AD 99-17-05

final rule
Data completeness: 70%

Airworthiness Directives; Israel Aircraft Industries, Ltd., Model Astra SPX Series Airplanes

AD Number
99-17-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
99-NM-204-AD
FR Citation
Federal Register: August 17, 1999 (Volume 64, Number 158)

Applicability

TypeManufacturerModelDetails
aircraft Gulfstream Aerospace LP Astra SPX Airworthiness Directives; Israel Aircraft Industries, Ltd., Model Astra SPX Series Airplanes

Unsafe Condition

Cracking of the main fuel tube assemblies of the left and right engines at the base of the 'T' joint weld (fuel pressure switch boss), which could result in fuel line fractures and consequent in-flight engine shutdowns or an increased risk of engine nacelle fires.

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

Required Actions

Perform a fluorescent penetrant inspection within 5 hours time-in-service after the effective date to detect cracking around the bases of the 'T' joint welds. Repeat inspections at intervals not exceeding 25 hours time-in-service. Replace the fuel tube assembly with a new or serviceable part before further flight if any crack is detected.

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

Compliance Time

Within 5 hours time-in-service after the effective date

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

Affected Aircraft

Model Astra SPX series airplanes, serial numbers 089 through 115 inclusive

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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