This section of the FEDERAL REGISTER

contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

33359 

Vol. 81, No. 102 

Thursday, May 26, 2016 

DEPARTMENT OF AGRICULTURE 

Agricultural Marketing Service 

7 CFR Part 948 

Irish Potatoes Grown in Colorado 

CFR Correction 

In Title 7 of the Code of Federal 

Regulations, Parts 900 to 999, revised as 

of January 1, 2016, on page 338, 

§ 948.215 is reinstated to read as 

follows: 

§ 948.215 Assessment rate. 

On or after July 1, 2005, an 

assessment rate of $0.02 per 

hundredweight is established for 

Colorado Area No. 3 potatoes. 

[70 FR 36816, June 27, 2005] 

[FR Doc. 2016–12582 Filed 5–25–16; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–7528; Directorate 

Identifier 2015–NM–004–AD; Amendment 

39–18524; AD 2016–10–13] 

RIN 2120–AA64 

Airworthiness Directives; Airbus 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all 

Airbus Model A300 B4–600, B4–600R, 

and F4–600R series airplanes, and 

Model A300 C4–605R Variant F 

airplanes (collectively called Model 

A300–600 series airplanes); and Model 

A310 series airplanes. This AD was 

prompted by reports of premature aging 

of certain passenger chemical oxygen 

generators that resulted in the 

generators failing to activate. This AD 

requires an inspection to determine if 

certain passenger chemical oxygen 

generators are installed and replacement 

of affected passenger chemical oxygen 

generators. We are issuing this AD to 

prevent failure of the passenger 

chemical oxygen generator to activate 

and consequently not deliver oxygen 

during an emergency, possibly resulting 

in injury to airplane occupants. 

DATES: This AD is effective June 30, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of June 30, 2016. 

ADDRESSES: For Airbus service 

information identified in this final rule, 

contact Airbus SAS, Airworthiness 

Office—EAW, 1 Rond Point Maurice 

Bellonte, 31707 Blagnac Cedex, France; 

telephone: +33 5 61 93 36 96; fax: +33 

5 61 93 44 51; email: account.airwortheas@airbus.com; Internet http://

www.airbus.com. For B/E Aerospace 

service information identified in this 

final rule, contact B/E Aerospace Inc., 

10800 Pflumm Road, Lenexa, KS 66215; 

telephone: 913–338–9800; fax: 913– 

469–8419; Internet http://

beaerospace.com/home/globalsupport. 

You may view this referenced service 

information at the FAA, Transport 

Airplane Directorate, 1601 Lind Avenue 

SW., Renton, WA. For information on 

the availability of this material at the 

FAA, call 425–227–1221. It is also 

available on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

7528. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

7528; or in person at the Docket 

Management Facility between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The AD docket 

contains this AD, the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Office (telephone 800–647– 

5527) is Docket Management Facility, 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue SE., 

Washington, DC 20590. 

FOR FURTHER INFORMATION CONTACT: Dan 

Rodina, Aerospace Engineer, 

International Branch, ANM–116 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; telephone: 425–227–2125; 

fax: 425–227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to all Airbus Model A300 B4–600, 

B4–600R, and F4–600R series airplanes, 

and Model A300 C4–605R Variant F 

airplanes (collectively called Model 

A300–600 series airplanes); and Model 

A310 series airplanes. The NPRM 

published in the Federal Register on 

December 23, 2015 (80 FR 79745) (‘‘the 

NPRM’’). The NPRM was prompted by 

reports of premature aging of certain 

passenger chemical oxygen generators 

that resulted in the generators failing to 

activate. The NPRM proposed to require 

an inspection to determine if certain 

passenger chemical oxygen generators 

are installed and replacement of affected 

passenger chemical oxygen generators. 

We are issuing this AD to prevent 

failure of the passenger chemical oxygen 

generator to activate and consequently 

not deliver oxygen during an 

emergency, possibly resulting in injury 

to airplane occupants. 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA AD 2015–0118, 

dated June 24, 2015 (referred to after 

this as the Mandatory Continuing 

Airworthiness Information, or ‘‘the 

MCAI’’), to correct an unsafe condition 

for all Airbus Model A300 B4–600, B4– 

600R, and F4–600R series airplanes, and 

Model A300 C4–605R Variant F 

airplanes (collectively called Model 

A300–600 series airplanes); and Model 

A310 series airplanes. The MCAI states: 

Reports have been received indicating 

premature ageing of certain chemical oxygen 

generators, Part Number (P/N) 117042–XX 

(XX representing any numerical value), 

manufactured by B/E Aerospace. Some 

operators reported that when they tried to 

activate generators, some older units failed to 

activate. Given the number of failed units 

reported, all generators manufactured in 


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33360 Federal Register / Vol. 81, No. 102 / Thursday, May 26, 2016 / Rules and Regulations 

1999, 2000, and 2001 were considered 

unreliable. 

