Airworthiness Directives; Aviat Aircraft Inc. Airplanes, 27930-27932 [2019-12621]
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27930
Federal Register / Vol. 84, No. 116 / Monday, June 17, 2019 / Rules and Regulations
required to furnish information to
entities that have received preliminary
approval for registration pursuant to
§ 1041.11(c)(1) but are not registered
pursuant to § 1041.11(c)(2).
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Section 1041.11—Registered
Information Systems
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11(c) Registration of Information
Systems Prior to November 19, 2020
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11(d) Registration of Information
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Examining the AD Docket
*
Dated: June 5, 2019.
Kathleen L. Kraninger,
Director, Bureau of Consumer Financial
Protection.
[FR Doc. 2019–12307 Filed 6–14–19; 8:45 am]
BILLING CODE 4810–AM–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2017–0418; Product
Identifier 2016–CE–041–AD; Amendment
39–19645; AD 2019–10–06]
RIN 2120–AA64
Airworthiness Directives; Aviat Aircraft
Inc. Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for certain
Aviat Aircraft Inc. Models A–1C–180
and A–1C–200 airplanes equipped with
a Rapco part number RA1798–00–1 fuel
vent check valve installed on either
wing or both. This AD was prompted by
a report that the fuel tank vent check
valves are sticking in the closed position
causing fuel starvation to the engine.
This AD requires revision of the
airplane flight manual (AFM) to add a
pre-flight check of the fuel vent check
valves for proper operation and
replacing any inoperative fuel vent
check valve with an airworthy part. We
are issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective July 22,
2019.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of July 22, 2019.
khammond on DSKBBV9HB2PROD with RULES
SUMMARY:
VerDate Sep<11>2014
15:54 Jun 14, 2019
For service information
identified in this final rule, contact
Aviat Aircraft Inc., P.O. Box 1240,
Afton, WY 83110; phone (307) 885–
3151; fax: (307) 885–9674; email: aviat@
aviataircraft.com; internet: https://
aviataircraft.com. You may view this
service information at the FAA, Policy
and Innovation Division, 901 Locust,
Kansas City, Missouri 64106. For
information on the availability of this
material at the FAA, call (816) 329–
4148. It is also available on the internet
at https://www.regulations.gov by
searching for and locating Docket No.
FAA–2017–0418.
ADDRESSES:
Jkt 247001
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2017–
0418; or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this final rule,
the regulatory evaluation, any
comments received, and other
information. The address for Docket
Operations (phone: 800–647–5527) is
Docket Operations, U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT:
Richard R. Thomas, Aviation Safety
Engineer, FAA, Denver Aircraft
Certification Office (ACO) Branch,
26805 East 68th Avenue, Room 214,
Denver, Colorado 80249; phone: (303)
342–1085; fax: (303) 342–1088; email:
richard.r.thomas@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain Aviat Aircraft Inc.
(Aviat) Models A–1C–180 and A–1C–
200 airplanes equipped with Rapco part
number (P/N) RA1798–00–1 fuel vent
check valves. The NPRM published in
the Federal Register on May 5, 2017 (82
FR 21142). The NPRM was prompted by
a report of the fuel tank vent check
valves sticking in the closed position
causing fuel starvation to the engine.
The incident airplane was equipped
with Rapco P/N RA1798–00–1 fuel vent
check valves. As designed, the check
valve ball seat on this P/N valve is
nearly the same diameter as the ball and
the ball can readily wedge itself in the
seat and block the fuel tank vent. The
NPRM proposed to require revising the
AFM to add a pre-flight check of the
PO 00000
Frm 00024
Fmt 4700
Sfmt 4700
fuel vent check valves for proper
operation and replacing any inoperative
fuel vent check valve with a Dukes
P/N 1798–00–1 fuel check valve.
