Federal Aviation Administration, DOT.
Notice of proposed rulemaking (NPRM).
This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Thales Avionics TA/RA VSI-TCAS indicators, installed on but not limited to certain transport category airplanes equipped with TCAS II change 7 computers (ACAS II). This proposal would require a revision to the Airplane Flight Manual (AFM) to advise the flightcrew to follow the audio annunciation when an RA fail message is triggered during a multi-aircraft encounter. This proposed AD would also require modification of the software for the TA/RA VSI-TCAS indicator, which would terminate the requirement for the AFM revision. This action is necessary to prevent the TA/RA VSI-TCAS indicator from displaying a conflicting “RA FAIL” message during a multi-aircraft encounter, which could result in the flightcrew ignoring the correct aural command and traffic display information if the flightcrew believes the TCAS II computer has malfunctioned, and consequently lead to a mid-air collision with other aircraft. This action is intended to address the identified unsafe condition.
Comments must be received by June 7, 2004.
Submit comments in triplicate to the Federal Aviation Administration (FAA), Transport Airplane Directorate, ANM-114, Attention: Rules Docket No. 2002-NM-284-AD, 1601 Lind Avenue, SW., Renton, Washington 98055-4056. Comments may be inspected at this location between 9 a.m. and 3 p.m., Monday through Friday, except Federal holidays. Comments may be submitted via fax to (425) 227-1232. Comments may also be sent via the Internet using the following address: firstname.lastname@example.org. Comments sent via fax or the Internet must contain “Docket No. 2002-NM-284-AD” in the subject line and need not be submitted in triplicate. Comments sent via the Internet as attached electronic files must be formatted in Microsoft Word 97 or 2000 or ASCII text.
The service information referenced in the proposed rule may be obtained from Thales Avionics, Air Transport Avionics, 105 avenue du General Eisenhower, BP 1147, 31036 Toulouse Cedex 1, France; or Thales Avionics, Regional and Business Aircraft Avionics, 105 avenue du General Eisenhower, BP 1147, 31036 Toulouse Cedex 1, France; or Thales Avionics, Avionics for Military Aircraft, Rue Toussaint Catros, 33187 Le Haillan Cedex, France. This information may be examined at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California.Start Further Info
FOR FURTHER INFORMATION CONTACT:
Abby Malmir, Aerospace Engineer, Systems and Equipment Branch, ANM-130L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, California 90712-4137; telephone (562) 627-5351; fax (562) 627-5210.End Further Info End Preamble Start Supplemental Information
Interested persons are invited to participate in the making of the proposed rule by submitting such written data, views, or arguments as they may desire. Communications shall identify the Rules Docket number and be submitted in triplicate to the address specified above. All communications received on or before the closing date for comments, specified above, will be considered before taking action on the proposed rule. The proposals contained in this action may be changed in light of the comments received.
Submit comments using the following format:
- Organize comments issue-by-issue. For example, discuss a request to change the compliance time and a request to change the service bulletin reference as two separate issues.
- For each issue, state what specific change to the proposed AD is being requested.
- Include justification (e.g., reasons or data) for each request.
Comments are specifically invited on the overall regulatory, economic, environmental, and energy aspects of the proposed rule. All comments submitted will be available, both before and after the closing date for comments, in the Rules Docket for examination by interested persons. A report summarizing each FAA-public contact concerned with the substance of this proposal will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments submitted in response to this action must submit a self-addressed, stamped postcard on which the following statement is made: “Comments to Docket Number 2002-NM-284-AD.” The postcard will be date stamped and returned to the commenter.
Availability of NPRMs
Any person may obtain a copy of this NPRM by submitting a request to the FAA, Transport Airplane Directorate, ANM-114, Attention: Rules Docket No. 2002-NM-284-AD, 1601 Lind Avenue, SW., Renton, Washington 98055-4056.
The FAA has become aware of an unsafe condition that may exist with Thales Avionics traffic advisory/resolution advisory (TA/RA) vertical speed indicator-traffic alert and collision avoidance system (VSI-TCAS) indicators, installed on but not limited to certain transport category airplanes equipped with TCAS II change 7 computers (ACAS II). During a ground test, the TA/RA VSI-TCAS indicator did not display the “DON'T CLIMB, DON'T DESCEND” RA command, under the scenario where the airplane is located between two other aircraft (one above and one below). Instead, the TA/RA Start Printed Page 25515VSI-TCAS indicator displayed an “RA FAIL” message, which conflicted with both the correct audio annunciation to “MAINTAIN VERTICAL SPEED, MAINTAIN” and traffic display information. A conflicting “RA FAIL” message during a multi-aircraft encounter, if not corrected, could result in the flightcrew ignoring the correct aural command and traffic display information if the flightcrew believes the TCAS II computer has malfunctioned, and consequently lead to a mid-air collision with other aircraft.
