83 FR 29472 - Special Conditions: Ultramagic S.A., Model M-56, M-56C, M-65, M-65C, M-77, M-77C, M-90, M-105, M-120, M-130, M-145, M-160, N-180, N-210, N-250, N-300, N-355, N-425, S-70, S-90, S-105, S-130, S-160, T-150, T-180, T-210, V-56, V-65, V-77, V-90, and V-105 Balloons; Balloon Passenger Basket, Model CV-08, Seat Installation
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 122 (June 25, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 122 (June 25, 2018)
| Page Range | 29472-29474 | |
| FR Document | 2018-13499 |
[Federal Register Volume 83, Number 122 (Monday, June 25, 2018)] [Proposed Rules] [Pages 29472-29474] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-13499] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 31 [Docket No. FAA-2018-0566; Notice No. 31-18-01-SC] Special Conditions: Ultramagic S.A., Model M-56, M-56C, M-65, M- 65C, M-77, M-77C, M-90, M-105, M-120, M-130, M-145, M-160, N-180, N- 210, N-250, N-300, N-355, N-425, S-70, S-90, S-105, S-130, S-160, T- 150, T-180, T-210, V-56, V-65, V-77, V-90, and V-105 Balloons; Balloon Passenger Basket, Model CV-08, Seat Installation AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed special conditions. ----------------------------------------------------------------------- SUMMARY: This action proposes special conditions for Ultramagic S.A. Model M-56, M-56C, M-65, M-65C, M-77, M-77C, M-90, M-105, M-120, M-130, M-145, M-160, N-180, N-210, N-250, N-300, N-355, N-425, S-70, S-90, S- 105, S-130, S-160, T-150, T-180, T-210, V-56, V-65, V-77, V-90, and V- 105 balloons. These balloons will have novel or unusual design features associated with a standard construction basket with a singular distribution that includes four occupant seats and a lower sidewall. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. These proposed special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. DATES: Send your comments on or before August 9, 2018. ADDRESSES: Send comments identified by docket number FAA-2018-0566 using any of the following methods: [squ] Federal eRegulations Portal: Go to http://www.regulations.gov and follow the online instructions for sending your comments electronically. [squ] Mail: Send comments to Docket Operations, M-30, U.S. Department of Transportation (DOT), 1200 New Jersey Avenue SE, Room W12-140, West Building Ground Floor, Washington, DC 20590-0001. [squ] Hand Delivery of Courier: Take comments to Docket Operations in Room W12-140 of the West Building Ground Floor at 1200 New Jersey Avenue SE, Washington, DC, between 9 a.m., and 5 p.m., Monday through Friday, except Federal holidays. [[Page 29473]] [squ] Fax: Fax comments to Docket Operations at 202-493-2251. Privacy: The FAA will post all comments it receives, without change, to http://regulations.gov, including any personal information the commenter provides. Using the search function of the docket website, anyone can find and read the electronic form of all comments received into any FAA docket, including the name of the individual sending the comment (or signing the comment for an association, business, labor union, etc.). DOT's complete Privacy Act Statement can be found in the Federal Register published on April 11, 2000 (65 FR 19477-19478), as well as at http://DocketsInfo.dot.gov. Docket: Background documents or comments received may be read at http://www.regulations.gov at any time. Follow the online instructions for accessing the docket or go to the Docket Operations in Room W12-140 of the West Building Ground Floor at 1200 New Jersey Avenue SE, Washington, DC, between 9 a.m., and 5 p.m., Monday through Friday, except Federal holidays. FOR FURTHER INFORMATION CONTACT: Robert Stegeman, FAA, AIR-691, Policy & Innovation Division, Small Airplane Standards Branch, Aircraft Certification Service, 901 Locust; Kansas City, Missouri 64106; telephone (816) 329-4140; facsimile (816) 329-4090. SUPPLEMENTARY INFORMATION: Comments Invited We invite interested people to take part in this rulemaking by sending written comments, data, or views. The most helpful comments reference a specific portion of the special conditions, explain the reason for any recommended change, and include supporting data. We ask that you send us two copies of written comments. We will consider all comments we receive on or before the closing date for comments. We will consider comments filed late if it is possible to do so without incurring expense or delay. We may change these special conditions based on the comments we receive. Background On August 4, 2016, Ultramagic S.A. (Ultramagic) applied for a change to Type Certificate (TC) No. B02CE \1\ to include new basket Model no. CV-08 for balloon Models M-56, M-56C, M-65, M-65C, M-77, M- 77C, M-90, M-105, M-120, M-130, M-145, M-160, N-180, N-210, N-250, N- 