Actions Since the NPRM was Issued
Since we issued the NPRM, Aviat
designed a new fuel vent check valve,
P/N 38266–501, that can be installed in
place of the Rapco fuel vent check
valve. We determined this Aviat fuel
vent check valve is not subject to the
unsafe condition. We also determined
that the Dukes fuel vent check valve, P/
N 1798–00–1, cannot be installed to
replace a Rapco fuel vent check valve
due to a difference in length.
Accordingly, we revised paragraph (i) of
this AD to require replacing inoperative
Rapco fuel vent check valves with Aviat
valves instead of Dukes valves. We also
removed the note from the Applicability
section that referenced the Dukes valve.
We are issuing this AD to correct the
unsafe condition on these products.
Comments
We gave the public the opportunity to
participate in developing this final rule.
We received no comments on the NPRM
or on the determination of the cost to
the public.
Additional Changes Made to the Final
Rule
We updated the on-condition parts
cost to reflect that removing and
replacing the Rapco fuel vent check
valve requires cutting a hole in the wing
skin and installing an access cover over
the hole once the valve has been
replaced. We added the minimal cost of
this cover to the on-condition parts cost.
Labor cost was unaffected by the cover
installation.
We clarified the requirement to
amend the AFM and added a fourth step
to the AFM amendment to alert the
owner/operator (pilot) that an
inoperative check valve must be
replaced in accordance with this AD.
We also removed the requirement to
make a maintenance entry under part
43, as revising a flight manual is not a
maintenance action. A record of the
AFM change must still be made as
required by 14 CFR 91.417(a)(2)(v).
We refined the requirements to
remove and replace an inoperative fuel
vent check valve by removing the
references to steps 4 and 9 of the service
information. Step 4 of the service
information is no longer necessary due
to other changes to this AD, and step 9
is unnecessary for this AD because it is
required by standard maintenance
practices under 14 CFR part 43. We also
changed the language regarding
replacing both valves with valves that
E:\FR\FM\17JNR1.SGM
17JNR1
Federal Register / Vol. 84, No. 116 / Monday, June 17, 2019 / Rules and Regulations
are unaffected by this AD from ‘‘the
repetitive pre-flight checks required in
paragraph (g) of this AD are terminated’’
to ‘‘you may remove the AFM revisions
required by paragraph (g) of this AD.’’
This change makes it clear that
operators do not need an alternative
method of compliance (AMOC) to return
the AFM to its pre-AD configuration if
they remove both Rapco valves.
Lastly, we added a second email
address for requesting an AMOC.
Requests must be submitted to both the
assigned Aviation Safety Engineer and
the Denver ACO Branch general email
addresses.
27931
dated November 11, 2016. The service
bulletin contains procedures for
checking the fuel vent check valve on
each wing of the airplane for proper
operation and replacing any inoperative
fuel vent check valve. This service
information is reasonably available
because the interested parties have
access to it through their normal course
of business or by the means identified
in the ADDRESSES section.
Conclusion
We reviewed the relevant data and
determined that air safety and the
public interest require adopting this
final rule as proposed except for the
changes previously discussed. We have
determined that these changes:
• Are consistent with the intent that
was proposed in the NPRM for
correcting the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
Costs of Compliance
Related Service Information Under 1
CFR Part 51
We reviewed Aviat Mandatory
Service Bulletin No. 33, Initial Release,
We estimate that this AD affects 98
airplanes of U.S. registry.
We estimate the following costs to
comply with this AD:
ESTIMATED COSTS
Action
Labor cost
Pre-flight check of the fuel vent check valve for proper operation as incorporated in the aircraft flight manual.
.5 work-hour × $85 per hour =
$42.50 per pre-flight check.
We conservatively estimated the cost
to do a single pre-flight check. We
recognize the pilot is allowed to perform
this check without the assistance of a
mechanic, which will significantly
reduce the estimated cost. We further
recognize that an individual airplane
will require this check every pre-flight
Parts cost
from the issuance of this AD until the
end of its useful life as long as at least
one P/N RA1798–00–1 fuel vent check
valve is installed on either wing. We
have no way of determining the total
cost of repeating this check every preflight either for a single product or for
all U.S. operators.
