AD 2001-18-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | 720 Series | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| aircraft | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | 720B Series | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| aircraft | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | 111 | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| aircraft | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-1159 | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| aircraft | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-1159A | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| aircraft | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-1159B | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| aircraft | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-159 | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| aircraft | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-IV | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| aircraft | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | Tires | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| appliance | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | 720 Series | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| appliance | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | 720B Series | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| appliance | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | 111 | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| appliance | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-1159 | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| appliance | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-1159A | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| appliance | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-1159B | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| appliance | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-159 | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| appliance | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | G-IV | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
| appliance | The Boeing Company | Gulfstream Aerospace Corporation | Goodyear Tire and Rubber Company | Tires | Airworthiness Directives; Goodyear Tire and Rubber Company Flight Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2 |
Unsafe Condition
Tire tread separations on Goodyear Flight Eagle tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2, with serial numbers 0168xxxx through 0185xxxx, which could result in structural damage to the aircraft, including damage to flaps, engine nacelles, and wheel wells.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect all Goodyear Flight Eagle tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2, to determine if they are within the affected serial number range (0168xxxx through 0185xxxx). Replace any tires within this serial number range.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Goodyear Tire and Rubber Company Flight Eagle tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2, with serial numbers 0168xxxx through 0185xxxx, installed on aircraft including Gulfstream GII, GIIB, GIII, GIV (serial numbers 1000 through 1213, except 1183), and Boeing 720 and 720B.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
This amendment adopts a new airworthiness directive (AD) that applies to certain Goodyear Tire and Rubber Company (Goodyear) Flight Eagle tires, 34X9.25-16 18PR 210MPH, Part Number (P/N) 348F83-2, that are installed on aircraft. This AD requires you to inspect these tires to determine if they are within a certain serial number range and replace any tires within this serial number range. This AD is the result of several instances of main landing gear (MLG) tire tread separations on Gulfstream aircraft. The actions specified by this AD are intended to remove these tires from service to prevent the potential of these tires experiencing tread separations during operation. These tread separations could result in structural damage to the aircraft, including damage to the flaps, engine nacelles, and wheel wells.
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 66, Number 171 (Tuesday, September 4, 2001)]
[Rules and Regulations]
[Pages 46214-46216]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 01-22083]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001-CE-27-AD; Amendment 39-12431; AD 2001-18-05]
RIN 2120-AA64
Airworthiness Directives; Goodyear Tire and Rubber Company Flight
Eagle Tires, 34X9.25-16 18PR 210MPH, Part Number 348F83-2
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: This amendment adopts a new airworthiness directive (AD) that
applies to certain Goodyear Tire and Rubber Company (Goodyear) Flight
Eagle tires, 34X9.25-16 18PR 210MPH, Part Number (P/N) 348F83-2, that
are installed on aircraft. This AD requires you to inspect these tires
to determine if they are within a certain serial number range and
replace any tires within this serial number range. This AD is the
result of several instances of main landing gear (MLG) tire tread
separations on Gulfstream aircraft. The actions specified by this AD
are intended to remove these tires from service to prevent the
potential of these tires experiencing tread separations during
operation. These tread separations could result in structural damage to
the aircraft, including damage to the flaps, engine nacelles, and wheel
wells.
DATES: This AD becomes effective on September 24, 2001.
The FAA must receive any comments on this rule on or before October
12, 2001.
ADDRESSES: Submit comments in triplicate to FAA, Central Region, Office
of the Regional Counsel, Attention: Rules Docket No. 2001-CE-27-AD, 901
Locust, Room 506, Kansas City, Missouri 64106.
You may get the service information referenced in this AD from
Goodyear Global Aviation Tires, Global Product Support, 1144 East
Market Street, Akron, Ohio 44316-0001; telephone: (330) 796-3293;
facsimile: (330) 796-6535; or Gulfstream Aerospace Corporation, 500
Gulfstream Road, P.O. Box 2206, Savannah, Georgia 31402-2206, as
applicable. You may examine this information at FAA, Central Region,
Office of the Regional Counsel, Attention: Rules Docket No. 2001-CE-27-
AD, 901 Locust, Room 506, Kansas City, Missouri 64106.
FOR FURTHER INFORMATION CONTACT: Roy Boffo, Aerospace Engineer, FAA,
Chicago Aircraft Certification Office, 2300 E. Devon Avenue, Des
Plaines, Illinois 60018; telephone: (847) 294-7564; facsimile: (847)
294-7834.
SUPPLEMENTARY INFORMATION:
Discussion
What Events Have Caused This AD?
The FAA has received reports of four incidents of main landing gear
(MLG) tire tread separations on Gulfstream aircraft. Two of these
incidents occurred during takeoff, and the other two are being
investigated.
Goodyear has identified a batch of Flight Eagle tires, 34X9.25-16
18PR 210MPH, Part Number (P/N) 348F83-2, that are susceptible to the
tire tread separations. The serial numbers of this batch are 0168xxxx
through 0185xxxx. This consists of approximately 300 tires.
These tires are installed on, but not limited to, the following
aircraft:
----------------------------------------------------------------------------------------------------------------
Type certificate holder Models Serial numbers
----------------------------------------------------------------------------------------------------------------
Gulfstream Aerospace Corporation....................... GII, GIIB, and GIII All serial numbers.
Gulfstream Aerospace Corporation....................... GIV Serial numbers 1000
through 1213, except
for serial number
1183.
The Boeing Company..................................... 720 and 720B All serial numbers.
----------------------------------------------------------------------------------------------------------------
[[Page 46215]]
What Are the Consequences if the Condition Is Not Corrected?
Tire tread separations, if not prevented, could result in
structural damage to the aircraft. This includes damage to the flaps,
engine nacelles, and wheel wells.
Is There Service Information That Applies to This Subject?
Goodyear has issued Service Bulletin GY SB 2001-32-006, dated July
28, 2001. In addition, Gulfstream Aerospace Corporation has issued
Alert Customer Bulletins #28 (GII/GIIB), #14 (GIII), and #28 (GIV), all
dated July 31, 2001.
These bulletins provide information that relates to removing the
affected tires from service.
The FAA's Determination and an Explanation of the Provisions of
This AD
What Has FAA Decided?
After examining the circumstances and reviewing all available
information related to the subject above, we have determined that:
--The unsafe condition referenced in this document exists or could
develop on type design aircraft equipped with certain Goodyear Flight
Eagle tires, 34X9.25-16 18PR 210MPH, P/N 348F83-2, serial numbers
0168xxxx through 0185xxxx;
--These tires should be removed from service; and
--AD action should be taken in order to correct this unsafe condition
What Would This AD Require?
This AD requires you to inspect all of these tires to determine if
they are within the affected serial number range and replace any tires
within this serial number range.
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 structural damage to the aircraft, including damage to the
flaps, engine nacelles, and wheel wells, FAA finds 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, we invite 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 in triplicate 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?
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of the rule that might
suggest a need to modify the rule. You may examine 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.
We are reviewing the writing style we currently use in regulatory
documents, in response to the Presidential memorandum of June 1, 1998.
That memorandum requires federal agencies to communicate more clearly
with the public. We are interested in your comments on whether the
style of this document is clear, and any other suggestions you might
have to improve the clarity of FAA communications that affect you. You
can get more information about the Presidential memorandum and the
plain language initiative at <a href="http://www.plainlanguage.gov">http://www.plainlanguage.gov</a>.
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. 2001-CE-27-AD.'' We will date stamp and mail
the postcard back to you.
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?
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 (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, 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 AD to read as follows:
2001-18-05 Goodyear Tire and Rubber Company: Amendment 39-12431;
Docket No. 2001-CE-27-AD.
(a) What aircraft are affected by this AD? This AD applies to
aircraft equipped with any Goodyear Flight Eagle tire, 34X9.25-16
18PR 210MPH, Part Number (P/N) 348F83-2. The following is a list of
aircraft where these tires could be installed. This is not a
comprehensive list and aircraft not on this list that have the tires
installed through field approval or other methods are still affected
by this AD:
----------------------------------------------------------------------------------------------------------------
Type certificate holder Models Serial numbers
----------------------------------------------------------------------------------------------------------------
Gulfstream Aerospace Corporation....................... GII, GIIB, and GIII All serial numbers.
[[Page 46216]]
Gulfstream Aerospace Corporation....................... GIV Serial numbers 1000
through 1213, except
for serial number
1183.
The Boeing Company..................................... 720 and 720B All serial numbers.
----------------------------------------------------------------------------------------------------------------
(b) Who must comply with this AD? Anyone who wishes to operate
any aircraft that is equipped with one or more of the above-
referenced Goodyear Flight Eagle tires must comply with this AD.
(c) What problem does this AD address? The actions specified by
this AD are intended to remove these tires from service to prevent
the potential of these tires experiencing tread separations during
operation. These tread separations could result in structural damage
to the aircraft, including damage to the flaps, engine nacelles, and
wheel wells.
(d) What must I do to address this problem? To address this
problem, you must accomplish the following actions:
------------------------------------------------------------------------
Action Compliance time Procedures
------------------------------------------------------------------------
(1) Inspect all Goodyear Within the next Goodyear Service
Flight Eagle tires, 34X9.25- 10 hours time-in- Bulletin GY SB 2001-
16 18PR 210MPH, P/N 348F83-2, service (TIS) 32-006, dated July
to determine if any are after September 28, 2001, and
within the serial number 24, 2001 (the Gulfstream Aerospace
range of 0168xxxx through effective date Corporation Alert
0185xxxx. of this AD). Customer Bulletins
#28 (GII/GIIB), #14
(GIII), and #28
(GIV), all dated
July 31, 2001,
contain information
that relates to this
subject.
(2) Replace any tire found Prior to further Goodyear Service
within the serial number flight after the Bulletin GY SB 2001-
range referenced in paragraph inspection 32-006, dated July
(d)(1) of this AD with an FAA- required by 28, 2001, and
approved tire that is not paragraph (d)(1) Gulfstream Aerospace
Goodyear Flight Eagle, of this AD. Corporation Alert
34X9.25-16 18 PR 210 MPH, P/N Customer Bulletins
348F83-2, serial number #28 (GII/GIIB), #14
0168xxxx through 0185xxxx. (GIII), and #28
(GIV), all dated
July 31, 2001,
contain information
that relates to this
subject.
(3) Do not install, on any As of September Not Applicable.
airplane, a Goodyear Flight 24, 2001 (the
Eagle tire, 34X9.25-16 18 PR effective date
210MPH, P/N 348F83-2, that is of this AD).
within the serial number
range of 0168xxxx through
0185xxxx.
------------------------------------------------------------------------
(e) Can I comply with this AD in any other way? You may use an
alternative method of compliance or adjust the compliance time if:
(1) Your alternative method of compliance provides an equivalent
level of safety; and
(2) The Manager, Chicago Aircraft Certification Office, approves
your alternative. Send your request through an FAA Principal
Maintenance Inspector, who may add comments and then send it to the
Manager, Chicago Aircraft Certification Office.
Note: This AD applies to any aircraft with a tire installed as
identified in paragraph (a) of this AD, regardless of whether the
aircraft 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 (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 you have not
eliminated the unsafe condition, specific actions you propose to
address it.
(f) Where can I get information about any already-approved
alternative methods of compliance? Contact Roy Boffo, Aerospace
Engineer, FAA, Chicago Aircraft Certification Office, 2300 E. Devon
Avenue, Des Plaines, Illinois 60018; telephone: (847) 294-7564;
facsimile: (847) 294-7834.
(g) What if I need to fly the airplane to another location to
comply with this AD? The FAA can issue a special flight permit under
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate your airplane to a location where
you can accomplish the requirements of this AD.
(h) How do I get copies of the documents referenced in this AD?
You may obtain copies of the documents referenced in this AD from
Goodyear Global Aviation Tires, Global Product Support, 1144 East
Market Street, Akron, Ohio 44316-0001; telephone: (330) 796-3293;
facsimile: (330) 796-6535; or Gulfstream Aerospace Corporation, 500
Gulfstream Road, P.O. Box 2206, Savannah, Georgia 31402-2206, as
applicable. You may examine these documents at FAA, Central Region,
Office of the Regional Counsel, 901 Locust, Room 506, Kansas City,
Missouri 64106.
(i) When does this amendment become effective? This amendment
becomes effective on September 24, 2001.
Issued in Kansas City, Missouri, on August 27, 2001.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 01-22083 Filed 8-31-01; 8:45 am]
BILLING CODE 4910-13-U
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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