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» Special Conditions: General Electric CT7-2E1 Turboshaft Engine
Special Conditions: General Electric CT7-2E1 Turboshaft Engine
Document ID:
FAA-2012-0745-0001
Document Type:
Proposed Rule
Agency:
Federal Aviation Administration
Topics:
Air Transportation, Aircraft, Aviation Safety, Safety
Federal Register Number:
2012-17560
CFR Citation:
14 CFR Part 33
View Document:
Details Information
Document Subtype:
Notice of Proposed Rulemaking (NPRM)
Received Date:
July 20 2012, at 12:00 AM Eastern Daylight Time
Start-End Page:
42677 - 42679
Page Count:
3
Comment Start Date:
July 20 2012, at 12:00 AM Eastern Standard Time
Comment Due Date:
September 18 2012, at 11:59 PM Eastern Standard Time
Comments
Total:
2
Honeywell Aerospace
Submitter:
Jose, Michael
Posted:
08/15/2012
ID:
FAA-2012-0745-0002
Comment Period Closed
Sep 18,2012 11:59 PM ET
European Aviation Safety Agency (EASA)
Submitter:
Mercy, Matthew
Posted:
09/07/2012
ID:
FAA-2012-0745-0003
Comment Period Closed
Sep 18,2012 11:59 PM ET
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Special Conditions: General Electric CT7-2E1 Turboshaft Engine
Details Information
Comments
Submitter: Jose, Michael Posted: 08/15/2012 ID: FAA-2012-0745-0002
Sep 18,2012 11:59 PM ET
Submitter: Mercy, Matthew Posted: 09/07/2012 ID: FAA-2012-0745-0003
Sep 18,2012 11:59 PM ET
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