Airworthiness Directives; Beech Aircraft Corporation Models 1900, 1900C, and 1900D Airplanes; Correction

[Federal Register Volume 60, Number 37 (Friday, February 24, 1995)]
[Rules and Regulations]
[Pages 10307-10308]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 95-4371]



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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 93-CE-41-AD; Amendment 39-9136; AD 95-02-18]


Airworthiness Directives; Beech Aircraft Corporation Models 1900, 
1900C, and 1900D Airplanes; Correction

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This action makes a correction to Airworthiness Directive (AD) 
95-02-18 concerning Beech Aircraft Corporation Models 1900, 1900C, and 
1900D airplanes, which was published in the Federal Register on 
February 3, 1995 (60 FR 6652). That publication inadvertently 
referenced an incorrect repetitive inspection interval for Models 1900 
and 1900C airplanes with a part number 129-910032-79 engine truss 
installed. The inspection interval in sections B and C of the engine 
truss should be 3,000 hours time-in-service (TIS) instead of 100 hours 
TIS. This action corrects the AD to reflect this repetitive inspection 
interval.

EFFECTIVE DATE: March 25, 1995.

FOR FURTHER INFORMATION CONTACT: Mr. Steven E. Potter, Wichita Aircraft 
Certification Office, FAA, 1801 Airport Road, Mid-Continent Airport, 
Wichita, Kansas 67209; telephone (316) 946-4124; facsimile (316) 946-
4407.

SUPPLEMENTARY INFORMATION: On January 26, 1995, the Federal Aviation 
Administration (FAA) issued AD 95-02-18, Amendment 39-9136 (60 FR 6652, 
February 3, 1995), which applies to Beech Models 1900, 1900C, and 1900D 
airplanes. This AD supersedes AD 92-06-09, Amendment 39-8189, with a 
new AD that requires repetitively inspecting the engine trusses for 
cracks, repairing or replacing any cracked engine truss, and installing 
reinforcement doublers on certain airplanes.
    The AD inadvertently references an incorrect repetitive inspection 
interval for Beech Models 1900 and 1900C airplanes with a part number 
129-910032-79 engine truss installed. The inspection interval in 
sections B and C of the engine truss should be 3,000 hours TIS instead 
of 100 hours TIS. This action corrects the AD to reflect this 
repetitive inspection interval.

Need for Correction

    As published, the final regulations have incorrectly referenced the 
repetitive inspection interval for Beech Models 1900 and 1900C 
airplanes with a part number 129-910032-79 engine truss installed. The 
way the final regulations are currently written will make operators 
repetitively inspect Sections B and C of the engine truss more often 
than was intended or proposed in the notice of proposed rulemaking.

Correction of Publication

    Accordingly, the publication of February 3, 1995 (60 FR 6652) of 
Amendment 39-9136; AD 95-02-18, which was the subject of FR Doc. 94-
2403, is corrected as follows:


Sec. 39.13  [Corrected]

    On page 6653, in paragraph (b), in the Chart that spreads across 
all three columns, change the second entry in the Repetitive Inspection 
column from ``Every 100 hours TIS.'' to ``Every 3,000 hours TIS.'' The 
chart will now read as follows:

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                                            Area specified in figure 1                                                                                  
                  Models                    of Beech SB No. 2255, rev.                  Initial inspection                      Repetitive inspection   
                                                        VI                                                                                              
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1900 and 1900C............................  A.........................  Upon accumulating 1,400 hours TIS*................  Every 100 hours TIS.        
1900 and 1900C............................   B and C..................  Upon accumulating 3,200 hours TIS*................  Every 3,000 hours TIS.      
1900D.....................................  A.........................  Upon accumulating 3,200 hours TIS*................  Every 450 hours TIS.        
1900D.....................................  B and C...................  Upon accumulating 3,200 hours TIS*................  Every 3,000 hours TIS       
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*Or within the next 100 hours TIS after the effective date of this AD, whichever occurs later.                                                          

    [[Page 10308]] Issued in Kansas City, Missouri, on February 15, 
1995.
Barry D. Clements,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 95-4371 Filed 2-23-95; 8:45 am]
BILLING CODE 4910-13-U

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