300, N-355, N-425, S-70, S-90, S-105, S-130, S-160, T-150, T-180, T- 210, V-56, V-65, V-77, V-90, and V-105. The CV-08 basket consists of a traditionally constructed basket, but incorporates seats with restraints and trays for all passengers, as well as a lower basket sidewall to offer a panoramic view for passengers. The CV-08 basket will be matched with one of the balloon envelopes associated with the balloon models listed in these special conditions. The volume of hot air, gores, maximum diameter, and total height defines the balloon envelope. --------------------------------------------------------------------------- \1\ See http://rgl.faa.gov/. --------------------------------------------------------------------------- Most balloon baskets accommodate standing passengers. The CV-08 differs by incorporating passenger seats, restraints, and a lower basket sidewall. Due to the lower sidewall and seat configuration, passengers would need to remain seated and restrained with safety belts during flight. This configuration should consider the static strength of the installations, the possible loads in an accident, and the effect on passenger safety. Accident impact should consider safety comparison between a restrained, sitting occupant; and a normal, standing occupant. Safety requirements for balloon-seated occupants are not included in the existing airworthiness regulations. These proposed special conditions evaluate the seat installations and restraints using methods consistent with special conditions issued by the European Aviation Safety Agency (EASA). The EASA special conditions are based upon a German standard for seats in hot air airships. Type Certification Basis Under the provisions of Sec. 21.101, Ultramagic must show that the M-56, M-56C, M-65, M-65C, M-77, M-77C, M-90, M-105, M-120, M-130, M- 145, M-160, N-180, N-210, N-250, N-300, N-355, N-425, S-70, S-90, S- 105, S-130, S-160, T-150, T-180, T-210, V-56, V-65, V-77, V-90, and V- 105 balloon models--coupled with the CV-08 basket--continues to meet the applicable provisions of the regulations incorporated by reference in TC No. B02CE or the applicable regulations in effect on the date of application for the change. The regulations incorporated by reference in the type certificate are commonly referred to as the ``original type certification basis.'' The regulations incorporated by reference in TC No. B02CE are as follows: 14 CFR 21.29 and part 31, effective on January, 1990, as amended by 31-1 through 31-5 inclusive. Equivalent level of Safety findings per provision of 14 CFR 21.21(b)(1): ACE-08-15 of August 1, 2008, Burners, 14 CFR 31.47(d) ACE-08-15A of November 05, 2013, Burners, 14 CFR 31.47(d), for Model S- 70 Special Conditions 31-001-SC applicable to MK-32 model burners. If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 31) do not contain adequate or appropriate safety standards for the balloon models listed in these proposed special conditions because of a novel or unusual design feature, special conditions are prescribed under the provisions of Sec. 21.16. Special conditions are initially applicable to the model(s) for which they are issued. Should the type certificate for that model be amended later to include any other model that incorporates the same or similar novel or unusual design feature, or should any other model already included on the same type certificate be modified to incorporate the same or similar novel or unusual design feature, the FAA would apply these special conditions to the other model under Sec. 21.101. The FAA issues special conditions, as defined in 14 CFR 11.19, in accordance with Sec. 11.38, and they become part of the type- certification basis under Sec. 21.101. Novel or Unusual Design Features The M-56, M-56C, M-65, M-65C, M-77, M-77C, M-90, M-105, M-120, M- 130, M-145, M-160, N-180, N-210, N-250, N-300, N-355, N-425, S-70, S- 90, S-105, S-130, S-160, T-150, T-180, T-210, V-56, V-65, V-77, V-90, and V-105 balloon models coupled with a CV-08 basket will incorporate the following novel or unusual design features: Occupant seats with restraints and a lowered basket side rail. Discussion Neither the FAA's airworthiness standards (14 CFR part 31, amendment 31-5), nor EASA's current Certification Specification (CS) for Hot Air Balloons (CS 31HB, amendment 1), incorporate specific requirements for seat and seat belts. EASA previously published a proposed special condition \2\ (now expired) for seats and seat belts for hot air balloon baskets. EASA based the requirements of its proposed special condition on the German airworthiness requirements for Hot Air Airships LFHLLS,\3\ incorporating hot air balloon basket requirements for seats, seat belts, and the loads in an emergency landing condition, similar to hot air airship [[Page 29474]] requirements. Ultramagic's