T-1 Ops Limits (Boldface)

Front 1

Takeoff, Time Limit

Back 1

5min

Front 2

Takeoff, Miximum Observed ITT

Back 2

700

Front 3

Takeoff, N2%

Back 3

96

Front 4

Takeoff, N1%

Back 4

104

Front 5

Takeoff, Oil Pressure PSI

Back 5

60 to 83

Front 6

Takeoff, Oil Temperature

Back 6

10 to 121

Front 7

Maximum Continuous, Time Limit

Back 7

Continuous

Front 8

Maximum Continuous, Miximum observed ITT

Back 8

680

Front 9

Maximum Continuous, N2

Back 9

96

Front 10

Maximum Continuous, N1

Back 10

104

Front 11

Maximum Continuous, Oil Pressure psi

Back 11

60 to 83

Front 12

Maximum Continuous, Oil Temperature

Back 12

10 to 121

Front 13

Idle, Time limit

Back 13

Continuous

Front 14

Idle, Maximum Observed ITT

Back 14

580

Front 15

Idle, N2

Back 15

52 (min)

Front 16

Idle, Oil Pressure psi

Back 16

40 (min)

Front 17

Idle, Oil Temperature

Back 17

-40 to 121

Front 18

Transient, Maximum Observed ITT

Back 18

720 2sec Max

Front 19

Transient, N2

Back 19

96

Front 20

Transient, N1

Back 20

106

Front 21

Transient, Oil Pressure psi

Back 21

95 for
90 sec

Front 22

Transient, Oil Temperature

Back 22

135 (max)
15min max

Front 23

Starting, Maximum Observed ITT

Back 23

550 - 600 4 sec
600 - 700 2 sec
700 - 720 1 sec

Front 24

NOTES:
(1) Time limit starts when throttle first advanced

Back 24

for take off thrust.

Front 25

NOTES:
(2) Normal flight: Normal oil pressure is ___ to ___ psi at N2 speeds above ___%. Oil pressure below ___ psi is undesirable and should be tolerated only for the safe recovery of the flight, preferably at reduced power setting. Oil pressure below ___ psi is unsafe.

Back 25

60
83
60
60 (undesirable)
40 (unsafe)

Front 26

NOTES:
(3) Under cold starting conditions, oil pressure between ___ psi and ___ psi is limited to ___ seconds.

Back 26

83
95
90

Front 27

NOTES:
(4) The ITT during ground starts should normally not exceed ___ C

Back 27

550

Front 28

Starter/Generator Limitations
Ground - Max for each generator ___ amps

Back 28

280

Front 29

Starter/Generator Limitations
Flight - Both generators operating
Up to 41,000ft ___ amps

Back 29

280

Front 30

Starter/Generator Limitations
Flight - One generator operating
Up to 32,500 ft ___ amps

Back 30

400

Front 31

Starter/Generator Limitations
Flight - One generator operating
32,500ft - 41,000ft ___ amps

Back 31

280

Front 32

Starter/Generator Limitations
Min battery voltage for battery start ___ volts DC

Back 32

22

Front 33

Starter/Generator Limitations
Max generator load prior to starting second engine ___ amps

Back 33

150

Front 34

Starter/Generator Limitations
Motoring of the starter is limited to
1st crank ___ sec then ___ min cooling
2nd crank ___ sec then ___ min cooling
3rd crank ___ sec then ___ min cooling

Back 34

1st crank 30 sec then 5 min cooling
2nd crank 30 sec then 15 min cooling
3rd crank 30 sec then 60 min cooling

Front 35

Airspeed & Mach Limitations
Extend flaps to 10 degrees ___ KIAS

Back 35

200

Front 36

Airspeed & Mach Limitations
Extend flaps >10 degrees ___ KIAS

Back 36

170

Front 37

Airspeed & Mach Limitations
Flaps extended > 10 degrees ___ KIAS

Back 37

165

Front 38

Airspeed & Mach Limitations
Aircraft is limited to ___ KIAS or ___ MACH whichever is less

Back 38

330
.78

Front 39

Airspeed & Mach Limitations
Landing gear/lights ___ KIAS/FL ___

Back 39

200
200

Front 40

Airspeed & Mach Limitations
Wipers ___ KIAS

Back 40

200

Front 41

Airspeed & Mach Limitations
Tire ___ Knots GS

Back 41

165

Front 42

Enroute Limitations
Max Operating Altitude

Back 42

FL410

Front 43

Enroute Limitations
Yaw damper required operable for flight above

Back 43

FL280

Front 44

Enroute Limitations
Do not use autopilot below ___ft AGL

Back 44

200

Front 45

Fuel Limitations
Min/Max Fuel Temperature

Back 45

-40C/50C

Front 46

Fuel Limitations
Emergency Fuel/Minimum Fuel

Back 46

300lbs/500lbs

Front 47

Fuel Limitations
Max Fuel Imbalance - T.O/Touch & Go

Back 47

100lbs

Front 48

Fuel Limitations
Max Fuel Imbalance - Flight

Back 48

300lbs

Front 49

Fuel Limitations
Max Fuel Imbalance - Landing

Back 49

300lbs

Front 50

Fuel Limitations
Fuel crossfeed with 2 engines operating is limited to level flight when less than ___lbs of fuel remains in the wing tank supplying fuel.

Back 50

600

Front 51

Takeoff & Landing Limitations
Max Tailwind

Back 51

10 Knots

Front 52

Takeoff & Landing Limitations
Max Crosswind (Dry)

Back 52

25 Knots

Front 53

Takeoff & Landing Limitations
Max Crosswind (Wet)

Back 53

15 Knots

Front 54

Takeoff & Landing Limitations
Max Crosswind (Icy)

Back 54

10 Knots

Front 55

Weight Limitations
Max Takeoff Weight

Back 55

16,100lbs

Front 56

Weight Limitations
Max Landing Weight

Back 56

15,700

Front 57

Anti-Ice Limitations
Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ___C OAT/SAT

Back 57

10

Front 58

Anti-Ice Limitations
Reduce throttles below ___ N1 prior to turning on engine or wing anti-ice.

Back 58

90

Front 59

Anti-Ice Limitations
Do not operate surface anti-ice systems inflight at ram air temperatures above ___C

Back 59

10

Front 60

Anti-Ice Limitations
To ensure proper wing anti-ice operation, the throttles must be kept at ___% N2 minimum

Back 60

70