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Airworthiness directives › 2002-09-03

AD 2002-09-03 Airworthiness Directives; Eurocopter France Model AS332L2 Helicopters

2002-05-17
2002-05-02
39-12736
2002-SW-04-AD
Airframe
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Models named: AS332L2. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

Model AS332L2 helicopters, with a life raft assembly, part number 00051047 or 00051048, installed, certificated in any category. Note 1: This AD applies to each helicopter identified in the preceding applicability provision, regardless of whether it has been otherwise modified, altered, or repaired in the area subject to the requirements of this AD. For helicopters that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (c) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

Compliance

Required before further flight, unless accomplished previously. To prevent inadvertent life raft inflation, loss of the life raft, contact with the main or tail rotor, and subsequent loss of control of the helicopter, accomplish the following: (a) Verify that the air vent is installed on the head of the inflation cylinder of each lift raft assembly as shown in FIGURE 1: ER02my02.000 If the air vent is missing, replace the cylinder head with an airworthy cylinder head before further flight. Note 2: Eurocopter France Alert Telex No. 25.01.06, dated September 17, 2001, pertains to the subject of this AD. (b) Replacing the cylinder head or verifying that the air vent is installed on the head of the inflation cylinder is terminating action for the requirements of this AD. (c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Regulations Group, Rotorcraft Directorate, FAA. Operators shall submit their requests through an FAA Principal Maintenance Inspector, who may concur or comment and then send it to the Manager, Regulations Group. Note 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Regulations Group. (d) Special flight permits will not be issued. (e) This amendment becomes effective on May 17, 2002. Note 4: The subject of this AD is addressed in Direction Generale De L'Aviation Civile (France) AD 2001-500-019(A), dated October 17, 2001. Issued in Fort Worth, Texas, on April 17, 2002. Larry M. Kelly, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 02-10649 Filed 5-1-02; 8:45 am] BILLING CODE 4910-13-P

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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1