Airworthiness Directive · Amendment 39-14948 · Boeing Model 767 Airplanes
Boeing Model 767 Airplanes
This AD applies to all Boeing Model 767-200, -300, -300F, and -400ER series airplanes, certificated in any category.
The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 767 airplanes. This AD requires an inspection of each main tank fuel boost pump for the presence of a pump shaft flame arrestor, and if the flame arrestor is missing, replacement of that pump with a pump having a pump shaft flame arrestor. This AD also requires repetitive measurements of the flame arrestor's position in the pump, and corrective actions if necessary. This AD also requires the replacement of the pump with a new or modified pump, which ends the repetitive measurements. This AD results from reports that certain fuel boost pumps may not have flame arrestors installed in the pump shaft and reports that the pin that holds the flame arrestor in place can break due to metal fatigue. We are issuing this AD to prevent the possible migration of a flame from a main tank fuel boost pump inlet to the vapor space of that fuel tank, and consequent ignition of fuel vapors, which could result in a fire or explosion.
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
For airplanes having line numbers (L/Ns) 1 through 914 inclusive, except as provided by paragraph (h) of this AD: Within 365 days after the effective date of this AD, do a detailed inspection of each main tank fuel boost pump to determine if the pump shaft flame arrestor is installed, a measurement of the flame arrestor's position in the pump, and all applicable corrective actions, by accomplishing all the actions specified in the Accomplishment Instructions of Boeing Alert Service Bulletin 767-28A0077 (for Model 767-200, -300, and -300F series airplanes) or Boeing Alert Service Bulletin 767-28A0081 (for Model 767-400ER series airplanes), both Revision 1, both dated July 8, 2004, as applicable. Repeat the measurement of the flame arrestor's position in the pump thereafter at intervals not to exceed the applicable time specified in paragraph (f)(1) or (f)(2) of this AD, until the replacement required by paragraph (i) of this AD is accomplished. All applicable corrective actions must be done before further flight.
Note 1: Any inspection/measurement of the pumps on the left and right main fuel tanks may be done separately provided that the actions are done on all pumps within the compliance time specified in paragraph (f) of this AD.
(1) For airplanes that have accumulated more than 15,000 total flight hours as of the date the initial actions are done in accordance with paragraph (f) of this AD: Repeat the measurement thereafter at intervals not to exceed 6,000 flight hours or 24 months, whichever comes first.
(2) For airplanes that have accumulated 15,000 total flight hours or fewer as of the date the initial actions are done in accordance with paragraph (f) of this AD: Do the measurement specified in paragraph (f) of this AD within 365 days after the date on which the airplane accumulates 15,000 total flight hours or within 24 months after performing the initial inspection required by paragraph (f) of this AD, whichever occurs later. Repeat the measurement thereafter at intervals not to exceed 6,000 flight hours or 24 months, whichever comes first.
Note 2: Boeing Alert Service Bulletins 767-28A0077 and 767-28A0081 reference Hamilton Sundstrand Service Bulletin 5006003-28-2, dated October 25, 2002, as an additional source of service information for accomplishment of the inspection and corrective actions. Although the Hamilton Sundstrand service bulletin specifies to return main tank fuel boost pumps with damaged, broken, or out-of-position flame arrestors to a repair shop, that action is not required by this AD.
Note 3: For the purposes of this AD, a detailed inspection is: “An intensive examination of a specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirror, magnifying lenses, etc., may be necessary. Surface cleaning and elaborate procedures may be required.”
(g) For airplanes having L/Ns 915 and on, except as provided by paragraph (h) of this AD: At the applicable time specified in paragraph (g)(1) or (g)(2) of this AD, do a detailed inspection of each main tank fuel boost pump to determine if the pump shaft flame arrestor is installed, a measurement of the flame arrestor's position in the pump, and all applicable corrective actions, by accomplishing all the actions specified in the Accomplishment Instructions of Boeing Alert Service Bulletin 767-28A0077 (for Model 767-200, -300, and -300F series airplanes) or Boeing Alert Service Bulletin 767-28A0081 (for Model 767-400ER series airplanes), both Revision 1, both dated July 8, 2004, as applicable. Repeat the measurement of the flame arrestor's position in the pump thereafter at intervals not to exceed 6,000 flight hours or 24 months, whichever comes first, until the replacement required by paragraph (i) of this AD is accomplished. All applicable corrective actions must be done before further flight.
Note 4: Any inspection/measurement of the pumps on the left and right main fuel tanks may be done separately provided that the actions are done on all pumps within the compliance time specified in paragraph (g) of this AD.
(1) For airplanes that have accumulated more than 15,000 total flight hours as of the effective date of this AD, do the actions within 365 days after the effective date of this AD.
(2) For airplanes that have accumulated 15,000 total flight hours or fewer as of the effective date of this AD, do the actions within 365 days after the date on which the airplane accumulates 15,000 total flight hours.
For any period when the part number (P/N) of a main tank fuel boost pump installed on any airplane, as conclusively determined from a review of airplane maintenance records, is P/N 5006003D, no further action is required by paragraphs (f), (g), and (i) of this AD for that pump only.
(i) Within 36 months after the effective date of this AD, replace the left and right main tank fuel boost pumps with new or modified pumps in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 767-28A0088 (for Model 767-200, -300, and -300F series airplanes) or Boeing Alert Service Bulletin 767-28A0089 (for Model 767-400ER series airplanes), both dated February 24, 2005, as applicable. Accomplishment of the replacement terminates the repetitive measurement requirements of paragraphs (f) and (g) of this AD for that pump only.
Note 5: Any replacement of the pumps on the left and right main fuel tanks may be done separately provided that all pumps are replaced within the compliance time specified in paragraph (i) of this AD.
Note 6: Boeing Alert Service Bulletins 767-28A0088 and 767-28A0089 reference Hamilton Sundstrand Service Bulletin 5006003-28-3, dated December 8, 2004, as the appropriate source of service information for modifying the pump.
Inspections accomplished before the effective date of this AD in accordance with Boeing Alert Service Bulletin 767-28A0077, dated March 6, 2003; or Boeing Alert Service Bulletin 767-28A0081, dated March 6, 2003; are considered acceptable for compliance with the corresponding action specified in paragraphs (f) and (g) of this AD.
As of the effective date of this AD, only main tank fuel boost pumps identified in paragraphs (k)(1) and (k)(2) of this AD may be installed on any airplane.
(1) Any main tank fuel boost pump that has been inspected, and on which all applicable corrective actions have been performed, in accordance with paragraph (f) or (g) of this AD.
(2) Any main tank fuel boost pump having P/N 5006003D.
