Federal Register / Vol. 88, No. 233 / Wednesday, December 6, 2023 / Rules and Regulations 84693 

TABLE 1 TO PARAGRAPH (g)(1)—MODEL AS907–1–1A ENGINES—Continued 

Engine time since new (TSN) Compliance time 

Fewer than 3,000 hours TSN ................................................................... Within 24 months or 800 FH after the effective date of this AD, whichever occurs first. 

(2) For AS907–2–1G engines with serial 

numbers (S/N) P130101 through P130240 

that have not incorporated Honeywell SB 

AS907–72–9063, and for AS907–2–1G 

engines with S/Ns P130241 through P130336, 

and S/Ns P130101 through P130240 that 

have incorporated Honeywell SB AS907–72– 

9063, before exceeding the applicable 

compliance time in Table 2 to paragraph 

(g)(2) of this AD, replace any installed ECU 

having P/N 2119576–3001 or P/N 2119576– 

3002 with an ECU eligible for installation. 

All four ECUs installed in both airplane 

engines must be replaced at the same time. 

Note 2 to paragraph (g)(2): Guidance for 

removing and replacing the ECU may be 

found in Honeywell SB AS907–76–9014, 

Revision 6, dated October 10, 2022. 

Note 3 to paragraph (g)(2): Guidance for 

converting a standard flow compressor to a 

high flow compressor for improving surge 

margin may be found in Honeywell SB 

AS907–72–9063, Revision 1, dated July 31, 

2019. 

TABLE 2 TO PARAGRAPH (g)(2)—MODEL AS907–2–1G ENGINES

Engine type Compliance time 

Standard Flow Compressor AS907–2–1G engines (engine S/Ns 

P130101 through P130240 that have not incorporated Honeywell SB 

AS907–72–9063).

Within 2 years or 800 FH after the effective date of this AD, whichever 

occurs first. 

High Flow Compressor AS907–2–1G engines (engine S/Ns P130241 

through P130336 and engines that have incorporated Honeywell SB 

AS907–72–9063).

Within 7 years or 2,800 FH after the effective date of this AD, whichever occurs first. 

(h) Installation Prohibition 

(1) After the effective date of this AD, do 

not install an ECU having P/N 2119576–1011 

and software version AS907_1001 in any 

AS907–1–1A engine. 

(2) Do not install an ECU having P/N 

2119576–3001 or P/N 2119576–3002 in any 

AS907–2–1G engine if the ECU has exceeded 

the compliance time specified in Table 2 to 

paragraph (g)(2) of this AD. 

(i) Definitions 

(1) For the purpose of this AD, for the 

AS907–1–1A engine, a ‘‘software version 

eligible for installation’’ is a software version 

that is not software version AS907_1001. 

(2) For the purpose of this AD, for the 

AS907–1–1A engine, an ‘‘ECU eligible for 

installation’’ is an ECU that does not have P/ 

N 2119576–1011. 

(3) For the purpose of this AD, for the 

AS907–2–1G engine, an ‘‘ECU eligible for 

installation’’ is an ECU that does not have P/ 

N 2119576–3001 or P/N 2119576–3002. 

(j) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, West Certification 

Branch, 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 West Certification 

Branch, send it to the attention of the person 

identified in paragraph (k) of this AD and 

email to: 9-ANM-LAACO-AMOC-Requests@

faa.gov. 

(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. 

(k) Additional Information 

For more information about this AD, 

contact Joseph Costa, Aviation Safety 

Engineer, FAA, 3960 Paramount Boulevard, 

Lakewood, CA 90712; phone: (562) 627– 

5246; email: joseph.costa@faa.gov. 

(l) Material Incorporated by Reference 

None. 

Issued on November 29, 2023. 

Victor Wicklund, 

Deputy Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2023–26636 Filed 12–5–23; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2023–1719; Project 

Identifier 2008–NM–202–AD; Amendment 

39–22621; AD 2010–26–05R1] 

RIN 2120–AA64 

Airworthiness Directives; Dassault 

Aviation Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; removal. 

SUMMARY: The FAA is removing 

Airworthiness Directive (AD) 2010–26– 

05, which applied to certain Dassault 

Aviation Model Falcon 10 airplanes; 

Model FAN JET FALCON, FAN JET 

FALCON SERIES C, D, E, F, and G 

airplanes; Model MYSTERE–FALCON 

20–C5, 20–D5, 20–E5, and 20–F5 

airplanes; and all Model MYSTERE– 

FALCON 200 airplanes; Model FALCON 

2000 and FALCON 2000EX airplanes; 

Model MYSTERE–FALCON 50 and 

MYSTERE–FALCON 900 airplanes; and 

Model FALCON 900EX airplanes. AD 

2010–26–05 required repetitive 

inspections for overpressure tightness 

on the pressurization control regulating 

valves and, if necessary, replacing the 

affected valve with a serviceable unit. 

