AD 2006-15-18

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 737-300, -400, -500, -600, -700, -700C, -800, and -900 Series Airplanes

AD Number
2006-15-18
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2004-19245
FR Citation
71 FR 43037

Applicability

TypeManufacturerModelDetails
aircraft Boeing 737-300 Airworthiness Directives; Boeing Model 737-300, -400, -500, -600, -700, -700C, -800, and -900 Series Airplanes

Unsafe Condition

The master dim and test system circuit does not have wiring separation of the test ground signal for redundant equipment in the flight compartment.

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

Required Actions

Modify the wiring for the master dim and test system. For certain airplanes, perform related concurrent actions as necessary.

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

Compliance Time

Within 48 months after the effective date of this AD.

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

Affected Aircraft

Boeing Model 737-300, -400, -500, -600, -700, -700C, -800, and -900 series airplanes, as identified in Boeing Special Attention Service Bulletin 737-33-1132, Revision 2, and Boeing Service Bulletin 737-33-1133, Revision 3, dated September 8, 2005.

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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