Airworthiness Directives; The Cessna Aircraft Company Models 208 and 208B Airplanes, 4663-4669 [E7-1604]
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Federal Register / Vol. 72, No. 21 / Thursday, February 1, 2007 / Proposed Rules
List of Subjects in 14 CFR Part 23
Aircraft, Aviation safety, Signs and
symbols.
Citation
The authority citation for these
special conditions is as follows:
Authority: 49 U.S.C. 106(g), 40113 and
44701; 14 CFR 21.16 and 21.17; and 14 CFR
11.38 and 11.19.
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The Special Conditions
Accordingly, the Federal Aviation
Administration (FAA) proposes the
following special conditions as part of
the type certification basis for the ATG
Model 100 airplanes.
Title 14 CFR, part 23, § 23.221(c) as
amended by Amendment 23–50
presents acrobatic category airplane
spin requirements. As the rule is
currently written, the acrobatic category
airplane must comply with normal
category spin requirements, acrobatic
category emergency egress requirements
in § 23.807, and acrobatic spin
requirements for each configuration
requested for spin approval.
ATG proposes to prohibit intentional
spins and requests that no configuration
be approved for spins. This proposal
leads to an acrobatic category airplane
that meets only normal category spin
requirements. This proposal is
unacceptable since the FAA has always
maintained that an acrobatic category
airplane must comply with acrobatic
category spin requirements despite the
wording in the current rule. The rule’s
history coupled with preamble
information for Amendment 23–50
reveals that the rule was changed to add
the normal category spin requirements
and to accommodate an applicant’s
desire to comply with the acrobatic spin
requirements for at least one
configuration, but not necessarily all
configurations.
Since the wording of the current rule
combined with ATG’s proposal does not
provide the level of safety envisioned
for an acrobatic category airplane, the
FAA proposes the following special
condition under the authority of 14
CFR, part 21, § 21.16 to replace
§ 23.221(c) in its entirety:
SC 23.221 Spinning
(c) Acrobatic category airplanes. An
acrobatic category airplane must meet
the spin requirements of paragraph (a)
of this section and § 23.807(b)(5). In
addition, the following requirements
must be met in an applicant-designated
acrobatic configuration, and in each
other configuration for which approval
for spinning is requested:
(1) The airplane must recover from
any point in a spin up to and including
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six turns, or any greater number of turns
for which certification is requested, in
not more than one and one-half
additional turns after initiation of the
first control action for recovery.
However, beyond three turns, the spin
may be discontinued if spiral
characteristics appear.
(2) The applicable airspeed limits and
limit maneuvering load factors must not
be exceeded. For flaps extended
configurations for which approval is
requested, the flaps must not be
retracted during the recovery.
(3) It must be impossible to obtain
unrecoverable spins with any use of the
flight or engine power controls either at
the entry into or during the spin.
(4) There must be no characteristics
during the spin (such as excessive rates
of rotation or extreme oscillatory
motion) that might prevent a successful
recovery due to disorientation or
incapacitation of the pilot.
(5) The airplane is considered to meet
the requirements of paragraph (c) of this
special condition with a specific
demonstration. The applicant must
demonstrate that it is extremely remote
for the airplane in the applicantdesignated acrobatic configuration, and
in each other configuration for which
approval for spinning is requested, to
enter a spin with any use of the flight
or engine power controls, either at or
after entry into the stall maneuver.
Issued in Kansas City, Missouri on January
24, 2007.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. E7–1610 Filed 1–31–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–26498; Directorate
Identifier 2006–CE–83–AD]
RIN 2120–AA64
Airworthiness Directives; The Cessna
Aircraft Company Models 208 and
208B Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to supersede
Airworthiness Directive (AD) 2006–06–
06, which applies to certain Cessna
Aircraft Company (Cessna) Models 208
SUMMARY:
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and 208B airplanes. AD 2006–06–06
currently requires you to incorporate
information into the applicable section
of the Airplane Flight Manual (AFM)
and Pilot’s Operating Handbook (POH)
and requires installation of placards.
Since we issued AD 2006–06–06,
Cessna issued further revisions to the
AFM Supplement S1 ‘‘Known Icing
Equipment’’ and developed a low
airspeed awareness system.
Consequently, this proposed AD would
require you to incorporate the AFM
Supplement revisions, to install the low
airspeed awareness system, and to
retain the requirements of AD 2006–06–
06 until the above requirements are
incorporated. We are proposing this AD
to assure that the pilot has enough
information and the necessary
equipment to prevent loss of control of
the airplane while in flight during icing
conditions.
DATES: We must receive comments on
this proposed AD by March 5, 2007.
ADDRESSES: Use one of the following
addresses to comment on this proposed
AD:
• DOT Docket Web site: Go to
https://dms.dot.gov and follow the
instructions for sending your comments
electronically.
• Government-wide rulemaking Web
site: Go to https://www.regulations.gov
and follow the instructions for sending
your comments electronically.
• Mail: Docket Management Facility;
U.S. Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590–
0001.
• Fax: (202) 493–2251.
• Hand Delivery: Room PL–401 on
the plaza level of the Nassif Building,
400 Seventh Street, SW., Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
• Federal eRulemaking Portal: https://
www.regulations.gov. Follow the
instructions for submitting comments.
For service information identified in
this proposed AD, contact The Cessna
Aircraft Company, Product Support,
P.O. Box 7706, Wichita, Kansas 67277.
FOR FURTHER INFORMATION CONTACT:
Robert P. Busto, Aerospace Engineer,
Wichita Aircraft Certification Office,
FAA, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946–
4157; fax: (316) 946–4107.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written
relevant data, views, or arguments
regarding this proposed AD. Send your
comments to an address listed under the
ADDRESSES section. Include the docket
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number, ‘‘FAA–2006–26498; Directorate
Identifier 2006–CE–83–AD’’ at the
beginning of your comments. We
specifically invite comments on the
overall regulatory, economic,
environmental, and energy aspects of
the proposed AD. We will consider all
comments received by the closing date
and may amend the proposed AD in
light of those comments.
We will post all comments we
receive, without change, to https://
dms.dot.gov, including any personal
information you provide. We will also
post a report summarizing each
substantive verbal contact we receive
concerning this proposed AD.
Discussion
Several accidents/incidents with
Cessna Models 208 and 208B airplanes
during operations in icing conditions,
including six accidents in the 2003/
2004 icing season and nine accidents in
the 2004/2005 icing season, caused us to
issue AD 2005–07–01, Amendment 39–
14025 (70 FR 15223), which required
the incorporation of revisions into
applicable section of the AFM, and AD
2006–01–11, Amendment 39–14450 (71
FR 16994). AD 2006–01–11 requires the
installation of a pilot assist handle,
pneumatic deicing boots on the cargo
pod and landing gear struts, and
changes to the Limitations Section of
the AFM if the airplane is to be operated
in ground icing conditions and
approved for flight into known or
forecast icing conditions. AD 2005–07–
01 was superseded by AD 2006–06–06,
Amendment 39–14514 (71 FR 13533,
March 16, 2006). AD 2006–06–06
currently requires the following on
certain Cessna Models 208 and 208B
airplanes:
• Incorporation of revisions to the
FAA-approved AFM and FAA-approved
AFM Supplement S1 ‘‘Known Icing
Equipment;’’
• Incorporation of new text in the
Limitations Section of the AFM and
AFM Supplement; and
• Incorporation of new text in the
Performance Section of the AFM
Supplement and the fabrication and
installation of placards.
