81 FR 3348 - Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company) Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 13 (January 21, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 13 (January 21, 2016)
| Page Range | 3348-3350 | |
| FR Document | 2016-00951 |
[Federal Register Volume 81, Number 13 (Thursday, January 21, 2016)] [Proposed Rules] [Pages 3348-3350] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-00951] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-0460; Directorate Identifier 2015-NM-078-AD] RIN 2120-AA64 Airworthiness Directives; Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company) Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain Beechcraft Corporation Model BAe.125 series 1000A and 1000B airplanes and Model Hawker 1000 airplanes. This proposed AD was prompted by reports of inadvertent stowage of the thrust reversers, which can result in high forward engine thrust even though the throttle is commanding reverse thrust. This proposed AD would require installing kits that include relays, associated wiring, and a thrust reverser fail annunciator. We are proposing this AD to prevent inadvertent stowage of the thrust reversers, which could cause a runway overrun during a rejected takeoff or landing, and consequent structural failure and possible injury to occupants. DATES: We must receive comments on this proposed AD by March 7, 2016. ADDRESSES: You may send comments, using the procedures found in 14 CFR [[Page 3349]] 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this proposed AD, Beechcraft Corporation, TMDC, P.O. Box 85, Wichita, KS 67201-0085; telephone 316- 676-8238; fax 316-671-2540; email [email protected]; Internet http://pubs.beechcraft.com. You may view this referenced service information at FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 0460; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Jeffrey Englert, Aerospace Engineer, Mechanical Systems and Propulsion Branch, ACE-116W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Dwight D. Eisenhower National Airport, Wichita, KS 67209; phone: 316-946-4167; fax: 316-946-4107; email: [email protected]. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2016-0460; Directorate Identifier 2015-NM-078-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD because of those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this proposed AD. Discussion We have received reports of inadvertent stowage of the thrust reversers, which can result in high forward engine thrust even though the throttle is commanding reverse thrust. These reports were on another type of airplane that utilizes a similar engine and thrust reverser system. The root cause is incorrect software logic within the engine's electronic control unit. This condition, if not corrected, could result in inadvertent stowage of the thrust reversers, which could cause a runway overrun during a rejected takeoff or during landing, and consequent structural failure and possible injury to occupants. Related Service Information Under 1 CFR Part 51 We reviewed Beechcraft Mandatory Service Bulletin 78-4133, dated May 2015. The service information describes procedures for installing kits having part numbers 140-9005 and 140-9006, which include relays, associated wiring, and a thrust reverser fail annunciator. 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. FAA's Determination We are proposing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design. Proposed AD Requirements This proposed AD would require accomplishing the actions specified in the service information described previously, except as discussed under ``Differences Between this Proposed AD and the Service Information.'' Differences Between This Proposed AD and the Service Information Although Beechcraft Mandatory Service Bulletin 78-4133, dated May 2015, specifies that ``Should any difficulty be encountered in accomplishing this Service Bulletin, contact Beechcraft Corporation,'' this proposed AD would require operators to resolve difficulties in accordance with a method approved by the FAA. Costs of Compliance We estimate that this proposed AD affects 38 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Installation........................ 340 work-hours x $85 $100,000 $128,900 $4,898,200 per hour = $28,900. ---------------------------------------------------------------------------------------------------------------- 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 determined that this proposed AD would not have federalism implications under Executive Order 13132. This [[Page 3350]] 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 this 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), (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 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. 