Explanation of Relevant Service Information
Thales Avionics has issued the following service bulletins:
|Service bulletin||Revision level||Date|
|457400-34-082||Original||November 28, 2002.|
|457400-34-083||03||January 26, 2004.|
|457400-34-084||02||December 19, 2003.|
|457400-34-085||00||February 5, 2004.|
These service bulletins describe procedures for modification of the software for the TA/RA VSI-TCAS indicator. The modification involves reprogramming memory MN9 of the graphic processor board for the TA/RA VSI-TCAS indicator, and reidentifying and testing the modified TA/RA VSI-TCAS indicator. Accomplishment of the actions specified in the service bulletin is intended to adequately address the identified unsafe condition. The Direction Generale de l'Aviation Civile (DGAC), which is the airworthiness authority for France, classified this service bulletin as mandatory and issued French airworthiness directive F-2004-042, dated March 31, 2004, to ensure the continued airworthiness of these airplanes in France.
This TA/RA VSI-TCAS indicator is manufactured in France and is type certificated for operation in the United States under the provisions of section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and the applicable bilateral airworthiness agreement.
Explanation of Requirements of Proposed Rule
Since an unsafe condition has been identified that is likely to exist or develop on other airplanes of the same type design registered in the United States, the proposed AD would require revising the Limitations Section of the Airplane Flight Manual (AFM) to advise the flightcrew to follow the audio annunciation when an RA fail message is triggered during a multi-aircraft encounter. This proposed AD would also require modifying the software for the TA/RA VSI-TCAS indicator, which would terminate the requirement for the AFM revision. The terminating action is required to be accomplished in accordance with the service bulletins described previously, except as discussed below.
Difference Between Proposed AD and French Airworthiness Directive
Operators should note that affected part number (P/N) 457400SB0711, as listed in Thales Avionics Service Bulletin 457400-34-083, Revision 03, dated January 26, 2004, was inadvertently omitted from French airworthiness directive F-2004-042, dated March 31, 2004. We have determined that the omitted part number is subject to the same unsafe condition of this proposed AD and, therefore, have included P/N 457400SB0711 in this proposed AD. Additionally, the DGAC has informed us that it plans to revise the French airworthiness directive to include the omitted part number.
Clarification Between Proposed AD and French Airworthiness Directive
The French airworthiness directive requires revising the Limitations Section of the AFM by inserting a temporary limitation. We have reviewed the language of the temporary limitation and determined that certain wording does not conform to the U.S. standard of writing AFM flightcrew instructions in either “must do” or “do not” statements for clarity and memorization. While we have clarified the language of the temporary limitation in this proposed AD, the intent of it remains the same.
We do not know how many aircraft, equipped with Thales Avionics TA/RA VSI-TCAS indicators and TCAS II change 7 computers (ACAS II), of the affected design are in the worldwide fleet or on the U.S. Register. We do, however, know that it would take approximately 2 work hours per airplane to accomplish the proposed actions, and that the average labor rate is $65 per work hour. Required parts, for 2 TCAS displays per airplane, would cost approximately between $1,316 and $1,826 per airplane. Based on these figures, the cost impact of the proposed AD on U.S. operators is estimated to be between $1,446 and $1,956 per airplane.
The cost impact figure discussed above is based on assumptions that no operator has yet accomplished any of the proposed requirements of this AD action, and that no operator would accomplish those actions in the future if this AD were not adopted. The cost impact figures discussed in AD rulemaking actions represent only the time necessary to perform the specific actions actually required by the AD. These figures typically do not include incidental costs, such as the time required to gain access and close up, planning time, or time necessitated by other administrative actions.
The regulations proposed herein would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government. Therefore, it is determined that this proposal would not have federalism implications under Executive Order 13132.