AD 2006–06–06 was intended to be an
interim action. Cessna has since
published revisions to the AFM
Supplement S1 ‘‘Known Icing
Equipment,’’ which incorporates climb
performance data in icing conditions.
This data is to be used for preflight
planning and as an in-flight limitation.
AD 2006–06–06 included a limitation
on autopilot use as an interim action
until the development of an acceptable
low speed awareness system. Cessna has
issued service information introducing
this system. Cessna has also developed
specific training for operation of the
Models 208 and 208B airplanes in icing
conditions. This training is available online at: https://www.cessnaelearning.com
or as part of the Cessna Winter
Awareness Seminars.
If the pilot does not have enough
information in the AFM or the necessary
equipment to conduct safe flight into
icing conditions, then loss of control
could occur.
Relevant Service Information
We have reviewed Cessna Caravan
Service Bulletin (SB) CAB06–8, dated
September 18, 2006; Cessna Caravan SB
CAB06–11, dated October 9, 2006; and
Cessna Caravan Service Kit (SK) 208–
171, dated October 9, 2006.
The service information includes the
following:
• Cessna Caravan SB CAB06–8:
revisions to the Pilot’s Operating
Handbook (POH) Supplement S1
‘‘Known Icing Equipment’’ and
installation instructions for installation
of operational placards; and
• Cessna Caravan SB CAB06–11:
announces the availability of a Service
Kit which provides parts and
instructions to install a new low
airspeed awareness system.
• Cessna Caravan SK208–171:
instructions for the installation of a new
icing low speed awareness system.
In addition, Cessna has developed
revisions to the AFM Supplement S1
‘‘Known Icing Equipment’’ as follows:
Document
Affects
Revision 9 of the Model 208 (675 SHP) FAA-approved Flight Manual
Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document
D1352–S1–09, dated August 24, 2006.
Cessna Model 208 airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114A turboprop engine installed (675 SHP) or FAA-approved
engine of equivalent or higher horsepower installed, equipped with
airframe deicing pneumatic boots, that are not currently prohibited
from flight in known or forecast icing.
Cessna Model 208 airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114 turboprop engine installed (600 SHP) or FAA-approved
engine of equivalent horsepower installed, equipped with airframe
deicing pneumatic boots, that are not currently prohibited from flight
in known or forecast icing.
Cessna Model 208B airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114A turboprop engine installed (675 SHP) or FAA-approved
engine of equivalent or higher horsepower installed, equipped with
airframe deicing pneumatic boots, that are not currently prohibited
from flight in known or forecast icing.
Cessna Model 208B airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114 turboprop engine installed (600 SHP) or FAA-approved
engine of equivalent horsepower installed, equipped with airframe
deicing pneumatic boots, that are not currently prohibited from flight
in known or forecast icing.
Revision 8 of the Model 208 (600 SHP) FAA-approved Flight Manual
Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document
D1307–S1–08, dated August 24, 2006.
Revision 9 of the 208B (675 SHP) FAA-approved Flight Manual Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document D1329–
S1–09, dated August 24, 2006.
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Revision 9 of the 208B (600 SHP) FAA-approved Flight Manual Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document D1309–
S1–09, dated August 24, 2006.
FAA’s Determination and Requirements
of the Proposed AD
We are proposing this AD because we
evaluated all information and
determined the unsafe condition
described previously is likely to exist or
develop on other products of the same
type design. This proposed AD would
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supersede AD 2006–06–06 with a new
AD that would:
• Require the actions in the
previously referenced service
information; and
• Retain the actions of AD 2006–06–
06 until the above requirements are
incorporated.
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Costs of Compliance
We estimate that this proposed AD
would affect 765 airplanes in the U.S.
registry.
We estimate the following costs to do
the proposed actions:
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Labor cost
Parts cost
Total cost per
airplane
Total cost on
U.S. operators
22 work-hours × $80 per hour = $1,760 .....................................................................................
$6,440
$8,200
$6,273,000
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII,
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
We are issuing this rulemaking under
the authority described in subtitle VII,
part A, subpart III, section 44701,
‘‘General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
Regulatory Findings
We have determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would not
have a substantial direct effect on the
States, on the relationship between the
national Government and the States, or
on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that the proposed regulation:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
3. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this proposed AD and placed it in the
AD docket.
Examining the AD Docket
You may examine the AD docket that
contains the proposed AD, the
regulatory evaluation, any comments
received, and other information on the
Internet at https://dms.dot.gov; or in
person at the Docket Management
Facility between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal
holidays. The Docket Office (telephone
(800) 647–5227) is located at the street
address stated in the ADDRESSES section.
Comments will be available in the AD
docket shortly after receipt.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Safety.
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by
removing Airworthiness Directive (AD)
2006–06–06, Amendment 39–14514, (71
FR 13533, March 16, 2006), and adding
the following new AD:
Cessna Aircraft Company: Docket No. FAA–
2006–26498; Directorate Identifier 2006–
CE–83–AD.
Comments Due Date
(a) We must receive comments on this
airworthiness directive (AD) action by March
5, 2007.
Affected ADs
(b) This AD supersedes AD 2006–06–06,
Amendment 39–14514.
Applicability
(c) This AD applies to Models 208 and
208B, all serial numbers that are certificated
in any category.
Unsafe Condition
(d) This AD results from our determination
that further revisions to the Airplane Flight
Manual (AFM) Supplement S1 ‘‘Known Icing
Equipment’’ are necessary, and the
installation of a low airspeed awareness
system is required. We are issuing this AD to
assure that the pilot has enough information
and the necessary equipment to prevent loss
of control of the airplane while in-flight
during icing conditions.
New Actions Required by This AD
(e) Within the next 30 days after the
effective date of this AD, do the following,
unless already done:
(1) For all Model 208 and 208B aircraft not
currently restricted from flight into known or
forecast icing: Install a low airspeed
awareness system following the instructions
in Cessna Service Bulletin CAB06–11 and
Service Kit SK 208–171, both dated October
9, 2006.
(2) Incorporate the following revisions to
the AFM Supplement S1 ‘‘Known Icing
Equipment’’ as applicable:
Document
Affects
(i) Revision 9 of the Model 208 (675 SHP) FAA-approved Flight Manual
Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document
D1352–S1–09, dated August 24, 2006.
Cessna Model 208 airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114A turboprop engine installed (675 SHP) or FAA-approved
engine of equivalent or higher horsepower installed, equipped with
airframe deicing pneumatic boots, that are not currently prohibited
from flight in known or forecast icing.
Cessna Model 208 airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114 turboprop engine installed (600 SHP) or FAA-approved
engine of equivalent horsepower installed, equipped with airframe
deicing pneumatic boots, that are not currently prohibited from flight
in known or forecast icing.
Cessna Model 208B airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114A turboprop engine installed (675 SHP) or FAA-approved
engine of equivalent or higher horsepower installed, equipped with
airframe deicing pneumatic boots, that are not currently prohibited
from flight in known or forecast icing.
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(ii) Revision 8 of the Model 208 (600 SHP) FAA-approved Flight Manual Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document
D1307–S1–08, dated August 24, 2006.
(iii) Revision 9 of the Model 208B (675 SHP) FAA-approved Flight
Manual Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document
D1329–S1–09, dated August 24, 2006.
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Document
Affects
(iv) Revision 9 of the Model 208B (600 SHP) FAA-approved Flight
Manual Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document
D1309–S1–09, dated August 24, 2006.
Cessna Model 208B airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114 turboprop engine installed (600 SHP) or FAA-approved
engine of equivalent horsepower installed, equipped with airframe
deicing pneumatic boots, that are not currently prohibited from flight
in known or forecast icing.
