Boldface & Ops Limits

Question 1

ENGINE SHUTDOWN PROCEDURE

Answer 1

1. CONDITION LEVER “FEATHER” (CP)
2. FIRE HANDLE “PULLED” (CP)
3. AGENT “DISCHARGED” (FOR FIRE OR NACELLE OVERHEAT) (CP)

Question 2

AUXILIARY POWER UNIT EMERGENCY SHUTDOWN (GROUND/IN-FLIGHT)

Answer 2

1. FIRE HANDLE “PULLED” (E)
2. AGENT “DISCHARGED” (FOR FIRE) (E)

Question 3

MULTIPLE ENGINE POWER LOSS/STALL/FLAMEOUT

Answer 3

1. TEMPERATURE DATUM CONTROL VALVE SWITCHES “NULL” (E)

Question 4

FUSELAGE FIRE/SMOKE AND FUME ELIMINATION

Answer 4

1. OXYGEN “ON, 100%” (ALL)

Question 5

RAPID DECOMPRESSION

Answer 5

1. OXYGEN “ON, 100%” (ALL)

Question 6

ENGINE SHUTDOWN CONDITIONS

Answer 6

a. Engine fire
b. Turbine overheat
c. START VALVE OPEN light illuminates
d. Nacelle overheat
e. Uncontrollable power
f. Certain propeller malfunctions
g. Uncontrollable rise in TIT
h. Uncontrollable drop in oil pressure
i. Uncontrollable rise in oil temperature
j. Unusual vibration or roughness
k. Throttle control cable failure
l. Excessive visible fluid leak

Question 7

POWER SOURCES FOR INSTRUMENTS

Answer 7

Torque Gage AC I&EFC
RPM Gage Self Generating
TIT Gage AC I&EFC
Fuel Flow AC I&EFC
Oil Temperature ESS DC
Oil Pressure AC I&EFC
Oil Quantity ESS DC
Oil Cooler Flaps ESS DC
Fuel Gage AC I&EFC
Hydraulic Gage AC I&EFC
Fire Detection System ESS DC
Fire Protection System BATT

Question 8

OPS LIMITS - STARTING ITT
Max Normal Start

Answer 8

200*C

Question 9

OPS LIMITS - STARTING ITT
Max Enrichment Start

Answer 9

100*C

Question 10

OPS LIMITS - STARTING ITT
781 Write Up

Answer 10

830-850*C

Question 11

OPS LIMITS - STARTING ITT
Stop Start (1 Restart)/781

Answer 11

850C - 965C

Question 12

OPS LIMITS - STARTING ITT
Overtemp Inspection/781

Answer 12

Exceeds 965*C

Question 13

OPS LIMITS - STARTING ITT
Temp Controlling Check

Answer 13

720-750*C

Question 14

Maintenance Action

Answer 14

<720*C

Question 15

BLEED AIR SYSTEM
14th Stage Temperature

Answer 15

600 degrees Fahrenheit

Question 16

BLEED AIR SYSTEM
14th Stage Pressure

Answer 16

125 PSI

Question 17

BLEED AIR SYSTEM
Minimum Engine Output

Answer 17

70 PSI

Question 18

BLEED AIR SYSTEM
Minimum APU Output

Answer 18

35 PSI

Question 19

BLEED AIR CHECKS
Engine (65 - 35 PSI)

Answer 19

16 Seconds

Question 20

BLEED AIR CHECKS
APU (30 - 15 PSI)

Answer 20

16 Seconds

Question 21

PRESSURIZATION
Cabin Differential

Answer 21

15.16 in Hg

Question 22

PRESSURIZATION
Safety Valve

Answer 22

-0.76 to 15.9 in Hg

Question 23

PRESSURIZATION
Press Controller

Answer 23

-1.2 to 15.8 in Hg

Question 24

PRESSURIZATION
Manual Control Hot to Cold

Answer 24

4 Minutes

Question 25

CRACKED WINDOW
Flight Station (1/2 Panes)

Answer 25

10 in Hg

Question 26

CRACKED WINDOW
Cargo Compartment (1 Pane)

Answer 26

10 in Hg

Question 27

CRACKED WINDOW
Cargo Compartment (2 Pane)

Answer 27

0 in Hg

Question 28

ANTI-ICING
Propeller / Spinner

Answer 28

65 to 90 Amps

Question 29

ANTI-ICING
Cycle

Answer 29

15 seconds On 45 seconds

Question 30

ANTI-ICING
Max Ground Cycles

Answer 30

2

Question 31

ANTI-ICING
Number of Ice Probes

Answer 31

2

Question 32

LEADING EDGE
Normal Range

Answer 32

75 degrees Fahrenheit to 200 degrees Fahrenheit

Question 33

LEADING EDGE
Overheat Light

Answer 33

200 degrees Fahrenheit

Question 34

LEADING EDGE
Maximum Ground Time

Answer 34

30 Seconds

Question 35

NESA
Max OAT

Answer 35

27 degrees Celcius (81 degrees Fahrenheit)

Question 36

NESA
Cold Start

Answer 36

-43 degrees Celcius (-45 degrees Fahrenheit)

Question 37

NESA
Operating Cycle

Answer 37

5 Sec on 10 Sec off

Question 38

OXYGEN SYSTEM
Lox Quantity

Answer 38

25 Liters

Question 39

OXYGEN SYSTEM
Lox Low Light

Answer 39

2.5 Liters

Question 40

SYSTEM PRESSURE
No Flow

Answer 40

270 - 455 PSI

Question 41

SYSTEM PRESSURE
Continuous

Answer 41

270 - 340 PSI