AD 89-22-09

final rule

Airworthiness Directives; CASA Model C-212 Series Airplanes

AD Number
89-22-09
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-111-AD
FR Citation
This information is not available.

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

The passenger door evacuation could be delayed due to the installation of a passenger entry step under STC SA906GL, which includes modifications to the door latch and associated hardware.

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

Required Actions

Remove the step, handrails, door latch modifications, and associated hardware installed per Fischer Brothers Aviation, Inc. Installation Instructions FBD-206 Rev F dated June 5, 1985, and restore the door handle to the original CASA configuration. Alternate compliance may be approved by the Manager, Chicago Aircraft Certification Office.

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, unless previously accomplished

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

Affected Aircraft

CASA Model C-212 series airplanes equipped with a passenger entry step installed under STC SA906GL

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

Federal Register Abstract

Passenger Door Evacuation

Applicability Source Text

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AD Number:
89-22-09
Document Type:
AD Final Rules
Docket Number:
89-NM-111-AD
Subject Heading:
Airworthiness Directives; CASA Model C-212 Series Airplanes
Subject:
Passenger Door Evacuation
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/20/1989
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: 89-22-09
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-111-AD

AMENDMENT:   39-6363

AD NUMBER:   89-22-09

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

ACTION:  

SUMMARY:  

DATES:   Effective November 20, 1989.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   89-22-09 CASA: Amendment 39-6363. Docket No. 89-NM-111-AD. Applicability: Model C-212 series airplanes equipped with a passenger entry step installed under Supplemental Type Certificate (STC) SA906GL, certificated in any category.

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

To prevent delay in opening the passenger door in the event of an emergency evacuation, accomplish the following:

A. Remove the step, handrails, door latch modifications, and associated hardware installed in accordance with Fischer Brothers Aviation, Inc., Installation Instructions for FBD-206, Revision F, dated June 5, 1985.

B. Restore the door handle to the original CASA configuration.

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, Chicago Aircraft Certification Office, ACE-115C, FAA, Central 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, Chicago Aircraft Certification Office, ACE-115C.

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.

The applicable service information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Chicago Aircraft Certification Office, 2300 East Devon Avenue, Des Plaines, Illinois.

This amendment (39-6363, AD 89-22-09) becomes effective November 20, 1989.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_89-22-09.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
89-22-09
Document Type:
AD Final Rules
Docket Number:
89-NM-111-AD
Subject Heading:
Airworthiness Directives; CASA Model C-212 Series Airplanes
Subject:
Passenger Door Evacuation
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/20/1989
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: 89-22-09
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   89-NM-111-AD

AMENDMENT:   39-6363

AD NUMBER:   89-22-09

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

ACTION:  

SUMMARY:  

DATES:   Effective November 20, 1989.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   89-22-09 CASA: Amendment 39-6363. Docket No. 89-NM-111-AD. Applicability: Model C-212 series airplanes equipped with a passenger entry step installed under Supplemental Type Certificate (STC) SA906GL, certificated in any category.

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

To prevent delay in opening the passenger door in the event of an emergency evacuation, accomplish the following:

A. Remove the step, handrails, door latch modifications, and associated hardware installed in accordance with Fischer Brothers Aviation, Inc., Installation Instructions for FBD-206, Revision F, dated June 5, 1985.

B. Restore the door handle to the original CASA configuration.

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, Chicago Aircraft Certification Office, ACE-115C, FAA, Central 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, Chicago Aircraft Certification Office, ACE-115C.

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.

The applicable service information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 17900 Pacific Highway South, Seattle, Washington, or the Chicago Aircraft Certification Office, 2300 East Devon Avenue, Des Plaines, Illinois.

This amendment (39-6363, AD 89-22-09) becomes effective November 20, 1989.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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