Limits

Question 1

TORQUE % – TAKEOFF/MAX

Answer 1

100 (8)

8. The PMU will govern maximum torque at 100 +/- 2 %. Torque above 102 % at a constant PCL setting and steady flight is indicative of a governing system malfunction.

Question 2

ITT °C MAX – TAKEOFF/MAX

Answer 2

820 MAX

Question 3

N1 % – TAKEOFF/MAX

Answer 3

104 MAX

Question 4

Np % – TAKEOFF/MAX

Answer 4

100 MAX (2)

2. With PMU OFF, permissible maximum NP is 100 +/- 2 %.

Question 5

OIL PRESSURE psi – TAKEOFF/MAX

Answer 5

90 to 120 (6)

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

Question 6

OIL TEMP °C – TAKEOFF/MAX

Answer 6

10 to 105

Question 7

TORQUE % – IDLE

Answer 7

1 to 10 % (9)
(ground)

9. Allowable torque range with Np stabilized and PCL at IDLE.

Question 8

ITT °C MAX – IDLE

Answer 8

750 MAX

Question 9

N1 % – IDLE

Answer 9

60 to 61 (ground)
67 Min (flight)

Question 10

Np % – IDLE

Answer 10

46 to 50
(ground)

Question 11

OIL PRESSURE psi – IDLE

Answer 11

90 Min

Question 12

OIL TEMP °C – IDLE

Answer 12

-40 to 105 (Grnd)
10 to 105 (Flt)
106 to 110 (7)

7. Acceptable for ground operation at and below 20% torque.

Question 13

ITT °C MAX – START

Answer 13

871-1000
(5 sec)

Question 14

OIL PRESSURE psi – START

Answer 14

200 Max

Question 15

OIL TEMP °C – START

Answer 15

-40 Min

Question 16

TORQUE % – TRANSIENT

Answer 16

101 to 107
(5 sec)(10)

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

Question 17

ITT °C MAX – TRANSIENT

Answer 17

821-870
(20 sec)

Question 18

N1 % – TRANSIENT

Answer 18

104 MAX

Question 19

Np % – TRANSIENT

Answer 19

110 (20 sec) (3)

3. Permissible at any operating condition “power setting” for completion of an in-flight emergency.

Question 20

OIL PRESSURE psi – TRANSIENT

Answer 20

40 to 130 (5)

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

Question 21

OIL TEMP °C – TRANSIENT

Answer 21

106 to 110
(10 minutes)

Question 22

2. With PMU OFF, permissible maximum NP is ___ +/- ___ %.

Answer 22

2. With PMU OFF, permissible maximum NP is 100 +/- 2 %.

Question 23

4. Avoid stabilized ground operation from __ to __ % NP.

Answer 23

4. Avoid stabilized ground operation from 62 to 80 % NP.

Question 24

5. Operation in this range permitted only during aerobatics or spins, and ___ to ___ psi for ___ seconds with PCL at IDLE.

Answer 24

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

Question 25

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

Answer 25

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

Question 26

7. Acceptable for ground operation at and below ___ torque.

Answer 26

7. Acceptable for ground operation at and below 20% torque.

Question 27

8. The PMU will govern maximum torque at ___ +/- ___ %. Torque above ___ % at a constant PCL setting and steady flight is indicative of a governing system malfunction.

Answer 27

8. The PMU will govern maximum torque at 100 +/- 2 %. Torque above 102 % at a constant PCL setting and steady flight is indicative of a governing system malfunction.

Question 28

10. With the PMU on, torque between ___ to ___ % is possible following rapid PCL movement or aerobatic maneuvers. Torque above ___ % is a limiting system malfunction.

Answer 28

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

Question 29

MAXIMUM AIRSPEED GEAR DOWN (V LE) & FLAP DOWN (V FE)

Answer 29

150 KIAS

Question 30

MAX OPERATING (V MO)

Answer 30

316 KIAS

Question 31

MAX MACH (M MO)

Answer 31

0.67 MACH

Question 32

TURBULENT AIR PENETRATION SPEED

Answer 32

MAXIMUM: 207 KIAS

RECCOMENDED: 180 KIAS

Question 33

STARTER CYCLE LIMITATIONS

STARTER DUTY CYCLE IS LIMITED TO FOUR ____ CYCLES
COOLING PERIOD AFTER FIRST STARTER CYCLE ____
COOLING PERIOD AFTER SECOND STARTER CYCLE ____
COOLING PERIOD AFTER THIRD STARTER CYCLE ____
COOLING PERIOD AFTER FOURTH STARTER CYCLE ____