For the reasons discussed above, I certify that this proposed regulation (1) is not a “significant regulatory action” under Executive Order 12866; (2) is not a “significant rule” under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); and (3) if promulgated, will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. A copy of the draft regulatory evaluation prepared for this action is contained in the Rules Docket. A copy of it may be obtained by contacting the Rules Docket at the location provided under the caption ADDRESSES.Start List of Subjects
List of Subjects in 14 CFR Part 39End List of Subjects Start Printed Page 25516
The Proposed Amendment
Accordingly, pursuant to the authority delegated to me by the Administrator, the Federal Aviation Administration proposes to amend part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:Start Part
PART 39—AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
2. Section 39.13 is amended by adding the following new airworthiness directive:
Thales Avionics (Formerly Sextant Avionique): Docket 2002-NM-284-AD.
Applicability: Thales Avionics traffic advisory/resolution advisory (TA/RA) vertical speed indicator-traffic alert and collision avoidance system (VSI-TCAS) indicators, part number (P/N) 457400-(*), except P/Ns 457400GA1502, 457400GB1502, 457400MA1502, 457400MB1502, 457400ZA1502, and 457400ZB1502, installed on but not limited to Airbus Model A300 B2, A300 B4, and A310 series airplanes; Model A300 B4-600, B4-600R, C4-605R Variant F, and F4-600R (collectively called A300-600) series airplanes; and Aerospatiale Model ATR42 and ATR72 series airplanes; certificated in any category; equipped with TCAS II change 7 computers (ACAS II).
Compliance: Required as indicated, unless accomplished previously.
To prevent the TA/RA VSI-TCAS indicator from displaying a conflicting “RA FAIL” message during a multi-aircraft encounter, which could result in the flightcrew ignoring the correct aural command and traffic display information if the flightcrew believes the TCAS II computer has malfunctioned, and consequently lead to a mid-air collision with other aircraft; accomplish the following:
Revision of the Airplane Flight Manual (AFM)
(a) Within 15 days after the effective date of this AD, revise the Limitations Section of the AFM to include the following statement (this may be accomplished by inserting a copy of this AD into the AFM):
When the TA/RA VSI-TCAS indicates an RA fail message, the flightcrew must follow the audio annunciation “Maintain Vertical Speed, Maintain” until “clear of the conflict” audio annunciation has occurred.
When a preventive Don't Climb/Don't Descend resolution advisory (RA) is triggered by simultaneous, multi-aircraft encounter configuration, the TA/RA VSI-TCAS may indicate an RA fail message. The audio annunciation “Maintain Vertical Speed, Maintain” and traffic display information are correct. In this specific case, the flightcrew must follow the audio annunciation and, therefore, maintain the vertical speed until clearance of the conflict condition has occurred.”
When a statement identical to that in paragraph (a) of this AD has been included in the general revisions of the AFM, the general revisions may be inserted into the AFM, and the copy of this AD may be removed from the AFM.
(b) Within 48 months after the effective date of this AD, modify the software for the TA/RA VSI-TCAS indicator by accomplishing all the actions specified in the Accomplishment Instructions of the applicable service bulletin listed in Table 1 of this AD. Doing this modification terminates the requirements of paragraph (a) of this AD. After accomplishing the modification, the AFM limitation required by paragraph (a) of this AD may be removed from the AFM.
|For P/N—||Thales Avionics service bulletin||Revision level||Date|
|457400EA0311||457400-34-083||03||January 26, 2004.|
|457400GA0011||457400-34-085||00||February 5, 2004.|
|457400GA0311||457400-34-083||03||January 26, 2004.|
|457400GA1900||457400-34-082||Original||November 28, 2002.|
|457400GB0011||457400-34-085||00||February 5, 2004.|
|457400GB0911||457400-34-083||03||January 26, 2004.|
|457400GB1900||457400-34-082||Original||November 28, 2002.|
|457400GB2000||457400-34-084||02||December 19, 2003.|
|457400GB2100||457400-34-083||03||January 26, 2004.|
|457400LA2000||457400-34-084||02||December 19, 2003.|
|457400MA0602||457400-34-083||03||January 26, 2004.|
|Start Printed Page 25517|
Alternative Methods of Compliance
(c) In accordance with 14 CFR 39.19, the Manager, Los Angeles Aircraft Certification Office, FAA, Transport Airplane Directorate, is authorized to approve alternative methods of compliance for this AD.
The subject of this AD is addressed in French airworthiness directive F-2004-042, dated March 31, 2004.
Issued in Renton, Washington, on April 28, 2004.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 04-10380 Filed 5-6-04; 8:45 am]
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