AD 87-07-05

final rule

Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes

AD Number
87-07-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Maryland Air Industries, Inc. F-27 Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27A Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27B Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27F Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27G Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27J Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes
aircraft Maryland Air Industries, Inc. F-27M Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes

Unsafe Condition

Inflight loss of the wing-to-fuselage fairing due to cracks or looseness around screws and grommets.

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

Required Actions

Conduct daily visual inspections of wing-to-fuselage fairings for cracks or looseness around screws and grommets. If found, install washer P/N AN970-3 and use screw P/N AN525-10R9 instead of P/N AN509-10R9 before further flight. Modify fairings per Fairchild Service Bulletin F27-53-9, Rev 1 or later FAA-approved revisions to terminate daily inspections.

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

Fairchild Republic Company Model F-27 series airplanes, Manufacturer's Serial Numbers 1 through 39, and 41 through 48; equipped with wing-to-fuselage fairings Part Numbers 27-100102-1/-2 or 27-100103-1/-2/-31/-32.

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

Federal Register Abstract

Wing-To-Fuselage Fairing

Applicability Source Text

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AD Final Rules - DRS_87-07-05.html
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AD Number:
87-07-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes
Subject:
Wing-To-Fuselage Fairing
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/20/1987
Make:
Maryland Air Industries, Inc.
Model:
F-27 | F-27A | F-27B | F-27F | F-27G | F-27J | F-27M
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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 87-07-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5596

AD NUMBER:   87-07-05

SUBJECT HEADING:   Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes


ACTION:  

SUMMARY:  

DATES:   Effective April 20, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-07-05 FAIRCHILD REPUBLIC COMPANY: Amendment 39-5596. Applies to Model F- 27 series airplanes, Manufacturer's Serial Numbers 1 through 39, and 41 through 48; equipped with wing-to-fuselage fairings, Part Numbers (P/N) 27-100102-1 or -2, and 27-100103-1, -2, -31, or -32; certificated in any category. Compliance required as indicated, unless previously accomplished.

To prevent the inflight loss of the wing-to-fuselage fairing, accomplish the following:

A. Conduct a daily visual inspection of wing-to-fuselage fairing, both right and left, for cracks or looseness around screws and grommets. If cracks or looseness is found, before further flight install washer P/N AN970-3, and use washer head screw P/N AN525-10R9 in place of P/N AN509-10R9. Daily inspections are to continue until the modification of the fairings, described in paragraph B., below, is accomplished.

NOTE: Caution should be used not to overtighten screws, as cracks may develop.

B. Modification of the wing-to-fuselage fairings in accordance with Fairchild Service Bulletin F27-53-9, Revision 1, dated May 13, 1959, or later FAA-approved revisions, constitutes terminating action for the daily inspection requirement of paragraph A., above.

C. Alternate means of compliance or adjustment of compliance time, which provide an acceptable level of safety, may be used when approved by the Manager, New York Aircraft Certification Office, FAA, New England Region.

D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this airworthiness directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Fairchild Republic Company, Showalter Road, Hagerstown, Maryland 21740. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the FAA, New England Region, New York Aircraft Certification Office, 181 South Franklin Avenue, Room 202, Valley Stream, New York.

This amendment supersedes AD 58-25-03.

This amendment becomes effective April 20, 1987.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_87-07-05.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
87-07-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes
Subject:
Wing-To-Fuselage Fairing
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/20/1987
Make:
Maryland Air Industries, Inc.
Model:
F-27 | F-27A | F-27B | F-27F | F-27G | F-27J | F-27M
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:
AIRWORTHINESS DIRECTIVES FINAL RULES: 87-07-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-5596

AD NUMBER:   87-07-05

SUBJECT HEADING:   Airworthiness Directives; FAIRCHILD REPUBLIC COMPANY Model F-27 Series Airplanes


ACTION:  

SUMMARY:  

DATES:   Effective April 20, 1987.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
87-07-05 FAIRCHILD REPUBLIC COMPANY: Amendment 39-5596. Applies to Model F- 27 series airplanes, Manufacturer's Serial Numbers 1 through 39, and 41 through 48; equipped with wing-to-fuselage fairings, Part Numbers (P/N) 27-100102-1 or -2, and 27-100103-1, -2, -31, or -32; certificated in any category. Compliance required as indicated, unless previously accomplished.

To prevent the inflight loss of the wing-to-fuselage fairing, accomplish the following:

A. Conduct a daily visual inspection of wing-to-fuselage fairing, both right and left, for cracks or looseness around screws and grommets. If cracks or looseness is found, before further flight install washer P/N AN970-3, and use washer head screw P/N AN525-10R9 in place of P/N AN509-10R9. Daily inspections are to continue until the modification of the fairings, described in paragraph B., below, is accomplished.

NOTE: Caution should be used not to overtighten screws, as cracks may develop.

B. Modification of the wing-to-fuselage fairings in accordance with Fairchild Service Bulletin F27-53-9, Revision 1, dated May 13, 1959, or later FAA-approved revisions, constitutes terminating action for the daily inspection requirement of paragraph A., above.

C. Alternate means of compliance or adjustment of compliance time, which provide an acceptable level of safety, may be used when approved by the Manager, New York Aircraft Certification Office, FAA, New England Region.

D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this airworthiness directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Fairchild Republic Company, Showalter Road, Hagerstown, Maryland 21740. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or the FAA, New England Region, New York Aircraft Certification Office, 181 South Franklin Avenue, Room 202, Valley Stream, New York.

This amendment supersedes AD 58-25-03.

This amendment becomes effective April 20, 1987.

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.