Airworthiness Directives; Eclipse Aviation Corporation Model EA500 Airplanes, 46542 [E8-18227]

Download as PDF jlentini on PROD1PC65 with RULES 46542 Federal Register / Vol. 73, No. 155 / Monday, August 11, 2008 / Rules and Regulations cargo compartment is occupied. There must be a placard located on or adjacent to the cargo door instructing occupants that the door must be closed and latched at all times except when someone is in the cargo compartment. This placard must also instruct the person entering the cargo compartment to keep the door open when they are in the cargo compartment and to immediately close and latch the door when they exit the cargo compartment. 3. There must be a (on/off) visual advisory/warning stating ‘‘Do Not Enter’’ (or similar words) to be located outside of and on or near the main entry door/hatch to the main deck cargo compartment. The advisory/warning is to be controlled from the flight deck. 4. There must be an aural and visual warning provided in the baggage compartment to alert an occupant when an oxygen mask must be donned immediately. 5. Oxygen dispensing units must be automatically presented and immediately available to an occupant(s) of the baggage compartment when they exit the compartment. For these special conditions, immediately available means the oxygen dispensing units are located in the passenger cabin near the main entry door/hatch to the main deck cargo compartment (no oxygen supply lines are allowed to be routed into the compartment). The number of oxygen dispensing units must be equal to the number of occupants allowed in the cargo compartment. There must be a placard located on or adjacent to the cargo door instructing occupants of the maximum number of occupants allowed in the cargo compartment. 6. For cargo and baggage placed in the baggage compartment whose primary retention means is by net, the net must be constructed so that the means of opening and closing or securing the net is easily identified and operated. 7. These special conditions apply to main deck accessible Class C cargo compartments with volumes of 10 m3 or less. Class C cargo compartments that are accessible to passengers with a volume greater than 10 m3 may be approved, but would likely require additional limitations or provisions to mitigate the larger volume. Note that there may also be a maximum volume above which access is not acceptable. 8. Operational limitations: The airplane has operational limitations associated with the level of screening required for baggage/cargo that is placed in the in-flight accessible Class C cargo compartment. These limitations must be documented in the Airplane Flight Manual (AFM). VerDate Aug<31>2005 15:34 Aug 08, 2008 Jkt 214001 (a) When the airplane is not operated for hire or offered for common carriage screening of the baggage/cargo placed in the in-flight accessible Class C compartment is the responsibility of the operator of the airplane. This provision does not preclude the operator from receiving remuneration to the extent consistent with 14 CFR parts 125 and 91, subpart F, as applicable. (b) When the airplane is operated for hire or operated for common carriage, the baggage/cargo placed in the in-flight accessible Class C compartment is subject to the screening requirements and operators security program as identified in 49 CFR part 1544. Issued in Renton, Washington, on July 31, 2008. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E8–18474 Filed 8–8–08; 8:45 am] Certification Office, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137–4298; telephone: (817) 222–5146; fax: (817) 222–5960. SUPPLEMENTARY INFORMATION: Discussion AD 2008–02–04, Amendment 39– 15334 (73 FR 3618, January 22, 2008), affects Eclipse Model EA500 airplanes and currently: • Requires incorporating a modification of the angle of attack (AOA) probe; • Limits the applicability to airplanes under S/N 000065; and • Retains the operating limitations from AD 2007–13–11 until the modification is incorporated. BILLING CODE 4910–13–P The FAA incorrectly referenced the issue date as ‘‘January 9, 2007’’ instead of ‘‘January 9, 2008.’’ This document corrects the issue date. DEPARTMENT OF TRANSPORTATION Need for the Correction Federal Aviation Administration This correction is needed to reflect the correct issue date on the AD. 14 CFR Part 39 [Docket No. FAA–2007–29316; Directorate Identifier 2007–CE–078–AD; Amendment 39–15334; AD 2008–02–04] RIN 2120–AA64 Airworthiness Directives; Eclipse Aviation Corporation Model EA500 Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. AGENCY: SUMMARY: This document makes a correction to Airworthiness Directive (AD) 2008–02–04, which was published in the Federal Register on January 22, 2008 (73 FR 3618), and applies to all Eclipse Aviation Corporation (Eclipse) Model EA500 airplanes. This AD requires incorporating a modification of the angle of attack (AOA) system, limits the applicability to airplanes under S/N 000065, and retains the operating limitations from AD 2007–13–11 until the modification is incorporated. The FAA incorrectly referenced the issue date of the AD as ‘‘January 9, 2007’’ instead of ‘‘January 9, 2008.’’ This document corrects the issue date. DATES: The effective date of this AD remains February 26, 2008, since the incorrect reference of the issue date of AD 2008–02–04 does not affect compliance. FOR FURTHER INFORMATION CONTACT: Al Wilson, Flight Test Pilot, Airplane PO 00000 Frm 00014 Fmt 4700 Sfmt 4700 Correction of Publication Accordingly, the publication of January 22, 2008 (73 FR 3618), which was the subject of FR Doc. E8–751, is corrected as follows: Section 39.13 [Corrected] On page 3619, in the third column, in the sixth and seventh lines from the bottom, under the heading § 39.13 [Amended], replace ‘‘January 9, 2007’’ with ‘‘January 9, 2008.’’ Action is taken herein to correct this reference in the AD. The effective date of this AD remains February 26, 2008, since the incorrect reference of the issue date of AD 2008– 02–04 does not affect compliance. Issued in Kansas City, Missouri, on August 1, 2008. James E. Jackson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E8–18227 Filed 8–8–08; 8:45 am] BILLING CODE 4910–13–P E:\FR\FM\11AUR1.SGM 11AUR1

