Airworthiness Directives; Raytheon Aircraft Company 90, 99, 100, 200, and 300 Series Airplanes, 7017-7019 [05-2604]
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Federal Register / Vol. 70, No. 27 / Thursday, February 10, 2005 / Rules and Regulations
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Safety.
Adoption of the Amendment
Accordingly, pursuant to 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:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
for this AD, follow the procedures in 14 CFR
39.19. Contact the Regulations and Policy
Group, Rotorcraft Directorate, FAA, for
information about previously approved
alternative methods of compliance.
(f) This amendment becomes effective on
March 17, 2005.
Note 3: The subject of this AD is addressed
in Transport Canada (Canada) AD No. CF–
2004–03, dated February 11, 2004.
Issued in Fort Worth, Texas, on January 24,
2005.
Mark R. Schilling,
Acting Manager, Rotorcraft Directorate,
Aircraft Certification Service.
[FR Doc. 05–2589 Filed 2–9–05; 8:45 am]
BILLING CODE 4910–13–P
[Amended]
2. Section 39.13 is amended by adding
a new airworthiness directive to read as
follows:
DEPARTMENT OF TRANSPORTATION
2005–03–07 Bell Helicopter Textron
Canada (Bell): Amendment 39–13963.
Docket No. 2004–SW–07–AD.
Applicability: Model 407 helicopters, with
landing gear crosstube assemblies, part
number (P/N) 407–050–101–101 and –103; P/
N 407–050–102–101 and –103; P/N 407–050–
201–101 and –103; P/N 407–050–202–101
and –103; P/N 407–704–007–119; P/N 407–
722–101; P/N 407–723–104; P/N 407–724–
101; or P/N 407–725–104, installed,
certificated in any category.
Note 1: This AD applicability includes
both Bell crosstube assemblies and Bell’s
approved production and spare alternate
crosstube assemblies from Aeronautical
Accessories Incorporated (AAI).
Compliance: Required as indicated, unless
accomplished previously.
To prevent fatigue failure of the crosstube
assembly and subsequent loss of control of
the helicopter, accomplish the following:
(a) Before further flight, create a
component history card or equivalent record
for each crosstube assembly.
(b) Before further flight, determine and
record the accumulated Retirement Index
Number (RIN) for each crosstube assembly as
follows:
(1) For each crosstube assembly, record one
(1) RIN for every run-on landing.
(2) For any crosstube assembly with an
unknown number of run-on landings, assume
and record ten (10) RINs for each 100 hours
TIS since the crosstube assembly was
installed (for example, 5,000 hours of timein-service equals 500 RIN).
(c) Replace any crosstube assembly on or
before reaching 5,000 RIN.
Note 2: Bell Helicopter Textron Alert
Service Bulletin No. 407–03–59, dated
October 15, 2003, pertains to the subject of
this AD.
(d) This AD revises the Airworthiness
Limitations section of the maintenance
manual by establishing a retirement life of
5,000 RIN for the affected crosstube
assemblies.
(e) To request a different method of
compliance or a different compliance time
14 CFR Part 39
I
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16:15 Feb 09, 2005
Jkt 205001
Federal Aviation Administration
[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
Federal Aviation
Administration, DOT.
ACTION: Final rule; correction.
AGENCY:
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: https://
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.
SUMMARY:
PO 00000
Frm 00019
Fmt 4700
Sfmt 4700
7017
Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590–
001 or on the Internet at https://
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 reissuing 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
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:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. FAA amends § 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:
I
2005–01–04 Raytheon Aircraft Company:
Amendment 39–13928; Docket No.
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7018
Federal Register / Vol. 70, No. 27 / Thursday, February 10, 2005 / Rules and Regulations
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?
What Airplanes Are Affected by This AD?
(c) This AD affects the following airplane
models and serial numbers that are
certificated in any category:
(b) This AD supersedes AD 98–15–13,
Amendment 39–10664.
Model
Series
(1) 65–90 ............................................................
(2) 65–A90 ..........................................................
(3) B90 ................................................................
(4) C90 ................................................................
(5) C90A .............................................................
(6) C90A .............................................................
(7) E90 ................................................................
(8) F90 ................................................................
(9) H90 ................................................................
(10) 100 ..............................................................
(11) A100 ............................................................
(12) A100–1 (RU–21J) .......................................
(13) B100 ............................................................
(14) 200 ..............................................................
LJ–1 through LJ–75, and LJ–77 through LJ–113.
LJ–76, LJ–114 through LJ–317, and LJ–178A.
LJ–318 through LJ–501.
LJ–502 through LJ–1062.
LJ–1063 through LJ–1287, LJ–1289 through LJ–1294, and LJ–1296 through LJ–1299.
LJ–1288, LJ–1295, and LJ–1300 through LJ–1445.
LW–1 through LW–347.
LA–2 through LA–236.
LL–1 through LL–61.
B–2 through B–89, and B–93.
B–1, B–90 through B–92, B–94 through B–204, and B–206 through B–247.
BB–3 through BB–5.
BE–1 through BE–137
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.
BL–1 through BL–23, and BL–25 through BL–36.
BN–1.
BT–1 through BT-BT–22, and BT–28.
BC–1 through BC–75, and BD–1 through BD–30.
BJ–1 through BJ–66.
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.
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
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.
BN–2 through BN–4, BU–11, BU–12, FG–1, and FG–2.
BT–23 through BT–27, and BT–29 through BT–38
FA–1 through BA–230, and FF–1 through FF–19.
FL–1 through FL–141.
FM–1 through FM–9, and FN–1.
U–1 through U–49, U–51 through U–145, and U–147
U–146, and U–148 through U–164.
U–50, and U–165 through U–239.
(15)
(16)
(17)
(18)
(19)
(20)
200C ............................................................
200CT ..........................................................
200T ............................................................
A200 ............................................................
A200C .........................................................
A200CT .......................................................
(21) B200 ............................................................
(22) B200C .........................................................
(23)
(24)
(25)
(26)
(27)
(28)
(29)
(30)
B200CT .......................................................
B200T ..........................................................
300 ..............................................................
B300 ............................................................
B300C .........................................................
99, 99A, A99, A99A ....................................
B99 ..............................................................
C99 ..............................................................
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
VerDate jul<14>2003
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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.
PO 00000
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What Must I Do To Address This Problem?
(e) To address this problem, you must do
the following:
E:\FR\FM\10FER1.SGM
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Federal Register / Vol. 70, No. 27 / Thursday, February 10, 2005 / Rules and Regulations
7019
Actions
Compliance
Procedures
(1) For airplanes manufactured prior to January
1, 1994, check airplane maintenance records
for any MIL–H–6000B fuel hose replacement
from January 1, 1994, up to and including
the effective date of this AD.
For all affected airplanes other than the Models 99, 99A, A99, A99A, B99, and C99:
Within 200 hours time-in-service (TIS) after
August 28, 1998 (the effective date of AD
98–15–13). For all affected Models 99, 99A,
A99, A99A, B99, and C99 airplanes: Within
the next 200 hours TIS after February 22,
2005 (the effective date of this AD).
Documented compliance with AD 98–15–13 or
follow PART II of the ACCOMPLISHMENT
INSTRUCTIONS section in Raytheon Aircraft Mandatory Service Bulletin SB 2718,
Revision 1, dated June 1997; or Revision 2,
dated April 2000. An owner/operator holding
at least a private pilot certificate as authorized by section 43.7 of 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 that a MIL–H–
6000B fuel hose has been replaced, inspect
the airplane fuel hoses for a 3⁄8-inch-wide red
or orange-red, length-wise stripe, with manufacturer’s code, 94519, printed periodically
along the line in red letters on one side. The
hoses have a spiral or diagonal outer wrap
with a fabric-type texture on the rubber surface.
For all affected airplanes other than the Models 99, 99A, A99, A99A, B99, and C99:
Within 200 hours TIS after August 28, 1998
(the effective date of AD 98–15–13). For all
affected Models 99, 99A, A99, A99A, B99,
and C99 airplanes: Within the next 200
hours TIS after February 22, 2005 (the effective date of this AD).
Documented compliance with AD 98–15–13 or
follow PART II of the ACCOMPLISHMENT
INSTRUCTIONS section in Raytheon Aircraft Mandatory Service Bulletin SB 2718,
Revision 1, dated June 1997; or Revision 2,
dated April 2000.
(3) Replace any fuel hose that matches the description in paragraph (e)(2) of AD with an
FAA-approved MIL–H–6000B fuel hose that
has a criss-cross or braided external wrap.
For all affected airplanes other than the Models 99, 99A, A99, A99A, B99, and C99:
Within 200 hours TIS after August 28, 1998
(the effective date of AD 98–15–13). For all
affected Models 99, 99A, A99, A99A, B99,
and C99 airplanes: Within the next 200
hours TIS after February 22, 2005 (the effective date of this AD).
Documented compliance with this AD 98–15–
13 or follow PART II of the ACCOMPLISHMENT INSTRUCTIONS section in Raytheon
Aircraft Mandatory Service Bulletin SB
2718, Revision 1, dated June 1997; or Revision 2, dated April 2000.
(4) For Raytheon Models C90A, B200, and
B300 airplanes that were manufactured on
January 1, 1994, and after, replace the MIL–
H–6000B fuel hoses.
Within 200 hours TIS after August 28, 1998
(the effective date of AD 98–15–13).
Documented compliance with AD 98–15–13 or
follow PART I of 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 hose having spiral or diagonal external wrap with a 3⁄8-inchwide red or orange-red, length-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.
As of February 22, 2005 (the effective date of
this AD).
Not applicable.
May I Request an Alternative Method of
Compliance?
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: https://
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 https://
dms.dot.gov. The docket number is FAA–
2004–19089.
(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
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PO 00000
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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
E:\FR\FM\10FER1.SGM
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]]>Agencies
[Federal Register Volume 70, Number 27 (Thursday, February 10, 2005)]
[Rules and Regulations]
[Pages 7017-7019]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-2604]
-----------------------------------------------------------------------
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.
-----------------------------------------------------------------------
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 https://
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]]
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Actions Compliance Procedures
------------------------------------------------------------------------
(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: https://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 https://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
