AD 84-19-06

final rule
Data completeness: 70%

Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes

AD Number
84-19-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Learjet Inc. 24 Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes
aircraft Learjet Inc. 24A Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes
aircraft Learjet Inc. 24B Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes
aircraft Learjet Inc. 24B-A Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes
aircraft Learjet Inc. 24C Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes
aircraft Learjet Inc. 24D Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes
aircraft Learjet Inc. 24D-A Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes
aircraft Learjet Inc. 24E Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes
aircraft Learjet Inc. 24F Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes
aircraft Learjet Inc. 24F-A Airworthiness Directives; Gates Model 24, 25, 28, 29, 35, 36 and 55 Series Airplanes

Unsafe Condition

Aileron/trim tab flutter due to a failure or disconnect of the tab control system

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace the trim tab balance weight and rebalance the left aileron in accordance with specified modification kits. Special flight permits may be issued under FAR 21.197 to operate to a base for compliance. Alternate means of compliance may be approved by the Manager, Wichita Aircraft Certification Office.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within the next 600 hours time in service, or the next aileron/trim tab removal or rebalance, whichever occurs first

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Gates Learjet Models 24 (serials 100-357), 25 (003-369), 28 (001-005), 29 (001-004), 35 (001-514), 36 (001-053), and 55 (001-105)

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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