FAA · Airworthiness Directive
Airworthiness Directives; Beech Aircraft Corporation Models 1900, 1900C, and 1900D Airplanes; Correction
Abstract
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.
Applicability
Aircraft makes and models this AD applies to, sorted by US-registered fleet size.
Federal Register text
Verbatim from the Federal Register publication — required actions, compliance times, parts/serial numbers, and methods of compliance. The Federal Register is the legally binding document; this rendering is for readability. Cite: 60 FR 10307.
[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:
-------------------------------------------------------------------------------------------------------------------------------------------------------- Area specified in figure 1 Models of Beech SB No. 2255, rev. Initial inspection Repetitive inspection VI -------------------------------------------------------------------------------------------------------------------------------------------------------- 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 -------------------------------------------------------------------------------------------------------------------------------------------------------- *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