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2018-10-15
article
Airworthiness Directives; The Boeing Company Airplanes
Proposed Rules
D09002ee1bdb85774
D09002ee1bdb857d5
United States
Department of Transportation
originator
org
United States Government Agency or Subagency
United States
Federal Aviation Administration
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org
United States Government Agency or Subagency
We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD was prompted by reports that frame web and frame integral inboard chord cracking is occurring on multiple airplanes in multiple locations below the passenger floor. This proposed AD would require repetitive detailed, general visual, and high frequency eddy current (HFEC) inspections of the section 43 lower lobe frames at certain stations; an inspection to determine if certain repairs are installed; and applicable on-condition actions. We are proposing this AD to address the unsafe condition on these products.
83 FR 52171
https://www.govinfo.gov/app/details/FR-2018-10-16/2018-22277
2018-22277
fr16oc18-19
RIN 2120-AA64
4910-13-P
Docket No. FAA-2018-0901
Product Identifier 2018-NM-114-AD
https://www.govinfo.gov/app/details/FR-2018-10-16/2018-22277
https://www.govinfo.gov/content/pkg/FR-2018-10-16/html/2018-22277.htm
https://www.govinfo.gov/content/pkg/FR-2018-10-16/pdf/2018-22277.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
52171
52173
83 FR 52171
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes; Federal Register Vol. 83, Issue
PRORULE
2018-22277
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2018-11-30
Docket No. FAA-2018-0901
Product Identifier 2018-NM-114-AD
4910-13-P
2018-22277
Notice of proposed rulemaking (NPRM).
We propose to adopt a new airworthiness directive (AD) for certain The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes. This proposed AD was prompted by reports that frame web and frame integral inboard chord cracking is occurring on multiple airplanes in multiple locations below the passenger floor. This proposed AD would require repetitive detailed, general visual, and high frequency eddy current (HFEC) inspections of the section 43 lower lobe frames at certain stations; an inspection to determine if certain repairs are installed; and applicable on-condition actions. We are proposing this AD to address the unsafe condition on these products.
We must receive comments on this proposed AD by November 30, 2018.
Lu Lu, Aerospace Engineer, Airframe Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3525; email: lu.lu@faa.gov.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
The Boeing Company Airplanes
,
9-ANM-LAACO-AMOC-Requests@faa.gov
george.garrido@faa.gov
lu.lu@faa.gov
http://www.regulations.gov
https://www.myboeingfleet.com
Federal Register
Vol. 83, no. 200
Office of the Federal Register, National Archives and Records Administration
2018-10-16
continuing
daily
deposited
born digital
199 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2018-10-16
P0b002ee19d59a9cf
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr16oc18
https://www.govinfo.gov/app/details/FR-2018-10-16
https://www.govinfo.gov/content/pkg/FR-2018-10-16/pdf/FR-2018-10-16.pdf
https://www.govinfo.gov/content/pkg/FR-2018-10-16/xml/FR-2018-10-16.xml
fdlp
52115
52304
DGPO
2018-10-15
2023-04-28
FR-2018-10-16
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FR-2018-10-16
83
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