Applicability
This airworthiness directive (AD) is applicable to Hartzell Propeller Inc.
model ( )HC-( )2Y( )-( ) propellers, with propeller hub part numbers
(P/N's) D-6522-1, D-6522-2, D-6529-1, and D-6559-3, with the serial
numbers (SN's) listed in the following Table 1:
TABLE 1.--APPLICABLE PROPELLERS AND HUBS
PROPELLER S/N HUB S/N HUB P/N
AU11115B A61365B D-6522-1
AU11116B A61366B D-6522-1
AU11117B A61367B D-6522-1
AU11119B A61369B D-6522-1
AU11125B A61375B D-6522-1
AU11131B A61381B D-6522-1
AU11134B A61384B D-6522-1
AU11135B A61385B D-6522-1
AY515B A61397B D-6522-2
AY516B A61398B D-6522-2
CH36140B A61409B D-6529-1
CH36141B A61410B D-6529-1
CH36151B A61420B D-6529-1
CH36152B A61421B D-6529-1
CH36153B A61422B D-6529-1
CH36157B A61427B D-6529-1
EU376B A61443B D-6559-3
CH36172B A61547B D-6529-1
CH36159B A61553B D-6529-1
CH36160B A61554B D-6529-1
CH36162B A61556B D-6529-1
CH36163B A61557B D-6529-1
CH36165B A61560B D-6529-1
CH36188B A61563B D-6529-1
CH36193B A61568B D-6529-1
CH36194B A61569B D-6529-1
CH36195B A61570B D-6529-1
CH36196B A61571B D-6529-1
CH36178B A61573B D-6529-1
CH36179B A61574B D-6529-1
CH36181B A61576B D-6529-1
CH36182B A61577B D-6529-1
CH36183B A61578B D-6529-1
CH36198B A61583B D-6529-1
CH36199B A61584B D-6529-1
CH36200B A61585B D-6529-1
CH36201B A61586B D-6529-1
CH36202B A61587B D-6529-1
CH36203B A61588B D-6529-1
CH36204B A61589B D-6529-1
CH36205B A61590B D-6529-1
CH36209B A61594B D-6529-1
CH36211B A61596B D-6529-1
CH36212B A61597B D-6529-1
CH36213B A61598B D-6529-1
CH36215B A61601B D-6529-1
CH36216B A61602B D-6529-1
AU11145B A61603B D-6522-1
AU11147B A61605B D-6522-1
AU11155B A61613B D-6522-1
AY520B A61743B D-6522-2
AU11175B A61893B D-6522-1
THESE PROPELLERS ARE INSTALLED ON, BUT NOT LIMITED TO THE FOLLOWING:
AMERICAN CHAMPION 8GCBC, 8KCAB
AERMACCHI S.p.A. S.208, S.208A
BEECH 95 series
BELLANCA 14-19-3, 14-19-3A
CESSNA 170 series, 172 series, 175 series,
177, A188A, A188B, T188C, 310 series
DIAMOND AIRCRAFT DA-40
LAKE (REVO) LA-4, LA-4-200
MAULE Aerospace Technology, Inc. M(T)-7-235( ), M-5-235C, M-6-235,
M(X)-7-235
MOONEY M20 series
Pilatus BRITTEN-NORMAN LTD BN-2 series, MK III, MK III-2, MK III-3
PIPER PA-23, PA-23-160, PA-24, PA-24-260,
PA-25-260, PA-28-140, PA-32-300,
PA-32S-300, PA-34-200, PA-44-180T
SOCATA--Groupe AEROSPATIALE MS-200, MS 894A, MS 894E, TB-20, TB-21
Sky International Inc. (Husky) A-1, S-1T, S-2A, S-2S (previous owners
were Christian Industries; Aviat, Inc.;
White International, LTD.)
Univair Aircraft Corporation 108 series (previous owner was Stinson)
Vulcanair S.p.A. P68 series (previous owner was
Partenavia Construzioni Aeronautiche
S.p.A)
Note 1: The parentheses that appear in the propeller models indicate the
presence or absence of additional letter(s) which vary the basic propeller
hub model designation. This airworthiness directive is applicable
regardless of whether these letters are present or absent on the propeller
hub model designation.
Note 2: This AD applies to each propeller identified in the preceding
applicability provision, regardless of whether it has been modified,
altered, or repaired in the area subject to the requirements of this AD.
For propellers that have been modified, altered, or repaired so that the
performance of the requirements of this AD is affected, the owner/operator
must request approval for an alternative method of compliance in
accordance with paragraph (d) of this AD. The request should include an
assessment of the effect of the modification, alteration, or repair on the
unsafe condition addressed by this AD; and, if the unsafe condition has
not been eliminated, the request should include specific proposed actions
to address it.
