Federal Register / Vol. 73, No. 153 / Thursday, August 7, 2008 / Rules and Regulations 45857 

* * * * * 

PART 352—NONDISCRIMINATION ON 

THE BASIS OF DISABILITY 

■ 3. The authority citation for part 352 

continues to read as follows: 

Authority: 12 U.S.C. 1819(a); 29 U.S.C. 

794d. 

■ 4. The second and third sentences of 

§ 352.9(b) are revised to read as follows: 

§ 352.9 Communications. 

* * * * * 

(b) * * * Interested persons may 

obtain such information by calling, 

writing or visiting the FDIC Office of 

Diversity and Economic Opportunity 

(ODEO), located at 3501 Fairfax Drive, 

Arlington, VA 22226. The FDIC 

telephone number is (877) 275–3342 or 

(703) 562–2473 (TTY). 

* * * * * 

■ 5. The last sentence of § 352.10(c) is 

revised to read as follows: 

§ 352.10 Compliance procedures. 

* * * * * 

(c) * * * All complaints should be 

sent to the FDIC’s Office of Diversity 

and Economic Opportunity, 3501 

Fairfax Drive, Arlington, VA 22226. 

* * * * * 

Dated this 31st day of July, 2008. 

Federal Deposit Insurance Corporation. 

Robert E. Feldman, 

Executive Secretary. 

[FR Doc. E8–18052 Filed 8–6–08; 8:45 am] 

BILLING CODE 6714–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2008–0837; Directorate 

Identifier 2008–CE–043–AD; Amendment 

39–15633; AD 2008–16–15] 

RIN 2120–AA64 

Airworthiness Directives; Eclipse 

Aviation Corporation Model EA500 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; request for 

comments. 

SUMMARY: The FAA is superseding 

emergency Airworthiness Directive (AD) 

2008–13–51, which currently applies to 

all owners/operators of Eclipse Aviation 

Corporation (Eclipse) Model EA500 

airplanes that received the emergency 

AD by letter issued June 12, 2008. 

Emergency AD 2008–13–51 requires 

owner/operators to insert temporary 

revisions into the emergency and 

normal procedures sections of the 

airplane flight manual (AFM), do a pilot 

evaluation of the throttles with 

replacement as necessary, and report the 

evaluation results to the FAA. 

Emergency AD 2008–13–51 was the 

result of the throttle position exceeding 

its maximum range. Since issuing that 

AD, Eclipse developed an FAAapproved test procedure and issued 

Eclipse Aviation Alert Service Bulletin 

SB 500–76–001, REV B, dated July 22, 

2008. The service bulletin provides a 

standardized procedure for testing and 

modifying (as applicable) the throttle 

lever with replacement as necessary. We 

are issuing this AD to mandate the 

actions in this service bulletin to be 

done by a person authorized to perform 

maintenance and reduce the likelihood 

of the throttle position signal exceeding 

its maximum range, which could cause 

loss of left and right engine control. This 

condition could result in the inability to 

maintain desired airspeed and/or 

altitude with consequent loss of control. 

DATES: This AD becomes effective on 

August 7, 2008. 

On August 7, 2008, the Director of the 

Federal Register approved the 

incorporation by reference of certain 

publications listed in this AD. 

We must receive any comments on 

this AD by October 6, 2008. 

ADDRESSES: Use one of the following 

addresses to comment on this AD. 

• Federal eRulemaking Portal: Go to 

http://www.regulations.gov. Follow the 

instructions for submitting comments. 

• Fax: (202) 493–2251. 

• Mail: U.S. Department of 

Transportation, Docket Operations, M–

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue, SE., 

Washington, DC 20590. 

• Hand Delivery: U.S. Department of 

Transportation, Docket Operations, M–

30, West Building Ground Floor, Room 

W12–140, 1200 New Jersey Avenue, SE., 

Washington, DC 20590, between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. 

To get the service information 

identified in this AD, contact Eclipse 

Aviation Corporation, 2503 Clark Carr 

Loop, SE., Albuquerque, New Mexico 

87106; telephone: (505) 724–1200. 

To view the comments to this AD, go 

to http://www.regulations.gov. The 

docket number is FAA–2008–0837; 

Directorate Identifier 2008–CE–043–AD. 

FOR FURTHER INFORMATION CONTACT: 

Mitchell Soth, Aerospace Engineer, 

FAA, Forth Worth Airplane 

Certification Office, 2601 Meacham 

Blvd., Fort Worth, Texas 76137; 

telephone: (817) 222–5104; fax: (817) 

222–5960. 

SUPPLEMENTARY INFORMATION: 

Discussion 

Following a wind shear encounter on 

final approach, the pilot of an Eclipse 

Model EA500 airplane applied full 

throttle using enough force against the 

forward stops to exceed the design 

throttle position signal maximum range. 

The associated fault mode held the 

engine thrust settings at the last known 

throttle position, which was maximum. 

Following the balked landing, the 

pilot elected to shutdown one engine. 

Upon shutdown of the one engine, the 

opposite engine thrust reduced to idle 

and was unresponsive to subsequent 

throttle lever movement. The pilot was 

able to land the airplane with no injury 

or substantial damage. Both main tires 

were blown during the event. 

Exceeding the throttle position signal 

maximum range could cause loss of left 

and right engine control, which could 

result in the inability to maintain 

desired airspeed and/or altitude with 

consequent loss of control. 

On June 12, 2008, the FAA issued 

emergency AD 2008–13–51 to require 

owner/operators to insert the following 

into emergency and normal procedures 

sections of the EA500 pilots operating 

handbook (POH) and airplane flight 

manual (AFM), as applicable: 

• Temporary Revision No. 005 To 

EA500 POH and FAA-Approved 

Airplane Flight Manual, L & R ENG 

CONTROL FAIL, AFM part number (P/ 

N) 06–122204, dated June 12, 2008; 

• Temporary Revision No. 006 To 

EA500 POH and FAA-Approved 

Airplane Flight Manual, THROTTLE 

STOPS, AFM P/N 06–122204, dated 

June 12, 2008; 

• Temporary Revision No. 007 To 

EA500 POH and FAA-Approved 

Airplane Flight Manual, L & R ENG 

CONTROL FAIL, AFM P/N 06–121654, 

dated June 12, 2008; 

• Temporary Revision No. 008 To 

EA500 POH and FAA-Approved 

Airplane Flight Manual, THROTTLE 

STOPS, AFM P/N 06–121654, dated 

June 12, 2008; 

• Temporary Revision No. 013 To 

EA500 POH and FAA-Approved 

Airplane Flight Manual, L & R ENG 

CONTROL FAIL, AFM P/N 06–100106, 

dated June 12, 2008; and 

• Temporary Revision No. 014 To 

EA500 POH and FAA-Approved 

Airplane Flight Manual, THROTTLE 

STOPS, AFM P/N 06–100106, dated 

June 12, 2008. 

The emergency AD also required an 

evaluation of the throttles with 


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45858 Federal Register / Vol. 73, No. 153 / Thursday, August 7, 2008 / Rules and Regulations 

replacement as necessary and a report of 

the evaluation results to the FAA. 

Emergency AD 2008–13–51 allowed 

the pilot to do the evaluation of the 

throttle. The FAA has since determined 

that the throttles must be inspected and 

modified (as applicable) by a person 

authorized to perform maintenance as 

specified in 14 CFR section 43.3 of the 

Federal Aviation Administration 

Regulations (14 CFR 43.3) following 

Eclipse Aviation Alert Service Bulletin 

SB 500–76–001, REV B, dated July 22, 

2008. The FAA has also determined the 

reporting requirement is no longer 

necessary. 

Relevant Service Information 

We reviewed Eclipse Aviation Alert 

Service Bulletin SB 500–76–001, REV B, 

dated July 22, 2008. The service 

information describes procedures for 

inspecting and modifying (as 

applicable) the throttles with 

replacement as necessary. 

FAA’s Determination and Requirements 

of This AD 

We are issuing this AD because we 

evaluated all the information and 

determined the unsafe condition 

described previously is likely to exist or 

develop on other products of the same 

type design. This AD supersedes 

emergency AD 2008–13–51 and requires 

the following: 

• Inserting the above-mentioned 

temporary revisions into the appropriate 

AFM; and 

• Inspecting and modifying (as 

applicable) the throttles with 

replacement as necessary. 

This is considered interim action. We 

may take future rulemaking action. 

FAA’s Determination of the Effective 

Date 

Since an unsafe condition exists that 

requires the immediate adoption of this 

AD, we determined that notice and 

opportunity for public comment before 

issuing this AD are impracticable, and 

that good cause exists for making this 

amendment effective in fewer than 30 

days. 

Comments Invited 

This AD is a final rule that involves 

requirements affecting flight safety, and 

we did not precede it by notice and an 

opportunity for public comment. We 

invite you to send any written relevant 

data, views, or arguments regarding this 

AD. Send your comments to an address 

listed under the ADDRESSES section. 

