AD 73-10-02

Active

Bendix Fuel Injectors

Key Information
73-10-02
Active
May 16, 1973
Not specified
Unknown
39-1634
Applicability
["Appliance"]
Not specified
Bendix Lycoming Engines Textron Lycoming, AVCO Corporation
Fuel Injectors AIO-320-A1A AIO-320-A1B AIO-320-A2A AIO-320-A2B AIO-320-B1B AIO-320-C1B AIO-360-A1A AIO-360-A1B AIO-360-A2A AIO-360-A2B AIO-360-B1B HIO-360-A1A HIO-360-B1A HIO-360-B1B HIO-360-C1A HIO-360-C1B IGO-480-A1A6 IO-320-A1A IO-320-A2A IO-320-B1A IO-320-B1B IO-320-B1C IO-320-B1D IO-320-B2A IO-320-C1A IO-320-D1A IO-320-D1B IO-320-E2A IO-320-E2B IO-360-A1A IO-360-A1B IO-360-A1B6 IO-360-A1B6D IO-360-A1C IO-360-A1D IO-360-A1D6 IO-360-A2A IO-360-A2B IO-360-A2C IO-360-B1B IO-360-B1C IO-360-B1D IO-360-B1E IO-360-B1F IO-360-B2E IO-360-B2F IO-360-B4A IO-360-C1A IO-360-C1B IO-360-C1C IO-360-C1D6 IO-360-C1E6 IO-360-C1F IO-360-D1A IO-360-E1A IO-360-F1A IO-540-C1B5 IO-540-C1C5 IO-540-C2C IO-540-C4B5 IO-540-C4C5 IO-540-D4A5 IO-540-D4B5 IO-540-J4A5 IO-540-L1A5 IO-540-M1A5 IO-540-M2A5D IO-540-N1A5 IO-540-R1A5 IVO-360-A1A IVO-540-A1A LIO-320-B1A LIO-360-C1E6 TIO-360-A1A TIO-360-A1B TIO-360-A3B6 TIO-540-A1A TIO-540-A1B TIO-540-A1C TIO-540-A2A TIO-540-A2B TIO-540-A2C TIO-540-C1A TIO-540-E1A TIO-540-G1A TIO-540-H1A IO-720-A1A IO-720-A1B IO-720-B1A IO-720-C1B
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.

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
FAA Documents