AD 87-16-04
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
Failure of the stall warning system to provide adequate warning could result in inadvertent stalls.
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Required Actions
Install an artificial stall warning system in accordance with CASA Service Bulletin S/B 212-31-12 dated May 12, 1987, or other approved method. An alternate means of compliance or adjustment may be used if approved by the FAA. Special flight permits may be issued under FAR 21.197 and 21.199.
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Compliance Time
Prior to January 31, 1988
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Affected Aircraft
CASA Model C-212 series airplanes including Indonesian manufactured serial numbers 64N and 73N
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Federal Register Abstract
Stall Warning System
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_87-16-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 87-16-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CASA Model C-212 Series Airplanes Subject: Stall Warning System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/31/1987 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| C-212-CE | C-212-CF | C-212-DE | C-212-DF Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 87-16-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5686 AD NUMBER: 87-16-04 SUBJECT HEADING: Airworthiness Directives; CASA Model C-212 Series Airplanes ACTION: SUMMARY: DATES: Effective August 31, 1987. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 87-16-04 CASA: Amendment 39-5686. Applies to all Model C-212 series airplanes, including Indonesian manufactured C-212's Serial Numbers 64N and 73N, certificated in any category. Compliance required as indicated, unless previously accomplished. To prevent inadvertent stalls, accomplish the following: A. Prior to January 31, 1988, install an artificial stall warning system in accordance with CASA Service Bulletin S/B 212-31-12, dated May 12, 1987, or other manner approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. B. 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. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of the modifications required by this AD. All persons affected by this directive who have not already received the appropriate service document from the manufacturer may obtain copies upon request to Construcciones Aeronauticas S.A., Getafe, Madrid, Spain. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective August 31, 1987. FOOTER:
Document Text
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AD Final Rules - DRS_87-16-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 87-16-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CASA Model C-212 Series Airplanes Subject: Stall Warning System Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/31/1987 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: 87-16-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5686 AD NUMBER: 87-16-04 SUBJECT HEADING: Airworthiness Directives; CASA Model C-212 Series Airplanes ACTION: SUMMARY: DATES: Effective August 31, 1987. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 87-16-04 CASA: Amendment 39-5686. Applies to all Model C-212 series airplanes, including Indonesian manufactured C-212's Serial Numbers 64N and 73N, certificated in any category. Compliance required as indicated, unless previously accomplished. To prevent inadvertent stalls, accomplish the following: A. Prior to January 31, 1988, install an artificial stall warning system in accordance with CASA Service Bulletin S/B 212-31-12, dated May 12, 1987, or other manner approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. B. 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. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of the modifications required by this AD. All persons affected by this directive who have not already received the appropriate service document from the manufacturer may obtain copies upon request to Construcciones Aeronauticas S.A., Getafe, Madrid, Spain. This document may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective August 31, 1987. FOOTER:
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