Federal Register
Information
[Federal Register Volume 78, Number 72 (Monday, April 15, 2013)]
[Pages 22182-22185]
[Federal Register Volume 78, Number 72 (Monday, April 15, 2013)]
[Pages 22182-22185]
Header
Information
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0933; Directorate Identifier 2012-NM-107-AD;
Amendment 39-17411; AD 2013-07-07]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
PDF Copy (If Available):
2013-07-07.pdf
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2012-0933; Directorate Identifier 2012-NM-107-AD;
Amendment 39-17411; AD 2013-07-07]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
PDF Copy (If Available):
2013-07-07.pdf
SUMMARY:
We are adopting a new airworthiness directive (AD) for all The Boeing Company
Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes. This AD was prompted by
reports of an incorrect procedure used to apply the wear and corrosion protective surface coating to
attach pins of the horizontal stabilizer rear spar. This AD requires inspecting to determine the part
number of the attach pins of the horizontal stabilizer rear spar, and replacing certain attach pins with
new, improved attach pins. We are issuing this AD to prevent premature failure of the attach pins,
which could cause reduced structural integrity of the horizontal stabilizer to fuselage attachment,