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EASA Regulations for Boeing 767

58 airworthiness directives and regulations affecting Boeing 767.

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New ADs and bulletins for Boeing 767, summarized like the ones below, every Monday.

EASA AD US-2026-18-08

Fuselage - Cargo Track Crown Fitting - Inspection

Fuselage - Cargo Track Crown Fitting - Inspection is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2026-18-08) addressing certain Boeing 767-300F series airplanes. This directive requires inspection and possible replacement of titanium cargo track crown fittings due to suspect material certifications. The AD aims to prevent cargo track failure that could compromise airplane controllability and damage critical systems in the main cargo compartment.

Airworthiness Directive

Boeing 767300F

EASA AD US-2026-16-06

Wings - Lower Outboard Wing Skin - Inspection

The document titled "Wings - Lower Outboard Wing Skin - Inspection" is a final rule Airworthiness Directive (AD 2026-16-06) issued by the Federal Aviation Administration (FAA) affecting certain Boeing 767-300 and 767-300F series airplanes equipped with Aviation Partners Boeing winglets installed under Supplemental Type Certificate ST01920SE. The directive mandates inspections for fatigue cracking in the lower outboard wing skin and requires repairs or modifications as necessary to ensure continued airworthiness.

Airworthiness Directive

Boeing 767300300F

EASA AD US-2026-13-16

Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment

The Navigation - 5G C-Band wireless Broadband Interference with Radio Altimeter System when operating in Canadian airspace - Amendment is a Federal Aviation Administration (FAA) airworthiness directive addressing interference issues affecting Boeing Model 757 and Model 767 airplanes. This directive responds to increased 5G Lower C-Band interference in Canadian airspace that compromises radio altimeter reliability and affects critical airplane systems during approach, landing, and go-around phases. It mandates revisions to the airplane flight manual to restrict certain operations relying on radio altimeter data when operating in Canadian airspace.

Airworthiness Directive

Boeing 757
Boeing 767

EASA AD US-2025-15-08

Equipment / Furnishings - Flight Crew Seats - Inspection / Check

Airworthiness Directive 2025-15-08 is a final rule issued by the Federal Aviation Administration (FAA) addressing The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes. It focuses on inspection and checks of the flight crew seats, specifically the Captain's and First Officer's seats, to ensure the horizontal movement system (HMS) functions safely. This directive corrects previous errors related to crediting compliance actions and clarifies inspection requirements.

Airworthiness Directive

Boeing 767

EASA AD US-2025-02-07

Navigation - Aeroplane Flight Manual - Revision / Software Installation

Airworthiness Directive 2025-02-07 is a final rule issued by the Federal Aviation Administration addressing certain Boeing airplanes including Model MD-11, MD-11F, 717-200, 737-600 through 737-9 series, 747-400 series, 757, 767, and 777. The directive focuses on updating the Aeroplane Flight Manual and installing updated multimode receiver (MMR) operational software to address issues with Coordinated Universal Time calculation errors and simultaneous MMR resets. This affects airplanes equipped with Collins GLU-2100 MMR part number 822-2532-100 with software versions earlier than COL4C-0087-0003.

Airworthiness Directive

Boeing 717
Boeing 737
Boeing 747
Boeing 757
Boeing 767
Boeing 777
Boeing MD-11

EASA AD US-2025-01-06

Superseded by FAA AD 2025-15-08

The FAA Airworthiness Directive 2025-01-06 supersedes AD 2019-14-13 and applies to all Boeing 767-200, -300, -300F, and -400ER series airplanes. It addresses uncommanded fore and aft movement of the Captain's and First Officer's seats by requiring identification of seat part and serial numbers, inspections of the horizontal movement system (HMS), and applicable on-condition actions. The directive incorporates updated Boeing and Ipeco service bulletins to include previously omitted seat part numbers.

Airworthiness Directive

Boeing 767

EASA AD US-2024-26-03

Water / Waste - Potable Water System - Installation / Leakage Test

The document titled 'Water / Waste - Potable Water System - Installation / Leakage Test' is a regulatory guideline focused on the installation and leakage testing procedures for potable water systems in aircraft. It addresses standards to ensure the integrity and safety of potable water installations, although no specific aircraft types or engine models are mentioned. The document aims to maintain the hygiene and operational reliability of potable water systems onboard.