N/A
Cost per
product
$42.50
Cost on U.S.
operators
$4,165
We estimate the following costs to do
any necessary replacements that will be
required based on the results of the preflight check. We have no way of
determining the number of airplanes
that may need these replacements.
ON-CONDITION COSTS
Action
Labor cost
Parts cost
Remove and replace inoper- 2 work-hours (1 work-hour to remove and 1 work-hour
ative fuel vent check valve.
to replace) × $85 per hour = $170 per fuel vent
check valve. (There are 2 fuel vent check valves per
airplane = $340 to remove and replace both.).
The access cover cost is for a solid
color. It does not include custom paint
schemes to match an individual
airplane.
khammond on DSKBBV9HB2PROD with RULES
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
VerDate Sep<11>2014
15:54 Jun 14, 2019
Jkt 247001
$330 per fuel vent check
valve and $25 per access cover. ($710 for
both.).
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.
This AD is issued in accordance with
authority delegated by the Executive
Director, Aircraft Certification Service,
as authorized by FAA Order 8000.51C.
In accordance with that order, issuance
of ADs is normally a function of the
Compliance and Airworthiness
Division, but during this transition
period, the Executive Director has
delegated the authority to issue ADs
applicable to small airplanes, gliders,
balloons, airships, domestic business jet
transport airplanes, and associated
appliances to the Director of the Policy
and Innovation Division.
PO 00000
Frm 00025
Fmt 4700
Sfmt 4700
Cost per product
$525 per fuel vent check
valve. ($1050 to remove
and replace both.)
Regulatory Findings
This AD will not have federalism
implications under Executive Order
13132. This AD will 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 this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Is not a ‘‘significant rule’’ under
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation
in Alaska, and
(4) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
E:\FR\FM\17JNR1.SGM
17JNR1
27932
Federal Register / Vol. 84, No. 116 / Monday, June 17, 2019 / Rules and Regulations
under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 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 adding
the following new airworthiness
directive (AD):
■
2019–10–06 Aviat Aircraft Inc.:
Amendment 39–19645; Docket No. FAA–
2017–0418; Product Identifier 2016–CE–041–
AD.
(a) Effective Date
This AD is effective July 22, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Aviat Aircraft Inc.
(Aviat) Models A–1C–180 and A–1C–200
airplanes, serial numbers 3181 through 3282,
certificated in any category, that are
equipped with a Rapco part number (P/N)
RA1798–00–1 fuel vent check valve on one
or both wings.
(d) Subject
Joint Aircraft System Component (JASC)
Code 2820, Fuel Distribution.
(e) Unsafe Condition
This AD was prompted by a report that
Rapco P/N RA1798–00–1 fuel vent check
valves are sticking in the closed position. We
are issuing this AD to detect and correct
failure of the fuel tank vent check valve,
which could result in fuel starvation to the
engine and cause the engine to shut down.
khammond on DSKBBV9HB2PROD with RULES
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Verify Proper Operation of the Fuel Vent
Check Valve on Each Wing
Before further flight after July 22, 2019 (the
effective date of this AD), revise the airplane
flight manual (AFM) as follows:
(1) Insert into the Limitations Section of
the AFM steps 1 through 3 of the
Accomplishment Instructions in Aviat
Aircraft Inc. Mandatory Service Bulletin
(MSB) No. 33, Initial Release, dated
November 11, 2016 (Aviat SB, No. 33, IR).
VerDate Sep<11>2014
15:54 Jun 14, 2019
Jkt 247001
(2) Immediately following steps 1 through
3, add the following language to the
Limitations Section of the AFM: Step 4. If
there is a stuck fuel vent check valve, it must
be replaced in accordance with AD 2019–10–
06 before further flight.
