LIMITATIONS Flashcards
MAX RAMP WEIGHT
12,590 LBS
MAX TAKEOFF
12,500 LBS
LANDING WEIGHT
12,500 LBS
ZERO FUEL WEIGHT
11,000 LBS
MAX BAGGAGE WEIGHT
370 LBS-550 LBS DEPENDENT ON SERIAL/ AND SEAT CONFIG
AIRSPEEDS
VMO-259
MMO-.52M
VMCA-86
VSO/VS1- DETERMINED BY PERFORMANCE CHARTS
VX-100
VXSE-115
VY-125
VYSE-121
VENR-121
VSSE-104
VA- 181
VFE APP-200
VFE FULL- 157
VLE-181
VLO EXT- 181
VLO RETRACT- 163
MAX DEMONSTRATED CROSSWIND
25 KTS
BALKED LANDING CLIMB
100 KTS
TURBULENT AIR PENETRATION
170 KTS
L FUEL PRESS/R FUEL PRESS
Corresponding red fuel pressure annunciator light, is limited to 10 hours before overhaul or replacement of the engine driven fuel pump.
MAX FUEL IMBALANCE
1,000 LBS (DO NOT TAKEOFF, if fuel quantity gages indicate yellow arc or less than 265 lbs of fuel in each main tank.
CROSSFEEDING
SINGLE ENGINE OPS ONLY
MAX USABLE FUEL
544 GALS/3,645 LBS
MAIN FUEL SYSTEM CAPACITY
386 GAL/2,586 LBS
AUX FUEL CAPACITY
158 GAL/1,059 LBS
MAX OPERATING ALTITUDE
35,000 FT
MAX OCCUPENCY LIMIT
PART 91: 15 INCLUDING CREW
PART 135: 9 PAX PLUS CREW
ICE VANE USAGE
EXTEND IN AMBIENT TEMPS OF +5C OR BELOW WHEN FLIGHT FREE OF VISIBLE MOISTURE CANNOT BE ASSURED.
RETRACTED FOR OPERATIONS IN AMBIENT TEMPS OF +15C OR ABOVE.
LANDING GEAR CYCLE LIMITS
1 UP/1 DOWN LIMITED TO ONE EVERY 5 MINS, FOR TOTAL OF 6 CYCLES FOLLOWED BY 15 MIN COOL DOWN.
STARTER TIME LIMITS
40 SEC ON/60 SEC OFF
40 SEC ON/60 SEC OFF
40 SEC ON/ 30 MINS OFF
PROP DIAMETER
HARTZELL: 98.5 IN
MCCAULEY: 98.0 IN
PROP SPEED LIMITS
TRANSIENT: 2200 RPM
REVERSE: 1900 RPM
ALL OTHER CONDITIONS: 2000 RPM
GENERATOR LIMITS
MAX SUSTAINED GEN LOAD:
IN FLIGHT:
SEA LEVEL-31,000 FT ALT: 1.00
ABOVE 31,000 FT ALT: .88
GROUND OPERATION: .85
MAX PRESSURE DIFF/CABIBN DIFF
6.6 PSI
