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CFR Citation: 14 CFR Part 39

Docket ID: [Docket No. 2003-CE-28-AD]

RIN ID: RIN 2120-AA64

NOTICE: PROPOSED RULES

ACTION: Airworthiness directives:

DOCUMENT ACTION: Notice of proposed rulemaking (NPRM).

SUBJECT CATEGORY: Airworthiness Directives; Cessna Aircraft Company Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H Airplanes

DATES: The Federal Aviation Administration (FAA) must receive any comments on this proposed rule on or before September 22, 2003.

DOCUMENT SUMMARY: This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Cessna Aircraft Company (Cessna) Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H airplanes that are equipped with a Honeywell KAP 140 autopilot computer system installed on the center instrument control panel near the throttle. This proposed AD would require you to install an update to the operating software of the KAP 140 autopilot computer system, change the unit's part number, and change the software modification identification tab. This proposed AD is the result of reports of inadvertent and undetected engagement of the autopilot system. The actions specified by this proposed AD are intended to prevent unintentionally engaging the KAP 140 autopilot computer system, which could cause the pilot to take inappropriate actions.

SUMMARY: Cessna,

SUPPLEMENTAL INFORMATION

How Do I Comment on This Proposed AD?

The FAA invites comments on this proposed rule. You may submit whatever written data, views, or arguments you choose. You need to include the proposed 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. We may amend this proposed rule in light of comments received. Factual information that supports your ideas and suggestions is extremely helpful in evaluating the effectiveness of this proposed AD action and determining whether we need to take additional rulemaking action.
Are There Any Specific Portions of This Proposed AD I Should Pay Attention To?

The FAA specifically invites comments on the overall regulatory, economic, environmental, and energy aspects of this proposed 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 proposed rule in the Rules Docket. We will file a report in the Rules Docket that summarizes each contact we have with the public that concerns the substantive parts of this proposed AD.

How Can I Be Sure FAA Receives My Comment?

If you want FAA to acknowledge the receipt of your mailed comments, you must include a selfaddressed, stamped postcard. On the postcard, write ``Comments to Docket No. 2003CE28AD.'' We will date stamp and mail the postcard back to you.
Discussion

What Events Have Caused This Proposed AD?

We have received reports of an unsafe condition on certain Cessna Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H airplanes that are equipped with a Honeywell KAP 140 autopilot computer system.

The KAP 140 autopilot computer system is located on the lower portion of the center instrument control panel near the throttle on these Cessna airplanes. Because of this location on the instrument control panel of the affected Cessna airplanes, the Autopilot Engage (AP) button could unintentionally be depressed when the pilot pushes the throttle knob forward. The pilot could also unintentionally engage the autopilot system by inadvertently bumping the Heading (HDG) button, Altitude (ALT) modeselect button, or Autopilot Engage (AP) button on the KAP 140 computer. Unless intentionally engaged, the pilot does not know that the autopilot system is engaged.

The Honeywell KAP 140 autopilot computer system is also installed in the New Piper, Inc. Model PA28181 airplanes. This proposed AD would not affect these airplanes because of the location of the equipment. The equipment is installed on the center instrument panel near the throttle on the affected airplanes, but is installed in the upper half of the instrument control
[[Page 44498]]
panel on the Piper airplanes. The unsafe condition only exists on the Cessna airplanes.

Honeywell has updated the operating software for the KAP 140 autopilot computer system, which will now only allow the AP button on the instrument control panel to engage the autopilot system. This update also adds two voice messages if auto trim operation is detected, lengthens the amount of time that the autopilot button must be depressed in order for it to engage, and changes how the flight control display shows that the AP has been engaged.
What Are the Consequences if the Condition Is Not Corrected?

If not corrected, inadvertent and undetected engagement of the autopilot system could cause the pilot to take inappropriate actions. Is There Service Information That Applies to This Subject?

Cessna has issued Service Bulletin SB022201, dated November 25, 2002.

Honeywell has issued Service Bulletin No: KC 140M1, dated August 2002; and Installation Bulletin No: 491, dated August 2002. What Are the Provisions of This Service Information?

Cessna Service Bulletin SB022202, dated November 25, 2002, specifies installing an update to the autopilot computer system operating software by accomplishing the actions in Honeywell Service Bulletin No: KC 140M1, dated August 2002.

Honeywell Service Bulletin No: KC 140M1, dated August 2002, includes procedures for:
Installing an update to the autopilot computer system operating software;
Changing the unit part number;
Placing an M tag on the unit serial number tag; and

Changing the unit's software modification tag.

Honeywell Installation Bulletin No: 491, dated August 2002, describes the operational changes the software update makes to the KC 140 autopilot computer system.
The FAA's Determination and an Explanation of the Provisions of this Proposed AD

What Has FAA Decided?

After examining the circumstances and reviewing all available information related to the incidents described above, we have determined that:
The unsafe condition referenced in this document exists or could develop on other Cessna Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H of the same type design;
The actions specified in the previouslyreferenced service
information should be accomplished on the affected airplanes; and AD action should be taken in order to correct this unsafe condition. What Would This Proposed AD Require?

This proposed AD would require you to update to the operating software of the KAP 140 autopilot computer system; change the unit's part number; and change the software modification identification tab. How Does the Revision to 14 CFR Part 39 Affect This Proposed AD?