Agencies

[Federal Register Volume 73, Number 155 (Monday, August 11, 2008)]
[Rules and Regulations]
[Page 46542]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-18227]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-29316; Directorate Identifier 2007-CE-078-AD; 
Amendment 39-15334; AD 2008-02-04]
RIN 2120-AA64


Airworthiness Directives; Eclipse Aviation Corporation Model 
EA500 Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; correction.

-----------------------------------------------------------------------

SUMMARY: This document makes a correction to Airworthiness Directive 
(AD) 2008-02-04, which was published in the Federal Register on January 
22, 2008 (73 FR 3618), and applies to all Eclipse Aviation Corporation 
(Eclipse) Model EA500 airplanes. This AD requires incorporating a 
modification of the angle of attack (AOA) system, limits the 
applicability to airplanes under S/N 000065, and retains the operating 
limitations from AD 2007-13-11 until the modification is incorporated. 
The FAA incorrectly referenced the issue date of the AD as ``January 9, 
2007'' instead of ``January 9, 2008.'' This document corrects the issue 
date.

DATES: The effective date of this AD remains February 26, 2008, since 
the incorrect reference of the issue date of AD 2008-02-04 does not 
affect compliance.

FOR FURTHER INFORMATION CONTACT: Al Wilson, Flight Test Pilot, Airplane 
Certification Office, FAA, 2601 Meacham Blvd., Fort Worth, Texas 76137-
4298; telephone: (817) 222-5146; fax: (817) 222-5960.

SUPPLEMENTARY INFORMATION:

Discussion

    AD 2008-02-04, Amendment 39-15334 (73 FR 3618, January 22, 2008), 
affects Eclipse Model EA500 airplanes and currently:
     Requires incorporating a modification of the angle of 
attack (AOA) probe;
     Limits the applicability to airplanes under S/N 000065; 
and
     Retains the operating limitations from AD 2007-13-11 until 
the modification is incorporated.

The FAA incorrectly referenced the issue date as ``January 9, 2007'' 
instead of ``January 9, 2008.'' This document corrects the issue date.

Need for the Correction

    This correction is needed to reflect the correct issue date on the 
AD.

Correction of Publication

    Accordingly, the publication of January 22, 2008 (73 FR 3618), 
which was the subject of FR Doc. E8-751, is corrected as follows:

Section 39.13 [Corrected]

    On page 3619, in the third column, in the sixth and seventh lines 
from the bottom, under the heading Sec.  39.13 [Amended], replace 
``January 9, 2007'' with ``January 9, 2008.''
    Action is taken herein to correct this reference in the AD.
    The effective date of this AD remains February 26, 2008, since the 
incorrect reference of the issue date of AD 2008-02-04 does not affect 
compliance.

    Issued in Kansas City, Missouri, on August 1, 2008.
James E. Jackson,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
 [FR Doc. E8-18227 Filed 8-8-08; 8:45 am]
BILLING CODE 4910-13-P

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