14794 Federal Register / Vol. 76, No. 53 / Friday, March 18, 2011 / Rules and Regulations 

board of directors, and noted in the 

minutes. 

(2) Customer identification program. 

Each bank is subject to the requirements 

of 31 U.S.C. 5318(l) and the 

implementing regulation jointly 

promulgated by the FDIC and the 

Department of the Treasury at 31 CFR 

1020.220. 

PART 334—FAIR CREDIT REPORTING 

■ 3. The authority citation for part 334 

continues to read: 

Authority: 12 U.S.C. 1818, 1819 (Tenth) 

and 1831 p–1; 15 U.S.C. 1681a, 1681b, 1681c, 

1681m, 1681s, 1681s–3, 1681t, 1681w, 6801 

and 6805, Pub. L. 108–159, 117 Stat. 1952. 

■ 4. In § 334.82, revise paragraph 

(c)(2)(i)(A) to read as follows: 

§ 334.82 Duties of users regarding address 

descrepancies. 

* * * * * 

(c) * * * 

(2) * * * 

(i) * * * 

(A) Obtains and uses to verify the 

consumer’s identity in accordance with 

the requirements of the Customer 

Identification Program (CIP) rules 

implementing 31 U.S.C. 5318(l) (31 CFR 

1020.220); 

* * * * * 

■ 5. In Appendix J to Part 334, revise 

Section III, paragraph (a) to read as 

follows: 

Appendix J to Part 334—Interagency 

Guidelines on Identity Theft Detection, 

Prevention, and Mitigation 

* * * * * 

III. Detecting Red Flags 

* * * * * 

(a) Obtaining identifying information 

about, and verifying the identity of, a person 

opening a covered account, for example, 

using the policies and procedures regarding 

identification and verification set forth in the 

Customer Identification Program rules 

implementing 31 U.S.C. 5318(l) (31 CFR 

1020.220); and 

* * * * * 

Dated at Washington, DC, this 15th day of 

March 2011. 

By order of the Board of Directors. 

Federal Deposit Insurance Corporation. 

Robert E. Feldman, 

Executive Secretary. 

[FR Doc. 2011–6460 Filed 3–17–11; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 25 

[Docket No. NM436; Special Conditions No. 

25–421–SC] 

Special Conditions: Boeing Model 

747–8 Airplanes, Systems and Data 

Networks Security—Isolation or 

Protection From Unauthorized 

Passenger Domain Systems Access 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final special conditions. 

SUMMARY: These special conditions are 

issued for Boeing Model 747–8 

airplanes. This airplane will have novel 

or unusual design features associated 

with connectivity of the passenger 

domain computer systems to the 

airplane critical systems and data 

networks. The applicable airworthiness 

regulations do not contain adequate or 

appropriate safety standards for these 

design features. 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 Date: April 18, 2011 

FOR FURTHER INFORMATION CONTACT: Will 

Struck, FAA, Airplane and Flight Crew 

Interface Branch, ANM–111, Transport 

Airplane Directorate, 1601 Lind 

Avenue, SW., Renton, Washington 

98057–3356; telephone (425) 227–2764; 

facsimile (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Background 

On November 4, 2005, The Boeing 

Company, P.O. Box 3707, Seattle, WA 

98124, applied for an amendment to 

Type Certificate Number A20WE to 

include the new Model 747–8 passenger 

airplane. The Model 747–8 is a 

derivative of the 747–400. The Model 

747–8 is a four-engine jet transport 

airplane that will have a maximum 

takeoff weight of 970,000 pounds and 

new General Electric GEnx-2B67 

engines. The Model 747–8 will have two 

flight crew and the capacity to carry 605 

passengers. 

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 (hereafter referred to as the 747– 

8) continues to meet the applicable 

provisions of 14 CFR part 25, as 

amended by Amendments 25–1 through 

25–117, except for §§ 25.809 and 25.812, 

which will remain at Amendment 

25–115. These regulations will be 

incorporated into Type Certificate No. 

A20WE after type certification approval 

of the 747–8. 

If the Administrator finds that the 

applicable airworthiness regulations 

(i.e., part 25) do not contain adequate or 

appropriate safety standards for the 

747–8 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 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, the special conditions 

would also apply to the other model 

under § 21.101. 

In addition to the applicable 

airworthiness regulations and special 

conditions, the 747–8 must comply with 

the fuel vent and exhaust emission 

requirements of 14 CFR part 34 and the 

noise certification requirements of 14 

CFR part 36. 

Special conditions, as defined in 

§ 11.19, are issued under § 11.38, and 

become part of the type certification 

basis under § 21.101. 

Novel or Unusual Design Features 

The Boeing Model 747–8 airplane will 

incorporate the following novel or 

unusual design features: Digital systems 

architecture composed of several 

connected networks. The network 

architecture would be used for a diverse 

set of functions, including: 

1. Flight-safety related control, 

communication, and navigation systems 

(Aircraft Control Domain), 

2. Airline business and administrative 

support (Airline Information Domain), 

3. Passenger information and 

entertainment systems (Passenger 

Entertainment Domain), and 

4. The capability to allow access to or 

by external network sources. 

Discussion of Comments 

Notice of proposed special conditions 

No. 25–10–01–SC for the Boeing Model 

747–8 airplane was published in the 

Federal Register on December 9, 2010 

(75 FR 76647). No comments were 

received and the special conditions are 

adopted as proposed. 

