AD: The Boeing Company Airplanes (737) | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Recent Daily Episodes

Episode Date

Monday

Tuesday

Wednesday

Thursday

Friday

Airborne On ANN

Airborne 01.16.17

Airborne 01.17.17

Airborne 01.11.17

Airborne 01.12.17

Airborne 01.13.17

Airborne Hi-Def On YouTube

Airborne 01.16.17

Airborne 01.17.17

Airborne 01.11.17

Airborne 01.12.17

Airborne 01.13.17

Thu, Jun 21, 2012

AD: The Boeing Company Airplanes (737)

AD NUMBER: 2012-12-05

PRODUCT: Certain Model 737-100, -200, -200C, -300, -400, and -500 series airplanes.
SUBJECT: Airworthiness Directive 2012-12-05
ACTION: Final Rule

SUMMARY: The FAA is superseding two existing airworthiness directives (ADs) for the products listed above. The first existing AD currently requires, for certain airplanes, repetitive inspections of the Station (STA) 348.2 frame to detect cracking under the stop fittings and intercostal flanges at stringers S-14L, S-15L, and S-16L, and corrective action if necessary. The second existing AD currently requires repetitive inspections to detect cracking of the intercostal webs, attachment clips, and stringer splice channels, and corrective action if necessary.

This new AD requires that the inspection for cracking under the stop fittings be done on additional airplanes; extends the repetitive interval for certain airplanes; adds a one-time inspection to detect missing fasteners; and updates or adds certain inspection and repair instructions. This new AD also requires, for certain airplanes, repetitive inspections of the cargo barrier net fitting for cracking, and repair if necessary. This new AD also adds, for certain airplanes, repetitive inspections for cracking of the stringer S-15L aft intercostal, and repair if necessary. This AD was prompted by reports of cracking of the STA 348.2 frame above the two outboard fasteners attaching the frame inner chord and door stop fittings, and in the outboard chord at stringer S-16L. We have also received reports of missing fasteners in the STA 348.2 frame inner chord.

The FAA is issuing this AD to detect and correct fatigue cracking of the intercostals on the forward and aft sides of the forward entry door cutout, which could result in loss of the forward entry door and rapid decompression of the airplane.

DATES: This AD is effective July 23, 2012.

FMI: AD

Advertisement

More News

Airborne 01.16.17: Dynon/EAA STC Expands, SpaceX, Chao Coy On ATC Privatization

Also: Project Titan, Part 23 Rule, SportAv HoF, Iran Air, FL's Space Coast, Galaxy Note7 Warnings, Boeing Employees When Dynon and EAA announced that they had worked together to ob>[...]

Airborne 01.16.17: Dynon/EAA STC Expands, SpaceX, Chao Coy On ATC Privatization

Also: Project Titan, Part 23 Rule, SportAv HoF, Iran Air, FL's Space Coast, Galaxy Note7 Warnings, Boeing Employees When Dynon and EAA announced that they had worked together to ob>[...]

Gone West: Astronaut Gene Cernan

Commander Of Apollo 17 Was The Last Man To Walk On The Moon Another icon of the space program has Gone West. Apollo 11 Commander Gene Cernan passed away Monday at the age of 82, ac>[...]

Airborne 01.13.17: G650ER Record Streak, False Drone Hit, Piper Archer Sale

Also: Parrot Layoffs, CES/AMA Expo/KSMO, 737 SAIB, Piper PA-31T, John Pope, Washington State, JetBlue Disturbance Pending sanctioning from the recognizing organizations, it looks l>[...]

ANN's Daily Aero-Linx (01.17.17)

All About Clouds If you sometimes have trouble differentiating between a stratocumulus and a billow cloud, this could be a site for you.>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2017 Web Development & Design by Pauli Systems, LC