[4910-I3-P]

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part39

(Docket No. Docket No. 2010-0041; Directorate Identifier 2009-NM-21S-AD;

\&Dq~ 1I-02-

Amendment 39-*****; AD 2010-**-**]

RIN 2120-AA64

Airworthiness Directives; Airbus Model A330-201, -202, -203, -223, -243, -301, -30

-303, -321, -322, -323, -341, -342, and -343 A+lanes, Model A340-211, -212, -213,

-311, -312, and -313 Airplanes, and Model A340-541 and ~642 Airplanes

I

AGENCY: Federal Aviation Administration (FAA), Department of Transportation

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* * * *

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ACTION: Final rule.

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SUMM.ARY: We are adopting a new ainvorthiness directive (AD) for the products Ii

above. This AD results from mandatory continLng airworthiness infonnation (MCA1) 2!JTl~:"~

originated by an aviation authority of another cluntry to identify and correct an unsan '":~<=J<;;~ATU~~ I CG4v--

condition on an aviation product. The MeAl describes the unsafe condition as: °::"/"';'0

Several reports have recently been Jeceived ofloase pneumatic fIOUTl"G"' •• ",,,.

quick-disconnect unions on GOOdli~hpitot probes PIN (part

number) 0851 HL. These may be th1result of mis-torque of the

affected unions at equipment manu~acturing level. Investigations

are still on-going to determine the r'i)otcause(s).

This condition, ifnot canected, coJd lead to an air leak, resulting

• • J

III licorrect total pressure measurenJent and consequent erroneous

Calibrated Airspeed (CAS)/MACH 'parameters delivered by the

Air Data Computer (ADC).

(DOT).

FAA Form 1360·14.1 (6-89) OFFICIAL FILE COPY

i::J u.s. GOVERNMENT PRINTING OFFICE: 1995·769·211

I
14910-n-PI

RIN 2120-AA64

DEPARTMENT OF TR<\NSPORTA nON

Federal A"iatioD Administration

14 eFR Part 39

(Docket No. Docket No. 2010-0041; Directorate Identifier 2009-NM-218-AD;

Amendment 39-*****; AD ZOlO-H_ .•.•.J

""""""'UwOOL

5ff!1r

AinvOTtbiness Directives. Airbus Model A330-201, -202, -203, -223. -243, -301, -30 !'1m'

-303, -321, -322, -323, -341, -342, and -343 Airplanes, Model A340-21I, -212, -213,

-311. -312. and -313 Airplanes, and Model A34O-541 and -642 Airplanes

~,,: ..•

AGENCY: Federal Aviation Administration (FAA), Department of Transportation

(DOT).

ACTION: Final rule.

SUMMARY: We are adopting a new airworthiness directive (AD) for the products Ii

above. This AD results from mandatory continUirl g airvlOrthiness infonnation (MeAl

r: r"",A'-"SICJ<""~' originated by an aviation authority of another cortry to identify and correct an unga!. OA'~

condition on an aviation product. The MeAl describes the unsafe condition as:

Several reports have recently been [jeive'd of loose pneumatic

quick-disconnect unions on Goodric~ pilot probes PIN (part

number) 0851HL. The:>emay be the ~csult afmis-torque oftbc

affected unions at equipment manufacturing level. Investigations

are still on-going to detennine the ro6t cause(s}.

This condition, ifoot corrected. could lead to an air leak, resulting

in incorrect total pressure measurement and consequent erroneous

Calibrated Airspeed (CAS)IMACH parametel"5 delivered by the

Air Data Computer (ADC) .

• • • • • • •

FAA Form 1360-14.1 (6-89) OFFICIAL FILE COpy