STC SB03242CH
FAA DRS lists SB03242CH as Current · Issued, held by Rainbow Ryders Inc., for Lindstrand Balloons 260A. Recorded change: Replace the Lindstrand Balloons Ltd Burner system with the Cameron Balloons Triple Burner, Part Number CB2081-2, S/N B5216, B5217, B5298. Replace the Lindstrand Balloons Ltd fuel tanks with the Cameron Balloons Fuel Tanks, Part Number CBUS426D, S/N 3159, Part Number CBUS1050D, S/N 230346, and Part Number CBUS1060A, S/Ns 50085 and 50089. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Replace the Lindstrand Balloons Ltd Burner system with the Cameron Balloons Triple Burner, Part Number CB2081-2, S/N B5216, B5217, B5298. Replace the Lindstrand Balloons Ltd fuel tanks with the Cameron Balloons Fuel Tanks, Part Number CBUS426D, S/N 3159, Part Number CBUS1050D, S/N 230346, and Part Number CBUS1060A, S/Ns 50085 and 50089.
SB03242CH 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: Lindstrand Balloons 260A. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Lindstrand Balloons 260A 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
Modification in accordance with FAA approved SIE Drawing List 9000 N/C,, dated August 7, 1991, or later FAA approved revisions, to permit an increased maximum zero fuel weight (MZFW), and maximum landing weight (MLW) of DC-8-61 airplanes.
FAA holder: Structural Integrity Engineering
Approval of maximum zero fuel weight increase from 138,000 pounds to 146,000 pounds. (727-200 SERIES S/N 19483, 19484, 19486, 19491, 20180, 20184, 20185, 20187, 20995, 20996, 19480, 19492, 19481, 19482, 19485, 20191 ONLY).
FAA holder: Structural Integrity Engineering
Approval of maximum zero fuel weight and maximum landing weight (Flaps 30) increases to 157,500 pounds and 166,000 pounds, respectively. (727-200 SERIES S/N 22080 ONLY).
FAA holder: Structural Integrity Engineering
Approval of maximum zero fuel weight increase to 132,000 pounds. (727-100 SERIES S/N 19183 ONLY).
FAA holder: Structural Integrity Engineering