AD 75-17-04

final rule

LOCKHEED Model 382 Series Airplanes

AD Number
75-17-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Lockheed Martin Corporation 382 LOCKHEED Model 382 Series Airplanes
aircraft Lockheed Martin Corporation 382B LOCKHEED Model 382 Series Airplanes
aircraft Lockheed Martin Corporation 382E LOCKHEED Model 382 Series Airplanes
aircraft Lockheed Martin Corporation 382F LOCKHEED Model 382 Series Airplanes
aircraft Lockheed Martin Corporation 382G LOCKHEED Model 382 Series Airplanes

Unsafe Condition

Cracks in the main frames

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect main frames in accordance with Lockheed Service Bulletin A382-189 or equivalent method. If cracks are found, contact the Chief, Engineering and Manufacturing Branch, FAA, Southern Region before further flight.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Within the next 325 hours' time in service on airplanes which have accumulated 10,000 or more flight hours and thereafter at each 'C' check inspection.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Lockheed Model 382 series airplanes, serial numbers 3946 and 4101 through 4751

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Main Frames

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-17-04.html
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AD Number:
75-17-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED Model 382 Series Airplanes
Subject:
Main Frames
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/21/1978
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Superseded AD: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Superseded By: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: 75-17-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3185

AD NUMBER:   75-17-04

SUBJECT HEADING:   LOCKHEED Model 382 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 21, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-17-04 LOCKHEED: Amendment 39-2300 as amended by Amendment 39-3185. Applies to all Model 382 series airplanes, serial numbers 3946 and 4101 through 4751, certificated in all categories.

Compliance required within the next 325 hours' time in service on airplanes which have accumulated 10,000 or more flight hours and thereafter at each "C" check inspection.

(a) To detect cracks in the main frames, inspect the frames in accordance with Lockheed Service Bulletin A382-189, or later FAA approved revision, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region.

(b) In the event a crack or cracks are found, before further flight, contact the Chief, Engineering and Manufacturing Branch, FAA, Southern Region, P.O. Box 20636, Atlanta, Georgia 30320.

(c) The inspection required by the A.D. may be discontinued on those airplanes which have been repaired in accordance with Lockheed Service Bulletin A382-189, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region.

Amendment 39-2300 became effective August 8, 1975.

This Amendment 39-3185 becomes effective April 21, 1978.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-17-04.html
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Document Versions
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Details
AD Number:
75-17-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED Model 382 Series Airplanes
Subject:
Main Frames
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/21/1978
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: 75-17-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3185

AD NUMBER:   75-17-04

SUBJECT HEADING:   LOCKHEED Model 382 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective April 21, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-17-04 LOCKHEED: Amendment 39-2300 as amended by Amendment 39-3185. Applies to all Model 382 series airplanes, serial numbers 3946 and 4101 through 4751, certificated in all categories.

Compliance required within the next 325 hours' time in service on airplanes which have accumulated 10,000 or more flight hours and thereafter at each "C" check inspection.

(a) To detect cracks in the main frames, inspect the frames in accordance with Lockheed Service Bulletin A382-189, or later FAA approved revision, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region.

(b) In the event a crack or cracks are found, before further flight, contact the Chief, Engineering and Manufacturing Branch, FAA, Southern Region, P.O. Box 20636, Atlanta, Georgia 30320.

(c) The inspection required by the A.D. may be discontinued on those airplanes which have been repaired in accordance with Lockheed Service Bulletin A382-189, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA, Southern Region.

Amendment 39-2300 became effective August 8, 1975.

This Amendment 39-3185 becomes effective April 21, 1978.

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.