AD 2007-03-07

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 737 Airplanes

AD Number
2007-03-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-26323
FR Citation
72 FR 4625

Applicability

TypeManufacturerModelDetails
aircraft Boeing 737 Airworthiness Directives; Boeing Model 737 Airplanes

Unsafe Condition

Failure of one of the two input control rods of the main rudder power control unit (PCU), which could result in reduced controllability of the airplane; and failure of any combination of two input control rods of the main rudder PCU and/or standby rudder PCU, which could cause an uncommanded rudder hardover event and result in loss of control of the airplane.

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

Required Actions

Install a new rudder control system and make changes to adjacent systems. Perform repetitive tests of the force fight monitor of the main rudder PCU and the standby hydraulic actuation system, followed by corrective action. Replace both input control rods of the main rudder PCU and the input control rod of the standby rudder PCU with new input control rods. For certain airplanes, install an enhanced rudder control system in accordance with new service information.

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

Compliance Time

Before further flight

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

Affected Aircraft

All Boeing Model 737 airplanes, with specific actions depending on the configuration and service history of the airplane.

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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