58586 Federal Register / Vol. 80, No. 189 / Wednesday, September 30, 2015 / Rules and Regulations 

by calling (202) 267–9677. Commenters 

must identify the docket or notice 

number of this rulemaking. 

All documents the FAA considered in 

developing this rule, including 

economic analyses and technical 

reports, may be accessed from the 

Internet through the Federal 

eRulemaking Portal referenced in item 

(1) above. 

List of Subjects 

14 CFR Part 11 

Reporting and recordkeeping 

requirements. 

14 CFR Part 121 

Air carriers, Aircraft, Aviation safety, 

Charter flights, Reporting and 

recordkeeping requirements. 

The Amendment 

In consideration of the foregoing, the 

Federal Aviation Administration 

amends chapter I of title 14, Code of 

Federal Regulations as follows: 

PART 11—GENERAL RULEMAKING 

PROCEDURES 

■ 1. The authority citation for part 11 

continues to read as follows: 

Authority: 49 U.S.C. 106(f), 106(g), 40101, 

40103, 40105, 40109, 40113, 44110, 44502, 

44701–44702, 44711, and 46102. 

■ 2. In § 11.201, in paragraph (b), revise 

the entry to Part 121 to read as follows: 

§ 11.201 Office of Management and Budget 

(OMB) control numbers assigned under the 

Paperwork Reduction Act. 

* * * * * 

(b) * * * 

14 CFR Part or section identified and 

described 

Current OMB control number 

*******

Part 121 ................. 2120–0008, 2120–0028, 2120–0535, 2120–0571, 2120–0600, 2120–0606, 2120–0614, 2120–0616, 2120–0631, 2120– 

0651, 2120–0653, 2120–0691, 2120–0702, 2120–0739, 2120–0760 

* * * * * * * 

PART 121—OPERATING 

REQUIREMENTS: DOMESTIC, FLAG, 

AND SUPPLEMENTAL OPERATIONS 

■ 3. The authority citation for part 121 

is revised to read as follows: 

Authority: 49 U.S.C. 106(f), 106(g), 40103, 

40113, 40119, 41706, 42301 preceding note 

added by Pub. L. 112–95, sec. 412, 126 Stat. 

89, 44101, 44701–44702, 44705, 44709– 

44711, 44713, 44716–44717, 44722, 44729, 

44732; 46105; Pub. L. 111–216, 124 Stat. 

2348 (49 U.S.C. 44701 note); Pub. L. 112–95 

126 Stat 62 (49 U.S.C. 44732 note). 

■ 4. In § 121.311, add paragraph (k) to 

read as follows: 

§ 121.311 Seats, safety belts, and shoulder 

harnesses. 

* * * * * 

(k) Seat dimension disclosure. (1) 

Each air carrier that conducts operations 

under this part and that has a Web site 

must make available on its Web site the 

width of the narrowest and widest 

passenger seats in each class of service 

for each airplane make, model and 

series operated by that air carrier in 

passenger-carrying operations. 

(2) For purposes of paragraph (k)(1) of 

this section, the width of a passenger 

seat means the distance between the 

inside of the armrests for that seat. 

■ 5. In § 121.583, revise paragraph (a) 

introductory text to read as follows: 

§ 121.583 Carriage of persons without 

compliance with the passenger-carrying 

requirements of this part. 

(a) When authorized by the certificate 

holder, the following persons, but no 

others, may be carried aboard an 

airplane without complying with the 

passenger-carrying airplane 

requirements in §§ 121.309(f), 121.310, 

121.391, 121.571, and 121.587; the 

passenger-carrying operation 

requirements in part 117 and 

§§ 121.157(c) and 121.291; the 

requirements pertaining to passengers in 

§§ 121.285, 121.313(f), 121.317, 121.547, 

and 121.573; and the information 

disclosure requirements in § 121.311(k): 

* * * * * 

Issued in Washington, DC, under the 

authority provided by 49 U.S.C. 106(f), 

44701(a), and 49 U.S.C. 42301 preceding note 

added by Public Law 112–95, sec. 412, 126 

Stat. 89, on September 18, 2015. 

Michael P. Huerta, 

Administrator. 

[FR Doc. 2015–24720 Filed 9–29–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 25 

[Docket No. FAA–2015–0309; Special 

Conditions No. 25–594–SC] 

Special Conditions: Boeing Model 747– 

8, Dynamic Test Requirements for 

Single-Occupant, Oblique (SideFacing) Seats With Airbag Devices 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final special conditions; request 

for comments. 

