AD 74-19-02

EMERGENCY AD emergency

Airworthiness Directives; PATHFINDER CORPORATION: Applies to Pathfinder Corporation Emergency Locator Transmitters

AD Number
74-19-02
Status
emergency
Effective Date
Product Category
appliance
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Pathfinder Corporation Emergency Locator Transmitters Airworthiness Directives; PATHFINDER CORPORATION: Applies to Pathfinder Corporation Emergency Locator Transmitters
appliance Pathfinder Corporation Emergency Locator Transmitters Airworthiness Directives; PATHFINDER CORPORATION: Applies to Pathfinder Corporation Emergency Locator Transmitters

Unsafe Condition

Corrosion may jam the cylindrical G force sensor plunger or cause inadvertent transmission of an emergency signal.

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

Required Actions

Inspect the ELT for corrosion, particularly in the G force sensor plunger area by removing the top dome assembly. Manually check plunger movement and test transmission. Repair or replace units with corrosion, jamming, or improper transmission before next flight, except under ferry flight provisions.

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

Compliance Time

within the next 60 days, and thereafter at each additional 60 days interval

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

Affected Aircraft

Pathfinder Corporation Emergency Locator Transmitters; all models.

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

Federal Register Abstract

Emergency Locator Transmitters

Applicability Source Text

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AD Final Rules - DRS_74-19-02.html
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AD Number:
74-19-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; PATHFINDER CORPORATION: Applies to Pathfinder Corporation Emergency Loca...Show more
Subject:
Emergency Locator Transmitters
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/13/1974
Make:
Pathfinder Corporation
Model:
Emergency Locator Transmitters
Product Type:
Appliance
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 74-19-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1956

AD NUMBER:   74-19-02

SUBJECT HEADING:   Airworthiness Directives; PATHFINDER CORPORATION: Applies to Pathfinder Corporation Emergency Locator Transmitters

ACTION:  

SUMMARY:  

DATES:   Effective September 13, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-19-02 PATHFINDER CORPORATION: Amendment 39-1956. Applies to Pathfinder Corporation Emergency Locator Transmitters; all models. Compliance required within the next 60 days, and thereafter at each additional 60 days interval.

To detect corrosion which may, (1) jam the cylindrical G force sensor plunger, or (2) cause inadvertent transmission of an emergency signal, accomplish the following: Inspect the ELT for evidence of corrosion, particularly in the area of the G force sensor plunger, by removing the top dome assembly, reference Pathfinder Installation and Operation Manual. Determine that the plunger is free to move by manually sliding the plunger along the guide rod so as to actuate the switch, and determine that the ELT transmits properly. ELT test transmissions are authorized in the first five minutes of any hour, or at other times if coordinated with the nearest FAA tower or flight service station, for a total of three audio sweeps, reference Advisory Circular 00-35A or 20-81. If any evidence of corrosion or jamming of the plunger is found, or if the ELT does not transmit properly, repair or replace with a serviceable unit prior to next flight, except that flight may be conducted in accordance with the ferry flight provisions of FAR 91.52(e). Any repaired or replacement unit must comply with the provisions of FAR 91.52 (performance standards of TSO-C91), or be an equivalent unit approved by the Chief, Engineering and Manufacturing Branch, Great Lakes Region.

This amendment becomes effective September 13, 1974.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_74-19-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
74-19-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; PATHFINDER CORPORATION: Applies to Pathfinder Corporation Emergency Loca...Show more
Subject:
Emergency Locator Transmitters
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
09/13/1974
Make:
Pathfinder Corporation
Model:
Emergency Locator Transmitters
Product Type:
Appliance
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 74-19-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1956

AD NUMBER:   74-19-02

SUBJECT HEADING:   Airworthiness Directives; PATHFINDER CORPORATION: Applies to Pathfinder Corporation Emergency Locator Transmitters

ACTION:  

SUMMARY:  

DATES:   Effective September 13, 1974.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
74-19-02 PATHFINDER CORPORATION: Amendment 39-1956. Applies to Pathfinder Corporation Emergency Locator Transmitters; all models. Compliance required within the next 60 days, and thereafter at each additional 60 days interval.

To detect corrosion which may, (1) jam the cylindrical G force sensor plunger, or (2) cause inadvertent transmission of an emergency signal, accomplish the following: Inspect the ELT for evidence of corrosion, particularly in the area of the G force sensor plunger, by removing the top dome assembly, reference Pathfinder Installation and Operation Manual. Determine that the plunger is free to move by manually sliding the plunger along the guide rod so as to actuate the switch, and determine that the ELT transmits properly. ELT test transmissions are authorized in the first five minutes of any hour, or at other times if coordinated with the nearest FAA tower or flight service station, for a total of three audio sweeps, reference Advisory Circular 00-35A or 20-81. If any evidence of corrosion or jamming of the plunger is found, or if the ELT does not transmit properly, repair or replace with a serviceable unit prior to next flight, except that flight may be conducted in accordance with the ferry flight provisions of FAR 91.52(e). Any repaired or replacement unit must comply with the provisions of FAR 91.52 (performance standards of TSO-C91), or be an equivalent unit approved by the Chief, Engineering and Manufacturing Branch, Great Lakes Region.

This amendment becomes effective September 13, 1974.

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.