change application applied the language in the EASA proposed special condition for CS 31HA.14(c), ``Occupant mass,'' CS 31HA.43(d), ``Fitting factor,'' CS 31HA.561(a) and (b)(1), ``Emergency landing conditions--General,'' and CS 31HA.785(a), (c), and (d), ``Seats and seat belts'' to the CV-08 basket. The FAA finds that these standards are appropriate for a seated, restrained occupant. --------------------------------------------------------------------------- \2\ Ref EASA Proposed Special Condition, ``Seats and seat belts for hot air balloons,'' Issue 1, dated October 3, 2014. \3\ LFHLLS (Luftt[uuml]chtigkeitsforderungen f[uuml]r Heissluft- Luftschiffe)--Airworthiness Requirements for Hot Air Ships, issued November 13, 1997, amended March 10, 1998, Germany. --------------------------------------------------------------------------- Applicability As discussed above, these special conditions are applicable to the Model M-56, M-56C, M-65, M-65C, M-77, M-77C, M-90, M-105, M-120, M-130, M-145, M-160, N-180, N-210, N-250, N-300, N-355, N-425, S-70, S-90, S- 105, S-130, S-160, T-150, T-180, T-210, V-56, V-65, V-77, V-90, and V- 105 balloons. Should Ultramagic apply at a later date for a change to the type certificate to include another model incorporating the same novel or unusual design feature, the FAA would apply these special conditions to that model as well. Conclusion This action affects only certain novel or unusual design features on the balloon models specified in these special conditions. It is not a rule of general applicability and it affects only the applicant who applied to the FAA for approval of these features on the airplane. These proposed special conditions are identical in intent to the EASA special conditions, although the formatting has been altered to meet these special condition requirements. List of Subjects in 14 CFR Part 23 Aircraft, Aviation safety. The authority citation for these special conditions is as follows: Authority: 49 U.S.C. 106(g), 40113, 44701-44702, 44704. The Proposed Special Conditions Accordingly, the FAA proposes the following special conditions as part of the type certification basis for Ultramagic S.A. Model M-56, M- 56C, M-65, M-65C, M-77, M-77C, M-90, M-105, M-120, M-130, M-145, M-160, N-180, N-210, N-250, N-300, N-355, N-425, S-70, S-90, S-105, S-130, S- 160, T-150, T-180, T-210, V-56, V-65, V-77, V-90, and V-105 balloons with a basket Model no. CV-08. 1. Hot Air Balloon Crashworthiness Requirements for Seat Installations and Restraints for Seated and Restrained Occupants a. Occupant Mass For calculation purposes, it should be assumed the mass of an occupant is at least 86 kilograms (190 pounds). b. Seats, Safety Belts, and Harnesses Factor of Safety For each seat, safety belt, and harness, its attachment to the structure must be shown, by analysis, tests, or both, to be able to withstand the inertia forces prescribed in paragraph (c) of these special conditions multiplied by a fitting factor of 1.33. c. Emergency Landing Conditions--General The balloon--although it may be damaged under emergency landing conditions--must be designed to give each occupant every reasonable chance of avoiding serious injury in a crash landing--when seat belts provided for in the design are properly used--and the occupant is subject to the following ultimate inertia forces acting relative to the surrounding structure as well as independently of each other. (1) Forward 6g (2) Sideways 6g (3) Downward 6g d. Seats and Seatbelts (1) Each seat and its supporting structure must be designed for an occupant mass in accordance paragraph (a) of these special conditions and for the maximum load factors corresponding to the specified flight and ground load conditions, including the emergency landing conditions prescribed in paragraph (c) of these special conditions. (2) Each seat or berth shall be fitted with an individual approved seat belt or harness. (3) Seat belts installed on the balloon must not fail under flight or ground load conditions or emergency landing conditions in accordance with paragraph (c) of these special conditions, taking into account the geometrical arrangement of the belt attachment and the seat. Issued in Kansas City, Missouri, on June 15, 2018. Pat Mullen, Manager, Small Airplane Standards Branch, Aircraft Certification Service. [FR Doc. 2018-13499 Filed 6-22-18; 8:45 am] BILLING CODE 4910-13-P
![29472 Federal Register / Vol. 83, No. 122 / Monday, June 25, 2018 / Proposed Rules
Phytophthora ramorum inoculum. The infestation by an inspector. The DEPARTMENT OF TRANSPORTATION
method for this determination will be inspection will focus on regulated
specified in the nursery’s compliance plants and other potential sources of Federal Aviation Administration
agreement with APHIS. Phytophthora ramorum inoculum.