This condition, if not corrected, could lead 

to failure of the generator to activate and 

consequently not deliver oxygen during an 

emergency, possibly resulting in injury to 

aeroplane occupants. 

To address this potential unsafe condition, 

Airbus issued Alert Operators Transmission 

(AOT) A35W008–14, making reference to 

B/E Aerospace Service Information Letter 

(SIL) D1019–01 (currently at Revision 1) and 

B/E Aerospace Service Bulletin (SB) 117042– 

35–001. Consequently, EASA issued AD 

2014–0280 [http://ad.easa.europa.eu/ad/

2014-0280] to require identification and 

replacement of the affected oxygen 

generators. 

Since EASA AD 2014–0280 was issued, 

and following new investigation results, 

EASA [has] decided to introduce a life 

limitation concerning all P/N 117042–XX 

chemical oxygen generators, manufactured 

by B/E Aerospace. 

For the reason described above, this 

[EASA] AD retains the requirements of EASA 

AD 2014–0280, which is superseded, 

expands the scope of the [EASA] AD to 

include chemical oxygen generators 

manufactured after 2001, and requires their 

removal from service before exceeding 10 

years since date of manufacture. 

You may examine the MCAI in the 

AD docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

7528. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM or 

on the determination of the cost to the 

public. 

Additional Change Made to This AD 

In paragraph (i) of the proposed AD, 

we inadvertently referred to Airbus 

Alert Operators Transmission (AOT) 

A35N006–14, including Appendix 01, 

dated December 10, 2014, as the 

appropriate source of service 

information for replacing 22 minute 

passenger chemical oxygen generators. 

We have corrected that error in 

paragraph (i) of this AD, which refers to 

Airbus AOT A35W008–14, dated 

December 18, 2014, including Appendix 

A, undated, as the appropriate source of 

service information for replacing 22 

minute passenger chemical oxygen 

generators. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting this AD 

with the change described previously, 

and minor editorial changes. We have 

determined that these minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM for 

correcting the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

We also determined that these 

changes will not increase the economic 

burden on any operator or increase the 

scope of this AD. 

Related Service Information Under 1 

CFR Part 51 

We reviewed the following service 

information. 

• Airbus AOT A35W008–14, dated 

December 18, 2014, including Appendix 

A, undated. 

• B/E Aerospace Service Bulletin 

117042–35–001, dated December 10, 

2014. 

This service information describes 

procedures to replace certain passenger 

chemical oxygen generators. This 

service information is reasonably 

available because the interested parties 

have access to it through their normal 

course of business or by the means 

identified in the ADDRESSES section. 

Costs of Compliance 

We estimate that this AD affects 166 

airplanes of U.S. registry. 

We also estimate that it will take 

about 2 work-hours per product to 

comply with the basic requirements of 

this AD, and 1 work-hour per product 

for reporting. The average labor rate is 

$85 per work-hour. Required parts will 

cost about $390 per product. Based on 

these figures, we estimate the cost of 

this AD on U.S. operators to be 

$107,070, or $645 per product. 

Paperwork Reduction Act 

A federal agency may not conduct or 

sponsor, and a person is not required to 

respond to, nor shall a person be subject 

to penalty for failure to comply with a 

collection of information subject to the 

requirements of the Paperwork 

Reduction Act unless that collection of 

information displays a current valid 

OMB control number. The control 

number for the collection of information 

required by this AD is 2120–0056. The 

paperwork cost associated with this AD 

has been detailed in the Costs of 

Compliance section of this document 

and includes time for reviewing 

instructions, as well as completing and 

reviewing the collection of information. 

Therefore, all reporting associated with 

this AD is mandatory. Comments 

concerning the accuracy of this burden 

and suggestions for reducing the burden 

should be directed to the FAA at 800 

Independence Ave. SW., Washington, 

DC 20591, ATTN: Information 

Collection Clearance Officer, AES–200. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

section 106, describes the authority of 

the FAA Administrator. ‘‘Subtitle VII: 

Aviation Programs,’’ describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in ‘‘Subtitle VII, 

Part A, Subpart III, Section 44701: 

General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We determined that this AD will not 

have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect on 

the States, on the relationship between 

the national government and the States, 

or on the distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify that this AD: 

1. Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

2. Is not a ‘‘significant rule’’ under the 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979); 

3. Will not affect intrastate aviation in 

Alaska; and 

4. Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 


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Federal Register / Vol. 81, No. 102 / Thursday, May 26, 2016 / Rules and Regulations 33361 

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

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

2016–10–13 Airbus: Amendment 39–18524. 

Docket No. FAA–2015–7528; Directorate 

Identifier 2015–NM–004–AD. 

(a) Effective Date 

This AD is effective June 30, 2016. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the airplanes identified 

in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), and 

(c)(5) of this AD, certificated in any category, 

all manufacturer serial numbers. 

(1) Airbus Model A300 B4–601, B4–603, 

B4–620, and B4–622 airplanes. 

(2) Airbus Model A300 B4–605R and B4– 

622R airplanes. 

(3) Airbus Model A300 F4–605R and F4– 

622R airplanes. 

(4) Airbus Model A300 C4–605R Variant F 

airplanes. 

(5) Airbus Model A310–203, –204, –221, 

–222, –304, –322, –324, and –325 airplanes. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 35, Oxygen. 

(e) Reason 

This AD was prompted by reports of 

premature aging of certain passenger 

chemical oxygen generators that resulted in 

the generators failing to activate. We are 

issuing this AD to prevent failure of the 

passenger chemical oxygen generator to 

activate and consequently not deliver oxygen 

during an emergency, possibly resulting in 

injury to airplane occupants. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Part Number Inspection 

Within 30 days after the effective date of 

this AD, do a one-time inspection of 

passenger chemical oxygen generators, part 

numbers (P/N) 117042–02 (15 minutes 

(min)—2 masks), 117042–03 (15 min—3 

masks), 117042–04 (15 min—4 masks), 

117042–22 (22 min—2 masks), 117042–23 

(22 min—3 masks), or 117042–24 (22 min— 

4 masks), to determine the date of 

manufacture, as specified in Airbus Alert 

Operators Transmission (AOT) A35W008–14, 

dated December 18, 2014, including 

Appendix A, undated. Refer to Figure 1 to 

paragraph (g) of this AD and Figure 2 to 

paragraph (g) of this AD for the location of 

the date. A review of airplane maintenance 

records is acceptable for the inspection 

required by this paragraph, provided the date 

of manufacture can be conclusively 

determined by that review. 

BILLING CODE 4910–13–P 


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BILLING CODE 4910–13–C 

(h) Replacement of Passenger Chemical 

Oxygen Generators Manufactured in 1999, 

2000, and 2001 

If, during any inspection required by 

paragraph (g) of this AD, any passenger 

chemical oxygen generator having a date of 

manufacture in 1999, 2000, or 2001 is found: 

At the applicable time specified in paragraph 

(h)(1), (h)(2), or (h)(3) of this AD, remove and 

replace the affected passenger chemical 

oxygen generator with a serviceable unit, in 

accordance with the Accomplishment 

Instructions of B/E Aerospace Service 

Bulletin 117042–35–001, dated December 10, 

2014 (for 15 minute passenger chemical 

oxygen generators); or Airbus AOT 

A35W008–14, dated December 18, 2014, 

including Appendix A, undated (for 22 

minute passenger chemical oxygen 

generators); as applicable. 

(1) For passenger chemical oxygen 

generators that have a date of manufacture in 

1999: Remove and replace within 30 days 

after the effective date of this AD. 

(2) For passenger chemical oxygen 

generators that have a date of manufacture in 

2000: Remove and replace within 6 months 

after the effective date of this AD. 

(3) For passenger chemical oxygen 

generators that have a date of manufacture in 

2001: Remove and replace within 12 months 

after the effective date of this AD. 

(i) Replacement of Passenger Chemical 

Oxygen Generators Manufactured in 2002 

and Later 

If, during any inspection required by 

paragraph (g) of this AD, any passenger 

chemical oxygen generator having a date 

specified in Table 1 to paragraph (i) of this 

AD is found: At the applicable time specified 

in Table 1 to paragraph (i) of this AD, remove 

and replace the affected passenger chemical 

oxygen generator with a serviceable unit, in 

accordance with the Accomplishment 

Instructions of B/E Aerospace Service 

Bulletin 117042–35–001, dated December 10, 

2014 (for 15 minute passenger chemical 

oxygen generators); or Airbus AOT 

A35W008–14, dated December 18, 2014, 

including Appendix A, undated (for 22 

minute passenger chemical oxygen 

generators); as applicable. 


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Federal Register / Vol. 81, No. 102 / Thursday, May 26, 2016 / Rules and Regulations 33363 

TABLE 1 TO PARAGRAPH (i) OF THIS AD—REPLACEMENT COMPLIANCE TIMES

Year of manufacture Compliance time 

2002 ......................................................... Within 12 months after the effective date of this AD. 