On July 10, 2002, FAA published a new version of 14 CFR part 39 (67 FR 47997, July 22, 2002), which governs FAA's AD system. This regulation now includes material that relates to special flight permits, alternative methods of compliance, and altered products. This material previously was included in each individual AD. Since this material is included in 14 CFR part 39, we will not include it in future AD actions.
Cost Impact

How Many Airplanes Would This Proposed AD Impact?

We estimate that this proposed AD affects 3,681 airplanes in the U.S. registry.
What Would Be the Cost Impact of This Proposed AD on Owners/Operators of the Affected Airplanes?

We estimate the following costs to accomplish this proposed modification:
Total cost Labor cost Parts cost per airplane 7 workhours x $65 per hour = $455.. Not applicable........ $455.

Not all Cessna Models 172R, 172S, 182S, 182T, T182T, 206H, and T206H airplanes on the U.S. registry have a KAP 140 autopilot computer system installed.

Honeywell will provide warranty credit for labor and parts to the extent noted under WARRANTY INFORMATION in each specified in Honeywell Service Bulletin No: KC 140M1, dated August 2002.
Regulatory Impact

Would This Proposed AD Impact Various Entities?

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 proposed rule would not have federalism implications under Executive Order 13132.
Would This Proposed AD Involve a Significant Rule or Regulatory Action?

For the reasons discussed above, I certify that this proposed action (1) is not a ``significant regulatory action'' under Executive Order 12866; (2) is not a ``significant rule'' under 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 has been placed in the Rules Docket. A copy of it may be obtained by contacting the Rules Docket at the location provided under the caption ADDRESSES.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Safety. The Proposed Amendment

Accordingly, under 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:

PART 39AIRWORTHINESS 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:
Cessna Aircraft Company: Docket No. 2003CE28AD
(a) What airplanes are affected by this AD? This AD affects the following airplane models and serial numbers that are:
(1) equipped with a KAP 140 autopilot computer system, part number (P/N) 065001762602, P/N 065001765402, or P/N 06500176 7702 ; and
(2) certificated in any category;
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Model Serial numbers
172R................ 17280001 through 17281073, 17281075 through 17281127, and 17281130
172S................ 172S8001 through 172S9195, 172S9197, 172S9198, and 172S9200 through 172S9203
182S................ 18280001 through 18280944
182T................ 18280945 through 18281064, 18281067 through 18281145, 18281147 through 18281163, 18281165 through 18281167, and 18281172
T182T............... T18208001 through T18208109, and T18208111 through T18208177
206H................ 20608001 through 20608183, 20608185, 20608187, and 20608188
T206H............... T20608001 through T20608039, T20608041 through T20608367, T20608269 through T20608379, T20608381, T20608382, and T20608385
(b) Who must comply with this AD? Anyone who wishes to operate any of the airplanes identified in paragraph (a) of this AD must comply with this AD.
(c) What problem does this AD address? The actions specified by this AD are intended to prevent unintentionally engaging the KAP 140 autopilot computer system, which could cause the pilot to take inappropriate actions.
(d) What actions must I accomplish to address this problem? To address this problem, you must accomplish the following, unless already accomplished:
Actions Compliance Procedures (1) Install and update the Within the next 100 In accordance with KC 140 autopilot computer hours timein Honeywell Service system operating software. service (TIS) after Bulletin No: KC 140 the effective date M1, dated August of this AD. 2002, as specified in Cessna Service Bulletin SB0222 01, dated November 25, 2002. (2) Accomplish the Prior to further In accordance with following: (i) Change the flight after Honeywell Service unit part number by installing the Bulletin No: KC 140 attaching flavor sticker, update to the KC M1, dated August part number (P/N) 05702203 140 autopilot 2002, as specified 0003, on the unit's serial computer system in Cessna Service tag; operating software. Bulletin SB0222 01, dated November 25, 2002. (ii) Attach an M decal, P/N
057029840501, in front of
the unit serial number
(this indicates that the
unit's P/N has been
changed); and.
(iii) Attach a software mod
tag, P/N 057052870301, in
place of the old tag to
indicate the software
change to SW MOD 03/01..
(3) Only install KC 140 As of the effective Not applicable. autopilot computer systems, date of this AD.
P/Ns 065001762602, 065
001765402, and 06500176
7702, that have been
modified as specified in
paragraphs (d)(1) and

(d)(2) of this AD.

You may request a revised flight manual supplement from Cessna or Honeywell at the address specified in paragraph (f) of this AD. (e) Can I comply with this AD in any other way? To use an alternative method of compliance or adjust the compliance time, follow the procedures in 14 CFR 39.19. Send these requests to the Manager, Wichita Aircraft Certification Office (ACO). For
information on any already approved alternative methods of compliance, contact Dan Withers, Aerospace Engineer, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Wichita, Kansas 67209; telephone: (316) 9464196; facsimile: (316) 9464107. (f) How do I get copies of the documents referenced in this AD? You may get copies of the documents referenced in this AD from Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277; telephone: (316) 5175800; facsimile: (316) 9429006 and Honeywell, Business, Regional, and General Aviation, 23500 W. 105th Street, Olathe, Kansas 66061. You may view these documents at FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106.

Issued in Kansas City, Missouri, on July 22, 2003. David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 0319197 Filed 72803; 8:45 am]
BILLING CODE 491013P

FOR FURTHER INFORMATION CONTACT Dan Withers, Aerospace Engineer, Wichita Aircraft Certification Office (ACO), FAA, 1801 Airport Road, MidContinent Airport, Wichita, Kansas 67209; telephone: (316) 946 4196; facsimile: (316) 9464407.