96-14867. Airworthiness Directives; Teledyne Continental Motors and Rolls- Royce, plc O-200 Series Reciprocating Engines  

  • [Federal Register Volume 61, Number 115 (Thursday, June 13, 1996)]
    [Rules and Regulations]
    [Pages 29931-29932]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 96-14867]
    
    
    
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    DEPARTMENT OF TRANSPORTATION
    14 CFR Part 39
    
    [Docket No. 94-ANE-53; Amendment 39-9648; AD 96-12-06]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Teledyne Continental Motors and Rolls-
    Royce, plc O-200 Series Reciprocating Engines
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Final rule.
    
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    SUMMARY: This amendment supersedes two existing airworthiness 
    directives (AD's), applicable to Teledyne Continental Motors and Rolls-
    Royce, plc O-200 series reciprocating engines, that currently require 
    resetting engine timing to 24 deg. Before Top Center (BTC). This 
    amendment returns to the 28 deg. BTC engine timing for those engines 
    equipped with improved cylinders that have strengthened heads. In 
    addition, this amendment drops the TCM O-200C model which never went 
    into production. This amendment is prompted by the availability of 
    improved cylinders. The actions specified by this AD are intended to 
    prevent possible cylinder cracking with subsequent loss of engine 
    power.
    
    DATES: Effective July 18, 1996.
    
        The incorporation by reference of certain publications listed in 
    the regulations is approved by the Director of the Federal Register as 
    of July 18, 1996.
    
    ADDRESSES: The service information referenced in this AD may be 
    obtained from Teledyne Continental Motors, P.O. Box 90, Mobile, AL 
    36601; telephone (334) 438-3411. This information may be examined at 
    the Federal Aviation Administration (FAA), New England Region, Office 
    of the Assistant Chief Counsel, 12 New England Executive Park, 
    Burlington, MA 01803-5299; or at the Office of the Federal Register, 
    800 North Capitol Street, NW., suite 700, Washington, DC.
    
    FOR FURTHER INFORMATION CONTACT: Jerry Robinette, Aerospace Engineer, 
    Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate, 
    Campus Building, 1701 Columbia Ave., Suite 2-160, College Park, GA 
    30337-2748; telephone (404) 305-7371, fax (404) 305-7348.
    
    SUPPLEMENTARY INFORMATION: A proposal to amend part 39 of the Federal 
    Aviation Regulations (14 CFR part 39) by superseding airworthiness 
    directive (AD) 77-13-03, Amendment 39-2925 (42 FR 31770, June 23, 
    1977), which is applicable to Teledyne Continental Motors (TCM) O-200A, 
    O-200B, was published in the Federal Register on June 15, 1995 (60 FR 
    31421). That action proposed to retain the 24 deg. before top center 
    (BTC) engine timing for engines with cylinders that have part number 
    (P/N) lower than 641917; allow the return to 28 deg. BTC engine timing 
    for those engines with cylinder P/N 641917 and subsequent (higher) part 
    numbers, restamp the engine data plate to indicate engine timing of 
    28 deg. BTC; and drop the TCM O-200C series engines from the AD's 
    applicability. The actions must be accomplished in accordance with TCM 
    Service Bulletin (SB) No. SB94-8, dated September 14, 1994.
        This AD also supersedes AD 78-19-02, Amendment 39-3301 (43 FR 
    41374, September 18, 1978), applicable to Rolls-Royce, plc (R-R) O-
    200A, O-200B, and O-200C series engines, which also requires resetting 
    the engine timing to 24 deg.. This AD combines the TCM applicability of 
    AD 77-13-03 with the R-R applicability of AD 78-19-02 into one, 
    superseding AD.
        Interested persons have been afforded an opportunity to participate 
    in the making of this amendment.
        One commenter (the manufacturer) states that the timing adjustment 
    may be set to the limits of (+1 deg., -1 deg.). The NPRM incorrectly 
    limited the timing adjustment to (+1 deg., -0 deg.). The FAA concurs 
    and has revised this final rule accordingly.
        After careful review of the available data, including the comments 
    noted above, the FAA has determined that air safety and the public 
    interest require the adoption of the rule with the changes described 
    previously. The FAA has determined that these changes will neither 
    increase the economic burden on any operator nor increase the scope of 
    the AD.
        The FAA estimates that 23,500 engines installed on aircraft of U.S. 
    registry will be affected by this AD, that it will take approximately 2 
    work hours per engine to accomplish the required actions, and that the 
    average labor rate
    
    [[Page 29932]]
    
    is $60 per work hour. This AD adds no additional requirements; the 
    resetting of engine timing for engines with the improved cylinders is 
    optional. Therefore, there is no cost imposed by the required actions. 
    However, if the timing was reset on all applicable engines, based on 
    these figures, the total cost impact of the AD on U.S. operators is 
    estimated to be $2,820,000.
        The regulations adopted herein will not have substantial direct 
    effects 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. Therefore, in 
    accordance with Executive Order 12612, it is determined that this final 
    rule does not have sufficient federalism implications to warrant the 
    preparation of a Federalism Assessment.
        For the reasons discussed above, I certify that this action (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. A final evaluation has been prepared for this action 
    and it is contained in the Rules Docket. A copy of it 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.
    
