AD 89-20-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Embraer S.A. | EMB-110P1 | Airworthiness Directives; Empresa Model EMB-110P1 and EMB-110P2 Series Airplanes |
| aircraft | Embraer S.A. | EMB-110P2 | Airworthiness Directives; Empresa Model EMB-110P1 and EMB-110P2 Series Airplanes |
Unsafe Condition
The right forward emergency exit could open during flight, which could damage the propeller.
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Required Actions
Revise the Pilot's Operating Handbook and CTA Approved Airplane Flight Manual within 15 days after the effective date to add checks for proper installation of the safety restraining cable and visually insure locking pins are engaged. Additionally, modify the right forward emergency exit per EMBRAER Service Bulletin 110-52-030 within 5 calendar months for specified serial numbers.
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Compliance Time
Within the next 15 days after the effective date of this AD, and within the next 5 calendar months after the effective date for specified serial numbers.
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Affected Aircraft
Embraer S.A. Model EMB-110P1 and EMB-110P2 (all serial numbers) airplanes.
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Federal Register Abstract
AFM Change - Emergency Exit
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_89-20-11.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-20-11 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Empresa Model EMB-110P1 and EMB-110P2 Series Airplanes Subject: AFM Change - Emergency Exit Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/24/1989 Make: Embraer S.A. Model: EMB-110P1 | EMB-110P2 Product Type: Aircraft Product Subtype: Small/Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 89-20-11 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6325 AD NUMBER: 89-20-11 SUBJECT HEADING: Airworthiness Directives; Empresa Model EMB-110P1 and EMB-110P2 Series Airplanes ACTION: SUMMARY: DATES: Effective October 24, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-20-11 EMPRESA BRASILEIRA DE AERONAUTICA S.A. (EMBRAER): Amendment 39-6325. Applicability: Models EMB-110P1 and EMB-110P2 (all serial numbers (S/N)) airplanes, certificated in any category. Compliance: Required as indicated in the body of the AD, unless already accomplished. To prevent the right forward emergency exit from opening during flight which could damage the propeller, accomplish the following: (a) Within the next 15 days after the effective date of this AD, revise the Pilot's Operating Handbook and CTA Approved Airplane Flight Manual, EMBRAER Publication No. TP-110P1/176, Section 4, Pre-Flight Check, by making a pen and ink change to add the following check on the following airplanes: (1) On Model EMB-110 airplanes, S/N 110146, 110153, 110156, 110157, 110161, 110165, 110184, 110186, 110189, 110190, 110192 thru 110283, 110285 thru 110346: "Check for proper installation of the safety restraining cable on the right forward emergency exit." (2) On all Model EMB-110 airplanes except S/N 110146, 110153, 110156, 110157, 110161, 110165, 110184, 110186, 110189, 110190, 110192 thru 110283, 110285 thru 110346: "Check for proper installation of the safety restraining cable on the right forward emergency exit." and, "Visually insure that the locking pins are properly engaged on the right forward emergency exit." (b) Within the next 5 calendar months after the effective date of this AD for Model EMB-110 airplanes, S/N 110146, 110153, 110156, 110157, 110161, 110165, 110184, 110186, 110189, 110190, 110192 thru 110283, 110285 thru 110346: (1) modify the right forward emergency exit in accordance with EMBRAER Service Bulletin 110-52-030, dated November 30, 1981, and (2) revise the Pilot's Operating Handbook and CTA Approved Airplane Flight Manual, EMBRAER Publication No. TP-110P1/176, Section 4, Pre-Flight Check, by making a pen and ink change which follows the previous pen and ink change specified in paragraph (a)(1) above, to add the following check: "Visually insure that the locking pins are properly engaged on the right forward emergency exit." (c) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished. (d) An alternate method of compliance or adjustment of the initial compliance times, which provides an equivalent level of safety, may be approved by the Manager, Atlanta Aircraft Certification Office, 1669 Phoenix Parkway, Suite 210C, Atlanta, Georgia 30349. NOTE: The request should be forwarded through an FAA Maintenance Inspector, who may add comments and then send it to the Manager, Atlanta Aircraft Certification Office, at the above address. All persons affected by this directive may obtain copies of the document referred to herein upon request to Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343-CEP, 12.225 Sao Jose dos Campos, Sao Paulo, Brazil; or may examine this document at the FAA, Office of the Assistant Chief Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106. This amendment (39-6325, AD 89-20-11) becomes effective on October 24, 1989. FOOTER:
Document Text
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AD Final Rules - DRS_89-20-11.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 89-20-11 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Empresa Model EMB-110P1 and EMB-110P2 Series Airplanes Subject: AFM Change - Emergency Exit Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/24/1989 Make: Embraer S.A. Model: EMB-110P1 | EMB-110P2 Product Type: Aircraft Product Subtype: Small/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: 89-20-11 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6325 AD NUMBER: 89-20-11 SUBJECT HEADING: Airworthiness Directives; Empresa Model EMB-110P1 and EMB-110P2 Series Airplanes ACTION: SUMMARY: DATES: Effective October 24, 1989. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 89-20-11 EMPRESA BRASILEIRA DE AERONAUTICA S.A. (EMBRAER): Amendment 39-6325. Applicability: Models EMB-110P1 and EMB-110P2 (all serial numbers (S/N)) airplanes, certificated in any category. Compliance: Required as indicated in the body of the AD, unless already accomplished. To prevent the right forward emergency exit from opening during flight which could damage the propeller, accomplish the following: (a) Within the next 15 days after the effective date of this AD, revise the Pilot's Operating Handbook and CTA Approved Airplane Flight Manual, EMBRAER Publication No. TP-110P1/176, Section 4, Pre-Flight Check, by making a pen and ink change to add the following check on the following airplanes: (1) On Model EMB-110 airplanes, S/N 110146, 110153, 110156, 110157, 110161, 110165, 110184, 110186, 110189, 110190, 110192 thru 110283, 110285 thru 110346: "Check for proper installation of the safety restraining cable on the right forward emergency exit." (2) On all Model EMB-110 airplanes except S/N 110146, 110153, 110156, 110157, 110161, 110165, 110184, 110186, 110189, 110190, 110192 thru 110283, 110285 thru 110346: "Check for proper installation of the safety restraining cable on the right forward emergency exit." and, "Visually insure that the locking pins are properly engaged on the right forward emergency exit." (b) Within the next 5 calendar months after the effective date of this AD for Model EMB-110 airplanes, S/N 110146, 110153, 110156, 110157, 110161, 110165, 110184, 110186, 110189, 110190, 110192 thru 110283, 110285 thru 110346: (1) modify the right forward emergency exit in accordance with EMBRAER Service Bulletin 110-52-030, dated November 30, 1981, and (2) revise the Pilot's Operating Handbook and CTA Approved Airplane Flight Manual, EMBRAER Publication No. TP-110P1/176, Section 4, Pre-Flight Check, by making a pen and ink change which follows the previous pen and ink change specified in paragraph (a)(1) above, to add the following check: "Visually insure that the locking pins are properly engaged on the right forward emergency exit." (c) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished. (d) An alternate method of compliance or adjustment of the initial compliance times, which provides an equivalent level of safety, may be approved by the Manager, Atlanta Aircraft Certification Office, 1669 Phoenix Parkway, Suite 210C, Atlanta, Georgia 30349. NOTE: The request should be forwarded through an FAA Maintenance Inspector, who may add comments and then send it to the Manager, Atlanta Aircraft Certification Office, at the above address. All persons affected by this directive may obtain copies of the document referred to herein upon request to Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343-CEP, 12.225 Sao Jose dos Campos, Sao Paulo, Brazil; or may examine this document at the FAA, Office of the Assistant Chief Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106. This amendment (39-6325, AD 89-20-11) becomes effective on October 24, 1989. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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