garnuflio 1.0

MAX - Vmo. 316. 320. 0.67.

Mmo. 0.65. 0.62. 0.67.

TURB AIR VG. 207. 227. 217.

MANEUVER. 227. 217. 237.

ZFW. 5850LB. 5800LB. 5900LB.

RAMP. 6900. 6950. 6850.

T/O - LDG. 6900. 6800. 7000.

TORQUE %. 100 (8), 1-10% (9) ground ,101-107 (10) 5seg. 110 (8), 1-10% (9) ground ,101-110 (10) 5seg. 100 (8), 1-20% (9) ground ,101-107 (10) 5seg.

ITT. 830 MAX , 720 MAX, 871-1000 5seg, 821-870 20 seg. 820 MAX , 750 MAX, 871-1000 5seg, 821-870 20 seg. 820 MAX , 750 MAX, 821-1000 5seg, 871-870 20 seg.

N1% (1). 103 MAX, 60-62 GROUND 62 FLIGHT ,104 MAX. 104 MAX , 60-61 GROUND, 67 MIN FLIGHT, 104 MAX. 104 MAX , 60-61 GROUND, 67 FLIGHT, 104 MAX.

NP (4). 100 MAX (2), 46-50 GROUND , 110 (3) 20 seg. 110 MAX (2), 46-55 GROUND , 110 (3) 20 seg. 100 MAX (2), 46-50 GROUND , 107 (3) 20 seg.

OIL PX. 90-120 (6), 90 MIN, 200 MAX , 40-130(5). 90-120 (6), 70 MIN, 200 MAX , 40-130(5). 90-120 (6), 90 MIN, 120 MAX , 40-130(5).

OIL TEMP. 10-105, 40-105 GND 10-105 FLIGHT 106-110 (7), 40 MIN, 106-110 10 MIN. 10-105, -40-105 GND 10-105 FLIGHT 106-110 (7), -40 MIN, 106-110 10 MIN. 10-105, -40-105 GND 10-105 FLIGHT 106-110 (7), -40 MIN, 106-110 05 MIN.

N1 values presented for PMU ...... With PMU ......, ........................... ON/ OFF/ N1 may vary from these values. OFF/ ON / N1 may vary from these values. OFF/ OFF/ N1 may vary from these values.

Permissible at any Operating Condition "Power Setting" for completion of an ....... in-flight emergencies. during operations. normal procedures.

Avoid stabilized ground operation from .............. 62 to 80% NP. 60 to 80% NP. 65 to 80% NP.

Operation in this range permitted only during................. , and .............. for 5 seconds with............. aerobatics or spins/ 15 to 40 psi/ PCL at IDLE. aerobatics or spins/ 2o to 40 psi/ PCL at IDLE. aerobatics or spins/ 15 to 40 psi/ PCL at MAX.

Normal oil pressure during steady state conditions is............ . Operation at oil pressure less than ....... at flight idle or above is indicative of.............. 90 to 120 psi/ 120 psi /oil system malfunction. 90 to 120 psi/ 90 psi /oil system malfunction. 90 to 120 psi/ 120 psi /oil system malfunction.

Acceptable for ground operation at and below .... torque. 20%. 30%. 40%.

The PMU will govern Maximum Torque at ........ Torque above .... at a constant PCL setting and steady state flight is indicative of a governing system malfunction. 100±2%/ 102%. 100±2%/ 106 %. 102±2%/ 102%.

Allowable torque range with NP stabilized and ............ PCL at OFF. PCL at MAX. PCL at IDLE.

With the PMU on, torque between ......... is possible following rapid PCL movement or aerobatic maneuvers. Torque above ........ is a limiting system malfunction. 102-107%/ 107%. 102-107%/ 106%. 100-107%/ 107%.

ACCELERATION LIMITS SYMMETRIC. CLEAN -3.5 TO 7,0 / GEAR FLAPS EXT 0 TO 2,0. CLEAN -3.5 TO 6,0 / GEAR FLAPS EXT 0 TO 2,0. CLEAN -2,0 TO 7,0 / GEAR FLAPS EXT 0 TO 2,0.

ASYMMETRIC. CLEAN -1,0 TO 4,7 / GEAR 0 TO 2,0. CLEAN -3,5 TO 4,7 / GEAR 0 TO 2,0. CLEAN -1,0 TO 4,7 / GEAR 1 TO 2,0.

MIN BATT CONNECT EXT PWR. 22,0 V. 23,5 V. 21,0 V.

MIN BATT START. 24,5 V. 23,5 V. 22,5 V.

GND TEMP. MIN -23°C / MAX 43°C. MIN -23°C / MAX 45 °C. MIN -22°C / MAX 43°C.