Category Archives: Aircraft

Textron/Cessna 400 series Spar Eddy Current inspection

FAA AD2018-03-03

SUMMARY: We are adopting a new airworthiness directive (AD) for certain Textron Aviation Inc. Models 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A 421, 421A, 421B, 421C, and 425 airplanes. This AD requires repetitively inspecting the left and the right forward lower carry through spar cap for cracks and replacing the carry through spar if cracks are found. This AD was prompted by a report of a fully cracked lower forward carry through spar cap found on an affected airplane. We are issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective February 28, 2018.

The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of February 28, 2018.

We must receive comments on this AD by March 30, 2018.

FAA AD 2017-13-13 Boeing B737 Cracking

SUMMARY: We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This AD was prompted by reports of frame web cracking at certain locations. This AD requires repetitive inspections in certain locations of the frame web, and corrective action if necessary. We are issuing this AD to address the unsafe condition on these products.

http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/ab04cbeb1014787786258154005410b1/$FILE/2017-13-13.pdf

 

 

FAA AD 2017-13-07 Airbus Model A319, A320, and A321 series airplanes

SUMMARY: We are adopting a new airworthiness directive (AD) for all Airbus Model A319, A320, and A321 series airplanes. This AD was prompted by a report that a main landing gear (MLG) door could not be closed due to rupture of the actuator fitting. This AD requires repetitive inspections for cracking of the MLG door actuator fitting and its components, and corrective actions if necessary. This AD also requires eventual replacement of all affected MLG door actuator fittings with new monoblock fittings, which would terminate the repetitive inspections. We are issuing this AD to address the unsafe condition on these products. HFEC and LFEC NDT inspections

Link to FAA.gov

http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgad.nsf/0/bbaed0d56e8330798625815400541180/$FILE/2017-13-07.pdf