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-09.23.24

Airborne-NextGen-10.01.24

Airborne-Unlimited-10.02.24

Airborne-AffordableFlyers-10.03.24

Airborne-Unlimited-09.27.24

Sun, Jul 04, 2010

AD: Boeing

AD NUMBER: 2010-14-07

MANUFACTURER: The Boeing Company Model 747 Airplanes
SUBJECT: Airworthiness Directive 2010-14-07

SUMMARY: The FAA is superseding an existing airworthiness directive (AD), which applies to certain Model 747 airplanes. That AD currently requires repetitive inspections of the body station (BS) 2598 bulkhead, and corrective actions if necessary. That AD also currently requires a terminating modification for certain repetitive inspections and a post- modification inspection of the modified area. This new AD continues to require those actions using revised service information. For certain airplanes, this AD requires new repetitive inspections, an interim modification, and post-interim modification inspections. For certain airplanes, this AD requires replacing any previously repaired aft inner chord and reinstalling the terminating modification. For airplanes that are converted to the Model 747-400 large cargo freighter (LCF) configuration, this new AD reduces the threshold and repeat intervals of certain post-modification inspections. For all airplanes, this new AD also requires certain inspections of the upper aft outer chords and diagonal brace attachment fittings, flanges, and rods to continue after the terminating modification. This AD results from reports of cracked aft inner chords on airplanes after certain requirements of the existing AD were done. The FAA is issuing this AD to prevent fatigue cracking of the BS 2598 bulkhead structure, which could result in inability of the structure to carry horizontal stabilizer flight loads, and loss of controllability of the airplane.

FMI: http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAD.nsf/0/E9BDB3585682700086257753005E0EF8?OpenDocument

Advertisement

More News

ANN's Daily Aero-Linx (09.29.24)

Aero Linx: The Great War Aviation Society Over the past 50 years, we’ve built a thriving community of over 1,000 members based in over 25 countries around the world. The Grea>[...]

ANN's Daily Aero-Term (09.29.24): Go Around

Go Around Instructions for a pilot to abandon his/her approach to landing. Additional instructions may follow. Unless otherwise advised by ATC, a VFR aircraft or an aircraft conduc>[...]

ANN's Daily Aero-Linx (09.30.24)

Aero Linx: American Aviation Historical Society AAHS is dedicated to the preservation and dissemination of the rich heritage of American aviation. Our purpose is to collect, preser>[...]

NTSB Final Report: Piper PA46

Review Of The Pilot’s Logbook Revealed That He Had About 47 Total Hours Of Flight Experience, With About 4 Hours Of Instruction In Simulated Instrument Conditions Analysis: T>[...]

Aero-News: Quote of the Day (09.30.24)

“The loss of any service member is an absolute tragedy, but the conversation surrounding the V-22 Osprey has become disproportionately negative, often overlooking key facts a>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC