Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes, 13538-13541 [06-2546]
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Federal Register / Vol. 71, No. 51 / Thursday, March 16, 2006 / Rules and Regulations
adequate stall warning when in icing
conditions.’’
Disregard any mention of approval for
flight in icing conditions within the POH/
AFM.’’
Appendix 3 to AD 2006–06–06—Cessna
Model 208 Airplanes and Model 208B
Airplanes, Equipped With Airframe
Deicing Pneumatic Boots, That Are Not
Currently Prohibited From Flight in
Known or Forecast Icing
Install a placard with black letters on a
white background. The placard shall be
located on the instrument panel in one of the
following areas: Under the radio stack,
immediately above the pilot’s flight
instruments, or below the pilot’s vertical
speed indicator. Lettering on the placard
shall be a minimum 1⁄8-inch tall and state the
following:
‘‘Continued flight after encountering
moderate or greater icing conditions is
prohibited. One or more of the following
defines moderate icing conditions for this
airplane:
Airspeed in level flight at constant power
decreases by 20 KIAS.
Engine torque required to maintain airspeed
increases by 400 ft. lbs.
120 KIAS cannot be maintained in level
flight.
Ice accretion of 1⁄4 inch observed on the wing
strut.’’
HSROBINSON on PROD1PC70 with RULES
Appendix 4 to AD 2006–06–06—
Changes to the Cessna Models 208 or
208B Pilot’s Operating Handbook (POH)
and FAA-Approved Airplane Flight
Manual Supplement S1
Affected Cessna Models 208 or 208B Pilot’s
Operating Handbook (POH) and FAAApproved Airplane Flight Manual (AFM)
and FAA-Approved Supplement S1
Insert the following text into the
LIMITATIONS section under the ‘‘AIRSPEED
LIMITATIONS’’ paragraph of the Cessna
Models 208 or 208B Pilot’s Operating
Handbook (POH) and FAA-Approved
Airplane Flight Manual (AFM), and Replace
the text in the KNOWN ICING EQUIPMENT
SUPPLEMENT S1 under the ‘‘MINIMUM
SPEED IN ICING CONDITIONS’’ paragraph
with the following text. This may be done by
inserting a copy of this AD into the POH/
AFM:
Minimum airspeed in icing conditions, for
all flight phases including approach, except
takeoff and landing:
Flaps up: 120 KIAS
Flaps 10°: 105 KIAS
Flaps 20°: 95 KIAS
Exception for flaps up: when climbing to
exit icing conditions airspeed can be reduced
to 110 KIAS minimum.
Flaps must be extended during all phases
(takeoff and landing included) at airspeeds
below 110 KIAS, except adhere to published
AFM procedures when operating with
ground deicing/anti-icing fluid applied.
WARNING
The aural stall warning system does not
function properly in all icing conditions and
should not be relied upon to provide
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Note: These are minimum speeds for
operations in icing conditions. Disregard any
reference to the original speeds within the
POH/AFM.
Appendix 5 to AD 2006–06–06—
Changes to the Cessna Models 208 or
208B Pilot’s Operating Handbook (POH)
and FAA-Approved Airplane Flight
Manual Supplement S1
Replace the text in the PERFORMANCE
section of the POH/AFM KNOWN ICING
EQUIPMENT SUPPLEMENT S1 under the
‘‘STALL SPEEDS’’ paragraph with the
following text:
‘‘Ice accumulation on the airframe may
result in a 20 KIAS increase in stall speed.
Either buffet or aural stall warning should be
treated as an imminent stall.’’
‘‘WARNING—The aural stall warning
system does not function properly in all icing
conditions and should not be relied upon to
provide adequate stall warning when in icing
conditions.’’
Issued in Kansas City, Missouri, on March
10, 2006.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 06–2544 Filed 3–15–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–21275; Directorate
Identifier 2005–CE–28–AD; Amendment 39–
14515; AD 2006–01–11 R1]
RIN 2120–AA64
Airworthiness Directives; The Cessna
Aircraft Company Models 208 and
208B Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
SUMMARY: This document clarifies the
intent of AD 2006–01–11, which was
published in the Federal Register on
January 12, 2006 (71 FR 1941). AD
2006–01–11 applies to Cessna Models
208 and 208B airplanes and requires the
installation of a pilot assist handle and
deicing boots on the cargo pod and
landing gear fairings; and the
incorporation of changes to the Pilot’s
Operating Handbook (POH) and FAAApproved Airplane Flight Manual
(AFM). The compliance time for the
AFM/POH change currently reads
‘‘prior to further flight’’ after the
installation of the pilot assist handle,
which is required within 125 days after
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the effective date. The AFM/POH
change is related to operation in ground
icing conditions and should not be
attributed to the pilot assist handle
installation. Therefore, the compliance
time should also be within 125 days
after the effective date. Additionally, the
requirement of installing the accessory
kit or installing a placard should only
apply to those airplanes equipped with
a cargo pod and pneumatic deicing
boots. The way it currently is written
makes it apply to all airplanes equipped
with pneumatic deicing boots. This AD
action rewords the compliance time and
the wording for the installation or
placard requirement to reflect the above
concerns.
