Airworthiness Directive 2024-20-07
recurringAirworthiness Directives; Various Helicopters
What this AD requires
The FAA is adopting a new airworthiness directive (AD) for various helicopters modified by certain supplemental type certificates (STCs) that approve the installation of an emergency float kit or an emergency float with a liferaft kit. This AD was prompted by the results of an accident investigation and subsequent reports of difficulty pulling the emergency float kit activation handle installed on the pilot cyclic. This AD requires repetitively inspecting the pull force on the float activation handle and for certain model helicopters, this AD also requires and replacing certain part-numbered float inflation reservoirs (reservoirs) and pull cable assemblies (cables) with other part-numbered reservoirs and cables. Finally, this AD prohibits installing certain part-numbered reservoirs and cables on specific helicopters. The FAA is issuing this AD to address the unsafe condition on these products.
Which aircraft AD 2024-20-07 applies to
Applies only to helicopters modified by the applicable Supplemental Type Certificate (STC): SR00831LA (Airbus Helicopters AS350B/BA/B1/B2/B3/C/D/D1, AS355E/F/F1/F2/N); SR00780LA (Airbus Helicopters EC120B); SR01687LA (Airbus Helicopters EC130B4); SR00856LA (Airbus Helicopters Deutschland GmbH BO-105A/C/S/LS A-3); SR01855LA (Airbus Helicopters Deutschland GmbH EC135P1/P2/P2+/P3/T1/T2/T2+/T3); SR02244LA (Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2/D-2); SR01779LA (Bell Textron Inc. 210/212/412/412CF/412EP; Leonardo S.p.a. AB412/AB412 EP); SR01459LA (Bell Textron Inc. 412/412CF/412EP); SR01535LA (Bell Textron Canada Limited 206A/206B/206L/206L-1/206L-3/206L-4/407); SR00932LA (MD Helicopters, LLC 369D/E/F/FF/HE/HM/HS/500N); SR02049LA (Robinson Helicopter Company R44/R44 II); SR02484LA (Robinson Helicopter Company R66); SR01902LA (Sikorsky Aircraft Corporation S-76A/B/C). Helicopters with an AS350B3e designation are Model AS350B3; EC135P3H = EC135P3; EC135T3H = EC135T3; MBB-BK 117 C-2e = MBB-BK 117 C-2; 206B3 = 206B; 206L-1+ = 206L-1; 206L-3+ = 206L-3.
Whether AD 2024-20-07 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.