AD 71-23-02

final rule
Data completeness: 70%

Airworthiness Directives; GRUMMAN Model G-159 Airplanes

AD Number
71-23-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Gulfstream Aerospace Corporation G-159 Airworthiness Directives; GRUMMAN Model G-159 Airplanes

Unsafe Condition

Cracking in the wing to fuselage attachment fittings at butt line 9 due to deformation, gaps, or improper shimming in Grumman Model G-159 airplanes.

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

Required Actions

Inspect the wing to fuselage attachment fittings (P/Ns 159WM10064, 159WM10065, 159WM10223 assembly, and 159WM10045) at butt line 9 for cracks, deformation, gaps, or improper shimming within six months time in service after the effective date. If issues are found, correct them within 100 hours time in service using Aircraft Service Change 190 or an approved method.

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

Compliance Time

within six months time in service after the effective date of this AD

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

Affected Aircraft

Grumman Model G-159 airplanes

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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