1. The authority citation for part 39 continues to read as follows:
[Amended]
2. Section 39.13 is amended by adding the following new airworthiness directive:
NARCO Avionics Inc. AT150 Transponders:
Docket No. 2002-NE-32-AD.
Applicability:
This airworthiness directive (AD) is applicable to NARCO Avionics Inc. AT150 transponders with “Chassis Level A”, serial numbers (SN's) 10000 through 12598 inclusive. These transponders might be installed on, but not limited to the following aircraft:
Cessna Aircraft Company
172, 182, R182, T182, 206, P206, U206, TP206, 210, T210, P210, 310, E310, T310, and 421 series airplanes.
Twin Commander Aircraft Company
500, 520, 560, 680, 681, 685, 690, 695, and 720 series airplanes.
The New Piper Aircraft Corporation
PA-31, PA-32, and PA-34 series airplanes.
Raytheon Aircraft Company
E33, F33, G33, 35, J35, K35, L35, M35, P35, S35, V35, 36, A26, B36, D55, E55, 56, A56, 58, 58A, 95, B95, D95, and E95 series airplanes.
Mooney Aircraft Corporation
M20 series airplanes.
McDonnell Douglas Helicopter Company
Model 500N rotorcraft.
Note 1:
This AD applies to each transponder identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For transponders 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
Compliance with this AD is required as indicated, unless already done.
To prevent loss of aircraft airspace separation, and the possibility of mid-air collision, do the following:
Transponders Not Modified In Accordance With Service Bulletin AT150 No. 1
(a) For AT150 transponders with a SN listed in this AD that are not modified in accordance with service bulletin (SB) AT150 No. 1, dated July 29, 1977, within six months after the effective date of this AD, do the following:
(1) Install resistor part number (P/N) 755610028 and transistor P/N 312180102; and
(2 ) Change transponder to “Chassis Level B”; and
(3) Test transponders in accordance with the Corrective Action, Testing the Modification, and Return to Service paragraphs of SB AT150 No. 6, dated January 31, 2003.
Transponders Modified In Accordance With Service Bulletin AT150 No. 1
(b) For AT150 transponders with a SN listed in this AD, that are modified in accordance with SB AT150 No. 1, dated July 29, 1977, do the following:
(1) Within six months after the effective date of this AD, change transponder to “Chassis Level B”; and
(2) Test transponders in accordance with the Testing the Modification paragraph of SB AT150 No. 6, dated January 31, 2003; and
(3) Perform a bench test to the transponder before returning it to service. Information on bench testing can be found in AT150 Manual P/N 03606-0600.
Alternative Methods of Compliance
(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, New York Aircraft Certification Office. Operators must submit their request through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, New York Aircraft Certification Office.
Note 2:
Information concerning the existence of approved alternative methods of compliance with this airworthiness directive, if any, may be obtained from the New York Aircraft Certification Office.
Special Flight Permits
(d) Special flight permits may be issued in accordance with §§ 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the aircraft to a location where the requirements of this AD can be done.