(3) This AFM revision requires preflight
checks of the fuel vent check valve on each
wing. This insertion and the steps therein
may be performed by the owner/operator
(pilot) holding at least a private pilot
certificate. The AFM revision must be
entered into the aircraft records showing
compliance with this AD in accordance with
14 CFR 91.417(a)(2)(v). The record must be
maintained as required by 14 CFR 91.417,
121.380, or 135.439.
(h) Remove Inoperative Fuel Vent Check
Valve
If a fuel vent check valve is not operating
properly, before further flight, remove the
inoperative valve by following steps 5 and 6
of the Accomplishment Instructions in Aviat
SB, No. 33, IR.
(i) Replace Inoperative Fuel Vent Check
Valve
Before further flight after removing any
inoperative fuel vent check valve as required
by paragraph (h) of this AD, replace it with
an airworthy fuel vent check valve by
following step 8 of the Accomplishment
Instructions in Aviat SB, No. 33, IR. If both
fuel vent check valves, Rapco P/N RA1798–
00–1, are replaced with Aviat P/N 38266–501
fuel vent check valves, you may remove the
AFM revisions required by paragraph (g)(1)
and (2) of this AD.
(j) Special Flight Permit
Special flight permits are not necessary for
the preflight checks. A special flight permit
is allowed for this AD per 14 CFR 39.23 with
limitations. Special flight permits are
permitted for the airplane to be flown visual
flight rules only to a location where the
inoperative fuel vent check valve can be
removed and replaced. No special flight
permits are allowed if both valves are found
to be inoperative.
(k) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Denver ACO Branch,
FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19. In accordance with
14 CFR 39.19, send your request to your
principal inspector or local Flight Standards
District Office, as appropriate. If sending
information directly to the manager of the
ACO, send it to the attention of the person
and office identified in paragraph (l)(1) of
this AD.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
(l) Related Information
For more information about this AD,
contact Richard R. Thomas, Aviation Safety
Engineer (ASE), FAA, Denver ACO Branch,
26805 East 68th Avenue, Room 214, Denver,
Colorado 80249; phone: (303) 342–1085; fax:
PO 00000
Frm 00026
Fmt 4700
Sfmt 4700
(303) 342–1088; email: richard.r.thomas@
faa.gov. If an AMOC is requested by email,
it must be sent to both the ASE’s email and
the Denver ACO Branch general email: 9Denver-Aircraft-Cert@faa.gov.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) Aviat Aircraft Inc. Mandatory Service
Bulletin No. 33, Initial Release, dated
November 11, 2016.
(ii) [Reserved]
(3) For service information identified in
this AD, contact Aviat Aircraft Inc., P.O. Box
1240, Afton, WY 83110; phone (307) 885–
3151; fax: (307) 885–9674; email: aviat@
aviataircraft.com; internet: https://
aviataircraft.com.
(4) You may view this service information
at FAA, Policy and Innovation Division, 901
Locust, Kansas City, Missouri 64106. For
information on the availability of this
material at the FAA, call (816) 329–4148.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA, call
202–741–6030, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued in Kansas City, Missouri, on June
10, 2019.
Melvin J. Johnson,
Aircraft Certification Service, Deputy
Director, Policy and Innovation Division,
AIR–601.
[FR Doc. 2019–12621 Filed 6–14–19; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–0392; Product
Identifier 2019–CE–020–AD; Amendment
39–19639; AD 2019–08–51]
RIN 2120–AA64
Airworthiness Directives; Cirrus
Design Corporation
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; request for
comments.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for all
Cirrus Design Corporation (Cirrus)
Model SF50 airplanes. This AD was sent
previously as an emergency AD to all
known U.S. owners and operators of
SUMMARY:
E:\FR\FM\17JNR1.SGM
17JNR1
Agencies
[Federal Register Volume 84, Number 116 (Monday, June 17, 2019)]
[Rules and Regulations]
[Pages 27930-27932]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-12621]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-0418; Product Identifier 2016-CE-041-AD; Amendment
39-19645; AD 2019-10-06]
RIN 2120-AA64
Airworthiness Directives; Aviat Aircraft Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Aviat Aircraft Inc. Models A-1C-180 and A-1C-200 airplanes equipped
with a Rapco part number RA1798-00-1 fuel vent check valve installed on
either wing or both. This AD was prompted by a report that the fuel
tank vent check valves are sticking in the closed position causing fuel
starvation to the engine. This AD requires revision of the airplane
flight manual (AFM) to add a pre-flight check of the fuel vent check
valves for proper operation and replacing any inoperative fuel vent
check valve with an airworthy part. We are issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective July 22, 2019.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 22,
2019.
