AD 2015-24-06

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes

AD Number
2015-24-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2015-6546
FR Citation
80 FR 75788

Applicability

TypeManufacturerModelDetails
aircraft Gulfstream Aerospace Corporation Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes

Unsafe Condition

Self-sealing couplings on the brake inlet fitting have been found backed out of the fully seated position, allowing the self-sealing mechanism to activate and cut off hydraulic pressure to the brake caliper, resulting in reduced or no braking ability on the affected wheel while the brake pressure indications remain normal.

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

Required Actions

Repetitive breakaway torque checks and torqueing of the brake inlet self-sealing couplings at intervals not to exceed 100 flight cycles. Revise the airplane flight manual to include procedures to follow in the event of certain display indications.

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

Compliance Time

Within 100 flight cycles

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Affected Aircraft

Gulfstream Aerospace Corporation Model GVI airplanes

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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