AD 84-02-03
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | EADS CASA | C-212-CB | Airworthiness Directives; CASA Models C-212CB and Model C- 212CC Airplanes |
| aircraft | EADS CASA | C-212-CC | Airworthiness Directives; CASA Models C-212CB and Model C- 212CC Airplanes |
Unsafe Condition
The potential for passenger injury during egress from the forward door and inability to open the aft left door during an emergency evacuation exists due to inadequate door locking mechanisms and cabin interior configuration.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the forward exit doors to automatically lock full open per CASA SB 212-52-13; install an outward opening rear passenger door or rearrange cabin interior per specified service bulletins; install an individual switch door warning light system per CASA SB 212-52-14 R2. Alternate compliance may be approved.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 600 hours time in service or 4 months after the effective date (February 27, 1984), whichever comes first, except for part B which must be done no later than March 31, 1984.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
CASA Models C-212CB and C-212CC airplanes certificated in all categories.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Exit Doors Modification
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_84-02-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-02-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CASA Models C-212CB and Model C- 212CC Airplanes Subject: Exit Doors Modification Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/27/1984 Make: EADS CASA Model: C-212-CB | C-212-CC Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 84-02-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4797 AD NUMBER: 84-02-03 SUBJECT HEADING: Airworthiness Directives; CASA Models C-212CB and Model C- 212CC Airplanes ACTION: SUMMARY: DATES: Effective February 27, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-02-03 CASA: Amendment 39-4797. Applies to all Model C-212CB and Model C- 212CC airplanes certificated in all categories. Compliance required as indicated. A. To reduce the potential for passenger injury during egress from the forward door, within 600 hours time in service or 4 months after the effective date of this AD, whichever comes first, unless already accomplished, modify the forward exit door on the CB model and doors on the CC model to automatically lock full open in accordance with CASA Service Bulletin 212-52-13 dated September 17, 1982. B. To prevent inability to open the aft left door during an emergency for evacuation, accomplish one of the following no later than March 31, 1984: (1) Install an outward opening rear passenger door in accordance with CASA Service Bulletin 212-53-29 dated July 14, 1983; or (2) Rearrange the cabin interior in accordance with CASA Service Bulletin 212-25-30 dated September 14, 1982, and Aircraft Furnishings International Limited Service Bulletin 25-89 dated September 1982. C. To preclude improper passenger door locking, within the next 600 hours time in service or four months, whichever occurs first, after the effective date of this AD, install an individual switch door warning light system for cockpit warning of an unlocked passenger door in accordance with CASA Service Bulletin 212-52-14 R2 dated February 14, 1983. D. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. E. 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 inspections and/or modifications required by this AD. This amendment becomes effective February 27, 1984. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_84-02-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-02-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; CASA Models C-212CB and Model C- 212CC Airplanes Subject: Exit Doors Modification Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 02/27/1984 Make: EADS CASA Model: C-212-CB | C-212-CC 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: 84-02-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4797 AD NUMBER: 84-02-03 SUBJECT HEADING: Airworthiness Directives; CASA Models C-212CB and Model C- 212CC Airplanes ACTION: SUMMARY: DATES: Effective February 27, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-02-03 CASA: Amendment 39-4797. Applies to all Model C-212CB and Model C- 212CC airplanes certificated in all categories. Compliance required as indicated. A. To reduce the potential for passenger injury during egress from the forward door, within 600 hours time in service or 4 months after the effective date of this AD, whichever comes first, unless already accomplished, modify the forward exit door on the CB model and doors on the CC model to automatically lock full open in accordance with CASA Service Bulletin 212-52-13 dated September 17, 1982. B. To prevent inability to open the aft left door during an emergency for evacuation, accomplish one of the following no later than March 31, 1984: (1) Install an outward opening rear passenger door in accordance with CASA Service Bulletin 212-53-29 dated July 14, 1983; or (2) Rearrange the cabin interior in accordance with CASA Service Bulletin 212-25-30 dated September 14, 1982, and Aircraft Furnishings International Limited Service Bulletin 25-89 dated September 1982. C. To preclude improper passenger door locking, within the next 600 hours time in service or four months, whichever occurs first, after the effective date of this AD, install an individual switch door warning light system for cockpit warning of an unlocked passenger door in accordance with CASA Service Bulletin 212-52-14 R2 dated February 14, 1983. D. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. E. 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 inspections and/or modifications required by this AD. This amendment becomes effective February 27, 1984. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.