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 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): Beechcraft Corporation (Type Certificate Previously Held by Hawker Beechcraft Corporation; Raytheon Aircraft Company): Docket No. FAA- 2016-0460; Directorate Identifier 2015-NM-078-AD. (a) Comments Due Date We must receive comments by March 7, 2016. (b) Affected ADs None. (c) Applicability This AD applies to Beechcraft Corporation (type certificate previously held by Hawker Beechcraft Corporation; Raytheon Aircraft Company) airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Model BAe.125 series 1000A and 1000B airplanes, serial numbers 258151, 258159, and 259004 through 259042 inclusive. (2) Model Hawker 1000 airplanes, serial numbers 259003 and 259043 through 259052 inclusive. (d) Subject Air Transport Association (ATA) of America Code 78, Exhaust. (e) Unsafe Condition This AD was prompted by reports of inadvertent stowage of the thrust reversers, which can result in high forward engine thrust even though the throttle is commanding reverse thrust. We are issuing this AD to prevent inadvertent stowage of the thrust reversers, which could cause a runway overrun during a rejected takeoff or landing, and consequent structural failure and possible injury to occupants. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Installation Within 600 flight hours or 12 months after the effective date of this AD, whichever occurs first: Install kits having part numbers 140-9005 and 140-9006, in accordance with the Accomplishment Instructions of Beechcraft Mandatory Service Bulletin 78-4133, dated May 2015, except as specified in paragraph (h) of this AD. (h) Exception to Service Information A note in the Accomplishment Instructions of Beechcraft Mandatory Service Bulletin 78-4133, dated May 2015, instructs operators to contact Beechcraft Corporation if any difficulty is encountered in accomplishing the service bulletin. However, any deviation from the actions required by paragraph (g) of this AD must be approved as an alternative method of compliance (AMOC) under paragraph (i)(1) of this AD. (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Wichita Aircraft Certification Office (ACO), 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 identified in paragraph (j)(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. (j) Related Information (1) For more information about this AD, contact Jeffrey Englert, Aerospace Engineer, Mechanical Systems and Propulsion Branch, ACE- 116W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Dwight D. Eisenhower National Airport, Wichita, KS 67209; phone: 316-946-4167; fax: 316-946-4107; email: [email protected]. (2) For service information identified in this AD, contact Beechcraft Corporation, TMDC, P.O. Box 85, Wichita, KS 67201-0085; telephone 316-676-8238; fax 316-671-2540; email [email protected]; Internet http://pubs.beechcraft.com. You may view this referenced service information at FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. Issued in Renton, Washington, on January 8, 2016. Jeffrey E. Duven, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2016-00951 Filed 1-20-16; 8:45 am] BILLING CODE 4910-13-P
![3348 Federal Register / Vol. 81, No. 13 / Thursday, January 21, 2016 / Proposed Rules
§ 39.13 [Amended] damage, in accordance with the MCAI may be found in the AD docket on the
■ 2. The FAA amends § 39.13 by Accomplishment Instructions of the Internet at http://www.regulations.gov by
removing Airworthiness Directive (AD) applicable service information specified in searching for and locating Docket No. FAA–
paragraph (i) of this AD. 2016–0459.
2015–10–03, Amendment 39–18158 (80 (2) If, during the detailed inspection (2) For service information identified in
FR 30608, May 29, 2015), and adding specified in paragraph (h)(1) of this AD, any this AD, contact Airbus SAS—Airworthiness
the following new AD: corrosion, pitting, or thread damage is found, Office—EAL, 1 Rond Point Maurice Bellonte,
Airbus: Docket No. FAA–2016–0459; before further flight, replace the upper cardan 31707 Blagnac Cedex, France; telephone +33
Directorate Identifier 2015–NM–081–AD. pin and/or nut, as applicable, in accordance 5 61 93 36 96; fax +33 5 61 93 45 80; email
with the Accomplishment Instructions of the airworthiness.A330-A340@airbus.com;
(a) Comments Due Date applicable service information specified in Internet http://www.airbus.com. You may
We must receive comments by March 7, paragraph (i) of this AD. view this service information at the FAA,
2016. (i) Applicable Service Information Transport Airplane Directorate, 1601 Lind
Avenue SW., Renton, WA. For information
(b) Affected ADs Do the actions required by paragraph (h) of on the availability of this material at the
This AD replaces 2015–10–03, Amendment this AD in accordance with the FAA, call 425–227–1221.
39–18158 (80 FR 30608, May 29, 2015). Accomplishment Instructions of the
applicable service information identified in Issued in Renton, Washington, on January
(c) Applicability paragraphs (i)(1), (i)(2), and (i)(3) of this AD. 8, 2016.
