Federal Register / Vol. 79, No. 39 / Thursday, February 27, 2014 / Rules and Regulations 10959 

information to the public shall be 

considered. It shall be presumed that a 

Representative of the News Media 

satisfies this consideration. 

(4) Whether the disclosure is likely to 

contribute significantly to public 

understanding of government operations 

or activities. The public’s understanding 

of the subject in question must be 

enhanced by the disclosure to a 

significant extent, as compared to the 

level of public understanding existing 

prior to the disclosure. The NCPC shall 

not make value judgments about 

whether information that would 

contribute significantly to public 

understanding of the operations or 

activities of the government is important 

enough to be made public. 

(c) To determine whether disclosure 

of the information is not primarily in 

the commercial interest of the 

Requester, the Requester shall 

demonstrate, and NCPC shall consider, 

the following factors: 

(1) Whether the Requester has a 

commercial interest that would be 

furthered by the Requested disclosure. 

The NCPC shall consider any 

commercial interest of the Requester 

(with reference to the definition of 

Commercial Use Request in § 456.3(f)), 

or of any person on whose behalf the 

Requester may be acting, that would be 

furthered by the Requested disclosure. 

Requesters shall be given an 

opportunity in the administrative 

process to provide explanatory 

information regarding this 

consideration. 

(2) Whether any identified 

commercial interest of the Requester is 

sufficiently large in comparison with 

the public interest in disclosure that 

disclosure is primarily in the 

commercial interest of the Requester. A 

Fee Waiver is justified where the public 

interest standard of paragraph (b) of this 

section is satisfied and that public 

interest is greater in magnitude than that 

of any identified commercial interest in 

disclosure. The NCPC ordinarily shall 

presume that a Representative of the 

News Media satisfies the public interest 

standard, and the public interest will be 

the interest primarily served by 

disclosure to that Requester. Disclosure 

to data brokers or others who merely 

compile and market government 

information for direct economic return 

shall not be presumed to primarily serve 

the public interest. 

(d) Where only some of the Records 

to be released satisfy the requirements 

for a Fee Waiver, a Fee Waiver shall be 

granted for those Records. 

(e) Requests for a Fee Waiver should 

address the factors listed in paragraphs 

(b) and (c) of this section, insofar as they 

apply to each Request. The NCPC shall 

exercise its discretion to consider the 

cost-effectiveness of its investment of 

administrative resources in this 

decision-making process in deciding to 

grant Fee Waivers. 

§ 456.16 Preservation of FOIA records. 

(a) The NCPC shall preserve all 

correspondence pertaining to FOIA 

Requests received and copies or Records 

provided until disposition or 

destruction is authorized by the NCPC’s 

General Records schedule of the 

National Archives and Records 

Administration (NARA) or other NARAapproved Schedule. 

(b) Materials that are responsive to a 

FOIA Request shall not be disposed of 

or destroyed while the Request or a 

related lawsuit is pending even if the 

Records would otherwise be authorized 

for disposition under the NCPC’s 

General Records Schedule or NARA or 

other NARA-approved records schedule. 

[FR Doc. 2014–04180 Filed 2–26–14; 8:45 am] 

BILLING CODE 7520–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2013–0695; Directorate 

Identifier 2011–NM–264–AD; Amendment 

39–17726; AD 2014–01–03] 

RIN 2120–AA64 

Airworthiness Directives; Saab AB, 

Saab Aerosystems Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Saab AB, Saab Aerosystems Model 340A 

(SAAB/SF340A) and SAAB 340B 

airplanes modified by Supplemental 

Type Certificate SA7971SW. This AD 

was prompted by reports of smoke, a 

burning odor, and possible fire in the 

flight deck and cabin of the airplane, 

which was caused by brushes wearing 

beyond their limits in the air 

conditioning motor. This AD requires an 

inspection to determine if a certain air 

compressor motor is installed, an 

inspection to determine the age of a 

certain compressor hour meter since 

new or overhauled, and repetitive 

replacement of the brushes on affected 

air conditioning compressor motor 

units. As an option to the replacement, 

this AD allows pulling the air 

conditioning circuit breaker and adding 

a placard. We are issuing this AD to 

detect and correct worn brushes 

contacting the commutator, which could 

result in a fire under the cabin floor 

with no means to detect or extinguish 

the fire. 

