![]() O Eliminated TBO of 1200 hours in favor of an on-condition interval. Improved nose wheel steering tiller ergonomics Provide a seat cushion that is wider than that of the previous design. O The new crew seats from Goodrich provide more adjustability (lumbar, seat pan, O This enables cabinetry to be more easily removed and reinstalled in the cabin. O Examples: AFIS, FDR provisions, 2nd HF provisions, TCAS II, EGPWS, CD-820 Inclusion of many former options into the standard airplane Honeywell P2000 Phase 7 IAC software to support max weight and thrust increases O Increased full fuel payload from 1,069 lb to 1,369 lb O Increased maximum takeoff weight from 35,700 to 36,100 lb O Increased maximum ramp weight from 36,000 to 36,400 lb New standby engine instrument to support higher ITT limits 5% increase in takeoff thrust per engine (designated as the 3007C1 engine) System reverts to requiring 68 degrees of input for full aileron travel.ħ50-0173 and on (2002 Block Point Change) If one of the hydraulic systems is inoperative, the This allows for better aileron responsiveness in gusty orĬrosswind landing operations. Subsequent to this change, the ailerons reach full travel at 34 degrees ofĬontrol wheel input. O Prior to this change, the ailerons reached full travel at 68 degrees of control wheel (A cross-tie relayĪllows the RH generator to power the LH buses, and vice-versa, in the event of a ![]() Generator and those that are powered by the RH generator. Isolation and independence between systems that are powered by the LH The split-bus architecture provides for greater O This change was undertaken to comply with European JAA requirements, which A brief synopsis of these modifications follows:
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