83 FR 44455 - 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 170 (August 31, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 170 (August 31, 2018)
| Page Range | 44455-44457 | |
| FR Document | 2018-18885 |
[Federal Register Volume 83, Number 170 (Friday, August 31, 2018)] [Rules and Regulations] [Pages 44455-44457] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-18885] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 31 [Docket No. FAA-2018-0566; Notice No. 31-002-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: Final special conditions. ----------------------------------------------------------------------- SUMMARY: These special conditions are issued for Ultramagic S.A. 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 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 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: These special conditions are effective August 31, 2018. [[Page 44456]] 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: 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 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 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 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. --------------------------------------------------------------------------- Discussion of Comments Notice of proposed special conditions No. 31-18-01-SC for the Ultramagic 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 was published in the Federal Register on June 25, 2018 (83 FR 29472). No comments were received, and the special conditions are adopted as proposed. 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. [[Page 44457]] 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 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 31 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 Special Conditions 0 Accordingly, pursuant to the authority delegated to me by the Administrator, the following special conditions are issued 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 August 23, 2018. Pat Mullen, Manager, Small Airplane Standards Branch, Aircraft Certification Service. [FR Doc. 2018-18885 Filed 8-30-18; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 83, No. 170 / Friday, August 31, 2018 / Rules and Regulations 44455
■ c. Removing the period at the end of ■ a. Removing paragraph (b)(4); (3) A municipal obligation that is
paragraph (c)(2)(vi) and adding ‘‘; or’’ in ■ b. Removing ‘‘; plus’’ at the end of investment grade under 12 CFR part 1
its place; and paragraph (c)(2) and adding in its place as of the calculation date.
■ d. Adding paragraph (c)(3). a period; Dated: August 20, 2018.
The republication and addition read ■ c. Removing paragraphs (c)(3), (f), and
Joseph M. Otting,
as follows: (g)(4);
Comptroller of the Currency.
■ d. Removing ‘‘; plus’’ at the end of
§ 50.20 High-quality liquid asset criteria.
paragraph (h)(2) and adding in its place By order of the Board of Governors of the
* * * * * a period; Federal Reserve System, August 21, 2018.
(c) Level 2B liquid assets. An asset is ■ e. Removing paragraphs (h)(3) and (k); Ann E. Misback,
a level 2B liquid asset if the asset is and Secretary of the Board.
liquid and readily-marketable and is one ■ f. Redesignating paragraphs (g)
of the following types of assets: through (j) as paragraphs (f) through (i), Dated at Washington, DC, on August 22,
* * * * * respectively. 2018.
(3) A municipal obligation that is By order of the Board of Directors.
investment grade under 12 CFR part 1 § 249.22 [Amended] Federal Deposit Insurance Corporation.
as of the calculation date. ■ 8. Amend § 249.22 by removing Valerie Jean Best,
Federal Reserve System paragraph (c) and redesignating Assistant Executive Secretary.
paragraph (d) as paragraph (c). [FR Doc. 2018–18610 Filed 8–30–18; 8:45 am]
PART 249—LIQUIDITY RISK Federal Deposit Insurance Corporation BILLING CODE 4810–33–P; 6210–01–P; 6714–01–P
MEASUREMENT STANDARDS
(REGULATION WW) PART 329—LIQUIDITY RISK
MEASUREMENT STANDARDS DEPARTMENT OF TRANSPORTATION
■ 4. The authority citation for part 249
continues to read as follows: ■ 9. The authority citation for part 329 Federal Aviation Administration
Authority: 12 U.S.C. 248(a), 321–338a, continues to read as follows:
481–486, 1467a(g)(1), 1818, 1828, 1831p–1, Authority: 12 U.S.C. 1815, 1816, 1818, 14 CFR Part 31
1831o–1, 1844(b), 5365, 5366, 5368. 1819, 1828, 1831p–1, 5412.
[Docket No. FAA–2018–0566; Notice No. 31–
■ 5. Amend § 249.3 by removing the ■ 10. Section 329.3 is amended by 002–SC]
definition for ‘‘General obligation’’ and revising the definition for ‘‘Liquid and
adding the definition for ‘‘Municipal readily-marketable’’ and adding the Special Conditions: Ultramagic S.A.,
obligation’’ in alphabetical order to read definition for ‘‘Municipal obligation’’ in Model M–56, M–56C, M–65, M–65C, M–
as follows: alphabetical order to read as follows: 77, M–77C, M–90, M–105, M–120, M–
§ 249.3 Definitions. 130, M–145, M–160, N–180, N–210, N–
§ 329.3 Definitions. 250, N–300, N–355, N–425, S–70, S–90,
* * * * * * * * * * S–105, S–130, S–160, T–150, T–180, T–
Municipal obligation means an
Liquid and readily-marketable has the 210, V–56, V–65, V–77, V–90, and V–
obligation of:
(1) A state or any political subdivision meaning given the term in 12 CFR 105 Balloons; Balloon Passenger
thereof; or 249.3. Basket, Model CV–08, Seat Installation
(2) Any agency or instrumentality of * * * * * AGENCY: Federal Aviation
a state or any political subdivision Municipal obligation means an
Administration (FAA), DOT.
thereof. obligation of:
(1) A state or any political subdivision ACTION: Final special conditions.
* * * * *
thereof; or SUMMARY: These special conditions are
■ 6. Amend § 249.20 by republishing (2) Any agency or instrumentality of
issued for Ultramagic S.A. Models M–
paragraph (c) introductory text, a state or any political subdivision
56, M–56C, M–65, M–65C, M–77, M–
removing the ‘‘or’’ at the end of thereof.
77C, M–90, M–105, M–120, M–130, M–
paragraph (c)(1)(iii), removing * * * * * 145, M–160, N–180, N–210, N–250, N–
paragraph (c)(2), redesignating
■ 11. Section 329.20 is amended by: 300, N–355, N–425, S–70, S–90, S–105,
paragraph (c)(3) as (c)(2), removing the
■ a. Republishing paragraph (c) S–130, S–160, T–150, T–180, T–210, V–
period at the end of newly redesignated
introductory text; 56, V–65, V–77, V–90, and V–105
paragraph (c)(2)(vi) and adding ‘‘; or’’ in
■ b. Removing the ‘‘or’’ at the end of balloons. These balloons will have
its place, and adding a new paragraph
paragraph (c)(1)(iii); novel or unusual design features
(c)(3) to read as follows:
■ c. Removing the period at the end of associated with a standard construction
§ 249.20 High-quality liquid asset criteria. paragraph (c)(2)(vi) and adding ‘‘; or’’ in basket with a singular distribution that
* * * * * its place; and includes four occupant seats and a
(c) Level 2B liquid assets. An asset is ■ d. Adding paragraph (c)(3). lower sidewall. The applicable
a level 2B liquid asset if the asset is The republication and addition read airworthiness regulations do not contain
liquid and readily-marketable and is one as follows: adequate or appropriate safety standards
of the following types of assets: for these design features. These special
§ 329.20 High-quality liquid asset criteria. conditions contain the additional safety
daltland on DSKBBV9HB2PROD with RULES
* * * * *
(3) A municipal obligation that is * * * * * standards the Administrator considers
investment grade under 12 CFR part 1 (c) Level 2B liquid assets. An asset is necessary to establish a level of safety
as of the calculation date. a level 2B liquid asset if the asset is equivalent to that established by the
liquid and readily-marketable and is one existing airworthiness standards.
§ 249.21 [Amended] of the following types of assets: DATES: These special conditions are
■ 7. Amend § 249.21 by: * * * * * effective August 31, 2018.
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Conclusion (2) Sideways 6g flight warning computers (FWCs) is
This action affects only certain novel (3) Downward 6g necessary to address the identified
or unusual design features on the unsafe condition. This AD requires the
d. Seats and Seatbelts
balloon models specified in these replacement or modifications of the two
special conditions. It is not a rule of (1) Each seat and its supporting FWCs. This AD also removes airplanes
general applicability and it affects only structure must be designed for an from the applicability. We are issuing
the applicant who applied to the FAA occupant mass in accordance paragraph this AD to address the unsafe condition
for approval of these features on the (a) of these special conditions and for on these products.
airplane. These special conditions are the maximum load factors DATES: This AD is effective October 5,
identical in intent to the EASA special corresponding to the specified flight and 2018.
conditions, although the formatting has ground load conditions, including the The Director of the Federal Register
been altered to meet these special emergency landing conditions approved the incorporation by reference
condition requirements. prescribed in paragraph (c) of these of a certain publication listed in this AD
special conditions. as of October 5, 2018.
List of Subjects in 14 CFR Part 31 (2) Each seat or berth shall be fitted The Director of the Federal Register
Aircraft, Aviation safety. with an individual approved seat belt or approved the incorporation by reference
The authority citation for these harness. of certain other publications listed in
special conditions is as follows: (3) Seat belts installed on the balloon this AD as of February 13, 2015 (80 FR
must not fail under flight or ground load 4762, January 29, 2015).