ADDRESSES: For service information identified in this final rule,
contact Aviat Aircraft Inc., P.O. Box 1240, Afton, WY 83110; phone
(307) 885-3151; fax: (307) 885-9674; email: [email protected];
internet: https://aviataircraft.com. You may view this service
information at the FAA, Policy and Innovation Division, 901 Locust,
Kansas City, Missouri 64106. For information on the availability of
this material at the FAA, call (816) 329-4148. It is also available on
the internet at https://www.regulations.gov by searching for and
locating Docket No. FAA-2017-0418.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2017-
0418; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, the regulatory evaluation, any comments received, and
other information. The address for Docket Operations (phone: 800-647-
5527) is Docket Operations, U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Richard R. Thomas, Aviation Safety
Engineer, FAA, Denver Aircraft Certification Office (ACO) Branch, 26805
East 68th Avenue, Room 214, Denver, Colorado 80249; phone: (303) 342-
1085; fax: (303) 342-1088; email: [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Aviat Aircraft Inc.
(Aviat) Models A-1C-180 and A-1C-200 airplanes equipped with Rapco part
number (P/N) RA1798-00-1 fuel vent check valves. The NPRM published in
the Federal Register on May 5, 2017 (82 FR 21142). The NPRM was
prompted by a report of the fuel tank vent check valves sticking in the
closed position causing fuel starvation to the engine. The incident
airplane was equipped with Rapco P/N RA1798-00-1 fuel vent check
valves. As designed, the check valve ball seat on this P/N valve is
nearly the same diameter as the ball and the ball can readily wedge
itself in the seat and block the fuel tank vent. The NPRM proposed to
require revising the AFM to add a pre-flight check of the fuel vent
check valves for proper operation and replacing any inoperative fuel
vent check valve with a Dukes P/N 1798-00-1 fuel check valve.
Actions Since the NPRM was Issued
Since we issued the NPRM, Aviat designed a new fuel vent check
valve, P/N 38266-501, that can be installed in place of the Rapco fuel
vent check valve. We determined this Aviat fuel vent check valve is not
subject to the unsafe condition. We also determined that the Dukes fuel
vent check valve, P/N 1798-00-1, cannot be installed to replace a Rapco
fuel vent check valve due to a difference in length. Accordingly, we
revised paragraph (i) of this AD to require replacing inoperative Rapco
fuel vent check valves with Aviat valves instead of Dukes valves. We
also removed the note from the Applicability section that referenced
the Dukes valve.
We are issuing this AD to correct the unsafe condition on these
products.
Comments
We gave the public the opportunity to participate in developing
this final rule. We received no comments on the NPRM or on the
determination of the cost to the public.
Additional Changes Made to the Final Rule
We updated the on-condition parts cost to reflect that removing and
replacing the Rapco fuel vent check valve requires cutting a hole in
the wing skin and installing an access cover over the hole once the
valve has been replaced. We added the minimal cost of this cover to the
on-condition parts cost. Labor cost was unaffected by the cover
installation.
We clarified the requirement to amend the AFM and added a fourth
step to the AFM amendment to alert the owner/operator (pilot) that an
inoperative check valve must be replaced in accordance with this AD. We
also removed the requirement to make a maintenance entry under part 43,
as revising a flight manual is not a maintenance action. A record of
the AFM change must still be made as required by 14 CFR
91.417(a)(2)(v).
We refined the requirements to remove and replace an inoperative
fuel vent check valve by removing the references to steps 4 and 9 of
the service information. Step 4 of the service information is no longer
necessary due to other changes to this AD, and step 9 is unnecessary
for this AD because it is required by standard maintenance practices
under 14 CFR part 43. We also changed the language regarding replacing
both valves with valves that
[[Page 27931]]
are unaffected by this AD from ``the repetitive pre-flight checks
required in paragraph (g) of this AD are terminated'' to ``you may
remove the AFM revisions required by paragraph (g) of this AD.'' This
change makes it clear that operators do not need an alternative method
of compliance (AMOC) to return the AFM to its pre-AD configuration if
they remove both Rapco valves.
Lastly, we added a second email address for requesting an AMOC.
Requests must be submitted to both the assigned Aviation Safety
Engineer and the Denver ACO Branch general email addresses.
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting this final rule as proposed except
for the changes previously discussed. We have determined that these
changes:
Are consistent with the intent that was proposed in the
NPRM for correcting the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
We reviewed Aviat Mandatory Service Bulletin No. 33, Initial
Release, dated November 11, 2016. The service bulletin contains
procedures for checking the fuel vent check valve on each wing of the
airplane for proper operation and replacing any inoperative fuel vent
check valve. This service information is reasonably available because
the interested parties have access to it through their normal course of
business or by the means identified in the ADDRESSES section.
Costs of Compliance
We estimate that this AD affects 98 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Pre-flight check of the fuel vent .5 work-hour x $85 per N/A $42.50 $4,165
check valve for proper operation as hour = $42.50 per pre-
incorporated in the aircraft flight flight check.
manual.
----------------------------------------------------------------------------------------------------------------
We conservatively estimated the cost to do a single pre-flight
check. We recognize the pilot is allowed to perform this check without
the assistance of a mechanic, which will significantly reduce the
estimated cost. We further recognize that an individual airplane will
require this check every pre-flight from the issuance of this AD until
the end of its useful life as long as at least one P/N RA1798-00-1 fuel
vent check valve is installed on either wing. We have no way of
determining the total cost of repeating this check every pre-flight
either for a single product or for all U.S. operators.
We estimate the following costs to do any necessary replacements
that will be required based on the results of the pre-flight check. We
have no way of determining the number of airplanes that may need these
replacements.
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Action Labor cost Parts cost Cost per product
----------------------------------------------------------------------------------------------------------------
Remove and replace inoperative fuel 2 work-hours (1 work-hour $330 per fuel vent $525 per fuel vent
vent check valve. to remove and 1 work-hour check valve and $25 check valve. ($1050
to replace) x $85 per hour per access cover. to remove and replace
= $170 per fuel vent check ($710 for both.). both.)
valve. (There are 2 fuel
vent check valves per
airplane = $340 to remove
and replace both.).
----------------------------------------------------------------------------------------------------------------
The access cover cost is for a solid color. It does not include
custom paint schemes to match an individual airplane.
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.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to small airplanes, gliders,
balloons, airships, domestic business jet transport airplanes, and
associated appliances to the Director of the Policy and Innovation
Division.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will 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 this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979),
(3) Will not affect intrastate aviation in Alaska, and
(4) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities
[[Page 27932]]
under the criteria of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 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. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2019-10-06 Aviat Aircraft Inc.: Amendment 39-19645; Docket No. FAA-
2017-0418; Product Identifier 2016-CE-041-AD.
(a) Effective Date
This AD is effective July 22, 2019.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Aviat Aircraft Inc. (Aviat) Models A-1C-180
and A-1C-200 airplanes, serial numbers 3181 through 3282,
certificated in any category, that are equipped with a Rapco part
number (P/N) RA1798-00-1 fuel vent check valve on one or both wings.
(d) Subject
Joint Aircraft System Component (JASC) Code 2820, Fuel
Distribution.