DATES: The effective date of this AD
remains February 22, 2006.
As of February 22, 2006, the Director
of the Federal Register previously
approved the incorporation by reference
of certain publications listed in the
regulation.
ADDRESSES: To get the service
information identified in this AD,
contact The Cessna Aircraft Company,
Product Support, P.O. Box 7706,
Wichita, Kansas 67277–7706; telephone:
(316) 517–5800; facsimile: (316) 942–
9006.
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–2005–21275; Directorate Identifier
2005–CE–28–AD.
FOR FURTHER INFORMATION CONTACT: Paul
Pellicano, Aerospace Engineer (Icing),
FAA, Small Airplane Directorate, c/o
Atlanta Aircraft Certification Office
(ACO), One Crown Center, 1985
Phoenix Boulevard, Suite 450, Atlanta,
GA 30349; telephone: (770) 703–6064;
facsimile: (770) 703–6097; or Robert P.
Busto, Aerospace Engineer, Wichita
ACO, FAA, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946–
4157; facsimile: (316) 946–4107.
SUPPLEMENTARY INFORMATION:
Discussion
What Prior Action Did FAA Take on
This Subject?
On January 5, 2006, FAA issued AD
2006–01–11, Amendment 39–14450 (71
FR 1941, January 12, 2006), which
applies to certain Cessna Models 208
and 208B airplanes.
AD 2006–01–11 requires:
• Installation of a pilot assist handle
(part number (P/N) SK208–146–2) (or
FAA-Approved equivalent part number)
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Federal Register / Vol. 71, No. 51 / Thursday, March 16, 2006 / Rules and Regulations
and deicing boots on the cargo pod and
landing gear fairings (part number (P/N)
AK208–6C) (or FAA-approved
equivalent part number); and
• Incorporation of changes to the
Pilot’s Operating Handbook (POH) and
FAA-approved Airplane Flight Manual
(AFM).
Why Is It Necessary To Change AD
2006–01–11?
The compliance time for the AFM/
POH change currently reads ‘‘prior to
further flight’’ after the installation of
the pilot assist handle, which is
required within 125 days after the
effective date. The AFM/POH change is
related to operation in ground icing
conditions and should not be attributed
to the pilot assist handle installation.
Therefore, the compliance time should
also be within 125 days after the
effective date. Additionally, the
requirement of installing the accessory
kit or installing a placard should only
apply to those airplanes equipped with
a cargo pod and pneumatic deicing
boots. The way it currently is written
makes it apply to all airplanes equipped
with pneumatic deicing boots. This
installation is not possible for those
airplanes that are not equipped with a
cargo pod and pneumatic deicing boots.
Correction of Publication
What Is the Purpose of This Document?
This document clarifies AD 2006–01–
11 to allow compliance with the AD and
assure the intent of the current AD is
clear. It also adds the amendment to
13539
section 39.13 of the Federal Aviation
Regulations (14 CFR 39.13).
We are clarifying and re-issuing the
AD in its entirety to help eliminate any
confusion that AD 2006–01–11 may
have created.
January 12, 2006), and by adding a new
AD to read as follows:
Is It Necessary To Seek Public Input?
Since this action only clarifies the
intent, it has no adverse economic
impact and imposes no additional
burden on any person than would have
been necessary to comply with AD
2006–01–11. Therefore, FAA has
determined that prior notice and
opportunity for public comment are
unnecessary.
When Does This AD Become Effective?
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
(c) This AD affects Models 208 and 208B,
all serial numbers, that are certificated in any
category.
Adoption of the Amendment
(d) This AD is the result of reports of
several accidents involving the affected
airplanes during operations in-flight and in
ground icing conditions. We are issuing this
AD to provide a safe method to detect ice,
snow, frost, or slush adhering to the upper
wing (a critical surface) prior to takeoff; and
to reduce drag in-flight by shedding ice on
the cargo pod and landing gear fairings. Ice
adhering to the upper wing surface, cargo
pod, or landing gear fairings could result in
a reduction in airplane performance with the
consequences that the airplane cannot
perform a safe takeoff or climb or maintain
altitude.
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) 2006–01–
11, Amendment 39–14450 (71 FR 1941,
I
2006–01–11 R1 The Cessna Aircraft
Company: Amendment 39–14515;
Docket No. FAA–2005–21275;
Directorate Identifier 2005–CE–28–AD.
(a) This AD becomes effective on February
22, 2006. The effective date of this AD is
retained from AD 2006–01–11.
What Other ADs Are Affected by This
Action?
(b) This AD revises AD 2006–01–11,
Amendment 39–14450.
What Airplanes Are Affected by This AD?
What Is the Unsafe Condition Presented in
This AD?
What Must I Do To Address This Problem?
(e) To address this problem, you must do
the following:
Compliance
Procedures
(1) Install the pilot assist handle SK208–146–2
subkit (part number (P/N) SK208–146–2) (or
FAA-approved equivalent part number) if the
airplane will be operated in the ground icing
conditions defined under ‘‘Visual/Tactile
Check’’ in the LIMITATIONS section of the
AFM after the compliance time.
