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2010-09-23
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Airworthiness Directives; Hartzell Propeller Inc. Model HC-B3TN-5( ) Propellers
Proposed Rules
D09002ee1bded19a0
D09002ee1bded1a3c
United States
Department of Transportation
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org
United States Government Agency or Subagency
United States
Federal Aviation Administration
originator
org
United States Government Agency or Subagency
The Federal Aviation Administration (FAA) proposes to adopt a new airworthiness directive (AD) that is applicable to Hartzell Propeller Inc. model HC-B3TN-5( ) propellers, with blades part number (P/N) T10176H(B,K)-5 or T10178H(B)-11(R) that are installed on Mitsubishi Heavy Industries, Ltd, MU-2 series airplanes. This proposal would require replacement of those blades with blades of the latest design. This proposal is prompted by a report of in-flight propeller blade separation that caused a severe out-of-balance condition, damage to the airplane, and resulted in engine shutdown and a safe landing. The actions specified by the proposed AD are intended to prevent propeller blade separation, damage to the airplane, and possible loss of the airplane.
67 FR 64321
https://www.govinfo.gov/app/details/FR-2002-10-18/02-26588
02-26588
fr18oc02-11
RIN 2120-AA64
4910-13-P
Docket No. 2001-NE-44-AD
https://www.govinfo.gov/app/details/FR-2002-10-18/02-26588
https://www.govinfo.gov/content/pkg/FR-2002-10-18/html/02-26588.htm
https://www.govinfo.gov/content/pkg/FR-2002-10-18/pdf/02-26588.pdf
Air Transportation
Aircraft
Aviation Safety
Safety
2 p.
64321
64322
67 FR 64321
Code of Federal Regulations
Title 14 Part 39
14 CFR Part 39
Regulation Identification Number 2120-AA64
RIN 2120-AA64
Airworthiness Directives; Hartzell Propeller Inc. Model HC-B3TN-5( ) Propellers; Federal Register Vol. 67, Issue
PRORULE
02-26588
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
2002-12-17
Docket No. 2001-NE-44-AD
4910-13-P
02-26588
Notice of proposed rulemaking (NPRM).
The Federal Aviation Administration (FAA) proposes to adopt a new airworthiness directive (AD) that is applicable to Hartzell Propeller Inc. model HC-B3TN-5( ) propellers, with blades part number (P/N) T10176H(B,K)-5 or T10178H(B)-11(R) that are installed on Mitsubishi Heavy Industries, Ltd, MU-2 series airplanes. This proposal would require replacement of those blades with blades of the latest design. This proposal is prompted by a report of in-flight propeller blade separation that caused a severe out-of-balance condition, damage to the airplane, and resulted in engine shutdown and a safe landing. The actions specified by the proposed AD are intended to prevent propeller blade separation, damage to the airplane, and possible loss of the airplane.
Comments must be received by December 17, 2002.
Tomaso DiPaolo, Aerospace Engineer, Chicago Aircraft Certification Office, FAA, Small Airplane Directorate, 2300 East Devon Avenue, Des Plaines, IL 60018; telephone (847) 294- 7031; fax (847) 294-7834.
Air Transportation
Aircraft
Aviation Safety
Safety
Airworthiness directives:
Hartzell Propeller Inc.,
9-ane-adcomment@faa.gov
Federal Register
Vol. 67, no. 202
Office of the Federal Register, National Archives and Records Administration
2002-10-18
continuing
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219 p.
Table of Contents:
AE 2.7:
GS 4.107:
AE 2.106:
KF70.A2
https://www.govinfo.gov/app/details/FR-2002-10-18
P0b002ee1809d471d
0097-6326
0042-1219
0364-1406
769-004-00000-9
000582072
f:fr18oc02
https://www.govinfo.gov/app/details/FR-2002-10-18
https://www.govinfo.gov/content/pkg/FR-2002-10-18/pdf/FR-2002-10-18.pdf
https://www.govinfo.gov/content/pkg/FR-2002-10-18/xml/FR-2002-10-18.xml
fdlp
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DGPO
2010-09-23
2023-05-04
FR-2002-10-18
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eng
FR
FR-2002-10-18
67
202