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86-22-05: Flap Sector Mounting Brackets Inspection

FAA order 86-22-05 is an airworthiness directive in force since November 10, 1986. The FAA's subject line: Flap Sector Mounting Brackets Inspection. It names Learjet 23, Learjet 24, Learjet 25, Learjet 35, Learjet 55: about 273 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Learjet Inc.
Models
23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 35, 35A (C-21A), 36, 36A, 55, 55B, 55C
On this site
Learjet 23 6 registered
Learjet 24 16 registered
Learjet 25 23 registered
Learjet 35 161 registered
Learjet 55 67 registered

Dates and paperwork

In force since
November 10, 1986
Docket
Unknown
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (2,498 characters)
86-22-05 GATES LEARJET: Amendment 39-5448. Applies to the following Gates Learjet series airplanes, models/serial number listed below, certificated in any category. MODEL SERIAL NUMBER 23 003 thru 089 (if equipped with dual flap actuators) 23 090 thru 099 24 100 thru 357 25 003 thru 373 28 001 thru 005 29 001 thru 004 35 002 thru 545, 589 thru 598 36 001 thru 053, and 055 55 001 thru 121 Compliance required as indicated, unless previously accomplished. To prevent impairment of flap operation, an asymmetric flap condition, false gear warning horn signals, or incorrect biasing of the stall warning system, due to flap sector upper mount bracket failures, accomplish the following: A. Within the next 50 hours time-in-service after the effective date of this AD, inspect the flap sector upper mounting brackets for cracks, in accordance with instructions in Gates Learjet Corporation Airplane Modification Kit (AMK) 86-4 or 55-86-2, as applicable. 1. If cracks are found in either the left-hand or right-hand flap sector upper mounting brackets (Figure I of AMK), prior to further flight, replace both brackets and install stiffeners in accordance with the applicable AMK. 2. If cracks are not found in the flap sector upper mounting brackets, replace the brackets and install stiffeners in accordance with the applicable AMK within 100 hours time-in-service after the effective date of this AD. B. If both flap sector upper mounting brackets have been previously replaced with steel brackets, compliance with this AD is not required. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD. D. Alternate means of compliance with this AD, which provides an acceptable level of safety, may be used when approved by the Manager, Wichita Aircraft Certification Office, FAA, Central Region. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Gates Learjet Corporation, P.O. Box 7707, Wichita, Kansas 67277. These documents may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or FAA, Central Region, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Wichita, Kansas. This supersedes AD 84-20-06, Amendment 39-4908. This amendment becomes effective November 10, 1986.

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
2011-08-22NM-11-48 · Ice and Rain Protection: Wing Transverse Duct Assembly
2004-05-06CE-04-67 ·

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 November 6, 2026. Connections as data: /graph/directive/86-22-05.json · aircraft systems.