Back to AD

AD 2005-14-11 ACTIVE

Failed propeller blade
Key Information
AD Number 2005-14-11 Status Active
Effective Date August 17, 2005 Issue Date July 05, 2005
Docket Number 2003-NE-53-AD Amendment 39-14188
Product Type ["Propeller"] Product Subtype Not specified
CFR Part --- - Part 39 CFR Section --- - _EMPTY_
Citation Federal Register: July 13, 2005 (Volume 70, Number 133)
Applicability
Manufacturer(s) Hartzell Propeller, Inc. McCauley Propeller Systems Sensenich Propeller Manufacturing Company, Inc.
Model(s) BHC-92W BHC-92ZF-1 BHC-92ZF-3 BHC-92ZF-8 BHC-A2V BHC-A2XF-1 BHC-A2XF-3 BHC-A2XF-G BHC-B3W BHC-C2Y BHC-G2YF-1 BHC-I2YF-1 BHC-I2YF-4 BHC-J2YF-1 BHC-J2YF-2 BHC-L2YF-1 BHC-L2YF-2 BHC-L2YF-4 CHC-C2Y DHC-C2Y DHC-E2Y EHC-A3MVF EHC-A3VF EHC-C3Y EHC-G3YF-1 EHC-G3YF-2 EHC-L3Y HA-12UF-1 HA-12UF-3 HA-12UO-1 HA-12UO-2 HA-A2MV20-1 HA-A2V20-1 HA-B3P HA-B3Z30-1 HC-102YF-1 HC-12V20-3 HC-12V20-7 HC-12V20-8 HC-12X20-1 HC-12X20-2 HC-12X20-3 HC-12X20-4 HC-12X20-5 HC-12X20-6 HC-12X20-7 HC-12X20-8 HC-12X20-9 HC-13X20-5 HC-13X20-6 HC-13X20-8 HC-42XF-2 HC-52X20-1 HC-82-XK-1 HC-82-XK-2 HC-82-XK-3 HC-82X20-1 HC-82X20-3 HC-82X20-5 HC-82XF-1 HC-82XF-2 HC-82XF-3 HC-82XF-6 HC-82XG-1 HC-82XG-2 HC-82XG-6 HC-82XL-1 HC-82XL-2 HC-82XL-6 HC-82XS-2 HC-83X20-1 HC-83X20-2 HC-83XF-1 HC-83XF-2 HC-83XF-3 HC-83XK-1 HC-83XK-2 HC-92W HC-92ZF-1 HC-92ZF-2 HC-92ZF-6 HC-92ZK-1 HC-92ZK-2 HC-92ZK-6 HC-92ZK-8 HC-92ZL-2 HC-93Z20-1 HC-93Z20-2 HC-93Z30-2 HC-93ZF-2 HC-A2MV HC-A2V HC-A2X20-1 HC-A2X20-2 HC-A2X20-4 HC-A2X20-5 HC-A2X20-G HC-A2XF-1 HC-A2XF-2 HC-A2XF-G HC-A2XK-1 HC-A2XK-2 HC-A2XK-G HC-A2XL-1 HC-A2XL-2 HC-A2XL-G HC-A3MV HC-A3V HC-A3X20-1 HC-A3X20-2 HC-A3X20-5 HC-A3X21-2 HC-A3XF-2 HC-A3XF-4 HC-A3XK-2 HC-A3XK-4 HC-B3M HC-B3P20-4 HC-B3P30-1 HC-B3P30-2 HC-B3R20-4 HC-B3R30-1 HC-B3R30-2 HC-B3R30-4 HC-B3T HC-B3W20 HC-B3W30 HC-B3WF HC-B3WN HC-B3Z20-1 HC-B3Z20-2 HC-B3Z22-7 HC-B3Z30-2 HC-B3ZF-2 HC-B4MN-5 HC-B4MP-3 HC-B4TN-3 HC-B4TN-5 HC-B4W40-2 HC-C2Y HC-C3Y HC-C4YF-1 HC-C4YF-2 HC-C4YN-2 HC-C4YR-2 HC-D2V20-3 HC-D2V20-7 HC-D2V20-8 HC-D3V20-6 HC-D4 HC-E2Y HC-E3YR-1 HC-E3YR-2 HC-E3YR-7 HC-E4 HC-E5 HC-F2YL-1 HC-F2YL-2 