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and failure of control box circuits. Also, the lights will be illuminated
any time the gear is down and locked, power is on the aircraft, and the
ANTI-SKID switch is OFF
PM-121
3-15
Change 3
Pilot's Manual
Learjet 31A
ANTI-SKID SWITCH
The ANTI-SKID switch is located on the center switch panel and has
two positions: On (ANTI-SKID) andOFF. When the switch is in the On
(ANTI-SKID) position, 28 VDC is applied to the anti-skid system control
circuits. Normally, the switch remains in the On (ANTI-SKID) position
for all operations .
3-16
PM-121
Change 3
Learjet 31A AFM Limitations
FM-121 I-1
FAA Approved 7-25-91
Change 14
SECTION I — LIMITATIONS
TABLE OF CONTENTS
General
Certification Status .................................................................................... 1-1
Type of Operation ..................................................................................... 1-1
Performance Configuration ..................................................................... 1-1
Minimum Flight Crew.............................................................................. 1-1
Weight and C.G. Limits
Maximum Ramp Weight.......................................................................... 1-2
Maximum Certified Takeoff Weight ...................................................... 1-2
Maximum Zero Fuel Weight ................................................................... 1-2
Maximum Allowable Takeoff Weight.................................................... 1-2
Maximum Certified Landing Weight..................................................... 1-3
Maximum Allowable Landing Weight .................................................. 1-3
Center-of-Gravity ...................................................................................... 1-3
Center-of-Gravity Envelope
Standard 15,500 Lb Takeoff Weight (Figure1-1)............................... 1-4
Optional 16,500 Lb Takeoff Weight (Figure 1-2) .......................... 1-4A
Optional 17,000 Lb Takeoff Weight (Figure 1-2A) ........................... 1-5
Airspeed/Mach Limits
Airspeed/Mach Limits (Figure 1-3)........................................................ 1-6
Airspeed/Mach Limits ............................................................................. 1-7
Maximum Operating Speed VMO/MMO ............................................... 1-7
Maneuvering Speed VA............................................................................ 1-7
Maximum Landing Gear Operating Speed VLO................................... 1-8
Maximum Landing Gear Extended Speed VLE .................................... 1-8
Maximum Flap Extended Speed VFE ..................................................... 1-8
Minimum Control Speed, Air VMCA...................................................... 1-8
Minimum Control Speed, Ground VMCG.............................................. 1-9
Critical Engine Failure Speed V1............................................................. 1-9
Rotation Speed VR..................................................................................... 1-9
Takeoff Safety Speed V2 ........................................................................... 1-9
Operational Limits/Requirements
Takeoff ...................................................................................................... 1-10
Enroute...................................................................................................... 1-10
Landing..................................................................................................... 1-10
Limitations Learjet 31A AFM
I-2 FM-121
FAA Approved 7-25-91
Change 28
TABLE OF CONTENTS (Cont)
Flight Load Acceleration Limits ........................................................... 1-11
Demonstrated Crosswind...................................................................... 1-11
Maneuvers................................................................................................ 1-11
Seat Belts and Shoulder Harnesses....................................................... 1-11
Ambient Temperature Limits (Figure 1-4) .......................................... 1-12
System Limits
Air Data System ...................................................................................... 1-13
Attitude Heading Reference System.................................................... 1-13
Autopilot/Flight Director...................................................................... 1-13
Cabin Pressurization .............................................................................. 1-13
Electronic Flight Instrument System (EFIS) ........................................ 1-14
　
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