EASA Regulations for Boeing 737-400

45 airworthiness directives and regulations affecting Boeing 737-400.

EASA AD US-2018-01-08

Fuselage - Frame Outboard Chord / Auxiliary Chord - Inspection

Federal Register Volume 83, Number 9 (2018-01-12) Final Rule Airworthiness Directive 2018-01-08 addresses all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates inspections for fatigue cracking in the frame outboard chord and the radius of the auxiliary chord, with required corrective actions if cracks are found. This directive aims to maintain structural integrity and prevent rapid decompression.

Jan 24, 2018

Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD US-2017-25-10

Stabilizers - Elevator Hinges - Inspections / Replacement

Federal Aviation Administration Airworthiness Directive 2017-25-10 is a final rule addressing all Boeing 737-100, -200, -200C, -300, -400, and -500 series airplanes. It mandates repetitive inspections, replacements, and tests of elevator hinge components and bearing plates to prevent potential disconnection of elevator hinges that could lead to horizontal stabilizer structural degradation. This directive aims to ensure continued airworthiness and safe flight by mitigating risks associated with bearing plate slider bushing wear.

Jan 18, 2018

Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD US-2017-24-05

[Correction] Wings - Upper Aft Skin - Inspection

Correction to Airworthiness Directive 2017-24-05 issued by the Federal Aviation Administration (FAA) affecting The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This directive addresses repetitive inspections and necessary repairs for cracking in the upper aft skin at the rear spar of the wings. The correction clarifies the applicability section regarding the affected airplane models.

Dec 22, 2017

Airworthiness DirectiveMaintenanceSafety MgmtBoeing 737Boeing 737-100Boeing 737-200Boeing 737-200CBoeing 737-300Boeing 737-400Boeing 737-500

EASA AD 2017-0149R1

Engine — Variable Stator Vane Actuating System — Check

EASA Airworthiness Directive 2017-0149R1 is a regulatory document addressing the CFM International CFM56-3 series engines installed on Boeing 737-300, -400, and -500 aircraft. It mandates repetitive checks of the variable stator vane (VSV) actuating system to detect corrosion-related issues that could cause loss of engine thrust control. The directive provides instructions for inspection, corrective actions, and optional terminating actions to ensure continued airworthiness.

Dec 5, 2017

Airworthiness DirectiveMaintenanceSafety MgmtCFM International CFM56-3Boeing 737-300Boeing 737-400Boeing 737-500

EASA SIB 2006-07R2

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.

Oct 2, 2006

Safety Information BulletinMaintenanceSafety MgmtBoeing 737-400