AD 88-10-06
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Lockheed Martin Corporation | 382 | LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA Model 382 Series Airplanes |
| aircraft | Lockheed Martin Corporation | 382B | LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA Model 382 Series Airplanes |
| aircraft | Lockheed Martin Corporation | 382E | LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA Model 382 Series Airplanes |
| aircraft | Lockheed Martin Corporation | 382F | LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA Model 382 Series Airplanes |
| aircraft | Lockheed Martin Corporation | 382G | LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA Model 382 Series Airplanes |
Unsafe Condition
Severe damage to the outer wing lower surface panels due to non-conforming repairs on the interior of the outer wing lower surface panel risers between outer wing stations 0.0 and 360.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 50 hours time-in-service after the effective date, inspect per Lockheed Service Bulletin A382-57-69 to check for riser repairs. If repairs exist but do not conform to SB 382-57-70, inspect further per SP-209 of SMP515A and repair cracks if found. Non-conforming repairs must be modified per SB 382-57-70 or reinspected every 450 flight hours until modified.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the next 50 hours time-in-service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Lockheed Aeronautical Systems Company-Georgia Model 382 series airplanes, serial numbers 3946 through 4541 (excluding those with outer wings equivalent to serial 4542 or later)
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Wing Panel Risers
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_88-10-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 88-10-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA Model 382 Series Airplanes Subject: Wing Panel Risers Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/25/1988 Make: Lockheed Martin Corporation Model: 382 | 382B | 382E | 382F | 382G 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: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 88-10-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5914 AD NUMBER: 88-10-06 SUBJECT HEADING: LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA Model 382 Series Airplanes ACTION: SUMMARY: DATES: Effective May 25, 1988. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 88-10-06 LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA: Amendment 39-5914. Applies to Model 382 series airplanes; Serial Numbers 3946 through 4541, except those airplanes having outer wings installed of a configuration equivalent to Serial Number 4542 or subsequent; certificated in any category. Compliance required as indicated, unless previously accomplished. To prevent severe damage to the outer wing lower surface panels, accomplish the following: A. Within the next 50 hours time-in-service after the effective date of this AD, perform an inspection in accordance with Lockheed Service Bulletin A382-57-69, dated November 30, 1987, to determine the existence of repairs on the interior of the outer wing lower surface panel risers between outer wing stations 0.0 and 360. B. If no outer wing lower surface panel riser repair exists, the airplane may be returned to normal service. C. If any outer wing lower surface panel riser repair exists that does not conform to Lockheed Service Bulletin 382-57-70, dated January 28, 1988, prior to further flight, perform inspections in accordance with Lockheed Service Bulletin A382-57-69, dated November 30, 1987, and Work Card SP-209 of SMP515A, Lockheed Hercules Airfreighter Inspection Procedures. 1. If crack(s) are found, prior to further flight, repair in accordance with an FAA-approved method. 2. If no cracks are found, accomplish either of the following: a. Prior to further flight, install repair modification in accordance with Lockheed Service Bulletin 382-57-70, dated January 28, 1988; or b. Reinspect repairs in accordance with Work Card SP-209 of SMP515A, Lockheed Hercules Airfreighter Inspection Procedures, at intervals not to exceed 450 flight hours, until the repair modification is installed, in accordance with Lockheed Service Bulletin 382-57-70. E. 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. F. 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, Aircraft Certification Office, FAA, Central Region. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who may add any comments and then send it to the Atlanta Aircraft Certification Office. All persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to Lockheed Aeronautical Systems Company-Georgia, Attn: Commercial and Customer Support, Department 72-05, Zone 80, 86 South Cobb Drive, Marietta, Georgia 30063. This information may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at FAA, Central Region, Atlanta Aircraft Certification Office, 1669 Phoenix Parkway, Suite 210, Atlanta, Georgia. This amendment becomes effective May 25, 1988. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_88-10-06.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 88-10-06 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA Model 382 Series Airplanes Subject: Wing Panel Risers Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/25/1988 Make: Lockheed Martin Corporation Model: 382 | 382B | 382E | 382F | 382G 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: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 88-10-06 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5914 AD NUMBER: 88-10-06 SUBJECT HEADING: LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA Model 382 Series Airplanes ACTION: SUMMARY: DATES: Effective May 25, 1988. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 88-10-06 LOCKHEED AERONAUTICAL SYSTEMS COMPANY-GEORGIA: Amendment 39-5914. Applies to Model 382 series airplanes; Serial Numbers 3946 through 4541, except those airplanes having outer wings installed of a configuration equivalent to Serial Number 4542 or subsequent; certificated in any category. Compliance required as indicated, unless previously accomplished. To prevent severe damage to the outer wing lower surface panels, accomplish the following: A. Within the next 50 hours time-in-service after the effective date of this AD, perform an inspection in accordance with Lockheed Service Bulletin A382-57-69, dated November 30, 1987, to determine the existence of repairs on the interior of the outer wing lower surface panel risers between outer wing stations 0.0 and 360. B. If no outer wing lower surface panel riser repair exists, the airplane may be returned to normal service. C. If any outer wing lower surface panel riser repair exists that does not conform to Lockheed Service Bulletin 382-57-70, dated January 28, 1988, prior to further flight, perform inspections in accordance with Lockheed Service Bulletin A382-57-69, dated November 30, 1987, and Work Card SP-209 of SMP515A, Lockheed Hercules Airfreighter Inspection Procedures. 1. If crack(s) are found, prior to further flight, repair in accordance with an FAA-approved method. 2. If no cracks are found, accomplish either of the following: a. Prior to further flight, install repair modification in accordance with Lockheed Service Bulletin 382-57-70, dated January 28, 1988; or b. Reinspect repairs in accordance with Work Card SP-209 of SMP515A, Lockheed Hercules Airfreighter Inspection Procedures, at intervals not to exceed 450 flight hours, until the repair modification is installed, in accordance with Lockheed Service Bulletin 382-57-70. E. 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. F. 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, Aircraft Certification Office, FAA, Central Region. NOTE: The request should be forwarded through an FAA Principal Maintenance Inspector (PMI), who may add any comments and then send it to the Atlanta Aircraft Certification Office. All persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to Lockheed Aeronautical Systems Company-Georgia, Attn: Commercial and Customer Support, Department 72-05, Zone 80, 86 South Cobb Drive, Marietta, Georgia 30063. This information may be examined at FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at FAA, Central Region, Atlanta Aircraft Certification Office, 1669 Phoenix Parkway, Suite 210, Atlanta, Georgia. This amendment becomes effective May 25, 1988. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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