T-6 Flashcards
Minimum weather for flying aerobatics and extended trail levels I, II, III
Clear of clouds with 3 NM in-flight visibility
Maximum oil pressure during start is _____
200
Oil temperatures up to ______ deg C are acceptable for ground operations at and below 20% torque
110
In a low altitude approach, a maximum _______ descent is normally planned.
400 feet per nautical mile
For a clean aircraft, asymmetric (rolling G’s) acceleration limits are:
+4.7 to -1.0
At honcho or wizard, you should offset (within a local TS7 pattern) when overtaking:
A. Takeoff traffic
B. A low approach
C. Touch and go traffic
D. All of the above
All of the above
G-suits are required on all sorties when planning to exceed 2 G’s during any portion of a sortie.
True
When flying a windshear-precautions approach, set takeoff flaps and fly approach up to _____ knots faster than normal.
10
Pattern checks are not authorized when the observation is reported below:
1000’ AGL/3 mile vis
Practice slow flight using the Flaps UP configuration and _______ knots
90-95
If the flaps are set to any position other than UP, the speed brake will:
A. Remain extended if already extended
B. Retract is already extended
C. Remain retracted if the pilot attempts to extend it after the flaps are extended
D. B & C
B and C
B. Retract is already extended
C. Remain retracted if the pilot attempts to extend it after the flaps are extended
The propeller system is designed to maintain a constant speed of ____ rpm (100% Np) during most flight controls
2000
The pitch trim actuator moves:
The pitch trim tab on the right side of the elevator
If the standby attitude gyro off flag appears after the battery bus has failed, the indicator will continue to operate for at least for ____ minutes.
9
Operating maneuvering speed (Vo) is the speed above which full or abrupt control movements in one axis can result in structural damage to the aircraft. Vo is ____ KIAS.
227
T/F: anti-ice heat is provided to both the pitot tube and the static ports.
False
The wheel brake system _____ affected by a failure of the aircraft hydraulic system
Is not
When established within a local RSU pattern, do not breakout:
A. When the status is restricted patterns
B. At night
C. Inside the final turn
E. Both a & c
D. All of the above
Both a & c
Essential steps of items which are to be checked in both cockpits, if occupied, are indicated by _____ following the step
(BOTH)
The remain within distance of a procedure turn is measured from ______ unless the IAP specifies otherwise:
The procedure turn fix
Terminal CDI scaling during a GPS approach is ____ nm; approach sensitivity (within 2NM of the FAWP) is ___ NM.
1, .3
_________ provides indication of takeoff trim setting
A green band on each trim indicator
Pilots shall perform the missed approach when the missed approach point, decision height (DH), or decision altitude (DA) is reached and any of the following conditions exist:
A. Runway environment is not in sight
B. Unable to make a safe landing
C. Directed to execute missed approach by the controlling agency
D. All of the above
D. All of the above
As AOA approaches stall angle (approximately ____ units on the gage), the AOA computer activates the ______, (15-16 units) providing stall warning
A. Spoilers
B. Speed brake
C. Pitch limiter
D. Stick shaker
Stick shaker
The LDG flag setting should be used for full stop landings when the heavy weight flaps up land distance is greater than or equal to ______ of the actual field length
A. 0.25
B. 0.75
C. 0.8
D. 1
0.8
If a RAIM flag/status annunciation appears after the FAWP
Climb to the missed approach altitude, proceed to the MWAO and execute a missed approach
Flap position is controlled by a three-position flap selector marked:
UP, TO, LDG
When computing required fuel reserves, turbine-powered aircraft use fuel consumption rates that provide:
Maximum endurance at 10,000 MSL
T/F: the PCLs are interconnected with a push-pull rod so that movement of one PCL moves the other
TRUE
By filling a flight plan, the PIC certifies
A. The flight was properly ordered, authorized, and released IAW AFI 11-401
B. Current NOTAMs, weather and other relevant information were obtained
C. Responsibility for the safety of the aircraft, the formation, and it’s occupants
D. The flight plan has been reviewed for completeness and accuracy
E. All of the above
E. All of the above
The speed brake _______ be stopped at an intermediate deflection
May not
