EASA Regulations for Boeing 767

58 airworthiness directives and regulations affecting Boeing 767.

EASA AD US-93-14-19R1

Nov 27, 2018

CANCELLED: Wings - Trailing Edge Wedge of the Leading Edge Slat - Inspections

Airworthiness Directive 93-14-19 issued by the U.S. Federal Aviation Administration addresses inspections of the trailing edge wedges of the leading edge slats on Boeing 767 series airplanes, line numbers 1 through 488. The directive mandates specific inspection methods and repair procedures to prevent separation of these components, ensuring continued airworthiness and safety of the affected aircraft.

Airworthiness Directive
  • Boeing 767

EASA AD US-2018-20-13

Nov 2, 2018

[Correction] Fuel - Motor-Operated Valve Actuators - Replacement / Maintenance or Inspection Program - Revision

Correction Fuel - Motor-Operated Valve Actuators - Replacement / Maintenance or Inspection Program - Revision is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2018-20-13) addressing certain Boeing Company airplanes including Model 737 (excluding -100, -200, -200C, -300, -400, and -500 series), Model 757, and Model 767 series. The AD targets latently failed motor-operated valve (MOV) actuators of fuel shutoff valves on engines and auxiliary power units (APUs). It mandates replacement of specific MOV actuators and revising maintenance or inspection programs to incorporate updated airworthiness limitations.

Airworthiness Directive
  • Boeing 737
  • Boeing 757
  • Boeing 767

EASA AD US-2018-13-06

Aug 15, 2018

Wings - Lower Outboard Wing Skin - Inspection

Airworthiness Directive 2018-13-06 is a final rule issued by the Federal Aviation Administration affecting certain Boeing 767-300 and 767-300F series airplanes. It addresses fatigue cracking in the lower outboard wing skin at the inboard segment of stringer L-9.5 on airplanes equipped with winglets installed per Supplemental Type Certificate ST01920SE. The directive mandates repetitive high frequency eddy current inspections and necessary repairs to ensure continued airworthiness.

Airworthiness Directive
  • Boeing 767300300F

EASA AD 2018-0157

Jul 24, 2018

Engine — Low Pressure Compressor Shafts — Life Reduction

EASA Airworthiness Directive 2018-0157 is an airworthiness directive addressing Rolls-Royce RB211-524G and -524H engines installed on Boeing 747 and Boeing 767 aircraft. It focuses on the low pressure compressor shafts, specifically part number UL24833, which have undergone unauthorized repairs affecting their approved life. The directive mandates life reduction and removal from service of affected shafts to prevent potential shaft fracture and consequent damage to the aircraft.

Airworthiness Directive
  • Rolls-Royce Deutschland Ltd & Co Kg RB211-524
  • Boeing 747
  • Boeing 767

EASA AD US-2018-11-08

Jun 15, 2018

Fuselage - Frame Web / Stub Beam Fitting Areas - Inspection

Federal Register Volume 83, Number 108 (AD 2018-11-08) is a final rule airworthiness directive issued by the FAA for certain Boeing 767-200 and 767-300 series airplanes. It mandates inspections of the fuselage frame web and stub beam fitting areas to detect cracks related to material review board (MRB) filler that may extend above the frame-to-stub-beam joint. The directive addresses structural integrity concerns due to cracking in the frame inner chord at specific stations.

Airworthiness Directive
  • Boeing 767200300

EASA AD US-2018-11-14

Jun 15, 2018

Wings - Lower Outboard Wing Skin - Inspection / Repair / Modification

The Federal Aviation Administration's Airworthiness Directive 2018-11-14 addresses fatigue cracking in the lower outboard wing skin of certain Boeing 767-300 and 767-300F series airplanes equipped with Aviation Partners Boeing winglets. This directive mandates high frequency eddy current inspections and requires repair or modification as necessary to ensure structural integrity. It also outlines follow-on actions including repetitive inspections or structural modifications to prevent wing and winglet separation.

Airworthiness Directive
  • Boeing 767300300F

EASA AD US-2018-01-02

Jan 4, 2018

Water / Waste - Potable Water System - Inspection / Modification

Airworthiness Directive 2018-01-02 is a final rule issued by the Federal Aviation Administration affecting certain Boeing 767-200, -300, and -400ER series airplanes. This directive addresses issues with the potable water system, specifically the plastic potable water coupling and hose assemblies, to prevent malfunctions in the engine indication and crew alerting system (EICAS) during flight. It mandates inspections, corrective actions, and installations to ensure system integrity and flight safety.

Airworthiness Directive
  • Boeing 767200300400ER

EASA SIB 2010-10R1

Nov 28, 2014

Fuel Tank Safety — Flammability Reduction System (FRS) for High Flammability Exposure Fuel Tanks

EASA Safety Information Bulletin 2010-10R1 is an informational document addressing fuel tank safety through the introduction of Flammability Reduction Systems (FRS) for high flammability exposure fuel tanks. It applies to Airbus A318, A319, A320, A321, A330, A340 and Boeing 737, 767, and 777 aircraft with center wing tanks manufactured from January 1, 2012. The bulletin provides background on the safety improvements following the TWA Flight 800 accident and outlines regulatory requirements for new production aircraft fuel tanks.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Airbus A330
  • Airbus A340
  • Boeing 737
  • Boeing 767
  • Boeing 777

EASA SIB 2014-29

Oct 24, 2014

WITHDRAWN: Comments received indicate the need for a review of applicable recommendation

EASA Safety Information Bulletin 2014-29 provides clarification on the minimum cabin crew requirements for twin aisle aeroplanes including Airbus A300, A310, A330, A340, A380, A350 series, Boeing 747, 767, 777, 787, DC10, MD11 series, and Lockheed L1011 series. It explains the operational and certification regulations governing cabin crew numbers, emphasizing the need for at least one cabin crew member per emergency exit on twin aisle aircraft due to evacuation management challenges. The bulletin addresses misunderstandings arising from Commission Regulation (EU) No 965/2012 and highlights the importance of adequate cabin crew supervision for passenger safety during evacuations.

Safety Information Bulletin
  • Airbus A300
  • Airbus A310
  • Airbus A330
  • Airbus A340
  • Airbus A380
  • Airbus A350
  • Boeing 747
  • Boeing 767
  • Boeing 777
  • Boeing 787
  • McDonnell Douglas DC10
  • McDonnell Douglas MD11
  • Lockheed L1011

EASA SIB NE-13-31

May 14, 2013

Pratt & Whitney PW4000 Engines — Scavenge Oil Tube Coking and Proper Cleaning at Overhaul

The Special Airworthiness Information Bulletin (SAIB) NE-13-31 issued by the FAA on May 9, 2013, addresses potential scavenge oil tube coking and nozzle blockage in Pratt & Whitney PW4000 series turbofan engines. This issue affects engines installed on aircraft such as the Airbus A300, A310, A330, Boeing 747-400, 767, 777, and McDonnell Douglas MD-11. The bulletin provides guidance on proper cleaning and inspection procedures during engine overhaul to prevent reduced oil flow and possible engine damage.

Safety Information Bulletin
  • Airbus A300
  • Airbus A310
  • Airbus A330
  • Boeing 747-400
  • Boeing 767
  • Boeing 777
  • McDonnell Douglas MD-11

EASA SIB 2010-32

May 25, 2011

WITHDRAWN - REPLACED BY EASA AD 2011-0043

EASA Safety Information Bulletin 2010-32 is an informational bulletin addressing the potential loss of ATC transponder transmissions caused by a loose resistor connection in Gables Engineering Inc ATC/TCAS control panels, specifically the G7490, G7492, and G7493 series. These control panels are installed on various aircraft types including Airbus A310, ATR 42, BAE Systems BAe146, Boeing 707 through 777 series, Fokker F28, Lockheed Hercules and Tristar, McDonnell Douglas DC and MD series, and Sabreliner NA-265 series. The bulletin provides guidance but does not mandate corrective action.

Safety Information Bulletin
  • Airbus A310
  • ATR 42
  • BAE Systems BAe146
  • Boeing 707
  • Boeing 717
  • Boeing 727
  • Boeing 737
  • Boeing 747
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Fokker F28
  • Lockheed Hercules
  • Lockheed Tristar
  • McDonnell Douglas DC series
  • McDonnell Douglas MD series
  • Sabreliner NA-265

EASA SIB NE-11-27

Apr 6, 2011

General Electric CF6-80 Engines - Improperly Welded Fuel Nozzles

The FAA Special Airworthiness Information Bulletin SAIB: NE-11-27 addresses improperly welded fuel nozzles in General Electric CF6-80A, CF6-80C2, and CF6-80E1 series turbofan engines. These engines are installed on aircraft including Airbus A300, A310, A330, Boeing 747, 767, and McDonnell Douglas MD-11 series airplanes. The bulletin informs operators and maintenance personnel about the discovery of incomplete welds on specific fuel injector nozzles, which could lead to fuel leaks and potential engine shutdowns.

