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ADs updated daily at www.Tdata.com
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| 2006-18-15 | HARTZELL
PROPELLER INC.:
Amendment 39-14754. Docket No. FAA-2006-25244; Directorate Identifier 2006-NE-25-AD. |
EFFECTIVE DATE (a) This airworthiness directive (AD) becomes effective September 25, 2006. AFFECTED ADS (b) None. APPLICABILITY (c) This AD applies to Hartzell Propeller Inc. ( )HC-( )2Y( )-( ) series propellers with non-suffix serial number (SN) propeller hubs installed on Lycoming O-, IO-, LO-, and AEIO-360 series reciprocating engines. These propellers and engines could be installed on, but not limited to: ______________________________________________________________________ O-360-A1A Piper Aircraft Comanche (PA-24) Lake Aircraft Colonial (C-2, LA -4, 4A, or 4P) Mooney Aircraft Mark "20B" (M-20B) Earl Horton Pawnee (Piper PA-25) Partenavia Oscar (P-66) Siai-Marchetti (S-205) Procaer Picchio (F-15-A) S.A.A.B. Safir (91-D) Malmo Vipan (MF-10B) Aero Boero AB-180 Beagle Airedale (A-109) DeHavilland Drover (DHA-3MK3) Kingsford-Smith Bushmaster (J5-6) O-360-A1AD S.O.C.A.T.A. Tabago TB-10 O-360-A1D Piper Aircraft Comanche (PA-24) Lake Aircraft Colonial (LA -4, 4A, or 4P) Doyn Aircraft Doyn-Beech (Beech 95) Mooney Aircraft Master "21" (M-20E), Mark "20B", "20D", (M20B, M20C), Mooney Statesman (M-20G) O-360-A1F6 Cessna Aircraft Cardinal O-360-A1F6D Cessna Aircraft Cardinal 177 O-360-A1G6 Teal III, Aero TSC (1A3) Commander O-360-A1G6D Beech Aircraft Duchess 76 O-360-A1H6 Piper Aircraft Seminole (PA-44) O-360-A1P Aviat Husky O-360-A2A Avion Jodel D-140-B S.O.C.A.T.A. Rallye Commodore (MS-893) Partenavia Oscar (P-66) Beagle Husky (D5-180) (J1-U) O-360-A2D Piper Aircraft Comanche (PA-24), Cherokee "C" (PA-28 "180") Mooney Aircraft Master "21" (M-20D), Mark "21" (M-20E) O-360-A2F Dynac Aerospace Aero Commander Model 100 Corp O-360-A2G Beech Aircraft Sport O-360-A3A C.A.A.R.P.S.A.N. (M-23III) Robin Regent (DR400/180), Remorqueur (DR400/180R), R-3170 S.O.C.A.T.A. Rallye 180GT, Sportavia Sportsman (RS-180) Norman Aeroplace NAC-1 Freelance Co. Nash Aircraft Ltd. Petrel O-360-A3AD S.O.C.A.T.A. TB-10 Robin Aiglon (R-1180T) O-360-A4A Piper Aircraft Cherokee "D" (PA-28 "180") O-360-A4D Varga Kachina O-360-A4G Beech Aircraft Musketeer Custom III O-360-A4K Grumman American Tiger Beech Aircraft Sundowner 180 O-360-A4M Piper Aircraft Archer II (PA-28 "18") Valmet PIK-23 O-360-A4N Cessna Aircraft 172 (Optional) O-360-A4P Penn Yan Super Cub Conversion O-360-A5AD C. Itoh and Co. Fuji FA-200 O-360-B2C Seabird Aviation SB7L O-360-C1A Intermountain Mfg. Call Air (A-6) Co. O-360-C1E Bellanca Aircraft Scout (8GCBC-CS) O-360-C1F Maule Star Rocket MX-7-180 O-360-C1G Christen Husky (A-1) O-360-C2E Bellanca Aircraft Scout (8GCBC FP) O-360-C4F Maule MX-7-180A O-360-C4P Penn Yan Super Cub Conversion O-360-F1A6 Cessna Aircraft Cutlass RG O-360-J2A Robinson R22 IO-360-B1A Beech Aircraft Travel-Air (B-95A) Doyn Aircraft Doyn-Piper (PA -23 "200") IO-360-B1B Beech Aircraft Travel-Air (B-95B) Doyn Aircraft Doyn-Piper (PA -23 "200") Fuji (FA-200) IO-360-B1D United Consultants See-Bee IO-360-B1E Piper Aircraft Arrow (PA-28 "180R") IO-360-B1F Utva 75 IO-360-B2E C.A.A.R.P. C.A.P. (10) IO-360-B1F6 Great Lakes Trainer IO-360-B1G6 American Blimp Spector 42 IO-360-B2F6 Great Lakes Trainer LO-360-A1G6D Beech Aircraft Duchess LO-360-A1H6 Piper Aircraft Seminole (PA-44) IO-360-E1A T.R. Smith Aerostar Aircraft IO-360-M1A Diamond Aircraft DA-40 IO-360-M1B Vans Aircraft RV6, RV7, RV8 Lancair 360 AEIO-360-B1F F.F.A. Bravo (200) Grob G115/Sport-Acro AEIO-360-B1G6 Great Lakes AEIO-360-B2F Mundry CAP-10 AEIO-360-B4A Pitts S-1S AEIO-360-H1A Bellanca Aircraft Super Decathalon (8KCAB-180) AEIO-360-H1B American Champion Super Decathalon ______________________________________________________________________ (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 still applies regardless of whether these letters are present or absent in the propeller model designation. PROPELLERS NOT AFFECTED BY THIS AD (e) Hartzell Propeller Inc. ( )HC-( )2Y( )-( ) series propellers installed on the following aircraft are not affected by this AD, but are affected by AD 2001-23-08 which addresses the same unsafe condition: (1) Aerobatic aircraft (including certificated aerobatic aircraft, military trainers, or any aircraft routinely exposed to aerobatic usage). (2) Agricultural aircraft. (3) Piper PA-32( ) series aircraft with Lycoming 540 series reciprocating engines rated at 300 HP or higher. (4) Britten Norman BN-2( ) series aircraft with Lycoming 540 series reciprocating engines. UNSAFE CONDITION (f) This AD results from a report of a propeller blade separating from a propeller hub. We are issuing this AD to prevent failure of the propeller hub causing blade separation and subsequent loss of airplane control. We are issuing this AD to prevent failure of the propeller hub causing blade separation and subsequent loss of airplane control. COMPLIANCE (g) You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been done. INITIAL PROPELLER HUB EDDY CURRENT INSPECTION (ECI) (h) Within 50 operating hours time-in-service (TIS) after the effective date of this AD, perform an initial ECI of the front cylinder half of the propeller hub for cracks. (i) Use paragraphs 3.A. through 3.A.(4)(g) of the Accomplishment Instructions of Hartzell Propeller Inc. Service Bulletin (SB) HC-SB-61 -269, dated April 18, 2005, to perform the ECI inspection. (j) If any cracks are found, remove the propeller hub from service before further flight. (k) If no cracks are found, mark the propeller using paragraph 3.A.(6)(a) of the Accomplishment Instructions of Hartzell Propeller Inc. Service Bulletin (SB) HC-SB-61-269, dated April 18, 2005, to indicate compliance with Hartzell Propeller Inc. SB HC-SB-61-269, dated April 18, 2005. REPETITIVE PROPELLER HUB ECIS (l) Within every 100 operating hours TIS after the last propeller hub ECI inspection, or at every annual inspection, whichever occurs first, perform repetitive ECIs of the front cylinder half of the propeller hub for cracks. (m) If any cracks are found, remove the propeller hub from service before further flight. OPTIONAL TERMINATING ACTION (n) As optional terminating action to the repetitive ECIs required by this AD: (1) Replace the non-suffix SN propeller hub with a propeller hub identified by an "A" or "B" suffix letter in the propeller hub SN; except (2) Do not install a suffix "A" propeller hub that was previously installed on an aircraft affected by the original issue or later revision of Hartzell Propeller Inc. SB HC-SB-61-227. (3) Replacement propeller hub part numbers can be found in paragraph 2.A., Material Information, of Hartzell Propeller Inc. SB HC-SB-61-269, dated April 18, 2005. ALTERNATIVE METHODS OF COMPLIANCE (o) 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 (p) Hartzell Propeller Inc. SB HC-SB-61-227, Revision 2, dated April 18, 2005, and AD 2001-23-08 pertain to the subject of this AD. MATERIAL INCORPORATED BY REFERENCE (q) You must use Hartzell Propeller Inc. Service Bulletin HC-SB-61-269, dated April 18, 2005, to perform the ECI inspections required by this AD. The Director of the Federal Register approved the incorporation by reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. 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 copies at the FAA, New England Region, Office of the Regional Counsel, 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. Issued in Burlington, Massachusetts, on August 30, 2006. Francis A. Favara, Manager, Engine and Propeller Directorate, Aircraft Certification Service. FOR FURTHER INFORMATION CONTACT: Tim 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.