DATES: This AD is effective April 3, 

2014. 

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–2013– 

0695; 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 address for the 

Docket Office (phone: 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: 

Gregory Thiele, Aerospace Engineer, 

Special Certification Office, ASW–190, 

FAA, 2601 Meacham Boulevard, Fort 

Worth, TX 76137; phone: (817) 222– 

5229; fax: (817) 222–5785; email: 

gregory.thiele@faa.gov. 

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 certain Saab AB, Saab 

Aerosystems Model 340A (SAAB/

SF340A) and SAAB 340B airplanes 

modified by Supplemental Type 

Certificate SA7971SW (http:// 

rgl.faa.gov/Regulatory_and_Guidance_

Library/rgstc.nsf/0/CE3676ED

FD53938785256CC20058E501?

OpenDocument&Highlight=sa7971sw). 

The NPRM published in the Federal 

Register on August 16, 2013 (78 FR 

49982). The NPRM was prompted by 

reports of smoke, a burning odor, and 

possible fire in the flight deck and cabin 

of the airplane, which was caused by 

brushes wearing beyond their limits in 

the air conditioning motor. The NPRM 

proposed to require an inspection to 

determine if a certain air compressor 

motor is installed, an inspection to 

determine the age of a certain 

compressor hour meter since new or 

overhauled, and repetitive replacement 

of the brushes on affected air 

conditioning compressor motor units. 

As an option to the replacement, the 

NPRM proposed to allow pulling the air 


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10960 Federal Register / Vol. 79, No. 39 / Thursday, February 27, 2014 / Rules and Regulations 

conditioning circuit breaker and adding 

a placard. We are issuing this AD to 

detect and correct worn brushes 

contacting the commutator, which could 

result in a fire under the cabin floor 

with no means to detect or extinguish 

the fire. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (78 

FR 49982, August 16, 2013) or on the 

determination of the cost to the public. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting this AD 

as proposed except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (78 FR 

49982, August 16, 2013) for correcting 

the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (78 FR 49982, 

August 16, 2013). 

Interim Action 

We consider this AD interim action. 

The inspection reports required by this 

AD will enable us to obtain better 

insight into the nature, cause, and 

extent of the brush wear, and eventually 

to develop final action to address the 

unsafe condition. Once final action has 

been identified, we might consider 

further rulemaking. 

Costs of Compliance 

We estimate that this AD affects 23 

airplanes of U.S. registry. 

We estimate the following costs to 

comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per product Cost on U.S. operators 

Inspection, drive motor assembly brush replacement; and parts return 

and report.

11 work-hours × $85 per 

hour = $935 per replacement cycle.

$252 per replacement 

cycle.

$1,187 per replacement 

cycle.

$27,301 per replacement 

cycle. 

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 

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 

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: 

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): 

2014–01–03 Saab AB, Saab Aerosystems: 

Amendment 39–17726; Docket No. 

FAA–2013–0695; Directorate Identifier 

2011–NM–264–AD. 

(a) Effective Date 

This AD is effective April 3, 2014. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Saab AB, Saab 

Aerosystems Model 340A (SAAB/SF340A) 

and SAAB 340B airplanes, certificated in any 

category, that have been modified as 

specified in Supplemental Type Certificate 

SA7971SW (http://rgl.faa.gov/Regulatory_

and_Guidance_Library/rgstc.nsf/0/

CE3676EDFD53938785256CC200

58E501?OpenDocument&Highlight=

sa7971sw). 

(d) Subject 

Air Transport Association (ATA) of 

America Code 21, Air Conditioning. 


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Federal Register / Vol. 79, No. 39 / Thursday, February 27, 2014 / Rules and Regulations 10961 

(e) Unsafe Condition 

This AD was prompted by reports of 

smoke, a burning odor, and possible fire in 

the flight deck and cabin of the airplane, 

which were caused by brushes wearing 

beyond their limits in the air conditioning 

motor. We are issuing this AD to detect and 

correct worn brushes contacting the 

commutator, which could result in a fire 

under the cabin floor with no means to detect 

or extinguish the fire. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Part Number (P/N) Inspection 

Within 30 days or 10 flight hours after the 

effective date of this AD, whichever occurs 

first: Inspect the air conditioner (A/C) 

compressor motor to determine if P/N 

1134104–1 is installed. A review of airplane 

maintenance records is acceptable in lieu of 

this inspection if the part number of the 

A/C compressor motor can be conclusively 

determined from that review. 

(h) Inspection of Compressor Hour Meter 

and Maintenance Records 

If, during the inspection required by 

paragraph (g) of this AD, any A/C compressor 

motor is found having P/N 1134104–1: 

Within 30 days or 10 flight hours after the 

effective date of this AD, whichever occurs 

first, determine the hour reading on the 

A/C compressor hour meter as specified in 

paragraphs (h)(1) and (h)(2) of this AD. 

(1) Inspect the number of hours on the 

A/C compressor hour meter. 

(2) Check the airplane logbook for any 

entry for replacing the A/C compressor motor 

brushes with new brushes, or for replacing 

the compressor motor or compressor 

condenser module assembly (pallet) with a 

motor or assembly that has new brushes. 

(i) If the logbook contains an entry for 

replacement of parts as specified in 

paragraph (h)(2) of this AD, determine the 

number of hours on the A/C compressor 

motor brushes by comparing the number of 

hours on the compressor motor since 

replacement and use this number in lieu of 

the number determined in paragraph (h)(1) of 

this AD. 

(ii) If, through the logbook check, the 

number of hours on the A/C compressor 

motor brushes cannot be positively 

determined as specified in paragraph (h)(2) of 

this AD, use the number of hours on the 

A/C compressor hour meter determined in 

paragraph (h)(1) of this AD, or assume the 

brushes have over 500 hours time-in-service. 

(i) Replacement 

Except as provided by paragraph (k) of this 

AD: Using the hour reading on the A/C 

compressor hour meter determined in 

paragraph (h) of this AD, replace the A/C 

compressor motor brushes with new brushes 

at the later of the times specified in 

paragraphs (i)(1) and (i)(2) of this AD. 

Thereafter, repeat the replacement of the 

A/C compressor motor brushes at intervals 

not to exceed 500 hours time-in-service on 

the A/C compressor motor. Do the 

replacement in accordance with the actions 

specified in paragraph (j) of this AD. 

(1) Before or when the A/C compressor 

motor reaches a total of 500 hours time-inservice. 

(2) Before further flight after the inspection 

required by paragraph (h) of this AD. 

(j) Motor Brush Replacement Instructions 

Do the actions specified in paragraphs (j)(1) 

through (j)(23) of this AD to replace the 

compressor motor brushes as required by 

paragraph (i) of this AD: 

(1) New brushes may be installed by first 

level maintenance personnel only under the 

conditions listed in paragraphs (j)(1)(i) 

through (j)(1)(iv) of this AD. If these 

conditions are not met, deactivate the A/C in 

accordance with paragraph (k)(1) of this AD 

until the conditions listed in paragraphs 

(j)(1)(i) through (j)(1)(iv) of this AD are met, 

or the entire compressor motor is replaced. 

(i) Motor was operating correctly prior to 

brush replacement. 

(ii) The motor is tested to verify proper 

operation and does not show any defects that 

would require motor replacement. 

(iii) Only approved vendor brushes are 

used (P/N 1251171). 

(iv) Brushes are installed, seated, and 

tested in accordance with paragraphs (j)(2) 

through (j)(23) of this AD. 

(2) Verify all electrical power is off to the 

system. 

(3) Remove all access panels and exhaust 

ducts to gain access to the drive motor. 

(4) Disconnect power leads from motor 

terminals (1/4–28). Tag the positive lead. 

(5) Remove condenser support bracket to 

provide access to brush cover fasteners and 

remove motor cuff shroud. 

(6) Loosen and unsnap brush cover 

assembly. Remove from the motor. 

(7) Verify all power is off, and that all 

panels, shrouds, brackets, and fairings are 

removed. 

(8) With a stiff wire hook or scribe, lift 

brush spring from holder and remove each 

worn brush set until all four sets are 

removed. 

(9) Remove brush shunt wire terminal 

screw. Continue this step until all four 

screws are removed. 

(10) With brushes removed and using shop 

air at 30–40 pounds per square inch gauge 

(psig) and nozzle, blow out as much carbon 

and/or copper dust as possible from the 

commutator, armature, and field windings. 

Purge from the commutator end of the motor. 

(11) Install each new brush set by lifting 

brush springs, sliding brush into holder (with 

brush leading edge in direction of motor 

rotation) and lightly releasing the brush 

spring on the brush. (See Figure 1 to 

paragraph (m)(4)(vii) of this AD.) CAUTION: 

Do not allow brush spring to strike hard into 

place or damage to brush may result. 

(12) Verify that the brush seats flat on the 

commutator and that no binding in the 

holder is present. Align brush spring in 

center of brush groove. 

(13) Install terminal screw and lock washer 

on brush shunt lead and other leads and 

tighten. Repeat this step for other brush sets. 

Torque to 15–20 in.-lbs. CAUTION: Do not 

cross thread or over torque brush lead screws 

or thread damage may result. 

(14) Seat new brushes in accordance with 

paragraph (j)(15) of this AD. All new brushes 

must be seated to assure proper motor 

operation and/or performance. 

(15) Brush Seating Procedure: Cut a 7 inch 

long by 1.5 inch wide (±0.125 inch, both 

dimensions) strip of 400–500 grit sand paper 

and place, with rough side out, on 

commutator. Secure one end of the paper to 

the commutator with masking tape in a 

manner such that the taped end will lead in 

the direction of shaft rotation (counterclockwise looking at fan end). The other end 

will remain loose and overlap the taped end. 

Raise each brush momentarily while rotating 

the shaft until the taped end passes under 

each brush. After the sand paper is properly 

located tight against the commutator and 

encompasses all brush surface areas, 

carefully rotate the armature, by hand, in the 

normal direction of rotation until a full seat 

is obtained on each new brush. Three or four 

rotations is usually adequate. Excessive 

seating is not advised. Brush life may be 

reduced. 

(16) Remove sand paper and blow out all 

carbon dust from the commutator and brush 

area. CAUTION: Eye, nose, and throat 

protection must be worn during this 

procedure. 

(17) Lay brush shunt leads in position 

carefully such as to prevent any shorting 

problems. Leads must be able to easily follow 

brush and spring movement as brush wear 

occurs. 

(18) Replace brush cover and attach motor 

power cables, if required. 

(19) Replace all bracketry and hardware 

removed to access motor. 

(20) Assure that brackets are properly 

installed, cooling fan does not interfere with 

shroud, motor drive belt aligned/tensioned, 

and belt cover is installed. 

(21) Test the motor to verify proper 

operation. Therefore, connect ground power 

source or verify aircraft power is on and turn 

system on. 

(22) Run system for a minimum of 15 

minutes to seat brushes and check motor 

operation. 

(23) Turn system and aircraft power off. 

System is ready for use. 

(k) Deactivation/Reactivation 

(1) In lieu of replacing the A/C compressor 

motor brushes as required by paragraphs (i) 

and (j) of this AD, before further flight, 

deactivate the A/C by doing the actions 

specified in paragraph (k)(1)(i) or (k)(1)(ii) of 

this AD, as applicable. 

(i) Single System: Pull the compressor 

control circuit breaker (cockpit right-hand 

10VU panel, ‘‘REAR AIR COND’’); install a 

placard by the A/C selection switch (copilot’s side panel) prohibiting use of the air 

conditioner; and document deactivation of 

the system in the airplane logbook referring 

to this AD as the reason for deactivation. 

(ii) Dual System: Pull the compressor 

control circuit breakers (cockpit right-hand 

10VU panel, ‘‘REAR AIR COND,’’ and 

cockpit left-hand 9VU panel, ‘‘FWD AIR 

COND’’); install a placard (or placards) by the 

A/C selection switches (co-pilot’s side panel) 

prohibiting use of the air conditioners; and 

document deactivation of the system in the 


TKELLEY on DSK3SPTVN1PROD with RULES
10962 Federal Register / Vol. 79, No. 39 / Thursday, February 27, 2014 / Rules and Regulations 

airplane logbook referring to this AD as the 

reason for deactivation. 

