AD 2001-13-18 R1

AD Final Rules - 011318R1.pdf
Copy URL
Document Versions
 Feedback
DetailsAttachments/Public Comments
AD Number:
2001-13-18 R1
Document Type:
AD Final Rules
Docket Number:
2000-CE-09-AD
Subject Heading:
Airworthiness Directives; Raytheon Aircraft Corporation Beech Models 45 (YT-34), A45 (T-34A, B-45), ...Show more
Subject:
Wing spar assembly
Status:
Current
Citation:
Federal Register: March 1, 2004 (Volume 69, Number 40)
Citation Publish Date:
03/01/2004
Effective Date:
03/15/2004
Make:
Textron Aviation Inc.
Model:
45 (Military YT-34) | A45 (Military T-34A, B-45) | D45 (Military T-34B)
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
2001-13-18
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
CORRECTION: [Federal Register: March 19, 2004 (Volume 69, Number 54); Page 13127; www.access.gpo.gov...Show more
Automatic Zoom
Actual Size
Page Fit
Page Width
⁨50⁩%
⁨75⁩%
⁨100⁩%
⁨125⁩%
⁨150⁩%
⁨200⁩%
⁨300⁩%
⁨400⁩%
125%
of ⁨8⁩
1


[Federal Register: March 19, 2004 (Volume 69, Number 54)]


[CORRECTIONS]


[Page 13127]


From the Federal Register Online via GPO Access [wais.access.gpo.gov]


[DOCID:fr19mr04-107]


–––––––––––––––––––––––––––––––––––


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:


§ 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 indicator glass by


accomplishing the following:


(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.


All actions required within


10 hours time-in-service


(TIS) after July 9, 1999


(the effective date of AD


99–12–02), unless already


accomplished.


Not Applicable.


(3) Mark the outside surface of the ‘‘g’’ meters


with lines of approximately
 
1
 
/
16
-inch by
 
3
 
/
 
16
-


inch, as follows:


All actions required within


10 hours time-in-service


(TIS) after July 9, 1999


(the effective date of AD


99–12–02), unless already


accomplished.


Not Applicable.


* *
 
* * *
 
* *


[FR Doc. C4-4372 Filed 3-18-04; 8:45 am]


BILLING CODE 1505-01-D
2


[Federal Register: March 1, 2004 (Volume 69, Number 40)]


[Rules and Regulations]


[Page 9526-9529]


From the Federal Register Online via GPO Access [wais.access.gpo.gov]


[DOCID:fr01mr04-5]


–––––––––––––––––––––––––––––––––––


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


AGENCY:
 
Federal Aviation Administration (FAA), DOT.


ACTION:
 
Final rule; request for comments.


–––––––––––––––––––––––––––––––––––


SUMMARY:
 
The FAA is revising Airworthiness Directive (AD) 2001-13-18, which applies to


Raytheon Aircraft Corporation (Raytheon) Beech Models 45 (YT-34), A45 (T-34A, B-45), and D45


(T-34B) airplanes. AD 2001-13-18 currently requires you to repetitively inspect the wing spar


assembly for cracks and replace any wing spar assembly found cracked (unless the spar assembly has


a crack indication in the filler strip where the direction of the crack is toward the outside edge of the


filler strip). AD 2001-13-18 also requires you to report the results of the initial inspection and


maintain the flight and operating restrictions required by AD 99-12-02 until the initial inspection is


done. We approved alternative methods of compliance (AMOCs) to AD 2001-13-18. We have since


determined that those AMOCs do not address all critical areas in the wing spar assemblies and should


no longer be valid. We are issuing this revision to AD 2001-13-18 for the purpose of eliminating the


AMOCs to AD 2001-13-18. The actions of this AD are intended to prevent wing spar failure caused


by fatigue cracks in the wing spar assemblies and ensure the operational safety of the above-


referenced airplanes.


DATES:
 
This AD becomes effective on March 15, 2004.


On August 16, 2001 (66 FR 34802, July 2, 2001), the Director of the Federal Register approved


the incorporation by reference of certain publications listed in the regulation.


We must receive any comments on this AD by April 26, 2004.


ADDRESSES:
 
Use one of the following to submit comments on this AD:


•
 
By mail: FAA, Central Region, Office of the Regional Counsel, Attention: Rules Docket No.


2000-CE-09-AD, 901 Locust, Room 506, Kansas City, Missouri 64106.


•
 
By fax: (816) 329-3771.


•
 
By e-mail: 9-ACE-7-Docket@faa.gov. Comments sent electronically must contain ''Docket No.


2000-CE-09-AD'' in the subject line. If you send comments electronically as attached electronic files,


the files must be formatted in Microsoft Word 97 for Windows or ASCII.