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庞巴迪公务机操作手册 利尔 Bombardier_Learjet-Limitations.pdf25页

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Limitations

SECTION I — LIMITATIONS
TABLE OF CONTENTS General ....................................................................................................... 1-1 Type of Operation .................................................................................. 1-1 Performance Configuration.................................................................. 1-1 Minimum Flight Crew .......................................................................... 1-1 Weight and C.G. Limits ........................................................................... 1-1 Maximum Ramp Weight....................................................................... 1-1 Maximum Certified Takeoff Weight.................................................... 1-1 Minimum Flight Weight ....................................................................... 1-2 Maximum Zero Fuel Weight ................................................................ 1-2 Maximum Allowable Takeoff Weight ................................................. 1-2 Maximum Certified Landing Weight.................................................. 1-2 Maximum Allowable Landing Weight ............................................... 1-2 Center-of-Gravity................................................................................... 1-2 Center-of-Gravity Envelope (Figure 1-1)............................................ 1-3 Airspeed/Mach Limits ............................................................................. 1-4 Airspeed/Mach Limits (Figure 1-2) .................................................... 1-4 Maximum Operating Speed VMO/MMO ............................................ 1-5 Maneuvering Speed VA......................................................................... 1-5 Maximum Landing Gear Operating Speed VLO ............................... 1-5 Maximum Landing Gear Extended Speed VLE ................................. 1-5 Maximum Flap Extended Speed VFE .................................................. 1-5 Minimum Control Speed Air VMCA.................................................... 1-6 Minimum Control Speed Ground VMCG............................................ 1-6 Minimum Control Speed Landing VMCL ........................................... 1-6 Takeoff Decision Speed V1 .................................................................... 1-6 Rotation Speed VR ................................................................................. 1-6 Takeoff Safety Speed V2 ........................................................................ 1-6 Operational Limits/Requirements ........................................................ 1-7 Takeoff ..................................................................................................... 1-7 En Route .................................................................................................. 1-7 Landing ................................................................................................... 1-7 Limit Maneuvering Load Factors ........................................................ 1-8 EICAS or MFD........................................................................................ 1-8 Flaps......................................................................................................... 1-8 Gear.......................................................................................................... 1-8 Maneuvers .............................................................................................. 1-8 Seat Belts and Shoulder Harnesses ..................................................... 1-8 Ambient Temperature Limits (Figure 1-3) ......................................... 1-9 Ground Operating Temperature ......................................................... 1-9 System Limits.......................................................................................... 1-10 Automatic Direction Finder (ADF) .................................................. 1-10 Air Data System .................................................................................. 1-10 FM-126 I-1
FAA Approved 5-19-2004


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