(2) 14 CFR 21.303 allows for replacement parts
through parts manufacturer approval (PMA).
The phrase ‘‘or FAA-approved equivalent part
number’’ in this AD is intended to signify
those parts that are PMA parts approved
through identicality to the design of the part
under the type certificate and parts to correct
the unsafe condition under PMA (other than
identicality). Equivalent replacement parts to
correct the unsafe condition under PMA
(other than identicality) may also be installed
provided they meet current airworthiness
standards, which include those actions cited
in this AD.
HSROBINSON on PROD1PC70 with RULES
Actions
Within the next 125 days after February 22,
2006 (the effective date of this AD), unless
already done.
Install the pilot assist handle SK208–146–2
subkit (part number (P/N) SK208–146–2)
(or FAA-approved equivalent part number)
following step 4 of the Accomplishment Instructions of Cessna Caravan Service Kit
No. SK208–146, dated October 4, 2004.
Not Applicable ..................................................
Not Applicable.
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13540
Federal Register / Vol. 71, No. 51 / Thursday, March 16, 2006 / Rules and Regulations
Compliance
Procedures
(3) Insert the text in Appendix 1 of this AD after
the ‘‘OTHER LIMITATIONS’’ in the LIMITATIONS section of the Cessna Models 208 or
208B Pilot’s Operating Handbook (POH) and
FAA-approved Airplane Flight Manual (AFM).
Within the next 125 days after February 22,
2006 (the effective date of this AD) unless
already done.
(4) For Cessna Model 208B with Pratt & Whitney of Canada Ltd., PT6A–114 Turbo Prop
engine installed (600 SHP) or equipped with
a cargo pod and pneumatic deicing boots, do
one of the following:
(i) Install Cessna Accessory Kit AK208–6C
per Cessna Service Bulletin CAB95–19;
or.
(ii) Install a placard in view of the pilot
which states ‘‘This airplane is prohibited
from flight in known or forecast icing’’.
Within the next 125 days after February 22,
2006 (the effective date of this AD), unless
already done.
(5) For all Cessna Model 208 and 208B airplanes equipped with a cargo pod and pneumatic deicing boots and not included in paragraph (e)(4) of this AD, do one of the following:
(i) Install Cessna Accessory Kit AK208–6C
per Cessna Service Bulletin CAB93–20
Revision 1; or
(ii) Install a placard in view of the pilot with
the following words: ‘‘This airplane is
prohibited from flight in known or forecast icing’’.
Within the next 125 days after February 22,
2006 (the effective date of this AD), unless
already done.
(6) Insert the text in Appendix 2 of this AD in
the ‘‘KINDS OF OPERATION LIMITS’’ in the
LIMITATIONS section of the Cessna Models
208 or 208B Pilot’s Operating Handbook
(POH) and FAA-approved Airplane Flight
Manual (AFM).
HSROBINSON on PROD1PC70 with RULES
Actions
Before further flight after compliance to paragraph (e)(4)(i) or (e)(5)(i) of this AD.
(7) Delete the text in Appendix 3 of this AD
from the ‘‘REQUIRED EQUIPMENT’’ in the
LIMITATIONS section of the Cessna Models
208 or 208B Pilot’s Operating Handbook
(POH) and FAA-approved Airplane Flight
Manual (AFM) Supplement S1 ‘‘Known Icing
Equipment’’.
Before further flight after compliance to paragraph (e)(4)(i) or (e)(5)(i) of this AD.
The owner/operator holding at least a private
pilot certificate as authorized by section
43.7 of the Federal Aviation Regulations
(14 CFR 43.7) may insert the information
into the POH as specified in paragraph
(e)(3) of this AD. You may insert a copy of
this AD into the appropriate sections of the
POH to comply with this action. Make an
entry into the aircraft records showing compliance with portion of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9).
Install the cargo pod and landing gear fairing
deice kit (part number (P/N) AK208–6C2)
(or FAA-approved equivalent part number)
following the Installation Instructions of
Cessna Caravan Service Bulletin No.
CAB95–19, dated October 13, 1995, and
Cessna Caravan Accessory Kit No. AK208–
6C, Revision C, dated August 27, 1993.
The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the Federal Aviation Regulations (14 CFR 43.7) may install the placard
as specified in paragraph (e)(4) of this AD.
You may insert a copy of this AD into the
appropriate sections of the POH to comply
with this action. Make an entry into the aircraft records showing compliance with portion of the AD in accordance with section
43.9 of the Federal Aviation Regulations
(14 CFR 43.9).
Do the installation following the Installation Instructions of Cessna Caravan Service Bulletin No. CAB93–20, Revision 1, dated October 13, 1995, and Cessna Caravan Accessory Kit No. AK208–6C, Revision C,
issued August 27, 1993. The owner/operator holding at least a private pilot certificate as authorized by section 43.7 of the
Federal Aviation Regulations (14 CFR 43.7)
may install the placard as specified in paragraph (e)(5)(ii) of this AD. Make an entry
into the aircraft records showing compliance
with portion of the AD in accordance with
section 43.9 of the Federal Aviation Regulations (14 CFR 43.9).
