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Airworthiness directives › 2022-04-07

AD 2022-04-07 Airworthiness Directives; General Electric Company Turbofan Engines

2022-03-09
2022-02-22
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Engine
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Applicability*9

This AD applies to all General Electric Company (GE) GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2, GEnx-1B67, GEnx-1B67/P1, GEnx-1B67/P2, GEnx-1B70, GEnx-1B70/75/P1, GEnx-1B70/75/P2, GEnx-1B70/P1, GEnx-1B70/P2, GEnx-1B70C/P1, GEnx-1B70C/P2, GEnx-1B74/75/P1, GEnx-1B74/75/P2, GEnx-1B76/P2, GEnx-1B76A/P2, GEnx-2B67, GEnx-2B67B, and GEnx-2B67/P model turbofan engines with: (1) A fuel metering unit (FMU) VIN 8062-1094 part number (P/N) 2122M20P07, VIN 8062-1176 P/N 2122M20P08, VIN 8062-1106 P/N 2459M17P01, or VIN 8062-1177 P/N 2459M17P02, installed; and (2) An FMU having a serial number (S/N) identified in Paragraph 4, Appendix A, Table 1, of either GE GEnx-1B Service Bulletin (SB) 73-0100 R00, dated December 3, 2021 (GEnx-1B SB 73-0100), or GE GEnx-2B SB 73-0092 R00, dated December 3, 2021 (GEnx-2B SB 73-0092).

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

(1) Within 150 flight cycles after the effective date of this AD, perform either an on-wing or off-wing shim check inspection using a 0.005 inch feeler gauge of the FMU BPV plug to verify the FMU BPV plug is properly installed using the Accomplishment Instructions, paragraph 3.A.(4) or paragraph 3.B.(3), of GEnx-1B SB 73-0100 (for GEnx-1B models) or the Accomplishment Instructions, paragraph 3.A.(4) or paragraph 3.B.(3), of GEnx-2B SB 73-0092 (for GEnx-2B models), as applicable. Perform the shim check inspection on any flat side of the FMU BPV plug. (2) If, during the inspection required by paragraph (g)(1) of this AD, the 0.005 inch feeler gauge can fit between the FMU BPV plug and the FMU housing on the flat side, before further flight, remove the FMU and replace with an FMU eligible for installation.

Unsafe condition

This AD was prompted by an in-flight shutdown (IFSD) of an engine and subsequent investigation by the manufacturer that revealed an improperly torqued FMU bypass valve (BPV) plug. The FAA is issuing this AD to prevent fuel system leakage from the FMU. The unsafe condition, if not addressed, could result in the loss of engine thrust control, IFSD, and reduced control of the aircraft.

Affected ADs

None.

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