AD 89-03-01 R1

final rule

Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires

AD Number
89-03-01 R1
Status
final_rule
Effective Date
Product Category
appliance
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Applicability

TypeManufacturerModelDetails
aircraft ATR - GIE Avions de Transport R gional | Goodyear ATR42-200 Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
aircraft ATR - GIE Avions de Transport R gional | Goodyear ATR42-300 Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
aircraft ATR - GIE Avions de Transport R gional | Goodyear ATR42-320 Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
aircraft ATR - GIE Avions de Transport R gional | Goodyear ATR42-500 Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
aircraft ATR - GIE Avions de Transport R gional | Goodyear Tires Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
appliance ATR - GIE Avions de Transport R gional | Goodyear ATR42-200 Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
appliance ATR - GIE Avions de Transport R gional | Goodyear ATR42-300 Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
appliance ATR - GIE Avions de Transport R gional | Goodyear ATR42-320 Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
appliance ATR - GIE Avions de Transport R gional | Goodyear ATR42-500 Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
appliance ATR - GIE Avions de Transport R gional | Goodyear Tires Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires

Unsafe Condition

Tire failure due to potential structural defects in Goodyear 32x8.8R16, 10PR, P/N 328Q08G2 radial tires with serial dates 8060Gxxx and above.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Remove from service tires with serial dates between 8060Gxxx and 8320Gxxx based on landing counts: those with 250+ landings since new must be removed within next 50 landings; those with less than 250 landings must be removed at or before 300 landings; tires without records must be removed within next 50 landings. Tires with serial dates 8340Gxxx and above must be removed within next 150 landings if they have 250+ landings, at or before 400 landings if under 250, or within 150 landings if no records. Allow ferrying under FAR 21.197/199 and consider alternate compliance via FAA approval.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Effective November 13, 1989. Compliance required as indicated in paragraphs (a) and (b) based on landing counts.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Goodyear 32x8.8R16, 10PR, P/N 328Q08G2 radial tires with serial dates 8060Gxxx and above, installed on but not limited to ATR-42 aircraft.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Radial Tires

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_89-03-01_R.html
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AD Number:
89-03-01 R1
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
Subject:
Radial Tires
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/13/1989
Make:
ATR - GIE Avions de Transport R gional | Goodyear
Model:
ATR42-200 | ATR42-300 | ATR42-320 | ATR42-500 | Tires
Product Type:
Appliance
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 89-03-01 R1
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-6334

AD NUMBER:   89-03-01 R1

SUBJECT HEADING:   Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires

ACTION:  

SUMMARY:  

DATES:   Effective November 13, 1989.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
89-03-01 R1 GOODYEAR: Amendment 39-6103 as revised by Amendment 39-6334.

Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 radial tires, with serial dates 8060Gxxx and above, installed on but not limited to ATR-42 aircraft.

Compliance: Required as indicated, unless already accomplished.

To prevent tire failure, accomplish the following:

(a) Remove from service, all tires with serial dates between 8060Gxxx and 8320Gxxx, as follows:

(1) Tires which have accumulated 250 or more landings since new on the effective date of this AD, within the next 50 landings.

(2) Tires which have accumulated less than 250 landings since new on the effective date of this AD, at or prior to accumulating 300 landings.

(3) Tires for which no landing record has been maintained, within the next 50 landings.

(b) Remove from service, all tires with serial dates 8340Gxxx and above, as follows:

(1) Tires which have accumulated 250 or more landings since new on the effective date of this AD, within the next 150 landings.

(2) Tires which have accumulated less than 250 landings since new on the effective date of this AD, at or prior to accumulating 400 landings.

(3) Tires for which no landing record has been maintained, within the next 150 landings.

NOTES: (1) Tires with serial dates 8060Gxxx and above may be used as replacements subject to the restrictions of paragraphs (a) and (b) above. Tires with serial dates prior to 8060Gxxx are approved without restrictions.

