

[Federal Register: December 26, 2007 (Volume 72, Number 246)]
[Rules and Regulations]               
[Page 72915-72917]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr26de07-3]                         

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-28876; Directorate Identifier 2000-NE-08-AD; 
Amendment 39-15311; AD 2007-26-09]
RIN 2120-AA64

 
Airworthiness Directives; Hartzell Propeller Inc. Compact Series 
Propellers

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: The FAA is superseding an existing airworthiness directive 
(AD) for all Hartzell Propeller Inc. models ( )HC-( )( )Y( )-( )( )( ) 
compact series, constant speed or feathering propellers with Hartzell 
manufactured ``Y'' shank aluminum blades. That AD currently requires 
initial blade inspections, with no repetitive inspections; rework of 
all ``Y'' shank aluminum blades including cold rolling of the blade 
shank retention radius, blade replacement and modification of pitch 
change mechanisms for certain propeller models; and changing the 
airplane operating limitations with specific models of propellers 
installed. This AD requires the same actions but clarifies certain 
areas of the compliance, and updates a certain service bulletin (SB) 
reference to the most recent SB. This AD results from operators 
requesting clarification of certain portions of AD 2002-09-08. We are 
issuing this AD to prevent failure of the propeller blade from fatigue 
cracks in the blade shank radius, which can result in damage to the 
airplane and loss of airplane control.

DATES: This AD becomes effective January 30, 2008. The Director of the 
Federal Register previously approved the incorporation by reference of 
certain publications listed in the regulations as of June 13, 2002 (67 
FR 31113, May 9, 2002). The Director of the Federal Register approved 
the incorporation by reference of certain publications listed in the 
regulations as of January 30, 2008.

ADDRESSES: You can get the service information identified in this AD 
from Hartzell Propeller Inc. Technical Publications Department, One 
Propeller Place, Piqua, OH 45356; telephone (937) 778-4200; fax (937) 
778-4391.
    The Docket Operations office is located at Docket Management 
Facility, U.S. Department of Transportation, 1200 New Jersey Avenue, 
SE., West Building Ground Floor, Room W12-140, Washington, DC 20590-
0001.

FOR FURTHER INFORMATION CONTACT: Tim Smyth, Senior Aerospace Engineer, 
Chicago Aircraft Certification Office, FAA, Small Airplane Directorate, 
2300 East Devon Avenue, Des Plaines, IL 60018-4696; e-mail: 
timothy.smyth@faa.gov; telephone (847) 294-8110; fax (847) 294-7132.


SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39 by 
superseding AD 2002-09-08, Amendment 39-12741 (67 FR 31113, May 9, 
2002) with a proposed AD. The proposed AD applies to Hartzell Propeller 
Inc. models ( )HC-( )( )Y ( )-( )( )( ) compact series, constant speed 
or feathering propellers with Hartzell manufactured ``Y'' shank 
aluminum blades. We published the proposed AD in the Federal Register 
on August 14, 2006 (71 FR 46413). That action proposed to require the 
same actions as AD 2002-09-08, but would clarify certain areas of the 
compliance and would update a certain SB reference to the most recent 
SB.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov
; or in person at the Docket Operations office 

between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains this AD, the regulatory evaluation, 
any comments received, and other information. The street address for 
the Docket Operations office (telephone (800) 647-5527) is provided in 
the ADDRESSES section. Comments will be available in the AD docket 
shortly after receipt.

Comments

    We provided the public the opportunity to participate in the 
development of this AD. We have considered the comment received.

Incorporate Service Documents by Reference and Publish Them in the 
Document Management System

    The Modification and Replacement Parts Association requests that 
all service documents deemed essential to the accomplishment of the AD 
be incorporated by reference into the regulatory instrument, and 
published in the Docket Management System. We partially agree. We have 
incorporated pertinent service material into the regulatory section of 
this AD. However, at this time, the FAA does not post service material 
on the Federal Docket Management System. We are in the process of 
reviewing issues surrounding the posting of service bulletins on the 
Federal Docket Management System as part of an AD docket. Once we have 
thoroughly examined all aspects of this issue and have made a final 
determination, we will consider whether our current practice needs to 
be revised.

Format Changes

    We changed the propeller blade shank cold rolling information from 
being a note, to paragraphs. We also added paragraphs to the 
alternative methods of compliance, to make the information more 
readable.

Conclusion

    We have carefully reviewed the available data, including the 
comment received, and determined that air safety and the public 
interest require adopting the AD with the changes described previously.

Costs of Compliance

    We estimate that this AD will affect 35,750 propellers installed on 
airplanes of U.S. registry. We expect this AD will cost about $700 per 
propeller. Total cost to U.S. operators for this AD would be about 
$25.025 million. However, we also expect that all of the affected 
propellers should have already been inspected to comply with the 
existing AD's requirements to inspect, and

[[Page 72916]]

rework or replace the aluminum blades. Therefore, we expect that this 
AD will have no additional cost.

Docket Number Change

    We are transferring the docket for this AD to the Federal Docket 
Management System as part of our on-going docket management 
consolidation efforts. The new Docket No. is FAA-2007-28876. The old 
Docket No. became the Directorate Identifier, which is 2000-NE-08-AD.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, Section 106, describes the 
authority of the FAA Administrator. Subtitle VII, Aviation Programs, 
describes in more detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in 
Subtitle VII, Part A, Subpart III, Section 44701, ``General 
requirements.'' Under that section, Congress charges the FAA with 
promoting safe flight of civil aircraft in air commerce by prescribing 
regulations for practices, methods, and procedures the Administrator 
finds necessary for safety in air commerce. This regulation is within 
the scope of that authority because it addresses an unsafe condition 
that is likely to exist or develop on products identified in this 
rulemaking action.

Regulatory Findings

    We have determined that this AD will not have federalism 
implications under Executive Order 13132. This AD will 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.
    For the reasons discussed above, I certify that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866;
    (2) Is not a ``significant rule'' under DOT Regulatory Policies and 
Procedures (44 FR 11034, February 26, 1979); and
    (3) Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.
    We prepared a summary of the costs to comply with this AD and 
placed it in the AD Docket. You may get a copy of this summary at the 
address listed under ADDRESSES.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator, 
the Federal Aviation Administration amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:


    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by removing Amendment 39-12741 (67 FR 
31113, May 9, 2002), and by adding a new airworthiness directive, 
Amendment 39-15311, to read as follows:
2007-26-09 Hartzell Propeller Inc.: Amendment 39-15311. Docket No. 
FAA-2007-28876; Directorate Identifier 2000-NE-08-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective January 
30, 2008.

Affected ADs

    (b) This AD supersedes AD 2002-09-08, Amendment 39-12741.

Applicability

    (c) This AD applies to all Hartzell Propeller Inc. models ( )HC-
( )( )Y( )-( )( )( ) compact series constant speed or feathering 
propellers with Hartzell manufactured ``Y'' shank aluminum blades. 
These propellers are used on, but not limited to, the following 
airplanes:

------------------------------------------------------------------------
              Manufacturer                        Airplane Model
------------------------------------------------------------------------
Aermacchi S.pA. (formerly Siai-          S-208
 Marchetti).
Aero Commander.........................  200B and 200D
Aerostar...............................  600
Beech..................................  24, 35, 36, 45, 55, 56TC, 58,
                                          60, and 95
Bellanca...............................  14 and 17 series
Cessna.................................  182 and 188
Embraer................................  EMB-200A
Maule..................................  M5
Mooney.................................  M20 and M22
Pilatus Britten Norman, or Britten       BN-2, BN-2A, and BN-2A-6
 Norman.
Piper..................................  PA-23, PA-24, PA-28, PA-30, PA-
                                          31, PA-32, PA-34, PA-36, and
                                          PA-39
Pitts..................................  S-1T and S-2A
Rockwell...............................  112, 114, 200, 500, and 685
                                          series
------------------------------------------------------------------------

    (d) The parentheses appearing in the propeller model number 
indicates the presence or absence of an additional letter(s) that 
varies the basic propeller model. This AD applies regardless of 
whether these letters are present or absent in the propeller model 
designation.

Unsafe Condition

    (e) This AD results from operators requesting clarification of 
certain portions of AD 2002-09-08. We are issuing this AD to prevent 
failure of the propeller blade from fatigue cracks in the aluminum 
blade shank radius, which can result in damage to the airplane and 
loss of airplane control.

Compliance

    (f) You are responsible for having the actions required by this 
AD performed within the compliance times specified unless the 
actions have already been done.
    (g) If the propeller maintenance records show compliance with AD 
77-12-06R2, then compliance was previously done and no further 
action is required.
    (h) Propellers are considered in compliance with the one-time 
inspection and rework requirements only, of this AD if:
    (1) All blades are serial number D47534 and above, or
    (2) All blades are identified with the letters ``PR'' or ``R'' 
which are ink-stamped on the camber side, or the letters ``RD'' 
which are metal-stamped on the blade butt.

Models ( )HC-( )( )Y( ) Compact Series ``Y'' Shank Propellers

    (i) If propeller models ( )HC-( )( )Y( ) have not been inspected 
and reworked in accordance with AD 77-12-06R2, then before further 
flight, do a one-time action to remove, inspect, rework, or replace 
blades if

[[Page 72917]]

necessary using Hartzell Service Bulletin (SB) No. 118A, dated 
February 15, 1977.

Propeller Blade Shank Cold Rolling

    (j) One requirement in Hartzell SB No. 118A is the cold rolling 
of the propeller blade shank.
    (1) Cold rolling is a critical requirement in the prevention of 
cracks in the blade. Propeller repair shops must obtain and maintain 
proper certification to perform the cold rolling procedure.
    (2) For a current list of propeller overhaul facilities approved 
to perform the blade shank cold rolling procedure, contact Hartzell 
Product Support, telephone (937) 778-4200.
    (3) Not all propeller repair facilities have the equipment to 
properly perform a cold roll of the blade shanks.
    (4) In addition, any rework in the blade shank area will also 
necessitate the cold rolling of the blade shank area, apart from the 
one-time cold rolling requirement of this AD.

Instrument Panel Modifications

    (k) If airplanes with propeller models ( )HC-C2YK-( )( )( )/( )( 
)7666A-( ), installed on (undampered) 200 or more horsepower 
Lycoming IO-360 series engines, have not been modified using AD 77-
12-06R2, then modify the airplane instrument panel according to the 
following subparagraphs before further flight. Airplanes include, 
but are not limited to, Mooney M20E and M20F (normal category), 
Piper PA-28R-200 (normal category), and Pitts S-1T and S-2A 
(acrobatic category).
    (1) For normal category airplanes, before further flight, remove 
the present vibration placard and affix a new placard near the 
engine tachometer that states:
    ``Avoid continuous operation:
    Between 2,000 and 2,350 rpm.''
    (2) For utility and acrobatic category airplanes, before further 
flight, remove the present vibration placard and affix a new placard 
near the engine tachometer that states:
    ``Avoid continuous operation:
    Between 2,000 and 2,350 rpm.
    Above 2,600 rpm in acrobatic flight.''
    (3) For normal category airplanes, re-mark the engine tachometer 
face or bezel with a red arc for the restricted engine speed range, 
between 2,000 and 2,350 rpm.
    (4) For acrobatic and utility airplanes, re-mark the engine 
tachometer face or bezel with a red arc for each restricted engine 
speed range, i.e., between 2,000 and 2,350 rpm and between 2,600 and 
2,700 rpm (red line).

Models ( )HC-C2YK-( )( )( )/( )( )8475( )-( ) or ( )( )8477( )-( ) 
Propellers

    (l) If propeller models ( )HC-C2YK-( )( )( )/( )( )8475( )-( ) 
or ( )( )8477( )-( ) have not been inspected and reworked in 
accordance with AD 74-15-02, then do the following maintenance 
before further flight.
    (1) Remove propeller from airplane.
    (2) Modify pitch change mechanism, and replace blades with 
equivalent model blades prefixed with letter ``F'' using Hartzell 
Service Letter No. 69, dated November 30, 1971 and Hartzell SB No. 
101D, dated December 19, 1974.
    (3) Inspect and repair or replace, if necessary, using Hartzell 
SB No. 118A, dated February 15, 1977.

Alternative Methods of Compliance

    (m) The Manager, Chicago Aircraft Certification Office, has the 
authority to approve alternative methods of compliance for this AD 
if requested using the procedures found in 14 CFR 39.19.
    (n) Alternative methods of compliance for Hartzell SB No. 118A, 
dated February 15, 1977, are: Hartzell SB No. 118B, November 28, 
1977; SB No. 118C, May 13, 1983; SB No. 118D, March 25, 1991; SB No. 
HC-SB-61-118E, December 14, 2001; SB No. HC-SB-61-118 revision F, 
dated August 15, 2002, and Hartzell Manual 133C.
    (o) An alternative method of compliance to Hartzell SB No. 101D, 
dated December 19, 1974, is Hartzell Manual 133C.
    (p) No adjustment in the compliance time is allowed.

Related Information

    (q) Contact Tim Smyth, Senior Aerospace Engineer, Chicago 
Aircraft Certification Office, FAA, Small Airplane Directorate, 2300 
East Devon Avenue, Des Plaines, IL 60018-4696; e-mail: 
timothy.smyth@faa.gov; telephone (847) 294-7132; fax (847) 294-7834, 

for more information about this AD.

Material Incorporated by Reference

    (r) You must use the service information specified in Table 1 of 
this AD to perform the actions required by this AD. The Director of 
the Federal Register previously approved the incorporation by 
reference of the documents listed in Table 1 of this AD in 
accordance with 5 U.S.C. 552(a) and 1 CFR part 51 on June 13, 2002. 
Contact Hartzell Propeller Inc. Technical Publications Department, 
One Propeller Place, Piqua, OH 45356; telephone (937) 778-4200; fax 
(937) 778-4391, for a copy of this service information. You may 
review service information copies at the FAA, New England Region, 12 
New England Executive Park, Burlington, MA; or at the National 
Archives and Records Administration (NARA). For information on the 
availability of this material at NARA, call (202) 741-6030, or go 
to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.


                  Table 1.--Incorporation by Reference
------------------------------------------------------------------------
 Hartzell service information      Page       Revision         Date
------------------------------------------------------------------------
SB No. 101D..................          All            D  December 19,
                                                          1974.
SB No. 118A..................          All            A  February 15,
                                                          1977.
SL No. 69....................          All            1  November 30,
                                                          1971.
------------------------------------------------------------------------


    Issued in Burlington, Massachusetts, on December 17, 2007.
Peter A. White,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. E7-24855 Filed 12-21-07; 8:45 am]

BILLING CODE 4910-13-P
