AD 73-10-02

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AD Number:
73-10-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BENDIX: Applies to Bendix Fuel Injectors Models RSA-5AD1, RSA-51B1 and RSA-10AD1
Subject:
Bendix Fuel Injectors
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/16/1973
Make:
Bendix | Lycoming Engines | Textron Lycoming, AVCO Corporation
Model:
Fuel Injectors | AIO-320-A1A | AIO-320-A1B | AIO-320-A2A | AIO-320-A2B | AIO-320-B1B | AIO-320-C1B |...Show more
Product Type:
Appliance
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 73-10-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1634

AD NUMBER:   73-10-02

SUBJECT HEADING:   Airworthiness Directives; BENDIX: Applies to Bendix Fuel Injectors Models RSA-5AD1, RSA-51B1 and RSA-10AD1

ACTION:  

SUMMARY:  

DATES:   Effective May 16, 1973.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
73-10-02 BENDIX: Amendment 39-1634. Applies to Bendix Fuel Injectors Models RSA-5AD1, RSA-51B1 and RSA-10AD1 installed on Lycoming Engines Models: IO540-C1B5, -C1C5, -C2C, -C4B5, -C4C5, -D4A5, -D4B5, -J4A5, -L1A5, -M1A5, -M2A5D, -N1A5, -R1A5; IO360-A1A, -A1B, -A1B6, -A1B6D, -A1C, -A1D, -A1D6, -A2A, -A2B, -A2C, -B1B, -B1C, -B1D, -B1E, -B1F, -B2E, -B2F, -B4A, -C1A, -C1B, -C1C, -C1D6, -C1E6, -C1F, -D1A, -E1A, -F1A; IO-320-A1A, -A2A, -E2A, -B1A, -B1B, -B1C, -B1D, -B2A, -C1A, -D1A, -D1B, -E2B; AIO-320-A1A, -A1B, -A2A, -A2B, -B1B, -C1B; LIO-320-B1A, -C1A; IGO-480-A1A6; IVO-360-A1A; HIO-360-A1A, -B1A, -B1B, -C1A, -C1B; AIO-360-A1A, -A2A, -A1B, -A2B, -B1B; LIO-360-C1E6; IO-720-A1A, -B1A; IVO-540-A1A; TIO-540-A1A, -A1B, -A1C, -A2A, -A2C, -A2B, -A1A, -B1A, -C1A, -E1A, -G1A, -H1A; TIO-360-A1A, -A1B, -A3B6; and IO-720-A1B, -C1B.

Compliance required within the next 25 hours time in service after the effective date of this Airworthiness Directive, and at each subsequent installation of the subject Fuel Injectors.

To detect defective diaphragm assemblies, Bendix P/N 2529470, in Bendix Fuel Injectors, accomplish the following:

a) Determine from the airplane and engine logbooks whether the fuel injector has been repaired and/or overhauled between September 30, 1972, and February 28, 1973. If it is established that the fuel injector has not been repaired and/or overhauled between September 30, 1972, and February 28, 1973 record compliance with Paragraph "a" of this Airworthiness Directive in the engine logbook.

b) If the fuel injector has been repaired and/or overhauled between September 30, 1972, and February 28, 1973, unless already accomplished, inspect the fuel injector in accordance with Bendix Service Bulletin No. RS-41 dated February 13, 1973, Bendix Service Bulletin No. RS-41 revised April 7, 1973, or subsequent FAA approved revisions; or by any other method approved by the Chief, Engineering and Manufacturing Branch, Great Lakes Region. Indicate compliance on airworthy parts by stamping a "T" after the fuel injector serial number, and record compliance in the engine logbook or return to service statement. Replace or repair fuel injectors having defective diaphragms with airworthy fuel injector units.

NOTE: Only appropriately rated FAA approved repair stations are authorized to perform the inspection in "b" above.

This amendment is effective May 16, 1973.

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