[Federal Register: February 10, 2005 (Volume 70, Number 27)]
[Rules and Regulations]
[Page 7017-7019]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr10fe05-8]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2000-CE-38-AD; Amendment 39-13928; AD 2005-01-04]
RIN 2120-AA64
Airworthiness Directives; Raytheon Aircraft Company 90, 99, 100,
200, and 300 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
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SUMMARY: This document incorporates corrections to Airworthiness
Directive (AD) 2005-01-04, which was published in the Federal Register
on January 6, 2005 (70 FR 1169) with regulatory corrections published
on January 27, 2005 (70 FR 3871). AD 2005-01-04 applies to certain
Raytheon Aircraft Company 90, 99, 100, 200, and 300 series airplanes.
This action incorporates the corrections into one document to help
eliminate any confusion. We are re-issuing the AD in its entirety.
EFFECTIVE DATE: The effective date of this AD remains February 22,
2005.
ADDRESSES: To get the service information identified in this AD,
contact Raytheon Aircraft Company, PO Box 85, Wichita, Kansas 67201-
0085; telephone: (800) 625-7043. To review this service information, go
to the National Archives and Records Administration (NARA). For
information on the availability of this material at NARA, go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
or call (202) 741-6030.
To view the AD docket, go to the Docket Management Facility; U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC 20590-001 or on the Internet at http://dms.dot.gov.
The docket number is FAA-2004-19089.
FOR FURTHER INFORMATION CONTACT: Jeffrey A. Pretz, Aerospace Engineer,
ACE-116W, 1801 Airport Road, Room 100, Wichita, Kansas 67209;
telephone: (316) 946-4153; facsimile: (316) 946-4407.
SUPPLEMENTARY INFORMATION:
Discussion
On December 27, 2004, FAA issued AD 2005-01-04, Amendment 39-13928
(70 FR 1169, January 6, 2005), which applies to certain Raytheon
Aircraft Company 90, 99, 100, 200, and 300 series airplanes. That AD
requires you to check the airplane maintenance records from January 1,
1994, up to and including the effective date of that AD, for any MIL-H-
6000B fuel hose replacements on the affected airplanes.
On January 20, 2005, FAA made corrections to that AD through
Federal Register publication (70 FR 3871). That AD correction changed
the model number C90B in the applicability section to C90A.
Need for This Action
For clarity purposes, FAA is incorporating the original AD
publication and the correction into one document to help eliminate any
confusion. Consequently, we are re-issuing the AD in its entirety.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the Federal Aviation Administration amends part 39 of the Federal
Aviation Regulations (14 CFR part 39) as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. FAA amends Sec. 39.13 by removing Airworthiness Directive (AD) 98-
15-13, Amendment 39-10664 (63 FR 38295-98, July 16, 1998), and by
adding a new AD to read as follows:
2005-01-04 Raytheon Aircraft Company: Amendment 39-13928; Docket No.
[[Page 7018]]
FAA-2004-19089; Directorate Identifier 2000-CE-38-AD.
When Does This AD Become Effective?
(a) The effective date of this AD (2005-01-04) remains February
22, 2005.
What Other ADs Are Affected by This Action?
(b) This AD supersedes AD 98-15-13, Amendment 39-10664.
What Airplanes Are Affected by This AD?
(c) This AD affects the following airplane models and serial
numbers that are certificated in any category:
------------------------------------------------------------------------
Model Series
------------------------------------------------------------------------
(1) 65-90.................... LJ-1 through LJ-75, and LJ-77 through LJ-
113.
(2) 65-A90................... LJ-76, LJ-114 through LJ-317, and LJ-
178A.
(3) B90...................... LJ-318 through LJ-501.
(4) C90...................... LJ-502 through LJ-1062.
(5) C90A..................... LJ-1063 through LJ-1287, LJ-1289 through
LJ-1294, and LJ-1296 through LJ-1299.
(6) C90A..................... LJ-1288, LJ-1295, and LJ-1300 through LJ-
1445.
(7) E90...................... LW-1 through LW-347.
(8) F90...................... LA-2 through LA-236.
(9) H90...................... LL-1 through LL-61.
(10) 100..................... B-2 through B-89, and B-93.
(11) A100.................... B-1, B-90 through B-92, B-94 through B-
204, and B-206 through B-247.
(12) A100-1 (RU-21J)......... BB-3 through BB-5.
