Airworthiness Directives; Raytheon Corporate Jets Model BAe 125- 800A and -1000A and Model Hawker 800 and 1000 Series Airplanes

DEPARTMENT OF TRANSPORTATION

14 CFR Part 39

[Docket No. 95-NM-43-AD]

Airworthiness Directives; Raytheon Corporate Jets Model BAe 125-

800A and -1000A and Model Hawker 800 and 1000 Series Airplanes

AGENCY: Federal Aviation Administration, DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: This document proposes the adoption of a new airworthiness

directive (AD) that is applicable to certain Raytheon Corporate Jets

Model BAe 125-800A and -1000A and Model Hawker 800 and 1000 series

airplanes. This proposal would require an inspection to determine if

the diode soldered connections are clean and functionally sound. This

proposal would also require remake of the soldered connection and

replacement of the diode with a new diode, if necessary. This proposal

is prompted by reports of imperfect soldered connections in the engine

starting and battery emergency control circuit. The actions specified

by the proposed AD are intended to prevent incorrect fault displays in

the cockpit and intermittent fault symptoms in the engine starting and

battery emergency control circuits, as a result of imperfect soldered

connections.

DATES: Comments must be received by October 27, 1995.

ADDRESSES: Submit comments in triplicate to the Federal Aviation

Administration (FAA), Transport Airplane Directorate, ANM-103,

Attention: Rules Docket No. 95-NM-43-AD, 1601 Lind Avenue, SW., Renton,

Washington 98055-4056. Comments may be inspected at this location

between 9:00 a.m. and 3:00 p.m., Monday through Friday, except Federal

holidays.

The service information referenced in the proposed rule may be

obtained from Raytheon Corporate Jets, Inc., Customer Support

Department, Adams Field, P.O. Box 3356, Little Rock, Arkansas 72203.

This information may be examined at the FAA, Transport Airplane

Directorate, 1601 Lind Avenue, SW., Renton, Washington.

FOR FURTHER INFORMATION CONTACT: Tim Backman, Aerospace Engineer,

Standardization Branch, ANM-113, FAA, Transport Airplane Directorate,

1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (206)

227-2797; fax (206) 227-1149.

SUPPLEMENTARY INFORMATION:

Comments Invited

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 notice may be changed in

light of the comments received.

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 notice must submit a self-addressed,

stamped postcard on which the following statement is made: ``Comments

to Docket Number 95-NM-43-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-103, Attention: Rules

Docket No. 95-NM-43-AD, 1601 Lind Avenue, SW., Renton, Washington

98055-4056.

Discussion

The Civil Aviation Authority (CAA), which is the airworthiness

authority for the United Kingdom, recently notified the FAA that an

unsafe condition may exist on certain Raytheon Corporate Jets Model BAe

125-800A and -1000A and Model Hawker 800 and 1000 series airplanes. The

CAA advises that it has received reports of imperfect soldered

connections in the engine starting and battery emergency control

circuit. Such connections have led to fault symptoms of an intermittent

nature in these circuits. This condition, if not corrected,

[[Page 47904]]

could lead to incorrect fault displays in the cockpit and intermittent

fault symptoms in the engine starting and battery emergency control

circuits.

Raytheon Corporate Jets has issued Hawker Service Bulletin SB 24-

317, dated December 22, 1994, which describes procedures for an

inspection to determine if diode soldered connections are clean and

functionally sound. This service bulletin also describes procedures for

remake of the soldered connection or replacement of the diode with a

new diode, if necessary. The CAA classified this service bulletin as

mandatory in order to assure the continued airworthiness of these

airplanes in the United Kingdom.

This airplane model is manufactured in the United Kingdom 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. Pursuant

to this bilateral airworthiness agreement, the CAA has kept the FAA

informed of the situation described above. The FAA has examined the

findings of the CAA, reviewed all available information, and determined

that AD action is necessary for products of this type design that are

certificated for operation in the United States.

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 an inspection to

determine if the diode soldered connections are clean and functionally

sound. The proposed AD would also require remake of the soldered

connection or replacement of the diode with a new diode, if necessary.

