20526 Federal Register / Vol. 77, No. 66 / Thursday, April 5, 2012 / Rules and Regulations 

(F) The List of Effective Pages for Chapter 

54 identifies an incorrect date for page 1 of 

Section 54–23–00; the correct date for that 

page is May 15, 1986. 

(G) The List of Effective Pages for Chapter 

54 identifies an incorrect date for page 4 of 

Section 54–32–00; the correct date for that 

page is March 15, 1992. 

(H) The List of Effective Pages for Chapter 

57 identifies an incorrect date for page 13 of 

Section 57–00–00; the correct date for that 

page is April 15, 2005. 

(I) The List of Effective Pages for Chapter 

57 identifies an incorrect date for pages 16 

and 18 of Section 57–12–00; the correct date 

for those pages is March 15, 1983. 

(J) The List of Effective Pages for Chapter 

57 identifies an incorrect date for pages 801, 

802, and 805/806 of Section 57–13–00; the 

correct date for those pages is December 15, 

2009. 

(K) The List of Effective Pages for Chapter 

57 identifies an incorrect date for pages 810 

through 819 of Section 57–51–00; the correct 

date for those pages is December 15, 2009. 

(L) The List of Effective Pages for Chapter 

57 identifies an incorrect date for page 4 of 

Section 57–52–00; the correct date for that 

page is December 15, 2009. 

(M) Page 25, dated March 15, 1983, and 

page 26, dated May 15, 1986, of Section 57– 

12–00 were inadvertently omitted from the 

List of Effective Pages for Chapter 57. 

(4) The following service information was 

approved for IBR November 2, 1995 (60 FR 

51713, October 3, 1995). 

(i) Lockheed Document Number 

LG92ER0060, ‘‘L–1011–385 Series 

Supplemental Inspection Document,’’ revised 

January 1994. 

(5) For service information identified in 

this AD, contact Lockheed Martin 

Corporation/Lockheed Martin Aeronautics 

Company, L1011 Technical Support Center, 

Dept. 6A4M, Zone 0579, 86 South Cobb 

Drive, Marietta, Georgia 30063–0579; 

telephone 770–494–5444; fax 770–494–5445; 

email L1011.support@lmco.com; Internet 

http://www.lockheedmartin.com/ams/tools/ 

TechPubs.html. 

(6) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, call 

425–227–1221. 

(7) You may also review copies of the 

service information that is incorporated by 

reference at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at an NARA facility, call 202–741– 

6030, or go to http://www.archives.gov/ 

federal_register/code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, WA, on March 1, 2012. 

Jeffrey E. Duven, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2012–8040 Filed 4–4–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2011–1318; Directorate 

Identifier 2010–NM–274–AD; Amendment 

39–17009; AD 2012–07–03] 

RIN 2120–AA64 

Airworthiness Directives; 328 Support 

Services GmbH Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are superseding an 

existing airworthiness directive (AD) for 

all 328 Support Services GmbH (Type 

Certificate previously held by AvCraft 

Aerospace GmbH; Fairchild Dornier 

GmbH; Dornier Luftfahrt GmbH) Model 

328–100 and –300 airplanes. That AD 

currently requires performing a detailed 

visual inspection of the cockpit door 

locking device and the surrounding area 

for proper installation, and corrective 

action if necessary. This new AD 

requires removing or replacing the 

locking device of the cockpit door; 

performing operational tests, and repair 

if necessary; and, for certain airplanes, 

installing gap filler parts. This AD was 

prompted by a report that a right-hand 

power lever jammed in flight-idle 

position during the landing roll-out, and 

the airplane was stopped by excessive 

braking. We are issuing this AD to 

detect and correct interference with the 

engine and flight control cables, which 

could result in reduced controllability 

of the airplane. 

DATES: This AD becomes effective May 

10, 2012. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of May 10, 2012. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain other publications listed in 

this AD as of November 20, 2009 (74 FR 

53151, October 16, 2009). 

ADDRESSES: You may examine the AD 

docket on the Internet at http://www.

regulations.gov or in person at the U.S. 

Department of Transportation, Docket 

Operations, M–30, West Building 

Ground Floor, Room W12–140, 1200 

New Jersey Avenue SE., Washington, 

DC. 

FOR FURTHER INFORMATION CONTACT: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, 

Washington 98057–3356; telephone 

(425) 227–1137; fax (425) 227–1149. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM was published in the Federal 

Register on December 12, 2011 (76 FR 

77159), and proposed to supersede AD 

2009–21–06, Amendment 39–16043 (74 

FR 53151, October 16, 2009). That 

NPRM proposed to correct an unsafe 

condition for the specified products. 

The MCAI states: 

An incident has been reported with a 

Dornier 328–100 aeroplane, where the righthand (RH) power lever jammed in flight-idle 

position during the landing roll-out. The 

aeroplane was stopped by excessive braking. 

The reason for the jamming was that the 

cockpit door locking device Part Number (P/ 

N) 001A252A3914012 had fallen off the RH 

cockpit wall, blocking the RH power/ 

condition lever pulley/cable cluster below 

the door. Although the affected aeroplane 

had been modified, the technical 

investigation showed that a loose Cockpit 

Door Locking device could also occur on 

328–100 and 328–300 aeroplanes with a 

standard installation. 

This condition, if not corrected, could 

cause interference with the engine and/or 

flight control cables, possibly resulting in 

reduced control of the aeroplane. 

To address that unsafe condition, EASA 

issued AD 2009–0082 [which corresponds to 

FAA AD 2009–21–06, Amendment 39–16043 

(74 FR 53151, October 16, 2009)] as an 

interim solution, to require a one-time 

inspection of the cockpit door locking device 

and the surrounding area and the reporting 

of all findings to the TC [type certificate] 

holder. 

Since that AD was issued, the TC holder 

has developed an improved cockpit door 

locking device, P/N 001A252A3914016. 

Consequently, this [EASA] AD retains the 

requirements of [EASA] AD 2009–0082, 

which is superseded, and requires the 

replacement of the current P/N 

001A252A3914012 with new designed P/N 

001A252A3914016 cockpit door locking 

device, or the removal of the cockpit door 

locking device P/N 001A252A3914012 and 

the installation of a gap filler, as applicable 

to aeroplane configuration. 

The required actions include performing 

operational tests, and repair if 

necessary. You may obtain further 

information by examining the MCAI in 

the AD docket. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (76 

FR 77159, December 12, 2011) or on the 

determination of the cost to the public. 


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Federal Register / Vol. 77, No. 66 / Thursday, April 5, 2012 / Rules and Regulations 20527 

Conclusion 

We reviewed the available data and 

determined that air safety and the 

public interest require adopting the 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 (76 FR 

77159, December 12, 2011) for 

correcting the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (76 FR 77159, 

December 12, 2011). 

Costs of Compliance 

We estimate that this AD will affect 

59 products of U.S. registry. 

The actions that are required by AD 

2009–21–06, Amendment 39–16043 (74 

FR 53151, October 16, 2009), and 

retained in this AD take about 1 workhour per product, at an average labor 

rate of $85 per work-hour. Based on 

these figures, the estimated cost of the 

currently required actions is $85 per 

product. 

We estimate that it will take about 6 

work-hours per product to comply with 

the new basic requirements of this AD. 

The average labor rate is $85 per workhour. Required parts will cost about 

$2,315 per product. Where the service 

information lists required parts costs 

that are covered under warranty, we 

have assumed that there will be no 

charge for these parts. As we do not 

control warranty coverage for affected 

parties, some parties may incur costs 

higher than estimated here. Based on 

these figures, we estimate the cost of 

this AD to the U.S. operators to be 

$166,675, or $2,825 per product. 

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. 

We prepared a regulatory evaluation 

of the estimated costs to comply with 

this AD and placed it in the AD docket. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://www.regulations.

gov; or in person at the Docket 

Operations office between 9 a.m. and 

5 p.m., Monday through Friday, except 

Federal holidays. The AD docket 

contains the NPRM (76 FR 77159, 

December 12, 2011), the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Operations office (telephone 

(800) 647–5527) is in the ADDRESSES

section. Comments will be available in 

the AD docket shortly after receipt. 

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 

removing airworthiness directive (AD) 

2009–21–06, Amendment 39–16043 (74 

FR 53151, October 16, 2009), and 

adding the following new AD: 

2012–07–03 328 Support Services GmbH 

(Type Certificate Previously Held by 

AvCraft Aerospace GmbH; Fairchild 

Dornier GmbH; Dornier Luftfahrt 

GmbH): Amendment 39–17009. Docket 

No. FAA–2011–1318; Directorate 

Identifier 2010–NM–274–AD. 