This AD applies to the airplanes, (1) Airbus Service Bulletin A330–32–3269, Jeffrey E. Duven,
certificated in any category, identified in dated February 17, 2015 (for Airbus Model Manager, Transport Airplane Directorate,
paragraphs (c)(1), (c)(2), and (c)(3) of this AD, A330–201, –202, –203, –223, –223F, –243, Aircraft Certification Service.
except airplanes on which an upper cardan –243F, –301, –302, –303, –321, –322, –323,
[FR Doc. 2016–00944 Filed 1–20–16; 8:45 am]
pin on a main landing gear (MLG) has never –341, –342, and –343 airplanes).
been replaced or reinstalled since first entry (2) Airbus Service Bulletin A340–32–4301, BILLING CODE 4910–13–P
into service of the airplane. dated February 17, 2015 (for Airbus Model
(1) Airbus Model A330–201, –202, –203, A340–211, –212, –213, –311, –312, and –313
–223, –223F, –243, –243F, –301, –302, –303, airplanes). DEPARTMENT OF TRANSPORTATION
–321, –322, –323, –341, –342, and –343 (3) Airbus Service Bulletin A340–32–5115,
airplanes, all manufacturer serial numbers . dated February 17, 2015 (for Airbus Model Federal Aviation Administration
(2) Airbus Model A340–211, –212, –213, A340–541 and –642 airplanes).
–311, –312, and –313 airplanes, all 14 CFR Part 39
(j) Other FAA AD Provisions
manufacturer serial numbers.
(3) Airbus Model A340–541 and –642 The following provisions also apply to this [Docket No. FAA–2016–0460; Directorate
airplanes, all manufacturer serial numbers. AD: Identifier 2015–NM–078–AD]
(1) Alternative Methods of Compliance
(d) Subject (AMOCs): The Manager, International RIN 2120–AA64
Air Transport Association (ATA) of Branch, ANM–116, Transport Airplane
America Code 32, Landing Gear. Directorate, FAA, has the authority to Airworthiness Directives; Beechcraft
approve AMOCs for this AD, if requested Corporation (Type Certificate
(e) Reason using the procedures found in 14 CFR 39.19. Previously Held by Hawker Beechcraft
This AD was prompted by a report that an In accordance with 14 CFR 39.19, send your Corporation; Raytheon Aircraft
MLG sidestay upper cardan pin migration request to your principal inspector or local Company) Airplanes
event had been caused by corrosion due to Flight Standards District Office, as
lack of jointing compound and inadequate appropriate. If sending information directly AGENCY: Federal Aviation
sealant application during the MLG to the International Branch, send it to ATTN: Administration (FAA), DOT.
installation. We are issuing this AD to detect Vladimir Ulyanov, Aerospace Engineer,
ACTION: Notice of proposed rulemaking
and correct migration of the sidestay upper International Branch, ANM 116, Transport
cardan pin, which could result in Airplane Directorate, FAA, 1601 Lind (NPRM).
disconnection of the sidestay upper arm from Avenue SW., Renton, WA 98057–3356;
the airplane structure, and could result in a telephone 425–227–1138; fax 425–227–1149. SUMMARY: We propose to adopt a new
landing gear collapse and consequent damage Information may be emailed to: 9-ANM-116- airworthiness directive (AD) for certain
to the airplane and injury to occupants. AMOC-REQUESTS@faa.gov. Before using Beechcraft Corporation Model BAe.125
any approved AMOC, notify your appropriate series 1000A and 1000B airplanes and
(f) Compliance principal inspector, or lacking a principal Model Hawker 1000 airplanes. This
Comply with this AD within the inspector, the manager of the local flight proposed AD was prompted by reports
compliance times specified, unless already standards district office/certificate holding of inadvertent stowage of the thrust
done. district office. The AMOC approval letter
must specifically reference this AD.
reversers, which can result in high
(g) Definition forward engine thrust even though the
(2) Contacting the Manufacturer: As of the
For the purpose of this AD, an upper effective date of this AD, for any requirement throttle is commanding reverse thrust.
cardan pin on a MLG is affected if it has been in this AD to obtain corrective actions from This proposed AD would require
installed as a replacement part, or reinstalled a manufacturer, the action must be installing kits that include relays,
since first entry of the airplane into service, accomplished using a method approved by associated wiring, and a thrust reverser
and if the installation was accomplished the Manager, International Branch, ANM– fail annunciator. We are proposing this
using the applicable airplane maintenance 116, Transport Airplane Directorate, FAA; or AD to prevent inadvertent stowage of
manual at a revision level prior to October 1, the European Aviation Safety Agency
2014. (EASA); or Airbus’s EASA Design
the thrust reversers, which could cause
jstallworth on DSK7TPTVN1PROD with PROPOSALS
Organization Approval (DOA). If approved by a runway overrun during a rejected
(h) Inspection and Replacement takeoff or landing, and consequent
the DOA, the approval must include the
(1) For an affected upper cardan pin on an DOA-authorized signature. structural failure and possible injury to
MLG: Before exceeding 96 months since its occupants.