The FAA issued AD 2010–26–05 to 

address failure of the pressurization 

control regulating valve (overpressure 

capsule), which will affect the aircraft’s 

overpressure protection. Since the FAA 

issued AD 2010–26–05, the FAA issued 

ADs 2021–04–20, 2020–02–13, 2020– 

03–24, 2020–03–19, 2020–01–13, 2023– 

05–15, 2023–04–10, 2023–02–13, 2023– 

04–18, and 2023–04–13 to address the 

unsafe condition. Therefore, the FAA 

has determined that AD 2010–26–05 is 

no longer necessary. Accordingly, AD 

2010–26–05 is removed. 

DATES: This AD becomes effective 

December 6, 2023. 

ADDRESSES: 

AD Docket: You may examine the AD 

docket at regulations.gov under Docket 

No. FAA–2023–1719; or in person at 

Docket Operations between 9 a.m. and 

5 p.m., Monday through Friday, except 

Federal holidays. The AD docket 

contains this final rule, the mandatory 

continuing airworthiness information 

(MCAI), any comments received, and 

other information. The address for 

Docket Operations is U.S. Department of 

Transportation, Docket Operations, M– 


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84694 Federal Register / Vol. 88, No. 233 / Wednesday, December 6, 2023 / Rules and Regulations 

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue SE, 

Washington, DC 20590. 

FOR FURTHER INFORMATION CONTACT: Tom 

Rodriguez, Aviation Safety Engineer, 

FAA, 1600 Stewart Avenue, Suite 410, 

Westbury, NY 11590; telephone: 206– 

231–3226; email: tom.rodriguez@

faa.gov. 

SUPPLEMENTARY INFORMATION: 

Background 

The FAA issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by removing AD 2010–26–05, 

Amendment 39–16544 (75 FR 79952, 

December 21, 2010) (AD 2010–26–05). 

The NPRM was published in the 

Federal Register on August 29, 2023 (88 

FR 59471). AD 2010–26–05 applied to 

certain Dassault Aviation Model Falcon 

10 airplanes; Model FAN JET FALCON, 

FAN JET FALCON SERIES C, D, E, F, 

and G airplanes; Model MYSTERE– 

FALCON 20–C5, 20–D5, 20–E5, and 20– 

F5 airplanes; and all Model FALCON 

2000 and FALCON 2000EX airplanes; 

Model MYSTERE–FALCON 200 

airplanes; Model MYSTERE–FALCON 

50 and MYSTERE–FALCON 900 

airplanes, and Model FALCON 900EX 

airplanes. AD 2010–26–05 was 

prompted by AD 2008–0072, dated 

April 18, 2008, issued by the European 

Union Aviation Safety Agency (EASA), 

which is the Technical Agent for the 

Member States of the European Union 

(EASA AD 2008–0072) (also referred to 

as the MCAI). The NPRM was prompted 

by a determination that AD 2010–26–05 

is no longer necessary, because the 

actions specified in the MCAI have been 

included in the airworthiness 

limitations section of the existing 

maintenance manual. EASA issued AD 

2008–0072–CN, dated October 5, 2020, 

which cancels EASA AD 2008–0072. 

Additionally, the FAA has issued the 

following ADs to address the unsafe 

condition by revising the existing 

maintenance or inspection program, as 

applicable, to incorporate new or more 

restrictive maintenance requirements 

and airworthiness limitations, including 

the actions specified in AD 2010–26–05. 

• AD 2021–04–20, Amendment 39– 

21442 (86 FR 12802, March 5, 2021), 

which addresses the unsafe condition 

for Model Falcon 10 airplanes. 

• AD 2020–02–13, Amendment 39– 

19827 (85 FR 6744, February 6, 2020), 

which addresses the unsafe condition 

for Model FAN JET FALCON, FAN JET 

FALCON SERIES C, D, E, F, and G 

airplanes on which the supplemental 

structural inspection program (SSIP) has 

been incorporated into the airplane’s 

maintenance program. 

• AD 2020–03–24, Amendment 39– 

19848 (85 FR 11289, February 27, 2020), 

which addresses the unsafe condition 

for Model MYSTERE–FALCON 20–C5, 

20–D5, 20–E5, and 20–F5 airplanes on 

which the SSIP (Dassault Service 

Bulletin 730) has been embodied into 

the airplane’s existing maintenance or 

inspection program. 

• AD 2020–03–19, Amendment 39– 

19843 (85 FR 11280, February 27, 2020), 

which address the unsafe condition for 

Model MYSTERE–FALCON 20–C5, 20– 

D5, 20–E5, and 20–F5 airplanes, except 

those on which the SSIP (Dassault 

Service Bulletin 730) has been 

embodied into the airplane’s existing 

maintenance or inspection program. 

• AD 2020–01–13, Amendment 39– 

19819 (85 FR 5313, January 30, 2020), 

which addresses the unsafe condition 

for Model MYSTERE–FALCON 200 

airplanes. 

• AD 2023–05–15, Amendment 39– 

22384 (88 FR 22374, April 13, 2023), 

which addresses the unsafe condition 

for Model MYSTERE–FALCON 50 

airplanes. 

• AD 2023–04–10, Amendment 39– 

22357 (88 FR 20743, April 7, 2023), 

which addresses the unsafe condition 

for Model MYSTERE–FALCON 900 

airplanes. 

• AD 2023–02–13, Amendment 39– 

22320 (88 FR 8740, February 10, 2023), 

which addresses the unsafe condition 

for Model FALCON 900EX airplanes. 

• AD 2023–04–18, Amendment 39– 

22365 (88 FR 15607, March 14, 2023), 

which addresses the unsafe condition 

for Model FALCON 2000 airplanes. 

• AD 2023–04–13, Amendment 39– 

22360 (88 FR 20741, April 7, 2023), 

which addresses the unsafe condition 

for Model FALCON 2000EX airplanes. 

The NPRM proposed to remove AD 

2010–26–05. The FAA is issuing this 

AD to remove AD 2010–26–05. 

Discussion of Final Airworthiness 

Directive 

Comments 

The FAA received no comments on 

the NPRM or on the determination of 

the cost to the public. 

Justification for Immediate Adoption 

and Determination of the Effective Date 

Section 553(b)(3)(B) of the 

Administrative Procedure Act (APA) (5 

U.S.C. 551 et seq.) authorizes agencies 

to dispense with notice and comment 

procedures for rules when the agency, 

for ‘‘good cause,’’ finds that those 

procedures are ‘‘impracticable, 

unnecessary, or contrary to the public 

interest.’’ Under this section, an agency, 

upon finding good cause, may issue a 

final rule without providing notice and 

seeking comment prior to issuance. 

Further, section 553(d) of the APA 

authorizes agencies to make rules 

effective in less than 30 days, upon a 

finding of good cause. Since the FAA 

issued AD 2010–26–05, the actions 

specified in the MCAI have been 

included in the airworthiness 

limitations section of the existing 

maintenance manual, and the FAA has 

issued ADs to require the incorporation 

of those airworthiness limitations. 

Therefore, the FAA is issuing this AD to 

remove AD 2010–26–05, and the FAA 

did not receive any adverse comments 

or useful information about this AD 

from U.S. operators that necessitates 

waiting 30 days for relief from this 

requirement. Accordingly, the FAA 

finds that good cause exists pursuant to 

5 U.S.C. 553(d) for making this 

amendment effective in less than 30 

days. 

Conclusion 

The FAA reviewed the relevant data 

and determined that air safety requires 

adopting this AD as proposed. Except 

for minor editorial changes, this AD is 

adopted as proposed in the NPRM. 

None of the changes will increase the 

economic burden on any operator. 

This AD removes all actions of AD 

2010–26–05. Therefore, the 

requirements of AD 2010–26–05 are 

terminated. 

Related Costs of Compliance 

This AD adds no costs. This AD 

removes AD 2010–26–05 from 14 CFR 

part 39; therefore, operators are no 

longer required to show compliance 

with that AD. 

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. 

The FAA is 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 


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Federal Register / Vol. 88, No. 233 / Wednesday, December 6, 2023 / Rules and Regulations 84695 

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. 

Regulatory Findings 

The FAA 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) Will not affect intrastate aviation 

in Alaska, and 

(3) 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. 

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: 

■ a. Removing Airworthiness Directive 

(AD) 2010–26–05, Amendment 39– 

16544 (75 FR 79952, December 21, 

2010), and 

■ b. Adding the following new AD: 

2010–26–05R1 Dassault Aviation: 

Amendment 39–22621; Docket No. 

FAA–2023–1719; Project Identifier AD– 

2008–NM–202–AD. 

(a) Effective Date 

This AD is effective December 6, 2023. 

(b) Affected AD 

This AD replaces AD 2010–26–05, 

Amendment 39–16544 (75 FR 79952, 

December 21, 2010) (AD 2010–26–05). 

(c) Applicability 

This action applies to the airplanes 

identified in paragraphs (c)(1) and (2) of this 

AD, certificated in any category. 

(1) Dassault Aviation Model Falcon 10 

airplanes; Model FAN JET FALCON, FAN 

JET FALCON SERIES C, D, E, F, and G 

airplanes; and Model MYSTERE–FALCON 

20–C5, 20–D5, 20–E5, and 20–F5 airplanes; 

all serial numbers, equipped with Liebherr or 

ABG-Semca pressurization outflow valves. 

(2) Dassault Aviation Model MYSTERE– 

FALCON 200 airplanes, Model MYSTERE– 

FALCON 50 and MYSTERE–FALCON 900 

airplanes, and FALCON 900EX airplanes; 

and Model FALCON 2000 and FALCON 

2000EX airplanes; all serial numbers. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 21, Air conditioning. 

(e) Terminating Action 

This AD terminates all requirements of AD 

2010–26–05. 

(f) Related Information 

For more information about this AD, 

contact Tom Rodriguez, Aviation Safety 

Engineer, FAA, 1600 Stewart Avenue, Suite 

410, Westbury, NY 11590; telephone: 206– 

231–3226; email: tom.rodriguez@faa.gov. 

(g) Material Incorporated by Reference 

None. 

Issued on November 29, 2023. 

Victor Wicklund, 

Deputy Director, Compliance & Airworthiness 

Division, Aircraft Certification Service. 

[FR Doc. 2023–26662 Filed 12–5–23; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 73 

[Docket No. FAA–2023–2220; Airspace 

Docket No. 23–AWP–59] 

RIN 2120–AA66 

Amendment of Restricted Area R–2512 

Holtville, CA 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: This action corrects a final 

rule published by the FAA in the 

Federal Register on November 16, 2023, 

that amends restricted area R–2512 in 

the vicinity of Holtville, CA. 

DATES: Effective date 0901 UTC, January 

25, 2024. 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 7400.10 and publication of 

conforming amendments. 

ADDRESSES: A copy of the Notice of 

Proposed Rulemaking (NPRM), all 

comments received, the final rule, this 

final rule correction, and all background 

material may be viewed online at 

www.regulations.gov using the FAA 

Docket number. Electronic retrieval help 

and guidelines are available on the 

website. It is available 24 hours each 

day, 365 days each year. 

FAA Order JO 7400.11H, Airspace 

Designations and Reporting Points, and 

subsequent amendments can be viewed 

online at www.faa.gov/air_traffic/ 

publications/. You may also contact the 

Rules and Regulations Group, Office of 

Policy, Federal Aviation 

Administration, 800 Independence 

Avenue SW, Washington, DC 20591; 

telephone: (202) 267–8783. 

FOR FURTHER INFORMATION CONTACT: 

Steven Roff, Rules and Regulations 

Group, Office of Policy, Federal 

Aviation Administration, 800 

Independence Avenue SW, Washington, 

DC 20591; telephone: (202) 267–8783. 

SUPPLEMENTARY INFORMATION: 

History 

The FAA published a final rule in the 

Federal Register for Docket No. FAA– 

2023–2220 (88 FR 78636; November 16, 

2023), that amended restricted area R– 

2512 in the vicinity of Holtville, CA. 

The section of 14 CFR part 73 to be 

amended by the final rule was 

incorrectly stated as 73.22. The correct 

section of 14 CFR part 73 to be amended 

is 73.25. This rule corrects this 

typographical error. 

Correction to Final Rule 

Accordingly, pursuant to the 

authority delegated to me, the airspace 

amendment reflected in Docket No. 

FAA–2023–2220, as published in the 

Federal Register of November 16, 2023 

(88 FR 78636), FR Doc. 2023–25347, is 

corrected as follows: 

§ 73.25 [Amended] 

■ 2. Section 73.25 is amended as 

follows: 

* * * * * 

R–2512 Holtville, CA [Amended] 

Boundaries. Beginning at lat. 

33°05′00′′ N, long. 115°17′33′′ W; to lat. 

33°00′00′′ N, long. 115°13′33′′ W; to lat. 

32°51′00′′ N, long. 115°05′33′′ W; to lat. 

32°51′00′′ N, long. 115°17′03′′ W; to lat. 

32°58′00′′ N, long. 115°17′33′′ W; to lat. 

33°05′00′′ N, long. 115°20′03′′ W; to the 

point of beginning. 

Designated altitudes. Surface to 

23,000 feet MSL. 

Time of designation. 0600–2300 local 

time daily; other times by NOTAM 24 

hours in advance. 

Controlling agency. FAA, Los Angeles 

ARTCC. 


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