[Federal Register Volume 62, Number 103 (Thursday, May 29, 1997)]
[Proposed Rules]
[Pages 29086-29088]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 97-13973]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 97-CE-11-AD]
RIN 2120-AA64


Airworthiness Directives; Raytheon Aircraft Company Models 1900, 
1900C, and 1900D Airplanes

AGENCY: Federal Aviation Administration, DOT.


[[Page 29087]]


ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: This document proposes to adopt a new airworthiness directive 
(AD) that would apply to certain Raytheon Aircraft Company (Raytheon) 
Models 1900, 1900C, and 1900D airplanes (formerly referred to as Beech 
Models 1900, 1900C, and 1900D airplanes). The proposed AD would require 
fabricating and installing a placard that restricts the use of the 
forward and aft vent blower assemblies to only the ``OFF'' or ``HIGH'' 
position. The proposed AD would also require incorporating a 
modification that would replace the bearings on the vent blower 
assemblies with improved design bearings, and provide thermal 
protection for the vent blowers, as applicable. Incorporating the 
proposed modification would eliminate the need for the placard. The 
proposed AD is the result of vent blower assembly bearings seizing and 
locking the blower motor on several of the affected airplanes. The 
actions specified by the proposed AD are intended to prevent the vent 
blower assembly bearings from seizing, which could result in smoke 
emanating from the insulating material covering the electrical wiring 
and entering the airplane cabin.

DATES: Comments must be received on or before July 25, 1997.

ADDRESSES: Submit comments in triplicate to the Federal Aviation 
Administration (FAA), Central Region, Office of the Assistant Chief 
Counsel, Attention: Rules Docket No. 97-CE-11-AD, Room 1558, 601 E. 
12th Street, Kansas City, Missouri 64106. Comments may be inspected at 
this location between 8 a.m. and 4 p.m., Monday through Friday, 
holidays excepted.
    Service information that applies to the proposed AD may be obtained 
from the Raytheon Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-
0085. This information also may be examined at the Rules Docket at the 
address above.

FOR FURTHER INFORMATION CONTACT: Mr. Harvey Nero, Aerospace Engineer, 
Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Mid-
Continent Airport, Wichita, Kansas 67209; telephone (316) 946-4137; 
facsimile (316) 946-4407.

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 should 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 that summarizes 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 No. 97-CE-11-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, Central Region, Office of the Assistant Chief Counsel, 
Attention: Rules Docket No. 97-CE-11-AD, Room 1558, 601 E. 12th Street, 
Kansas City, Missouri 64106.

Discussion

    The FAA has received reports of vent blower assembly bearings 
seizing and locking the blower motor on several Raytheon Model 1900D 
airplanes. Power was not interrupted in each of these incidents, and 
high current continued to flow through the low speed resistors. This 
caused smoke to emanate from the insulating material covering the 
electrical wiring. This condition, if not corrected, could result in 
smoke emanating from the insulating material covering the electrical 
wiring and entering the airplane cabin.
    The affected vent blower assemblies incorporate Raytheon (Beech) 
part number (P/N) 114-380028-1 or P/N 114-380028-3.

Relevant Service Information

    Raytheon has issued Service Bulletin No. 2721, Issued: January, 
1997, which specifies the incorporation of the following modification 
kits:

--Electromech Technologies Kit No. EM630-201-1 or EM630-201-2 (as 
appropriate for the blower serial number). When incorporated, these 
kits would replace the bearings in the vent blower assemblies with 
improved design bearings, and provide thermal protection for the vent 
blowers on the P/N 114-380028-1 vent blower assembly. The procedures 
for incorporating these kits are included in the Update Procedures for 
the Electromech Technologies EM630 Blower (Raytheon P/N 114-380028-1 
for Installation of Kit P/N's 630-201-1 and 630-201-2), dated December 
9, 1996; and
--Advanced Industries Kit No. BC80A905. When incorporated, this kit 
would provide thermal protection for the vent blowers on the P/N 114-
380028-3 vent blower assembly. The procedures for incorporating this 
kit are included in Advanced Industries, Inc. Installation Procedure 
for the Resistor Wiring Harness Kit on the BC80A-1 Blower, dated 
December 19, 1996.

The FAA's Determination

    After examining the circumstances and reviewing all available 
information related to the incidents described above, including the 
service information previously referenced, the FAA has determined that 
AD action should be taken to prevent other vent blower assembly 
bearings from seizing, which could result in smoke emanating from the 
insulating material covering the electrical wiring and entering the 
airplane cabin.

Explanation of the Provisions of the Proposed AD

    Since an unsafe condition has been identified that is likely to 
exist or develop in other Raytheon Models 1900, 1900C, and 1900D 
airplanes (formerly referred to as Beech Models 1900, 1900C, and 1900D 
airplanes) of the same type design that are equipped with either P/N 
114-380028-1 vent blower assemblies or P/N 114-380028-3 vent blower 
assemblies, the FAA is proposing an AD. The proposed AD would require 
(1) fabricating and installing a placard that restricts the use of the 
vent blower assemblies; and (2) incorporating a modification that would 
replace the bearings in the vent blower assemblies with improved design 
bearings, and provide thermal protection for the vent blowers, as 
applicable. Incorporating the proposed modification would eliminate the 
need for the placard. Accomplishment of the proposed modifications 
would be required in accordance with the service information previously 
referenced.

