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[Federal Register: May 4, 2010 (Volume 75, Number 85)]
[Rules and Regulations]               
[Page 23579-23580]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr04my10-8]                         

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2000-NM-418-AD; Amendment 39-12964; AD 2002-23-20]
RIN 2120-AA64

 
Airworthiness Directives; DASSAULT AVIATION Model FALCON 900EX 
and MYSTERE-FALCON 900 Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; correction.

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SUMMARY: This document corrects a typographical error that appeared in 
airworthiness directive (AD) 2002-23-20 that was published in the 
Federal Register on November 29, 2002 (67 FR 71098). The typographical 
error resulted in an incorrect part number. This AD is applicable to 
Model FALCON 900EX and MYSTERE-FALCON 900 airplanes. This AD requires 
repetitive operational tests of the flap asymmetry detection system to 
verify proper functioning, and repair if necessary; repetitive 
replacement of the inboard flap jackscrews with new or reconditioned 
jackscrews; and repetitive measurement of the screw/nut play of the 
jackscrews on the inboard and outboard flaps to detect discrepancies, 
and corrective action if necessary. This AD also requires revision of 
the Airplane Flight Manual.

DATES: This correction is effective May 4, 2010. The effective date of 
AD 2002-23-20 remains January 3, 2003.

FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,

[[Page 23580]]

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: AD 2002-23-20, amendment 39-12964, 
applicable to Model FALCON 900EX and MYSTERE-FALCON 900 airplanes, was 
published in the Federal Register on November 29, 2002 (67 FR 71098). 
That AD requires repetitive operational tests of the flap asymmetry 
detection system to verify proper functioning, and repair if necessary; 
repetitive replacement of the inboard flap jackscrews with new or 
reconditioned jackscrews; and repetitive measurement of the screw/nut 
play of the jackscrews on the inboard and outboard flaps to detect 
discrepancies, and corrective action if necessary. That AD also 
requires revision of the Airplane Flight Manual.
    As published, paragraph (e)(1) of the AD specifies in error 
jackscrew part number 5818-1 Amdt A. P/N 5818-1 Amdt A. does not exist. 
The correct part number is 5318-1 Amdt A.
    Since no other part of the regulatory information has been changed, 
the final rule is not being republished in the Federal Register.
    The effective date of this AD remains January 3, 2003.

Sec.  39.13  [Corrected]

0
On page 71101, in the first column, paragraph (e)(1) of AD 2002-23-20 
is corrected to read as follows:
* * * * *
    (1) The jackscrew has been reconditioned and reidentified as P/N 
5318-1 Amdt A, in accordance with Dassault Service Bulletin AVIAC 5318-
27-01, dated September 16, 1999.
* * * * *

    Issued in Renton, Washington, on April 22, 2010.
Jeffrey E. Duven,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2010-9943 Filed 5-3-10; 8:45 am]
BILLING CODE 4910-13-P
```