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2022-05-01: Spoilers

FAA order 2022-05-01 is an airworthiness directive in force since March 9, 2022. The FAA's subject line: Spoilers. It names Learjet 35, Learjet 55, Learjet 60: about 467 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Learjet Inc.
Models
35, 35A (C-21A), 36, 36A, 55, 55B, 55C, 60
On this site
Learjet 35 161 registered
Learjet 55 67 registered
Learjet 60 239 registered

Dates and paperwork

In force since
March 9, 2022
Published
February 22, 2022 (signed February 16, 2022)
Docket
FAA-2022-0144
Status
Current
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for certain Learjet, Inc., Model 35, 35A (C-21A), 36, 36A, 55, 55B, 55C, and 60 airplanes. This AD was prompted by a report indicating that a repair station approved Learjet spoiler assemblies for return to service after extending their life limit. This AD requires removing certain spoiler assemblies from service and prohibits their installation. The FAA is issuing this AD to address the unsafe condition on these products.

The order itself the regulatory text, as published

Show the full text (3,289 characters)
1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. 2. The FAA amends § 39.13 by adding the following new airworthiness directive: 2022-05-01 Learjet, Inc.: Amendment 39-21952; Docket No. FAA-2022-0144; Project Identifier AD-2022-00042-T. (a) Effective Date This airworthiness directive (AD) is effective March 9, 2022. (b) Affected ADs None. (c) Applicability This AD applies to Learjet, Inc., Model 35, 35A (C-21A), 36, 36A, 55, 55B, 55C, and 60 airplanes, certificated in any category, with any spoiler assembly that meets any of the criteria identified in paragraph (c)(1) or (2) of this AD. (1) The spoiler assembly's life limit was extended by Restored Aircraft Sales and Service, LLC. (2) The maintenance records related to the life limit for the spoiler assembly are missing or incomplete. (d) Subject Air Transport Association (ATA) of America Code 5755, Spoilers. (e) Unsafe Condition This AD was prompted by a report indicating that a repair station performed a life extension program on spoiler assemblies that had reached or were close to reaching their life limit. The FAA is issuing this AD to prevent use of a spoiler assembly beyond its FAA-approved life limit, which could lead to undetected cracking and consequent failure or separation of the spoiler assembly, resulting in a reduction or complete loss of control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Spoiler Assembly Removal For each spoiler assembly identified in paragraph (c) of this AD: Remove the spoiler assembly from service before further flight. (h) Parts Installation Prohibition As of the effective date of this AD, no person may install, on any airplane, a spoiler assembly identified in paragraph (c) of this AD. (i) Special Flight Permit Special flight permits, as described in 14 CFR 21.197 and 21.199, may be issued to operate the airplane to a location where the requirements of this AD can be accomplished, but concurrence by the Manager, Wichita ACO Branch, FAA, is required before issuance of the special flight permit. (j) Alternative Methods of Compliance (AMOCs) (1) The Manager, Wichita ACO Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or responsible Flight Standards Office, as appropriate. If sending information directly to the manager of the certification office, send it to the attention of the person identified in paragraph (k) of this AD. (2) Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office. (k) Related Information For more information about this AD, contact Tara Shawn, Aerospace Engineer, Airframe and Services Section, FAA, Wichita ACO Branch, 1801 Airport Road, Room 100, Wichita, KS 67209; phone: 316-946-4141; email: Tara.Shawn@faa.gov. (l) Material Incorporated by Reference None. Issued on February 16, 2022. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022-03805 Filed 2-17-22; 11:15 am]BILLING CODE 4910-13-P

Related safety bulletins advice on the same designs, not orders

2026-03-192026-07 · MAIN LANDING GEAR ATTACH SECTION, Trunnion Pins
2016-09-15NM-16-24 · Fuselage: Main Plate/Skin
2013-06-24NM-13-38 · Flight Controls Control Column Section
2012-04-16NM-12-25 · Auto Flight: Altitude Controller
2011-08-22NM-11-48 · Ice and Rain Protection: Wing Transverse Duct Assembly

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 7, 2026. Connections as data: /graph/directive/2022-05-01.json · aircraft systems.