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Another excellent brief , and very well presented…. As with all your other ABNM PROC, the visuals of the ECAM PFD ND are vital, as they always say “ a picture tells a thousand words” Thanks again , great resource material Capt SQ
Why would landing gear retraction be unavailable green hydraulic is available, shouldn't gears be retractable? Just an academic question... i I couldn't find the answer I am really grateful for super videos... your channel is one of the most underrated youtube channel... super content
There is safety valve which will cut off green hydraulic supply to the landing gear system if aircraft is flying faster than 260kt, hence landing gear unable to EXT OR RET when above the speed . The speed input is from ADR 1 or ADR 3, therefore when ADR 1 + ADR 3 fault or off the safety valve is controlled closed. Hope this help but you need to refer with your instructor also. REF: FCOM 32-10-10 LANDING GEARS AND DOOR OPERATION FCOM PRO ABN NAV ADR 1+3 FAULT
Could you provide clarifications on how to crosscheck which ADR's are faulty? Lets say we start with ADR1, we write down the readings on PFD1? and then ADR2/PDF2 and then ADR3/Stby Instruments or ... how? This part is rather confusing.
Hi Captain, I have a question related IR procedure alignment in att mode. When is the right moment that you use this procedure ? When an IR is failed? Thank you,
@@Captain_SQ so this what I could find Capt, some variants have it for adirs 1 and some for adirs 2. The APU ECB and BLEED AIR pressure indication ALWAYS RELIES on the adirs 1 or 2 STATIC AIR source for DATA reference. The ecb also needs to know the ambient pressure for supplying bleed. This is all I could find