latest installation on an airplane, or within (k) Related Information
DATES: We must receive comments on
12 months after the effective date of this AD, (1) Refer to Mandatory Continuing
whichever occurs later, do a detailed Airworthiness Information (MCAI) EASA this proposed AD by March 7, 2016.
inspection of the upper cardan pin and nut Airworthiness Directive 2015–0079, dated ADDRESSES: You may send comments,
threads for any corrosion, pitting, or thread May 7, 2015, for related information. This using the procedures found in 14 CFR
VerDate Sep<11>2014 15:09 Jan 20, 2016 Jkt 238001 PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 E:\FR\FM\21JAP1.SGM 21JAP1](https://thefederalregister.org/doc/81_FR_3361/page/1.svg)
![3350 Federal Register / Vol. 81, No. 13 / Thursday, January 21, 2016 / Proposed Rules
proposed AD would not have a (d) Subject http://pubs.beechcraft.com. You may view
substantial direct effect on the States, on Air Transport Association (ATA) of this referenced service information at FAA,
the relationship between the national America Code 78, Exhaust. Transport Airplane Directorate, 1601 Lind
Avenue SW., Renton, WA. For information
Government and the States, or on the (e) Unsafe Condition on the availability of this material at the
distribution of power and FAA, call 425–227–1221.
This AD was prompted by reports of
responsibilities among the various inadvertent stowage of the thrust reversers, Issued in Renton, Washington, on January
levels of government. which can result in high forward engine 8, 2016.
For the reasons discussed above, I thrust even though the throttle is Jeffrey E. Duven,
certify this proposed regulation: commanding reverse thrust. We are issuing
this AD to prevent inadvertent stowage of the Manager, Transport Airplane Directorate,
(1) Is not a ‘‘significant regulatory
thrust reversers, which could cause a runway Aircraft Certification Service.
action’’ under Executive Order 12866,
(2) Is not a ‘‘significant rule’’ under overrun during a rejected takeoff or landing, [FR Doc. 2016–00951 Filed 1–20–16; 8:45 am]
and consequent structural failure and BILLING CODE 4910–13–P
the DOT Regulatory Policies and possible injury to occupants.
Procedures (44 FR 11034, February 26,
1979), (f) Compliance
DEPARTMENT OF TRANSPORTATION
(3) Will not affect intrastate aviation Comply with this AD within the
in Alaska, and compliance times specified, unless already
done.
Federal Aviation Administration
(4) Will not have a significant
economic impact, positive or negative, (g) Installation 14 CFR Part 39
on a substantial number of small entities Within 600 flight hours or 12 months after
under the criteria of the Regulatory [Docket No. FAA–2016–0457; Directorate
the effective date of this AD, whichever
Identifier 2015–NM–084–AD]
Flexibility Act. occurs first: Install kits having part numbers
140–9005 and 140–9006, in accordance with RIN 2120–AA64
List of Subjects in 14 CFR Part 39 the Accomplishment Instructions of
Air transportation, Aircraft, Aviation Beechcraft Mandatory Service Bulletin 78– Airworthiness Directives; BAE
safety, Incorporation by reference, 4133, dated May 2015, except as specified in Systems (Operations) Limited
paragraph (h) of this AD. Airplanes
Safety.
(h) Exception to Service Information
The Proposed Amendment AGENCY: Federal Aviation
A note in the Accomplishment Instructions Administration (FAA), DOT.
Accordingly, under the authority of Beechcraft Mandatory Service Bulletin 78–
ACTION: Notice of proposed rulemaking
delegated to me by the Administrator, 4133, dated May 2015, instructs operators to
the FAA proposes to amend 14 CFR part contact Beechcraft Corporation if any (NPRM).