(b) Nurseries in quarantined areas 14 CFR Part 31
shipping non-host nursery stock (2) Sampling. Samples must be taken
interstate. Nurseries located in from host plants, soil, standing water, [Docket No. FAA–2018–0566; Notice No. 31–
quarantined areas and that move non- drainage water, water for irrigation, 18–01–SC]
host nursery stock interstate must meet growing media, and any other articles
determined by the inspector to be Special Conditions: Ultramagic S.A.,
the requirements of this paragraph or Model M–56, M–56C, M–65, M–65C, M–
the requirements of paragraph (a) of this possible sources of Phytophthora
ramorum inoculum. The number of 77, M–77C, M–90, M–105, M–120, M–
section. If such nurseries contain any 130, M–145, M–160, N–180, N–210, N–
regulated or restricted articles, the samples taken may vary depending on
250, N–300, N–355, N–425, S–70, S–90,
nursery must meet the requirements of the possible sources of inoculum
S–105, S–130, S–160, T–150, T–180, T–
paragraph (a) of this section. This identified at the nursery, as well as the
210, V–56, V–65, V–77, V–90, and V–
paragraph (b) only applies if there are number of host articles in the nursery. 105 Balloons; Balloon Passenger
no regulated or associated articles or (3) Testing. Samples must be labeled Basket, Model CV–08, Seat Installation
nursery stock at the nursery. Nurseries and sent for testing to a laboratory
that do not meet the requirements of AGENCY: Federal Aviation
approved by APHIS and must be tested
paragraph (a) of this section or this Administration (FAA), DOT.
using a test method approved by APHIS
paragraph (b) are prohibited from ACTION: Notice of proposed special
moving non-host nursery stock in accordance with § 301.92–12.
conditions.
interstate. (4) Negative results; certification. If all
(1) Annual visual inspection. The samples tested in accordance with this SUMMARY: This action proposes special
nursery must be visually inspected section and § 301.92–12 return negative conditions for Ultramagic S.A. Model
annually for symptoms of Phytophthora results for Phytophthora ramorum, an M–56, M–56C, M–65, M–65C, M–77, M–
ramorum. Inspections and inspector may certify that the nursery is 77C, M–90, M–105, M–120, M–130, M–
determinations of freedom from free of Phytophthora ramorum at the 145, M–160, N–180, N–210, N–250, N–
evidence of Phytophthora ramorum time of the inspection. For purposes of 300, N–355, N–425, S–70, S–90, S–105,
infestation must occur at the time when § 301.92–5(b), regulated, restricted, and S–130, S–160, T–150, T–180, T–210, V–
the best expression of symptoms is associated articles at a certified nursery 56, V–65, V–77, V–90, and V–105
anticipated. balloons. These balloons will have
are considered free from Phytophthora
(2) Sampling. All plants showing novel or unusual design features
symptoms of infection with ramorum until the time of the next
inspection. associated with a standard construction
Phytophthora ramorum upon inspection basket with a singular distribution that
will be sampled and tested in (5) Positive results. If any samples includes four occupant seats and a
accordance with § 301.92–12. If tested in accordance with this section lower sidewall. The applicable
symptomatic plants are found upon and § 301.92–12 return positive results airworthiness regulations do not contain
inspection, the following plants must be for Phytophthora ramorum, the nursery adequate or appropriate safety standards
withheld from interstate shipment until may ship lots of regulated, restricted, for these design features. These
testing is completed and the nursery is and associated articles interstate proposed special conditions contain the
found free of evidence of Phytophthora pursuant to § 301.92–5(b) only if the lot additional safety standards the
ramorum in accordance with this is determined to be free from Administrator considers necessary to
paragraph and § 301.92–12: All Phytophthora ramorum inoculum. The establish a level of safety equivalent to
symptomatic plants, any plants located method for this determination will be that established by the existing
in the same lot as the suspect plant, and specified in the nursery’s compliance airworthiness standards.
any plants located within 2 meters of
agreement with APHIS. DATES: Send your comments on or
this lot of plants.