(3) For all Model 208 and 208B aircraft
equipped with pneumatic deicing boots, and
not currently restricted from flight into
known or forecast icing: incorporate the
following information in the Limitations
Section of the Airplane Flight Manual (AFM)
Supplement S1 ‘‘Known Icing Equipment’’ to
require pilot training before further flight into
known or forecast icing conditions. 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 specified in paragraphs (e)(3)(i) and
(e)(3)(ii) 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 this portion of the AD in
accordance with section 43.9 of the Federal
Aviation Regulations (14 CFR 43.9):
(i) ‘‘The pilot-in-command must
successfully complete specific training for
flight into icing conditions provided by
Cessna Aircraft Company within the 12
calendar months preceding any flight into
known or forecast icing conditions.
Completion of either of the following
courses will meet this training requirement:
Caravan Cold Wx Ops Onsite—C14694—
(CAC 14694)
Caravan Cold Wx Ops Online—C14695—
(CAC 14695)’’
(ii) ‘‘Note: The three-hour, on-line training
course became available on October 2, 2006,
at: https://www.cessnaelearning.com. The
three-hour on-site training courses are
scheduled annually in October at various
locations and provided by Cessna Aircraft
Company at no cost as part of the Cessna
Winter Awareness Seminars. Confirmation of
pilot training completion will be maintained
by Cessna Aircraft Company. Please note that
all operators of the affected airplanes must
initiate action to notify and ensure that flight
crewmembers are aware of this requirement.’’
(f) The actions in paragraphs (g) and (h)
below are retained in this AD from AD 2006–
06–06. The new actions required by this AD
in paragraph (e) above terminates the
requirement for the actions in paragraphs (g)
and (h).
(g) No later than March 27, 2006 (3 days
after March 24, 2006, which is the effective
date of AD 2006–06–06), incorporate the
following revisions into the Airplane Flight
Manual (AFM), unless already accomplished:
Affected airplanes
Incorporate the following AFM revision document
(1) Cessna Model 208 airplanes and Model 208B airplanes, all serial
numbers.
Section 2: Limitations and Section 4: Normal Procedures: Temporary
Revision 208PHTR05, dated June 27, 2005, to the POH and FAAapproved AFM.
Section 9: Optional Systems Description and Operating Procedures:
Revision 6 of the 208 (675 SHP) POH/FAA-approved AFM Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document D1352–S1–
06, dated June 27, 2005.
(2) Cessna Model 208 airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114A turboprop engine installed (675 SHP) or FAA-approved
engine of equivalent horsepower installed, equipped with airframe
deicing pneumatic boots, that are not currently prohibited from flight
in known or forecast icing.
(3) Cessna Model 208 airplanes with a Pratt & Whitney of Canada Ltd.,
PT6A–114 turboprop engine installed (600 SHP) or FAA-approved
engine of equivalent horsepower installed, equipped with airframe
deicing pneumatic boots, that are not currently prohibited from flight
in known or forecast icing.
(4) Cessna Model 208B airplanes with a Pratt & Whitney of Canada
Ltd., PT6A–114A turboprop engine installed (675 SHP) or FAA-approved engine of equivalent horsepower installed, equipped with airframe deicing pneumatic boots, that are not currently prohibited from
flight in known or forecast icing.
(5) Cessna Model 208B airplanes with a Pratt & Whitney of Canada
Ltd., PT6A–114 turboprop engine installed (600 SHP) or FAA-approved engine of equivalent horsepower installed, equipped with airframe deicing pneumatic boots, that are not currently prohibited from
flight in known or forecast icing.
(h) You must do the following actions,
unless already done. These changes are to the
Section 9: Optional Systems Description and Operating Procedures:
Revision 6 of the Cessna Model 208 (600 SHP) POH/FAA-approved
AFM Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document
D1307–S1–06, dated June 27, 2005.
Section 9: Optional Systems Description and Operating Procedures:
Revision 7 of the 208B (675 SHP) POH/FAA-approved AFM Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document D1329–S1–
07, dated June 27, 2005.
Section 9: Optional Systems Description and Operating Procedures:
Revision 6 of the 208B (600 SHP) POH/FAA-approved AFM Supplement S1 ‘‘Known Icing Equipment,’’ Cessna document D1309–S1–
06, dated June 27, 2005.
POH and FAA-approved AFM and to the
POH/FAA-approved AFM Supplement S1
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Actions
Compliance
(1) For Cessna Model 208 airplanes and Model
208B airplanes, all serial numbers, equipped
with airframe deicing pneumatic boots, that
are not currently prohibited from flight in
known or forecast icing: You are prohibited
from continued flight after encountering moderate or greater icing conditions. The airplane can dispatch into forecast areas of
icing but must exit moderate or greater icing
conditions if encountered.
No later than March 27, 2006 (3 days after
March 24, 2006, which is the effective date
of AD 2006–06–06).
‘‘Known Icing Equipment’’ mandated in
paragraph (g) of this AD:
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Procedures
Not Applicable.
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Actions
Compliance
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(2) For Cessna Model 208 airplanes and Model No later than March 27,
208B airplanes, all serial numbers, equipped
March 24, 2006, which
with airframe deicing pneumatic boots, that
of AD 2006–06–06).
are not currently prohibited from flight in
known or forecast icing:
(i) Insert the text in Appendix 1 of this AD
preceding the KINDS OF OPERATION
LIMITS paragraph in the LIMITATIONS
section of the Cessna Models 208 or
208B POH and FAA-approved AFM.
(ii) Insert the text in Appendix 2 of this AD
in the LIMITATIONS section of the
Cessna Models 208 or 208B POH and
FAA-approved AFM KNOWN ICING
EQUIPMENT SUPPLEMENT S1 at the
beginning of the paragraph ‘‘REQUIRED
EQUIPMENT.’’
(3) For Cessna Model 208 airplanes and Model No later than March 27,
208B airplanes, all serial numbers, equipped
March 24, 2006, which
with airframe deicing pneumatic boots, that
of AD 2006–06–06).
are not currently prohibited from flight in
known or forecast icing: Install 3 placards
with black letters on a white background.
The placards 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 height of 1⁄8-inch.
(i) Placard 1 shall include the text of Appendix 3 of this AD.
(ii) Placard 2 shall include the following
text: ‘‘120 KIAS Minimum in Icing Flaps
Up except 110 KIAS if Climbing to Exit
Icing.’’
(iii) Placard 3 shall include the following
text: ‘‘Disconnect autopilot at first indication of ice accretion.’’
(4) For Cessna Model 208 airplanes and Model No later than March 27,
208B airplanes, all serial numbers, equipped
March 24, 2006, which
with airframe deicing pneumatic boots, that
of AD 2006–06–06).
are not currently prohibited from flight in
known or forecast icing:
(i) Insert the text in Appendix 4 of this AD
under the ‘‘AIRSPEED LIMITATIONS’’
paragraph in the LIMITATIONS section
of the Cessna Models 208 or 208B POH
and FAA-approved AFM.
(ii) Replace the text in the KNOWN ICING
EQUIPMENT SUPPLEMENT S1 under
the ‘‘MINIMUM SPEED IN ICING CONDITIONS’’ paragraph with the text in Appendix 4.
(iii) Insert the following text in the LIMITATIONS section of the POH/AFM under
the ‘‘OTHER LIMITATIONS’’ paragraph
and in the LIMITATIONS section of the
KNOWN ICING EQUIPMENT SUPPLEMENT S1 under the ‘‘AUTOPILOT OPERATION IN ICING CONDITIONS’’
paragraph: ‘‘Disconnect autopilot at first
indication of ice accretion.’’