The owner/operator holding at least a private
pilot certificate as authorized by section
43.7 of the Federal Aviation Regulations
(14 CFR 43.7) may insert the information
into the POH as specified in paragraph
(e)(3) of this AD. You may insert a copy of
this AD into the appropriate sections of the
POH to comply with this action. Make an
entry into the aircraft records showing compliance with portion of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9).
The owner/operator holding at least a private
pilot certificate as authorized by section
43.7 of the Federal Aviation Regulations
(14 CFR 43.7) may insert the information
into the POH as specified in paragraph
(e)(3) of this AD. You may insert a copy of
this AD into the appropriate sections of the
POH to comply with this action. Make an
entry into the aircraft records showing compliance with portion of the AD in accordance with section 43.9 of the Federal Aviation Regulations (14 CFR 43.9).
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Federal Register / Vol. 71, No. 51 / Thursday, March 16, 2006 / Rules and Regulations
Note: Cessna Caravan Service Bulletin No.
CAB04–9, dated October 4, 2004, also
addresses the installation of the pilot assist
handle.
May I Request an Alternative Method of
Compliance?
(f) The Manager, Wichita Aircraft
Certification Office (ACO), FAA, has the
authority to approve alternative methods of
compliance for this AD, if requested using
the procedures found in 14 CFR 39.19. For
information on any already approved
alternative methods of compliance, contact
Paul Pellicano, Aerospace Engineer (Icing),
FAA, Small Airplane Directorate, c/o Atlanta
ACO, One Crown Center, 1985 Phoenix
Boulevard, Suite 450, Atlanta, GA 30349;
telephone: (770) 703–6064; facsimile: (770)
703–6097; or Robert P. Busto, Aerospace
Engineer, Wichita ACO, FAA, 1801 Airport
Road, Wichita, Kansas 67209; telephone:
(316) 946–4157; facsimile: (316) 946–4107.
Does This AD Incorporate Any Material by
Reference?
(g) You must do the actions required by
this AD following the instructions in Cessna
Caravan Service Kit No. SK208–146, dated
October 4, 2004, and Cessna Caravan
Accessory Kit No. AK208–6C, Revision C,
dated August 27, 1993.
(1) On February 22, 2006 (71 FR 1941,
January 12, 2006), and in accordance with 5
U.S.C. 552(a) and 1 CFR part 51, the Director
of the Federal Register previously approved
the incorporation by reference of Cessna
Caravan Service Kit No. SK208–146, dated
October 4, 2004, and Cessna Caravan
Accessory Kit No. AK208–6C, Revision C,
dated August 27, 1993.
(2) To get a copy of this service
information, contact The Cessna Aircraft
Company, Product Support, P.O. Box 7706,
Wichita, Kansas 67277–7706; telephone:
(316) 517–5800; facsimile: (316) 942–9006.
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 20590–001 or on the Internet at https://
dms.dot.gov. The docket number is FAA–
2005–21275; Directorate Identifier 2005–CE–
28–AD.
HSROBINSON on PROD1PC70 with RULES
Appendix 1 to AD 2006–01–11 R1
Changes to the Cessna Models 208 or
208B Pilot’s Operating Handbook (POH)
and FAA-Approved Airplane Flight
Manual
Affected Cessna Models 208 or 208B Pilot’s
Operating Handbook (POH) and FAAApproved Airplane Flight Manual (AFM)
Insert the following text after the ‘‘OTHER
LIMITATIONS’’ in the LIMITATIONS section
of the Cessna Models 208 or 208B Pilot’s
Operating Handbook (POH) and FAAApproved Airplane Flight Manual (AFM):
COLD WEATHER OPERATIONS.
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14:40 Mar 15, 2006
Jkt 208001
The airplane must be equipped with the
following equipment when operating at an
airport in the ground icing conditions
defined under ‘‘Visual/Tactile Check’’ in the
LIMITATIONS section:
1. Pilot assist handle, Cessna P/N SK208–
146–2 (or FAA-approved equivalent part
number).
