AD 81-07-06

Active

AC Fuel Pumps

Key Information
81-07-06
Active
April 01, 1981
Not specified
Unknown
39-4071
Applicability
["Engine"]
Not specified
Continental Motors Continental Motors
A-65-1 A-65-12 A-65-12F A-65-12FJ A-65-12J A-65-14 A-65-14F A-65-14FJ A-65-14J A-65-3 A-65-6 A-65-6J A-65-7 A-65-8 A-65-8F A-65-8FJ A-65-8J A-65-9 A-65-9F A-65-9FJ A-65-9J A100-1 A100-2 A75-3 A75-6 A75-6J A75-8 A75-8F A75-8FJ A75-8J A75-9 A75-9J C-125-1 C-125-2 C90-12F C90-12FH C90-12FJ C90-12FP C90-14F C90-14FH C90-14FJ C90-16F C90-8F C90-8FJ O-200-A O-200-B O-200-C C75-12F C75-12FH C75-12FJ C75-12J C75-15 C75-8F C75-8FHJ C75-8FJ C85-12F C85-12FJ C85-12J C85-14F C85-15 C85-15F C85-8FHJ C85-8FJ
Regulatory Text

81-07-06 TELEDYNE CONTINENTAL MOTORS: Amendment 39-4071. Applies to Continental A-65, A75, C75, C85, C90, A-100, C125, and O-200 series engines with AC fuel pumps, TCM part number 40585, 40695 or 631391 installed. Compliance required within 30 days after the effective date of this AD, or within the next 25 hours time in service after the effective date of this AD, whichever occurs first, unless already accomplished within the last 12 months and at intervals not to exceed 12 months after the last inspection. To prevent fuel starvation due to fuel flow restriction through the pump screen accomplish the following:
a. Remove safety wire and bolt from fuel pump top cover. Discard fiber washer under bolt.
b. Remove the fuel pump top cover. Discard cork cover gasket.
c. Remove fuel pump screen.
d. Inspect the fuel pump and fuel pump screen for contamination.
(1) If contaminated, clean fuel pump and fuel pump screen.
(2) If fuel pump is damaged by corrosion, replace with an applicable serviceable fuel pump.
(3) If fuel pump screen is damaged by corrosion or handling, replace with a serviceable fuel pump screen, TCM P/N 643913.
e. Reinstall fuel pump screen, fuel pump cover with new cork cover gasket, TCM P/N 643915 and new bolt gasket P/N 643914. Torque bolt to 30 5 inch-pounds.
f. Resafety wire fuel pump top cover bolt and check for leaks.
g. Make the appropriate maintenance record entry.
An equivalent method of compliance may be approved by the Chief, Engineering and Manufacturing Branch, Federal Aviation Administration, Southern Region.
Teledyne Continental Motors Service Bulletin M81-8, dated March 9, 1981, pertains to this subject.
This amendment becomes effective April 1, 1981.

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References
This information is not available.
--- - Part 39
FAA Documents