(13) B100.................... BE-1 through BE-137
(14) 200..................... BB-2, BB-6 through BB-185, BB-187 through
BB-202, BB-204 through BB-269, BB-271
through BB-407, BB-409 through BB-468,
BB-470 through BB-488, BB-490 through BB-
509, BB-511 through BB-529, BB-531
through BB-550, BB-552 through BB-562,
BB-564 through BB-572, BB-574 through BB-
590, BB-592 through BB-608, BB-610
through BB-626, BB-628 through BB-646,
BB-648 through BB-664, BB-735 through BB-
792, BB-794 through BB-797, BB-799
through BB-822, BB-824 through BB-828,
BB-830 through BB-853, BB-872, BB-873,
BB-892, BB-893, and BB-912.
(15) 200C.................... BL-1 through BL-23, and BL-25 through BL-
36.
(16) 200CT................... BN-1.
(17) 200T.................... BT-1 through BT-BT-22, and BT-28.
(18) A200.................... BC-1 through BC-75, and BD-1 through BD-
30.
(19) A200C................... BJ-1 through BJ-66.
(20) A200CT.................. BP-1, BP-7 through BP-11, BP-22, BP-24
through BP-63, FC-1 through FC-3, FE-1
through FE-36, and GR-1 through GR-19.
(21) B200.................... BB-829, BB-854 through BB-870, BB-874
through BB-891, BB-894, BB-896 through
BB-911, BB-913 through BB-990, BB-992
through BB-1051, BB-1053 through BB-
1092, BB-1094, BB-1095, BB-1099 through
BB-1104, BB-1106 through BB-1116, BB-
1118 through BB-1184, BB-1186 through BB-
1263, BB-1265 through BB-1288, BB-1290
through BB-1300, BB-1302 through BB-
1425, BB-1427 through BB-1447, BB-1449,
BB-1450, BB-1452, BB-1453, BB-1455, BB-
1456, and BB-1458 through BB-1536
(22) B200C................... BL-37 through BL-57, BL-61 through BL-
140, BU-1 through BU-10, BV-1 through BV-
12, and BW-1 through BW-21.
(23) B200CT.................. BN-2 through BN-4, BU-11, BU-12, FG-1,
and FG-2.
(24) B200T................... BT-23 through BT-27, and BT-29 through BT-
38
(25) 300..................... FA-1 through BA-230, and FF-1 through FF-
19.
(26) B300.................... FL-1 through FL-141.
(27) B300C................... FM-1 through FM-9, and FN-1.
(28) 99, 99A, A99, A99A...... U-1 through U-49, U-51 through U-145, and
U-147
(29) B99..................... U-146, and U-148 through U-164.
(30) C99..................... U-50, and U-165 through U-239.
------------------------------------------------------------------------
What Is the Unsafe Condition Presented in This AD?
(d) This AD is the result of blockage of fuel hose due to hose
delamination. The actions specified in this AD are intended to
prevent fuel flow interruption, which could lead to uncommanded loss
of engine power and loss of control of the airplane.
What Must I Do To Address This Problem?
(e) To address this problem, you must do the following:
[[Page 7019]]
------------------------------------------------------------------------
Actions Compliance Procedures
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(1) For airplanes manufactured For all affected Documented
prior to January 1, 1994, check airplanes other compliance with
airplane maintenance records than the Models AD 98-15-13 or
for any MIL-H-6000B fuel hose 99, 99A, A99, follow PART II of
replacement from January 1, A99A, B99, and the
1994, up to and including the C99: Within 200 ACCOMPLISHMENT
effective date of this AD. hours time-in- INSTRUCTIONS
service (TIS) section in
after August 28, Raytheon Aircraft
1998 (the Mandatory Service
effective date of Bulletin SB 2718,
AD 98-15-13). For Revision 1, dated
all affected June 1997; or
Models 99, 99A, Revision 2, dated
A99, A99A, B99, April 2000. An
and C99 owner/operator
airplanes: Within holding at least
the next 200 a private pilot
hours TIS after certificate as
February 22, 2005 authorized by
(the effective section 43.7 of
date of this AD). the Federal
Aviation
Regulations (14
CFR 43.7), and
must be entered
into the aircraft
records showing
compliance with
this AD in
accordance with
section 43.7 of
the Federal
Aviation
Regulations (14
CFR 43.9) can
accomplish
paragraph (e)(1)
required of this
AD.
