[Federal Register Volume 63, Number 199 (Thursday, October 15, 1998)]
[Rules and Regulations]
[Pages 55321-55324]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-27605]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 98-CE-88-AD; Amendment 39-10844; AD 98-21-21]
RIN 2120-AA64


Airworthiness Directives; Bob Fields Aerocessories Inflatable 
Door Seals

AGENCY: Federal Aviation Administration, DOT.

ACTION: Final rule; request for comments.

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SUMMARY: This document publishes in the Federal Register an amendment 
adopting Airworthiness Directive (AD) 98-21-21, which was sent 
previously to all known U.S. owners and operators of aircraft equipped 
with Bob Fields Aerocessories inflatable door seals installed in 
accordance with the applicable supplemental type certificate (STC). 
These inflatable door seals could also be installed on aircraft through 
field approval.This AD requires either de-activating the electric door 
seal inflation system; fabricating and installing a placard specifying 
that the system is inoperative; and inserting a copy of the AD into the 
Limitations Section of the airplane flight manual (AFM); or removing 
all provisions of the Bob Fields Aerocessories inflatable door seals 
installation, and installing original equipment manufacturer door seals 
or an FAA-approved equivalent that is of different design than the 
referenced Bob Fields Aerocessories inflatable door seals. The AD 
resulted from occurrences of overheated components associated with the 
electric door seal inflation system on aircraft equipped with the 
affected inflatable door seals. The actions specified by this AD are 
intended to prevent smoke and a possible fire in the cockpit caused by 
overheating of the electric door seal inflation systems, which could 
result in passenger injury.

DATES: Effective October 30, 1998, to all persons except those to whom 
it was made immediately effective by priority letter AD 98-21-21, 
issued October 2, 1998, which contained the requirements of this 
amendment.
    Comments for inclusion in the Rules Docket must be received on or 
before December 13, 1998.

ADDRESSES: Submit comments in triplicate to the Federal Aviation 
Administration (FAA), Central Region, Office of the Regional Counsel, 
Attention: Rules Docket 98-CE-88-AD, Room 1558, 601 E. 12th Street, 
Kansas City, Missouri 64106.
    Information related to this AD may be examined at the FAA at the 
address referenced above.

FOR FURTHER INFORMATION CONTACT: Mr. Paul S. Wells, Jr., Aerospace 
Engineer, FAA, Los Angeles Aircraft Certification Office, 3960 
Paramount Boulevard, Lakewood, California 90712; telephone: (562) 627-
5354; facsimile: (562) 627-5210.

SUPPLEMENTARY INFORMATION:

Discussion

    On October 2, 1998, the FAA issued priority letter AD 98-21-21, 
which applies to aircraft equipped with Bob Fields Aerocessories 
inflatable door seals installed in accordance with either the 
applicable supplemental type certificate (STC) or through field 
approval. This AD requires either:

--de-activating the electric door seal inflation system; fabricating 
and installing a placard specifying that the system is inoperative; and 
inserting a copy of the AD into the Limitations Section of the airplane 
flight manual (AFM); or
--removing all provisions of the Bob Fields Aerocessories inflatable 
door seals installation, and installing original equipment manufacturer 
door seals or an FAA-approved equivalent that is of different design 
than the referenced Bob Fields Aerocessories inflatable door seals.

    That AD resulted from numerous reported occurrences of overheated 
components associated with the electric door seal inflation system on 
aircraft equipped with Bob Fields Aerocessories inflatable door seals 
installed in accordance with the applicable supplemental type 
certificate (STC).
    One of the above-referenced occurrences resulted in a safety 
recommendation from the National Transportation Safety Board (NTSB). In 
this incident, an in-flight electrical fire caused the pilot of a 
Cessna Model P210N to initiate an emergency descent with a successful 
landing and only minor airplane damage. NTSB investigation revealed 
that the fire originated on the cabin sidewall, under the left side of 
the instrument panel and resulted in burned vinyl, plastic, and 
insulation material. An overheated resistor used in an electric door 
seal inflation system caused the fire. The resistor was used to reduce 
the 28-volt aircraft electrical system's voltage to meet the power 
requirements of the door seal system's 14-volt air pump motor.
    The inflatable door seals on this airplane were installed in 
accordance with STC SA4212WE, which the FAA issued to Bob Fields 
Aerocessories. The purpose of the seals is to decrease in-flight cabin 
noise caused by ill-fitting cabin doors. The FAA has issued

[[Page 55322]]

numerous other STC's that allow this installation on other make and 
model airplanes. In addition, these Bob Fields Aerocessories inflatable 
door seals could be installed on aircraft through field approvals.
    All of the aircraft involved in the occurrences incorporate Bob 
Fields Aerocessories inflatable door seals. Investigation results of 
three other occurrences reveal the following:

--An electric door seal inflation pump that was mounted on the forward 
side of the nose bulkhead was found heavily charred;
--The pump assembly and resistors of the electric door seal inflation 
system were partially melted; and
--Vinyl, plastic, and insulation material in the proximity of the 
electric door seal inflation system were found burned.

