United States Government Publishing Office
publisher
pbl
distributor
dst
United States
National Archives and Records Administration
Office of the Federal Register
author
aut
Government Organization
text
government publication
eng
FR
Regulatory Information
2016_register
executive
2018-02-07
article
Airworthiness Directives; International Aero Engines AG Turbofan Engines
Proposed Rules
D09002ee1bdc1d45c
D09002ee1bdc1d4f1
United States
Department of Transportation
originator
org
United States Government Agency or Subagency
United States
Federal Aviation Administration
originator
org
United States Government Agency or Subagency
We propose to adopt a new airworthiness directive (AD) for certain International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2525- D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines. This proposed AD was prompted by the fracture of the high-pressure turbine (HPT) stage 2 hub during flight, which resulted in an in-flight shutdown (IFSD), undercowl fire, and smoke in the cabin. This proposed AD would require inspecting the HPT stage 1 hub and HPT stage 2 hub, and, if necessary, their replacement with parts that are eligible for installation. We are proposing this AD to prevent failure of the HPT stage 1 or HPT stage 2 hubs, which could result in uncontained HPT blade release, damage to the engine, and damage to the airplane.
81 FR 19516
https://www.govinfo.gov/app/details/FR-2016-04-05/2016-07579
2016-07579
fr05ap16-24
RIN 2120-AA64
4910-13-P
Docket No. FAA-2016-4123
Directorate Identifier 2016-NE-06-AD
https://www.govinfo.gov/app/details/FR-2016-04-05/2016-07579
https://www.govinfo.gov/content/pkg/FR-2016-04-05/html/2016-07579.htm
https://www.govinfo.gov/content/pkg/FR-2016-04-05/pdf/2016-07579.pdf
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
3 p.
19516
19518
81 FR 19516
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; International Aero Engines AG Turbofan Engines; Federal Register Vol. 81, Issue
PRORULE
2016-07579
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2016-06-06
Docket No. FAA-2016-4123
Directorate Identifier 2016-NE-06-AD
4910-13-P
2016-07579
Notice of proposed rulemaking (NPRM).
We propose to adopt a new airworthiness directive (AD) for certain International Aero Engines AG (IAE) V2522-A5, V2524-A5, V2525- D5, V2527-A5, V2527E-A5, V2527M-A5, V2528-D5, V2530-A5, and V2533-A5 turbofan engines. This proposed AD was prompted by the fracture of the high-pressure turbine (HPT) stage 2 hub during flight, which resulted in an in-flight shutdown (IFSD), undercowl fire, and smoke in the cabin. This proposed AD would require inspecting the HPT stage 1 hub and HPT stage 2 hub, and, if necessary, their replacement with parts that are eligible for installation. We are proposing this AD to prevent failure of the HPT stage 1 or HPT stage 2 hubs, which could result in uncontained HPT blade release, damage to the engine, and damage to the airplane.
We must receive comments on this proposed AD by June 6, 2016.
Brian Kierstead, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7772; fax: 781- 238-7199; email: brian.kierstead@faa.gov.
Air Transportation
Aircraft
Aviation Safety
Incorporation by Reference
Safety
Airworthiness Directives:
International Aero Engines AG Turbofan Engines
,
ANE-AD-AMOC@faa.gov
brian.kierstead@faa.gov
iaeinfo@iaev2500.com
http://www.regulations.gov
https://www.iaeworld.com
Federal Register
Vol. 81, no. 65
Office of the Federal Register, National Archives and Records Administration
2016-04-05
continuing
daily
deposited
born digital
399 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2016-04-05
P0b002ee198594675
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr05ap16
https://www.govinfo.gov/app/details/FR-2016-04-05
https://www.govinfo.gov/content/pkg/FR-2016-04-05/pdf/FR-2016-04-05.pdf
https://www.govinfo.gov/content/pkg/FR-2016-04-05/xml/FR-2016-04-05.xml
fdlp
19467
19856
DGPO
2018-02-07
2023-04-29
FR-2016-04-05
machine generated
eng
FR
FR-2016-04-05
81
65