HC-F2YR-1 HC-F2YR-2 HC-F3YK-1 HC-F3YK-2 HC-F3YR-1 HC-F3YR-2 HC-F4YR-1 HC-F4YR-2 HC-G3YF-1 HC-G3YF-2 HC-H3YF-1 HC-H3YF-2 HC-H3YF-3 HC-H3YN-2 HC-I2YF-1 HC-I2YF-4 HC-I2YR-1 HC-I3Y1R-1 HC-I3YR-1 HC-I3YR-2 HC-J3Y HC-L2YF-2 HC-L2YF-4 HC-M2YR-1 HC-M2YR-2 HC-M3YR-1 PHC-C3Y PHC-G3YF-1 PHC-G3YF-2 PHC-H3YF-1 PHC-H3YF-2 PHC-I3YF-1 PHC-I3YF-2 PHC-J3Y PHC-L3Y 1A100 1A101 1A102 1A103/TCM 1A105 1A106 1A110-GF 1A110-GM 1A135 1A162 1A170 1A175 1A180/SEM 1A200 1A230/AFC 1A90 1B175 1B200 1B235/BFA 1B235/DFC 1B235/EFC 1B90 1C160/CTM 1C160/DTM 1C160/EGM 1C160/FGM 1C160/VCM 1C172/AGM 1C172/BTM 1C172/EM 1C172/MDM 1C172/MFA 1C172/MGM 1C172/MTM 1C172/SBTM 1C172/TM 1C200 1C235/LFA 1C90 1D200 1P235/AFA 1P235/PFA 2A31C21 2A34C 2A36C1 2A36C18 2A36C23 2A36C29 2A36C43 2A36C82 2A37C 2AF31C10 2AF34C55 2AF36C26 2AF36C38 2AF36C39 2AF36C68 2AF36C89 2B36C7 2C36C9 2D34C 2D34CT69 2D36C14 2D36C28 2DF36C30 2DF36C35 2E34C57 3A32C406 3A32C418 3A32C76 3A34C422 3A34C423 3A36C434 3AF32C504 3AF32C505 3AF32C506 3AF32C507 3AF32C508 3AF32C509 3AF32C511 3AF32C512 3AF32C515 3AF32C521 3AF32C522 3AF32C523 3AF32C524 3AF32C528 3AF32C72 3AF32C75 3AF32C87 3AF32C93 3AF34C502 3AF34C503 3AF34C74 3AF34C86 3AF34C92 3AF36C514 3AF36C525 3AF37C510 3AF37C516 3FF32C501 3FF34C529 3GFR34C601 3GFR34C602 3GFR34C701 3GFR34C702 3GFR34C703 3GFR34C704 B2A31C63 B2A34C B2A36C31 B2A37C B2D34C B2D34CT69 B2D37C B3D32C407 B3D32C412 B3D32C414 B3D32C417 B3D32C419 B3D34C405 B3D34C413 B3D36C416 B3D36C424 B3D36C427 B3D36C428 B3D36C429 B3D36C431 B3D36C432 B3D36C433 B3D36C442 B3DF36C526 B3DF36C527 C2A34C C2A36C32 C2D37C C3D36C415 D2A34C D2A36C31 D2A36C33 D2A36C45 D2A37C D2AF34C D2AF36C48 D3A32C408 D3A32C409 D3A32C411 D3A32C425 D3A32C426 D3A32C77 D3A32C79 D3A32C88 D3A32C90 D3A34C401 D3A34C402 D3A34C403 D3A34C404 D3A34C420 D3A34C443 D3A34C444 D3A34C447 D3A36C410 D3A36C430 D3A36C435 D3A36C436 D3A36C445 D3AF32C35 D3AF32C80 D3AF32C87 E2A34C E2A37C F2A34C 69CK 70CM6 70CM7 72CC 72CK 74CK 74DC 74DM6 74DM7 74DR 76AK-2 76AM6-2 76E Series 80BM8 C-2FB1 C-2FB2 C-2FM3 C-2FM4 C-2FM5 C-2FM6-1 C3FC3 C3FR4 CS-2FM4 CS-2FM5 CS-2FM6 CS-3FM4 CS-3FR5 PHC-J3YF-1 PHC-J3YF-2
Summary

The FAA is adopting a new airworthiness directive (AD) for Hartzell Propeller, Inc., McCauley Propeller Systems, and Sensenich Propeller Manufacturing Company, Inc. propellers. This AD requires maintenance actions amounting to an overhaul of the affected propellers. This AD results from the investigation of a failed propeller blade and subsequent inspections of various propeller models returned to service by Southern California Propeller Service, of Inglewood, CA. We are issuing this AD to prevent blade failure that could result in separation of a propeller blade and loss of control of the airplane.

Action Required

Final rule.

Regulatory Text

2005-14-11 Hartzell Propeller, Inc., McCauley Propeller Systems, and Sensenich Propeller Manufacturing Company, Inc. Propellers: Amendment 39-14188. Docket No. 2003-NE-53-AD.

Effective Date

(a) This airworthiness directive (AD) becomes effective August 17, 2005.

Affected ADs

(b) None.

Applicability

(c) This AD applies to the Hartzell Propeller, Inc., McCauley Propeller Systems, and Sensenich Propeller Manufacturing Company, Inc. propeller models last returned to service by Southern California Propeller Service of Inglewood, CA., listed in the following Table 1:

Table 1.--Applicable Propeller Models

Hartzell Propeller, Inc.
()HC ()(2,3,4)Y() ().

()HC ()(2,3,4)(X,V,MV,W,Z,P,R) (F,G,L,K,R,20,30,31) ().
()HA () ().
HC B(3,4)(M,P,R,T)(A,N,P) ().
HC (D,E)(4,5)(A,B,N,P) ().
McCauley Propeller Systems

()2()()3()C()()() (): All constant speed two-bladed propeller models.

()3()()3()C()()() (): All constant speed three-bladed propellermodels.
1()()()()/(): All metal propeller models.

Sensenich Propeller Manufacturing
Company, Inc.
All metal propeller models.

(d) These actions are against propeller models returned to service by Southern California Propeller Service. Southern California Propeller Service is not to be confused with propeller repair stations known as California Propeller or as Propeller Service of California. Southern California Propeller Service was issued Air Agency Certificate number of VXSR617L in 1992, which was revoked in June of 1998.

(e) For Hartzell and McCauley propeller models listed in Table 1 of this AD, any letter or number (or lack of a letter or number) could appear where open parentheses are shown in the model number. Model numbers could show any combination of letters or numbers where the model number shows parentheses with a series of numbers or letters.

(f) For propeller models listed in Table 1 of this AD, that have been overhauled since being returned to service by Southern California Propeller Service by an authorized repair station other than Southern California Propeller Service, no further action is required.

Unsafe Condition

(g) This AD results from the investigation of a failed propeller blade and subsequent inspections of various propeller models returned to service by Southern California Propeller Service, of Inglewood, CA. We are issuing this AD to prevent blade failure that could result in separation of a propeller blade and loss of control of the airplane.

Compliance

(h) You are responsible for having the actions required by this AD performed within 10 hours time-in-service after the effective date of this AD.

Required Actions

(i) Perform the actions specified in paragraph (j) of this AD on propeller models listed in Table 1 of this AD. You can find information on performing the actions in the applicable propeller manufacturer's service documentation.

(j) Perform the following actions:

(1)Disassemble,

(2) Clean,

(3) Inspect for the following:

(i) Cracks,

(ii) Corrosion or pits,

(iii) Nicks,

(iv) Scratches,

(v) Blade minimum dimensions,

(vi) Unapproved localized heating of blade,

(vii) Unapproved use of helicoil inserts in actuating pin holes,

(viii) Improperly drilled actuating pin holes,

(ix) Chemical conversion coat or paint or both applied over corrosion,

(x) Lack of chemical conversion coating,

(xi) Lack of paint on internal surfaces,

(xii) Bolts incorrectly torqued,

(xiii) Incorrect parts,

(xiv) Incorrect installation of parts,

(xv) Reinstallation of parts intended for one-time use, and

(xvi) Lack of proper shot peening.

(4) Repair and replace with serviceable parts, as necessary,

(5) Reassemble and test.

Alternative Methods of Compliance

(k) The Manager, Chicago Aircraft Certification Office, has the authority to approve alternative methods of compliance (AMOCs) for this AD if requested using the procedures found in 14 CFR 39.19.

Special Flight Permits

(l) Under 14 CFR 39.23, we are limiting the special flight permits for this AD by not allowing any flights with apparent cracks in propellers.

Related Information

(m) Special Airworthiness Information Bulletin No. NE-01-19, dated March 20, 2001, pertains to the subject of this AD.

Supplementary Information

The FAA proposed to amend 14 CFR part 39 with a proposed airworthiness directive (AD). The proposed AD applies to certain Hartzell Propeller, Inc., McCauley Propeller Systems, and Sensenich Propeller Manufacturing Company, Inc. propellers returned to service by Southern California Propeller Service. We published the proposed AD in the Federal Register on May 20, 2004 (69 FR 29111). That action proposed to require maintenance actions that amount to an overhaul of Hartzell Propeller, Inc., McCauley Propeller Systems, and Sensenich Propeller Manufacturing Company, Inc. propellers returned to service by Southern California Propeller Service.

Examining the AD Docket

You may examine the AD Docket (including any comments and service information), by appointment, between 8 a.m. and 4:30 p.m., Monday through Friday, except Federal holidays. See ADDRESSES for the location.