SUMMARY: These special conditions are 

issued for Boeing Model 747–8 

airplanes. This airplane will have novel 

or unusual design features associated 

with oblique-angled, single-occupant 

seats equipped with airbag systems. 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: The effective date of these 

special conditions is September 30, 

2015. We must receive your comments 

by November 16, 2015. 

ADDRESSES: Send comments identified 

by docket number FAA–2015–0309 

using any of the following methods: 

Federal eRegulations Portal: Go to 

http://www.regulations.gov/ and follow 

the online instructions for sending your 

comments electronically. 

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. 

Hand Delivery or 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 

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Federal Register / Vol. 80, No. 189 / Wednesday, September 30, 2015 / Rules and Regulations 58587 

a.m. and 5 p.m., Monday through 

Friday, except Federal holidays. 

Fax: Fax comments to Docket 

Operations at 202–493–2251. 

Privacy: The FAA will post all 

comments it receives, without change, 

to http://www.regulations.gov/, 

including any personal information the 

commenter provides. Using the search 

function of the docket Web site, 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 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: John 

Shelden, Airframe and Cabin Safety, 

ANM–115, Transport Airplane 

Directorate, Aircraft Certification 

Service, 1601 Lind Avenue SW., 

Renton, Washington 98057–3356; 

telephone 425–227–2785; facsimile 

425–227–1149. 

SUPPLEMENTARY INFORMATION: The FAA 

has determined that notice of, and 

opportunity for, prior public comment 

on these special conditions are 

impracticable because these procedures 

would significantly delay issuance of 

the design approval and thus delivery of 

the affected airplane. 

In addition, the substance of these 

special conditions has been subject to 

the public-comment process in several 

prior instances with no substantive 

comments received. The FAA therefore 

finds that good cause exists for making 

these special conditions effective upon 

issuance. 

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 will consider all comments we 

receive by the closing date for 

comments. We may change these special 

conditions based on the comments we 

receive. 

Background 

On February 3, 2014, the Boeing 

Company applied for an amendment to 

Type Certificate no. A20WE to allow 

installation of single-occupant, obliqueangled (side-facing) seats with airbag 

devices in Boeing Model 747–8 

airplanes. 

Boeing requested special conditions 

to allow installation of oblique businessclass passenger seats in the Boeing 

Model 747–8 airplane. The seating 

configuration Boeing proposes in 

Certification Plan no. 15090, 

‘‘Installation of Business Class Zodiac 

Seats and Furniture for 747–8 TRX 

RC076,’’ consists of Zodiac Cirrus III 

model side-facing, pod-style, businessclass seats (with surrounding shells and 

front-row furniture) installed at an angle 

of up to 30 degrees to the airplane 

longitudinal centerline. These seats will 

include inflatable restraint (airbag) 

systems for occupant restraint and 

injury protection. 

The Model 747–8 airplane, a 

derivative of the Model 747–400 

airplane, is a bi-level, wide-body 

airplane powered by four wing-mounted 

General Electric GEnx-2B engines. The 

airplane will have a maximum seating 

capacity of 605 passengers and two crew 

members, and a maximum takeoff 

weight of 987,000 pounds. 

Type Certification Basis 

Under the provisions of Title 14, Code 

of Federal Regulations (14 CFR) 21.101, 

Boeing must show that the Model 747– 

8 airplane meets the applicable 

provisions of the regulations listed in 

Type Certificate no. A20WE, or the 

applicable regulations in effect on the 

date of application for the change, 

except for earlier amendments as agreed 

upon by the FAA. The regulations listed 

in the type certificate are commonly 

referred to as the ‘‘original type 

certification basis.’’ The regulations 

listed in Type Certificate no. A20WE are 

as follows: 

14 CFR part 25, Amendments 25–1 

through 25–120, with exceptions 

permitted by § 21.101. In addition, the 

certification basis includes certain 

special conditions, exemptions, or later 

amended sections of the applicable part 

that are not relevant to these special 

conditions. 

If the Administrator finds that the 

applicable airworthiness regulations 

(i.e., 14 CFR part 25) do not contain 

adequate or appropriate safety standards 

for Boeing Model 747–8 airplanes 

because of a novel or unusual design 

feature, special conditions are 

prescribed under § 21.16. 

