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Stage: Final Publications
Regulatory Agency Final Publications
amc_gm_to_part-spo_-_issue_1_amendment_19
amc_gm_to_part-spa_-_issue_1_amendment_14
amc_gm_to_part-oro_-_issue_2_amendment_23
amc_gm_to_part-nco_-_issue_2_amendment_16
amc_gm_to_part-ncc_-_issue_1_amendment_19
amc_gm_to_part-cat_-_issue_2_amendment_23
amc_gm_to_part-aro_-_issue_3_amendment_14
AC_20-141B_Change_1
FAA AC 33.15-3 Powder Bed Fusion Additive Date: AC No: 33.15-3 Manufacturing Process for Aircraft Engine Initiated By: AIR-621 Parts
This advisory circular (AC) describes an acceptable means for demonstrating
compliance with Title 14, Code of Federal Regulations (14 CFR) 33.15 for aircraft
engine parts with materials produced by the powder bed fusion (PBF) additive
manufacturing (AM) process. Guidance is also p
FAA AC 33.15-3
FAA PS-AIR-25-13-R1 Final Electromagnetic Compatibility Demonstration for Airplane Wireless Radio Frequency Networks
This policy statement provides additional Federal Aviation Administration (FAA) guidance on
demonstrating electromagnetic compatibility (EMC) for wireless radio frequency (RF) systems
that are installed on transport category airplanes. RF systems include portable wireless RF
transmitters and receivers carried onboard by passengers, crewmembers, and in baggage or
cargo, and installed wireless RF devices that communicate with other RF devices. Installed
wireless RF systems use standards such as, but not limited to, Bluetooth, Wi-Fi, or mobile
telephony. This policy statement defines an acceptable means for demonstrating compliance with
Title 14, Code of Federal Regulation (14 CFR) part 25 airworthiness regulations.
This policy does not apply to installed airplane radio systems that intentionally communicate
with radios outside the airplane, such as those that communicate with satellites, ground stations,
and radios in other airplanes.