Appendix 2 to AD 2006–01–11 R1
Changes to the Cessna Models 208 or
208B Pilot’s Operating Handbook (POH)
and FAA-Approved Airplane Flight
Manual
Affected Cessna Models 208 or 208B Pilot’s
Operating Handbook (POH) and FAAApproved Airplane Flight Manual (AFM)
Add the following to the equipment listed
under ‘‘FLIGHT INTO KNOWN ICING’’ in
the ‘‘KINDS OF OPERATION LIMITS’’ in the
LIMITATIONS section of the FAA-Approved
Airplane Flight Manual:
Lower main landing gear leading edge deice
boots
Cargo pod nosecap deice boot
Appendix 3 to AD 2006–01–11 R1
Changes to the Cessna Models 208 or
208B Pilot’s Operating Handbook (POH)
and FAA-Approved Airplane Flight
Manual Supplement S1
Affected Cessna Models 208 or 208B Pilot’s
Operating Handbook (POH) and FAAApproved Airplane Flight Manual (AFM)
Supplement S1
Remove the paragraph under ‘‘REQUIRED
EQUIPMENT’’ in the Limitations section of
the FAA-Approved Flight Manual
Supplement S1 ‘‘Known Icing Equipment’’,
that currently reads as follows:
‘‘The following additional equipment is
not required for flight into icing conditions
as defined by FAR 25, but may be installed
on early serial airplanes by using optional
accessory Kit AK208–6. On later serial
airplanes, this equipment may be included
with the flight into known icing package. If
installed, this equipment must be fully
operational:’’
Issued in Kansas City, Missouri, on March
10, 2006.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 06–2546 Filed 3–15–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF HEALTH AND
HUMAN SERVICES
Food and Drug Administration
21 CFR Parts 510, 520, 522, 524, and
529
New Animal Drugs; Change of
Sponsor’s Drug Labeler Code
AGENCY:
Food and Drug Administration,
HHS.
PO 00000
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13541
Final rule; technical
amendment.
ACTION:
SUMMARY: The Food and Drug
Administration (FDA) is amending the
animal drug regulations to reflect a
change of drug labeler code for MedPharmex, Inc.
DATES: This rule is effective March 16,
2006.
FOR FURTHER INFORMATION CONTACT:
Charles Eastin, Center for Veterinary
Medicine (HFV–210), Food and Drug
Administration, 7519 Standish Pl.,
Rockville, MD 20855, 240–276–9077, email: charles.eastin@fda.hhs.gov.
SUPPLEMENTARY INFORMATION: FDA has
found that the animal drug regulations
do not reflect the correct drug labeler
code for Med-Pharmex, Inc.
Accordingly, the agency is amending
the regulations in 21 CFR 510.600,
520.1044a, 520.1195, 520.1484,
520.1485, 520.2220a, 520.2345d,
522.900, 524.1044b, 524.1044f,
524.1044g, 524.1193, 524.1443,
524.1580b, 524.1580e, 524.1600a,
524.2481, and 529.1044b to correct this
error. In addition, 21 CFR 524.1044b,
524.1044f, 524.1443, and 524.2481 are
being revised to reflect a current format.
This rule does not meet the definition
of ‘‘rule’’ in 5 U.S.C. 804(3)(A) because
it is a rule of ‘‘particular applicability.’’
Therefore, it is not subject to the
congressional review requirements in 5
U.S.C. 801–808.
List of Subjects
21 CFR Part 510
Administrative practice and
procedure, Animal drugs, Labeling,
Reporting and recordkeeping
requirements.
21 CFR Parts 520, 522, 524, and 529
Animal drugs.
Therefore, under the Federal Food,
Drug, and Cosmetic Act and under
authority delegated to the Commissioner
of Food and Drugs and redelegated to
the Center for Veterinary Medicine, 21
CFR parts 510, 520, 522, 524, and 529
are amended as follows:
I
PART 510—NEW ANIMAL DRUGS
1. The authority citation for 21 CFR
part 510 continues to read as follows:
I
Authority: 21 U.S.C. 321, 331, 351, 352,
353, 360b, 371, 379e.
2. Amend § 510.600 in the table in
paragraph (c)(1) in the entry for ‘‘MedPharmex, Inc.’’ by removing ‘‘051259’’
and by adding in its place ‘‘054925’’;
and in the table in paragraph (c)(2) by
removing the entry for ‘‘051259’’ and by
I
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]]>Agencies
[Federal Register Volume 71, Number 51 (Thursday, March 16, 2006)]
[Rules and Regulations]
[Pages 13538-13541]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-2546]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21275; Directorate Identifier 2005-CE-28-AD;
Amendment 39-14515; AD 2006-01-11 R1]
RIN 2120-AA64
Airworthiness Directives; The Cessna Aircraft Company Models 208
and 208B Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document clarifies the intent of AD 2006-01-11, which was
published in the Federal Register on January 12, 2006 (71 FR 1941). AD
2006-01-11 applies to Cessna Models 208 and 208B airplanes and requires
the installation of a pilot assist handle and deicing boots on the
cargo pod and landing gear fairings; and the incorporation of changes
to the Pilot's Operating Handbook (POH) and FAA-Approved Airplane
Flight Manual (AFM). The compliance time for the AFM/POH change
currently reads ``prior to further flight'' after the installation of
the pilot assist handle, which is required within 125 days after the
effective date. The AFM/POH change is related to operation in ground
icing conditions and should not be attributed to the pilot assist
handle installation. Therefore, the compliance time should also be
within 125 days after the effective date. Additionally, the requirement
of installing the accessory kit or installing a placard should only
apply to those airplanes equipped with a cargo pod and pneumatic
deicing boots. The way it currently is written makes it apply to all
airplanes equipped with pneumatic deicing boots. This AD action rewords
the compliance time and the wording for the installation or placard
requirement to reflect the above concerns.
DATES: The effective date of this AD remains February 22, 2006.