    Further analysis of all of these occurrences revealed leaks in the 
Bob Fields Aerocessories inflatable door seals. Each electric door seal 
inflation system consists of an electric motor, an air pump, inflatable 
silicon door seals, a pressure sensing switch, an air supply control 
valve, a resistor assembly, a 7.5-amp in-line fuse, a caution light, 
and electrical wiring. The motor draws power directly from the 
airplane's battery bus and is used to inflate the door seals to a 
pressure of about 10 pounds per square inch (psi). A sensor in the air 
pump determines when the pressure drops below 10 psi, at which time the 
air pump motor starts back up again until obtaining proper pressure. 
The standard time period for the air pump to inflate the door seal is 
about 4 to 12 seconds. During this time, the caution light remains 
illuminated.
    If the door seal has a small leak, the pump turns on and off to 
maintain the desired inflation pressure. When this small leak develops 
to a larger leak, the air pump may run continuously to keep the door 
seal inflated. This could cause the resistors or the air pump motor to 
overheat. This would cause smoke and a possible fire in the cockpit.

The FAA's Determination and Explanation of the AD

    Since an unsafe condition has been identified that is likely to 
exist or develop in other aircraft equipped with Bob Fields 
Aerocessories inflatable door seals installed in accordance with either 
the applicable supplemental type certificate (STC) or through field 
approval, the FAA issued priority letter AD 98-21-21 to prevent smoke 
and a possible fire in the cockpit caused by overheating of the 
electric door seal inflation systems, which could result in passenger 
injury.

Determination of the Effective Date of the AD

    Since it was found that immediate corrective action was required, 
notice and opportunity for prior public comment thereon were 
impracticable and contrary to the public interest, and good cause 
existed to make the AD effective immediately by individual letters 
issued on October 2, 1998, to all known U.S. operators of aircraft 
equipped with the affected inflatable door seals that were installed in 
accordance with the applicable STC. These conditions still exist, and 
the AD is hereby published in the Federal Register as an amendment to 
section 39.13 of the Federal Aviation Regulations (14 CFR 39.13) to 
make it effective as to all persons.

Comments Invited

    Although this action is in the form of a final rule that involves 
requirements affecting immediate flight safety and, thus, was not 
preceded by notice and opportunity to comment, comments are invited on 
this rule. Interested persons are invited to comment on this 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 will be considered, 
and this rule may be amended in light of the comments received. Factual 
information that supports the commenter's ideas and suggestions is 
extremely helpful in evaluating the effectiveness of the AD action and 
determining whether additional rulemaking action would be needed.
    Comments are specifically invited on the overall regulatory, 
economic, environmental, and energy aspects of the rule that might 
suggest a need to modify the 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 
AD will be filed in the Rules Docket.
    Commenters wishing the FAA to acknowledge receipt of their comments 
submitted in response to this rule must submit a self-addressed, 
stamped postcard on which the following statement is made: ``Comments 
to Docket No. 98-CE-88-AD.'' The postcard will be date stamped and 
returned to the commenter.

Regulatory Impact

    The regulations adopted herein will 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 final 
rule does not have sufficient federalism implications to warrant the 
preparation of a Federalism Assessment.
    The FAA has 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. A copy of it, if filed, may 
be obtained from 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.

Adoption of the Amendment

    Accordingly, pursuant to 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 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:

98-21-21 Bob Fields Aerocessories: Amendment 39-10844; Docket No. 
98-CE-88-AD.

    Applicability: Inflatable door seals, installed either in 
accordance with the applicable supplemental type certificate (STC) 
or through field approval, that are installed on, but not limited 
to, the following aircraft:

[[Page 55323]]