Special conditions are initially 

applicable to the model for which they 

are issued. Should the type certificate 

for that model be amended later to 

include any other model that 

incorporates the same novel or unusual 

design feature, or should any other 

model already included on the same 

type certificate be modified to 

incorporate the same novel or unusual 

design feature, these special conditions 

would also apply to the other model 

under § 21.101. 

In addition to the applicable 

airworthiness regulations and special 

conditions, the Boeing Model 747–8 

airplane must comply with the fuel-vent 

and exhaust-emission requirements of 

14 CFR part 34, and the noisecertification requirements of 14 CFR 

part 36. 

The FAA issues special conditions as 

defined in 14 CFR 11.19, in accordance 

with § 11.38, and they become part of 

the type certification basis under 

§ 21.101. 

Novel or Unusual Design Features 

The business-class seating 

configuration Boeing proposes is novel 

or unusual due to the seat installation 

at 30 degrees to the airplane centerline, 

the airbag-system installation, and the 

seat/occupant interface with the 

surrounding furniture that introduces 

occupant alignment and loading 

concerns. The proposed business-class 

seating configuration also is beyond the 

limits of current acceptable equivalentlevel-of-safety findings. 

Ongoing research is progressing to 

establish acceptable limits. Until those 

limits become available, the FAA 

proposes a set of interim limits based on 

the current literature available, current 

National Highway Traffic Safety 

Administration (NHTSA) regulations, 

and preliminary test data from the 

research program. 

The existing regulations do not 

provide adequate or appropriate safety 

standards for occupants of obliqueangled seats with airbag systems. To 

provide a level of safety that is 

equivalent to that afforded occupants of 

forward- and aft-facing seats, additional 

airworthiness standards, in the form of 

special conditions, are necessary. These 

special conditions supplement part 25 

and, more specifically, supplement 

§§ 25.562 and 25.785. The requirements 

contained in these special conditions 

consist of both test conditions and 

injury pass/fail criteria. 

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58588 Federal Register / Vol. 80, No. 189 / Wednesday, September 30, 2015 / Rules and Regulations 

Discussion 

Amendment 25–15 to part 25, dated 

October 24, 1967, introduced the subject 

of side-facing seats, and a requirement 

that each occupant in a side-facing seat 

must be protected from head injury by 

a safety belt and a cushioned rest that 

will support the arms, shoulders, head, 

and spine. 

Subsequently, Amendment 25–20, 

dated April 23, 1969, clarified the 

definition of side-facing seats to require 

that each occupant of a seat, positioned 

at more than an 18-degree angle to the 

vertical plane of the airplane 

longitudinal centerline, must be 

protected from head injury by a safety 

belt and an energy-absorbing rest that 

will support the arms, shoulders, head, 

and spine; or by a safety belt and 

shoulder harness that will prevent the 

head from contacting any injurious 

object. The FAA concluded that an 18- 

degree angle would provide an adequate 

level of safety based on tests that were 

performed at that time, and thus 

adopted that standard. 

Part 25 was amended June 16, 1988, 

by Amendment 25–64, to revise the 

emergency-landing conditions that must 

be considered in the design of the 

airplane. Amendment 25–64 revised the 

static-load conditions in 14 CFR 25.561, 

and added the new § 25.562 that 

requires dynamic testing for all seats 

approved for occupancy during takeoff 

and landing. The intent of Amendment 

25–64 is to provide an improved level 

of safety for occupants on transportcategory airplanes. Because most seating 

is forward-facing on transport-category 

airplanes, the pass/fail criteria 

developed in Amendment 25–64 

focused primarily on these seats. As a 

result, the FAA issued Policy 

Memorandums ANM–03–115–30 and 

PS–ANM–100–2000–00123 to provide 

the additional guidance necessary to 

demonstrate the level of safety required 

by the regulations for side-facing seats. 

To reflect current research findings, 

the FAA developed a methodology to 

address all fully side-facing seats (i.e., 

seats positioned in the airplane with the 

occupant facing 90 degrees to the 

vertical plane of the airplane 

centerline), and has documented those 

requirements in a set of new special 

conditions. The FAA issued Policy 

Statement PS–ANM–25–03–R1 to define 

revised injury criteria associated with 

neck and leg injuries. 