(e) Unsafe Condition
This AD was prompted by a report that Rapco P/N RA1798-00-1 fuel
vent check valves are sticking in the closed position. We are
issuing this AD to detect and correct failure of the fuel tank vent
check valve, which could result in fuel starvation to the engine and
cause the engine to shut down.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Verify Proper Operation of the Fuel Vent Check Valve on Each Wing
Before further flight after July 22, 2019 (the effective date of
this AD), revise the airplane flight manual (AFM) as follows:
(1) Insert into the Limitations Section of the AFM steps 1
through 3 of the Accomplishment Instructions in Aviat Aircraft Inc.
Mandatory Service Bulletin (MSB) No. 33, Initial Release, dated
November 11, 2016 (Aviat SB, No. 33, IR).
(2) Immediately following steps 1 through 3, add the following
language to the Limitations Section of the AFM: Step 4. If there is
a stuck fuel vent check valve, it must be replaced in accordance
with AD 2019-10-06 before further flight.
(3) This AFM revision requires preflight checks of the fuel vent
check valve on each wing. This insertion and the steps therein may
be performed by the owner/operator (pilot) holding at least a
private pilot certificate. The AFM revision must be entered into the
aircraft records showing compliance with this AD in accordance with
14 CFR 91.417(a)(2)(v). The record must be maintained as required by
14 CFR 91.417, 121.380, or 135.439.
(h) Remove Inoperative Fuel Vent Check Valve
If a fuel vent check valve is not operating properly, before
further flight, remove the inoperative valve by following steps 5
and 6 of the Accomplishment Instructions in Aviat SB, No. 33, IR.
(i) Replace Inoperative Fuel Vent Check Valve
Before further flight after removing any inoperative fuel vent
check valve as required by paragraph (h) of this AD, replace it with
an airworthy fuel vent check valve by following step 8 of the
Accomplishment Instructions in Aviat SB, No. 33, IR. If both fuel
vent check valves, Rapco P/N RA1798-00-1, are replaced with Aviat P/
N 38266-501 fuel vent check valves, you may remove the AFM revisions
required by paragraph (g)(1) and (2) of this AD.
(j) Special Flight Permit
Special flight permits are not necessary for the preflight
checks. A special flight permit is allowed for this AD per 14 CFR
39.23 with limitations. Special flight permits are permitted for the
airplane to be flown visual flight rules only to a location where
the inoperative fuel vent check valve can be removed and replaced.
No special flight permits are allowed if both valves are found to be
inoperative.
(k) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Denver ACO Branch, FAA, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request
to your principal inspector or local Flight Standards District
Office, as appropriate. If sending information directly to the
manager of the ACO, send it to the attention of the person and
office identified in paragraph (l)(1) of this AD.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(l) Related Information
For more information about this AD, contact Richard R. Thomas,
Aviation Safety Engineer (ASE), FAA, Denver ACO Branch, 26805 East
68th Avenue, Room 214, Denver, Colorado 80249; phone: (303) 342-
1085; fax: (303) 342-1088; email: [email protected]. If an
AMOC is requested by email, it must be sent to both the ASE's email
and the Denver ACO Branch general email: [email protected].
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Aviat Aircraft Inc. Mandatory Service Bulletin No. 33,
Initial Release, dated November 11, 2016.
(ii) [Reserved]
(3) For service information identified in this AD, contact Aviat
Aircraft Inc., P.O. Box 1240, Afton, WY 83110; phone (307) 885-3151;
fax: (307) 885-9674; email: [email protected]; internet:
https://aviataircraft.com.
(4) You may view this service information at FAA, Policy and
Innovation Division, 901 Locust, Kansas City, Missouri 64106. For
information on the availability of this material at the FAA, call
(816) 329-4148.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Kansas City, Missouri, on June 10, 2019.
Melvin J. Johnson,
Aircraft Certification Service, Deputy Director, Policy and Innovation
Division, AIR-601.
[FR Doc. 2019-12621 Filed 6-14-19; 8:45 am]
BILLING CODE 4910-13-P