------------------------------------------------------------------------
         Affected STC               Make and model aircraft affected
------------------------------------------------------------------------
SA3735NM.....................  Cessna Models 170, 170A, and 170B
                                Airplanes.
SA4136WE.....................  Cessna Models 310, 310A, 310B, 310C,
                                310D, 310E, 310F, 310G, 310H, 310I,
                                310J, 310K, 310L, 310N, 310P, 310Q,
                                310R, T310P, T310Q, and T310R Airplanes.
SA2226NM.....................  Cessna Models P210N and P210R Airplanes.
SA3736NM.....................  Cessna Models 185, 185A, 185B, 185C,
                                185D, A185E, and A185F Airplanes.
SA4177WE.....................  Cessna Models 175, 175A, 175B, and 175C
                                Airplanes.
SA4212WE.....................  Cessna Models 210, 210A, 210B, 210C,
                                210D, 210E, 210F, 210G, 210H, 210J,
                                210K, 210L, 210M, 210N, T210F, T210G,
                                T210H, T210J, T210K, T210L, T210M,
                                T210N, 210-5 (205), and 210-5A (205A)
                                Airplanes.
SA4213WE.....................  Cessna Models 310, 310A, 310B, 310C,
                                310D, 310F, 310G, 310H, 310I, 310J,
                                310K, 310L, 310N, 310P, 310Q, 310R,
                                T310P, T310Q, and T310R Airplanes.
SA4283WE.....................  Cessna Models 172, 172A, 172B, 172C,
                                172D, 172E, 172F, 172G, 172H, 172I,
                                172K, 172L, 172M, and 172N Airplanes.
SA4284WE.....................  Cessna Models 180, 180A, 180B, 180C,
                                180D, 180E, 180F, 180G, 180H, 180J, and
                                180K Airplanes.
SA4285WE.....................  Cessna Models 182, 182A, 182B, 182C,
                                182D, 182E, 182F, 182G, 182H, 182J,
                                182K, 182L, 182M, 182N, 182P, 182Q,
                                R182, and TR182 Airplanes.
SA4286WE.....................  Cessna Models 206, P206, P206A, P206B,
                                P206C, P206D, P206E, TP206A, TP206B,
                                TP206C, TP206D, TP206E, U206, U206A,
                                U206B, U206C, U206D, U206E, U206F,
                                U206G, TU206A, TU206B, TU206C, TU206D,
                                TU206E, TU206F, and TU206G Airplanes.
SA4287WE.....................  Cessna Models 320, 320A, 320B, 320C,
                                320D, 320E, 320F, and 320-1 Airplanes.
SA4180WE.....................  Raytheon (Beech) Models H35, J35, K35,
                                M35, N35, P35, S35, V35, V35A, V35B, 35-
                                33, 35-A33, 35-B33, 35-C33, 35-C33A,
                                E33, E33A, E33C, F33, F33A, F33C, G33,
                                36, A36, A36TC, and B36TC Airplanes.
SA4184WE.....................  Raytheon (Beech) Models 95, B95, B95A,
                                E95, 95-55, 95-A55, 95-B55, 95-B5A, 95-
                                B55B, 95-C55, D55, E55, 56TC, 58, and
                                58A Airplanes.
SA4239WE.....................  Raytheon (Beech) Models 58P, 58PA, 58TC,
                                and 58TCA Airplanes.
SA4240WE.....................  Raytheon (Beech) Models 50, B50, C50,
                                D50, D50A, D50B, D50C, D50E, D50E-5990,
                                E50, F50, G50, H50, and J50 Airplanes.
SA4282WE.....................  Raytheon (Beech) Models 35, A35, B35,
                                C35, D35, E35, F35, G35, and 35R
                                Airplanes.
SA4178WE.....................  Mooney Models M20, M20A, M20C, M20D,
                                M20E, M20F, M20G, M20J, and M20K
                                Airplanes.
SA4472NM.....................  Aerostar Models PA-60-601P, PA-60-602P,
                                and PA-60-700P Airplanes.
SA4234WE.....................  The New Piper Aircraft, Inc. (Piper)
                                Models PA-34-200, PA-34-200T, and PA-34-
                                220T Airplanes.
SA4179WE.....................  Piper Models PA-24, PA-24-250, PA-24-260,
                                and PA-24-400 Airplanes.
SA4235WE.....................  Piper Models PA-44-180 and PA-44-180T
                                Airplanes.
SA4236WE.....................  Piper Models PA-28-140, PA-28-150, PA-28-
                                160, PA-28-180, PA-28-235, PA-28-151, PA-
                                28-181, PA-28-161, PA-28-236, PA-28-
                                201T, PA-285-160, PA-28S-160, PA-28S-
                                180, PA-28R-180, PA-28R-200, PA-28R-201,
                                PA-28R-201T, PA-28RT-201, and PA-28RT-
                                201T Airplanes.
SA4237WE.....................  Piper Models PA-23, PA-23-160, PA-23-235,
                                PA-23-250, and PA-E23-250 Airplanes.
SA4238WE.....................  Piper Models PA-30, PA-39, and PA-40
                                Airplanes.
SA4385WP.....................  Piper Models PA-31, PA-31-300, PA-31-325,
                                and PA-31-350 Airplanes.
SA4288WE.....................  Piper Models PA-32-260, PA-32-300, PA-32S-
                                300, PA-32-301, PA-32-301T, PA-32R-300,
                                PA-32R-301, PA-32R-301T, PA-32RT-300,
                                and PA-32RT-300T Airplanes.
SA2511NM.....................  Bellanca Models 17-30, 17-31, and 17-31TC
                                Airplanes.
SA2510NM.....................  Bellanca Models 17-30A, 17-31A, and 17-
                                31ATC Airplanes.
SA4316WE.....................  Wing Aircraft Company Model D-1
                                Airplanes.
------------------------------------------------------------------------

    Note 1: This AD applies to each aircraft identified in the 
preceding applicability provision that has the affected inflatable 
door seals installed, regardless of whether it has been modified, 
altered, or repaired in the area subject to the requirements of this 
AD. For aircraft 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 (f) 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 prior to further flight after the effective 
date of this AD, unless already accomplished.
    To prevent smoke and a possible fire in the cockpit caused by 
overheating of the electric door seal inflation systems, which could 
result in passenger injury, accomplish the following:
    (a) Deactivate the electric door seal inflation system by 
accomplishing the following:
    (1) Disconnect the battery.
    (2) Locate the air pump and identify the power wire to the air 
pump.
    (3) Trace the power wire to its connection to the airplane's 
original electrical power system. Disconnect the power wire at its 
attachment to the airplane's electrical power system and stow the 
wire end.
    (4) For non-pressurized airplanes or for airplanes that have an 
operating manual door seal inflation system, fabricate a placard 
that incorporates the following words utilizing letters that are at 
least 0.10-inch in height, and install this placard on the 
instrument panel within the pilot's clear view:

``ELECTRIC DOOR SEAL INFLATION SYSTEM INOPERATIVE''

    (5) For pressurized airplanes or for airplanes that do not have 
an operating manual door seal inflation system, fabricate a placard 
that incorporates the following words utilizing letters that are at 
least 0.10-inch in height, and install this placard on the 
instrument panel within the pilot's clear view:

``ELECTRIC DOOR SEAL INFLATION SYSTEM INOPERATIVE. THIS AIRPLANE CAN 
ONLY BE OPERATED IN UNPRESSURIZED FLIGHT''

    (6) Reconnect the battery before returning to service.
    (b) Insert a copy of this AD into the Limitations Section of the 
airplane flight manual (AFM).
    (c) As an alternative method of compliance to the actions of 
paragraph (a), including all subparagraphs, and paragraph (b) of 
this AD, remove all provisions of the Bob Fields Aerocessories 
inflatable door seals, and install original equipment manufacturer 
door seals or an FAA-approved equivalent that is of different design 
than the referenced Bob Fields Aerocessories inflatable door seals.
    (d) As of the effective date of this AD, no person may install 
on any aircraft, Bob Fields Aerocessories inflatable door seals 
either in accordance with the applicable STC or through field 
approval.
    (e) Special flight permits may be issued in accordance with 
Secs. 21.197 and 21.199 of the

[[Page 55324]]

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 provided the following are adhered to, as applicable:
    (1) Locate and remove the in-line fuse for the electric door 
seal inflation system; or
    (2) Pull the system circuit breaker for the electric door seal 
inflation system; and
    (3) For pressurized airplanes or for airplanes that do not have 
an operating manual door seal inflation system, operate the airplane 
in unpressurized flight only.
    (f) An alternative method of compliance or adjustment of the 
compliance time that provides an equivalent level of safety may be 
approved by the Manager, FAA, Los Angeles Aircraft Certification 
Office (ACO), 3960 Paramount Blvd., Lakewood, California 90712. The 
request shall be forwarded through an appropriate FAA Maintenance 
Inspector, who may add comments and then send it to the Manager, Los 
Angeles ACO.

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

    (g) Information related to this AD may be examined at the FAA, 
Central Region, Office of the Regional Counsel, Room 1558, 601 E. 
12th Street, Kansas City, Missouri 64106.
    (h) This amendment becomes effective on October 30, 1998, to all 
persons except those persons to whom it was made immediately 
effective by priority letter AD 98-21-21, issued October 2, 1998, 
which contained the requirements of this amendment.

    Issued in Kansas City, Missouri, on October 7, 1998.
Marvin R. Nuss,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 98-27605 Filed 10-14-98; 8:45 am]
BILLING CODE 4910-13-U