VerDate Aug<31>2005
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Fmt 4702
4667
Procedures
2006 (3 days after
is the effective date
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/AFM as specified in paragraph
(h)(2) of this AD. You may insert a copy of
this AD into the appropriate sections of the
POH/AFM 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).
2006 (3 days after
is the effective date
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 placards as specified in paragraph (h)(3) 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).
2006 (3 days after
is the effective date
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/AFM as specified in paragraph
(h)(4) of this AD. You may insert a copy of
this AD into the appropriate sections of the
POH/AFM 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).
Sfmt 4702
E:\FR\FM\01FEP1.SGM
01FEP1
4668
Federal Register / Vol. 72, No. 21 / Thursday, February 1, 2007 / Proposed Rules
Actions
Compliance
Procedures
(5) For Cessna Model 208 airplanes and Model
208B airplanes, all serial numbers, equipped
with airframe deicing pneumatic boots, that
are not currently prohibited from flight in
known or forecast icing:
(i) Replace the text in the PERFORMANCE section of the Cessna Models
208 or 208B POH and FAA-approved
AFM KNOWN ICING EQUIPMENT
SUPPLEMENT S1 under the ‘‘STALL
SPEEDS’’ paragraph with the text in Appendix 5.
(ii) Replace the ‘‘WARNING’’ text in the
LIMITATIONS section of the Cessna
Models 208 or 208B POH and FAA-approved AFM KNOWN ICING EQUIPMENT SUPPLEMENT S1 under ‘‘ENVIRONMENTAL
CONDITIONS’’
with:
‘‘FLIGHT IN THESE CONDITIONS ARE
PROHIBITED.’’
(iii) Replace the last two sentences in the
LIMITATIONS section of the Cessna
Models 208 or 208B POH and FAA-approved AFM KNOWN ICING EQUIPMENT SUPPLEMENT S1 under ‘‘ENVIRONMENTAL CONDITIONS’’ with the
following text: ‘‘Exit strategies should be
determined during pre-flight planning.’’.
No later than March 27, 2006 (3 days after
March 24, 2006, which is the effective date
of AD 2006–06–06).
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/AFM as specified in paragraph
(h)(5) of this AD. You may insert a copy of
this AD into the appropriate sections of the
POH/AFM 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).
Alternative Methods of Compliance
(AMOCs)
(i) The Manager Wichita Aircraft
Certification Office (ACO), FAA, ATTN:
Robert P. Busto, Aerospace Engineer, Wichita
Aircraft Certification Office, FAA, 1801
Airport Road, Wichita, Kansas 67209;
telephone: (316) 946–4157; fax: (316) 946–
4107, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19.
defines moderate icing conditions for this
airplane:
Indicated airspeed in level cruise flight at
constant power decreases by 20 knots. Engine
torque required to maintain airspeed
increases by 400 ft. lbs. Airspeed of 120 KIAS
cannot be maintained in level flight. An
accretion of 1⁄4-inch of ice is observed on the
wing strut.
Disregard any mention of approval for
flight in icing conditions within the POH/
AFM.’’
Appendix 3 Retained From AD 2006–
06–06
Related Information
(j) To get copies of the service information
referenced in this AD, contact: The Cessna
Aircraft Company, Product Support, P.O. Box
7706, Wichita, Kansas 67277. 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, or on the
Internet at https://dms.dot.gov. The docket
number is Docket No. FAA–2006–26498;
Directorate Identifier 2006–CE–83–AD.
Appendix 1 Retained From AD 2006–
06–06
rmajette on PROD1PC67 with PROPOSALS
Changes to the Cessna Models 208 or 208B
Pilot’s Operating Handbook (POH) and FAAApproved Airplane Flight Manual (AFM)
Affected Cessna Models 208 or 208B POH
and FAA-Approved AFM
Insert the following text at the beginning of
the KINDS OF OPERATION LIMITS
paragraph in the LIMITATIONS section of
the Cessna Models 208 or 208B POH and
FAA-approved AFM. This may be done by
inserting a copy of this AD into the POH/
AFM:
‘‘Continued flight after encountering
moderate or greater icing conditions is
prohibited. One or more of the following
VerDate Aug<31>2005
15:30 Jan 31, 2007
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Appendix 2 Retained From AD 2006–
06–06
Changes to the Cessna Models 208 or 208B
Pilot’s Operating Handbook (POH) and FAAApproved Airplane Flight Manual (AFM)
Affected Cessna Models 208 or 208B POH
and FAA-Approved AFM
Insert the following text in the
LIMITATIONS section of the POH and FAAapproved AFM KNOWN ICING EQUIPMENT
SUPPLEMENT S1, at the beginning of the
paragraph ‘‘REQUIRED EQUIPMENT.’’ This
may be done by inserting a copy of this AD
into the POH/AFM:
‘‘Continued flight after encountering
moderate or greater icing conditions is
prohibited. One or more of the following
defines moderate icing conditions for this
airplane:
Indicated airspeed in level flight at
constant power decreases by 20 knots. Engine
torque required to maintain airspeed
increases by 400 ft. lbs. Airspeed of 120 KIAS
cannot be maintained in level flight. An
accretion of 1⁄4-inch of ice is observed on the
wing strut.
Disregard any mention of approval for
flight in icing conditions within the POH/
AFM.’’
PO 00000
Frm 00009
Fmt 4702
Sfmt 4700
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.’’
Appendix 4 Retained From AD 2006–
06–06
Changes to the Cessna Models 208 or 208B
Pilot’s Operating Handbook (POH) and FAAApproved Airplane Flight Manual (AFM)
Supplement S1
Affected Cessna Models 208 or 208B POH
and FAA-Approved AFM and FAA-Approved
Supplement S1
Insert the following text into the
LIMITATIONS section under the ‘‘AIRSPEED
LIMITATIONS’’ paragraph of the Cessna
E:\FR\FM\01FEP1.SGM
01FEP1
Federal Register / Vol. 72, No. 21 / Thursday, February 1, 2007 / Proposed Rules
Models 208 or 208B POH and FAA-approved
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
adequate stall warning when in icing
conditions.’’
Note: These are minimum speeds for
operations in icing conditions. Disregard any
reference to the original speeds within the
POH/AFM.
Appendix 5 Retained From AD 2006–
06–06
Changes to the Cessna Models 208 or 208B
Pilot’s Operating Handbook (POH) and FAAApproved Airplane Flight Manual (AFM)
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 January
25, 2007.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. E7–1604 Filed 1–31–07; 8:45 am]
rmajette on PROD1PC67 with PROPOSALS
BILLING CODE 4910–13–P
DEPARTMENT OF HOMELAND
SECURITY
Coast Guard
33 CFR Part 100
[CGD05–07–001]
RIN 1625–AA08
Special Local Regulations for Marine
Events; Severn River, College Creek,
Weems Creek and Carr Creek,
Annapolis, MD
Coast Guard, DHS.
ACTION: Notice of proposed rulemaking.
AGENCY:
SUMMARY: The Coast Guard proposes to
amend the special local regulations at
33 CFR 100.518. This rulemaking is
intended to accommodate changes in
event dates for recurring marine events
specified in this regulation. The marine
events included in this proposed rule
include the Safety at Sea Seminar, U.S.
Naval Academy Crew Races and the
Blue Angels Air Show. This proposed
rule is intended to restrict vessel traffic
in portions of the Severn River during
the period of these marine events and is
necessary to provide for the safety of life
on navigable waters during the event.
DATES: Comments and related material
must reach the Coast Guard on or before
March 5, 2007.
