AD 75-17-16

final rule

Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes

AD Number
75-17-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft American Champion Aircraft Corp. 7ECA Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes
aircraft American Champion Aircraft Corp. 7GCAA Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes
aircraft American Champion Aircraft Corp. 7GCBC Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes
aircraft American Champion Aircraft Corp. 7KCAB Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes
aircraft American Champion Aircraft Corp. 8GCBC Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes
aircraft American Champion Aircraft Corp. 8KCAB Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes

Unsafe Condition

Engine power loss due to fatigue failure of the carburetor alternate air valves.

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

Required Actions

Install Bellanca service kits (No. 248A or 251) within 10 hours time in service after specified dates. Inspect the alternate air valve for cracks at each annual, progressive, or 100-hour inspection and replace if cracks are found.

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

Compliance Time

Within the next 10 hours time in service after the effective date of this AD or June 25, 1975, as specified for each model and serial range.

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

Affected Aircraft

Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC with specific serial ranges: Models 7ECA (S/N 985-74-1108-75; 723-70-984-73), 7GCAA (S/N 280-74-319-75; 205-70-279-73), 7GCBC (S/N 604-74-859-75; 202-70-603-73), 7KCAB (S/N 405-74-532-75; 209-70-404-73), 8KCAB (S/N 12074-204-75; 4-71-119-73), 8GCBC (S/N 1-74-181-75).

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

Federal Register Abstract

Engine Power Loss

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-17-16.html
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AD Number:
75-17-16
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes
Subject:
Engine Power Loss
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/12/1975
Make:
American Champion Aircraft Corp.
Model:
7ECA | 7GCAA | 7GCBC | 7KCAB | 8GCBC | 8KCAB
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: 75-17-16
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2309

AD NUMBER:   75-17-16

SUBJECT HEADING:   Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 12, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-17-16 BELLANCA: Amendment 39-2309. Applies to the Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC airplanes as set forth below.

Compliance required as indicated, unless previously accomplished. A special flight permit pursuant to FAR 21.197 may be issued to allow ferrying of the aircraft to a facility where the required maintenance can be performed.

To prevent possible engine power loss due to fatigue failure of the carburetor alternate air valves, accomplish the following:

A). Within the next 10 hours time in service after the effective date of this AD on Models 7ECA (S/N 985-74 thru 1108-75), 7GCAA (S/N 280-74 thru 319-75), 7GCBC (S/N 604- 74 thru 859-75), 7KCAB (S/N 405-74 thru 532-75), 8KCAB (S/N 12074 thru 204-75), 8GCBC (S/N 1-74 thru 181-75), install Bellanca service Kit No. 248A. Bellanca Service Letter No. 118A pertains to this subject.

B). Within the next 10 hours time in service after June 25, 1975, on the Models 7ECA (S/N 723-70 thru 984-73), 7GCAA (S/N 205-70 thru 279-73), 7GCBC (S/N 202-70 thru 603-73), 7KCAB (S/N 209-70 thru 404-73), 8KCAB (S/N 4-71 thru 119-73), install Bellanca Service Kit No. 251. Bellanca Service Letter No. 120 applies to this subject.

C). At each annual, progressive, or 100-hour inspection as required by Federal Aviation Regulation 91.169, on the Models covered by paragraphs A and B and all subsequent serials of those same models, inspect the alternate air valve for cracks. If any cracks are noted, replace the alternate air valve by installing Bellanca Service Kit 251 on Models 7ECA (S/N 723- 70 thru 984-73), 7GCAA (S/N 205-70 thru 279-73), 7GCBC (S/N 202-70 thru 603-73) 7KCAB (S/N 209-70 thru 404-73), 8KCAB (S/N 4-71 thru 119- 73); Bellanca Service Kit #248A on Models 7ECA (S/N 985-74 and up), 7GCAA (S/N 280-74 and up), 7GCBC (604-74 and up), 7KCAB (405-74 and up), 8KCAB (S/N 120-74 and up), 8GCBC (S/N 1-74 and up).

Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, Great Lakes Region, 2300 E. Devon Avenue, Des Plaines, Illinois, 60018.

This Amendment supersedes Amendment 39-2173, 40 F. R. 17138, AD 75-09-02 as amended by Amendment 39-2243, and Amendment 39-2261.

This amendment becomes effective August 12, 1975.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-17-16.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-17-16
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes
Subject:
Engine Power Loss
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/12/1975
Make:
American Champion Aircraft Corp.
Model:
7ECA | 7GCAA | 7GCBC | 7KCAB | 8GCBC | 8KCAB
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: 75-17-16
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2309

AD NUMBER:   75-17-16

SUBJECT HEADING:   Airworthiness Directives; Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 12, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-17-16 BELLANCA: Amendment 39-2309. Applies to the Bellanca Models 7ECA, 7GCAA, 7GCBC, 7KCAB, 8KCAB, and 8GCBC airplanes as set forth below.

Compliance required as indicated, unless previously accomplished. A special flight permit pursuant to FAR 21.197 may be issued to allow ferrying of the aircraft to a facility where the required maintenance can be performed.

To prevent possible engine power loss due to fatigue failure of the carburetor alternate air valves, accomplish the following:

A). Within the next 10 hours time in service after the effective date of this AD on Models 7ECA (S/N 985-74 thru 1108-75), 7GCAA (S/N 280-74 thru 319-75), 7GCBC (S/N 604- 74 thru 859-75), 7KCAB (S/N 405-74 thru 532-75), 8KCAB (S/N 12074 thru 204-75), 8GCBC (S/N 1-74 thru 181-75), install Bellanca service Kit No. 248A. Bellanca Service Letter No. 118A pertains to this subject.

B). Within the next 10 hours time in service after June 25, 1975, on the Models 7ECA (S/N 723-70 thru 984-73), 7GCAA (S/N 205-70 thru 279-73), 7GCBC (S/N 202-70 thru 603-73), 7KCAB (S/N 209-70 thru 404-73), 8KCAB (S/N 4-71 thru 119-73), install Bellanca Service Kit No. 251. Bellanca Service Letter No. 120 applies to this subject.

C). At each annual, progressive, or 100-hour inspection as required by Federal Aviation Regulation 91.169, on the Models covered by paragraphs A and B and all subsequent serials of those same models, inspect the alternate air valve for cracks. If any cracks are noted, replace the alternate air valve by installing Bellanca Service Kit 251 on Models 7ECA (S/N 723- 70 thru 984-73), 7GCAA (S/N 205-70 thru 279-73), 7GCBC (S/N 202-70 thru 603-73) 7KCAB (S/N 209-70 thru 404-73), 8KCAB (S/N 4-71 thru 119- 73); Bellanca Service Kit #248A on Models 7ECA (S/N 985-74 and up), 7GCAA (S/N 280-74 and up), 7GCBC (604-74 and up), 7KCAB (405-74 and up), 8KCAB (S/N 120-74 and up), 8GCBC (S/N 1-74 and up).

Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, Great Lakes Region, 2300 E. Devon Avenue, Des Plaines, Illinois, 60018.

This Amendment supersedes Amendment 39-2173, 40 F. R. 17138, AD 75-09-02 as amended by Amendment 39-2243, and Amendment 39-2261.

This amendment becomes effective August 12, 1975.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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