Include the docket number ‘‘FAA–

2008–0837; Directorate Identifier 2008–

CE–043–AD’’ at the beginning of your 

comments. We specifically invite 

comments on the overall regulatory, 

economic, environmental, and energy 

aspects of the AD. We will consider all 

comments received by the closing date 

and may amend the AD in light of those 

comments. 

We will post all comments we 

receive, without change, to http:// 

www.regulations.gov, including any 

personal information you provide. We 

will also post a report summarizing each 

substantive verbal contact we receive 

concerning this 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. 

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 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979); 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. 

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 that 

contains the AD, the regulatory 

evaluation, any comments received, and 

other information on the Internet at 

http://www.regulations.gov; or in person 

at the Docket Management Facility 

between 9 a.m. and 5 p.m., Monday 

through Friday, except Federal holidays. 

The Docket Office (telephone (800) 647–

5527) is located at the street address 

stated 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 adding 

a new AD to read as follows: 

2008–16–15 Eclipse Aviation Corporation: 

Amendment 39–15633; Docket No. 

FAA–2008–0837; Directorate Identifier 

2008–CE–043–AD. 

Effective Date 

(a) This AD becomes effective on August 7, 

2008. 

Affected ADs 

(b) This AD supersedes emergency AD 

2008–13–51, which was sent by individual 

letter issued June 12, 2008, to owners/ 

operators of Eclipse Model EA500 airplanes. 

Applicability 

(c) This AD affects Model EA500 airplanes, 

all serial numbers, that are certificated in any 

category. 

Unsafe Condition 

(d) This AD is the result of the throttle 

position exceeding its maximum range. We 

are issuing this AD to reduce the likelihood 

of the throttle position signal exceeding its 

maximum range, which could cause loss of 

left and right engine control. This condition 

could result in the inability to maintain 

desired airspeed and/or altitude with 

consequent loss of control. 

Compliance 

(e) To address this problem, you must do 

the following, unless already done: 


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Federal Register / Vol. 73, No. 153 / Thursday, August 7, 2008 / Rules and Regulations 45859 

Actions Compliance Procedures 

(1) Insert the following into the emergency and 

normal procedures sections of the applicable 

EA500 pilots operating handbook (POH) and 

airplane flight manual (AFM): 

(i) For POH/AFM part number (P/N) 06– 

122204: Temporary Revision No. 005 To 

EA500 POH and FAA-Approved Airplane 

Flight Manual, L & R ENG CONTROL 

FAIL, dated June 12, 2008; and Temporary 

Revision No. 006 To EA500 POH and 

FAA-Approved Airplane Flight Manual, 

THROTTLE STOPS, dated June 12, 2008. 

Before further flight after August 7, 2008 (the 

effective date of this AD). If you previously 

did this action per compliance with emergency AD 2008–13–51, then you may take 

‘‘unless already done’’ credit for this portion 

of the AD. 

Under 14 CFR section 43.7 of the Federal 

Aviation Administration Regulations (14 

CFR 43.7), the owner/operator holding at 

least a private pilot certificate is allowed to 

insert the AFM temporary revisions. Make 

an entry into the aircraft logbook showing 

compliance with this portion of the AD per 

compliance with section 43.9 of the Federal 

Aviation Regulations (14 CFR 43.9). 

(ii) For POH/AFM P/N 06–121654: Temporary Revision No. 007 To EA500 POH 

and FAA-Approved Airplane Flight Manual, 

L & R ENG CONTROL FAIL, dated June 

12, 2008; and Temporary Revision No. 008 

To EA500 POH and FAA-Approved Airplane Flight Manual, THROTTLE STOPS, 

dated June 12, 2008. 

(iii) For POH/AFM P/N 06–100106: Temporary Revision No. 013 To EA500 POH 

and FAA-Approved Airplane Flight Manual, 

L & R ENG CONTROL FAIL, dated June 

12, 2008; and Temporary Revision No. 

014, To EA500 POH and FAA-Approved 

Airplane Flight Manual, THROTTLE 

STOPS, dated June 12, 2008. 

(2) For POH/AFM P/N 06–122204, inserting 

Section 3, Emergency Procedures, Revision 

1, dated June 25, 2008; and Section 4, Normal Procedures, Revision 1, dated June 25, 

2008, satisfies the requirement specified in 

paragraph (e)(1)(i) of this AD. 

Before further flight after August 7, 2008 (the 

effective date of this AD). 

