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Limitation FM 132 I 1 FAA Approved 9-24-2004 Change 2 General ....................................................................................................... 1-1 Type of Operation .................................................................................. 1-1 Performance Configuration.................................................................. 1-1 Minimum Flight Crew .......................................................................... 1-1 Weight and C.G. Limits ........................................................................... 1-2 Maximum Ramp Weight....................................................................... 1-2 Maximum Certified Takeoff Weight.................................................... 1-2 Minimum Flight Weight ....................................................................... 1-2 Maximum Zero Fuel Weight ................................................................ 1-2 Maximum Allowable Takeoff Weight ................................................. 1-2 Maximum Certified Landing Weight...............................................1-2A Maximum Allowable Landing Weight ............................................1-2A Center-of-Gravity................................................................................1-2A Center-of-Gravity Envelope (Figure 1-1)............................................ 1-3 Airspeed/Mach Limits ............................................................................. 1-5 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........................................................ 1-7 EICAS or MFD........................................................................................ 1-7 Flaps......................................................................................................... 1-7 Gear.......................................................................................................... 1-8 Maneuvers .............................................................................................. 1-8 Seat Belts and Shoulder Harnesses ..................................................... 1-8 Ambient Temperature Limits (Figure 1-3) ......................................... 1-8 Ground Operating Temperature ......................................................... 1-9 System Limits............................................................................................ 1-9 Air Data System ..................................................................................... 1-9 Attitude Heading Reference System (AHRS).................................... 1-9 Autopilot/Flight Director..................................................................... 1-9 SECTION I — LIMITATIONS TABLE OF CONTENTS Limitation I 2 FM 132 FAA Approved 9-24-2004 Change 1 TABLE OF CONTENTS (Cont) System Limits (Cont) Pressurization....................................................................................... 1-10 Environmental Control System......................................................... 1-10 Primus 1000 Integrated Avionics System......................................... 1-10 Engine Synchronizer ........................................................................... 1-10 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：BOMBARDIER_Learjet_0-Limitations1
