AD 84-03-06
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 747-100 Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747-100B Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747-100B SUD Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747-200B Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747-200C Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747-200F Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747-300 Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747-400 Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747-400D Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747-400F Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747SP Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | 747SR Series | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-10-10 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-10-10F | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-10-15 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-10-30 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-10-40 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-10-40F | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-11 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-12 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-13 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-14 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-15 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-15F | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-21 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-31 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-32 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-32 (VC-9C) | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-32F | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-32F (C-9A) | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-32F (C-9B) | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-33F | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-34 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-34F | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-41 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-51 | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-81 (MD-81) | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-82 (MD-82) | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-83 (MD-83) | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
| aircraft | The Boeing Company | DC-9-87 (MD-87) | Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series |
Unsafe Condition
The installation of certain components listed by serial number in Table I of this AD in the landing gear assembly could result in failure of the fuel tank pump conduits due to inadequate design or manufacturing conformity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 180 days from the effective date, determine if any components listed in Table I are installed. Replace affected components with approved parts before further flight. Prohibit future use of listed components unless manufacturer confirms conformity to type design.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 180 days from the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 747 (747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-SP series) and McDonnell Douglas Model DC-9 and DC-10 series airplanes. Components purchased prior to January 1, 1979, or obtained from Boeing, Douglas, or Cleveland Pneumatics as spares are excluded.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Fuel Tank Pump Conduits
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_84-03-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-03-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series Subject: Fuel Tank Pump Conduits Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/19/1984 Make: The Boeing Company Model: 747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...Show more 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: 84-03-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4805 AD NUMBER: 84-03-06 SUBJECT HEADING: Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series ACTION: SUMMARY: DATES: Effective March 19, 1984 ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-03-06 BOEING AND McDONNELL DOUGLAS: Amendment 39-4805. Applies to Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series airplanes certificated in all categories: A. Within 180 days from the effective date of this AD, unless already accomplished, determine if any components listed by serial number in Table I, below, are installed on or in the landing gear assembly. This determination may be made by review of records or by inspection of parts to determine serial numbers. Components delivered with production airplanes or purchased from Boeing, Douglas, or Cleveland Pneumatics, as spares, are not affected by this AD. Components purchased prior to January 1, 1979, are not affected by this AD. B. If any components listed in Table I are found, replace them with approved parts before further flight. C. Future use of any components listed by serial number in Table I is prohibited, unless it is determined by the manufacturer or demonstrated to the FAA that the component is in conformity to type design. D. Upon request of the operator, an FAA Principal Maintenance Inspector may adjust the compliance times if the request contains substantiating data to justify the change, and subject to prior approval by the Manager, Seattle Aircraft Certification Office, for the Boeing Model 747, or the Manager, Los Angeles Aircraft Certification Office, for the McDonnell Douglas Models DC-9 and DC-10. E. Alternate means of compliance with the AD which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office for the Boeing Model 747, or the Manager, Los Angeles Aircraft Certification Office for the McDonnell Douglas Models DC-9 and