ADDRESSES: You may mail comments
and related material to Commander
(dpi), Fifth Coast Guard District, 431
Crawford Street, Portsmouth, Virginia
23704–5004, hand-deliver them to
Room 415 at the same address between
9 a.m. and 2 p.m., Monday through
Friday, except Federal holidays, or fax
them to (757) 391–8149. The Inspection
and Compliance Branch, Fifth Coast
Guard District, maintains the public
docket for this rulemaking. Comments
and material received from the public,
as well as documents indicated in this
preamble as being available in the
docket, will become part of this docket
and will be available for inspection or
copying at the above address between 9
a.m. and 2 p.m., Monday through
Friday, except Federal holidays.
FOR FURTHER INFORMATION CONTACT:
Dennis M. Sens, Project Manager,
Inspections and Compliance Branch, at
(757) 398–6204.
SUPPLEMENTARY INFORMATION:
Request for Comments
We encourage you to participate in
this rulemaking by submitting
comments and related material. If you
do so, please include your name and
address, identify the docket number for
this rulemaking (CGD05–07–001),
VerDate Aug<31>2005
15:30 Jan 31, 2007
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4669
indicate the specific section of this
document to which each comment
applies, and give the reason for each
comment. Please submit all comments
and related material in an unbound
format, no larger than 81⁄2 by 11 inches,
suitable for copying. If you would like
to know they reached us, please enclose
a stamped, self-addressed postcard or
envelope. We will consider all
comments and material received during
the comment period. We may change
this proposed rule in view of them.
Public Meeting
We do not now plan to hold a public
meeting. But you may submit a request
for a meeting by writing to the address
listed under ADDRESSES explaining why
one would be beneficial. If we
determine that one would aid this
rulemaking, we will hold one at a time
and place announced by a later notice
in the Federal Register.
Background and Purpose
We propose to amend 33 CFR 100.518
to accommodate changes to the
enforcement period for U.S. Naval
Academy sponsored marine events.
Each year the U.S. Naval Academy hosts
various marine events on the Severn
River adjacent to the academy.
Organized collegiate crew races are
typically held annually during
weekends in March, April and May. The
Blue Angels air show is normally
scheduled during graduation week at
the U.S. Naval Academy. Maritime
traffic is prohibited from using the
regulated area of the Severn River
during air show performances in
accordance with Federal Aviation
Administration requirements. The
proposed dates for marine events for
2007 will be; Safety at Sea Seminar on
March 24, 2007; U.S. Naval Academy
crew races on May 6 and May 27, 2007;
and the Blue Angels air show on May
23 and May 24, 2007. The events will
be enforced from 5 a.m. to 6 p.m. on
those days and if the event’s daily
activities should conclude prior to 6
p.m., enforcement of this proposed
regulation may be terminated for that
day at the discretion of the Patrol
Commander. The U.S. Naval Academy
is the sponsor for all of these events and
intends to hold them annually on the
dates provided in 33 CFR 100.518.
Discussion of Proposed Rule
The Coast Guard proposes to amend
the regulations at 33 CFR 100.518 to
accommodate the dates of annual
recurring U.S. Naval Academy marine
events. The changes are necessary to
reflect new enforcement dates. These
proposed changes are needed to control
E:\FR\FM\01FEP1.SGM
01FEP1
]]>Agencies
[Federal Register Volume 72, Number 21 (Thursday, February 1, 2007)]
[Proposed Rules]
[Pages 4663-4669]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-1604]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-26498; Directorate Identifier 2006-CE-83-AD]
RIN 2120-AA64
Airworthiness Directives; The Cessna Aircraft Company Models 208
and 208B Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to supersede Airworthiness Directive (AD) 2006-06-
06, which applies to certain Cessna Aircraft Company (Cessna) Models
208 and 208B airplanes. AD 2006-06-06 currently requires you to
incorporate information into the applicable section of the Airplane
Flight Manual (AFM) and Pilot's Operating Handbook (POH) and requires
installation of placards. Since we issued AD 2006-06-06, Cessna issued
further revisions to the AFM Supplement S1 ``Known Icing Equipment''
and developed a low airspeed awareness system. Consequently, this
proposed AD would require you to incorporate the AFM Supplement
revisions, to install the low airspeed awareness system, and to retain
the requirements of AD 2006-06-06 until the above requirements are
incorporated. We are proposing this AD to assure that the pilot has
enough information and the necessary equipment to prevent loss of
control of the airplane while in flight during icing conditions.
DATES: We must receive comments on this proposed AD by March 5, 2007.
ADDRESSES: Use one of the following addresses to comment on this
proposed AD:
DOT Docket Web site: Go to https://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to https://
www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401,
Washington, DC 20590-0001.
Fax: (202) 493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
Federal eRulemaking Portal: https://www.regulations.gov.
Follow the instructions for submitting comments.
For service information identified in this proposed AD, contact The
Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita,
Kansas 67277.
FOR FURTHER INFORMATION CONTACT: Robert P. Busto, Aerospace Engineer,
Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Wichita,
Kansas 67209; telephone: (316) 946-4157; fax: (316) 946-4107.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments regarding this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include the docket
[[Page 4664]]
number, ``FAA-2006-26498; Directorate Identifier 2006-CE-83-AD'' at the
beginning of your comments. We specifically invite comments on the
overall regulatory, economic, environmental, and energy aspects of the
proposed AD. We will consider all comments received by the closing date
and may amend the proposed AD in light of those comments.
We will post all comments we receive, without change, to https://
dms.dot.gov, including any personal information you provide. We will
also post a report summarizing each substantive verbal contact we
receive concerning this proposed AD.
Discussion
Several accidents/incidents with Cessna Models 208 and 208B
airplanes during operations in icing conditions, including six
accidents in the 2003/2004 icing season and nine accidents in the 2004/
2005 icing season, caused us to issue AD 2005-07-01, Amendment 39-14025
(70 FR 15223), which required the incorporation of revisions into
applicable section of the AFM, and AD 2006-01-11, Amendment 39-14450
(71 FR 16994). AD 2006-01-11 requires the installation of a pilot
assist handle, pneumatic deicing boots on the cargo pod and landing
gear struts, and changes to the Limitations Section of the AFM if the
airplane is to be operated in ground icing conditions and approved for
flight into known or forecast icing conditions. AD 2005-07-01 was
superseded by AD 2006-06-06, Amendment 39-14514 (71 FR 13533, March 16,
2006). AD 2006-06-06 currently requires the following on certain Cessna
Models 208 and 208B airplanes:
Incorporation of revisions to the FAA-approved AFM and
FAA-approved AFM Supplement S1 ``Known Icing Equipment;''
Incorporation of new text in the Limitations Section of
the AFM and AFM Supplement; and
Incorporation of new text in the Performance Section of
the AFM Supplement and the fabrication and installation of placards.
AD 2006-06-06 was intended to be an interim action. Cessna has
since published revisions to the AFM Supplement S1 ``Known Icing
Equipment,'' which incorporates climb performance data in icing
conditions. This data is to be used for preflight planning and as an
in-flight limitation. AD 2006-06-06 included a limitation on autopilot
use as an interim action until the development of an acceptable low
speed awareness system. Cessna has issued service information
introducing this system. Cessna has also developed specific training
for operation of the Models 208 and 208B airplanes in icing conditions.
This training is available on-line at: https://www.cessnaelearning.com
or as part of the Cessna Winter Awareness Seminars.
If the pilot does not have enough information in the AFM or the
necessary equipment to conduct safe flight into icing conditions, then
loss of control could occur.
