EASA Regulations for Learjet 60

7 airworthiness directives and regulations affecting Learjet 60.

Get the next one by email

New ADs and bulletins for Learjet 60, summarized like the ones below, every Monday.

EASA SIB SAIB-2026-07

Mar 23, 2026

Main Landing Gear Attach Section - Trunnion Pins

The FAA Special Airworthiness Information Bulletin SAIB: 2026-07 addresses the potential improper installation of the aft trunnion pin in the main landing gear of Learjet Model 23, 24, 25, 28, 29, 31, 35, 36, 55, and 60 airplanes. This bulletin informs owners, operators, and maintainers about the risk of main landing gear collapse during taxi, takeoff, or landing due to this issue. It provides recommended inspections and maintenance manual revisions to mitigate the risk.

Safety Information Bulletin
  • Learjet, 23
  • Learjet, 24
  • Learjet, 25
  • Learjet, 28
  • Learjet, 29
  • Learjet, 31
  • Learjet, 35
  • Learjet, 36
  • Learjet, 55
  • Learjet, 60
  • Learjet 23
  • Learjet 24
  • Learjet 25
  • Learjet 28
  • Learjet 29
  • Learjet 31
  • Learjet 35
  • Learjet 36
  • Learjet 55
  • Learjet 60

EASA AD US-2022-05-01

Feb 24, 2022

Wings - Spoiler Assemblies - Removal

Federal Register Volume 87, Number 35 (February 22, 2022) - Airworthiness Directive 2022-05-01 issued by the FAA addresses certain Learjet, Inc. airplanes including Models 35, 35A (C-21A), 36, 36A, 55, 55B, 55C, and 60. This directive targets spoiler assemblies that had their FAA-approved life limits improperly extended by a repair station, posing a safety risk. The AD mandates removal of these spoiler assemblies from service and prohibits their reinstallation to ensure continued airworthiness.

Airworthiness Directive
  • Learjet, 31
  • Learjet, 35
  • Learjet, 36
  • Learjet, 55
  • Learjet, 60
  • Learjet 35
  • Learjet 35A
  • Learjet 36
  • Learjet 36A
  • Learjet 55
  • Learjet 55B
  • Learjet 55C
  • Learjet 60

EASA AD US-2020-11-04

Jun 22, 2020

Engine Exhaust - Thrust Reverser Voice Command Warning System - Installation

Federal Register Volume 85, Number 99 (May 21, 2020) is a final rule airworthiness directive issued by the FAA addressing certain Learjet Inc. Model 60 airplanes. It mandates the installation of a thrust reverser Voice Command Warning System (VCWS) to alert flight crews of thrust reverser malfunctions that could cause unintended acceleration during reverse thrust commands.

Airworthiness Directive
  • Learjet, 60
  • Learjet 60

EASA AD US-2019-17-01

Oct 1, 2019

Fuselage - Upper Fuselage Skin - Inspection / Repair

Federal Register Airworthiness Directive 2019-17-01 is a final rule issued by the FAA addressing certain Learjet, Inc. Model 60 airplanes. It mandates inspections and repairs of the upper fuselage skin to detect and correct corrosion that could compromise structural integrity. This directive updates previous requirements by clarifying inspection areas and compliance times.

Airworthiness Directive
  • Learjet, 60
  • Learjet 60

EASA AD US-2018-19-04

Sep 20, 2018

Flight Controls - Flap Nose Roller Fitting, Nose Roller Support Bracket, and Adjacent Rib Support Structure - Replacement

Federal Aviation Administration Airworthiness Directive 2018-19-04 is a final rule addressing certain Learjet, Inc. Models 28, 29, 31, 31A, 35, 35A, 36, 36A, 55, 55B, 55C, and 60 airplanes. The directive mandates replacement of the flap nose roller fitting, nose roller support bracket, and adjacent rib support structure with improved components to prevent fatigue cracks caused by repetitive flap loads.

Airworthiness Directive
  • Learjet, 28
  • Learjet, 29
  • Learjet, 31
  • Learjet, 35
  • Learjet, 36
  • Learjet, 55
  • Learjet, 60
  • Learjet 28
  • Learjet 29
  • Learjet 31
  • Learjet 31A
  • Learjet 35
  • Learjet 35A
  • Learjet 36
  • Learjet 36A
  • Learjet 55
  • Learjet 55B
  • Learjet 55C
  • Learjet 60

EASA SIB NM-12-25

Apr 20, 2012

Hawker Beechcraft 400/400A and Learjet 60 Aeroplanes — Rockwell Collins Altitude Awareness Panel 115VAC Power Transient Failures

The Special Airworthiness Information Bulletin SAIB: NM-12-25 is an FAA informational bulletin addressing 115VAC power transient failures in Rockwell Collins Altitude Awareness Panels installed on Hawker Beechcraft 400/400A and Learjet 60 airplanes. It informs operators about issues related to the AAP-850 and AAP-851 altitude awareness panels that may cause smoke in the cockpit due to a varistor protection device failure. The bulletin provides guidance but does not mandate corrective action.

Safety Information Bulletin
  • Hawker Beechcraft 400
  • Hawker Beechcraft 400A
  • Learjet 60

EASA SIB 2008-07R1

Mar 19, 2008

WITHDRAWN - TRANSPORT CANADA AD CF-2008-08R1 HAS BEEN ADOPTED BY EASA

The document titled WITHDRAWN - TRANSPORT CANADA AD CF-2008-08R1 HAS BEEN ADOPTED BY EASA is an EASA Safety Information Notice No. 2008-07 R1 issued on 2008-03-19. It addresses the identification and removal from service of low pressure (LP) compressor fan blades on Pratt & Whitney Canada PW305A and PW305B engines, which are installed on aircraft including the Hawker Beechcraft BAe125-1000A, BAe125-1000B, Hawker 1000, and Learjet 60. The notice informs stakeholders about the adoption of Transport Canada Airworthiness Directive CF-2008-08R1 by EASA and provides relevant safety information.

Safety Information Bulletin
  • Hawker Beechcraft BAe125-1000A
  • Hawker Beechcraft BAe125-1000B
  • Hawker 1000
  • Learjet 60