2003 ......................................................... Within 16 months after the effective date of this AD. 

2004 ......................................................... Within 20 months after the effective date of this AD. 

2005 ......................................................... Within 24 months after the effective date of this AD. 

2006 ......................................................... Within 28 months after the effective date of this AD. 

2007 ......................................................... Within 32 months after the effective date of this AD. 

2008 ......................................................... Within 36 months after the effective date of this AD. 

2009 ......................................................... Before exceeding 10 years since date of manufacture of the passenger chemical oxygen generator. 

(j) Definition of Serviceable 

For the purpose of this AD, a serviceable 

unit is a passenger chemical oxygen 

generator having P/N 117042–XX (XX 

represents any numerical value) with a 

manufacturing date not older than 10 years, 

or any other approved part number, provided 

that the generator has not exceeded the life 

limit established for that generator by the 

manufacturer. 

(k) Reporting 

At the applicable time specified in 

paragraph (k)(1) or (k)(2) of this AD, submit 

a report of the findings (both positive and 

negative) of the inspection required by 

paragraph (g) of this AD, in accordance with 

paragraph 7., ‘‘Reporting,’’ of Airbus AOT 

A35W008–14, dated December 18, 2014, 

including Appendix A, undated. The report 

must include the information specified in 

Appendix A, undated, of Airbus AOT 

A35W008–14, dated December 18, 2014. 

(1) If the inspection was done on or after 

the effective date of this AD: Submit the 

report within 30 days after the inspection. 

(2) If the inspection was done before the 

effective date of this AD: Submit the report 

within 30 days after the effective date of this 

AD. 

(l) Parts Installation Limitation 

As of the effective date of this AD, no 

person may install a passenger chemical 

oxygen generator, unless it is determined, 

prior to installation, that the oxygen 

generator is a serviceable unit (as defined in 

paragraph (j) of this AD). 

(m) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, FAA, has the authority to 

approve AMOCs for this AD, if requested 

using the procedures found in 14 CFR 39.19. 

In accordance with 14 CFR 39.19, send your 

request to your principal inspector or local 

Flight Standards District Office, as 

appropriate. If sending information directly 

to the International Branch, send it to ATTN: 

Dan Rodina, Aerospace Engineer, 

International Branch, ANM–116 Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone: 425–227- 2125; fax: 425–227– 

1149. Information may be emailed to: 9- 

ANM-116-AMOC-REQUESTS@faa.gov. 

Before using any approved AMOC, notify 

your appropriate principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office/

certificate holding district office. The AMOC 

approval letter must specifically reference 

this AD. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer, the action must 

be accomplished using a method approved 

by the Manager, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the European Aviation Safety Agency 

(EASA); or Airbus’s EASA Design 

Organization Approval (DOA). If approved by 

the DOA, the approval must include the 

DOA-authorized signature. 

(3) Reporting Requirements: A federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave. SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

(n) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA AD 

2015–0118, dated June 24, 2015, for related 

information. This MCAI may be found in the 

AD docket on the Internet at http://

www.regulations.gov by searching for and 

locating Docket No. FAA–2015–7528. 

(o) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless this AD specifies otherwise. 

(i) Airbus Alert Operators Transmission 

(AOT) A35W008–14, dated December 18, 

2014, including Appendix A, undated. 

(ii) B/E Aerospace Service Bulletin 

117042–35–001, dated December 10, 2014. 

(3) For Airbus service information 

identified in this AD, contact Airbus SAS, 

Airworthiness Office—EAW, 1 Rond Point 

Maurice Bellonte, 31707 Blagnac Cedex, 

France; telephone: +33 5 61 93 36 96; fax: 

+33 5 61 93 44 51; email: account.airwortheas@airbus.com; Internet http://

www.airbus.com. 

(4) For B/E Aerospace service information 

identified in this AD, contact B/E Aerospace 

Inc., 10800 Pflumm Road, Lenexa, KS 66215; 

telephone: 913–338–9800; fax: 913–469– 

8419; Internet http://beaerospace.com/home/ 

globalsupport. 

(5) You may view this service information 

at the FAA, Transport Airplane Directorate, 

1601 Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(6) You may view this service information 

that is incorporated by reference at the 

National Archives and Records 

Administration (NARA). For information on 

the availability of this material at NARA, call 

202–741–6030, or go to: http://

www.archives.gov/federal-register/cfr/ibrlocations.html. 

Issued in Renton, Washington, on May 12, 

2016. 

Suzanne Masterson, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–12156 Filed 5–25–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–2457; Directorate 

Identifier 2014–NM–209–AD; Amendment 

39–18525; AD 2016–10–14] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 


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