Contact Phase Test Flashcards
Is OG approval for a gross weight reduction for takeoff allowed
With squadron supervisor approval, pilots may reduce gross weight by burning down fuel to a predetermined usable fuel weight (2T-38 Vol 3)
(Tinder) Center closed approved
Pull closed into Tinder’s pattern
(Tinder) Center turn crosswind
turn crosswind into Tinder’s pattern
(Tinder) Center maintain runway heading
maintain runway heading climbing to 2,800’ MSL until approved to enter Tinder’s pattern
(Tinder) Center Breakout
fly runway heading to 4,000 then perform a VFR breakout
(Tinder) Abort
Abort the takeoff
(Tinder) Go around
Discontinue approach or landing and initiate procedures to become or remain airborne
(Tinder) Breakout
Leave the traffic pattern, using altitude deconfliction as the primary method
(Tinder) Late Break
Cleared to break as required for spacing behind the last aircraft on inside downwind
(Tinder) Standby
Maintain runway heading until 1 mile past departure end then turn crosswind
(Tinder) Extend
Maintain runway heading at or below 2,300 to dep end and then at or below 2800
What is Bingo fuel
A prebriefed fuel state which allows the aircraft to return to the base of intended landing or alternate, if required, using preplanned recovery parameters and arriving with normal recovery fuel
What is Normal Recovery Fuel
The fuel on initial or at the final approach fix (FAF) at the base of intended landing or alternate, if required. Fuel quantity will be as established locally or 800 pounds, whichever is higher
Altitude restriction to exit first ring MOAs
At or below 14K
Altitude restriction leaving other MOAs
At or below 17K
Min Fuel
600 lbs
Marshaller require
10-24 ft not in parking area, in taxi lane w/o Majcom waiver
<10 ft with Majcom/DO waiver
Wing walker required
Same as Marshaller except <10 ft with waiver
Can you taxi with a gen light on (failed to reset)
No
When does the gear horn sound
Below 96%, 210 kts, 10,000 ft
When can you combine climb and level off checks
Below 18k
Can you taxi with EGI not fully aligned
Yes (standards say have EGI fully aligned “to the max extent possible”, but it’s not required for taxi)
Per the -1, course alignment takes 2 minutes, and the fine alignment occurs between 2 and 4 minutes, so you should at least wait 2 minutes
Min speed for inside DW
220 until configuring
When can you start the final turn
Flaps have tracked at least 60% and no asymmetry exists
Don’t perch when
Straight-in inside 4 NM unless normal spacing can be maintained behind straight-in
Can’t maintain spacing with traffic in front
Don’t break when
Straight-in between 9 and 4 NM
Can’t maintain spacing with traffic in front
What is the break zone
first 3,000 ft
Indication for single TRU failure
PFL
Will XFER RECT illuminate with a single TRU failure
No
Comm out alt gear extension procedure
rear pilot will lower the gear handle and leave it down
How long do you hold the alt gear extension
All 3 gears unlocks according to the -1
How long will the batter last? Assuming what % charged
15 mins
80%
Optimum braking can be done below what speed
100 kts
Can you restart with and Oil malfunction
YES
When can you not pull closed
Between initial and in the break
Someone between 9 and 4 (?)
35 Closed procedure with Civilian departure
Cross centerline of 17 at or above 2300
Acknowledge closed approved with tally traffic
If traffic not insight climb to 2800’ and turn crosswind (maintain below 2300 for departure end restrictions
What happens if you crossfeed and tank runs out
Dual engine flame out with occur
Engagement speed for barriers
MA-1A: 60-150 kts
BAK-15: 0-200
Nose wheel will fail above 120 when heavyweight
Crosswind procedures
No alternate side landings
Do not aerobrake
Touchdown on upwind side
Outside DW straight-in (15L only)
Make request abream prison
If cleared, call 9 NM (fuel) and turn at the grain bins
If approved descent to 2300 and slow to final turn speed
Call 4 NM gear down (no flap, full stop) as normal
Touch and go alts
at or below 2,300 until departure end
single engine go alt
100 (Flaps 60%)
300 (Flaps Full)
Desired touchdown zone
150-1000 ft
SETOS
The computed SETOS is the minimum speed at which the aircraft will take off and be able to fly out of ground effect with a minimum of 100 fpm rate of climb
Instrument cockpit check numbers
1/2: Tac/VOR within .5 or 3: 3% error on TAC/VOR distance 4: degrees of BP error 5: EHSI difference from know heading 6 7: altimeters read wihin 75 ft 8: degrees between Mag and EHSI 9
Reduce bank does what to stall speed and AoA
decreases AoA and stall speed
Min TP stall RPM
80% (FL200)
Min MOA maneuvering speed
150 kts
What do you add gust factor to
final/final approach and touchdown speed
Do you disconnect from main oxygen when using emergency O2
Yes
IF one flap motor fails will the flaps still extend
Yes because they are connected by a rotary shaft
Engine start time limits
12 seconds
Motor for 2 mins
No higher than 360 at EGT rise (may initially be higher but must deecrease below 360 before light off)
Utility Hydraulic system
F: flight controls A: augmenter (stability) N: nose wheel steering G: landing gear S: speed brake
Single engine best climb speed
60% flaps and gear up = 200 kts
220 with flaps up and gear down
Flight time limit with hydraulic gauge reading zero
35 mins
Abort criteria for AB
if AB does not light within 5 seconds or not within limits
Dont cross feed when?
B: boost pump failure I: Fuel indicator failure L: low level L: Leak L: low fuel