(2) Goodyear Alert Service Bulletins 32-001, dated December 5, 1988, and 32-002, Revision 1, dated July 14, 1989, apply to this AD.

(c) Aircraft may be ferried in accordance with the provisions of FAR 21.197 and 21.199 to a base where the AD can be accomplished.

(d) Upon submission of substantiating data by an owner or operator through an FAA Airworthiness Inspector, an alternate method of compliance with the requirements of this AD or adjustments to the compliance times specified in this AD may be approved by the Manager, Boston Aircraft Certification Office, Engine and Propeller Directorate, Aircraft Certification Service, Federal Aviation Administration, 12 New England Executive Park, Burlington, Massachusetts 01803.

This AD revises AD 89-03-01, Amendment 39-6103 (54 FR 1342; January 13, 1989) which became effective on February 12, 1989.

This amendment (39-6334, AD 89-03-01 R1) becomes effective on November 13, 1989.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_89-03-01_R.html
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Print/Save as PDF
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 Feedback
Details
AD Number:
89-03-01 R1
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires
Subject:
Radial Tires
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/13/1989
Make:
ATR - GIE Avions de Transport R gional | Goodyear
Model:
ATR42-200 | ATR42-300 | ATR42-320 | ATR42-500 | Tires
Product Type:
Appliance
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 89-03-01 R1
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-6334

AD NUMBER:   89-03-01 R1

SUBJECT HEADING:   Airworthiness Directives; GOODYEAR: Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 Radial Tires

ACTION:  

SUMMARY:  

DATES:   Effective November 13, 1989.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
89-03-01 R1 GOODYEAR: Amendment 39-6103 as revised by Amendment 39-6334.

Applicability: 32x8.8R16, 10PR, P/N 328Q08G2 radial tires, with serial dates 8060Gxxx and above, installed on but not limited to ATR-42 aircraft.

Compliance: Required as indicated, unless already accomplished.

To prevent tire failure, accomplish the following:

(a) Remove from service, all tires with serial dates between 8060Gxxx and 8320Gxxx, as follows:

(1) Tires which have accumulated 250 or more landings since new on the effective date of this AD, within the next 50 landings.

(2) Tires which have accumulated less than 250 landings since new on the effective date of this AD, at or prior to accumulating 300 landings.

(3) Tires for which no landing record has been maintained, within the next 50 landings.

(b) Remove from service, all tires with serial dates 8340Gxxx and above, as follows:

(1) Tires which have accumulated 250 or more landings since new on the effective date of this AD, within the next 150 landings.

(2) Tires which have accumulated less than 250 landings since new on the effective date of this AD, at or prior to accumulating 400 landings.

(3) Tires for which no landing record has been maintained, within the next 150 landings.

NOTES: (1) Tires with serial dates 8060Gxxx and above may be used as replacements subject to the restrictions of paragraphs (a) and (b) above. Tires with serial dates prior to 8060Gxxx are approved without restrictions.

(2) Goodyear Alert Service Bulletins 32-001, dated December 5, 1988, and 32-002, Revision 1, dated July 14, 1989, apply to this AD.

(c) Aircraft may be ferried in accordance with the provisions of FAR 21.197 and 21.199 to a base where the AD can be accomplished.

(d) Upon submission of substantiating data by an owner or operator through an FAA Airworthiness Inspector, an alternate method of compliance with the requirements of this AD or adjustments to the compliance times specified in this AD may be approved by the Manager, Boston Aircraft Certification Office, Engine and Propeller Directorate, Aircraft Certification Service, Federal Aviation Administration, 12 New England Executive Park, Burlington, Massachusetts 01803.

This AD revises AD 89-03-01, Amendment 39-6103 (54 FR 1342; January 13, 1989) which became effective on February 12, 1989.

This amendment (39-6334, AD 89-03-01 R1) becomes effective on November 13, 1989.

FOOTER:

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Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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