95-18246. Airworthiness Directives; Piper Aircraft Corporation PA28 and PA32 Series Airplanes  

  • [Federal Register Volume 60, Number 142 (Tuesday, July 25, 1995)]
    [Proposed Rules]
    [Pages 37968-37969]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: 95-18246]
    
    
    
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    DEPARTMENT OF TRANSPORTATION
    14 CFR Part 39
    
    [Docket No. 95-CE-28-AD]
    
    
    Airworthiness Directives; Piper Aircraft Corporation PA28 and 
    PA32 Series Airplanes
    
    AGENCY: Federal Aviation Administration, DOT.
    
    ACTION: Advance notice of proposed rulemaking (ANPRM).
    
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    SUMMARY: The Federal Aviation Administration (FAA) recently became 
    aware of two incidents in the Netherlands where corrosion on the wing 
    spars of Piper Aircraft Corporation (Piper) PA28 series airplanes was 
    so extensive that the wings were replaced. The corrosion, which was 
    discovered in the wing tank area, caused the wing spar material to come 
    off in flakes and strips (exfoliation). A review of the U.S. service 
    difficulty history on Piper PA28 and PA32 series airplanes revealed 
    several incidents where exfoliation corrosion was found on the wing 
    spar in the wing tank area. The purpose of this advance notice is to 
    seek comments from interested persons regarding the best action (if 
    any) to take in order to correct any possible problems with exfoliation 
    corrosion on the wing spar on Piper PA28 and PA32 series airplanes. All 
    comments will be evaluated by the FAA and the FAA will research the 
    situation to decide whether rulemaking is needed.
    
    DATES: Comments must be received on or before October 20, 1995.
    
    ADDRESSES: Submit comments in triplicate to the FAA, Central Region, 
    Office of the Assistant Chief Counsel, Attention: Rules Docket No. 95-
    CE-28-AD, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. 
    Comments may be inspected at this location between 8 a.m. and 4 p.m., 
    Monday through Friday, holidays excepted.
    
    FOR FURTHER INFORMATION CONTACT: Christina Marsh, Aerospace Engineer, 
    FAA, Atlanta Aircraft Certification Office, Campus Building, 1701 
    Columbia Avenue, suite 2-160, College Park, Georgia 30337-2748; 
    telephone (404) 305-7362; facsimile (404) 305-7348.
    
    SUPPLEMENTARY INFORMATION:
    
    Comments Invited
    
        Interested persons are invited to participate in the making of any 
    proposed rulemaking actions that may occur as a result of this ANPRM by 
    submitting such written data or views as they may desire. 
    Communications should identify the Rules Docket number and be submitted 
    in triplicate to the address specified above. All communications 
    received on or before the closing date for comments, specified above, 
    will be considered before any proposed rulemaking is initiated.
        All comments submitted will be available, both before and after the 
    closing date for comments, in the Rules Docket for examination by 
    interested persons. A report that summarizes each FAA-public contact 
    concerned with the 
    
    [[Page 37969]]
    substance of this document will be filed in the Rules Docket.
        Commenters wishing the FAA to acknowledge receipt of their comments 
    submitted in response to this notice must submit a self-addressed, 
    stamped postcard on which the following statement is made: ``Comments 
    to Docket No. 95-CE-28-AD.'' The postcard will be date stamped and 
    returned to the commenter.
    
    Availability of ANPRM's
    
        Any person may obtain a copy of this ANPRM by submitting a request 
    to the FAA, Central Region, Office of the Assistant Chief Counsel, 
    Attention: Rules Docket No. 95-CE-28-AD, Room 1558, 601 E. 12th Street, 
    Kansas City, Missouri 64106.
    
    Discussion
    
        The FAA is currently reviewing two incidents in the Netherlands 
    where corrosion on the wing spars of Piper Aircraft Corporation (Piper) 
    PA28 series airplanes was so extensive that the wings were replaced. 
    The corrosion, which was discovered in the wing tank area, caused the 
    wing spar material to come off in flakes and strips (exfoliation).
        A review of the U.S. service difficulty history on Piper PA28 and 
    PA32 series airplanes revealed several incidents where exfoliation 
    corrosion was found on the wing spar. The corrosion specified in these 
    reports showed that the exfoliation corrosion also was in the wing tank 
    area. In at least two instances, the exfoliation corrosion was found on 
    the affected airplanes upon removal of the fuel tanks during a repair.
        In order to adequately make a determination as to what type of 
    action to take (if any) regarding possible exfoliation corrosion on 
    Piper PA28 and PA32 series airplanes, the FAA is issuing this advance 
    notice of proposed rulemaking (ANPRM) to provide an opportunity for the 
    general public to participate in the decision whether to initiate 
    rulemaking. Interested persons are encouraged to provide information 
    that describes what they consider the best action (if any) to be taken 
    to correct the possible problem. In this regard, the FAA is especially 
    interested in comments and viewpoints on the following:
        1. Have you removed or had the fuel tanks removed on one of the 
    affected airplanes? If so, did you detect or was corrosion detected on 
    the wing spar (upper cap, lower cap, or web) in the fuel tank bay?
        2. Did you detect or has corrosion been detected on the main wing 
    spar in the vicinity of the fuel tanks (inboard of the fuel tank or 
    outboard of the fuel tank)? If so, where was the corrosion and how much 
    corrosion was found?
        3. Did you repair or replace the wing or has the wing been repaired 
    or replaced because of corrosion in the fuel tank area?
        4. In your opinion, how accessible is the main wing spar in the 
    vicinity of the fuel tank for inspection purposes? Would it be helpful 
    to install additional access plates inboard and outboard of the fuel 
    tank?
        5. Please provide the following:
        a. model, serial number, and total number of hours time-in-service 
    of the airplane.
        b. the present geographical location of your airplane and the known 
    geographical history of the airplane.
    
        Issued in Kansas City, Missouri, on July 17, 1995.
    Henry A. Armstrong,
    Acting Manager, Small Airplane Directorate, Aircraft Certification 
    Service.
    [FR Doc. 95-18246 Filed 7-24-95; 8:45 am]
    BILLING CODE 4910-13-U
    
    

Document Information

Published:
07/25/1995
Department:
Transportation Department
Entry Type:
Proposed Rule
Action:
Advance notice of proposed rulemaking (ANPRM).
Document Number:
95-18246
Dates:
Comments must be received on or before October 20, 1995.
Pages:
37968-37969 (2 pages)
Docket Numbers:
Docket No. 95-CE-28-AD
PDF File:
95-18246.pdf
CFR: (1)
14 CFR 39