Normal Procedures Flashcards
If the Aircraft will not accept external power and the ground power unit checks good, _______ may actuate necessary relays to allow the aircraft to accept external AC power. (TO 1T-38C-1TO: 2-2)
Cycling the battery switch OFF then ON
Upon initial inspection of the nose gear tire, you see one cord on the nose tire sidewall. Is this acceptable?
No, 0 cords may be visible on the nose tire sidewall. (TO 1T-38C-1TO: 2-7)
Upon initial inspection of the hydraulic fluid indicator, you see that the fluid is above the upper line. Is this acceptable? (TO 1T-38C-1TO: 2-9)
Yes, fluid level above the upper line is acceptable for flight.
tire px check is good for
6 hours
Do not operate the seat adjust switch for more than _____ minute(s) during any 8-minute period.
1 minute. (TO 1T-38C-1TO: 2-13)
If battery voltage is less than ____ VDC, the EED display powers up at full brightness regardless of switch position and reverts to selected brightness when the first generator comes on line. (TO 1T-38C-1TO: 2-16)
22 VDC
During engine start, if EGT does not begin to rise within 12 seconds after the first indication of fuel flow, _______. (TO 1T-38C-1TO: 2-18)
Abort the start, maintain airflow on the engine for 2 minutes
If unsafe gear indication occur after engine start (Stall Warning, Break-X, loss of AoA Symbol), what action should be taken? (TO 1T-38C-1TO: 2-18)
- Do not touch the gear lever
- Shut down the engines as soon as possible
- Have the gear pins installed
Sufficient cooling airflow for the pitot static system is generated at _____ knots. (TO 1T-38C-1TO: 2-18)
25 knots
During the TAKE OFF TRIM test, ensure at least _____ of stick travel before repositioning the trim.
½ inch. (TO 1T-38C-1TO: 2-19)
The flap system should indicate 60% +/- _____% during the Before Taxi Checklist. (TO 1T-38C-1TO: 2-19)
+/- 5%
Nosewheel tires are severely damaged when maximum rudder deflection turns are attempted at ground speeds in excess of ______ knots. (TO 1T-38C-1TO: 2-27)
10 knots
To prevent possible damage to the canopy downlock mechanism, what canopy configurations should be used to the max extent practical? (TO 1T-38C-1TO: 2-27)
Both canopies open or both canopies closed
Allow a minimum of ___ minutes before takeoff behind a large type aircraft or helicopter, and ____ minutes behind a heavy type aircraft. (TO 1T-38C-1TO: 2-29)
2 minutes, 4 minutes
A crosswind component of over ___ knots may reduce the interval time for wake turbulence.
5 knots. (TO 1T-38C-1TO: 2-29)
The takeoff should be aborted if either afterburner fails to light within ___ seconds or if the light off is abnormal. (TO 1T-38C-1TO: 2-29)
5 seconds
Wheel braking is limited to cautious braking from _____ to _____ KCAS, with optimum braking below ______ KCAS. (TO 1T-38C-1TO: 2-32)
130 to 100 KCAS, 100 KCAS
Variation in landing technique could increase landing distance as much as _____% from that computed from the landing distance chart. (TO 1T-38C-1TO: 2-32)
50%
If a tire skid(s) is detected, what immediate action should be taken? (TO 1T-38C-1TO: 2-32)
Immediately release both brakes and cautiously re-apply
How do you accomplish a Minimum Roll Landing? (TO 1T-38C-1TO: 2-32)
- Flying 10 knots below final approach speed (Green Speed)
- Attempt to land with a 12o NH attitude
- Just prior to loss of elevator authority, lower the nosewheel and apply optimum braking
- For wet runways, firm touchdown will reduce effects of hydroplaning
Fuel required for a Closed Pattern is approx. _____ pounds. (TO 1T-38C-1TO: 2-33)
150 pounds
Define Optimum Braking. (TO 1T-38C-1TO: 2-34)
A single, smooth application, increasing as airspeed decreases.
When executing a go-around, can runway contact be made if conditions do not permit an aerial go-around? (TO 1T-38C-1TO: 2-35)
Yes. Do not try to hold the aircraft off the runway if conditions do not permit an aerial go-around. If touchdown is made, lower the nose slightly to accelerate and establish the takeoff attitude.
Before engine shutdown, operate the engines at ____% or below for 1 minute to allow for engine cooling.
70%. (TO 1T-38C-1TO: 2-36)
For an Instrument Climb, power settings between ____ and ____ % RPM will provide comfortable climb rates at 300 KCAS for intermediate level-offs. (TO 1T-38C-1TO: 2-38)
90-95% RPM
If conditions require a MAX thrust climb, maintain 2o to 5o climb until reaching recommended climb Mach, then rotate to approx. _____ to _____ o nose high climb. (TO 1T-38C-1TO: 2-38)
20-25o NH
Hold at airspeeds between ____ and ____ KCAS. (TO 1T-38C-1TO: 2-38)
250-265 KCAS
A Radar Approach requires approx. ___ pounds of fuel. (TO 1T-38C-1TO: 2-40)
325 pounds
Crossfeeding is recommended when fuel differences exceed ____ pounds. (TO 1T-38C-1TO: 2-42)
200 pounds
Crossfeed is not recommended under what conditions? (TO 1T-38C-1TO: 2-43)
- Fuel Quantity failure
- Fuel Leak
- Low Altitude (BEO)
- Low Fuel (BEO)
Under low fuel conditions, how should fuel balance be managed? (TO 1T-38C-1TO: 2-42)
Differential power settings
The FULL line on the Oil Dipstick equates to ____ pints of oil. (TO 1T-38C-1TO: 2-45)
8 pints
Each ADD line on the Oil Dipstick is equivalent to ____ pint of oil consumption. (TO 1T-38C-1TO: 2-45)
1 pint
For a standard instrument ride (1.2 hours), ensure no greater than ____ of a pint have been depleted from the oil system. (TO 1T-38C-1TO: 2-45)
¾ of a pint
The oil system levels should be checked with ___ minutes of engine shutdown. (TO 1T-38C-1TO: 2-45)
15 minutes
The tire pressure of the main wheel tire is ____ PSI while the nose wheel is ____ PSI.
265 psi, 75 psi
