Learjet 36A - Section I: Limitations; Weight and Center of Gravity Limits; Airspeed and Mach Limits

FAA APPROVED 4-30-76 I-1
REISSUED 2-25-81, CHANGE 10
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
Maneuvers ...............................................................................1-1
Weight and C.G. Limits
Maximum Ramp Weight............................................................1-2
Maximum Certified Takeoff Weight.............................................1-3
Maximum Zero Wing and Tip Fuel Weight ..................................1-3
Maximum Allowable Takeoff Weight...........................................1-4
Maximum Certified Landing Weight............................................1-4
Maximum Allowable Landing Weight..........................................1-5
Center-of-Gravity Envelope........................................................1-5
Aircraft Certified for 17,000 Pounds Takeoff Weight.............1-6
(Figure 1-1) ........................................................................1-6
Aircraft Certified for 18,000 Pounds Takeoff Weight.............1-7
(Figure 1-2) ........................................................................1-7
Aircraft Certified for 18,300 Pounds Takeoff Weight.............1-8
(Figure 1-3) ........................................................................1-8
Airspeed/Mach Limits
Maximum Operating Speed V
MO/MMO ......................................1-9
Maneuvering Speed V
A .............................................................1-9
Maximum Landing Gear Operating Speed V
LO ...........................1-9
Airspeed/Mach Limits (Figure 1-4) ...........................................1-10
Maximum Landing Gear Extended Speed V
LE ...........................1-11
Maximum Flap Extended Speed V
FE.........................................1-11
Minimum Control Speed Air V
MCA...........................................1-11
Minimum Control Speed Ground V
MCG ....................................1-11
Critical Engine Failure Speed V
1 ..............................................1-11
Rotation Speed V
R .................................................................1-12
Takeoff Safety Speed V
2 .........................................................1-12
Ambient Temperature Limits (Figure 1-4A).............................1-12
CHANGE
FAA APPROVED 4-30-76 I-1
REISSUED 2-25-81, CHANGE 10
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
Maneuvers ...............................................................................1-1
Weight and C.G. Limits
Maximum Ramp Weight............................................................1-2
Maximum Certified Takeoff Weight.............................................1-3
Maximum Zero Wing and Tip Fuel Weight ..................................1-3
Maximum Allowable Takeoff Weight...........................................1-4
Maximum Certified Landing Weight............................................1-4
Maximum Allowable Landing Weight..........................................1-5
Center-of-Gravity Envelope........................................................1-5
Aircraft Certified for 17,000 Pounds Takeoff Weight.............1-6
(Figure 1-1) ........................................................................1-6
Aircraft Certified for 18,000 Pounds Takeoff Weight.............1-7
(Figure 1-2) ........................................................................1-7
Aircraft Certified for 18,300 Pounds Takeoff Weight.............1-8
(Figure 1-3) ........................................................................1-8
Airspeed/Mach Limits
Maximum Operating Speed V
MO/MMO ......................................1-9
Maneuvering Speed V
A .............................................................1-9
Maximum Landing Gear Operating Speed V
LO ...........................1-9
Airspeed/Mach Limits (Figure 1-4) ...........................................1-10
Maximum Landing Gear Extended Speed V
LE ...........................1-11
Maximum Flap Extended Speed V
FE.........................................1-11
Minimum Control Speed Air V
MCA...........................................1-11
Minimum Control Speed Ground V
MCG ....................................1-11
Critical Engine Failure Speed V
1 ..............................................1-11
Rotation Speed V
R .................................................................1-12
Takeoff Safety Speed V
2 .........................................................1-12
Ambient Temperature Limits (Figure 1-4A).............................1-12
CHANGE