(2) If an operator chooses to deactivate the 

system and then later chooses to return the 

airplane to service: Before returning the A/C 

system to service and removing the 

placard(s), do the inspection specified in 

paragarph (g) of this AD, and, as applicable, 

the inspection specified in paragraph (h) of 

this AD, and the replacements specified in 

paragraph (i) of this AD at the times specified 

in paragraph (i) of this AD. 

(l) Parts Installation Limitation 

As of the effective date of this AD, no 

person may install an A/C compressor motor 

having P/N 1134104–1 on any airplane, 

unless the inspection specified in paragraph 

(h) of this AD has been done, and the 

replacements specified in paragraph (i) of 

this AD are done at the times specified in 

paragraph (i) of this AD. 

(m) Reporting Requirement 

Submit a report of the results of the 

determination of hours required by paragraph 

(h) of this AD to the Special Certification 

Office, ASW–190, FAA, Attn: Gregory Thiele, 

Aerospace Engineer, 2601 Meacham 

Boulevard, Fort Worth, TX 76137; or email 

to: 9-ASW-190-COS@faa.gov. The report 

must include the information specified in 

paragraphs (m)(1) through (m)(4) of this AD. 

(1) The model and serial number of the 

airplane. 

(2) The elapsed amount of flight hours 

since the last brush/motor replacement, if 

known. 

(3) The amount of hours on the hour meter 

of the A/C compressor motor. 

(4) The amount of wear on the brushes 

(including overall length and total calculated 

wear), calculated as specified in paragraphs 

(m)(4)(i) through (m)(4)(ix) of this AD. 

(i) Verify all electrical power is off to the 

system. 

(ii) Remove all access panels and exhaust 

ducts to gain access to the drive motor. 

(iii) Disconnect power leads from motor 

terminals (1/4–28). Tag positive lead. 

(iv) Remove condenser support bracket to 

provide access to brush cover fasteners and 

remove motor cuff shroud. 

(v) Loosen and unsnap brush cover 

assembly. Remove from motor. 

(vi) Lift brush spring and remove brush 

with wire hook or scribe. 

(vii) Measure each brush as shown in 

figure below and record values. 

(viii) Using the brush with the shortest 

measured length, calculate the wear by 

subtracting the measured value from 1.000 

inch. 

(ix) Replace brushes in accordance with 

the instructions specified in paragraphs (j)(9) 

through (j)(23) of this AD. 

(n) Compliance Time for Reporting 

Submit the report required by paragraph 

(m) of this AD at the applicable time 

specified in paragraph (n)(1) or (n)(2) of this 

AD. 

(1) If the determination of hours was done 

on or after the effective date of this AD: 

Submit the report within 30 days after the 

inspection. 

(2) If the determination of hours was done 

before the effective date of this AD: Submit 

the report within 30 days after the effective 

date of this AD. 

(o) Special Flight Permit 

Special flight permits may be issued in 

accordance with sections 21.197 and 21.199 

of the Federal Aviation Regulations (14 CFR 

21.197 and 21.199) to operate the airplane to 

an appropriately rated repair station, 

provided that the A/C is deactivated as 

specified in paragraph (k)(1) of this AD on 

airplanes on which the A/C has been 

operated for 500 hours or more, and 

replacement brushes are not available. 

(p) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Special Certification 

Office, ASW–190, 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 manager of the Special Certification 

Office, send it to the attention of the person 

identified in paragraph (q) of this AD. 

(2) 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. 

(q) Related Information 

For more information about this AD, 

contact Gregory Thiele, Aerospace Engineer, 

Special Certification Office, ASW–190, FAA, 

2601 Meacham Boulevard, Fort Worth, TX 

76137; phone: (817) 222–5229; fax: (817) 

222–5785; email: gregory.thiele@faa.gov. 

(r) Material Incorporated by Reference 

None. 

Issued in Renton, Washington, on January 

7, 2014. 

Jeffrey E. Duven, 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2014–03817 Filed 2–26–14; 8:45 am] 

BILLING CODE 4910–13–P 


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