BAGGAGE COMPARTMENT CAPACITY:
Maximum w/o fuel extension tanks -
With fuel extension tanks -
Floor Loading -
MAXIMUM CERTIFICATED WEIGHTS: ZFW - Landing - Takeoff - Ramp -
FUEL TANK CAPACITY:
W/O extension tanks -
With extension tanks -
Maximum lateral fuel unbalance -
MAXIMUM N1 and N2:
Transient -
Overspeed -
Prior to Shutdown -
MAXIMUM ITT: Starting - Takeoff - Takeoff with APR activated - Continuous - Climb (recommended) Cruise (recommended)
OIL PRESSURE (AT NORMAL OPERATING TEMP): Start - Idle - Takeoff, Climb, Cruise - Transient -
OIL TEMPERATURE:
Up to 30,000 ft -
Above 30,000 ft -
Transient -
START TIMES: Light-off (from initial fuel flow) - From light-off to idle - Starter-assist air starts (from initial FF to 60% N2 - Windmilling air start -
APU LIMITS: Maximum altitude for operation - Maximum altitude for start - Not approved for \_\_\_\_\_\_\_ operations How much time must be allowed between shut-down and the next start - Do not operated APU if -
MAXIMUM NORMAL OPERATION SPEEDS (VMO/MMO):
Autopilot Engaged or Mach Trim operative -
Autopilot Disengaged and Mach Trim inoperative -
- Below 23,900 - 353 KIAS, Above .816 M
MANEUVERING SPEEDS (Va) 24,650 - 22,000 - 20,000 - 18,000 - 16,000 - 14,000 -
MAXIMUM SPEEDS Slats - Flaps 12 - Flaps 20 - Flaps 40 - Landing Gear - ALTN Extension - Tire Speed - Vmca /Vmcg -
PROHIBITED MANEUVERS AND OPERATIONS
Prohibited Maneuvers -
Do not takeoff -
Do not extend SLATS, FLAPS or LANDING GEAR -
MAXIMUM APPROVED OPERATING ALTITUDES: Enroute - Autopilot and Y/D inoperative - Cabin Door light or defect - Takeoff and Landing -
OPERATING PERFORMANCE LIMITATIONS (Takeoff and Landing): Ambient Temperature (On Ground) - Runway Slope - Tailwind Component - Demonstrated Crosswind Component -
THRUST REVERSER LIMITS: Maximum N1 for Reverse Thrust - Do not exceed Idle Deploy position - Do not Deploy T/R for more than - Thrust Reverser ARM switch must be OFF -
HYDRAULIC SYSTEM LIMITATIONS:
Preferred Fluid -
ENVIRONMENTAL CONTROL SYSTEM LIMITATIONS:
Max Cabin Differential Pressure -
ANTI-ICE SYSTEM LIMITATIONS:
Ground -
InFlight (Engine Anti-Ice) -
InFlight (De-Ice Systems) -
ELECTRICAL SYSTEM LIMITATIONS: Engine Generator Load - Clearing Engine - Minimum Battery Voltage - Aircraft with NO APU - DO NOT Takeoff if -
LONGITUDINAL TRIM SYSTEM LIMITS:
Takeoff is PROHIBITED -
With either NORMAL, OVRRD or EMER trim systems inoperative
AUTOPILOT ENGAGEMENT OPERATIONS:
On Takeoff -
On Landing -
During Flight -