AD 89-23-16

final rule

Airworthiness Directives; CASA Model C-212 Series Airplanes

AD Number
89-23-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-122-AD
FR Citation
This information is not available.
Technical illustration of an aircraft turbine engine assembly
Problem area Engine

Applicability

TypeManufacturerModelDetails
aircraft EADS CASA C-212-CB Airworthiness Directives; CASA Model C-212 Series Airplanes
aircraft EADS CASA C-212-CC Airworthiness Directives; CASA Model C-212 Series Airplanes
aircraft EADS CASA C-212-CD Airworthiness Directives; CASA Model C-212 Series Airplanes
aircraft EADS CASA C-212-CE Airworthiness Directives; CASA Model C-212 Series Airplanes
aircraft EADS CASA C-212-CF Airworthiness Directives; CASA Model C-212 Series Airplanes
aircraft EADS CASA C-212-DE Airworthiness Directives; CASA Model C-212 Series Airplanes
aircraft EADS CASA C-212-DF Airworthiness Directives; CASA Model C-212 Series Airplanes

Unsafe Condition

Damage to or failure of the remaining engine caused by overtorquing following an engine failure on takeoff.

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

Required Actions

Modify the Automatic Power Reserve (APR) system in accordance with CASA Service Bulletin 212-72-05, Revision 1, dated June 1, 1989. Revise the FAA-approved Airplane Flight Manual to include the appropriate revision with new procedures for setting power as specified in the service bulletin.

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

Compliance Time

within 60 days after the effective date of this AD

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

Affected Aircraft

All Model C-212 series airplanes, certificated in any category.

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

Federal Register Abstract

Power Reserve System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_89-23-16.html
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AD Number:
89-23-16
Document Type:
AD Final Rules
Docket Number:
89-NM-122-AD
Subject Heading:
Airworthiness Directives; CASA Model C-212 Series Airplanes
Subject:
Power Reserve System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/12/1989
Make:
EADS CASA
Model:
C-212-CB | C-212-CC | C-212-CD | C-212-CE | C-212-CF | C-212-DE | C-212-DF
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: 89-23-16
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-122-AD

AMENDMENT:   39-6391

AD NUMBER:   89-23-16

SUBJECT HEADING:   Airworthiness Directives; CASA Model C-212 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   DATE: Effective December 12, 1989.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   89-23-16 CASA: Amendment 39-6391. Docket No. 89-NM-122-AD.

Applicability: All Model C-212 series airplanes, certificated in any category.

Compliance: Required within 60 days after the effective date of this AD, unless previously accomplished.

To prevent, following an engine failure on takeoff, damage to or failure of the remaining engine caused by overtorquing, accomplish the following:

A. Modify the Automatic Power Reserve (APR) system in accordance with CASA Service Bulletin 212-72-05, Revision 1, dated June 1, 1989.

B. Upon accomplishment of the modification required by paragraph A., above, revise the FAA-approved Airplane Flight Manual to include the appropriate revision, which provides new procedures for setting power, as specified in Paragraph 1.B. of CASA Service Bulletin 212-72-05, Revision 1, dated June 1, 1989.

C. An 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, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

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 Construcciones Aeronauticas, S.A. (CASA), Getafe, Madrid, Spain. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6391, AD 89-23-16) becomes effective on December 12, 1989.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_89-23-16.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
89-23-16
Document Type:
AD Final Rules
Docket Number:
89-NM-122-AD
Subject Heading:
Airworthiness Directives; CASA Model C-212 Series Airplanes
Subject:
Power Reserve System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/12/1989
Make:
EADS CASA
Model:
C-212-CB | C-212-CC | C-212-CD | C-212-CE | C-212-CF | C-212-DE | C-212-DF
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: 89-23-16
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-122-AD

AMENDMENT:   39-6391

AD NUMBER:   89-23-16

SUBJECT HEADING:   Airworthiness Directives; CASA Model C-212 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   DATE: Effective December 12, 1989.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   89-23-16 CASA: Amendment 39-6391. Docket No. 89-NM-122-AD.

Applicability: All Model C-212 series airplanes, certificated in any category.

Compliance: Required within 60 days after the effective date of this AD, unless previously accomplished.

To prevent, following an engine failure on takeoff, damage to or failure of the remaining engine caused by overtorquing, accomplish the following:

A. Modify the Automatic Power Reserve (APR) system in accordance with CASA Service Bulletin 212-72-05, Revision 1, dated June 1, 1989.

B. Upon accomplishment of the modification required by paragraph A., above, revise the FAA-approved Airplane Flight Manual to include the appropriate revision, which provides new procedures for setting power, as specified in Paragraph 1.B. of CASA Service Bulletin 212-72-05, Revision 1, dated June 1, 1989.

C. An 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, Standardization Branch, ANM-113, FAA, Northwest Mountain Region.

NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who will either concur or comment and then send it to the Manager, Standardization Branch, ANM-113.

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 Construcciones Aeronauticas, S.A. (CASA), Getafe, Madrid, Spain. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Standardization Branch, 9010 East Marginal Way South, Seattle, Washington.

This amendment (39-6391, AD 89-23-16) becomes effective on December 12, 1989.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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