), and 7 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Boeing Airplane Wichita Division IB75A and Boeing Airplane Wichita Division E75N1, and 8 more aircraft configurations model, serial range, and configuration?
- 02Which powerplant configuration, limits, instruments, and maintenance data apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related engine and powerplant STCs
Installation of modified Pratt & Whitney R-1340 engine. This mod must be done concurrently with STC SE01200LA which modifies R-1340 engine.
FAA holder: Aircraft Cylinder & Turbine Inc.
Change Aeronca Model 7AC powerplant from Teledyne Continental Motors (TCM) model C65-8 to TCM model C85-12 or C85-12F or change Aeronca model 7BCM from TCM model C85-8 series engine to the C85-12 or C85-12F in accordance with Star Aircraft Company Instruction S.A. 301 and Report No. 300R. Either modification can use the Sensenich model 72GK propeller with pitch settings from 44 through 50 inches. The Notes Section of Type Certificate Data Sheet, P-170, has information concerning required plates, flange adapters, etc.
FAA holder: Lasher Charles David
Installation of air intake louvers on the rear engine lower cowl in accordance with Aviation Enterprises Installation Instructions, dated June 15, 2003, or later FAA approved revision.
FAA holder: Aviation Enterprises