DC-10. F. Aircraft may be ferried to a base for maintenance in accordance with Sections 21.197 and 21.199 of the Federal Aviation Regulations. This amendment becomes effective March 19, 1984. AD 84-03-06 TABLE I PART AIRCRAFT SERIAL AIRCRAFT NOMENCLATURE MANUFACTURERS NUMBERS PART NO. Boeing Brace Assembly 65B05280 CPT 1163 PTM 747-100 Side Body CPT 1257 PTM /200 Landing Gear Axle 65B05133 CPT 2474 PTM Wing & Body CPT 2714 PTM Gear CPT 2828 PTM CPT 2836 PTM CPT 2838 PTM CPT 2839 PTM CPT 2886 PTM CPT 2908 PTM CPT 2959 PTM CPT 2981 PTM CPT 2982 PTM CPT 2991 PTM CPT 3048 PTM CPT 3056 PTM CPT 3063 PTM CPT 3090 PTM CPT 3091 PTM CPT 3101 PTM CPT 3149 PTM CPT 3691 PTM CPT 3733 PTM Boeing Axle 65B19917 CPT 3398 PTM 747-SP Wing & Body Gear McDonnell Nose Gear Cylinder 5920602-5 CPT 1134 PTM Douglas or CPT 1160 PTM DC-9 5920602-501 CPT 1201 PTM CPT 1207 PTM CPT 1210 PTM CPT 1129 PTM Nose Gear Piston 5920603-501 CPT 1395 PTM or CPT 1310 PTM 5920603-5 CPT 1308 PTM CPT 1417 PTM CPT 1422 PTM CPT 1440 PTM CPT 1301 PTM CPT 1306 PTM CPT 1160 PTM CPT 1161 PTM CPT 1178 PTM CPT 1208 PTM CPT 1209 PTM CPT 1246 PTM McDonnell Main Gear Link Assy ARG7009-501 Douglas Lower Down Lock or CPT 402 PTM DC-10 ARG7009-7 CPT 421 PT Axle MLG ARG7313-3 or CPT 4361 PTM ARG7313-1 Link ARG7107-5 or ARG7107-1 CPT 0886 PTM Bolt - Torque ARG7323-1 M 495 PTM Link - Upper MLG Arm - Downlock ARG7147-1 CPT 1328 PTM MLG or ARG7147-3 Link Assembly ARG7019-1 CPT 019 PTM Forward Brake or CPT 941 PTM ARG7019-5 Link Assembly ARG7378-1 CPT 672 PTM Forward Brake or CPT 941 PTM MLG ARG7378-3 Bolt - Torque ARG7337-1 CPT 063 PTM Link - Lower CPT 039 PTM MLG CPT 073 PTM CPT 040 PTM CPT 041 PTM FOOTER:
Document Text
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AD Final Rules - DRS_84-03-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 84-03-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series Subject: Fuel Tank Pump Conduits Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/19/1984 Make: The Boeing Company Model: 747-100 Series | 747-100B Series | 747-100B SUD Series | 747-200B Series | 747-200C Series | 747-200...Show more 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: 84-03-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4805 AD NUMBER: 84-03-06 SUBJECT HEADING: Airworthiness Directives; Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series ACTION: SUMMARY: DATES: Effective March 19, 1984 ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 84-03-06 BOEING AND McDONNELL DOUGLAS: Amendment 39-4805. Applies to Boeing Model 747 and McDonnell Douglas Model DC-9 and DC-10 series airplanes certificated in all categories: A. Within 180 days from the effective date of this AD, unless already accomplished, determine if any components listed by serial number in Table I, below, are installed on or in the landing gear assembly. This determination may be made by review of records or by inspection of parts to determine serial numbers. Components delivered with production airplanes or purchased from Boeing, Douglas, or Cleveland Pneumatics, as spares, are not affected by this AD. Components purchased prior to January 1, 1979, are not affected by this AD. B. If any components listed in Table I are found, replace them with approved parts before further flight. C. Future use of any components listed by serial number in Table I is prohibited, unless it is determined by the manufacturer or demonstrated to the FAA that the component is in conformity to type design. D. Upon request of the operator, an FAA Principal Maintenance Inspector may adjust the compliance times if the request contains substantiating data to justify the change, and subject to prior approval by the Manager, Seattle Aircraft Certification Office, for the Boeing Model 747, or the Manager, Los Angeles Aircraft Certification Office, for the McDonnell Douglas Models DC-9 and DC-10. E. Alternate means of compliance with the AD which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office for the Boeing Model 747, or the Manager, Los Angeles Aircraft Certification Office for the McDonnell Douglas Models DC-9 and DC-10. F. Aircraft may be ferried to a base for maintenance in accordance with Sections 21.197 and 21.199 of the Federal Aviation Regulations. This amendment becomes effective March 19, 1984. AD 84-03-06 TABLE I PART AIRCRAFT SERIAL AIRCRAFT NOMENCLATURE MANUFACTURERS NUMBERS PART NO. Boeing Brace Assembly 65B05280 CPT 1163 PTM 747-100 Side Body CPT 1257 PTM /200 Landing Gear Axle 65B05133 CPT 2474 PTM Wing & Body CPT 2714 PTM Gear CPT 2828 PTM CPT 2836 PTM CPT 2838 PTM CPT 2839 PTM CPT 2886 PTM CPT 2908 PTM CPT 2959 PTM CPT 2981 PTM CPT 2982 PTM CPT 2991 PTM CPT 3048 PTM CPT 3056 PTM CPT 3063 PTM CPT 3090 PTM CPT 3091 PTM CPT 3101 PTM CPT 3149 PTM CPT 3691 PTM CPT 3733 PTM Boeing Axle 65B19917 CPT 3398 PTM 747-SP Wing & Body Gear McDonnell Nose Gear Cylinder 5920602-5 CPT 1134 PTM Douglas or CPT 1160 PTM DC-9 5920602-501 CPT 1201 PTM CPT 1207 PTM CPT 1210 PTM CPT 1129 PTM Nose Gear Piston 5920603-501 CPT 1395 PTM or CPT 1310 PTM 5920603-5 CPT 1308 PTM CPT 1417 PTM CPT 1422 PTM CPT 1440 PTM CPT 1301 PTM CPT 1306 PTM CPT 1160 PTM CPT 1161 PTM CPT 1178 PTM CPT 1208 PTM CPT 1209 PTM CPT 1246 PTM McDonnell Main Gear Link Assy ARG7009-501 Douglas Lower Down Lock or CPT 402 PTM DC-10 ARG7009-7 CPT 421 PT Axle MLG ARG7313-3 or CPT 4361 PTM ARG7313-1 Link ARG7107-5 or ARG7107-1 CPT 0886 PTM Bolt - Torque ARG7323-1 M 495 PTM Link - Upper MLG Arm - Downlock ARG7147-1 CPT 1328 PTM MLG or ARG7147-3 Link Assembly ARG7019-1 CPT 019 PTM Forward Brake or CPT 941 PTM ARG7019-5 Link Assembly ARG7378-1 CPT 672 PTM Forward Brake or CPT 941 PTM MLG ARG7378-3 Bolt - Torque ARG7337-1 CPT 063 PTM Link - Lower CPT 039 PTM MLG CPT 073 PTM CPT 040 PTM CPT 041 PTM FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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