AD 2003-18-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 757 | Airworthiness Directives; Boeing Model 757 Series Airplanes Powered by Pratt & Whitney Engines |
Unsafe Condition
Fatigue cracking in primary strut structure and consequent reduced structural integrity of the strut.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the nacelle strut and wing structure on both sides of the airplane in accordance with Boeing Service Bulletin 757-54-0034 or Revision 1. Accomplish the actions specified in Boeing Service Bulletins 757-54-0027 and 757-54-0036 as applicable. Repair any damage to airplane structure found during the modification, as required.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 3,000 flight cycles after November 13, 2000, or prior to the accumulation of 37,500 total flight cycles, or within 20 years since the date of manufacture, whichever occurs first.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 757 series airplanes powered by Pratt & Whitney engines, line numbers 1 through 735 inclusive, 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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.