N563TM Limitations Flashcards
Maximum Ramp Wt.
16,500
Maximum Design Takeoff Wt.
16,300
Maximum Takeoff Wt. limited by…
…the most restrictive of the following requirements.
- Max Certified Takeoff Weight
- Max Wt. Permitted by Climb Requirements
- Takeoff Field Length (TOFL)
Maximum Design Landing Wt.
15,200
Maximum Landing Wt. limited by…
…the most restrictive of the following requirements:
- Max Certified Landing Weight
- Max Wt. Permitted by Climb Requirements
- Landing Distance
Maximum Design Zero Fuel Wt.
12,200
Center of Gravity Limits
Refer to Figure 2-1
Engine Type
Pratt and Whitney Canada, Inc
JT15D-5A
2900lb Thrust
Max Takeoff ITT
700 (5 min) (10 min OEI)
Max Continuous ITT
680
Max Flight Idle ITT
580
Max Ground Idle ITT
580
Max Starting ITT
700 - 2 sec
Refer to Figure 2-3
Max Transient ITT
700
Max Takeoff N2
96.0%
Max Continuous N2
96.0%
Min Flight Idle N2
52% (Min)
Min Ground Idle N2
46% (Min)
Max Takeoff N1
104%
Limited by Takeoff Fan Charts-Section IV
Max Continuous N1
104%
Limited by Clim Fan Charts-Section IV
Max Transient N1
106%
Normal Oil Pressure
60-83psi (above 52% N2)
Min Flight Idle Oil Pressure
40(MIN)
Min Ground Idle Oil Pressure
40(MIN)