The actions would be required to be accomplished in accordance with the

service bulletin described previously.

As a result of recent communications with the Air Transport

Association (ATA) of America, the FAA has learned that, in general,

some operators may misunderstand the legal effect of AD's on airplanes

that are identified in the applicability provision of the AD, but that

have been altered or repaired in the area addressed by the AD. The FAA

points out that all airplanes identified in the applicability provision

of an AD are legally subject to the AD. If an airplane has been altered

or repaired in the affected area in such a way as to affect compliance

with the AD, the owner or operator is required to obtain FAA approval

for an alternative method of compliance with the AD, in accordance with

the paragraph of each AD that provides for such approvals. A note has

been included in this notice to clarify this long-standing requirement.

The FAA estimates that 19 airplanes of U.S. registry would be

affected by this proposed AD, that it would take approximately 1 work

hour per airplane to accomplish the proposed actions, and that the

average labor rate is $60 per work hour. Based on these figures, the

total cost impact of the proposed AD on U.S. operators is estimated to

be $1,140, or $60 per airplane.

The total 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 regulations proposed herein would not have substantial direct

effects 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, in

accordance with Executive Order 12612, it is determined that this

proposal would not have sufficient federalism implications to warrant

the preparation of a Federalism Assessment.

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.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Safety.

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:

PART 39--AIRWORTHINESS DIRECTIVES

1. The authority citation for part 39 continues to read as follows:

Authority: 49 USC 106(g), 40101, 40113, 44701.

Sec. 39.13 [Amended]

2. Section 39.13 is amended by adding the following new

airworthiness directive:

Raytheon Corporate Jets, Inc. (Formerly DeHavilland, Hawker

Siddeley, British Aerospace PLC): Docket 95-NM-43-AD.

Applicability: Model BAe 125-800A and -1000A, and Model Hawker

800 and 1000 series airplanes, as listed in Raytheon Corporate Jets

Hawker Service Bulletin SB 24-317, dated December 22, 1994;

certificated in any category.

Note 1: This AD applies to each airplane 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 airplanes that have been modified,

altered, or repaired so that the performance of the requirements of

this AD is affected, the owner/operator must use the authority

provided in paragraph (b) of this AD to request approval from the

FAA. This approval may address either no action, if the current

configuration eliminates the unsafe condition; or different actions

necessary to address the unsafe condition described in this AD. Such

a request should include an assessment of the effect of the changed

configuration on the unsafe condition addressed by this AD. In no

case does the presence of any modification, alteration, or repair

remove any airplane from the applicability of this AD.

Compliance: Required as indicated, unless accomplished

previously.

To prevent incorrect fault displays in the cockpit and

intermittent fault symptoms in the engine starting and battery

emergency control circuits, as a result of imperfect soldered

connections, accomplish the following:

(a) Within 6 months after the effective date of this AD, perform

an inspection to determine if each diode soldered connection is

clean and functionally sound, in accordance with Hawker Service

Bulletin SB 24-317, dated December 22, 1994. If any diode soldered

connection is not clean or not functionally sound, prior to further

flight, remake the soldered connection or replace the diode with a

new diode, in accordance with the service bulletin.

(b) 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, Standardization Branch, ANM-113,

FAA, Transport Airplane Directorate. Operators shall submit their

requests through an appropriate FAA Principal Maintenance Inspector,

who may add comments and then send it to the Manager,

Standardization Branch, ANM-113.

Note 2: Information concerning the existence of approved

alternative methods of compliance with this AD, if any, may be

obtained from the Standardization Branch, ANM-113.

(c) Special flight permits may be issued in accordance with

sections 21.197 and 21.199

[[Page 47905]]

of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to

operate the airplane to a location where the requirements of this AD

can be accomplished.

Issued in Renton, Washington, on September 11, 1995.

D.L. Riggin,

Acting Manager, Transport Airplane Directorate, Aircraft Certification

Service.

[FR Doc. 95-22968 Filed 9-14-95; 8:45 am]

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