AD 78-08-10

final rule

Airworthiness Directives; Piper Models PA-31 and PA-31-325 Aircraft

AD Number
78-08-10
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Inc. PA-31 Airworthiness Directives; Piper Models PA-31 and PA-31-325 Aircraft
aircraft Piper Aircraft Inc. PA-31-325 Airworthiness Directives; Piper Models PA-31 and PA-31-325 Aircraft

Unsafe Condition

The fuel selector lever may become disconnected due to missing parts, including MS24694-S63 screw, MS20365-1032C nut, AN960-10 washer, and ESNA Part Number 59-022-094-0625 roll pin.

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

Required Actions

Inspect each fuel selector lever for missing hardware (screw, nut, washer, roll pins), install any missing parts, and inspect lever operation before reinstalling components.

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

Compliance Time

within the next 10 hours in service

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

Affected Aircraft

Piper Models PA-31 and PA-31-325 NAVAJO, serial numbers 31-7612040 thru 31-7812023, 31-7812025 thru 31-7812035, 31-7812038 thru 31-7812041, and 31-7812043 thru 31-7812047

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

Federal Register Abstract

Fuel Selector Lever

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_78-08-10.html
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AD Number:
78-08-10
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-31 and PA-31-325 Aircraft
Subject:
Fuel Selector Lever
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
04/20/1978
Effective Date:
04/25/1978
Make:
Piper Aircraft Inc.
Model:
PA-31 | PA-31-325
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 78-08-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3192

AD NUMBER:   78-08-10

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-31 and PA-31-325 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective April 25, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
78-08-10 PIPER: Amendment 39-3192. Applies to Piper Aircraft Models PA-31 and PA-31-325 NAVAJO, Serial Numbers:


31-7612040 thru 31-7812023


31-7812025 thru 31-7812035


31-7812038 thru 31-7812041 and


31-7812043 thru 31-7812047

To prevent hazards associated with the fuel selector lever becoming disconnected due to missing parts, accomplish the following within the next 10 hours in service:

1. Remove fuel control panel royalite cover and two belly access plates immediately forward of the main spar, exposing the left and right selector lever pivot attachment points.

2. Inspect each lever for the following attachment hardware (per lever):

a) One (1) MS24694-S63 screw (Piper Part Number 410 050);

b) One (1) MS20365-1032C nut (Piper Part Number 407 807);

c) One (1) AN960-10 washer (Piper Part Number 407 564);

d) Two (2) ESNA Part Number 59-022-094-0625 roll pin (Piper Part Number 480 696).

NOTE: The nut, washer, and roll pins are on the aft side of the fuel control panel and are more easily viewed from the belly access holes.

3. Install any missing hardware.

4. Inspect lever operation and reinstall panel cover and access plates.

5. The aircraft may be flown in accordance with FAR 21.197 to a location where the AD can be accomplished. (Piper Service Bulletin No. 592, February 16, 1978, pertains to this subject.)

This amendment is effective April 25, 1978.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_78-08-10.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
78-08-10
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Piper Models PA-31 and PA-31-325 Aircraft
Subject:
Fuel Selector Lever
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
04/20/1978
Effective Date:
04/25/1978
Make:
Piper Aircraft Inc.
Model:
PA-31 | PA-31-325
Product Type:
Aircraft
Product Subtype:
Small Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
AIR-700: Compliance & Airworthiness Division
Office of Primary Responsibility:
AIR-720: Operational Safety Branch
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 78-08-10
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3192

AD NUMBER:   78-08-10

SUBJECT HEADING:   Airworthiness Directives; Piper Models PA-31 and PA-31-325 Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective April 25, 1978.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
78-08-10 PIPER: Amendment 39-3192. Applies to Piper Aircraft Models PA-31 and PA-31-325 NAVAJO, Serial Numbers:


31-7612040 thru 31-7812023


31-7812025 thru 31-7812035


31-7812038 thru 31-7812041 and


31-7812043 thru 31-7812047

To prevent hazards associated with the fuel selector lever becoming disconnected due to missing parts, accomplish the following within the next 10 hours in service:

1. Remove fuel control panel royalite cover and two belly access plates immediately forward of the main spar, exposing the left and right selector lever pivot attachment points.

2. Inspect each lever for the following attachment hardware (per lever):

a) One (1) MS24694-S63 screw (Piper Part Number 410 050);

b) One (1) MS20365-1032C nut (Piper Part Number 407 807);

c) One (1) AN960-10 washer (Piper Part Number 407 564);

d) Two (2) ESNA Part Number 59-022-094-0625 roll pin (Piper Part Number 480 696).

NOTE: The nut, washer, and roll pins are on the aft side of the fuel control panel and are more easily viewed from the belly access holes.

3. Install any missing hardware.

4. Inspect lever operation and reinstall panel cover and access plates.

5. The aircraft may be flown in accordance with FAR 21.197 to a location where the AD can be accomplished. (Piper Service Bulletin No. 592, February 16, 1978, pertains to this subject.)

This amendment is effective April 25, 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.