[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]
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