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.

FAA-listed holder

Rainbow Ryders Inc.

Aircraft configurations

FAA revision date

July 24, 2013

FAA status

Current · Issued

Recorded modification

What the FAA record covers

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.

Lindstrand Balloons 260AB82EU

Buyer checks

Confirm before sourcing

SA5510NMFuel systemsRevised Dec 29, 2003

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

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ST00633ATFuel systemsRevised Dec 29, 2003

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

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ST00720ATFuel systemsRevised Dec 29, 2003

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

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ST00782ATFuel systemsRevised Dec 29, 2003

Approval of maximum zero fuel weight increase to 132,000 pounds. (727-100 SERIES S/N 19183 ONLY).

FAA holder: Structural Integrity Engineering

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What the FAA record covers

Aircraft named in FAA DRS

Confirm before sourcing

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.

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).

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).

Approval of maximum zero fuel weight increase to 132,000 pounds. (727-100 SERIES S/N 19183 ONLY).