As of February 22, 2006, the Director of the Federal Register
previously approved the incorporation by reference of certain
publications listed in the regulation.
ADDRESSES: To get the service information identified in this AD,
contact The Cessna Aircraft Company, Product Support, P.O. Box 7706,
Wichita, Kansas 67277-7706; telephone: (316) 517-5800; facsimile: (316)
942-9006.
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-2005-21275; Directorate
Identifier 2005-CE-28-AD.
FOR FURTHER INFORMATION CONTACT: Paul Pellicano, Aerospace Engineer
(Icing), FAA, Small Airplane Directorate, c/o Atlanta Aircraft
Certification Office (ACO), One Crown Center, 1985 Phoenix Boulevard,
Suite 450, Atlanta, GA 30349; telephone: (770) 703-6064; facsimile:
(770) 703-6097; or Robert P. Busto, Aerospace Engineer, Wichita ACO,
FAA, 1801 Airport Road, Wichita, Kansas 67209; telephone: (316) 946-
4157; facsimile: (316) 946-4107.
SUPPLEMENTARY INFORMATION:
Discussion
What Prior Action Did FAA Take on This Subject?
On January 5, 2006, FAA issued AD 2006-01-11, Amendment 39-14450
(71 FR 1941, January 12, 2006), which applies to certain Cessna Models
208 and 208B airplanes.
AD 2006-01-11 requires:
Installation of a pilot assist handle (part number (P/N)
SK208-146-2) (or FAA-Approved equivalent part number)
[[Page 13539]]
and deicing boots on the cargo pod and landing gear fairings (part
number (P/N) AK208-6C) (or FAA-approved equivalent part number); and
Incorporation of changes to the Pilot's Operating Handbook
(POH) and FAA-approved Airplane Flight Manual (AFM).
Why Is It Necessary To Change AD 2006-01-11?
The compliance time for the AFM/POH change currently reads ``prior
to further flight'' after the installation of the pilot assist handle,
which is required within 125 days after the effective date. The AFM/POH
change is related to operation in ground icing conditions and should
not be attributed to the pilot assist handle installation. Therefore,
the compliance time should also be within 125 days after the effective
date. Additionally, the requirement of installing the accessory kit or
installing a placard should only apply to those airplanes equipped with
a cargo pod and pneumatic deicing boots. The way it currently is
written makes it apply to all airplanes equipped with pneumatic deicing
boots. This installation is not possible for those airplanes that are
not equipped with a cargo pod and pneumatic deicing boots.
Correction of Publication
What Is the Purpose of This Document?
This document clarifies AD 2006-01-11 to allow compliance with the
AD and assure the intent of the current AD is clear. It also adds the
amendment to section 39.13 of the Federal Aviation Regulations (14 CFR
39.13).
We are clarifying and re-issuing the AD in its entirety to help
eliminate any confusion that AD 2006-01-11 may have created.
Is It Necessary To Seek Public Input?
Since this action only clarifies the intent, it has no adverse
economic impact and imposes no additional burden on any person than
would have been necessary to comply with AD 2006-01-11. Therefore, FAA
has determined that prior notice and opportunity for public comment are
unnecessary.
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)
2006-01-11, Amendment 39-14450 (71 FR 1941, January 12, 2006), and by
adding a new AD to read as follows:
2006-01-11 R1 The Cessna Aircraft Company: Amendment 39-14515;
Docket No. FAA-2005-21275; Directorate Identifier 2005-CE-28-AD.
When Does This AD Become Effective?
(a) This AD becomes effective on February 22, 2006. The
effective date of this AD is retained from AD 2006-01-11.
What Other ADs Are Affected by This Action?
(b) This AD revises AD 2006-01-11, Amendment 39-14450.
What Airplanes Are Affected by This AD?
(c) This AD affects Models 208 and 208B, all serial numbers,
that are certificated in any category.
What Is the Unsafe Condition Presented in This AD?
(d) This AD is the result of reports of several accidents
involving the affected airplanes during operations in-flight and in
ground icing conditions. We are issuing this AD to provide a safe
method to detect ice, snow, frost, or slush adhering to the upper
wing (a critical surface) prior to takeoff; and to reduce drag in-
flight by shedding ice on the cargo pod and landing gear fairings.
Ice adhering to the upper wing surface, cargo pod, or landing gear
fairings could result in a reduction in airplane performance with
the consequences that the airplane cannot perform a safe takeoff or
climb or maintain altitude.
What Must I Do To Address This Problem?
(e) To address this problem, you must do the following:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) Install the pilot assist Within the next 125 Install the pilot
handle SK208-146-2 subkit days after February assist handle SK208-
(part number (P/N) SK208- 22, 2006 (the 146-2 subkit (part
146-2) (or FAA-approved effective date of number (P/N) SK208-
equivalent part number) if this AD), unless 146-2) (or FAA-
the airplane will be already done. approved equivalent
operated in the ground part number)
icing conditions defined following step 4 of
under ``Visual/Tactile the Accomplishment
Check'' in the LIMITATIONS Instructions of
section of the AFM after Cessna Caravan
the compliance time. Service Kit No.
SK208-146, dated
October 4, 2004.
(2) 14 CFR 21.303 allows for Not Applicable...... Not Applicable.
replacement parts through
parts manufacturer approval
(PMA). The phrase ``or FAA-
approved equivalent part
number'' in this AD is
intended to signify those
parts that are PMA parts
approved through
identicality to the design
of the part under the type
certificate and parts to
correct the unsafe
condition under PMA (other
than identicality).
Equivalent replacement
parts to correct the unsafe
condition under PMA (other
than identicality) may also
be installed provided they
meet current airworthiness
standards, which include
those actions cited in this
AD.
[[Page 13540]]
(3) Insert the text in Within the next 125 The owner/operator
Appendix 1 of this AD after days after February holding at least a
the ``OTHER LIMITATIONS'' 22, 2006 (the private pilot
in the LIMITATIONS section effective date of certificate as
of the Cessna Models 208 or this AD) unless authorized by
208B Pilot's Operating already done. section 43.7 of the
Handbook (POH) and FAA- Federal Aviation
approved Airplane Flight Regulations (14 CFR
Manual (AFM). 43.7) may insert
the information
into the POH as
specified in
paragraph (e)(3) of
this AD. You may
insert a copy of
this AD into the
appropriate
sections of the POH
to comply with this
action. Make an
entry into the
aircraft records
showing compliance
with portion of the
AD in accordance
with section 43.9
of the Federal
Aviation
Regulations (14 CFR
43.9).
(4) For Cessna Model 208B Within the next 125 Install the cargo
with Pratt & Whitney of days after February pod and landing
Canada Ltd., PT6A-114 Turbo 22, 2006 (the gear fairing deice
Prop engine installed (600 effective date of kit (part number (P/
SHP) or equipped with a this AD), unless N) AK208-6C2) (or
cargo pod and pneumatic already done. FAA-approved
deicing boots, do one of equivalent part
the following: number) following
(i) Install Cessna Accessory the Installation
Kit AK208-6C per Cessna Instructions of
Service Bulletin CAB95-19; Cessna Caravan
or. Service Bulletin
(ii) Install a placard in No. CAB95-19, dated
view of the pilot which October 13, 1995,
states ``This airplane is and Cessna Caravan
prohibited from flight in Accessory Kit No.
known or forecast icing''. AK208-6C, Revision
C, dated August 27,
1993. The owner/
operator holding at
least a private
pilot certificate
as authorized by
section 43.7 of the
Federal Aviation
Regulations (14 CFR
43.7) may install
the placard as
specified in
paragraph (e)(4) of
this AD. You may
insert a copy of
this AD into the
appropriate
sections of the POH
to comply with this
action. Make an
entry into the
aircraft records
showing compliance
with portion of the
AD in accordance
with section 43.9
of the Federal
Aviation
Regulations (14 CFR
43.9).
(5) For all Cessna Model 208 Within the next 125 Do the installation
and 208B airplanes equipped days after February following the
with a cargo pod and 22, 2006 (the Installation
pneumatic deicing boots and effective date of Instructions of
not included in paragraph this AD), unless Cessna Caravan
(e)(4) of this AD, do one already done. Service Bulletin
of the following: No. CAB93-20,
(i) Install Cessna Accessory Revision 1, dated
Kit AK208-6C per Cessna October 13, 1995,
Service Bulletin CAB93-20 and Cessna Caravan
Revision 1; or. Accessory Kit No.
(ii) Install a placard in AK208-6C, Revision
view of the pilot with the C, issued August
following words: ``This 27, 1993. The owner/
airplane is prohibited from operator holding at
flight in known or forecast least a private
icing''. pilot certificate
as authorized by
section 43.7 of the
Federal Aviation
Regulations (14 CFR
43.7) may install
the placard as
specified in
paragraph
(e)(5)(ii) of this
AD. Make an entry
into the aircraft
records showing
compliance with
portion of the AD
in accordance with
section 43.9 of the
Federal Aviation
Regulations (14 CFR
43.9).
(6) Insert the text in Before further The owner/operator
Appendix 2 of this AD in flight after holding at least a
the ``KINDS OF OPERATION compliance to private pilot
LIMITS'' in the LIMITATIONS paragraph (e)(4)(i) certificate as
section of the Cessna or (e)(5)(i) of authorized by
Models 208 or 208B Pilot's this AD. section 43.7 of the
Operating Handbook (POH) Federal Aviation
and FAA-approved Airplane Regulations (14 CFR
Flight Manual (AFM). 43.7) may insert
the information
into the POH as
specified in
paragraph (e)(3) of
this AD. You may
insert a copy of
this AD into the
appropriate
sections of the POH
to comply with this
action. Make an
entry into the
aircraft records
showing compliance
with portion of the
AD in accordance
with section 43.9
of the Federal
Aviation
Regulations (14 CFR
43.9).
