Discussion
What Events Have Caused This AD?
The FAA has received evidence of chafing and/or arcing of the electrical wiring leading to the fuel boost pump reservoir. Further investigation revealed confirmed reports of chafing and/or arcing of the fuel boost pump wiring inside the fuel pump reservoir that supplies fuel to each engine.
What Are the Consequences if the Condition Is Not Corrected?
This condition, if not corrected, could result in ignition of explosive vapor within the fuel storage system.
Is There Service Information That Applies to This Subject?
Cessna has issued Conquest Service Bulletin No. CQB02-1R1, Revision 1, dated April 22, 2002.
The service bulletin includes procedures for:
-Inspecting the 5718106-1 wire harness and fuel boost pump lead wires for chafing or damage; and
-Repairing or replacing the chafed or damaged wiring as necessary.
The FAA's Determination and an Explanation of the Provisions of This AD
What Has FAA Decided?
The FAA has reviewed all available information, including the service information referenced above; and determined that:
-The unsafe condition referenced in this document exists or could develop on other Cessna Model CESSNA 441 airplanes of the same type design;
-The actions specified in the previously-referenced service information (as specified in this AD) should be accomplished on the affected airplanes; and
-AD action should be taken in order to correct this unsafe condition.
What Does This AD Require?
This AD requires you to: (1) Do a one-time inspection of the electrical wiring going to the fuel boost pump reservoir and the boost pump wiring inside the reservoir, and (2) repair or replace the wiring as necessary.
In preparation of this rule, we contacted type clubs and aircraft operators to obtain technical information and information on operational and economic impacts. We did not receive any information through these contacts. If received, we would have included, in the rulemaking docket, a discussion of any information that may have influenced this action.
The FAA is not including a repetitive inspection requirement in this AD. The Administrative Procedure Act does not permit the FAA to "bootstrap" a long-term requirement into an urgent safety of flight action where the rule becomes effective at the same time the public has the opportunity to comment. The short-term action and the long-term action are analyzed separately for justification to bypass prior public notice.
After issuing this AD, the FAA may initiate further AD action (notice of proposed rulemaking followed by a final rule) to require these inspections to be repetitive. Credit will be given in any subsequent action for the initial inspection done under this AD.
Will I Have the Opportunity To Comment Prior to the Issuance of the Rule?
Because the unsafe condition described in this document could result in ignition of explosive vapor within the fuel storage system, we find that notice and opportunity for public prior comment are impracticable. Therefore, good cause exists for making this amendment effective in less than 30 days.
Comments Invited
How Do I Comment on This AD?
Although this action is in the form of a final rule and was not preceded by notice and opportunity for public comment, FAA invites your comments on the rule. You may submit whatever written data, views, or arguments you choose. You need to include the rule's docket number and submit your comments to the address specified under the caption ADDRESSES. We will consider all comments received on or before the closing date specified above. We may amend this rule in light of comments received. Factual information that supports your ideas and suggestions is extremely helpful in evaluating the effectiveness of the AD action and determining whether we need to take additional rulemaking action.
Are There Any Specific Portions of the AD I Should Pay Attention to?
We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of the rule that might suggest a need to modify the rule. You may view all comments we receive before and after the closing date of the rule in the Rules Docket. We will file a report in the Rules Docket that summarizes each FAA contact with the public that concerns the substantive parts of this AD.
How Can I Be Sure FAA Receives My Comment?
If you want us to acknowledge the receipt of your comments, you must include a self-addressed, stamped postcard. On the postcard, write "Comments to Docket No. 2002-CE-17-AD." We will date stamp and mail the postcard back to you.
Compliance Time of This AD
What Is the Compliance Time of This AD?
The compliance time of this proposed AD is within the next 25 hours time-in-service (TIS) or 60 calendar days, whichever occurs first, after the effective date of this AD.Why Is the Compliance Time of This AD Presented in Both Hours TIS and Calendar Time?
The affected airplanes are used in general aviation operations. Those operators may accumulate 25 hours TIS on the airplane in less than 60 calendar days and many owners have numerous affected airplanes. We have determined that the dual compliance time:
-Gives all owners/operators of the affected airplanes adequate time to schedule and do the actions in this AD; and
-Ensures that the unsafe condition referenced in this AD will be corrected within a reasonable time period without inadvertently grounding any of the affected airplanes.
Regulatory Impact
Does This AD Impact Various Entities?
These regulations will 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, FAA has determined that this final rule does not have federalism implications under Executive Order 13132.
Does This AD Involve a Significant Rule or Regulatory Action?
We have determined that this regulation is an emergency regulation that must be issued immediately to correct an unsafe condition in aircraft, and is not a significant regulatory action under Executive Order 12866. It has been determined further that this action involves an emergency regulation under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979). If it is determined that this emergency regulation otherwise would be significant under DOT Regulatory Policies and Procedures, a final regulatory evaluation will be prepared and placed in the Rules Docket (otherwise, an evaluation is not required). A copy of it, if filed, may be obtained from the Rules Docket.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety.
Adoption of the Amendment
Accordingly,under the authority delegated to me by the Administrator, the Federal Aviation Administration amends part 39 of the Federal Aviation Regulations (14 CFR part 39) as follows:
PART 39-AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
2. FAA amends Sec. 39.13 by adding a new airworthiness directive (AD) to read as follows: