AD 97-14-04

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes

AD Number
97-14-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-NM-29-AD
FR Citation
(Federal Register: June 30, 1997 (Volume 62, Number 125))

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 737-100 Series Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes
aircraft The Boeing Company 737-200 Series Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes
aircraft The Boeing Company 737-300 Series Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes
aircraft The Boeing Company 737-400 Series Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes
aircraft The Boeing Company 737-500 Series Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes

Unsafe Condition

Fracturing of the vernier control rod bolts due to the shank of the bolt running into the threads on the nutplate during installation, which could result in uncommanded movements of the rudder and consequent reduced controllability of the airplane.

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

Required Actions

Replace the main rudder power control unit (PCU) with newly designed units having specific part numbers, replace vernier control rod bolts with newly designed bolts, perform leak tests of the PCU at specified intervals, and revise the FAA-approved maintenance program to include the leak test requirements.

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

Compliance Time

Within 2 years after the effective date of this AD (August 4, 1997) for replacement actions, and leak tests must be performed within 4,000 flight hours after the effective date (for applicable airplanes) or within 6,400 flight hours after PCU replacement, with subsequent intervals not exceeding 6,400 flight hours.

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

Affected Aircraft

Boeing Model 737-100, -200, -300, -400, and -500 Series airplanes.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.