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-
12.02.25

Airborne-Unlimited-12.03.25

Airborne-FltTraining-12.04.25

AirborneUnlimited-12.05.25

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

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

NTSB Final Report: Patriot Aircraft LLC CX1900A

After Draining Both Wing Fuel Tanks, A Significant Amount Of Water Was Observed In The Right Wing Fuel Tank Analysis: The pilot, who was also the owner of the experimental amateur->[...]

Aero-News: Quote of the Day (12.06.25)

“Airbus apologises for any challenges and delays caused to passengers and airlines by this event. The Company thanks its customers, the authorities, its employees and all rel>[...]

ANN's Daily Aero-Term (12.06.25): High Speed Taxiway

High Speed Taxiway A long radius taxiway designed and provided with lighting or marking to define the path of aircraft, traveling at high speed (up to 60 knots), from the runway ce>[...]

ANN's Daily Aero-Linx (12.06.25)

Aero Linx: Taylorcraft Foundation, Inc. The Taylorcraft Foundation is exclusively organized for charitable, educational & scientific activities and will preserve the history an>[...]

Airborne-NextGen 12.02.25: Honda eVTOL, Arctus High-Alt UAS, Samson Patent

Also: USAF Reaper Accident, Baikonur Damage, Horizon eVTOL IFR/FIKI, New Glenn Update Honda has outlined its clearest timeline yet for its entry into the world of electric vertical>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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