Under 14 CFR section 43.7 of the Federal 

Aviation Administration Regulations (14 

CFR 43.7), the owner/operator holding at 

least a private pilot certificate is allowed to 

insert the AFM temporary revisions. Make 

an entry into the aircraft logbook showing 

compliance with this portion of the AD per 

compliance with section 43.9 of the Federal 

Aviation Regulations (14 CFR 43.9). 

(3) Inspect and modify (as applicable) the throttle quadrant assembly (TQA). (i) If you have done all the actions of emergency AD 2008–13–51 before August 7, 

2008 (the effective date of this AD), an appropriately-licensed mechanic must do the 

inspection required by this AD at whichever 

of the following occurs first: 

Follow the instructions in Eclipse Aviation 

Alert Service Bulletin SB 500–76–001, REV 

B, dated July 22, 2008. 

(A) No later than the next maintenance check; 

or 

(B) Within the next 60 days after August 7, 

2008 (the effective date of this AD). 

(ii) If you have not done all of the actions of 

emergency AD 2008–13–51 as of August 7, 

2008 (the effective date of this AD), an appropriately-licensed mechanic must do the 

inspection required by this AD before further flight after August 7, 2008 (the effective 

date of this AD). You may operate the airplane up to 10 hours time-in-service to 

reposition the airplane to the service center 

or maintenance facility doing the inspection 

provided the flight(s) occur(s) within 30 

days after August 7, 2008 (the effective 

date of this AD). 

(4) If any TQA fails the inspection required in 

paragraph (e)(3) of this AD, replace the TQA 

with a TQA that passes the test procedure 

set forth in Eclipse Aviation Alert Service Bulletin SB 500–76–001, REV B, dated July 22, 

2008. 

Before further flight after the inspection where 

any TQA failed. 

Replace the TQA using FAA-approved procedures. Contact the FAA at the address in 

paragraph (f) of this AD for an FAA-approved procedure. 

Note: To get copies of the temporary 

revisions specified in this AD, contact 

Eclipse Aviation Corporation, 2503 Clark 

Carr Loop, SE., Albuquerque, NM 87105, fax: 

505–241–8802; e-mail: 

customercare@eclipseaviation.com. 

Alternative Methods of Compliance 

(f) The Manager, Fort Worth Airplane 

Certification Office, FAA, ATTN: Mitchell 

Soth, FAA, 2601 Meacham Blvd, Fort Worth, 


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45860 Federal Register / Vol. 73, No. 153 / Thursday, August 7, 2008 / Rules and Regulations 

Texas 76137; telephone: (817) 222–5104; fax: 

(817) 222–5960, has the authority to approve 

AMOCs for this AD, if requested using the 

procedures found in 14 CFR 39.19. Before 

using any approved AMOC on any airplane 

to which the AMOC applies, notify your 

appropriate principal inspector (PI) in the 

FAA Flight Standards District Office (FSDO), 

or lacking a PI, your local FSDO. 

Material Incorporated by Reference 

(g) You must use Eclipse Aviation Alert 

Service Bulletin SB 500–76–001, REV B, 

dated July 22, 2008, to do the actions 

required by this AD, unless the AD specifies 

otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

this service information under 5 U.S.C. 

552(a) and 1 CFR part 51. 

(2) For service information identified in 

this AD, contact Eclipse Aviation 

Corporation, 2503 Clark Carr Loop, SE., 

Albuquerque, NM 87105, fax: 505–241–8802; 

e-mail: customercare@eclipseaviation.com. 

(3) You may review copies at the FAA, 

Central Region, Office of the Regional 

Counsel, 901 Locust, Room 506, Kansas City, 

Missouri 64106; or 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/ibr-locations.html. 

Issued in Kansas City, Missouri, on July 29, 

2008. 

James E. Jackson, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. E8–17786 Filed 8–6–08; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 97 

[Docket No. 30620; Amdt. No 3280] 

Standard Instrument Approach 

Procedures, and Takeoff Minimums 

and Obstacle Departure Procedures; 

Miscellaneous Amendments 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This Rule establishes, 

amends, suspends, or revokes 

STANDARD Instrument Approach 

Procedures (SIAPs) and associated 

Takeoff Minimums and Obstacle 

Departure Procedures for operations at 

certain airports. These regulatory 

actions are needed because of the 

adoption of new or revised criteria, or 

because of changes occurring in the 

National Airspace System, such as the 

commissioning of new navigational 

facilities, adding new obstacles, or 

changing air traffic requirements. These 

changes are designed to provide safe 

and efficient use of the navigable 

airspace and to promote safe flight 

operations under instrument flight rules 

at the affected airports. 

