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Rudderpedal centeringand artificialfeelis providedby aprimaryfeelunit,located on the copilots rudderpedalpivot assembly. A secondaryfeelunit,locatedin theaftfuselage, ensures thatthe rudder remains centeredin theeventof acontroldisconnect. Inthe eventof acontroljam, thepilotsand copilot’s pedals willremain operable through anti-jammechanisms, however additionalpedalforce willbe requiredto obtain rudder deflection. Two rudderloadlimiter assemblies, installedin the vertical stabilizer, give overload(stress) protection tothe ruddercontrolsystemmechanical components. A rudderloadlimiter, installedin thePCUinput assembly, allows continued controlinput movementtothe remainingPCU’s if onePCUbecomes jammed. Flight Crew Operating Manual MASTER CSP A- 013 Vol. 1 11--30--2 Flight Crew Operating Manual MASTER CSP A- FLIGHT CONTROLS Vol. 1 11--30--3 Rudder REV 56, Jan 31/03 The ruddertrim is electricallyoperatedand manually controlled usingthe trim selector on the centerpedestal. Operatingthetrim selector totheNL/NR(nose left/nose right) repositions therudder control cables tomove therudder. Hydraulic pressure from atleast oneofthe hydraulic system is requiredto move the rudder. Actuation ofthe ruddertrimwillnot cause rudderpedaldeflection.
NL- NR -
Flight Crew Operating Manual MASTER
Rudder REV 56, Jan 31/03 中国公务机网 www.gongwuji.com 公务机翻译 www.aviation.cn 本文链接地址：庞巴迪CRJ200公务机机组操作手册 Bombardier CRJ-飞行操纵(7) |