COMPLIANCE
Compliance with this AD is required as indicated, unless already done.
To prevent in-flight propeller blade separation resulting in airframe and
engine damage, and possible loss of the airplane, do the following:
(a) For Piper PA-32( ) series airplanes with Lycoming 540 series engines
rated at 300 horse power or higher, Britten Norman BN-2 series
airplanes with Lycoming 540 series engines, acrobatic
airplanes including certificated acrobatic airplanes, military
trainers, any airplanes routinely exposed to acrobatics usage, and
airplanes used for agricultural purposes, remove affected hubs listed
by SN in Table 1 of this AD within 50 hours time-since-new (TSN) or
12 months from the effective date of this AD, whichever occurs
first, and replace with serviceable hubs, in accordance with
paragraphs 3.A. through 3.B.(3) of ASB HC-ASB-61-259, dated
September 4, 2002.
(b) For airplanes other than those listed in paragraph (a) of this AD,
remove affected hubs listed by SN in Table 1 of this AD within 100
hours TSN or 12 months from the effective date of this AD,
whichever occurs first, and replace with serviceable hubs, in
accordance with paragraphs 3.A. through 3.B.(3) of ASB HC-ASB-61-259,
dated September 4, 2002.
(c) After the effective date of this AD, do not install any propeller
assembly that has a hub with a P/N D-6522-1, D-6522-2, D-6529-1,
or D-6559-3, with a SN listed in Table 1 of this AD.
ALTERNATIVE METHODS OF COMPLIANCE
(d) An alternative method of compliance or adjustment of the compliance
time that provides an acceptable level of safety may be used if approved
by the Manager, Chicago Aircraft Certification Office (ACO). Operators
must submit their requests through an appropriate FAA Principal
Maintenance Inspector, who may add comments and then send it to the
Manager, Chicago ACO.
Note 3: Information concerning the existence of approved alternative
methods of compliance with this airworthiness directive, if any, may be
obtained from the Chicago ACO.
SPECIAL FLIGHT PERMITS
(e) Special flight permits may be issued in accordance with §§ 21.197 and
21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to
operate the airplane to a location where the requirements of this AD can
be done.
DOCUMENTS THAT HAVE BEEN INCORPORATED BY REFERENCE
(f) The propeller hub replacements must be done in accordance with Alert
Service Bulletin Hartzell Propeller Inc. HC-ASB-61-259, dated September 4,
2002. This incorporation by reference was approved by the Director of the
Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51.
Copies may be obtained from Hartzell Propeller Inc. Technical Publications
Department, One Propeller Place, Piqua, OH 45356; telephone (937) 778
-4200; fax (937) 778-4391. Copies may be inspected at the FAA, New England
Region, Office of the Regional Counsel, 12 New England Executive Park,
Burlington, MA; or at the Office of the Federal Register, 800 North
Capitol Street, NW., suite 700, Washington, DC.
EFFECTIVE DATE
(g) This amendment becomes effective on January 23, 2003.
FOR FURTHER INFORMATION CONTACT: 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.
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; request for comments.
SUMMARY: This amendment adopts a new airworthiness directive (AD) that is
applicable to Hartzell Propeller Inc. model ( )HC-( )2Y( )-( ) propellers,
with certain serial numbers (SN's) of two-bladed aluminum propeller hubs
part numbers (P/N's) D-6522-1, D-6522-2, D-6529-1, and D-6559-3 installed.
This action requires removal from service of those certain SN's of two
- bladed aluminum propeller hubs and replacement with serviceable hubs.
This amendment is prompted by a two-bladed aluminum propeller hub
manufacturing quality control problem. The actions specified in this AD
are intended to prevent in-flight propeller blade separation resulting in
airframe and engine damage, and possible loss of the airplane.
DATES: Effective January 23, 2003. The incorporation by reference of
certain publications listed in the rule is approved by the Director of the
Federal Register as of January 23, 2003.
Comments for inclusion in the Rules Docket must be received on or before
March 10, 2003. ADDRESSES: Submit comments in triplicate to the Federal
Aviation Administration (FAA), New England Region, Office of the Regional
Counsel, Attention: Rules Docket No. 2002-NE-25-AD, 12 New England
Executive Park, Burlington, MA 01803-5299. Comments may be inspected at
this location, by appointment, between 8 a.m. and 4:30 p.m., Monday
through Friday, except Federal holidays. Comments may also be sent via the
Internet using the following address: "9-ane-adcomment@faa.gov". Comments
sent via the Internet must contain the docket number in the subject line.
The service information referenced in this AD may be obtained from
Hartzell Propeller Inc. Technical Publications Department, One Propeller
Place, Piqua, OH 45356; telephone (937) 778-4200; fax (937) 778-4391. This
information may be examined, by appointment, at the FAA, New England
Region, Office of the Regional Counsel, 12 New England Executive Park,
Burlington, MA; or at the Office of the Federal Register, 800 North
Capitol Street, NW., suite 700, Washington, DC.
FOR FURTHER INFORMATION CONTACT: 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.
SUPPLEMENTARY INFORMATION: On August 19, 2002, the FAA was notified by
Hartzell Propeller Inc. that certain two-bladed aluminum propeller hub
SN's installed in 2-bladed propellers were found to have subsurface
discontinuities in the aluminum. Some of these hubs have been installed in
propellers and some have been shipped as spares. The discontinuities were
not removed during the propeller hub forging process, and could initiate
fatigue cracking in the propeller hub arms. This final rule; request for
comments, replaces affected hubs determined to be under higher stresses
based on specific airplane installation, within 50 hours time-since-new
(TSN) or 12 months from the effective date of the AD, whichever occurs
first, and affected hubs determined to be under lower stresses based on
specific airplane installation, within 100 hours TSN or 12 months from the
effective date of this AD, whichever occurs first. This condition, if not
corrected, could result in in- flight propeller blade separation, airframe
and engine damage, and possible loss of the airplane.
Manufacturer's Service Information
The FAA has reviewed and approved the technical contents of Hartzell
Propeller Inc. Alert Service Bulletin (ASB) HC-ASB-61-259, dated September
4, 2002, that provides a SN list of 123 affected propeller hubs and
describes procedures for hub replacement. This AD action has denoted the
remaining 52 serial numbered propeller hubs that need to be replaced.
FAA's Determination of an Unsafe Condition and Required Actions
Since an unsafe condition has been identified that is likely to exist or
develop on other propeller hubs of the same type design, this AD is being
issued to prevent in-flight propeller blade separation resulting in
airframe and engine damage, and possible loss of airplane control. This AD
requires removal from service of certain two-bladed aluminum propeller
hubs identified by SN and replacement with serviceable two-bladed aluminum
propeller hubs. This action lists the remaining 52 serial numbered
propeller hubs that need to be replaced. The actions are required to be
done in accordance with the alert service bulletin described previously.
Immediate Adoption of This AD
Since a situation exists that requires the immediate adoption of this
regulation, it is found that notice and opportunity for prior public
comment hereon are impracticable, and that good cause exists for making
this amendment effective in less than 30 days.
Comments Invited
Although this action is in the form of a final rule that involves
requirements affecting flight safety and, thus, was not preceded by notice
and an opportunity for public comment, comments are invited on this rule.
Interested persons are invited to comment on this rule by submitting such
written data, views, or arguments as they may desire. Communications
should identify the Rules Docket number and be submitted in triplicate to
the address specified under the caption ADDRESSES. All communications
received on or before the closing date for comments will be considered,
and this rule may be amended in light of the comments received. Factual
information that supports the commenter's ideas and suggestions is
extremely helpful in evaluating the effectiveness of the AD action and
determining whether additional rulemaking action would be needed.
Comments are specifically invited on the overall regulatory, economic,
environmental, and energy aspects of the rule that might suggest a need to
modify the rule. All comments submitted will be available, both before and
after the closing date for comments, in the Rules Docket for examination
by interested persons. A report that summarizes each FAA-public contact
concerned with the substance of this AD will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments
submitted in response to this action must submit a self-addressed, stamped
postcard on which the following statement is made: "Comments to Docket
Number 2002-NE-25-AD." The postcard will be date stamped and returned to
the commenter.
Regulatory Analysis
This final rule does not have federalism implications, as defined in
Executive Order 13132, because it would not have a substantial direct
effect on the States, on the relationship between the national government
and the States, or on the distribution of power and responsibilities among
the various levels of government. Accordingly, the FAA has not consulted
with state authorities prior to publication of this final rule.
The FAA has determined that this regulation is an emergency regulation
that must be issued immediately to correct an unsafe condition in
aircraft, and is not a "significant regulatory action" under Executive
Order 12866. It has been determined further that this action involves an
emergency regulation under DOT Regulatory Policies and Procedures (44 FR
11034, February 26, 1979). If it is determined that this emergency
regulation otherwise would be significant under DOT Regulatory Policies
and Procedures, a final regulatory evaluation will be prepared and placed
in the Rules Docket. A copy of it, if filed, may be obtained from the
Rules Docket at the location provided under the caption ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration amends part 39 of the
Federal Aviation Regulations (14 CFR part 39) as follows:
PART 39--AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13 [Amended]
2. Section 39.13 is amended by adding the following new airworthiness
directive: