EASA Regulations for Boeing 747

80 airworthiness directives and regulations affecting Boeing 747.

EASA AD 2018-0259R1

Feb 7, 2019

Superseded by EASA AD 2021-0234

EASA Airworthiness Directive 2018-0259R1 is an updated directive addressing safety concerns related to USB receptacles installed in various aircraft including Fokker F27 and F28 models, Airbus A318 through A340 series, ATR42 and ATR72, Boeing 737 through 777, and Bombardier CL-600 and DHC-8 aircraft. The directive mandates modifications to the affected Lone Star Aviation USB receptacle part number LS03-05050-A to prevent overheating and smoke/fumes in the cockpit. It applies to aircraft with these USB receptacles installed via Fokker Services Supplemental Type Certificates, Service Bulletins, or minor modifications.

Airworthiness DirectiveSuperseded

Airbus A318
Airbus A319
Airbus A320
Airbus A321
Airbus A330
Airbus A340
ATR ATR42
ATR ATR72
Boeing 737
Boeing 757
Boeing 767
Boeing 777
Bombardier CL-600 (Challenger)
De Havilland Canada DHC-8
Fokker CRR-0185
Fokker CRR-0186
Fokker CRR-0190
Fokker CRR-0210
Fokker CRR-0241
Fokker CRR-0265
Fokker CRR-0300
MHI RJ Aviation CL-600 (Regional Jet)
Fokker F27
Fokker F28
Boeing 747
Bombardier CL-600
Bombardier DHC-8

EASA AD US-2018-23-13

Nov 30, 2018

Oxygen - Flightcrew Oxygen Masks - Inspection / Replacement

Federal Aviation Administration Airworthiness Directive 2018-23-13 is a final rule applicable to all Boeing Model 747-8 and 747-8F series airplanes. It addresses an unsafe condition where flightcrew oxygen masks and regulators did not function as designed during flight testing, potentially delaying mask deployment. This directive mandates inspection and replacement of certain oxygen masks and regulators to ensure proper functionality.

Airworthiness Directive

Boeing 74788F

EASA AD US-2018-19-23

Oct 4, 2018

Doors - Cargo Door Control Switches - Replacement / Installation

Airworthiness Directive 2018-19-23 is a final rule issued by the Federal Aviation Administration addressing certain Boeing 747 and 757 series airplanes. It mandates replacement of specific cargo door control switches with improved versions, installation of an arm switch on certain cargo doors, and requires operational and functional testing. This directive aims to prevent uncommanded cargo door operations that could cause injury or damage.

Airworthiness Directive

Boeing 747
Boeing 757

EASA AD US-2018-16-06

Aug 9, 2018

Fuselage - Boeing Material Specification (BMS) 8-39 Flexible Urethane Foam - Inspection / Modification / Replacement

The Federal Aviation Administration's Airworthiness Directive 2018-16-06 addresses certain Boeing Model 747 series airplanes, including the 747-100, -200, -300, -400, 747SP, 747SR, and 747-8 series. This directive focuses on inspecting, modifying, and replacing Boeing Material Specification (BMS) 8-39 flexible urethane foam used in fuselage floor panel assemblies and power drive unit cover assemblies. The AD aims to mitigate fire risks associated with the degradation of this foam material.

Airworthiness Directive

Boeing 7471002003004008
Boeing 747SP
Boeing 747SR

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-2018-09-12

May 24, 2018

Oxygen - Low-Pressure Passenger Oxygen System - Replacement / Inspection

Airworthiness Directive 2018-09-12 issued by the Federal Aviation Administration addresses certain Boeing 747-200B, 747-300, and 747-400 series airplanes equipped with therapeutic oxygen in the gaseous passenger oxygen system. The directive mandates replacement of specific low-pressure oxygen flex-hoses with new non-conductive versions and requires a general visual inspection to verify minimum clearance of oxygen system components from adjacent structures. This directive aims to prevent potential oxygen-fed fires caused by electrical short circuits affecting the oxygen flex-hoses.

Airworthiness Directive

Boeing 747200B300400

EASA AD US-2018-07-06

Apr 10, 2018

Airplane Flight Manual - Revision / Landing Gear - Main Entry Door 3 Intercostal Webs - Modification

Airplane Flight Manual - Revision / Landing Gear - Main Entry Door 3 Intercostal Webs - Modification is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2018-07-06) that applies to certain Boeing 747-8 series airplanes. It addresses an unsafe condition related to restricted movement of the right brake pedals after landing rollout. The AD requires revising the airplane flight manual (AFM) to add an autobrake system limitation and mandates modification of intercostal webs near main entry door 3 to terminate the AFM limitation.

Airworthiness Directive

Boeing 7478

EASA AD US-2018-04-07

Mar 12, 2018

Wings - Structural Significant Items (SSIs) - Revision of the Maintenance or Inspection Program / Inspection

The Federal Aviation Administration's Airworthiness Directive 2018-04-07 titled 'Wings - Structural Significant Items (SSIs) - Revision of the Maintenance or Inspection Program / Inspection' applies to all Boeing Model 747 series airplanes including 747-100, 747-200, 747-300, 747-400, 747SR, and 747SP variants. This directive addresses fatigue cracking issues identified in aging transport category airplanes by requiring updates to maintenance and inspection programs to include inspections of structural significant items (SSIs).

Airworthiness Directive

Boeing 747100200300400
Boeing 747SR
Boeing 747SP

EASA AD US-2017-22-10

Dec 4, 2017

Equipment / Furnishings - Fastener Assemblies - Replacement

The Federal Aviation Administration's Airworthiness Directive 2017-22-10 addresses certain Boeing Model 747-400, 747-400F, and 747-8F series airplanes. This directive mandates the replacement of fastener assemblies on the crew access ladder handrails due to reported failures. The directive aims to prevent potential serious or fatal injuries resulting from loose fastener assemblies.

Airworthiness Directive

Boeing 747400400F8F

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 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 2009-15

Jun 4, 2009

Freighter Aeroplanes with Class E Cargo Compartment on Main Deck

EASA Safety Information Bulletin 2009-15 is an advisory document addressing freighter aeroplanes with Class E cargo compartments on the main deck, specifically including Boeing 747 series aircraft. It highlights safety considerations and recommended practices for in-flight access by non-crewmembers, such as supernumeraries, to these cargo compartments. The bulletin supports FAA Special Airworthiness Information Bulletin NM-09-27 and extends its recommendations to all operators of affected freighter aeroplanes within the European Union and associated countries.

Safety Information Bulletin

Boeing 747

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 2008-46

Jul 10, 2008

Rolls-Royce RB211-535 and -524 Engines - Faulty Inspection of High Pressure Turbine Discs

EASA Safety Information Bulletin SIB No. 2008-46 addresses the faulty inspection of High Pressure (HP) Turbine Discs on Rolls-Royce RB211-535 and RB211-524 series engines. These engines are commonly installed on Boeing 747 and 757 aircraft. The bulletin highlights concerns about improper inspection of cooling air holes on HP Turbine Discs, which are subject to existing Airworthiness Directives.

Safety Information Bulletin

Boeing 747
Boeing 757

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

EASA SIB 2007-20

Aug 8, 2007

FAA SAIB NE-07-41 - Pratt & Whitney JT9D-7A and -7J Engines - Maintenance of the High Pressure Turbine (HPT) 2nd Stage Vane Assemblies

FAA Special Airworthiness Information Bulletin NE-07-41 is an informational bulletin addressing maintenance issues with Pratt & Whitney JT9D-7A and -7J series engines, specifically the high pressure turbine (HPT) 2nd stage vane assemblies. The bulletin highlights an engine separation event on a Boeing 747 caused by improper installation of the HPT 2nd stage vane assembly, which led to disk rim failure. It applies primarily to Boeing 747 aircraft equipped with these engines.

Safety Information Bulletin

Boeing 747