(a) Effective Date 

This airworthiness directive (AD) becomes 

effective May 10, 2012. 

(b) Affected ADs 

This AD supersedes AD 2009–21–06, 

Amendment 39–16043 (74 FR 53151, October 

16, 2009). 

(c) Applicability 

This AD applies to 328 Support Services 

GmbH (Type Certificate previously held by 

AvCraft Aerospace GmbH; Fairchild Dornier 

GmbH; Dornier Luftfahrt GmbH) Model 328– 

100 and –300 airplanes, certificated in any 

category, all serial numbers. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 25: Equipment/Furnishings. 

(e) Reason 

This AD was prompted by a report that a 

right-hand power lever jammed in flight-idle 

position during the landing roll-out, and the 

airplane was stopped by excessive braking. 

We are issuing this AD detect and correct 

interference with the engine and flight 

control cables, which could result in reduced 

controllability of the airplane. 

(f) Compliance 

You are responsible for having the actions 

required by this AD performed within the 

compliance times specified, unless the 

actions have already been done. 

(g) Restatement of Certain Requirements of 

AD 2009–21–06, Amendment 39–16043 

(74 FR 53151, October 16, 2009): Inspection 

Within 3 months after November 20, 2009 

(the effective date of AD 2009–21–06, 

Amendment 39–16043 (74 FR 53151, October 

16, 2009)), do a detailed visual inspection of 

the cockpit door locking device and the 

surrounding area for proper installation, in 

accordance with the Accomplishment 

Instructions of 328 Support Services Service 

Bulletin SB–328–25–485 or SB–328J–25–235, 

both dated January 28, 2009, as applicable. 

(h) Corrective Action 

If any discrepancy is found during the 

inspection specified in paragraph (g) of this 

AD, before further flight, do the corrective 

action, in accordance with the 

Accomplishment Instructions of 328 Support 

Services Service Bulletin SB–328–25–485 or 

SB–328J–25–235, both dated January 28, 

2009, as applicable. 

(i) New Requirements of This AD: Install, 

Replace, and Test 

Within 4,000 flight hours or 24 months 

after the effective date of this AD, whichever 

occurs first, do the applicable actions 

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

AD. 


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20528 Federal Register / Vol. 77, No. 66 / Thursday, April 5, 2012 / Rules and Regulations 

(1) For airplanes on which a door locking 

device with Option 521K010 is installed: 

Remove the locking device of the cockpit 

door, part number (P/N) 001A252A3914012, 

install the gap filler parts, and do operational 

tests, in accordance with the 

Accomplishment Instructions of 328 Support 

Services Service Bulletin SB–328–25–492, 

dated March 18, 2010 (for Model 328–100 

airplanes); or 328 Support Services Service 

Bulletin SB–328J–25–244, dated March 18, 

2010 (for Model 328–300 airplanes). 

(2) For airplanes on which a door locking 

device with Option 521K010 is not installed: 

Replace the locking device of the cockpit 

door, P/N 001A252A3914012, with a new 

locking device, P/N 001A252A3914016, and 

do operational tests, in accordance with the 

Accomplishment Instructions of 328 Support 

Services Service Bulletin SB–328–25–491, 

dated March 18, 2010 (for Model 328–100 

airplanes); or 328 Support Services Service 

Bulletin SB–328J–25–243, dated March 18, 

2010 (for Model 328–300 airplanes). 

(j) Repair 

If any operational test fails during the 

actions specified in paragraph (i)(1) or (i)(2) 

of this AD: Before further flight, repair in 

accordance with a method approved by the 

Manager, International Branch, ANM–116, 

Transport Airplane Directorate, FAA, or the 

European Aviation Safety Agency (or its 

delegated agent). 

(k) Parts Installation 

As the effective date of this AD, no person 

may install a locking device of the cockpit 

door having P/N 001A252A3914012 on any 

airplane. 

(l) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, 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: 

Tom Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, Washington 98057– 

3356; telephone (425) 227–1137; 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) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(m) Related Information 

Refer to MCAI EASA Airworthiness 

Directive 2010–0169, dated August 13, 2010, 

and the service bulletins specified in 

paragraphs (m)(1) through (m)(6) of this AD, 

for related information. 

(1) 328 Support Services Service Bulletin 

SB–328–25–485, dated January 28, 2009. 

(2) 328 Support Services Service Bulletin 

SB–328J–25–235, dated January 28, 2009. 

(3) 328 Support Services Service Bulletin 

SB–328–25–491, dated March 18, 2010. 

(4) 328 Support Services Service Bulletin 

SB–328J–25–243, dated March 18, 2010. 

(5) 328 Support Services Service Bulletin 

SB–328–25–492, dated March 18, 2010. 

(6) 328 Support Services Service Bulletin 

SB–328J–25–244, dated March 18, 2010. 

(n) Material Incorporated by Reference 

(1) You must use the following service 

information to do the actions required by this 

AD, unless the AD specifies otherwise. The 

Director of the Federal Register approved the 

incorporation by reference (IBR) of the 

following service information under 5 U.S.C. 

552(a) and 1 CFR part 51 on the date 

specified: 

(i) 328 Support Services Service Bulletin 

SB–328–25–485, dated January 28, 2009, 

approved for IBR November 20, 2009 (74 FR 

53151, October 16, 2009). Only the oddnumbered pages of this document contain the 

issue date of the document. 

(ii) 328 Support Services Service Bulletin 

SB–328J–25–235, dated January 28, 2009, 

approved for IBR November 20, 2009 (74 FR 

53151, October 16, 2009). Only the oddnumbered pages of this document contain the 

issue date of the document. 

(iii) 328 Support Services Service Bulletin 

SB–328–25–491, dated March 18, 2010, 

approved for IBR May 10, 2012. Only the 

odd-numbered pages of this document 

contain the issue date of the document. 

(iv) 328 Support Services Service Bulletin 

SB–328–25–492, dated March 18, 2010, 

approved for IBR May 10, 2012. Only the 

odd-numbered pages of this document 

contain the issue date of the document. 

(v) 328 Support Services Service Bulletin 

SB–328J–25–243, dated March 18, 2010, 

approved for IBR May 10, 2012. Only the 

odd-numbered pages of this document 

contain the issue date of the document. 

(vi) 328 Support Services Service Bulletin 

SB–328J–25–244, dated March 18, 2010, 

approved for IBR May 10, 2012. Only the 

odd-numbered pages of this document 

contain the issue date of the document. 

(2) For service information identified in 

this AD, contact 328 Support Services GmbH, 

Global Support Center, P.O. Box 1252, D– 

82231 Wessling, Federal Republic of 

Germany; telephone +49 8153 88111 6666; 

fax +49 8153 88111 6565; email 

gsc.op@328support.de; Internet http:// 

www.328support.de. 

(3) You may review copies of the service 

information at the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue SW., Renton, 

Washington. For information on the 

availability of this material at the FAA, call 

425–227–1221. 

(4) You may also review copies of the 

service information that is incorporated by 

reference at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at an NARA facility, call 202–741– 

6030, or go to http://www.archives.gov/ 

federal_register/code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Renton, Washington, on March 

23, 2012. 

Ali Bahrami 

Manager, Transport Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2012–7850 Filed 4–4–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2011–1386; Airspace 

Docket No. 11–ANE–11] 

RIN 2120–AA66 

Modification, Revocation and 

Establishment of Air Traffic Service 

Routes; Windsor Locks Area; CT 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action modifies four 

VOR Federal airways, revokes one VOR 

Federal airway, and establishes three 

area navigation (RNAV) routes in the 

vicinity of Windsor Locks, CT. The FAA 

is taking this action to adjust the airway 

route structure due to the planned 

decommissioning of the Bradley VHF 

omnirange/tactical air navigation 

(VORTAC) aid located on Bradley 

International Airport, Windsor Locks, 

CT. This action also adjusts the 

termination point of V–203 due to 

Canadian airspace reconfiguration. 

DATES: Effective date 0901 UTC, May 31, 

2012. The Director of the Federal 

Register approves this incorporation by 

reference action under 1 CFR part 51, 

subject to the annual revision of FAA 

Order 7400.9 and publication of 

conforming amendments. 

FOR FURTHER INFORMATION CONTACT: Paul 

Gallant, Airspace, Regulations and ATC 

Procedures Group, Office of Airspace 

Services, Federal Aviation 

Administration, 800 Independence 

Avenue SW., Washington, DC 20591; 

telephone: (202) 267–8783. 

SUPPLEMENTARY INFORMATION: 

History 

On January 24, 2012, the FAA 

published in the Federal Register a 

notice of proposed rulemaking to 

modify certain VOR Federal airways 


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