Airworthiness Directives; Boeing Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747SR, and 747SP Series Airplanes
airworthiness · Rule · Final rule. · Published 2003-12-23 · Effective 2004-01-27 · 68 FR 74167
Document
Document number
03-31195
Federal Register citation
68 FR 74167
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2003-12-23
Effective date
2004-01-27
FAA docket
Docket No. 2001-NM-180-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing airplane models, that requires a one-time inspection to identify all H-11 steel bolts installed in the latch fittings of the cargo doors, repetitive inspections for cracked or broken H-11 steel bolts, and follow-on and corrective actions if necessary. This amendment also requires eventual replacement of all H- 11 steel bolts in the latch fittings of the cargo doors with Inconel bolts. This action is necessary to prevent broken bolts in the latch fittings, which could reduce the capability of the door latch to keep the door closed, and result in loss of a cargo door and consequent rapid depressurization of the airplane. This action is intended to address the identified unsafe condition.