max. ramp weight
3150 lbs
max. takeoff weight
max. landing weight
max. zero fuel weight
no structural limit
Max. Weight in Baggage Compartment
130 lbs
Stop and Go’s
Solo
Not Allowed
Dual
Touch and Go’s
Allowed
Short field obstacle (dual only)
Soft field (dual only)
Maximum crosswind component including gusts
20 knots
12 knots
Maximum tailwind component
10 knots
6 knots
Enroute Operational Limits
Minimum Safe Altitude
Airwork
3000’ AGL
1500' AGL
Stalls
Unusual Attitudes, Spiral Dive, High Performance Maneuvers, Upset Prevention and Recovery Training
Not allowed
Enroute
See LAT DE VFR Flight Planning Handbook
Night Traffic Patterns
Published TPA
Ground Reference Maneuvers
1000’ AGL
Weather Limits
VFR Company Weather Minima
Condition
Ceiling
Visibility
Flight Instructor Training/Flight Instructor Flights
As per FAR's
Student Pilot Training
As per FAR’s
Solo Student Pilots TP
Night Traffic pattern
Cross country
1500’ AGL
1000’ above MSA
3 Statute Miles
5 Statute Miles
FAR: Federal Aviation Regulations
IFR Company Weather Minima
Destination Minimums
DESTINATION MINIMUMS
Precision Approach
DA (H)
Student Pilot training
Visual Meteorological Conditions
As published
.75 Statute Mile
Flight Instructor training/Flight Instructor flights
Non-Precision Approach
MDA (H)
.90 Statute Mile
Circle To Land
2.0 Statute Miles
Alternate Minimums
ALTERNATE MINIMUMS
Approach Available
Minima
Ceiling / Visibility
CAT1/PAR
Published non-precision DA (H) and RVR
650’/2 s.m.
Non-precision
Published non-precision MDA (H) plus 200’ and RVR plus 3280’.
850’/2 s.m.
Circling
Published circling MDA (H) and visibility
Maximum Operating Altitude
Type of Flight
Maximum Altitude
Time
12,000' MSL
30 minutes
10,500' MSL
None
Flight Maneuvering Load Acceleration Limits (3150lbs)
Flaps 0%
+ 3.8 G
- 1.9 G
Flaps 50% & 100%
+ 1.9 G
- 0 G
Prohibited Maneuvers
• Flight into known icing conditions.
• Spins, including spin entry.
• Aerobatic maneuvers (bank angle more than 60° and/or pitch attitude more than 30°).
•Maximum Slip duration is 30 seconds.
Airspeed Tape Markings
Marking
KCAS Value or Range
KIAS Value or Range
Significance
White Range Strip
57-104
62-110
Full flap operating range.
Green Range Strip
67-166
71-164
Normal operating range.
Yellow Range Strip
166-204
164-201
Operate with caution, only in smooth air.
Red Range Strip
204
201
Maximum speed for all operations
Never exceed - Vne
201 KIAS
Do not exceed this speed in any operation.
Maximum structural cruising - Vno or Vc
164 KIAS
Do not exceed this speed except in smooth air and then only with caution.
Operating Maneuvering - VO (3150 lbs)
133 KIAS
Do not make full or abrupt control movements above this speed.
Maximum flap extension/extended - VFE
Approach flaps 50% (16°)
* LAT US policy for flaps 50% (16°)
Full down 100% (32°)
VFE 50%: 150 IAS
*LAT policy for 50%: 130 IAS
100%: 110 IAS
Do not extend flaps or operate with flaps extended above this speed.
* LAT US policy to reduce maintenance due to the high volume of flap operations.
Maximum Demonstrated Parachute Deployment Speed - VPD
Do not exceed this speed. This is the maximum speed at which parachute deployment has been demonstrated.
Vx
81 KIAS
Vy
96 KIAS
Best glide
100 KIAS (3150lbs)
92 KIAS (2600lbs)
Initial Climb Speed
96 KIAS (500’ to 1000’ AGL)
*less than Vy should be short duration
LAT US Cruise Climb
110 KIAS (1000’ AGL and above)
Center of Gravity Limits
• Forward Limits
139.1 inches aft of datum to 2700 pounds with straight line variation to 140.7 inches at 3050 pounds.
• Aft Limits
148.1 inches aft of datum at all weights.
