AD: Boeing | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-12.08.25

AirborneNextGen-
12.09.25

Airborne-Unlimited-12.10.25

Airborne-AffordableFlyers-12.11.25

AirborneUnlimited-12.12.25

AFE 2025 LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Wed, Apr 16, 2008

AD: Boeing

AD NUMBER: 2008-08-10
MANUFACTURER: Boeing
SUBJECT: Airworthiness Directive 2008-08-10
SUMMARY:
We are adopting a new airworthiness directive (AD) for all Boeing Model 737-100, -200, -200C,-300, -400, and -500 series airplanes. For certain airplanes, this AD requires replacing the outboard stabilizing fitting and certain adjacent components of the main landing gear (MLG)support beam. This AD also requires repetitive inspections for discrepancies of the outboard stabilizing fitting, walking beam hanger, and rear spar attachment, and corrective actions if necessary. For certain airplanes, this AD provides an alternative one-time inspection of the outboard stabilizing fitting for discrepancies, and corrective actions if necessary, which would extend the compliance time for the replacement of the outboard stabilizing fitting. For certain other airplanes, this AD also requires performing a torque check of the aft pin of the outboard stabilizing fitting, and corrective actions if necessary. This AD results from reports of findings of fatigue cracking of the outboard stabilizing fitting and stress corrosion cracking of the bolts attaching the fitting to the wing rear spar. We are issuing this AD to detect and correct that cracking, which could result in disconnection of the MLG actuator from the rear spar and support beam, consequent damage to the hydraulic system, and possible loss of the 'A' and 'B' hydraulic systems and damage or jamming of the flight control cables. Damage or jamming of the flight control cables could result in loss of control of the airplane.

FMI: www.faa.gov/regulations_policies/airworthiness_directives/

Advertisement

More News

ANN's Daily Aero-Term (12.13.25): Light Gun

Light Gun A handheld directional light signaling device which emits a brilliant narrow beam of white, green, or red light as selected by the tower controller. The color and type of>[...]

Aero-News: Quote of the Day (12.13.25)

“We have performed extensive ground testing by comparing warm up times, full power tethered pulls, and overall temperatures in 100 degree environments against other aircraft >[...]

NTSB Final Report: Gippsland GA-8

While Taxiing To Parking The Right Landing Gear Leg Collapsed, Resulting In Substantial Damage Analysis: The pilot made a normal approach with full flaps and landed on the runway. >[...]

Classic Aero-TV: Historically Unique -- Marlin Horst's Exquisite Fairchild 71

From 2014 (YouTube Edition): Exotic Rebuild Reveals Aerial Work Of Art During EAA AirVenture 2014, ANN's Michael Maya Charles took the time to get a history lesson about a great ai>[...]

Airborne 12.12.25: Global 8000, Korea Pilot Honors, AV-30 Update

Also: Project Talon, McFarlane Acquisition, Sky-Tec Service, JPL Earth Helo Tests Bombardier has earned a round of applause from the business aviation community, celebrating the fo>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC