AD 81-19-06
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dassault Aviation | Falcon 10 | AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Series Airplanes |
Unsafe Condition
Loosening of seat belt screws, jamming of movement locking spigots, rupture of movement actuator coupling endfitting, and rupture of backrest housings in pilot and co-pilot seats.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify pilot and co-pilot seat belt attachments per Service Bulletin F10 0085 Rev 1 for serial numbers 1-20, 22-31, 33-38, 41,42. Modify seat fore/aft movement locking control per Service Bulletins F10 0143 Rev 1 and 376/F10/BS02 Rev 1 for serial numbers 1-49, 51-90, 92,94-97,99,100,102,104. Improve greasing of actuator endfitting per Service Bulletins F10 0148 Rev 2 and 376/F10/BS03 Rev 1 based on seat part numbers and serial ranges. Modify seat backrest housings per Service Bulletins F10 0193 Rev 1 and 376-0017 Rev 2 for serial numbers 1-102,104-123,125-128,133.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 300 hours time in service after 10/14/1981 (for parts a and b) and within the next 600 hours time in service after 10/14/1981 or before 1600 hours time in service, whichever occurs later (for parts c and d).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Dassault Aviation Falcon 10 series airplanes with serial numbers 1 through 128 and 133, with specific serial ranges for each modification as listed in the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Seat Belt Attachments
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_81-19-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 81-19-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Series Airplanes Subject: Seat Belt Attachments Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/14/1981 Make: Dassault Aviation Model: Falcon 10 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 81-19-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4218 AD NUMBER: 81-19-06 SUBJECT HEADING: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Series Airplanes ACTION: SUMMARY: DATES: Effective October 14, 1981. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 81-19-06 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-4218. Applies to Model Falcon 10 series airplanes, certificated in all categories. Compliance is required as indicated, unless already accomplished. To prevent loosening of seat belt screws, jamming of movement locking spigots, rupture of movement actuator coupling endfitting, and rupture of backrest housings in pilot and co-pilot seats, accomplish the following: (a) Within the next 300 hours time in service after the effective date of this AD, on Falcon 10 airplanes serial numbers 1 through 20, 22 through 31, 33 through 38, 41 and 42, modify the pilot and co-pilot seat belt attachments in accordance with paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Avions Marcel Dassault - Breguet Aviation Service Bulletin No. F10 0085, Revision 1, dated November 30, 1979, or an FAA-approved equivalent. (b) Within the next 300 hours time in service after the effective date of this AD, on Falcon 10 airplanes serial numbers 1 through 49, 51 through 90, 92, 94 through 97, 99, 100, 102 and 104, modify the pilot and co-pilot seat fore and aft movement locking control in accordance with paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Avions Marcel Dassault - Breguet Aviation Service Bulletin No. F10 0143, Revision 1, dated November 30, 1979, and SICMA AERO-SEAT Service Bulletin No. 376/F10/BS02, Revision 1, dated November 30, 1979, or an FAA-approved equivalent. (c) Within the next 600 hours time in service after the effective date of this AD, or before the accumulation of 1600 hours time in service, whichever occurs later, modify and improve greasing of the actuator endfitting on the following pilot and co-pilot seats in accordance with the instructions in paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Avions Marcel Dassault - Breguet Aviation Service Bulletin No. F10 0148, Revision 2, dated February 1, 1980, and SICMA AERO-SEAT Service Bulletin No. 376/F10/BS03, Revision 1, dated November 30, 1979, or an FAA-approved equivalent: Part No. Seat Serial Numbers Pilot Seat 376-2R1 1 through 52 376-211 53 through 117 376-22 118 through 123 Co-Pilot Seat 376-3R1 1 through 52 376-311 53 through 83 and 85 through 117 376-32 118 through 122 (d) Within the next 600 hours time in service after the effective date of this AD or before the accumulation of 1600 hours time in service, whichever occurs later, on Falcon 10 airplanes serial numbers 1 through 102, 104 through 123, 125 through 128, and 133, modify the pilot and co-pilot seat backrest housings in accordance with the instructions in paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Avions Marcel Dassault - Breguet Aviation Service Bulletin No. F10 0193, Revision 1, dated November 30, 1979, and SICMA AERO-SEAT Service Bulletin No. 376-0017, Revision 2, dated November 30, 1979, or an FAA-approved equivalent. (e) If an equivalent means of compliance is used in complying with this AD, that equivalent means must be approved by the Chief, Aircraft Certification Staff, AEU-100, FAA, Europe, Africa, and Middle East Office, c/o American Embassy, Brussels, Belgium. The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Falcon Jet Corporation, 90 Moonachie Avenue, Moonachie, New Jersey 07074. These documents may be examined at FAA Headquarters, Room 916, 800 Independence Avenue, SW., Washington DC 20591. This amendment becomes effective October 14, 1981. FOOTER:
Document Text
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AD Final Rules - DRS_81-19-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 81-19-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Series Airplanes Subject: Seat Belt Attachments Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/14/1981 Make: Dassault Aviation Model: Falcon 10 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: 81-19-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4218 AD NUMBER: 81-19-06 SUBJECT HEADING: AVIONS MARCEL DASSAULT - BREGUET AVIATION Model Falcon 10 Series Airplanes ACTION: SUMMARY: DATES: Effective October 14, 1981. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 81-19-06 AVIONS MARCEL DASSAULT - BREGUET AVIATION: Amendment 39-4218. Applies to Model Falcon 10 series airplanes, certificated in all categories. Compliance is required as indicated, unless already accomplished. To prevent loosening of seat belt screws, jamming of movement locking spigots, rupture of movement actuator coupling endfitting, and rupture of backrest housings in pilot and co-pilot seats, accomplish the following: (a) Within the next 300 hours time in service after the effective date of this AD, on Falcon 10 airplanes serial numbers 1 through 20, 22 through 31, 33 through 38, 41 and 42, modify the pilot and co-pilot seat belt attachments in accordance with paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Avions Marcel Dassault - Breguet Aviation Service Bulletin No. F10 0085, Revision 1, dated November 30, 1979, or an FAA-approved equivalent. (b) Within the next 300 hours time in service after the effective date of this AD, on Falcon 10 airplanes serial numbers 1 through 49, 51 through 90, 92, 94 through 97, 99, 100, 102 and 104, modify the pilot and co-pilot seat fore and aft movement locking control in accordance with paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Avions Marcel Dassault - Breguet Aviation Service Bulletin No. F10 0143, Revision 1, dated November 30, 1979, and SICMA AERO-SEAT Service Bulletin No. 376/F10/BS02, Revision 1, dated November 30, 1979, or an FAA-approved equivalent. (c) Within the next 600 hours time in service after the effective date of this AD, or before the accumulation of 1600 hours time in service, whichever occurs later, modify and improve greasing of the actuator endfitting on the following pilot and co-pilot seats in accordance with the instructions in paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Avions Marcel Dassault - Breguet Aviation Service Bulletin No. F10 0148, Revision 2, dated February 1, 1980, and SICMA AERO-SEAT Service Bulletin No. 376/F10/BS03, Revision 1, dated November 30, 1979, or an FAA-approved equivalent: Part No. Seat Serial Numbers Pilot Seat 376-2R1 1 through 52 376-211 53 through 117 376-22 118 through 123 Co-Pilot Seat 376-3R1 1 through 52 376-311 53 through 83 and 85 through 117 376-32 118 through 122 (d) Within the next 600 hours time in service after the effective date of this AD or before the accumulation of 1600 hours time in service, whichever occurs later, on Falcon 10 airplanes serial numbers 1 through 102, 104 through 123, 125 through 128, and 133, modify the pilot and co-pilot seat backrest housings in accordance with the instructions in paragraph 2, "ACCOMPLISHMENT INSTRUCTIONS," of Avions Marcel Dassault - Breguet Aviation Service Bulletin No. F10 0193, Revision 1, dated November 30, 1979, and SICMA AERO-SEAT Service Bulletin No. 376-0017, Revision 2, dated November 30, 1979, or an FAA-approved equivalent. (e) If an equivalent means of compliance is used in complying with this AD, that equivalent means must be approved by the Chief, Aircraft Certification Staff, AEU-100, FAA, Europe, Africa, and Middle East Office, c/o American Embassy, Brussels, Belgium. The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1). All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to Falcon Jet Corporation, 90 Moonachie Avenue, Moonachie, New Jersey 07074. These documents may be examined at FAA Headquarters, Room 916, 800 Independence Avenue, SW., Washington DC 20591. This amendment becomes effective October 14, 1981. FOOTER:
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