(1) A maximum type-certificated passenger capacity of 30 or more, or
(2) A maximum payload capacity of 7,500 pounds or more.
(b) If the application was made on or after June 6, 2001, the requirements of 14 CFR 25.981 in effect on December 26, 2008, apply.
[Doc. No. FAA–2005–22997, 73 FR 42499, July 21, 2008, as amended by Amdt. 26–3, 74 FR 31619, July 2, 2009]
NEXT: Sec. 26.39 - Newly produced airplanes: Fuel tank flammability.
PREVIOUS: Sec. 26.35 - Changes to type certificates affecting fuel tank flammability.