AD 75-17-35

final rule

LOCKHEED Model 382 Series Airplanes

AD Number
75-17-35
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft propeller assembly
Problem area Propeller

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

Propeller control may not pass the torque check, leading to potential loss of propeller control.

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

Required Actions

Perform the propeller torque check in accordance with Lockheed Alert Service Bulletin A 382-190. Replace the propeller control if it does not pass the torque check.

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

Compliance Time

before further flight

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

Affected Aircraft

Lockheed Model 382 series airplanes through serial number 4610

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

Federal Register Abstract

Propeller Torque Check

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-17-35.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-17-35
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED Model 382 Series Airplanes
Subject:
Propeller Torque Check
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/13/1975
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Superseded AD: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Superseded By: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: 75-17-35
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2325

AD NUMBER:   75-17-35

SUBJECT HEADING:   LOCKHEED Model 382 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 13, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-17-35 LOCKHEED: Amendment 39-2325. Applies to all Model 382 series airplanes through serial number 4610. Before further flight, unless already accomplished, perform the propeller torque check in accordance with Lockheed Alert Service Bulletin A 382-190. If the propellers do not pass the torque check, replace the propeller control with a control that will pass the above operational check prior to further flight.

This amendment is effective August 13, 1975, and was effective on receipt for all recipients of the telegram dated July 25, 1975 which contained this amendment.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-17-35.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-17-35
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
LOCKHEED Model 382 Series Airplanes
Subject:
Propeller Torque Check
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/13/1975
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: 75-17-35
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2325

AD NUMBER:   75-17-35

SUBJECT HEADING:   LOCKHEED Model 382 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 13, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-17-35 LOCKHEED: Amendment 39-2325. Applies to all Model 382 series airplanes through serial number 4610. Before further flight, unless already accomplished, perform the propeller torque check in accordance with Lockheed Alert Service Bulletin A 382-190. If the propellers do not pass the torque check, replace the propeller control with a control that will pass the above operational check prior to further flight.

This amendment is effective August 13, 1975, and was effective on receipt for all recipients of the telegram dated July 25, 1975 which contained this amendment.

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.