Relevant Service Information
We have reviewed Cessna Caravan Service Bulletin (SB) CAB06-8,
dated September 18, 2006; Cessna Caravan SB CAB06-11, dated October 9,
2006; and Cessna Caravan Service Kit (SK) 208-171, dated October 9,
2006.
The service information includes the following:
Cessna Caravan SB CAB06-8: revisions to the Pilot's
Operating Handbook (POH) Supplement S1 ``Known Icing Equipment'' and
installation instructions for installation of operational placards; and
Cessna Caravan SB CAB06-11: announces the availability of
a Service Kit which provides parts and instructions to install a new
low airspeed awareness system.
Cessna Caravan SK208-171: instructions for the
installation of a new icing low speed awareness system.
In addition, Cessna has developed revisions to the AFM Supplement
S1 ``Known Icing Equipment'' as follows:
------------------------------------------------------------------------
Document Affects
------------------------------------------------------------------------
Revision 9 of the Model 208 (675 SHP) Cessna Model 208 airplanes with
FAA-approved Flight Manual Supplement a Pratt & Whitney of Canada
S1 ``Known Icing Equipment,'' Cessna Ltd., PT6A-114A turboprop
document D1352-S1-09, dated August 24, engine installed (675 SHP) or
2006. FAA-approved engine of
equivalent or higher
horsepower installed, equipped
with airframe deicing
pneumatic boots, that are not
currently prohibited from
flight in known or forecast
icing.
Revision 8 of the Model 208 (600 SHP) Cessna Model 208 airplanes with
FAA-approved Flight Manual Supplement a Pratt & Whitney of Canada
S1 ``Known Icing Equipment,'' Cessna Ltd., PT6A-114 turboprop
document D1307-S1-08, dated August 24, engine installed (600 SHP) or
2006. FAA-approved engine of
equivalent horsepower
installed, equipped with
airframe deicing pneumatic
boots, that are not currently
prohibited from flight in
known or forecast icing.
Revision 9 of the 208B (675 SHP) FAA- Cessna Model 208B airplanes
approved Flight Manual Supplement S1 with a Pratt & Whitney of
``Known Icing Equipment,'' Cessna Canada Ltd., PT6A-114A
document D1329-S1-09, dated August 24, turboprop engine installed
2006. (675 SHP) or FAA-approved
engine of equivalent or higher
horsepower installed, equipped
with airframe deicing
pneumatic boots, that are not
currently prohibited from
flight in known or forecast
icing.
Revision 9 of the 208B (600 SHP) FAA- Cessna Model 208B airplanes
approved Flight Manual Supplement S1 with a Pratt & Whitney of
``Known Icing Equipment,'' Cessna Canada Ltd., PT6A-114
document D1309-S1-09, dated August 24, turboprop engine installed
2006. (600 SHP) or FAA-approved
engine of equivalent
horsepower installed, equipped
with airframe deicing
pneumatic boots, that are not
currently prohibited from
flight in known or forecast
icing.
------------------------------------------------------------------------
FAA's Determination and Requirements of the Proposed AD
We are proposing this AD because we evaluated all information and
determined the unsafe condition described previously is likely to exist
or develop on other products of the same type design. This proposed AD
would supersede AD 2006-06-06 with a new AD that would:
Require the actions in the previously referenced service
information; and
Retain the actions of AD 2006-06-06 until the above
requirements are incorporated.
Costs of Compliance
We estimate that this proposed AD would affect 765 airplanes in the
U.S. registry.
We estimate the following costs to do the proposed actions:
[[Page 4665]]
----------------------------------------------------------------------------------------------------------------
Total cost per Total cost on
Labor cost Parts cost airplane U.S. operators
----------------------------------------------------------------------------------------------------------------
22 work-hours x $80 per hour = $1,760........................ $6,440 $8,200 $6,273,000
----------------------------------------------------------------------------------------------------------------
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
subtitle VII, part A, subpart III, section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We have determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify that the proposed
regulation:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this proposed AD and placed it in the AD docket.
Examining the AD Docket
You may examine the AD docket that contains the proposed AD, the
regulatory evaluation, any comments received, and other information on
the Internet at https://dms.dot.gov; or in person at the Docket
Management Facility between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The Docket Office (telephone (800) 647-5227)
is located at the street address stated in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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]
2. The FAA amends Sec. 39.13 by removing Airworthiness Directive
(AD) 2006-06-06, Amendment 39-14514, (71 FR 13533, March 16, 2006), and
adding the following new AD:
Cessna Aircraft Company: Docket No. FAA-2006-26498; Directorate
Identifier 2006-CE-83-AD.
Comments Due Date
(a) We must receive comments on this airworthiness directive
(AD) action by March 5, 2007.
Affected ADs
(b) This AD supersedes AD 2006-06-06, Amendment 39-14514.
Applicability
(c) This AD applies to Models 208 and 208B, all serial numbers
that are certificated in any category.
Unsafe Condition
(d) This AD results from our determination that further
revisions to the Airplane Flight Manual (AFM) Supplement S1 ``Known
Icing Equipment'' are necessary, and the installation of a low
airspeed awareness system is required. We are issuing this AD to
assure that the pilot has enough information and the necessary
equipment to prevent loss of control of the airplane while in-flight
during icing conditions.
New Actions Required by This AD
(e) Within the next 30 days after the effective date of this AD,
do the following, unless already done:
(1) For all Model 208 and 208B aircraft not currently restricted
from flight into known or forecast icing: Install a low airspeed
awareness system following the instructions in Cessna Service
Bulletin CAB06-11 and Service Kit SK 208-171, both dated October 9,
2006.
(2) Incorporate the following revisions to the AFM Supplement S1
``Known Icing Equipment'' as applicable:
------------------------------------------------------------------------
Document Affects
------------------------------------------------------------------------
(i) Revision 9 of the Model 208 (675 Cessna Model 208 airplanes with
SHP) FAA-approved Flight Manual a Pratt & Whitney of Canada
Supplement S1 ``Known Icing Ltd., PT6A-114A turboprop
Equipment,'' Cessna document D1352-S1- engine installed (675 SHP) or
09, dated August 24, 2006. FAA-approved engine of
equivalent or higher
horsepower installed, equipped
with airframe deicing
pneumatic boots, that are not
currently prohibited from
flight in known or forecast
icing.
(ii) Revision 8 of the Model 208 (600 Cessna Model 208 airplanes with
SHP) FAA-approved Flight Manual a Pratt & Whitney of Canada
Supplement S1 ``Known Icing Ltd., PT6A-114 turboprop
Equipment,'' Cessna document D1307-S1- engine installed (600 SHP) or
08, dated August 24, 2006. FAA-approved engine of
equivalent horsepower
installed, equipped with
airframe deicing pneumatic
boots, that are not currently
prohibited from flight in
known or forecast icing.
(iii) Revision 9 of the Model 208B (675 Cessna Model 208B airplanes
SHP) FAA-approved Flight Manual with a Pratt & Whitney of
Supplement S1 ``Known Icing Canada Ltd., PT6A-114A
Equipment,'' Cessna document D1329-S1- turboprop engine installed
09, dated August 24, 2006. (675 SHP) or FAA-approved
engine of equivalent or higher
horsepower installed, equipped
with airframe deicing
pneumatic boots, that are not
currently prohibited from
flight in known or forecast
icing.
[[Page 4666]]
(iv) Revision 9 of the Model 208B (600 Cessna Model 208B airplanes
SHP) FAA-approved Flight Manual with a Pratt & Whitney of
Supplement S1 ``Known Icing Canada Ltd., PT6A-114
Equipment,'' Cessna document D1309-S1- turboprop engine installed
09, dated August 24, 2006. (600 SHP) or FAA-approved
engine of equivalent
horsepower installed, equipped
with airframe deicing
pneumatic boots, that are not
currently prohibited from
flight in known or forecast
icing.
