Qualification Testing of Turbojet and Turbofan Engine Thrust Reversers

AC 20-18B Current Issued 2015-07-07 OPR ANE-111 FAA PDF ↗

14 CFR Parts this AC applies to

Derived from the AC's subject series via the FAA's published numbering scheme.

Document overview

Structured fields from the FAA Dynamic Regulatory System (DRS). Full body text lives in the linked PDF.

Subject: Qualification Testing of Turbojet and Turbofan Engine Thrust Reversers
Status: Current
Office: AIR-620: Technical Innovation Policy Branch
Cancels: AC 20-18A
Referenced 14 CFR Parts: Part 23, Part 25, Part 33
Referenced sections: Sec. 23.933, Sec. 23.934, Sec. 25.933, Sec. 25.934, Sec. 33.28, Sec. 33.63, Sec. 33.85, Sec. 33.87, Sec. 33.89, Sec. 33.97, Sec. 33.99