EASA Regulations & Airworthiness Directives

Browse 5,166 EASA regulations with AI-powered summaries.

Aircraft:AllAirbus A320286Airbus A321285Airbus A319253Airbus A350224Airbus A330221Airbus A318189Airbus A380182Boeing 737175Airbus A340141Airbus A350-941134Airbus BD-500 (A220 Series)123Airbus Helicopters AS 332119Airbus Helicopters EC 225116Airbus Helicopters SA 330116Boeing 787116Show all...

EASA SIB 2006-06R2

Dec 22, 2006

WITHDRAWN / CANCELLED - SEE EXPLANATION IN REMARKS

The EASA Safety Information Notice No. 2006 – 06 Revision 2 addresses issues with 3rd Stage Low Pressure Turbine Blades P/N 798403 installed on Pratt & Whitney engine models JT8D-219 and JT8D-217C. The notice highlights failures of these blades repaired by Chromalloy Southwest between September 30, 2005 and September 11, 2006, which led to in-flight shutdowns. It provides updated recommendations following the reopening of the repair process after an internal investigation.

Safety Information Bulletin

EASA SIB 2006-07R2

Oct 2, 2006

Boeing 737-400 - Incident on 15 June 2006, at Catania Fontanarossa airport (Italy)

The Boeing 737-400 - Incident on 15 June 2006, at Catania Fontanarossa airport (Italy) is a Safety Information Bulletin focused on airworthiness concerns related to the Boeing 737-400 aircraft. The document addresses safety issues identified following an incident involving this aircraft type at Catania Fontanarossa airport. It aims to inform operators and maintenance organizations about potential risks and necessary precautions.

Safety Information Bulletin
  • Boeing 737-400

EASA SIB 2006-08

Aug 30, 2006

Superseded by EASA SIB 2009-18

EASA Safety Information Notice No. 2006-08 is an advisory document addressing the failure of the main rotor blade retention bolt (part number 900R310E0001-103) on MD Helicopters, Inc. MD900 series helicopters. The notice highlights previous failures and references FAA Airworthiness Directive 2003-14-51 and MDHI Service Bulletin SB900-092 Rev 1. It aims to raise awareness among flight crews about the issue and recommends specific inspection procedures.

Safety Information Bulletin
  • MD Helicopters MD900

EASA SIB 2006-05

Jul 28, 2006

FAA SAIB SW-06-55 - Robinson R22 and R44 Helicopters Main Rotor Blades

FAA SAIB SW-06-55 is a Special Airworthiness Information Bulletin addressing main rotor blade issues on Robinson R22 and R44 helicopters. It focuses on disbond findings at the tips of the inboard doubler on Robinson R22 MRB part number A016-4 and R44 MRB part numbers C016-2/5. The bulletin provides guidance based on Robinson Service Letters SL-55 for the R22 and SL-31 for the R44.

Safety Information Bulletin
  • Robinson R22
  • Robinson R44

EASA SIB 2006-03

May 19, 2006

Repairs for Messier-Bugatti carbon brakes P/Ns C20225( ), C20449( ), C20524( ), C20534( ), C20194( ) and C20210( ) by third parties invalidating the ETSO Authorisation

EASA Safety Information 2006-03 is a safety communication addressing unauthorized repairs to Messier-Bugatti carbon brakes with part numbers C20225, C20449, C20524, C20534, C20194, and C20210. The document highlights that third-party repairs not approved by Messier-Bugatti or EASA invalidate the ETSO Authorisation for these carbon brakes. This issue affects the safety and performance of the brakes used on aircraft equipped with these parts.

Safety Information Bulletin
All aircraft

EASA SIB 2006-02

Apr 12, 2006

AIRBUS A300 aircraft series B2, B4, C4 and F4, except for the A300-600 series - Non-Conformance of maintenance requiring visual inspection of slat transmission shafts number 21 and asymmetry pick off units - DGAC F Airworthiness Directive No. F-2005-213R1

AIRBUS A300 aircraft series B2, B4, C4 and F4, except for the A300-600 series - Non-Conformance of maintenance requiring visual inspection of slat transmission shafts number 21 and asymmetry pick off units - DGAC F Airworthiness Directive No. F-2005-213R1 is an airworthiness directive issued by the DGAC, the French civil aviation authority. It applies to Airbus A300 aircraft series B2, B4, C4, and F4 and mandates a one-time visual inspection of slat transmission shafts number 21 and asymmetry pick off units to ensure proper connection and functionality.

Airworthiness Directive
  • Airbus A300