AD 89-23-16
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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
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Affected Aircraft
All Model C-212 series airplanes, certificated in any category.
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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 Copy URL 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| C-212-CE | C-212-CF | C-212-DE | C-212-DF Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 89-23-16 CITATION: This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:
Document Text
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AD Final Rules - DRS_89-23-16.html Copy URL 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:
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