39 as follows: difficulty is encountered in accomplishing
SUMMARY: We propose to supersede
the service bulletin. However, any deviation
from the actions required by paragraph (g) of Airworthiness Directive (AD) 2012–11–
PART 39—AIRWORTHINESS 15, for all BAE Systems (Operations)
DIRECTIVES this AD must be approved as an alternative
method of compliance (AMOC) under Limited Model 4101 airplanes. AD
■ 1. The authority citation for part 39 paragraph (i)(1) of this AD. 2012–11–15 currently requires a one-
continues to read as follows: (i) Alternative Methods of Compliance time detailed inspection for cracks,
(AMOCs) corrosion, and other defects of the rear
Authority: 49 U.S.C. 106(g), 40113, 44701. face of the wing rear spar, and repair if
(1) The Manager, Wichita Aircraft
§ 39.13 [Amended] Certification Office (ACO), FAA, has the necessary. Since we issued AD 2012–
authority to approve AMOCs for this AD, if 11–15, we received new reports of
■ 2. The FAA amends § 39.13 by adding
requested using the procedures found in 14 cracking found in the wing rear spar and
the following new airworthiness
CFR 39.19. In accordance with 14 CFR 39.19, technical analysis results confirmed that
directive (AD): send your request to your principal inspector the crack initiation and propagation are
Beechcraft Corporation (Type Certificate or local Flight Standards District Office, as due to fatigue, with no indication of any
Previously Held by Hawker Beechcraft appropriate. If sending information directly other crack initiation mechanism (e.g.
Corporation; Raytheon Aircraft to the manager of the ACO, send it to the stress corrosion). This proposed AD
Company): Docket No. FAA–2016–0460; attention of the person identified in
Directorate Identifier 2015–NM–078–AD. paragraph (j)(1) of this AD. would require repetitive detailed
(2) Before using any approved AMOC, inspections, and repair if necessary. We
(a) Comments Due Date notify your appropriate principal inspector, are proposing this AD to detect and
We must receive comments by March 7, or lacking a principal inspector, the manager correct cracking in the wing rear spar,
2016. of the local flight standards district office/ which could propagate to a critical
certificate holding district office. length, possibly affecting the structural
(b) Affected ADs
(j) Related Information integrity of the area and resulting in a
None.
(1) For more information about this AD,
fuel tank rupture, with consequent
(c) Applicability damage to the airplane and possible
contact Jeffrey Englert, Aerospace Engineer,
This AD applies to Beechcraft Corporation Mechanical Systems and Propulsion Branch, injury to its occupants.
(type certificate previously held by Hawker ACE–116W, FAA, Wichita Aircraft DATES: We must receive comments on
Beechcraft Corporation; Raytheon Aircraft Certification Office, 1801 Airport Road, this proposed AD by March 7, 2016.
jstallworth on DSK7TPTVN1PROD with PROPOSALS
Company) airplanes, certificated in any Room 100, Dwight D. Eisenhower National ADDRESSES: You may send comments by
category, as identified in paragraphs (c)(1) Airport, Wichita, KS 67209; phone: 316–946–
and (c)(2) of this AD. 4167; fax: 316–946–4107; email: any of the following methods:
(1) Model BAe.125 series 1000A and 1000B jeffrey.englert@faa.gov. • Federal eRulemaking Portal: Go to
airplanes, serial numbers 258151, 258159, (2) For service information identified in http://www.regulations.gov. Follow the
and 259004 through 259042 inclusive. this AD, contact Beechcraft Corporation, instructions for submitting comments.
(2) Model Hawker 1000 airplanes, serial TMDC, P.O. Box 85, Wichita, KS 67201– • Fax: 202–493–2251.
numbers 259003 and 259043 through 259052 0085; telephone 316–676–8238; fax 316–671– • Mail: U.S. Department of
inclusive. 2540; email tmdc@beechcraft.com; Internet Transportation, Docket Operations, M–
VerDate Sep<11>2014 15:09 Jan 20, 2016 Jkt 238001 PO 00000 Frm 00010 Fmt 4702 Sfmt 4702 E:\FR\FM\21JAP1.SGM 21JAP1](https://thefederalregister.org/doc/81_FR_3361/page/3.svg)
Document Created: 2018-02-02 12:33:29
Document Modified: 2018-02-02 12:33:29
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by March 7, 2016. | |
| Contact | Jeffrey Englert, Aerospace Engineer, Mechanical Systems and Propulsion Branch, ACE-116W, FAA, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Dwight D. Eisenhower National Airport, Wichita, KS 67209; phone: 316-946-4167; fax: 316-946-4107; email: [email protected] | |
| FR Citation | 81 FR 3348 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR