AD 98-16-13

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747 Series Airplanes

AD Number
98-16-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-NM-210-AD
FR Citation
(Federal Register: August 03, 1998 (Volume 63, Number 148))

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 747-100 Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-100B Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-100B SUD Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-200B Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-200C Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-200F Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-300 Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-400 Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-400D Series Airworthiness Directives; Boeing Model 747 Series Airplanes
aircraft The Boeing Company 747-400F Series Airworthiness Directives; Boeing Model 747 Series Airplanes

Unsafe Condition

Missing fasteners from the splice fitting of the forward inner chord of the BS 2598 bulkhead could result in accelerated fatigue cracking of the inner chords, leading to inability of the structure to carry horizontal stabilizer flight loads and consequent reduced controllability of the airplane.

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

Required Actions

Perform a one-time visual inspection for missing fasteners of the splice fitting of the forward inner chord of the BS 2598 bulkhead. If fasteners are missing, perform corrective actions including detailed visual inspection, high frequency eddy current inspection for cracking of the forward and aft inner chords, repair if necessary, and install the fasteners.

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

Compliance Time

Required as indicated, unless accomplished previously.

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

Affected Aircraft

Boeing Model 747 series airplanes, line positions 1 through 1157; 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 8, 2026

Rights: U.S. Government Public Domain

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