Applicability 

As discussed above, these special 

conditions are applicable to Boeing 

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Federal Register / Vol. 76, No. 53 / Friday, March 18, 2011 / Rules and Regulations 14795 

Model 747–8 airplanes. Should Boeing 

apply at a later date for a change to the 

type certificate to include another 

model incorporating the same novel or 

unusual design features, the special 

conditions would apply to that model as 

well. 

Conclusion 

This action affects only certain novel 

or unusual design features of the Boeing 

Model 747–8 airplane. It is not a rule of 

general applicability. 

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. 

The design must prevent all inadvertent or 

malicious changes to, and all adverse impacts 

upon, all systems, networks, hardware, 

software, and data in the Aircraft Control 

Domain and in the Airline Information 

Domain from all points within the Passenger 

Information and Entertainment Domain. 

Issued in Renton, Washington, on March 9, 

2011. 

Ali Bahrami, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2011–6323 Filed 3–17–11; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 25 

[Docket No. NM437; Special Conditions No. 

25–422–SC] 

Special Conditions: Gulfstream Model 

GVI Airplane; Electronic Flight Control 

System Mode Annunciation. 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final special conditions. 

SUMMARY: These special conditions are 

issued for the Gulfstream GVI airplane. 

This airplane will have novel or 

unusual design features when compared 

to the state of technology envisioned in 

the airworthiness standards for 

transport category airplanes. These 

design features include an electronic 

flight control system. The applicable 

airworthiness regulations do not contain 

adequate or appropriate safety standards 

for these design features. 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 Date: April 18, 2011. 

FOR FURTHER INFORMATION CONTACT: Joe 

Jacobsen, FAA, Airplane and Flight 

Crew Interface Branch, ANM–111, 

Transport Standards Staff, Transport 

Airplane Directorate, Aircraft 

Certification Service, 1601 Lind 

Avenue, SW., Renton, Washington 

98057–3356; telephone (425) 227–2011; 

facsimile (425) 227–1320. 

SUPPLEMENTARY INFORMATION: 

Background 

On March 29, 2005, Gulfstream 

Aerospace Corporation (hereafter 

referred to as ‘‘Gulfstream’’) applied for 

an FAA type certificate for its new 

Gulfstream Model GVI passenger 

airplane. Gulfstream later applied for, 

and was granted, an extension of time 

for the type certificate, which changed 

the effective application date to 

September 28, 2006. The Gulfstream 

Model GVI airplane will be an all-new, 

two-engine jet transport airplane with 

an executive cabin interior. The 

maximum takeoff weight will be 99,600 

pounds, with a maximum passenger 

count of 19 passengers. 

Type Certification Basis 

Under provisions of Title 14 Code of 

Federal Regulations (14 CFR) 21.17, 

Gulfstream must show that the 

Gulfstream Model GVI airplane 

(hereafter referred to as ‘‘the GVI’’) meets 

the applicable provisions of 14 CFR part 

25, as amended by Amendments 25–1 

through 25–119, 25–122 and 25–124. 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 GVI 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 type certificate 

for that model be amended later to 

include any other model that 

incorporates the same novel or unusual 

design features, the special conditions 

would also apply to the other model 

under the provisions of § 21.101. 

In addition to complying with the 

applicable airworthiness regulations 

and special conditions, the GVI must 

comply with the fuel vent and exhaust 

emission requirements of 14 CFR part 

34 and the noise certification 

requirements of 14 CFR part 36. The 

FAA must also issue a finding of 

regulatory adequacy pursuant to section 

611 of Public Law 92–574, the ‘‘Noise 

Control Act of 1972.’’ 

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 

§ 21.17(a)(2). 

Novel or Unusual Design Features 

The GVI will have a fly-by-wire 

electronic flight control system. This 

system provides an electronic interface 

between the pilot’s flight controls and 

the flight control surfaces for both 

normal and failure states, and it 

generates the actual surface commands 

that provide for stability augmentation 

and control about all three airplane 

axes. Because electronic flight control 

system technology has outpaced 

existing regulations (primarily §§ 25.671 

and 25.672), a special condition is 

needed to ensure appropriate mode 

recognition by the flight crew for events 

which significantly change the 

operating mode of the electronic flight 

control system. 

Discussion of Comments 

Notice of proposed special conditions 

No. 25–10–02–SC for Gulfstream GVI 

airplanes was published in the Federal 

Register on December 13, 2010 (75 FR 

77569). Only one comment was 

received. 

Clarification of Conditions That Should 

Be Annunciated 

The commenter, Gulfstream, 

requested that the special conditions be 

revised to clarify the conditions in 

which the mode annunciation should 

occur. Gulfstream suggested that 

additional annunciation should not be 

required when transitioning from one 

normal operation mode to another in 

response to flight crew actions, such as 

extending flaps or landing gear. 

We do not agree with the commenter’s 

recommendation. The current verbiage 

clearly states that the mode 

annunciation is only required when 

‘‘normal handling or operational 

characteristics’’ of the airplane are 

significantly changed or degraded. In 

the scenario that Gulfstream refers to, 

there would be no change to the ‘‘normal 

handling or operational characteristics.’’ 

Therefore, no annunciation would be 

required. No changes were made as a 

result of this comment and the special 

conditions are adopted as proposed. 

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