Section 2 N/w/c

Front 1

NOTE: Determine the capacity of the external
power unit prior to using the _______. If the external power unit is not
rated at _______, it is not capable
of supporting the large initial electrical load
requirements of the _______.

Back 1

AUX hydraulic
pumps

80 KVA or above

AUX hydraulic pumps

Front 2

CAUTION: To prevent fuselage fire, ______
shall be applied to the aircraft prior to
connecting ________. Electrical power
shall not be disconnected when external
high pressure pneumatics are being supplied
to the aircraft.

Back 2

electrical power

an external high pressure pneumatic air source

Front 3

CAUTION: If there is a total loss of electrical power
during high pressure pneumatic air supply
operation, fuselage fire may result.
Immediately shut down the ______.

Back 3

pneumatic
cart

Front 4

WARNING: Do not use _____ with battery
switch OFF. Fire detection/protection and
radio communication will not be available
during an emergency should the _______ fail

Back 4

external power

external
power source

Front 5

CAUTION: To preclude damage to the ______, the
APU should not be started or operated with
___________. If the
APU must be started with ________, they should be retracted as soon
as possible.

Back 5

slat seals

the slats in the extended position

the slats
extended

Front 6

NOTE: The APU PWR switch can trip off for a
transient fault. Under these conditions, _______ reset(s) should be accomplished.

Back 6

only one

Front 7

CAUTION: If FIREX AGENT DISCHARGE 1 POWER
CB on the overhead panel is open, the _______ switch will be inoperative.

Back 7

APU Fire Agent DISCH

Front 8

CAUTION: Continuing an APU start with a flashing
RPM indicator may result in _______.

Back 8

an APU exhaust fire, damage to the aircraft and injury to personnel

Front 9

WARNING: With the APU running, a right MANIFOLD FAIL annunciation could indicate escape of bleed air inside the air conditioning compartment. Immediately ______ and confirm ______ in order to prevent automatic reopening of the APU pneumatic shutoff valve and cycling of the air conditioning packs. Do not turn this switch back on until cleared by maintenance.

Back 9

press the APU bleed air switch

the flow line is extinguished

Front 10

CAUTION: If the flaps/slats are not retracted during
extended ERO using reverse idle, the
fixed wing leading edge will heat up
faster than normal. One or both engine
_______.

Back 10

FIREX bottles may discharge uncommanded

Front 11

WARNING: Failure to place the IRCM mode control knob in ______ could result in unintended firing of the laser on the ground if the IRCM WOW MAINT ORIDE switch
in the left EPC is subsequently switched to
ORIDE.

Back 11

STBY or OFF

Front 12

CAUTION: Operating engines in idle reverse thrust for
extended periods during high OAT’s may
cause one or more engine ______.

Back 12

FIREX bottles to
discharge uncommanded

Front 13

NOTE: Use of thrust reversers during engine running
offload may cause lower than normal
EPR rating to be provided by the EEC’s.
This may result in the MC calculating a
maximum takeoff gross weight much
_____ than actual aircraft capability

Back 13

lower

Front 14

NOTE: To preclude overly restrictive MC TOLD calculations, place the throttles in IDLE for a minimum of ______
before engaging TOGA.

Back 14

3 minutes

Front 15

WARNING: Do not attempt to take off if the _____ is
open. A manifold duct failure would cause extensive
damage.

Back 15

ISOL valve

Front 16

CAUTION: Abrupt use of ___ or other maneuvers that
extend the nose gear strut to the limit with the
tiller turned will damage the centering cams.

Back 16

brakes

Front 17

When backing the aircraft, the aircraft gross weight
effectively increases because of thrust reverser downloads.
This increase can be as much as ______ lbs.
CAUTION: If the effective gross weight exceeds the weight
bearing capacity of an airfield surface, damage to
the surface may result

Back 17

89,000

Front 18

WARNING: Do not stand on the main landing gear
(MLG) components or apply force to the
MLG components. The MLG may collapse
causing injury/death and/or aircraft damage.

Back 18

True

Front 19

NOTE: Before entering NAV/DNAV mode, IRU
INOP 1,2 and IRU INOP 3,4 will assert on
the WAP unless ______.
If ________ are set, an IRU INOP X message indicates an actual IRU
failure.

Back 19

both parking brakes are set

both parking brakes

Front 20

CAUTION: If STORED HEADING ALN message is
displayed on the MCD, accept the stored
heading alignment only _________. Otherwise, realign the
IRU’s. Refer to TO 1C-17A-1-2, Section II.

Back 20

if intentionally performed
per procedures described in
TO 1C-17A-1-2

Front 21

NOTE: If the preflight inspection is being accomplished
to cock the aircraft for alert purposes,
(do/do not?) select NAV mode.

Back 21

do not

Front 22

CAUTION: Do not hold aileron trim knob hardover for
more than ___ seconds. Motor may overheat
and fail.

Back 22

24

Front 23

CAUTION: Do not change the ENGINE IGNITION
source during engine start. Switching
sources may result in a tailpipe fire.

Back 23

True

Front 24

CAUTION: Do not change or adjust the _____ during a start. Do not use more
than ___ type(s) of air supply source (APU,
crossbleed, or external air) simultaneously
for a start. Do not select _____ on or off during a start. Resulting
unstable bleed air supply may cause damage
to the starter

Back 24

bleed air supply source

one

air conditioning packs

Front 25

WARNING: Do not attempt to take off if the ISOL
valve is open. A ____
would cause extensive damage.

Back 25

manifold duct failure

Front 26

CAUTION: Ground operations longer than ___ minutes
with OAT above _____ may result
in IRCM TX x FAIL and degraded IRCM
performance.

Back 26

25 minutes

38 °C/100 °F

Front 27

CAUTION: Pressing the Transfer Pump switchlight
while _______ is illuminated
will shut down AUX pumps controlled
from the cargo compartment panels. Coordinate
with the LM before selecting
AUTO.

Back 27

LM HYD CONTROL

Front 28

NOTE: (Checking flt controls in mech) A rudder shudder lasting no more than
__ seconds is considered acceptable. A
rudder shudder sustained for 10 seconds
should be stopped within 10 more seconds
by moving the ______ on the
FCS ACTR panel from _____.

Back 28

10

YAW switch

MECH to EFCS

Front 29

NOTE: (checking the flt cont in mech) The roll control stick may have a stiff
feel within the last one inch of left wing
down stick deflection that is not felt in
the right wing down direction.

Back 29

True

Front 30

CAUTION: TOGA mode engagement checks the validity
and ability of various aircraft systems
to support flight in EFCS. If takeoff is
made with TOGA being unable to display
the ____, the EFCS could revert to _____ and damage to the rudder/
vertical stabilizer may result.

Back 30

F/D

FROZEN
GAINS

Front 31

NOTE: To preclude overly restrictive MC
TOLD calculations, place the throttles in
FWD IDLE for a minimum of ___ minutes
before engaging TOGA.

Back 31

3 minutes

Front 32

WARNING: If an RSC value from ___ or greater and
RCR less than ___ are reported, actual runway
required for takeoff/landing could
exceed runway available. Adjust TOLD
IAW TO 1C-17A-1-1 and TO 1C-17A-

Back 32

> 0.1 RSC

< 12 RCR

Front 33

NOTE: To reduce susceptibility to engine surge while
maneuvering in reverse, select all engine bleed
valves ___ and air conditioning packs ___. Further
protection from engine surge may be achieved by
selecting engine cowl anti-ice on for the period of
time reverse thrust must be used above idle

Back 33

open

on

Front 34

CAUTION: (while backing) Abrupt use of brakes should be avoided to prevent
_________.

Back 34

the aircraft from setting on its tail

Front 35

WARNING: Do not attempt takeoff with any hydraulic
reservoir temperature indicating less than
_____. Low rudder temperature indicates
insufficient rate of rudder deflection to correct
for an engine failure on takeoff.

Back 35

7 °C

Front 36

does this work?

Back 36

yes

Front 37

CAUTION: High speed operations through standing water
deeper than ___ inch may damage the landing gear
doors, pod access doors, stabilizer strut doors and
underbelly.

Back 37

1/2 inch

Front 38

NOTE: If ∗SEND is not displayed, reset the transmit
inhibit condition on the NAV EMITTER
CONTROL page by cycling _____ from ACTIVE to STANDBY, then back to
ACTIVE.

Back 38

AERO−I

Front 39

NOTE: If the external power cart is rated at less than
___ KVA and the APU generator is not used, do not
operate any AUX pump. Starting an AUX pump
could overload the external power cart and cause
reversion to battery power.

Back 39

80

Front 40

NOTE: The purge valve should be in the _____ position except during preflight
and when oxygen is in use where smoke or
fumes are not present and goggles are not
required.

Back 40

OPEN
(pulled out)

Front 41

WARNING: If a GPWS/TAWS aural or visual warning is received during an approach in
Instrument Meteorological Conditions (IMC), ________. Exceptions will be annotated in command guidance.

Back 41

execute a missed approach or
go-around

Front 42

NOTE: CMBT LTG Visible landing lights will not
be available when the MODE SELECT
switch is in ______. If the visible landing
lights appear inoperable during a non-
NVG approach/landing, ensure the MODE
SELECT switch is in NORM.

Back 42

MIX or IR

Front 43

CAUTION: Maximum full flap landing weight is ______

Back 43

502,100
lb.

Front 44

CAUTION: (Assault Landing) If the sink rate reduction is delayed below ___
feet AGL, the aircraft may land short.

Back 44

40' AGL

Front 45

WARNING: On landing deceleration, if ALS flashes on the
PFD, hold _____ stick until airspeed is
below ____ KCAS.

Back 45

full forward

50 KCAS

Front 46

CAUTION: Do not reverse any engine that displays an
______ message on the WAP.
Severe engine stall may develop

Back 46

ENG STABILITY X

Front 47

NOTE: If AGS does not deploy on landing, DLC
spoilers are available to manually deploy ____
of AGS effectiveness.

Back 47

25%

Front 48

WARNING: (touch and go) Rotate at ___________,
whichever occurs first.

Back 48

VMCO or 1,000 feet remaining

Front 49

WARNING: If the spoilers fail to automatically
retract, the PF ________ and the PM ________
to retract and disarm the spoilers

Back 49

PF will advance the throttles
to MAX

PM will manually set
the Spoilers switch to the vertical position

Front 50

NOTE: (engine shutdown) Operate the engines at ____ EPR or less
for __ minutes before shutdown to reduce
wear, heat soakback, and oil system
coking.

Back 50

1.05 EPR

3 minutes

Front 51

NOTE: (engine shutdown) If APU is inoperative, ensure either a
________ is in place or
_________ before shutting down
the last engine.

Back 51

fire guard/fire extinguisher

air cart connected

Front 52

NOTE: The APU PWR switch can trip off for a transient
fault. Under these conditions, ______ reset(s)
should be accomplished.

Back 52

only one