AD 53-08-01

final rule

Airworthiness Directives; All Navion Models Except Those Incorporating Palo Alto Airport Co. or Symon Engineering Co. Horizontal Stabilizer Modifications

AD Number
53-08-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Sierra Hotel Aero, Inc. Navion (Army L-17A) Airworthiness Directives; All Navion Models Except Those Incorporating Palo Alto Airport Co. or Symon Engineering Co. Horizontal Stabilizer Modifications
aircraft Sierra Hotel Aero, Inc. Navion A (Army L-17B and L-17C) Airworthiness Directives; All Navion Models Except Those Incorporating Palo Alto Airport Co. or Symon Engineering Co. Horizontal Stabilizer Modifications
aircraft Sierra Hotel Aero, Inc. Navion B Airworthiness Directives; All Navion Models Except Those Incorporating Palo Alto Airport Co. or Symon Engineering Co. Horizontal Stabilizer Modifications

Unsafe Condition

Improper rivet edge distance on 145-21404-1 and -2 front fittings of the horizontal stabilizer may result in structural failure due to insufficient material extending beyond the rivet holes.

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

Required Actions

Inspect both 145-21404-1 and -2 front fittings for proper rivet edge distance. If the edge distance is less than 1/16 inch, install new fittings with proper edge distance.

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

Compliance Time

June 15, 1953, or next 100-hour inspection, whichever is first

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

Affected Aircraft

Sierra Hotel Aero, Inc. Navion models (Army L-17A), Navion A (Army L-17B and L-17C), Navion B, except those incorporating Palo Alto Airport Co. or Symon Engineering Co. horizontal stabilizer modifications.

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

Federal Register Abstract

Horizontal Stabilizer Fitting

Applicability Source Text

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AD Final Rules - DRS_53-08-01.html
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AD Number:
53-08-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; All Navion Models Except Those Incorporating Palo Alto Airport Co. or Symo...Show more
Subject:
Horizontal Stabilizer Fitting
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Sierra Hotel Aero, Inc.
Model:
Navion (Army L-17A) | Navion A (Army L-17B and L-17C) | Navion B
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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 53-08-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   53-08-01

SUBJECT HEADING:   Airworthiness Directives; All Navion Models Except Those Incorporating Palo Alto Airport Co. or Symon Engineering Co. Horizontal Stabilizer Modifications

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   53-08-01 NAVION: Applies to All Models Except Those Incorporating Palo Alto Airport Co. or Symon Engineering Co. Horizontal Stabilizer Modifications.

Compliance required by June 15, 1953, or next 100-hour inspection, whichever is first.

Inspect both 145-21404-1 and -2 front fittings on the horizontal stabilizer for proper rivet edge distance. If the entire outboard edge of the steel fitting extends past the outboard edge of the butt rib, no further action is required. On the other hand, if the edge of the fitting disappears behind the rib, it will be necessary to ascertain that at least 1/16 inch of material (steel fitting) extends beyond the edge of all rivet holes. Whenever the edge distance is found to be less than 1/16 inch, a new fitting should be installed with proper edge distance.

(A method of conducting the above inspection is described in Ryan Field Service Bulletin No. 19, dated February 16, 1953, which covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_53-08-01.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
53-08-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; All Navion Models Except Those Incorporating Palo Alto Airport Co. or Symo...Show more
Subject:
Horizontal Stabilizer Fitting
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Sierra Hotel Aero, Inc.
Model:
Navion (Army L-17A) | Navion A (Army L-17B and L-17C) | Navion B
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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 53-08-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   53-08-01

SUBJECT HEADING:   Airworthiness Directives; All Navion Models Except Those Incorporating Palo Alto Airport Co. or Symon Engineering Co. Horizontal Stabilizer Modifications

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   53-08-01 NAVION: Applies to All Models Except Those Incorporating Palo Alto Airport Co. or Symon Engineering Co. Horizontal Stabilizer Modifications.

Compliance required by June 15, 1953, or next 100-hour inspection, whichever is first.

Inspect both 145-21404-1 and -2 front fittings on the horizontal stabilizer for proper rivet edge distance. If the entire outboard edge of the steel fitting extends past the outboard edge of the butt rib, no further action is required. On the other hand, if the edge of the fitting disappears behind the rib, it will be necessary to ascertain that at least 1/16 inch of material (steel fitting) extends beyond the edge of all rivet holes. Whenever the edge distance is found to be less than 1/16 inch, a new fitting should be installed with proper edge distance.

(A method of conducting the above inspection is described in Ryan Field Service Bulletin No. 19, dated February 16, 1953, which covers this same subject.)

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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