Safety Information Bulletin
  • Airbus A300
  • Airbus A310
  • Airbus A330
  • Boeing 747
  • Boeing 767
  • McDonnell Douglas MD-11

EASA SIB 2010-25

Aug 27, 2010

Cabin Oxygen Mask Service Recommendations from Original Equipment Manufacturers, and Cabin Oxygen Masks with B/E Aerospace In-line Flow Indicators Part Number (P/N) 118023-02

EASA Safety Information Bulletin SIB No. 2010-25 provides service recommendations regarding cabin oxygen masks equipped with B/E Aerospace in-line flow indicators part number 118023-02. The bulletin applies to CS1-23 and CS-25 category aeroplanes, including Airbus A318, A319, A320, A321, Boeing 737, 747, 757, 767, 777, and Fokker F28 models. It addresses failures of the in-line flow indicators that can cause oxygen flow interruption during use.

Safety Information Bulletin
  • Airbus A318
  • Airbus A319
  • Airbus A320
  • Airbus A321
  • Boeing 737
  • Boeing 747
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Fokker F28

EASA SIB NE-10-37

Aug 2, 2010

General Electric - CF6-80C2 FADEC Fuel Metering Valve Resolver Feedback Faults

The General Electric - CF6-80C2 FADEC Fuel Metering Valve Resolver Feedback Faults Special Airworthiness Information Bulletin (SAIB NE-10-37) informs operators of airplanes equipped with GE CF6-80C2 series turbofan engines about potential engine in-flight shutdowns caused by fuel metering valve feedback faults. This bulletin applies to engines on Boeing 747, 767, Airbus A300, and McDonnell Douglas MD-11 aircraft, except Boeing 747 and 767 airplanes with FADEC software version 8.2.R or later. The bulletin provides guidance to prevent dual-channel faults that can lead to uncommanded engine shutdowns.

Safety Information Bulletin
  • Boeing 747
  • Boeing 767
  • Airbus A300
  • McDonnell Douglas MD-11

EASA SIB 2009-06R1

May 26, 2009

WITHDRAWN - Rockwell-Collins GPS Receiver — Date Roll-Over Anomaly

EASA Safety Information Bulletin 2009-06R1 is an informational bulletin addressing a software anomaly in certain Rockwell-Collins Multi-Mode Receivers (MMR) installed on various Boeing, Airbus, and Bombardier aircraft models. The anomaly causes a date roll-over error at midnight on 20/21 June 2009, resulting in the receiver reporting an incorrect date approximately 19.7 years off. Affected aircraft include Boeing 737, 747, 757, 767, 777, Airbus A300-600, A310, A320, A330, A340, A380, and Bombardier CL-600 series.

Safety Information Bulletin
  • Boeing 737
  • Boeing 747
  • Boeing 757
  • Boeing 767
  • Boeing 777
  • Airbus A300-600
  • Airbus A310
  • Airbus A320
  • Airbus A330
  • Airbus A340
  • Airbus A380
  • Bombardier CL-600

EASA SIB 2008-83

Dec 10, 2008

Failure of USDOT Type 3HT Passenger Oxygen Cylinder

EASA Safety Information Bulletin SIB No: 2008-83 is an advisory document addressing the failure of USDOT Type 3HT passenger and crew stationary oxygen cylinders. It highlights a decompression incident on a Qantas Boeing 747-400 caused by a ruptured oxygen cylinder with part number 10003367, used on various aircraft including Airbus A300-600, A310, A320 series, Boeing 707, 727, 737, 747, 757, 767 series, and McDonnell Douglas DC-9, DC-10, and MD-11 series. The bulletin informs operators and maintenance organizations about the potential risk and ongoing investigation.

Safety Information Bulletin
  • Airbus A300-600
  • Airbus A310
  • Airbus A320
  • Boeing 707
  • Boeing 727
  • Boeing 737
  • Boeing 747
  • Boeing 757
  • Boeing 767
  • McDonnell Douglas DC-9
  • McDonnell Douglas DC-10
  • McDonnell Douglas MD-11

EASA SIB 2008-25

Apr 1, 2008

WITHDRAWN - FAA UPN TRANSFERRED TO EASA SUP WEBPAGE

EASA Safety Information Notice No. 2008-25 is an informational notice regarding Main Landing Gear (MLG) truck beams that have been improperly maintained and returned to service. It specifically affects Boeing 707, 747, 757, and 767 aircraft equipped with the identified MLG truck beams. The notice references the FAA Unapproved Parts Notification No. 2008-S20080110024, which details the investigation findings.

Safety Information Bulletin
  • Boeing 707
  • Boeing 747
  • Boeing 757
  • Boeing 767