Answer 33

STARTER DUTY CYCLE IS LIMITED TO FOUR 20 SEC CYCLES
COOLING PERIOD AFTER FIRST STARTER CYCLE 30 SEC
COOLING PERIOD AFTER SECOND STARTER CYCLE 2MIN
COOLING PERIOD AFTER THIRD STARTER CYCLE 5 MIN
COOLING PERIOD AFTER FOURTH STARTER CYCLE 30 MIN

Question 34

FLIGHT MANEUVERING LIMITATIONS

INVERTED FLIGHT

Answer 34

60 sec

Question 35

FLIGHT MANEUVERING LIMITATIONS

INTENTIONAL ZERO G FLIGHT

Answer 35

5 sec

Question 36

FLIGHT MANEUVERING LIMITATIONS

NEGATIVE G OPERATIONS

Answer 36

60 sec

Question 37

FLIGHT MANEUVERING LIMITATIONS

DO NOT EXCEED -2.5 G FOR LONGER THAN

Answer 37

30 sec

Question 38

FLIGHT MANEUVERING LIMITATIONS

MIN. POS. Gs UPRIGHT BEFORE ADDITIONAL NEG Gs

Answer 38

60 sec

Question 39

ACCELERATION LIMITATIONS

SYMMETRIC CLEAN

Answer 39

+7.0 TO -3.5 Gs

Question 40

ACCELERATION LIMITATIONS

SYMMETRIC GEAR & FLAPS EXTENDED

Answer 40

+2.5 TO 0.0 Gs

Question 41

ACCELERATION LIMITATIONS

ASYMMETRIC CLEAN

Answer 41

+4.7 TO -1.0 Gs

Question 42

ACCELERATION LIMITATIONS

ASYMMETRIC GEAR & FLAPS EXTENDED

Answer 42

+2.0 TO 0.0 Gs

Question 43

ACCELERATION LIMITATIONS

UNCOORDINATED ROLLING MANEUVERS INITIATED AT ____ G SHALL BE LIMITED TO A ____ DEGREE BANK ANGLE CHANGE

Answer 43

UNCOORDINATED ROLLING MANEUVERS INITIATED AT -1 G SHALL BE LIMITED TO A 180 DEGREE BANK ANGLE CHANGE

Question 44

OTHER LIMITATIONS

MIN VOLTAGE FOR BATTERY START

Answer 44

23.5 VOLTS

Question 45

OTHER LIMITATIONS

MAX CROSSWIND FOR DRY RUNWAY

Answer 45

25 KNOTS

Question 46

OTHER LIMITATIONS

MAX CROSSWIND FOR WET RUNWAY

Answer 46

10 KNOTS

Question 47

OTHER LIMITATIONS

MAX CROSSWIND FOR ICY RUNWAY

Answer 47

5 KNOTS

Question 48

OTHER LIMITATIONS

MAX TAILWIND COMPONENT FOR TAKEOFF

Answer 48

10 KNOTS

Question 49

OTHER LIMITATIONS

MAXIMUM FUEL FLOW

Answer 49

799 PPH OR LESS

Question 50

PROHIBITED MANEUVERS

Answer 50

1. INVERTED STALLS
2. INVERTED SPINS
3. SPINS WITH PCL ABOVE IDLE
4. SPINS WITH THE LANDING GEAR, FLAPS, OR SPEED BRAKE EXTENDED
5. SPINS WITH PMU OFF
6. AGGRAVATED SPINS PAST TWO TURNS
7. SPINS BELOW 10,000 FEET PRESSURE ALTITUDE
8. SPINS ABOVE 22,000 FEET PRESSURE ALTITUDE
9. ABRUPT CROSS-CONTROLLED (SNAP) MANEUEVERS
10. AEROBATIC MANEUVERS, SPINS, OR STALLS WITH A FUEL IMBALANCE GREATER THAN 50 POUNDS BETWEEN WINGS
11. TAIL SLIDES

Question 51

THE AIRCRAFT HAS BEEN APPROVED ONLY FOR TRANSIT THROUGH ____ FEET OF ____________ ICE.

Answer 51

THE AIRCRAFT HAS BEEN APPROVED ONLY FOR TRANSIT THROUGH 5000 FEET OF LIGHT RIME ICE.

Question 52

MINIMUM BATTERY VOLTAGE:

Answer 52

22.0 VOLTS

Question 53

HYDRAULIC CAUTION:

Answer 53

< 1800 PSI, > 3500 PSI

Question 54

FUEL CAUTION LIGHT:

Answer 54

< 110 POUNDS IN RESPECTIVE WING TANK

Question 55

COCKPIT PRESSURIZATION SCHEDULE LIMIT:

Answer 55

3.6 +/- 0.2 PSI