AD 50-25-01

final rule

Airworthiness Directives; STINSON Model All Model 108 Series Aircraft

AD Number
50-25-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Univair Aircraft Corporation 108 Airworthiness Directives; STINSON Model All Model 108 Series Aircraft
aircraft Univair Aircraft Corporation 108-1 Airworthiness Directives; STINSON Model All Model 108 Series Aircraft
aircraft Univair Aircraft Corporation 108-2 Airworthiness Directives; STINSON Model All Model 108 Series Aircraft
aircraft Univair Aircraft Corporation 108-3 Airworthiness Directives; STINSON Model All Model 108 Series Aircraft

Unsafe Condition

Fuel seepage into the space between the inner cabin trim and the outer fabric covering of the fuselage, resulting in soaking of insulating material in the cabin wall due to fuel spillage during filling, thermal expansion in full tanks, or tank leakage.

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

Required Actions

Install a drip strip similar to that shown in Figure 1 on the underside of each wing to prevent fuel from flowing from the wing to the fuselage.

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

Compliance Time

not later than September 1, 1950

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

Affected Aircraft

Univair Aircraft Corporation Model 108, 108-1, 108-2, 108-3 aircraft

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

Federal Register Abstract

Fuel drip strip

Applicability Source Text

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AD Final Rules - DRS_50-25-01.html
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Details
AD Number:
50-25-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; STINSON Model All Model 108 Series Aircraft
Subject:
Fuel drip strip
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Univair Aircraft Corporation
Model:
108 | 108-1 | 108-2 | 108-3
Product Type:
Aircraft
Product Subtype:
Small 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Superseded AD: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Superseded By: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: 50-25-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   50-25-01

SUBJECT HEADING:   Airworthiness Directives; STINSON Model All Model 108 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   50-25-01 STINSON: Applies to All Model 108 Series Aircraft.
Compliance required not later than September 1, 1950.
Reports have been received of fuel seepage into the space between the inner cabin trim and the outer fabric covering of the fuselage. This results in soaking of insulating material in the cabin wall. The source of the fuel can be spillage during filling of tanks, thermal expansion of fuel in full tanks, or tank leakage. This fuel runs to the under surface of the wing, adhering to the lower curved surface of the trailing edge of the wing at the flap well, thence inboard to the fuselage and across the rear window. Since the window seal is often not perfectly tight the fuel may then enter the cabin wall.
To preclude the fire hazard of fuel soaked insulation within the cabin wall due to these causes, a drip strip similar to that shown in Figure 1 should be installed on the underside of each wing. This drip strip will prevent fuel from flowing from the wing to the fuselage.
(Piper Service Bulletin No. 115, dated March 31, 1950, covers this same subject.)


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_50-25-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
50-25-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; STINSON Model All Model 108 Series Aircraft
Subject:
Fuel drip strip
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Univair Aircraft Corporation
Model:
108 | 108-1 | 108-2 | 108-3
Product Type:
Aircraft
Product Subtype:
Small 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: 50-25-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   50-25-01

SUBJECT HEADING:   Airworthiness Directives; STINSON Model All Model 108 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   50-25-01 STINSON: Applies to All Model 108 Series Aircraft.
Compliance required not later than September 1, 1950.
Reports have been received of fuel seepage into the space between the inner cabin trim and the outer fabric covering of the fuselage. This results in soaking of insulating material in the cabin wall. The source of the fuel can be spillage during filling of tanks, thermal expansion of fuel in full tanks, or tank leakage. This fuel runs to the under surface of the wing, adhering to the lower curved surface of the trailing edge of the wing at the flap well, thence inboard to the fuselage and across the rear window. Since the window seal is often not perfectly tight the fuel may then enter the cabin wall.
To preclude the fire hazard of fuel soaked insulation within the cabin wall due to these causes, a drip strip similar to that shown in Figure 1 should be installed on the underside of each wing. This drip strip will prevent fuel from flowing from the wing to the fuselage.
(Piper Service Bulletin No. 115, dated March 31, 1950, covers this same subject.)


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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