The FAA has recently adopted the attached AD for turbocharged, reciprocating engine powered airplanes and helicopters and turbocharged reciprocating engines with a certain v-band coupling installed. This AD was prompted by multiple failures of spot-welded, multi-segment v-band couplings at the tailpipe to the turbocharger exhaust housing flange. This AD establishes a life limit for the spot-welded, multi-segment exhaust tailpipe v-band coupling and requires repetitively inspecting the spot-welded, multi-segment exhaust tailpipe v-band coupling.
Stage: Final Publications
Regulatory Agency Final Publications
FAA_Final_Rule_V_Band_Clamp_AD_Docket_No_FAA_2022_0891_AD_2023_09_09_RIN_2120_AA64
ED Decision 2023/007/R Helicopter emergency medical service performance and public interest sites
The objective of this Decision is to facilitate the implementation of the new requirements introduced into Regulation (EU) No 965/2012 (the ‘Air OPS Regulation’) by Commission Implementing Regulation (EU) 2023/1020 (the ‘HEMS Regulation’).
The amendments introduced by the HEMS Regulation and the acceptable means of compliance (AMC) and guidance material (GM) introduced in this Decision will modernise the European Union (EU) aviation regulatory framework applicable to helicopter emergency medical services, and are expected to increase safety and foster efficiency and proportionality, while keeping the economic impact on HEMS operators at a minimum.
en_to_ed_decision_2023-007-r
ed_decision_2023-007-r
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
