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Engine Bleed Fan Air Valve

36-11-04A

Repair interval C

Nbr installed 2

Nbr required 1

Placard Yes

One may be inoperative provided that the associated engine bleed air supply system is considered inoperative.
Refer to Item 36-11-01 Engine Bleed Air Supply System

For details see MEL for your Company

— RESET PROCEDURE—

36-11-00-740-001-A BITE Test of the BMC 1(2)

TSM 36-11-00-810-886-A Low Bleed Temperature of the Engine 1(2) in Climb(Cruise, Descent)

36-11-34 PB 401 BLEED MONITORING COMPUTER (BMC) replace

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All instructions and limitations given in those documents that relate to the resetting of systems both on the ground and in the air must be respected. No reset should be attempted without a thorough appreciation of the technical ramifications. No more than one computer should be reset at any one time. No reset should be attempted in flight unless specifically permitted by the QRH. Maintenance messages remaining after a reset require engineering investigation.

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ACARS (4) ACSC (18) ADIRU (19) AEVC (10) ANTI ICE SYSTEM (14) AOA (3) APU (4) ATC (1) ATSU (5) BAT (3) BCL (5) BMC (29) BSCU (12) BTC (3) CHC (1) CIDS (7) CPC (15) CZC (1) DFDR (4) DMC (8) ECB (1) ECMU (7) EFCS (18) EIVMU (18) ELAC (6) EMCU (1) ESS (5) FAC (8) FADEC (24) FCDC (4) FCMC (25) FCPC (21) FCSC (4) FCU (3) FDU (12) FM (2) FMGEC (5) FQI (3) FTIS (1) FWC (22) GCU (9) GPCU (2) GPS (1) GPWS (2) HF (1) HSMU (20) ICE DET (2) ILS (2) IR (1) LGCIU (21) MMR (2) PBC (2) PHC (36) PSCU (12) PWS (2) RAD ALT (2) RPCU (1) SATCOM (1) SDAC (9) SDCU (22) SEC (10) SFCC (15) TCAS/T2CAS (1) TR (3) VC (20) VHF (1) WHC (8)

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