Boeing 767

EASA AD US-2024-25-08

Landing Gear - Outer Cylinder - Replacement

The document titled 'Landing Gear - Outer Cylinder - Replacement' is a regulatory directive concerning the replacement procedures for the outer cylinder component of aircraft landing gear. It addresses maintenance and safety requirements related to this specific landing gear part. The document does not specify particular aircraft types or engine models affected.

Airworthiness Directive

Boeing 767

EASA AD US-2024-24-05

Equipment / Furnishings - Cargo Compartment Insulation Blankets - Replacement

The document titled 'Equipment / Furnishings - Cargo Compartment Insulation Blankets - Replacement' is a regulatory communication concerning the replacement of insulation blankets in aircraft cargo compartments. It addresses requirements related to the maintenance and replacement of these specific furnishings to ensure safety and compliance. The document does not specify particular aircraft types or engine models affected.

Boeing 767

EASA AD US-2024-15-05

Electrical Power - Electrical Support Bracket - Installation / Wire Bundles - Re-installation

Electrical Power - Electrical Support Bracket - Installation / Wire Bundles - Re-installation is a regulatory document addressing the installation and re-installation procedures for electrical support brackets and wire bundles in aircraft electrical power systems. The document aims to ensure proper mounting and secure wiring to maintain electrical system integrity and safety. No specific aircraft types, engine models, or part numbers are mentioned in the document.

Boeing 767

EASA AD ISR-I-34-2024-07-1

Pitot-Static tubing improper rerouting after aircraft conversion from PAX to Freighter

Airworthiness Directive ISR I-34-2024-07-1 issued by the Civil Aviation Authority of Israel addresses improper rerouting of pitot-static tubing after conversion of Boeing 767-300 aircraft from passenger to freighter configuration. This directive applies to aircraft with the CAAI STC SA-218 modification installed, affecting the pitot and static system tubing connected to the first officer's Air Data Computer. The issue involves potential water traps in specific flexible hoses and rigid tubes that may impair system functionality.

Airworthiness Directive

Boeing 767300
Israel Aerospace Industries CAA Israel STC SA218

EASA AD US-2024-05-03

Fuselage - Forward Entry Door and Service Door Cutout Aft Lower Corner Fuselage Skin and Bear Strap - Repetitive Inspections

Fuselage - Forward Entry Door and Service Door Cutout Aft Lower Corner Fuselage Skin and Bear Strap - Repetitive Inspections is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2024-05-03) that applies to certain Boeing Model 767 airplanes. It addresses the detection of cracks in the aft lower corner fuselage skin and bear strap near the forward entry and service door cutouts. The directive mandates repetitive inspections and necessary corrective actions to maintain structural integrity.

Airworthiness Directive

Boeing 767

EASA AD 2024-0069-E

Engine — High Pressure Compressor / Stage 1 and 2 Rotor Path Liners — Inspection

EASA Airworthiness Directive 2024-0069-E is an emergency directive addressing inspection requirements for the high pressure compressor stage 1 and 2 rotor path liners on Rolls-Royce Deutschland RB211-524H-36 and RB211-524H-T-36 engines, commonly installed on Boeing 767 aircraft. The directive mandates borescope inspections to detect potential damage that could lead to engine surges and dual engine shutdown. It applies to all manufacturer serial numbers of the affected engines.

Airworthiness Directive

Rolls-Royce Deutschland Ltd & Co Kg RB211-524
Boeing 767

EASA AD US-2023-13-12

Oxygen - Chemical Oxygen Generators - Replacements

The Federal Aviation Administration's Airworthiness Directive 2023-13-12 addresses premature aging of certain passenger chemical oxygen generators installed on various Boeing aircraft models including the 737 series (100 through 900ER), 757 series, and 767 series airplanes. This final rule mandates repetitive replacement of affected chemical oxygen generators and restricts installation of certain parts to ensure safety during emergencies. The directive aims to prevent failure of oxygen generators to activate, which could jeopardize occupant safety.