Comments

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

Question of Why the FAA Is Changing the Rules

One commenter asks "Why change the rules just because one repair station, Southern California Propeller Service, of Inglewood, CA didn't follow the existing rules?'' The commenter feels that the existing rules have worked for well over 50 years, and asks how making general aviation cost more is going to solve the problem. The commenter feels that the proposed AD is counterproductive because it will force people to go to "cut-rate'' outfits like Southern California Propeller Service. We don't agree that we are "changing the rules.'' We are issuing an AD to correct unsafe conditions introduced by Southern California Propeller Services. The Code of Federal Regulations, 14 CFR part 39 allows us to issue ADs to correct unsafe conditions. While the public will incur costs to comply with this action, the action will address the unsafe conditions found in other propellers.

Request To Add Hartzell HC and HA Series Propellers to the Applicability

One commenter asks if we should add Hartzell HC series and HA series propellers to the Applicability of this AD. We don't agree that we need to add the Hartzell "HC'' or "HA'' series propellers at this time. We reviewed the repair station certificate and responses from the public, and found no evidence that Southern California Propeller Service worked on Hartzell five-bladed steel hub propellers. While we were developing Special Airworthiness Information Bulletin (SAIB) No. NE-01-09, we were advised to include a reference to Sensenich propellers (even though the repair station certificate doesn't denote them). However, if someone sends us information that documents work done by Southern California Propeller Service on propellers beyond those denoted in the AD, we will review the AD for an expanded applicability. We have not changed the propeller model numbering to maintain consistency with the NPRM and SAIB No. NE-01-09.

Request To Change the Wording in Paragraph "2(e)'' of the AD

The same commenter asks us to change the wording in paragraph "2(e)'' of the AD to read, "For Hartzell and McCauley propellers listed in Table 1 of this AD, any letter, number, or any combination of letters or numbers (or lack of a letter or number) could appear where open parentheses are shown in the model number. Model numbers could show any combination of letters or numbers where the model number contains an open parentheses with a series of numbers or letters.'' We do not agree. The suggested change adds nothing, so we choose to not alter the wording.

Request To Change the Wording in Paragraphs "2(f)'' and "2(i)'' of the AD

The same commenter asks us to change the wording in paragraph "2(f)'' of the AD from, "For propeller models listed in Table 1'' to "For propeller models addressed in Table 1 of this AD.'' The commenter also asks us to change paragraph "2(i)'' from "Perform the actions specifiedin paragraph (j) of this AD on propeller models listed in Table 1 of this AD'' to "Perform the actions specified in paragraph (j) of this AD on the propeller models addressed, regardless of serial number, in Table 1 of this AD.'' We partially agree. We will change "propellers listed in Table 1'' to "propeller models listed in Table 1'' throughout the regulatory text of the AD, specifically in paragraphs (e), (f), and (i), to maintain consistency.

Request To Ensure Compliance by Southern California Propeller Services With Previous ADs

The same commenter asks us to add an action requirement to ensure that previous ADs signed off by Southern California Propeller Service are re-evaluated, reinspected, or repeated as appropriate. We do not agree. The required actions specified in this AD are equivalent to any AD applicable to the affected propellers.

Conclusion

We have carefully reviewed the available data, including the comments received, and determined that air safety and the public interest require adopting the AD with the changes described previously. We have determined that these changes will neither increase the economic burden on any operator nor increase the scope of the AD.

Costs of Compliance

We estimate that 1,000 propellers installed on aircraft of U.S. registry will be affected by this AD and that it will cost on average about $3,000 to overhaul each propeller. Based on these figures, we estimate the total cost of the AD to U.S. operators to be $3,000,000.

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 by sending a request to us at the address listed under ADDRESSES. Include "AD Docket No. 2003-NE-53-AD'' in your request.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Safety.

Adoption of the Amendment

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

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:

Addresses

You may examine the AD docket at the FAA, New England Region, Office of the Regional Counsel, 12 New England Executive Park, Burlington, MA.

For Further Information Contact

Timothy Smyth, Aerospace Engineer, Chicago Aircraft Certification Office, FAA, Small Airplane Directorate, 2300 East Devon Avenue, Des Plaines, IL 60018-4696; telephone (847) 294-7132, fax (847) 294-7834 for Hartzell Propellers.

Contact Jeff Janusz, Aerospace Engineer, Wichita Aircraft Certification Office, FAA, Small Airplane Directorate, 1801 Airport Road, Room 100, Wichita, Kansas 67209; telephone (316) 946-4148; fax (316) 946-4107 for McCauley Propellers.

Contact James Delisio, Aerospace Engineer, New York Aircraft Certification Office, FAA, Engine and Propeller Directorate, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone (516) 228- 7321, fax (516) 794-5531 for Sensenich Propellers.

Office of Primary Responsibility
["AIR-720: Operational Safety Branch"]