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
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：BOMBARDIER_Learjet_0-Limitations1