Reference Datum
• Datum is 100 inches forward of center line through forward of firewall
Rate of Descent Limits
The maximum rate of descent below 1000’ AGL is 1000’/minute.
System Limitations
Instrument Markings
Maximum and minimum limits
red barber pole
Caution area
yellow range strip
Normal area
green range strip
Alternator/Battery Limitations
System - 28 volt (ALT 1),
28.75 volt (ALT 2)
Alternator – ALT 1; 100-amp Gear-Driven,
ALT 2; 70-amp, Belt-Driven
Caution: Continued operation with the alternators switched off will reduce battery power enough to open the battery relay, remove power from the alternator field, and prevent alternator restart.
Battery - 24 volt, 10-amp (BAT 1),
two 12 volt in series (=24V), 7-amp (BAT 2)
External Power Receptacle* - standard AN-type plug
Note: A negative ground external power source is required. 28VDC
*receptacle = Stecker
Emergency Equipment
First Aid Kit - 3.5 lbs. (located rear baggage compartment)
Survival Kit - 9.5 lbs. (located in rear baggage compartment)
Fuel System
To select RIGHT or LEFT, turn fuel pump to ON then rotate the selector to the desired position. To select OFF, first RAISE the fuel selector knob release and then rotate the knob to OFF.
Warning: SOLO STUDENT SHALL NOT CHANGE THE FUEL SELECTOR IN THE TRAFFIC PATTERN! If required, during DUAL flights only,CM1 may change the fuel selector when the aircraft is on downwind .
Fuel Flow
Maximum
20.0 GPH
Minimum
1.5 GPH
Operating range
6.9 to 18.0 GPH
Max Allowable Fuel Quantity
Total capacity
58.6 US gallons
Usable fuel
56.0 gallons
Visual measuring tab
26 gallons usable fuel (13 gallons per fuel tank)
Fuel Loading
LAT US aircraft are filled to the top of approximately 58.6 gallons total fuel (56 gallons usable). Special fuel requirements may be requested to stay within maximum weight limits.
Warning: When the fuel tanks are 1/4 full or less, prolonged uncoordinated flight such as slips or skids can uncover the fuel tank outlets. Therefore, if operating with one fuel tank dry or if operating on LEFT or RIGHT tank when 1/4 full or less, do not allow the airplane to remain in uncoordinated flight for periods in excess of 30 seconds.
Fuel Usage
To avoid excessive maintenance on the aileron trim system, maintain fuel balance within approximately a 1/4 tank differential (7.5 US gallon).
Type of Fuel
Preferred grade
100LL (blue color)
Optional grade
100/130 (green color)
Landing Gear
The main landing gears are bolted to composite wing structure between the wing spar and shear web. The landing gear struts are constructed of composite material for fatigue resistance. Each main gear wheel is equipped with an independent, hydraulically operated single cylinder, dual piston, disc brake.
Engine
• Lycoming engine, model IO-390 C3B6,
• with 215 HP @ 2700 RPM. The engine has
• 4 cylinders horizontally opposed and is
• fuel injected and air cooled
Ignition/Starter
Caution: Limit cranking to intervals of 10 sec. with a 30sec. cooling period between cranks.
Tachometer (RPM) / Manifold Pressure (MAP)
RPM
2700
500 to 2700
MAP
29.5 in Hg
15 to 29.5 in Hg
Note: Due to the mechanical design of the propeller governor, it is normal for the engine to temporarily exceed 2700 RPM during some phases of flight. If necessary, a slight reduction in throttle setting will decrease the RPM to keep the engine operating at or below 2700 RPM.
Cylinder Head Temperature
Note: Maximum Caution Range 435 ̊F to 465 ̊F.
Maximum 465° F
Oil
Pressure (psi)
Temperature (°F)
Quantity (quarts)
115
235
7
25
100 (takeoff)
6
55 to 95
100 to 235
Normal range
6 to 7
Caution: Oil Pressure Caution when oil pressure is between 25 and 54 psi and RPM is greater than 1000.
Oil Pressure Warning when oil pressure is below 25 psi, OR oil pressure is above 115 psi.
Taxi RPM
1000 RPM
Power settings slightly above 1000 RPM are permissible to start motion, on soft surfaces and on inclines.
Last changeda year ago