---------------------------------
(2) If the airplane records show For all affected Documented
that a MIL-H-6000B fuel hose airplanes other compliance with
has been replaced, inspect the than the Models AD 98-15-13 or
airplane fuel hoses for a \3/8\- 99, 99A, A99, follow PART II of
inch-wide red or orange-red, A99A, B99, and the
length-wise stripe, with C99: Within 200 ACCOMPLISHMENT
manufacturer's code, 94519, hours TIS after INSTRUCTIONS
printed periodically along the August 28, 1998 section in
line in red letters on one (the effective Raytheon Aircraft
side. The hoses have a spiral date of AD 98-15- Mandatory Service
or diagonal outer wrap with a 13). For all Bulletin SB 2718,
fabric-type texture on the affected Models Revision 1, dated
rubber surface. 99, 99A, A99, June 1997; or
A99A, B99, and Revision 2, dated
C99 airplanes: April 2000.
Within the next
200 hours TIS
after February
22, 2005 (the
effective date of
this AD).
---------------------------------
(3) Replace any fuel hose that For all affected Documented
matches the description in airplanes other compliance with
paragraph (e)(2) of AD with an than the Models this AD 98-15-13
FAA-approved MIL-H-6000B fuel 99, 99A, A99, or follow PART II
hose that has a criss-cross or A99A, B99, and of the
braided external wrap. C99: Within 200 ACCOMPLISHMENT
hours TIS after INSTRUCTIONS
August 28, 1998 section in
(the effective Raytheon Aircraft
date of AD 98-15- Mandatory Service
13). For all Bulletin SB 2718,
affected Models Revision 1, dated
99, 99A, A99, June 1997; or
A99A, B99, and Revision 2, dated
C99 airplanes: April 2000.
Within the next
200 hours TIS
after February
22, 2005 (the
effective date of
this AD).
---------------------------------
(4) For Raytheon Models C90A, Within 200 hours Documented
B200, and B300 airplanes that TIS after August compliance with
were manufactured on January 1, 28, 1998 (the AD 98-15-13 or
1994, and after, replace the effective date of follow PART I of
MIL-H-6000B fuel hoses. AD 98-15-13). ACCOMPLISHMENT
INSTRUCTIONS
section in
Raytheon Aircraft
Mandatory Service
Bulletin SB 2718,
Revision 1, dated
June 1997; or
Revision 2, dated
April 2000.
---------------------------------
(5) Do not install a rubber fuel As of February 22, Not applicable.
hose having spiral or diagonal 2005 (the
external wrap with a \3/8\-inch- effective date of
wide red or orange-red, length- this AD).
wise stripe running down the
side of the hose, with the
manufacturer's code, 94519,
printed periodically along the
line in red letters on any of
the affected airplanes.
------------------------------------------------------------------------
May I Request an Alternative Method of Compliance?
(f) You may request a different method of compliance or a
different compliance time for this AD by following the procedures in
14 CFR 39.19. Unless FAA authorizes otherwise, send your request to
your principal inspector. The principal inspector may add comments
and will send your request to the Manager, Standards Office, Small
Airplane Directorate, FAA. For information on any already approved
alternative methods of compliance, contact Jeffrey A. Pretz,
Aerospace Engineer, ACE-116W, 1801 Airport Road, Room 100, Wichita,
Kansas 67209; telephone: (316) 946-4153; facsimile: (316) 946-4407.
Does This AD Incorporate Any Material by Reference?
(g) You must do the actions required by this AD following the
instructions in Raytheon Aircraft Mandatory Service Bulletin SB
2718, Revision 1, dated June 1997; or Revision 2, dated April 2000.
The Director of the Federal Register approved the incorporation by
reference of this service bulletin in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. To get a copy of this service information,
contact Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas
67201-0085; telephone: (800) 625-7043. To review copies of this
service information, go to the National Archives and Records
Administration (NARA). For information on the availability of this
material at NARA, go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
or call (202)
741-6030. To view the AD docket, go to the Docket Management
Facility; U.S. Department of Transportation, 400 Seventh Street,
SW., Nassif Building, Room PL-401, Washington, DC 20590-0001 or on
the Internet at http://dms.dot.gov. The docket number is FAA-2004-
19089.
Issued in Kansas City, Missouri, on February 4, 2005.
Nancy C. Lane,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-2604 Filed 2-9-05; 8:45 am]
BILLING CODE 4910-13-P