(3) Certification. If all plant samples (Approved by the Office of Management and before August 9, 2018.
tested in accordance with this section Budget under control number 0579–0310) ADDRESSES: Send comments identified
and § 301.92–12 return negative results by docket number FAA–2018–0566
for Phytophthora ramorum, or if an § 301.92–12 [Amended] using any of the following methods:
inspector at the nursery determines that b Federal eRegulations Portal: Go to
■ 11. In § 301.92–12, paragraph (a) http://www.regulations.gov and follow
plants in a nursery exhibit no signs of
infection with Phytophthora ramorum, introductory text is amended by the online instructions for sending your
the inspector may certify that the removing the words ‘‘prescreen plant comments electronically.
nursery free of evidence of samples’’ and adding the words b Mail: Send comments to Docket
Phytophthora ramorum infestation at ‘‘prescreen samples’’ in their place. Operations, M–30, U.S. Department of
the time of inspection. Certification is Done in Washington, DC, this 19th day of Transportation (DOT), 1200 New Jersey
valid for 1 year and must be renewed June 2018. Avenue SE, Room W12–140, West
each year to continue shipping plants Kevin Shea, Building Ground Floor, Washington, DC
amozie on DSK3GDR082PROD with PROPOSALS1
interstate. 20590–0001.
Administrator, Animal and Plant Health
(c) Regulated establishments shipping Inspection Service.
b Hand Delivery of Courier: Take
regulated, restricted, or associated comments to Docket Operations in
[FR Doc. 2018–13560 Filed 6–22–18; 8:45 am]
articles of interstate. (1) Inspections. To Room W12–140 of the West Building
meet the conditions of § 301.92–5(b), the BILLING CODE 3410–34–P Ground Floor at 1200 New Jersey
regulated establishment must be Avenue SE, Washington, DC, between 9
inspected at least twice annually for a.m., and 5 p.m., Monday through
symptoms of Phytophthora ramorum Friday, except Federal holidays.
VerDate Sep<11>2014 16:25 Jun 22, 2018 Jkt 244001 PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 E:\FR\FM\25JNP1.SGM 25JNP1](https://thefederalregister.org/doc/83_FR_29594/page/1.svg)
![29474 Federal Register / Vol. 83, No. 122 / Monday, June 25, 2018 / Proposed Rules
requirements. Ultramagic’s change 1. Hot Air Balloon Crashworthiness DEPARTMENT OF TRANSPORTATION
application applied the language in the Requirements for Seat Installations and
EASA proposed special condition for CS Restraints for Seated and Restrained Federal Aviation Administration
31HA.14(c), ‘‘Occupant mass,’’ CS Occupants
31HA.43(d), ‘‘Fitting factor,’’ CS 14 CFR Part 39
a. Occupant Mass
31HA.561(a) and (b)(1), ‘‘Emergency [Docket No. FAA–2018–0406; Product
landing conditions—General,’’ and CS For calculation purposes, it should be Identifier 2013–NE–30–AD]
31HA.785(a), (c), and (d), ‘‘Seats and assumed the mass of an occupant is at
RIN 2120–AA64
seat belts’’ to the CV–08 basket. The least 86 kilograms (190 pounds).
FAA finds that these standards are b. Seats, Safety Belts, and Harnesses Airworthiness Directives; General
appropriate for a seated, restrained Factor of Safety Electric Company Turbofan Engines
occupant.
For each seat, safety belt, and harness, AGENCY: Federal Aviation
Applicability its attachment to the structure must be Administration (FAA), DOT.
shown, by analysis, tests, or both, to be ACTION: Notice of proposed rulemaking
As discussed above, these special
able to withstand the inertia forces (NPRM).
conditions are applicable to the Model prescribed in paragraph (c) of these
M–56, M–56C, M–65, M–65C, M–77, M– special conditions multiplied by a SUMMARY: We propose to supersede
77C, M–90, M–105, M–120, M–130, M– fitting factor of 1.33. Airworthiness Directive (AD) 2017–07–
145, M–160, N–180, N–210, N–250, N– 04, which applies to General Electric
300, N–355, N–425, S–70, S–90, S–105, c. Emergency Landing Conditions— Company (GE) GE90–110B1 and GE90–
S–130, S–160, T–150, T–180, T–210, V– General 115B turbofan engines with certain
56, V–65, V–77, V–90, and V–105 The balloon—although it may be high-pressure compressor (HPC) rotor
balloons. Should Ultramagic apply at a damaged under emergency landing stage 2–5 spools installed. AD 2017–07–
later date for a change to the type conditions—must be designed to give 04 resulted from reports of cracks in
certificate to include another model each occupant every reasonable chance HPC rotor stage 2–5 spool aft spacer
incorporating the same novel or unusual of avoiding serious injury in a crash arms. Since we issued AD 2017–07–04,
design feature, the FAA would apply landing—when seat belts provided for GE released a new service bulletin (SB)
these special conditions to that model as in the design are properly used—and that increases the number of affected
well. the occupant is subject to the following HPC rotor stage 2–5 spools.
