[Federal Register Volume 70, Number 220 (Wednesday, November 16, 2005)]
[Proposed Rules]
[Pages 69472-69474]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-22712]


=======================================================================
-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-22898; Directorate Identifier 2005-NE-10-AD]
RIN 2120-AA64


Airworthiness Directives; McCauley Propeller Systems Models 
3A32C406/82NDB-X and D3A32C409/82NDB-X Propellers

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for McCauley Propeller Systems models 3A32C406/82NDB-X and D3A32C409/
82NDB-X propellers, installed on Teledyne Continental Motors (TCM) IO-
520, TSIO-520, or IO-550 reciprocating engines. These propellers are 
herein referred to as C406 and C409 propellers, respectively. This 
proposed AD would require adding an operational revolutions per minute 
(rpm) restriction on the C406 and C409 propellers, and installing an 
rpm restriction placard in the cockpit. This proposed AD would also add 
a 10,000-hour total time-in-service (TIS) life limit for these 
propellers. This proposed AD would also remove from service any 
propeller that has 10,000 hours or more total TIS, or that has an 
unknown total TIS. Also, this proposed AD would require initial and 
repetitive propeller blade inspections for damage, and repair if 
necessary. This proposed AD results from testing by the manufacturer 
that identified stress conditions that affect the fatigue life and 
damage tolerance of C406 and C409 propellers, when installed on TCM IO-
520, TSIO-520, or IO-550 reciprocating engines. We are proposing this 
AD to prevent blade or hub failure that could result in separation of a 
propeller blade and loss of control of the airplane.

DATES: We must receive any comments on this proposed AD by January 17, 
2006.

ADDRESSES: Use one of the following addresses to comment on this 
proposed AD.
     DOT Docket web site: Go to http://dms.dot.gov and follow 
the instructions for sending your comments electronically.
     Government-wide rulemaking web site: Go to http://www.regulations.gov and follow the instructions for sending your 
comments electronically.
     Mail: Docket Management Facility; U.S. Department of 
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, 
Washington, DC 20590-0001.
     Fax: (202) 493-2251.
     Hand Delivery: Room PL-401 on the plaza level of the 
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    Contact McCauley Propeller Systems, P.O. Box 7704, Wichita, KS 
67277-7704; telephone (800) 621-7767, for the service information 
identified in this AD.
    You may examine the comments on this proposed AD in the AD docket 
on the Internet at http://dms.dot.gov.

FOR FURTHER INFORMATION CONTACT: Timothy Smyth, Aerospace Engineer, 
Chicago Aircraft Certification Office, FAA, Small Airplane Directorate, 
2300 East Devon Avenue, Des Plaines, IL 60018; telephone: (847) 294-
7132; fax: (847) 294-7834.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to send us any written relevant data, views, or 
arguments regarding this proposal. Send your comments to an address 
listed under ADDRESSES. Include ``Docket No. FAA-2005-22898; 
Directorate Identifier 2005-NE-10-AD'' in the subject line of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of the proposed AD. We will 
consider all comments received by the closing date and may amend the 
proposed AD in light of those comments.
    We will post all comments we receive, without change, to http://dms.dot.gov, including any personal information you provide. We will 
also post a report summarizing each substantive verbal contact with FAA 
personnel concerning this proposed AD. Using the search function of the 
DMS web site, anyone can find and read the comments in any of our 
dockets, including the name of the individual who sent the comment (or 
signed the comment on behalf of an association, business, labor union, 
etc.). You may review the DOT's complete Privacy Act Statement in the 
Federal Register published on April 11, 2000 (65 FR 19477-78) or you 
may visit http://dms.dot.gov.

Examining the AD Docket

    You may examine the docket that contains the proposal, any comments 
received and, any final disposition in person at the DMS Docket Offices 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The Docket Office (telephone (800) 647-5227) is located on 
the plaza level of the Department of Transportation Nassif Building at 
the street address stated in ADDRESSES. Comments will be available in 
the AD docket shortly after the DMS receives them.

Discussion

    McCauley Propeller Systems recently conducted tests to measure 
vibratory stress on C406 and C409 propellers. The tests identified a 
high stress condition that reduces the fatigue life and damage 
tolerance of C406 and C409 propellers when installed on TCM IO-520, 
TSIO-520, or IO-550 reciprocating engines. This condition, if not 
corrected, could result in blade or hub failure that could result in 
separation of a propeller blade and loss of control of the airplane.

Relevant Service Information

    We reviewed and approved the technical contents of McCauley 
Propeller Systems Alert Service Bulletin (ASB) No. ASB248, dated 
January 17, 2005, that does the following:
     Adds an rpm restriction that states continuous propeller 
operation between 2,350 rpm and 2,450 rpm at 24 inches Hg and higher 
manifold pressure is prohibited.
     Installs an rpm restriction placard in the cockpit.
     Adds a 10,000-hour total TIS life limit for C406 and C409 
propellers.
     Removes from service any propeller that has 10,000 hours 
or more total TIS, or that has an unknown total TIS.
     Requires initial and repetitive propeller blade 
inspections for damage, and repair if necessary.

FAA's Determination and Requirements of the Proposed AD

    We evaluated all pertinent information and identified an unsafe 
condition that is likely to exist or

[[Page 69473]]

develop on other C406 and C409 propellers of this same type design. We 
are proposing this AD, which would require:
     Within 10 hours TIS after the effective date of the 
proposed AD, installing an rpm restriction placard on the pilot's 
console in front of the pilot, that states that continuous propeller 
operation between 2,350 and 2,450 rpm at 24 inches Hg and higher 
manifold pressure is prohibited.
     Adding a 10,000-hour total TIS propeller life limit.
     Within 50 hours TIS after the effective date of the 
proposed AD, removing from service any propeller that has 10,000 hours 
or more total TIS, or that has an unknown total TIS.
     Initially inspecting propeller blades for damage within 
100 hours TIS after the effective date of the proposed AD, and 
repairing if necessary.
     Thereafter, repetitively inspecting propeller blades for 
damage every 100 hours TIS or next annual inspection, whichever occurs 
first.
    The proposed AD would require you to use the service information 
described previously to perform these actions.

Costs of Compliance

    About 2,350 C406 and C409 propellers installed on airplanes of U.S. 
registry would be affected by this proposed AD. We also estimate it 
would take about 3 work hours per propeller to perform the proposed 
inspections and repairs, and each propeller would have three 
inspections per year. We also estimate it would take about 0.5 work 
hour to install the proposed cockpit placard, and about 950 airplanes 
would require the placard. The average labor rate is $65 per work hour. 
A replacement propeller blade would cost about $10,500. We estimate 500 
propellers in the fleet (or about 21%) would require parts replacement. 
Based on these figures, we estimate the total cost of the proposed AD 
to U.S. operators to be $2,585,500.

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 determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD 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.
    For the reasons discussed above, I certify that the proposed 
regulation:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979); and
    3. Would 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 proposal 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, Safety.

The Proposed Amendment

    Under the authority delegated to me by the Administrator, the 
Federal Aviation Administration proposes to amend 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.


Sec.  39.13  [Amended]

    2. The FAA amends Sec.  39.13 by adding the following new 
airworthiness directive:

McCauley Propeller Systems: Docket No. FAA-2005-22898; Directorate 
Identifier 2005-NE-10-AD.

Comments Due Date

    (a) The Federal Aviation Administration (FAA) must receive 
comments on this airworthiness directive (AD) action by January 17, 
2006.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to McCauley Propeller Systems models 
3A32C406/82NDB-X and D3A32C409/82NDB-X propellers, herein referred 
to as C406 and C409 propellers, respectively. These propellers are 
installed on, but not limited to, the airplanes in the following 
Table 1:

  Table 1.--Airplanes That Propellers Are Installed on, But Not Limited
                                   to:
------------------------------------------------------------------------
            Airplane models:                    With engine model:
------------------------------------------------------------------------
Beech:
    A35, B35, C35, D35, E35, F35, G35,   Teledyne Continental Motors
     H35, J35, K35, M35, N35, P35, S35,   (TCM) IO-520 series and IO-550
     V35, V35A, V35B, 35-33, 35-33A, 35-  series reciprocating engines.
     C33, 35[dash]C33A, E33, E33A,
     E33C, F33, F33A, F33C, 36, A36,
     A45, and D45.
Beech:
    A36TC, B36TC, S35, V35A, V35B......  TCM TSIO-520 series
                                          reciprocating engines.
Navion:
    A (L-17B, C), B, D, E, F, G, and H.  TCM IO-550 and TSIO-520 series
                                          reciprocating engines.
------------------------------------------------------------------------

Unsafe Condition

    (d) This AD results from testing by the manufacturer, that 
identified stress conditions that affect the fatigue life and damage 
tolerance of C406 and C409 propellers when installed on TCM IO-520, 
TSIO-520, or IO-550 reciprocating engines. We are issuing this AD to 
prevent blade or hub failure that could result in separation of a 
propeller blade and loss of control of the airplane.

Compliance

    (e) You are responsible for having the actions required by this 
AD performed within the compliance times specified unless the 
actions have already been done.

[[Page 69474]]

Installation of Cockpit Placard for RPM Restriction

    (f) Within 10 hours time-in-service (TIS) after the effective 
date of this AD, install a placard on the pilot's console in front 
of the pilot, that states, in \1/4\ inch-high or higher characters, 
``Continuous propeller operation between 2,350 rpm and 2,450 rpm at 
24 inches Hg and higher manifold pressure is prohibited''.

Propellers With Unknown Total Hours TIS, or 10,000 or More Hours Total 
TIS on the Effective Date of This AD

    (g) For propellers that the total TIS is unknown, or that have 
10,000 or more hours total TIS on the effective date of this AD, 
remove the propeller from service within 50 hours TIS after the 
effective date of this AD.

Propellers With Fewer Than 10,000 Hours Total TIS on the Effective Date 
of This AD

    (h) For propellers with fewer than 10,000 total hours TIS on the 
effective date of this AD, do the following:
    (1) Perform an inspection of the propeller blades and repair if 
necessary, within 100 hours after the effective date of this AD, 
using paragraphs 2.B. through 2.F. of Accomplishment Instructions of 
McCauley ASB No. ASB248, dated January 17, 2005.
    (2) At the next propeller overhaul or next major propeller 
disassembly, life-limit-stamp the letter ``L'' on the propeller hub 
and blades, using paragraph 3 of Accomplishment Instructions of 
McCauley Propeller Systems Alert Service Bulletin (ASB) No. ASB248, 
dated January 17, 2005.
    (3) Thereafter, within every 100 hours TIS or at next annual 
inspection, whichever occurs first, inspect, and repair if 
necessary, the propeller blades using paragraphs 2.B. through 2.F. 
of Accomplishment Instructions of McCauley ASB No. ASB248, dated 
January 17, 2005.
    (4) Remove the propeller from service at or before reaching the 
life limit of 10,000 hours total TIS.

Alternative Methods of Compliance

    (i) 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.

Related Information

    (j) None.

    Issued in Burlington, Massachusetts, on November 7, 2005.
Peter A. White,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 05-22712 Filed 11-15-05; 8:45 am]
BILLING CODE 4910-13-P