1Check each INU and GPS is in the ___ mode, evaluate the nav accuracy, check GPS keys status, and position service selected
NAV
2The airplane must remain stationary during the first ____ minutes after IRCM power up
2 minutes
3IRCM CIU must display ____ indicating successful completion of warm-up/cool down SBIT, prior to selecting OPR or OPR/F
STBY V
4When setting the parking brake, check ____
BRAKES light is on and for proper brake pressure
5Should an APU shutdown during or immediately after an engine is started ____
Do not attempt to restart until MX checks the APU accessory drive shaft
6If all engines are required to be shutdown prior to takeoff accomplish ____
After Landing check before the Engine Shutdown check
7Do not pushback with the MLG ___
Castered
8If any MLG is more than ___ degress from another; do not taxi the aircraft
4*
9If using the MLG Bogie Positioning switches, do not exceed ____ degrees
15
10If hydraulic system #____ is lost, alternate caster procedures should be avoided or kept to a minimum because ____
#1; the gear may not remain centered
11Asymmetric thrust is 20,000 lbs pf thrust or approx ____ %N1
70
12Asymmetric braking is defined as ______
brake application on one side while the braked wheels are still rolling at speeds up to 5 knots
13Aysmmetric brake application that prevents the braked wheels from rolling (i.e. pivot turn) ____
is not authorized
14When attempting to start a turn from stationary position and the aft MLG initialy centered, avoid nose gear steering angles greater than 45* at the start of a turn
15Wet surfaces may add ___ feet to turn radius
6
16What do you look for / check on "Flight Instruments" checklist step?
1. copilot checks mag compass
2. slip indicator (ball is free in tube)
3. all heading indicators read correctly
4. compass repeaters are aligned and rotating
5. ALTITUDE MISCOMPARE / AIRSPEED MISCOMPARE / ATTITUDE MISCOMPARE / HEADING MISCOMPARE CWAs are removed
6. check for reasonable groundspeed indications (erroneous values may indicate an issue with the INU)
17EGIs and MIRS sensed true headins must be within ___ degrees of each other
2 degrees - check this through the NAV SENSOR INDEX page
18Copilot's, Pilot's altimeters and SAI must be within ___ ft of each other and +/- ___ ft of the known elevation
70;75
19Trim - "Checked and set" - what is the expanded step
co pilot shall make sure the aileron and rudder trim are properly set
the stablizer trim shall be checked for proper operation and then set for takeoff using the pitch trim switches
20A rolling takeoff shall be made:
1. tailwind componenet exceeds 10 knots
2. crosswinds exceed 25 knots below 6,000' (10 knots above 6,000')
3. if the airplane begins to creep at while at higher takeoff power settings
21A static takeoff shall be made:
1. when obstacle clearance or critical field length is a limiting factor
2. an RSC is present
22Engine range for initial power push on rollong or static takeoffs
45-70% N1
23The EECs will / will not prevent engine overtemperature on takeoff
will not
24There is a delay of ___ seconds when transitioning from from nosewheel steering to rudder pedal steering
3 seconds
25(Not modified by TCTO 1C-5M-545) EGPWS provides windshear alerts during takeoff between ____ and ____ feet AGL
10 to 1,500 feet AGL
26Windshear recovery procedures (takeoff continued)
1. Increase power to MTO
2. gain as much speed prior to rotating using the remaining runway as possible
3. initially use 10* pitch then 15-18* pitch remaining below shaker onset
4. if stick shaker is encountered make small nose down pitch adjustments
5. when a safe altitude is reached, maintain positive rate of climb, retract gearm accelerate to Vmco+10 knots
6. flaps may be retracted when flap retsract airspeed and altitude are reached and the airplane is clear of windshear
27After takeoff the thrust reverser interlock is not activated until after ______ or ______
after the MLG wheels spin down OR radar altimeters are above 8 feet
28On takeoff autopilot may be engaged above ___ ft AGL
200 ft
29After flap retraction do not exceed _____ degrees of bank until accelerating to a minimum of 15 knots above Vmfr
10 degrees
30AFCS bank limiter only limits bank during turns using ____
HDG SEL
31With landing gear lever down do not place the landing gear lever UP if:
1. any MLG indicates in transit
2. a bogie pitch CWA is displayed or intermittent
32If all MLG remain in a green wheels condition, the most probable cause is
a failure of th eanti-rotation system -- allow 2 minutes for wheen spin-down
33If one AFT MLG fails to retract and remains in a green wheels position, do this ____ before in-flight toruble shooting
Landing gr - DN
Caster switch - caster, center
Landing gr - UP
34A complete crew briefing (for landing) shall be made prior to ______
each full stop and the first of each series of touch and go landings
35After placing the gear lever down, prior to calling "down and aligned" check for____
1. green wheels
2. light in the handle is extinguished
3. check the MLG position indicators for alignment
36Before takeoff checklist - caster control "center" what does the copilot look for?
1. MLG FREE lights are off
2. MLG is aligned to 0 degrees
37If the EMERG SW ON light (center console) is illumated ____ extend the gear
Do not extend
38If on an GPS approach what alerts apply if you are NOT in GPS only
UNABLE RNP
39If on a GPS approach and operating in GPS-only mode what alerts apply
UNABLE RAIM or RAIM ALERT
40What will be displayed if you are flying a GPS-Only GPS approach
NO APPR
41What is the configuration / min airspeed for the downwind portion of the circling manuever?
Flaps 40 // Vapp +20
42Tolerances for continuing a CAT II approach past 100' above DH to DH are _______ +/- 5 knots, +/- 1/2 dot glideslope AND localalizer
+/- 5 knots, +/- 1/2 dot glideslope AND localalizer
43Can you two engine taxi on SCTS missions?
No
44Engine shutdown may be accomplished 1 minute after landing if_____ or _____
Final approach EGT less than 650*C or thrust reverse less than 750*C
45When changing the brake switch to EMER check for
EMERG HYD light to illuminate and proper brake pressure
46After engine shutdown and parking brake is set, the copilot will monitor selected brake pressure until the applicable ATM is started or chocks are installed -- why?
parking brake accumulator pressure could rapidly deplete if the No.4 system is not pressurized.
47Emergency Generator - "Checked" (P,E) --- what are you checking?
1. EMER PWR ON light comes on
2. observe FAIL indications on the pilot PFD are removed from view