AD 2000-14-07

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 727 Series Airplanes

AD Number
2000-14-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-NM-75-AD
FR Citation
65 FR 43228

Applicability

TypeManufacturerModelDetails
aircraft Boeing 727 Airworthiness Directives; Boeing Model 727 Series Airplanes

Unsafe Condition

Cracking of the rear spar web, which could permit fuel leakage into the airflow multiplier, and could result in an electrical short that could cause a fire.

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

Required Actions

Accomplish inspections to detect cracking of the rear spar web or fuel leakage of the wing center section, using either a visual inspection with a borescope or mirror, or an ultrasonic and high frequency eddy current (HFEC) inspection. Repair any detected cracking or fuel leakage prior to further flight, in accordance with the specified service bulletins.

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

Compliance Time

Within 300 flight cycles after December 27, 1997, or prior to the accumulation of 15,000 total flight cycles, whichever occurs later.

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

Affected Aircraft

Boeing Model 727 series airplanes with line numbers 858 through 864, 867 through 869, 872 through 883, and 885 through 1832, certificated in any category.

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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View Official Source ↗ Find More ADs for Boeing 727

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