ultimate inertia forces acting relative to Additionally, we learned that we
Conclusion inadvertently omitted certain HPC rotor
the surrounding structure as well as
independently of each other. stage 2–5 spools from the applicability
This action affects only certain novel of AD 2017–07–04. This proposed AD
or unusual design features on the (1) Forward 6g would require removing certain HPC
balloon models specified in these (2) Sideways 6g rotor stage 2–5 spools from service
special conditions. It is not a rule of (3) Downward 6g before reaching the new reduced life
general applicability and it affects only limit and replacing them with parts
the applicant who applied to the FAA d. Seats and Seatbelts eligible for installation. We are
for approval of these features on the (1) Each seat and its supporting proposing this AD to correct the unsafe
airplane. These proposed special structure must be designed for an condition on these products.
conditions are identical in intent to the occupant mass in accordance paragraph DATES: We must receive comments on
EASA special conditions, although the (a) of these special conditions and for this proposed AD by August 9, 2018.
formatting has been altered to meet the maximum load factors ADDRESSES: You may send comments,
these special condition requirements. corresponding to the specified flight and using the procedures found in 14 CFR
List of Subjects in 14 CFR Part 23 ground load conditions, including the 11.43 and 11.45, by any of the following
emergency landing conditions methods:
Aircraft, Aviation safety. prescribed in paragraph (c) of these • Federal eRulemaking Portal: Go to
special conditions. http://www.regulations.gov. Follow the
The authority citation for these instructions for submitting comments.
special conditions is as follows: (2) Each seat or berth shall be fitted
with an individual approved seat belt or • Fax: 202–493–2251.
Authority: 49 U.S.C. 106(g), 40113, 44701– harness. • Mail: U.S. Department of
44702, 44704. Transportation, Docket Operations, M–
(3) Seat belts installed on the balloon
30, West Building Ground Floor, Room
The Proposed Special Conditions must not fail under flight or ground load
W12–140, 1200 New Jersey Avenue SE,
conditions or emergency landing
Accordingly, the FAA proposes the Washington, DC 20590.
conditions in accordance with
following special conditions as part of • Hand Delivery: Deliver to Mail
paragraph (c) of these special
the type certification basis for address above between 9 a.m. and 5
conditions, taking into account the
p.m., Monday through Friday, except
Ultramagic S.A. Model M–56, M–56C, geometrical arrangement of the belt
Federal holidays.
amozie on DSK3GDR082PROD with PROPOSALS1
M–65, M–65C, M–77, M–77C, M–90, M– attachment and the seat.
For service information identified in
105, M–120, M–130, M–145, M–160, N– Issued in Kansas City, Missouri, on June this NPRM, contact General Electric
180, N–210, N–250, N–300, N–355, N– 15, 2018. Company, One Neumann Way, Room
425, S–70, S–90, S–105, S–130, S–160, Pat Mullen, 285, Cincinnati, OH; phone: 513–552–
T–150, T–180, T–210, V–56, V–65, V– Manager, Small Airplane Standards Branch, 3272; email: geae.aoc@ge.com. You may
77, V–90, and V–105 balloons with a Aircraft Certification Service. view this service information at the
basket Model no. CV–08. [FR Doc. 2018–13499 Filed 6–22–18; 8:45 am] FAA, Engine and Propeller Standards
BILLING CODE 4910–13–P Branch, 1200 District Avenue,
VerDate Sep<11>2014 16:25 Jun 22, 2018 Jkt 244001 PO 00000 Frm 00010 Fmt 4702 Sfmt 4702 E:\FR\FM\25JNP1.SGM 25JNP1](https://thefederalregister.org/doc/83_FR_29594/page/3.svg)
Document Created: 2018-06-23 02:29:10
Document Modified: 2018-06-23 02:29:10
| 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 special conditions. | |
| Dates | Send your comments on or before August 9, 2018. | |
| Contact | Robert Stegeman, FAA, AIR-691, Policy & Innovation Division, Small Airplane Standards Branch, Aircraft Certification Service, 901 Locust; Kansas City, Missouri 64106; telephone (816) 329-4140; facsimile (816) 329-4090. | |
| FR Citation | 83 FR 29472 |
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