C4-4372. Airworthiness Directives; Raytheon Aircraft Corporation Beech Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) Airplanes  

  • [Federal Register Volume 69, Number 54 (Friday, March 19, 2004)]
    [Corrections]
    [Page 13127]
    From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
    [FR Doc No: C4-4372]
    
    
    -----------------------------------------------------------------------
    
    DEPARTMENT OF TRANSPORTATION
    
    Federal Aviation Administration
    
    14 CFR Part 39
    
    [Docket No. 2000-CE-09-AD; Amendment 39-13496; AD 2001-13-18 R1]
    RIN 2120-AA64
    
    
    Airworthiness Directives; Raytheon Aircraft Corporation Beech 
    Models 45 (YT-34), A45 (T-34A, B-45), and D45 (T-34B) Airplanes
    
    Correction
    
        In rule document 04-4372 beginning on page 9526 in the issue of 
    Monday, March 1, 2004, make the following correction:
    
    
    Sec.  39.13  [Corrected]
    
        On page 9528, in 39.13, the table is corrected in part to read as 
    follows:
    
    ------------------------------------------------------------------------
               Action                     When           In accordance with
    ------------------------------------------------------------------------
     * *                           * * *..............   * *
    (2) Modify each airspeed      All actions required  Not Applicable.
     indicator glass by            within 10 hours
     accomplishing the             time-in-service
     following:                    (TIS) after July 9,
                                   1999 (the effective
                                   date of AD 99-12-
                                   02), unless already
                                   accomplished.
    (i) Place a red radial line
     on each indicator glass at
     175 miles per hour (mph)
     (152 knots).
    (ii) Place a white slippage
     index mark between each
     airspeed indicator glass
     and case to visually verify
     that the glass has not
     rotated.
    (3) Mark the outside surface  All actions required  Not Applicable.
     of the ``g'' meters with      within 10 hours
     lines of approximately \1/    time-in-service
     16\-inch by \3/16\-inch, as   (TIS) after July 9,
     follows:                      1999 (the effective
                                   date of AD 99-12-
                                   02), unless already
                                   accomplished.
     * *                           * * *..............   * *
    ------------------------------------------------------------------------
    
    
    [FR Doc. C4-4372 Filed 3-18-04; 8:45 am]
    BILLING CODE 1505-01-D
    
    
    

Document Information

Published:
03/19/2004
Department:
Federal Aviation Administration
Entry Type:
Correction
Document Number:
C4-4372
Pages:
13127-13127 (1 pages)
Docket Numbers:
Docket No. 2000-CE-09-AD, Amendment 39-13496, AD 2001-13-18 R1
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
PDF File:
c4-4372.pdf
CFR: (1)
14 CFR 39.13