Authority: 49 U.S.C. 106(g), 40113, 44701–
44702, 44704. conditions or emergency landing ADDRESSES: For service information
conditions in accordance with identified in this final rule, contact
The Special Conditions paragraph (c) of these special Airbus SAS, Airworthiness Office—
■ Accordingly, pursuant to the authority conditions, taking into account the EAW, Rond-Point Emile Dewoitine No:
delegated to me by the Administrator, geometrical arrangement of the belt 2, 31700 Blagnac Cedex, France;
the following special conditions are attachment and the seat. telephone +33 5 61 93 36 96; fax +33 5
issued as part of the type certification Issued in Kansas City, Missouri, on August 61 93 44 51; email account.airworth-
basis for Ultramagic S.A. Model M–56, 23, 2018. eas@airbus.com; internet http://
M–56C, M–65, M–65C, M–77, M–77C, Pat Mullen, www.airbus.com. You may view this
M–90, M–105, M–120, M–130, M–145, Manager, Small Airplane Standards Branch, referenced service information at the
M–160, N–180, N–210, N–250, N–300, Aircraft Certification Service. FAA, Transport Standards Branch, 2200
N–355, N–425, S–70, S–90, S–105, S– [FR Doc. 2018–18885 Filed 8–30–18; 8:45 am] South 216th St., Des Moines, WA. For
130, S–160, T–150, T–180, T–210, V–56, BILLING CODE 4910–13–P information on the availability of this
V–65, V–77, V–90, and V–105 balloons material at the FAA, call 206–231–3195.
with a basket Model no. CV–08. It is also available on the internet at
DEPARTMENT OF TRANSPORTATION http://www.regulations.gov by searching
1. Hot Air Balloon Crashworthiness
for and locating Docket No. FAA–2018–
Requirements for Seat Installations and Federal Aviation Administration 0169.
Restraints for Seated and Restrained
Occupants 14 CFR Part 39 Examining the AD Docket
a. Occupant Mass You may examine the AD docket on
[Docket No. FAA–2018–0169; Product
For calculation purposes, it should be Identifier 2017–NM–095–AD; Amendment
the internet at http://
assumed the mass of an occupant is at 39–19372; AD 2018–17–18] www.regulations.gov by searching for
least 86 kilograms (190 pounds). and locating Docket No. FAA–2018–
RIN 2120–AA64 0169; or in person at Docket Operations
b. Seats, Safety Belts, and Harnesses between 9 a.m. and 5 p.m., Monday
Factor of Safety Airworthiness Directives; Airbus SAS through Friday, except Federal holidays.
Airplanes The AD docket contains this final rule,
For each seat, safety belt, and harness,
its attachment to the structure must be AGENCY: Federal Aviation the regulatory evaluation, any
shown, by analysis, tests, or both, to be Administration (FAA), Department of comments received, and other
able to withstand the inertia forces Transportation (DOT). information. The address for Docket
prescribed in paragraph (c) of these ACTION: Final rule.
Operations (phone: 800–647–5527) is
special conditions multiplied by a Docket Operations, U.S. Department of
fitting factor of 1.33. SUMMARY: We are superseding Transportation, Docket Operations, M–
Airworthiness Directive (AD) 2015–02– 30, West Building Ground Floor, Room
c. Emergency Landing Conditions— 17, which applied to all Airbus Model W12–140, 1200 New Jersey Avenue SE,
General A330–200, A330–200 Freighter, and Washington, DC 20590.
The balloon—although it may be A330–300 series airplanes. AD 2015– FOR FURTHER INFORMATION CONTACT:
damaged under emergency landing 02–17 required revising the electrical Vladimir Ulyanov, Aerospace Engineer,
conditions—must be designed to give emergency configuration procedure in International Section, Transport
each occupant every reasonable chance the Emergency Procedures section of the Standards Branch, FAA, 2200 South
of avoiding serious injury in a crash airplane flight manual (AFM) to include 216th St., Des Moines, WA 98198;
landing—when seat belts provided for procedures for deploying the ram air telephone and fax 206–231–3229.
daltland on DSKBBV9HB2PROD with RULES
in the design are properly used—and turbine manually to provide sufficient SUPPLEMENTARY INFORMATION:
the occupant is subject to the following hydraulic power and avoid constant
ultimate inertia forces acting relative to speed motor/generator (CSM/G) Discussion
the surrounding structure as well as shedding. Since we issued AD 2015–02– We issued a notice of proposed
independently of each other. 17, we have determined that rulemaking (NPRM) to amend 14 CFR
(1) Forward 6g replacement or modification of the two part 39 to supersede AD 2015–02–17,
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Document Created: 2018-08-31 00:53:02
Document Modified: 2018-08-31 00:53:02
| 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 | Rules and Regulations | |
| Action | Final special conditions. | |
| Dates | These special conditions are effective August 31, 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 44455 | |
| CFR Associated | Aircraft and Aviation Safety |
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