14122 Federal Register / Vol. 82, No. 51 / Friday, March 17, 2017 / Rules and Regulations 

Issued in Renton, Washington, on February 

23, 2017. 

Michael Kaszycki, 

Assistant Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2017–05334 Filed 3–16–17; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 25 

[Docket No. FAA–2014–0078; Special 

Conditions No. 25–543–SC] 

Special Conditions: Embraer S.A. 

Model ERJ–170 Airplanes; Seats With 

Large, Non-Traditional, Non-Metallic 

Panels 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final special conditions; request 

for comments; correction. 

SUMMARY: This document corrects an 

error that appeared in Federal Docket 

no. FAA–2014–0078, Special 

Conditions no. 25–543–SC, which was 

published in the Federal Register on 

March 3, 2014 (79 FR 11679). The error 

is in the type-certificate number 

referenced in the Background and Type 

Certification Basis sections of the 

special conditions. It is being corrected 

herein. 

DATES: The effective date of this 

correction is March 17, 2017 

FOR FURTHER INFORMATION CONTACT: 

Jayson Claar, FAA, Airframe and Cabin 

Safety Branch, ANM–111, Transport 

Airplane Directorate, Aircraft 

Certification Service, 1601 Lind Avenue 

SW., Renton, Washington 98057–3356; 

telephone 425–227–2194; facsimile 

425–227–1149. 

SUPPLEMENTARY INFORMATION: 

Background 

Special Conditions no. 25–543–SC 

was published in the Federal Register 

on March 3, 2014 (79 FR 11679). The 

document issued special conditions 

pertaining to seats with large, nontraditional, non-metallic panels. 

As published, the document 

contained four errors, each referring to 

the type-certificate number for the 

Embraer S.A. Model ERJ–170 airplane. 

Because no other part of the 

regulatory information has been 

changed, the special conditions 

document is not being re-published. 

Correction 

In the Final Special Conditions, 

Request for Comments document [FR 

Doc. 2014–04559 Filed 2–28–14; 8:45 

a.m.] published on March 3, 2014 (79 

FR 11679), make the following 

correction: 

On page 11679, column 3, in the first 

and second paragraphs of the 

Background section; and on page 11680, 

column 1, in the first paragraph of the 

Type Certification Basis section, change 

‘‘A57NM’’ to ‘‘A56NM.’’ 

Issued in Renton, Washington on February 

10, 2017. 

Michael Kaszycki, 

Assistant Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2017–05328 Filed 3–16–17; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 25 

[Docket No. FAA–2016–8247; Special 

Conditions No. 25–652–SC] 

Special Conditions: Aerocon 

Engineering Company, Boeing Model 

777–200 Airplane; Access Hatch 

Installed Between the Cabin and the 

Class C Cargo Compartment To Allow 

In-Flight Access to the Cargo 

Compartment 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final special conditions. 

SUMMARY: These special conditions are 

issued for the Boeing Model 777–200 

airplane. This airplane, as modified by 

Aerocon Engineering Company 

(Aerocon), will have a novel or unusual 

design feature when compared to the 

state of technology envisioned in the 

airworthiness standards for transportcategory airplanes. This design feature 

is an access hatch, installed between the 

cabin and the Class C cargo 

compartment, to allow in-flight access 

to the Class C cargo compartment. 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: Effective April 17, 2017. 

FOR FURTHER INFORMATION CONTACT: John 

Shelden, FAA, Airframe and Cabin 

Safety Branch, ANM–115, Transport 

Airplane Directorate, Aircraft 

Certification Service, 1601 Lind Avenue 

SW., Renton, Washington 98057–3356; 

telephone 425–227–2785; facsimile 

425–227–1320. 

SUPPLEMENTARY INFORMATION: 

Background 

On June 26, 2015, Aerocon applied for 

a supplemental type certificate to install 

an access hatch between the cabin and 

Class C cargo compartment in the 

Boeing Model 777–200 airplane. This 

airplane is a twin-engine, transportcategory airplane with a VIP interior 

configuration. The Model 777–200 has a 

maximum passenger capacity of 440, 

and a maximum takeoff weight of 

535,000 pounds. 

Type Certification Basis 

Under the provisions of Title 14, Code 

of Federal Regulations (14 CFR) 21.101, 

Aerocon must show that the Boeing 

Model 777–200 airplane, as changed, 

continues to meet the applicable 

provisions of the regulations listed in 

Type Certificate No. T00001SE, or the 

applicable regulations in effect on the 

date of application for the change, 

except for earlier amendments as agreed 

upon by the FAA. 

If the Administrator finds that the 

applicable airworthiness regulations 

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

adequate or appropriate safety standards 

for the Boeing Model 777–200 airplane, 

as changed, because of a novel or 

unusual design feature, special 

conditions are prescribed under the 

provisions of § 21.16. 

Special conditions are initially 

applicable to the model for which they 

are issued. Should the applicant apply 

for a supplemental type certificate to 

modify any other model included on the 

same type certificate 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 777–200 

airplane, as modified by Aerocon, must 

comply with the fuel-vent and exhaustemission requirements of 14 CFR part 

34, and the noise-certification 

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 Boeing Model 777–200 airplane, 

as modified by Aerocon, will 

incorporate the following novel or 

unusual design feature: An access hatch 

installed between the cabin and the 

Class C cargo compartment, to allow inmstockstill on DSK3G9T082PROD with RULES