AD: The Boeing Company Airplanes | 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-05.12.25

Airborne-NextGen-05.13.25

AirborneUnlimited-05.14.25

Airborne-FlightTraining-05.15.25

AirborneUnlimited-05.16.25

Sat, Jul 17, 2021

AD: The Boeing Company Airplanes

AD 2021-13-10 Requires Repetitive Inspections For Any Existing Repair Of The Wing Lower Skin Fuel Tank...

The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 777 airplanes.

This AD was prompted by reports indicating that during investigation of a fuel leak, fatigue cracking was found on the forward inboard side of the fuel tank access door cutouts on the left and right lower wing skin. The cause of the cracking is attributed to corrosion damage. This AD requires repetitive inspections for any existing repair of the wing lower skin fuel tank and dry bay access door cutouts on the left and right lower wing skin, and applicable on-condition actions. The FAA is issuing this AD to address the unsafe condition on these products. This AD is effective August 19, 2021.

Supplementary Information: The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain The Boeing Company Model 777 airplanes. The NPRM published in the Federal Register on November 18, 2020 (85 FR 73430). The NPRM was prompted by reports indicating that during investigation of a fuel leak, fatigue cracking was found on the forward inboard side of the fuel tank access door cutouts on the left and right lower wing skin. The cause of the cracking is attributed to corrosion damage.

In the NPRM, the FAA proposed to require repetitive inspections for any existing repair of the wing lower skin fuel tank and dry bay access door cutouts on the left and right lower wing skin, and applicable on-condition actions. The FAA is issuing this AD to address fatigue cracking, which could result in the inability of a principal structural element to sustain limit load, and consequent reduced structural integrity of the airplane.

FMI: www.regulations.gov

Advertisement

More News

Aero-News: Quote of the Day (05.20.25)

“From the beginning, the RV-15X’s performance has been very good, as reported and demonstrated in videos. However, we’ve continued to work hard to achieve the con>[...]

ANN's Daily Aero-Term (05.20.25): Handoff

Handoff An action taken to transfer the radar identification of an aircraft from one controller to another if the aircraft will enter the receiving controller's airspace and radio >[...]

ANN's Daily Aero-Linx (05.20.25)

Aero Linx: The de Havilland Moth Club Ltd The de Havilland Moth Club evolved from a belief that an association of owners and operators of Moth aeroplanes should be formed to create>[...]

Airborne-NextGen 05.20.25: Drone Regs, Zero-Emission Cargo, Door-Dash Drone

Also: Blackhawk’s Replacement, Supersonic Flight, Archer 1Q/25, Long-Range VTOL Program U.S. Secretary of Transportation Sean P. Duffy released an update on progress being ma>[...]

Airborne 05.19.25: Kolb v Tornados, Philippine Mars, Blackhawk Antler Theft

Also: Tentative AirVenture Airshow Lineup, Supersonic Flight Regs, Private Pilot Oral Exam Guide, Boeing Deal The sport aircraft business can be a tough one... especially when Moth>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

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