------------------------------------------------------------------------
(3) For all Model 208 and 208B aircraft equipped with pneumatic
deicing boots, and not currently restricted from flight into known
or forecast icing: incorporate the following information in the
Limitations Section of the Airplane Flight Manual (AFM) Supplement
S1 ``Known Icing Equipment'' to require pilot training before
further flight into known or forecast icing conditions. 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 specified in paragraphs
(e)(3)(i) and (e)(3)(ii) 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 this portion of the AD in accordance with section 43.9 of the
Federal Aviation Regulations (14 CFR 43.9):
(i) ``The pilot-in-command must successfully complete specific
training for flight into icing conditions provided by Cessna
Aircraft Company within the 12 calendar months preceding any flight
into known or forecast icing conditions.
Completion of either of the following courses will meet this
training requirement:
Caravan Cold Wx Ops Onsite--C14694--(CAC 14694)
Caravan Cold Wx Ops Online--C14695--(CAC 14695)''
(ii) ``Note: The three-hour, on-line training course became
available on October 2, 2006, at: https://www.cessnaelearning.com.
The three-hour on-site training courses are scheduled annually in
October at various locations and provided by Cessna Aircraft Company
at no cost as part of the Cessna Winter Awareness Seminars.
Confirmation of pilot training completion will be maintained by
Cessna Aircraft Company. Please note that all operators of the
affected airplanes must initiate action to notify and ensure that
flight crewmembers are aware of this requirement.''
(f) The actions in paragraphs (g) and (h) below are retained in
this AD from AD 2006-06-06. The new actions required by this AD in
paragraph (e) above terminates the requirement for the actions in
paragraphs (g) and (h).
(g) No later than March 27, 2006 (3 days after March 24, 2006,
which is the effective date of AD 2006-06-06), incorporate the
following revisions into the Airplane Flight Manual (AFM), unless
already accomplished:
------------------------------------------------------------------------
Incorporate the following AFM
Affected airplanes revision document
------------------------------------------------------------------------
(1) Cessna Model 208 airplanes and Section 2: Limitations and
Model 208B airplanes, all serial Section 4: Normal Procedures:
numbers. Temporary Revision 208PHTR05,
dated June 27, 2005, to the
POH and FAA-approved AFM.
(2) Cessna Model 208 airplanes with a Section 9: Optional Systems
Pratt & Whitney of Canada Ltd., PT6A- Description and Operating
114A turboprop engine installed (675 Procedures: Revision 6 of the
SHP) or FAA-approved engine of 208 (675 SHP) POH/FAA-approved
equivalent horsepower installed, AFM Supplement S1 ``Known
equipped with airframe deicing Icing Equipment,'' Cessna
pneumatic boots, that are not document D1352-S1-06, dated
currently prohibited from flight in June 27, 2005.
known or forecast icing.
(3) Cessna Model 208 airplanes with a Section 9: Optional Systems
Pratt & Whitney of Canada Ltd., PT6A- Description and Operating
114 turboprop engine installed (600 Procedures: Revision 6 of the
SHP) or FAA-approved engine of Cessna Model 208 (600 SHP) POH/
equivalent horsepower installed, FAA-approved AFM Supplement S1
equipped with airframe deicing ``Known Icing Equipment,''
pneumatic boots, that are not Cessna document D1307-S1-06,
currently prohibited from flight in dated June 27, 2005.
known or forecast icing.
(4) Cessna Model 208B airplanes with a Section 9: Optional Systems
Pratt & Whitney of Canada Ltd., PT6A- Description and Operating
114A turboprop engine installed (675 Procedures: Revision 7 of the
SHP) or FAA-approved engine of 208B (675 SHP) POH/FAA-
equivalent horsepower installed, approved AFM Supplement S1
equipped with airframe deicing ``Known Icing Equipment,''
pneumatic boots, that are not Cessna document D1329-S1-07,
currently prohibited from flight in dated June 27, 2005.
known or forecast icing.
(5) Cessna Model 208B airplanes with a Section 9: Optional Systems
Pratt & Whitney of Canada Ltd., PT6A- Description and Operating
114 turboprop engine installed (600 Procedures: Revision 6 of the
SHP) or FAA-approved engine of 208B (600 SHP) POH/FAA-
equivalent horsepower installed, approved AFM Supplement S1
equipped with airframe deicing ``Known Icing Equipment,''
pneumatic boots, that are not Cessna document D1309-S1-06,
currently prohibited from flight in dated June 27, 2005.
known or forecast icing.
------------------------------------------------------------------------
(h) You must do the following actions, unless already done.
These changes are to the POH and FAA-approved AFM and to the POH/
FAA-approved AFM Supplement S1 ``Known Icing Equipment'' mandated in
paragraph (g) of this AD:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
(1) For Cessna Model 208 No later than Not Applicable.
airplanes and Model 208B March 27, 2006 (3
airplanes, all serial numbers, days after March
equipped with airframe deicing 24, 2006, which
pneumatic boots, that are not is the effective
currently prohibited from date of AD 2006-
flight in known or forecast 06-06).
icing: You are prohibited from
continued flight after
encountering moderate or
greater icing conditions. The
airplane can dispatch into
forecast areas of icing but
must exit moderate or greater
icing conditions if encountered.
[[Page 4667]]
(2) For Cessna Model 208 No later than The owner/operator
airplanes and Model 208B March 27, 2006 (3 holding at least
airplanes, all serial numbers, days after March a private pilot
equipped with airframe deicing 24, 2006, which certificate as
pneumatic boots, that are not is the effective authorized by
currently prohibited from date of AD 2006- section 43.7 of
flight in known or forecast 06-06). the Federal
icing: Aviation
(i) Insert the text in Appendix Regulations (14
1 of this AD preceding the CFR 43.7) may
KINDS OF OPERATION LIMITS insert the
paragraph in the LIMITATIONS information into
section of the Cessna Models the POH/AFM as
208 or 208B POH and FAA- specified in
approved AFM.. paragraph (h)(2)
(ii) Insert the text in Appendix of this AD. You
2 of this AD in the LIMITATIONS may insert a copy
section of the Cessna Models of this AD into
208 or 208B POH and FAA- the appropriate
approved AFM KNOWN ICING sections of the
EQUIPMENT SUPPLEMENT S1 at the POH/AFM to comply
beginning of the paragraph with this action.
``REQUIRED EQUIPMENT.''. 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).
(3) For Cessna Model 208 No later than The owner/operator
airplanes and Model 208B March 27, 2006 (3 holding at least
airplanes, all serial numbers, days after March a private pilot
equipped with airframe deicing 24, 2006, which certificate as
pneumatic boots, that are not is the effective authorized by
currently prohibited from date of AD 2006- section 43.7 of
flight in known or forecast 06-06). the Federal
icing: Install 3 placards with Aviation
black letters on a white Regulations (14
background. The placards shall CFR 43.7) may
be located on the instrument install the
panel in one of the following placards as
areas: under the radio stack, specified in
immediately above the pilot's paragraph (h)(3)
flight instruments, or below of this AD. Make
the pilot's vertical speed an entry into the
indicator. Lettering on the aircraft records
placard shall be a minimum showing
height of \1/8\-inch. compliance with
(i) Placard 1 shall include the portion of the AD
text of Appendix 3 of this AD.. in accordance
(ii) Placard 2 shall include the with section 43.9
following text: ``120 KIAS of the Federal
Minimum in Icing Flaps Up Aviation
except 110 KIAS if Climbing to Regulations (14
Exit Icing.''. CFR 43.9).