[[Page 29088]]

Cost Impact

    The FAA estimates that 500 airplanes in the U.S. registry would be 
affected by the proposed AD, that it would take approximately 7 
workhours per airplane to accomplish the proposed modification, and 
that the average labor rate is approximately $60 an hour. Parts cost 
approximately $500 per airplane. Based on these figures, the total cost 
impact of the proposed AD on U.S. operators is estimated to be 
$460,000. These figures are based on the presumption that no owner/
operator of the affected airplanes has incorporated the proposed 
modification.
    Raytheon has informed the FAA that approximately 700 kits have been 
shipped from the Raytheon Aircraft Authorized Service Center. This is 
enough to equip 350 of the affected airplanes (two vent blower 
assemblies per airplane). Presuming that each of the 350 sets of kits 
is incorporated on an affected airplane, this would reduce the cost 
impact of the proposed AD by $322,000 from $460,000 to $138,000.

Regulatory Impact

    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 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, 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), 40113, 44701.

Sec. 39.13  [Amended]

    2. Section 39.13 is amended by adding a new airworthiness directive 
(AD) to read as follows:

Raytheon Aircraft Company: Docket No. 97-CE-11-AD.

    Applicability: The following model and serial number airplanes, 
certificated in any category, that are equipped with either P/N 114-
380028-1 vent blower assemblies or P/N 114-380028-3 vent blower 
assemblies:

------------------------------------------------------------------------
                Model                            Serial numbers         
------------------------------------------------------------------------
1900.................................  UA-2 and UA-3.                   
1900C................................  UB-1 through UB-74, and UC-1     
                                        through UC-174.                 
1900C (C-12J)........................  UD-1 through UD-6.               
1900D................................   UE-1 through UE-244.            
------------------------------------------------------------------------

    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 request approval for an 
alternative method of compliance in accordance with paragraph (e) 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: Required as indicated in the body of this AD, unless 
already accomplished.
    To prevent the vent blower assembly bearings from seizing, which 
could result in smoke emanating from the insulating material 
covering the electrical wiring and entering the airplane cabin, 
accomplish the following:
    (a) Within the next 100 hours time-in-service (TIS) after the 
effective date of this AD, accomplish the following:
    (1) Fabricate a placard, using letters at least \1/8\-inch in 
height, with the words: ``Operate vent blowers in HIGH or OFF 
position only''.
    (2) Install this placard near the vent blower control switch 
within the pilot's clear view.
    (3) This placard requirement may be terminated when the 
modifications required by paragraph (b) of this AD are incorporated.
    (b) Upon accumulating 2,000 total hours TIS or within the next 
1,000 hours TIS after the effective date of this AD, whichever 
occurs later, incorporate one of the following kits, as applicable, 
in accordance with the referenced kit instructions, as specified in 
Raytheon Service Bulletin No. 2721. Issued: January, 1997:
    (1) For P/N 114-380028-1 vent blower assemblies: Electromech 
Technologies Kit No. EM630-201-1 or EM630-201-2 (as appropriate for 
the blower serial number), in accordance with the Update Procedures 
for the Electromech Technologies EM630 Blower (Raytheon P/N 114-
380028-1 for Installation of Kit P/N's 630-201-1 and 630-201-2), 
dated December 9, 1996. These kits, when incorporated, replace the 
bearings on the vent blower assemblies with improved design 
bearings, and provide thermal protection for the vent blowers; or
    (2) For P/N 114-380028-3: Advanced Industries Kit No. BC80A905 
in accordance with Advanced Industries, Inc. Installation Procedure 
for the Resistor Wiring Harness Kit on the BC80A-1 Blower, dated 
December 19, 1996. This kit, when incorporated, provides thermal 
protection for the vent blowers.
    (c) As of the effective date of this AD, no person may install 
P/N 114-380028-1 or P/N 114-380028-3 vent blower assemblies without 
first incorporating the appropriate kit(s), as referenced in 
paragraphs (b)(1) and (b)(2) of this AD.
    (d) Special flight permits may be issued in accordance with 
sections 21.197 and 21.199 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.
    (e) An alternative method of compliance or adjustment of the 
compliance time that provides an equivalent level of safety may be 
approved by the Manager, Wichita Aircraft Certification Office 
(ACO), 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, 
Kansas 67209. The request shall be forwarded through an appropriate 
FAA Maintenance Inspector, who may add comments and then send it to 
the Manager, Wichita ACO.

    Note 2: Information concerning the existence of approved 
alternative methods of compliance with this AD, if any, may be 
obtained from the Wichita ACO.

    (f) All persons affected by this directive may obtain copies of 
the document referred to herein upon request to the Raytheon 
Aircraft Company, P.O. Box 85, Wichita, Kansas 67201-0085; or may 
examine this document at the FAA, Central Region, Office of the 
Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, 
Missouri 64106.

    Issued in Kansas City, Missouri, on May 21, 1997.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 97-13973 Filed 5-28-97; 8:45 am]
BILLING CODE 4910-13-U