(7) Delete the text in Before further The owner/operator
Appendix 3 of this AD from flight after holding at least a
the ``REQUIRED EQUIPMENT'' compliance to private pilot
in the LIMITATIONS section paragraph (e)(4)(i) certificate as
of the Cessna Models 208 or or (e)(5)(i) of authorized by
208B Pilot's Operating this AD. section 43.7 of the
Handbook (POH) and FAA- Federal Aviation
approved Airplane Flight Regulations (14 CFR
Manual (AFM) Supplement S1 43.7) may insert
``Known Icing Equipment''. the information
into the POH as
specified in
paragraph (e)(3) of
this AD. You may
insert a copy of
this AD into the
appropriate
sections of the POH
to comply with this
action. Make an
entry into the
aircraft records
showing compliance
with portion of the
AD in accordance
with section 43.9
of the Federal
Aviation
Regulations (14 CFR
43.9).
------------------------------------------------------------------------
[[Page 13541]]
Note: Cessna Caravan Service Bulletin No. CAB04-9, dated October
4, 2004, also addresses the installation of the pilot assist handle.
May I Request an Alternative Method of Compliance?
(f) The Manager, Wichita Aircraft Certification Office (ACO),
FAA, has the authority to approve alternative methods of compliance
for this AD, if requested using the procedures found in 14 CFR
39.19. For information on any already approved alternative methods
of compliance, contact Paul Pellicano, Aerospace Engineer (Icing),
FAA, Small Airplane Directorate, c/o Atlanta ACO, One Crown Center,
1985 Phoenix Boulevard, Suite 450, Atlanta, GA 30349; telephone:
(770) 703-6064; facsimile: (770) 703-6097; or Robert P. Busto,
Aerospace Engineer, Wichita ACO, FAA, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946-4157; facsimile: (316) 946-4107.
Does This AD Incorporate Any Material by Reference?
(g) You must do the actions required by this AD following the
instructions in Cessna Caravan Service Kit No. SK208-146, dated
October 4, 2004, and Cessna Caravan Accessory Kit No. AK208-6C,
Revision C, dated August 27, 1993.
(1) On February 22, 2006 (71 FR 1941, January 12, 2006), and in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51, the Director of
the Federal Register previously approved the incorporation by
reference of Cessna Caravan Service Kit No. SK208-146, dated October
4, 2004, and Cessna Caravan Accessory Kit No. AK208-6C, Revision C,
dated August 27, 1993.
(2) To get a copy of this service information, contact The
Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita,
Kansas 67277-7706; telephone: (316) 517-5800; facsimile: (316) 942-
9006. 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 20590-001 or on the Internet at https://
dms.dot.gov. The docket number is FAA-2005-21275; Directorate
Identifier 2005-CE-28-AD.
Appendix 1 to AD 2006-01-11 R1 Changes to the Cessna Models 208 or 208B
Pilot's Operating Handbook (POH) and FAA-Approved Airplane Flight
Manual
Affected Cessna Models 208 or 208B Pilot's Operating Handbook (POH) and
FAA-Approved Airplane Flight Manual (AFM)
Insert the following text after the ``OTHER LIMITATIONS'' in the
LIMITATIONS section of the Cessna Models 208 or 208B Pilot's
Operating Handbook (POH) and FAA-Approved Airplane Flight Manual
(AFM): COLD WEATHER OPERATIONS.
The airplane must be equipped with the following equipment when
operating at an airport in the ground icing conditions defined under
``Visual/Tactile Check'' in the LIMITATIONS section:
1. Pilot assist handle, Cessna P/N SK208-146-2 (or FAA-approved
equivalent part number).
Appendix 2 to AD 2006-01-11 R1 Changes to the Cessna Models 208 or 208B
Pilot's Operating Handbook (POH) and FAA-Approved Airplane Flight
Manual
Affected Cessna Models 208 or 208B Pilot's Operating Handbook (POH) and
FAA-Approved Airplane Flight Manual (AFM)
Add the following to the equipment listed under ``FLIGHT INTO
KNOWN ICING'' in the ``KINDS OF OPERATION LIMITS'' in the
LIMITATIONS section of the FAA-Approved Airplane Flight Manual:
Lower main landing gear leading edge deice boots
Cargo pod nosecap deice boot
Appendix 3 to AD 2006-01-11 R1 Changes to the Cessna Models 208 or 208B
Pilot's Operating Handbook (POH) and FAA-Approved Airplane Flight
Manual Supplement S1
Affected Cessna Models 208 or 208B Pilot's Operating Handbook (POH) and
FAA-Approved Airplane Flight Manual (AFM) Supplement S1
Remove the paragraph under ``REQUIRED EQUIPMENT'' in the
Limitations section of the FAA-Approved Flight Manual Supplement S1
``Known Icing Equipment'', that currently reads as follows:
``The following additional equipment is not required for flight
into icing conditions as defined by FAR 25, but may be installed on
early serial airplanes by using optional accessory Kit AK208-6. On
later serial airplanes, this equipment may be included with the
flight into known icing package. If installed, this equipment must
be fully operational:''
Issued in Kansas City, Missouri, on March 10, 2006.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 06-2546 Filed 3-15-06; 8:45 am]
BILLING CODE 4910-13-P