The proposed Model 747–8, a 

Transaero Airlines business-class seat 

installation, is novel such that the 

current Model 747–8 airplane 

certification basis does not adequately 

address protection of the occupant’s 

neck and spine for seat configurations 

that are positioned at an angle greater 

than 18 degrees from the airplane 

centerline. Therefore, The Boeing 

Company’s proposed configuration will 

require new special conditions. 

These special conditions will provide 

head injury criteria, neck injury criteria, 

spine injury criteria, and body-to-wall 

contact criteria. They contain the 

additional safety standards that the 

Administrator considers necessary to 

establish a level of safety equivalent to 

that established by the existing 

airworthiness standards. 

Applicability 

These special conditions are 

applicable to the Boeing Model 747–8 

airplanes configured with the businessclass seating defined in Boeing 

Certification Plan. Should Boeing apply 

at a later date for a change to the type 

certificates to include another model 

incorporating the same novel or unusual 

design feature, or should any other 

model already included on the same 

type certificate be modified to 

incorporate the same novel or unusual 

design feature, these special conditions 

would apply to the other model as well. 

Conclusion 

This action affects only certain novel 

or unusual design features on one model 

airplane. It is not a rule of general 

applicability. 

The substance of these special 

conditions has been subjected to the 

notice and comment period in several 

prior instances and has been derived 

without substantive change from those 

previously issued. It is unlikely that 

prior public comment would result in a 

significant change from the substance 

contained herein. Therefore, because a 

delay would significantly affect the 

certification of the airplane, which is 

imminent, the FAA has determined that 

prior public notice and comment are 

unnecessary and impracticable, and 

good cause exists for adopting these 

special conditions upon publication in 

the Federal Register. The FAA is 

requesting comments to allow interested 

persons to submit views that may not 

have been submitted in response to the 

prior opportunities for comment 

described above. 

List of Subjects in 14 CFR Part 25 

Aircraft, Aviation safety, Reporting 

and recordkeeping requirements. 

The authority citation for these 

special conditions is as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701, 

44702, 44704. 

The Special Conditions 

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 the Boeing Model 

747–8 airplane. 

Side-Facing Seats Special Conditions 

In addition to the requirements of 

§ 25.562: 

1. Head Injury Criteria. 

Compliance with § 25.562(c)(5) is 

required, except that, if the 

anthropomorphic test device (ATD) has 

no apparent contact with the seat/

structure but has contact with an airbag, 

a head-injury criterion (HIC) unlimited 

score in excess of 1000 is acceptable, 

provided the HIC15 score (calculated in 

accordance with 49 CFR 571.208) for 

that contact is less than 700. 

2. Body-to-Wall/Furnishing Contact. 

If a seat is installed aft of structure 

(e.g., an interior wall or furnishing) that 

does not provide a homogenous contact 

surface for the expected range of 

occupants and yaw angles, then 

additional analysis and/or test(s) may be 

required to demonstrate that the injury 

criteria are met for the area that an 

occupant could contact. For example, if 

different yaw angles could result in 

different airbag performance, then 

additional analysis or separate test(s) 

may be necessary to evaluate 

performance. 

3. Neck Injury Criteria. 

The seating system must protect the 

occupant from experiencing serious 

neck injury. The assessment of neck 

injury must be conducted with the 

airbag device activated, unless there is 

reason to also consider that the neckinjury potential would be higher for 

impacts below the airbag-device 

deployment threshold. 

a. The Nij (calculated in accordance 

with 49 CFR 571.208) must be below 

1.0, where Nij =Fz/Fzc + My/Myc, and Nij

critical values are: 

i. Fzc = 1530 lb for tension 

ii. Fzc = 1385 lb for compression 

iii. Myc = 229 lb-ft in flexion 

iv. Myc = 100 lb-ft in extension 

b. In addition, peak Fz must be below 

937 lb in tension and 899 lb in 

compression. 

c. Rotation of the head about its 

vertical axis, relative to the torso, is 

limited to 105 degrees in either 

direction from forward-facing. 

d. The neck must not impact any 

surface that would produce 

concentrated loading on the neck. 

