AD 90-11-10

final rule

Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes

AD Number
90-11-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-144-AD
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 757-200 Series Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes
aircraft The Boeing Company 757-200CB Series Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes
aircraft The Boeing Company 757-200PF Series Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes
aircraft The Boeing Company 757-300 Series Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes
aircraft The Boeing Company 767-200 Series Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes
aircraft The Boeing Company 767-300 Series Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes
aircraft The Boeing Company 767-300F Series Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes

Unsafe Condition

Intermittent altitude hold, altitude capture, and/or flight director mistracking anomalies due to Collins flight control computers (FCC) with specific Boeing part numbers (S241T100-103, -105, -106).

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

Required Actions

Remove Collins FCCs with Boeing P/N S241T100-103 and replace with reworked units P/N S241T100-108 within 24 months. Remove FCCs with P/N S241T100-105/-106 and replace with P/N S241T100-108 within 12 months. Follow Collins Service Bulletins FCC-701-22-10 (Rev 2) and FCC-701-22-16.

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

Compliance Time

Within the next 24 months after the effective date of this AD (July 2, 1990) for P/N S241T100-103; within the next 12 months after the effective date for P/N S241T100-105/-106.

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

Affected Aircraft

BOEING Model 757 and 767 series airplanes equipped with Collins flight control computers (FCC), certified in any category.

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

Federal Register Abstract

Flight Control Computers

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_90-11-10.html
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AD Number:
90-11-10
Document Type:
AD Final Rules
Docket Number:
89-NM-144-AD
Subject Heading:
Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes
Subject:
Flight Control Computers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/02/1990
Make:
The Boeing Company
Model:
757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 Series | 767-200 Series | 767-300 Ser...Show more
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-11-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-144-AD

AMENDMENT:   39-6608

AD NUMBER:   90-11-10

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective July 2, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-11-10 BOEING: Amendment 39-6608. Docket No. 89-NM-144-AD.

Applicability: Model 757 and 767 series airplanes, equipped with Collins flight control computers (FCC), certified in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent intermittent altitude hold, altitude capture, and/or flight director mistracking anomalies, accomplish the following:

A. Within the next 24 months after the effective date of this AD, remove Collins manufactured FCC's which have Boeing P/N S241T100-103, and replace with units reworked to P/N S241T100-108, in accordance with Collins Service Bulletins FCC-701-22-10, Revision 2, dated March 24, 1988, and FCC-701-22-16, dated October 14, 1988.

B. Within the next 12 months after the effective date of this AD, remove Collins manufactured FCC's which have Boeing P/N S241T100-105 or -106, and replace with units reworked to P/N S241T100-108, in accordance with Collins Service Bulletin FCC-701-22-16, dated October 14, 1988.

C. Alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Avionics Inspector, who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office.

D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6608, AD 90-11-10) becomes effective on July 2, 1990.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_90-11-10.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
90-11-10
Document Type:
AD Final Rules
Docket Number:
89-NM-144-AD
Subject Heading:
Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes
Subject:
Flight Control Computers
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/02/1990
Make:
The Boeing Company
Model:
757-200 Series | 757-200CB Series | 757-200PF Series | 757-300 Series | 767-200 Series | 767-300 Ser...Show more
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 90-11-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-144-AD

AMENDMENT:   39-6608

AD NUMBER:   90-11-10

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 757 and 767 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective July 2, 1990.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
90-11-10 BOEING: Amendment 39-6608. Docket No. 89-NM-144-AD.

Applicability: Model 757 and 767 series airplanes, equipped with Collins flight control computers (FCC), certified in any category.

Compliance: Required as indicated, unless previously accomplished.

To prevent intermittent altitude hold, altitude capture, and/or flight director mistracking anomalies, accomplish the following:

A. Within the next 24 months after the effective date of this AD, remove Collins manufactured FCC's which have Boeing P/N S241T100-103, and replace with units reworked to P/N S241T100-108, in accordance with Collins Service Bulletins FCC-701-22-10, Revision 2, dated March 24, 1988, and FCC-701-22-16, dated October 14, 1988.

B. Within the next 12 months after the effective date of this AD, remove Collins manufactured FCC's which have Boeing P/N S241T100-105 or -106, and replace with units reworked to P/N S241T100-108, in accordance with Collins Service Bulletin FCC-701-22-16, dated October 14, 1988.

C. Alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Avionics Inspector, who will either concur or comment and then send it to the Manager, Seattle Aircraft Certification Office.

D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplanes, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or Seattle Aircraft Certification Office, FAA, Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6608, AD 90-11-10) becomes effective on July 2, 1990.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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