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| AGENCY: Federal Aviation
Administration (FAA), Department of Transportation (DOT).
ACTION: Final rule; request for comments. SUMMARY: The FAA is adopting a new airworthiness directive (AD) for Hartzell Propeller Inc. ( )HC-( )2Y( )-( ) series propellers with non- suffix serial number (SN) propeller hubs installed on Lycoming O-, IO-, LO-, and AEIO-360 series reciprocating engines. This AD requires initial and repetitive eddy current inspections (ECI) of the front cylinder half of the propeller hub for cracks and removing cracked hubs from service before further flight. In addition, this AD allows installation of an improved design propeller hub (suffix SN "A" or "B") as terminating action to the repetitive ECI. This AD results from a report of a propeller blade separating from a propeller hub. We are issuing this AD to prevent failure of the propeller hub causing blade separation and subsequent loss of airplane control. DATES: This AD becomes effective
September 25, 2006. The Director of the Federal Register approved the incorporation
by reference of certain publications listed in the regulations as of September
25, 2006.
ADDRESSES: Use one of the
following addresses to comment on this AD:
Contact Hartzell Propeller Inc. Technical Publications Department, One Propeller Place, Piqua, OH 45356; telephone (937) 778-4200; fax (937) 778-4391, for the service information identified in this AD. FOR FURTHER INFORMATION CONTACT: Tim 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. SUPPLEMENTARY INFORMATION: In April 2006, we received a report of a propeller blade separation on a Hartzell Propeller Inc. two blade, aluminum hub, "compact" ( )HC-( )2Y( )-( ) series propeller. Also, to date, we received seven reports of excessive vibration determined to be caused by cracks in the propeller hub fillet. Those propellers were manufactured before December 1991 (non-suffix SN propeller hubs) and are installed on Lycoming O-, IO-, LO-, and AEIO-360 series reciprocating engines. This condition, if not corrected, could result in blade separation and subsequent loss of airplane control. Relevant Service Information We have reviewed and approved the technical contents of Hartzell Propeller Inc. Service Bulletin (SB) HC-SB-61-269, dated April 18, 2005. That SB describes procedures for eddy current inspections of propeller hubs on affected propellers. That SB also lists improved design replacement propeller hub part numbers. FAA's Determination and Requirements of This AD The unsafe condition described previously
is likely to exist or develop on other Hartzell Propeller Inc.
FAA's Determination of the Effective Date Since an unsafe condition exists that requires the immediate adoption of this AD, we have found that notice and opportunity for public comment before issuing this AD are impracticable, and that good cause exists for making this amendment effective in less than 30 days. Comments Invited This AD is a final rule that involves
requirements affecting flight safety and was not preceded by notice and
an opportunity for public comment; however, we invite you to send us any
written relevant data, views, or arguments regarding this AD. Send your
comments to an address listed under ADDRESSES. Include "AD Docket No. FAA-2006-25244;
Directorate Identifier 2006-NE-25-AD" in the subject line of your comments.
We specifically invite comments on the overall regulatory, economic, environmental,
and energy aspects of the rule that might suggest a need to modify it.
Examining the AD Docket You may examine the docket that contains the AD, any comments received, and any final disposition in person at the Docket Management Facility Docket Office 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. 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.
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.
List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation
safety, Incorporation by reference, Safety.
Under 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. Sec. 39.13 [Amended] 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive: |