4. Spine and Torso Injury Criteria 

a. The shoulders must remain aligned 

with the hips throughout the impact 

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Federal Register / Vol. 80, No. 189 / Wednesday, September 30, 2015 / Rules and Regulations 58589 

sequence, or support for the upper torso 

must be provided to prevent forward or 

lateral flailing beyond 45 degrees from 

the vertical during significant spinal 

loading. Alternatively, the lumbar spine 

tension (Fz) cannot exceed 1200 lb. 

b. Significant concentrated loading on 

the occupant’s spine, in the area 

between the pelvis and shoulders 

during impact, including rebound, is 

not acceptable. During this type of 

contact, the interval for any rearward 

(X-direction) acceleration exceeding 20g 

must be less than 3 milliseconds as 

measured by the thoracic 

instrumentation specified in 49 CFR 

part 572, subpart E, filtered in 

accordance with SAE International 

(SAE) J211–1. 

c. Occupant must not interact with 

the armrest or other seat components in 

any manner significantly different than 

would be expected for a forward-facing 

seat installation. 

5. Longitudinal test(s), conducted to 

measure the injury criteria above, must 

be performed with the FAA Hybrid III 

ATD, as described in SAE 1999–01– 

1609. The test(s) must be conducted 

with an undeformed floor, at the mostcritical yaw case(s) for injury, and with 

all lateral structural supports (armrests/ 

walls) installed. 

Note: Boeing must demonstrate that the 

installation of seats via plinths or pallets 

meets all applicable requirements. 

Compliance with the guidance contained in 

FAA Policy Memorandum PS–ANM–100– 

2000–00123, dated February 2, 2000, titled 

‘‘Guidance for Demonstrating Compliance 

with Seat Dynamic Testing for Plinths and 

Pallets,’’ is acceptable to the FAA. 

Inflatable Airbag Systems Special 

Conditions 

If inflatable airbag systems are 

installed on single-place side-facing 

seats, the airbag systems must meet 

Special Conditions no. 25–589–SC. 

Issued in Renton, Washington, on 

September 1, 2015. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2015–24724 Filed 9–29–15; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 25 

[Docket No. FAA–2015–2884; Special 

Conditions No. 25–595–SC] 

Special Conditions: Embraer Model 

EMB–545 Airplanes; Seats With 

Inflatable Lap Belts 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final special conditions; request 

for comments. 

SUMMARY: These special conditions are 

issued for Embraer Model EMB–545 

airplanes. These airplanes will have a 

novel or unusual design feature 

associated with seats with inflatable lap 

belts. The applicable airworthiness 

regulations do not contain adequate or 

appropriate safety standards for this 

design feature. These special conditions 

contain the additional safety standards 

that the Administrator considers 

necessary to establish a level of safety 

equivalent to that established by the 

existing airworthiness standards. 

DATES: The effective date of these 

special conditions is September 30, 

2015. We must receive your comments 

by November 16, 2015. 

ADDRESSES: Send comments identified 

by docket number FAA–2015–2884 

using any of the following methods: 

• Federal eRegulations Portal: Go to 

http://www.regulations.gov/and follow 

the online instructions for sending your 

comments electronically. 

• 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. 

• Hand Delivery or 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. 

• Fax: Fax comments to Docket 

Operations at 202–493–2251. 

Privacy: The FAA will post all 

comments it receives, without change, 

to http://www.regulations.gov/, 

including any personal information the 

commenter provides. Using the search 

function of the docket Web site, 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 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: 

Jayson Claar, FAA, Airframe and Cabin 

Safety Branch, ANM–115, Transport 

Airplane Directorate, Aircraft 

Certification Service, 1601 Lind Avenue 

SW., Renton, Washington, 98057–3356; 

telephone (425) 227–2194, facsimile 

(425) 227–1232. 

SUPPLEMENTARY INFORMATION: The FAA 

has determined that notice of, and 

opportunity for, prior public comment 

on these special conditions are 

impracticable because these procedures 

would significantly delay issuance of 

the design approval and thus delivery of 

the affected airplane. 

In addition, the substance of these 

special conditions has been subject to 

the public-comment process in several 

prior instances with no substantive 

comments received. The FAA therefore 

finds that good cause exists for making 

these special conditions effective upon 

issuance. 

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 will consider all comments we 

receive by the closing date for 

comments. We may change these special 

conditions based on the comments we 

receive. 

Background 

On October 14, 2010, Embraer S.A. 

applied for an amendment to Type 

Certificate No. TC00062IB to include the 

new Embraer Model EMB–545 airplane. 

These special conditions allow 

installation of inflatable lap belts for 

head-injury protection on certain seats 

in Embraer Model EMB–545 airplanes. 

The Embraer Model EMB–545 

airplane is a derivative of the Model 

EMB–550 airplane currently approved 

under Type Certificate No. TC00062IB. 

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