AD 95-06-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 737-200 Series | Airworthiness Directives; Boeing Model 737-200 and -300 Series Airplanes |
| aircraft | The Boeing Company | 737-300 Series | Airworthiness Directives; Boeing Model 737-200 and -300 Series Airplanes |
Unsafe Condition
Fatigue cracking in the fuselage frames below the lower jamb of the main deck cargo door between stringers 20L and 21L at water line 180 at frame stations 380, 400, 420, 440, 460, and/or 480, which may initiate at the radius of the frame webs modified under STC SA2969SO.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a detailed close visual inspection to detect cracking of the fuselage frames below the lower jamb of the upper deck main cargo door between stringers 20L and 21L at water line 180, and repair any cracking found, in accordance with Pemco Alert Service Letter 737-53-0004.
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Compliance Time
Within 50 flight cycles after the effective date of this AD or within 50 flight cycles after the installation of STC SA2969SO, whichever occurs later.
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Affected Aircraft
Boeing Model 737-200 and -300 series airplanes equipped with main deck cargo doors installed in accordance with supplemental type certificate (STC) SA2969SO.
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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