DATES: This rule is effective August 7, 

2008. The compliance date for each 

SIAP, associated Takeoff Minimums, 

and ODP is specified in the amendatory 

provisions. 

The incorporation by reference of 

certain publications listed in the 

regulations is approved by the Director 

of the Federal Register as of August 7, 

2008. 

ADDRESSES: Availability of matters 

incorporated by reference in the 

amendment is as follows: 

For Examination—

1. FAA Rules Docket, FAA 

Headquarters Building, 800 

Independence Avenue, SW., 

Washington, DC 20591; 

2. The FAA Regional Office of the 

region in which the affected airport is 

located; 

3. The National Flight Procedures 

Office, 6500 South MacArthur Blvd., 

Oklahoma City, OK 73169 or 

4. 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/ 

code_of_federal_regulations/ 

ibr_locations.html. 

Availability—All SIAPs and Takeoff 

Minimums and ODPs are Available 

online free of charge. Visit nfdc.faa.gov 

to register. Additionally, individual 

SIAP and Takeoff Minimums and ODP 

copies may be obtained from: 

1. FAA Public Inquiry Center (APA–

200), FAA Headquarters Building, 800 

Independence Avenue, SW., 

Washington, DC 20591; or 

2. The FAA Regional Office of the 

region in which the affected airport is 

located. 

FOR FURTHER INFORMATION CONTACT: 

Harry J. Hodges, Flight Procedure 

Standards Branch (AFS–420), Flight 

Technologies and Programs Divisions, 

Flight Standards Service, Federal 

Aviation Administration, Mike 

Monroney Aeronautical Center, 6500 

South MacArthur Blvd., Oklahoma City, 

OK 73169 (Mail Address: P.O. Box 

25082, Oklahoma City, OK 73125) 

Telephone: (405) 954–4164. 

SUPPLEMENTARY INFORMATION: This rule 

amends Title 14 of the Code of Federal 

Regulations, Part 97 (14 CFR part 97), by 

Establishing, amending, suspending, or 

revoking SIAPS, Takeoff Minimums 

and/or ODPS. The complete regulators 

description of Each SIAP and its 

associated Takeoff Minimums or ODP 

for an Identified airport is listed on FAA 

form documents which are Incorporated 

by reference in this amendment under 5 

U.S.C. 552(a), 1 CFR part 51, and 14 

CFR part 97.20. The applicable FAA 

Forms are FAA Forms 8260–3, 8260–4, 

8260–5, 8260–15A, and 8260–15B when 

required by an entry on 8260–15A. 

The large number of SIAPs, Takeoff 

Minimums and ODPs, in addition to 

their complex nature and the need for 

a special format make publication in the 

Federal Register expensive and 

impractical. Furthermore, airmen do not 

use the regulatory text of the SIAPs, 

Takeoff Minimums or ODPs, but instead 

refer to their depiction on charts printed 

by publishers of aeronautical materials. 

This, the advantages of incorporation by 

reference are realized and publication of 

the complete description of each SIAP, 

Takeoff Minimums and ODP listed on 

FAA forms is unnecessary. This 

amendment provides the affected CFR 

sections and specifies the types of SIAPs 

and the effective dates of the Associated 

Takeoff Minimums and ODPs. This 

amendment also identifies the airport 

and its location, the procedure, and the 

amendment number. 

The Rule 

This amendment to 14 CFR part 97 is 

effective upon publication of each 

separate SIAP, Takeoff Minimums and 

ODP as contained in the transmittal. 

Some SIAP and Takeoff Minimums and 

textual ODP amendments may have 

been issued previously by the FAA in a 

Flight Data Center (FDC) Notice to 

Airmen (NOTAM) as an emergency 

action of immediate flight safety relating 

directly to published aeronautical 

charts. The circumstances which 

created the need for some SIAP and 

Takeoff Minimums and ODP 

amendments may require making them 

effective in less than 30 days. For the 

remaining SIAPS and Takeoff 

Minimums and ODPS, an effective date 

at least 30 days after publication is 

provided. 

Further, the SIAPs and Takeoff 

Minimums and ODPS contained in this 

amendment are based on the criteria 

contained in the U.S. Standard for 

Terminal Instrument Procedures 

(TERPS). In developing these SIAPS and 

Takeoff Minimums and ODPs, the 

TERPS criteria were applied to the 

conditions existing or anticipated at the 

affected airports. Because of the close 

and immediate relationship between 

these SIAPs, Takeoff Minimums and 

ODPs, and safety in air commerce, I find 

that notice and public procedures before 

adopting these SIAPS, Takeoff 


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