    
    Sec. 39.13  [Amended]
    
        2. Section 39.13 is amended by removing Amendment 39-2925 (42 FR 
    31770, June 23, 1977), and Amendment 39-3301 (43 FR 41374, September 
    18, 1978), and by adding a new airworthiness directive, Amendment 39-
    9648, to read as follows:
    
    96-12-06  Teledyne Continental Motors and Rolls-Royce, plc.: 
    Amendment 39-9648. Docket 94-ANE-53. Supersedes AD 77-13-03, 
    Amendment 39-2925 and AD 78-19-02, Amendment 39-3301.
    
        Applicability: Teledyne Continental Motors (TCM) Model O-200A 
    and O-200B and Rolls-Royce, plc. Model O-200A, O-200B, and O-200C 
    reciprocating engines. These engines are installed on but not 
    limited to American Champion Models 7ECA and 402; Cessna Model 150, 
    150A through 150M, A150K through A150M; Reims Models F-150G through 
    F-150M, FA-150K and FA-150L; and Taylorcraft Model F19 aircraft.
    
        Note: This airworthiness directive (AD) applies to each engine 
    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 engines that have been 
    modified, altered, or repaired so that the performance of the 
    requirements of this AD is affected, the owner/operator must use the 
    authority provided in paragraph (g) to request approval from the 
    Federal Aviation Administration (FAA). This approval may address 
    either no action, if the current configuration eliminates the unsafe 
    condition, or different actions necessary to address the unsafe 
    condition described in this AD. Such a request should include an 
    assessment of the effect of the changed configuration on the unsafe 
    condition addressed by this AD. In no case does the presence of any 
    modification, alteration, or repair remove any engine from the 
    applicability of this AD.
    
        Compliance: Required as indicated, unless accomplished 
    previously.
        To prevent possible cylinder cracking with subsequent loss of 
    engine power, accomplish the following:
        (a) For engines that have one or more cylinders with part 
    numbers (P/N) lower than 641917, within the next 50 hours time in 
    service (TIS) after the effective date of this AD, reset the engine 
    timing to 24 deg. (+1 deg., -1 deg.) Before Top Center (BTC) on both 
    magnetos in accordance with the magneto to engine timing procedure 
    for direct drive engines in TCM Service Bulletin (SB) No. SB94-8, 
    dated September 14, 1994.
        (b) For engines that have all four cylinders with P/N 641917 or 
    higher, the engine timing may be reset to 28 deg. (+1 deg., -1 deg.) 
    BTC on both magnetos in accordance with the magneto engine timing 
    procedure for direct drive engines in TCM SB No. SB94-8, dated 
    September 14, 1994.
        (c) Subsequent installation of cylinders must be of the P/N 
    listed in paragraph (b) of this AD to retain the 28 deg. BTC timing.
    
        Note: The P/N is stamped on the cylinder barrel flange.
        (d) This AD supersedes AD 77-13-03 and AD 78-19-02.
        (e) When paragraph (a) is accomplished, restamp the engine data 
    plate to indicate magneto timing of 24 deg. BTC.
        (f) When paragraph (b) is accomplished, restamp the engine data 
    plate to indicate magneto timing of 28 deg. BTC.
        (g) 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, Atlanta Aircraft Certification 
    Office. The request should be forwarded through an appropriate FAA 
    Maintenance Inspector, who may add comments and then send it to the 
    Manager, Atlanta Aircraft Certification Office.
    
        Note: Information concerning the existence of approved 
    alternative method of compliance with this AD, if any, may be 
    obtained from the Atlanta Aircraft Certification Office.
    
        (h) Special flight permits may be issued in accordance with 
    sections 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 
    21.197 and 21.199) to operate the aircraft to a location where the 
    requirements of this AD can be accomplished.
        (i) The actions required by this AD shall be done in accordance 
    with the following service bulletin:
    
    ------------------------------------------------------------------------
                 Document No.               Pages             Date          
    ------------------------------------------------------------------------
    TCM SB No. SB94-8....................      1-6  September 14, 1994.     
      Total pages: 6.                                                       
    ------------------------------------------------------------------------
    
        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 Teledyne Continental Motors, 
    P.O. Box 90, Mobile, AL 36601; telephone (334) 438-3411. Copies may 
    be inspected at the FAA, New England Region, Office of the Assistant 
    Chief 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.
        (j) This amendment becomes effective on July 18, 1996.
    
        Issued in Burlington, Massachusetts, on May 29, 1996.
    Robert E. Guyotte,
    Acting Manager, Engine and Propeller Directorate, Aircraft 
    Certification Service.
    [FR Doc. 96-14867 Filed 6-12-96; 8:45 am]
    BILLING CODE 4910-13-U
    
    

Document Information

Effective Date:
7/18/1996
Published:
06/13/1996
Department:
Transportation Department
Entry Type:
Rule
Action:
Final rule.
Document Number:
96-14867
Dates:
Effective July 18, 1996.
Pages:
29931-29932 (2 pages)
Docket Numbers:
Docket No. 94-ANE-53, Amendment 39-9648, AD 96-12-06
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
96-14867.pdf
CFR: (1)
14 CFR 39.13