(iii) Placard 3 shall include
the following text:
``Disconnect autopilot at first
indication of ice accretion.''.
(4) For Cessna Model 208 No later than The owner/operator
airplanes and Model 208B March 27, 2006 (3 holding at least
airplanes, all serial numbers, days after March a private pilot
equipped with airframe deicing 24, 2006, which certificate as
pneumatic boots, that are not is the effective authorized by
currently prohibited from date of AD 2006- section 43.7 of
flight in known or forecast 06-06). the Federal
icing: Aviation
(i) Insert the text in Appendix Regulations (14
4 of this AD under the CFR 43.7) may
``AIRSPEED LIMITATIONS'' insert the
paragraph in the LIMITATIONS information into
section of the Cessna Models the POH/AFM as
208 or 208B POH and FAA- specified in
approved AFM.. paragraph (h)(4)
(ii) Replace the text in the of this AD. You
KNOWN ICING EQUIPMENT may insert a copy
SUPPLEMENT S1 under the of this AD into
``MINIMUM SPEED IN ICING the appropriate
CONDITIONS'' paragraph with the sections of the
text in Appendix 4.. POH/AFM to comply
(iii) Insert the following text with this action.
in the LIMITATIONS section of Make an entry
the POH/AFM under the ``OTHER into the aircraft
LIMITATIONS'' paragraph and in records showing
the LIMITATIONS section of the compliance with
KNOWN ICING EQUIPMENT portion of the AD
SUPPLEMENT S1 under the in accordance
``AUTOPILOT OPERATION IN ICING with section 43.9
CONDITIONS'' paragraph: of the Federal
``Disconnect autopilot at first Aviation
indication of ice accretion.''. Regulations (14
CFR 43.9).
[[Page 4668]]
(5) For Cessna Model 208 No later than The owner/operator
airplanes and Model 208B March 27, 2006 (3 holding at least
airplanes, all serial numbers, days after March a private pilot
equipped with airframe deicing 24, 2006, which certificate as
pneumatic boots, that are not is the effective authorized by
currently prohibited from date of AD 2006- section 43.7 of
flight in known or forecast 06-06). the Federal
icing: Aviation
(i) Replace the text in the Regulations (14
PERFORMANCE section of the CFR 43.7) may
Cessna Models 208 or 208B POH insert the
and FAA-approved AFM KNOWN information into
ICING EQUIPMENT SUPPLEMENT S1 the POH/AFM as
under the ``STALL SPEEDS'' specified in
paragraph with the text in paragraph (h)(5)
Appendix 5.. of this AD. You
(ii) Replace the ``WARNING'' may insert a copy
text in the LIMITATIONS section of this AD into
of the Cessna Models 208 or the appropriate
208B POH and FAA-approved AFM sections of the
KNOWN ICING EQUIPMENT POH/AFM to comply
SUPPLEMENT S1 under with this action.
``ENVIRONMENTAL CONDITIONS'' Make an entry
with: ``FLIGHT IN THESE into the aircraft
CONDITIONS ARE PROHIBITED.''. records showing
(iii) Replace the last two compliance with
sentences in the LIMITATIONS portion of the AD
section of the Cessna Models in accordance
208 or 208B POH and FAA- with section 43.9
approved AFM KNOWN ICING of the Federal
EQUIPMENT SUPPLEMENT S1 under Aviation
``ENVIRONMENTAL CONDITIONS'' Regulations (14
with the following text: ``Exit CFR 43.9).
strategies should be determined
during pre-flight planning.''.
------------------------------------------------------------------------
Alternative Methods of Compliance (AMOCs)
(i) The Manager Wichita Aircraft Certification Office (ACO),
FAA, ATTN: Robert P. Busto, Aerospace Engineer, Wichita Aircraft
Certification Office, FAA, 1801 Airport Road, Wichita, Kansas 67209;
telephone: (316) 946-4157; fax: (316) 946-4107, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19.
Related Information
(j) To get copies of the service information referenced in this
AD, contact: The Cessna Aircraft Company, Product Support, P.O. Box
7706, Wichita, Kansas 67277. 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, or on the
Internet at https://dms.dot.gov. The docket number is Docket No. FAA-
2006-26498; Directorate Identifier 2006-CE-83-AD.
Appendix 1 Retained From AD 2006-06-06
Changes to the Cessna Models 208 or 208B Pilot's Operating Handbook
(POH) and FAA-Approved Airplane Flight Manual (AFM)
Affected Cessna Models 208 or 208B POH and FAA-Approved AFM
Insert the following text at the beginning of the KINDS OF
OPERATION LIMITS paragraph in the LIMITATIONS section of the Cessna
Models 208 or 208B POH and FAA-approved AFM. This may be done by
inserting a copy of this AD into the POH/AFM:
``Continued flight after encountering moderate or greater icing
conditions is prohibited. One or more of the following defines
moderate icing conditions for this airplane:
Indicated airspeed in level cruise flight at constant power
decreases by 20 knots. Engine torque required to maintain airspeed
increases by 400 ft. lbs. Airspeed of 120 KIAS cannot be maintained
in level flight. An accretion of \1/4\-inch of ice is observed on
the wing strut.
Disregard any mention of approval for flight in icing conditions
within the POH/AFM.''
Appendix 2 Retained From AD 2006-06-06
Changes to the Cessna Models 208 or 208B Pilot's Operating Handbook
(POH) and FAA-Approved Airplane Flight Manual (AFM)
Affected Cessna Models 208 or 208B POH and FAA-Approved AFM
Insert the following text in the LIMITATIONS section of the POH
and FAA-approved AFM KNOWN ICING EQUIPMENT SUPPLEMENT S1, at the
beginning of the paragraph ``REQUIRED EQUIPMENT.'' This may be done
by inserting a copy of this AD into the POH/AFM:
``Continued flight after encountering moderate or greater icing
conditions is prohibited. One or more of the following defines
moderate icing conditions for this airplane:
Indicated airspeed in level flight at constant power decreases
by 20 knots. Engine torque required to maintain airspeed increases
by 400 ft. lbs. Airspeed of 120 KIAS cannot be maintained in level
flight. An accretion of \1/4\-inch of ice is observed on the wing
strut.
Disregard any mention of approval for flight in icing conditions
within the POH/AFM.''
Appendix 3 Retained From 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.''
Appendix 4 Retained From AD 2006-06-06
Changes to the Cessna Models 208 or 208B Pilot's Operating Handbook
(POH) and FAA-Approved Airplane Flight Manual (AFM) Supplement S1
Affected Cessna Models 208 or 208B POH and FAA-Approved AFM and
FAA-Approved Supplement S1
Insert the following text into the LIMITATIONS section under the
``AIRSPEED LIMITATIONS'' paragraph of the Cessna
[[Page 4669]]
Models 208 or 208B POH and FAA-approved 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[deg]: 105 KIAS
Flaps 20[deg]: 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 adequate
stall warning when in icing conditions.''
Note: These are minimum speeds for operations in icing
conditions. Disregard any reference to the original speeds within
the POH/AFM.
Appendix 5 Retained From AD 2006-06-06
Changes to the Cessna Models 208 or 208B Pilot's Operating Handbook
(POH) and FAA-Approved Airplane Flight Manual (AFM) 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 January 25, 2007.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. E7-1604 Filed 1-31-07; 8:45 am]
BILLING CODE 4910-13-P