Airworthiness Directive

Boeing 737
Boeing 757
Boeing 767

EASA SIB SAFO23004

Erroneous Maximum Takeoff Weight Calculation from Boeing Performance Engineer's Tool Reporters

The document titled 'Erroneous Maximum Takeoff Weight Calculation from Boeing Performance Engineer's Tool Reporters' is a Safety Alert for Operators (SAFO 23004) issued by the FAA. It addresses an issue affecting Boeing airplane models 737-200, 737-300, 737-400, 737-500, 747-200, 747-300, 747-400, 757-200, 767-200, and 767-300, where the Boeing Performance Engineer's Tool (PET) Reporters may calculate incorrect Maximum Takeoff Weight (MTOW) values. This error impacts takeoff performance calculations, particularly when using the Improved Climb feature, potentially leading to safety risks such as runway overruns or insufficient climb performance.

Safety Information Bulletin

Boeing 737
Boeing 747
Boeing 757
Boeing 767

EASA AD US-2023-13-09

[Correction] Limit Switch and Position Transmitter Module - Repetitive Inspections

Correction to Airworthiness Directive 2023-13-09 issued by the Federal Aviation Administration (FAA) addresses all Boeing Company Model 767 airplanes. The directive mandates repetitive inspections and maintenance actions on limit switch and position transmitter modules (LSPTMs) and associated electrical wiring to prevent malfunction of horizontal stabilizer trim switches. It also requires installation of additional drain holes on certain aircraft to mitigate water accumulation risks.

Airworthiness Directive

Boeing 767

EASA AD US-2023-12-23

Placards and Markings - First Observer Seat - Placard Installation / Airplane Flight Manual Revision

Federal Aviation Administration Airworthiness Directive 2023-12-23 is a final rule affecting certain Boeing Company Model 767-300F airplanes. It mandates the installation of placards in the flight deck to indicate the correct position of the first observer seat during taxi, takeoff, and landing, and requires revisions to the airplane flight manual. This directive addresses a safety issue related to improper installation of the first observer seat that could cause injury during emergency landings.

Airworthiness Directive

Boeing 767300F

EASA AD US-2023-12-12

Aircraft Flight Manual - Limitations / Operating Procedures - Amendment

The Aircraft Flight Manual - Limitations / Operating Procedures - Amendment is a final rule issued by the Federal Aviation Administration (FAA) addressing Boeing Model 757 and 767 airplanes. This amendment supersedes previous airworthiness directives and updates the airplane flight manual (AFM) to include specific operating procedures related to interference from 5G C-Band wireless broadband signals affecting radio altimeters and related systems.

Airworthiness Directive

Boeing 757
Boeing 767

EASA AD 2021-0234R1

Information Systems — Electronic Flight Bag Universal Serial Bus Receptacle — Modification

EASA Airworthiness Directive 2021-0234R1 is a regulatory update addressing the modification of Electronic Flight Bag (EFB) Universal Serial Bus (USB) receptacles installed on various aircraft including Fokker F27 and F28 models, Airbus A318 through A340 series, ATR42 and ATR72, Boeing 737 through 777 models, Bombardier CL-600 series, and De Havilland Canada DHC-8 aircraft. The directive mandates modifications to affected USB receptacles to prevent overheating and potential smoke or fumes in the cockpit. This AD applies to specific manufacturer serial numbers as detailed in the directive's appendix.

Airworthiness Directive

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-0146
Fokker CRR-0185
Fokker CRR-0186
Fokker CRR-0190
Fokker CRR-0206
Fokker CRR-0210
Fokker CRR-0241
Fokker CRR-0265
Fokker CRR-0290
Fokker CRR-0300
Fokker CRR-0309
MHI RJ Aviation CL-600 (Regional Jet)
Fokker F27
Fokker F28
Boeing 747
Bombardier CL-600

EASA AD 2022-0237

Engine — Low Pressure Turbine Stage 1 Discs — Life Reduction

EASA Airworthiness Directive 2022-0237 is an airworthiness directive addressing life reduction for Low Pressure Turbine Stage 1 discs on Rolls-Royce RB211-524 series engines. These engines are commonly installed on Boeing 747 and Boeing 767 aircraft. The directive mandates updated life limits and removal requirements for specific turbine discs to ensure continued airworthiness and safety.

Airworthiness Directive

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