STC SB04179CH
FAA DRS lists SB04179CH as Current · Issued, held by Ending, John, for Balony Kubicek spol sro BB26E. Recorded change: Replace the Balony Kubicek Basket/Burner system and fuel tanks with the FireFly (Balloon Works) Basket Model 4.9 A1, S/N 295; the FireFly (Balloon Works) Burner Model F1 Mirage, S/N 117; and FireFly (Balloon Works) fuel tanks, Model No. 3229 (S/N 65339J) and 3035 (S/Ns 64810J, 64793J, 45883J, and 65361J). Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Replace the Balony Kubicek Basket/Burner system and fuel tanks with the FireFly (Balloon Works) Basket Model 4.9 A1, S/N 295; the FireFly (Balloon Works) Burner Model F1 Mirage, S/N 117; and FireFly (Balloon Works) fuel tanks, Model No. 3229 (S/N 65339J) and 3035 (S/Ns 64810J, 64793J, 45883J, and 65361J).
SB04179CH 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: Balony Kubicek spol sro BB26E. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Balony Kubicek spol sro BB26E model, serial range, and configuration?
- 02Which tanks, plumbing, usable-fuel assumptions, and inspections apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related fuel systems STCs
Installation of P/N GL204-501, lower center fuel tank bladder cells, as a replacement for original bladder P/N 5630204-501.
FAA holder: Floats & Fuel Cells
Installation of left (right) hand forward inboard fuel tank bladder cells, P/N DF060-507 (LH) and 508(RH) as a replacement for original bladders P/N 5630060-507 (508).
FAA holder: Floats & Fuel Cells
Installation of left hand and right hand fuel cell assemblies.
FAA holder: A/C Fuel Cells Worldwide
Modification to permit an increase in maximum allowable zero fuel weight of DC-8-62 airplanes, (1) which are certified to a 335,000 lbs. maximum takeoff gross weight or (2) which are certified to a 350,000 lbs. maximum takeoff gross weight.
FAA holder: Leth & Associates