MQF Flashcards
Fire extinguishing capability is reduced above____ KIAS due to the airflow through the engine compartment at higher airspeeds. Airspeed should be reduced to ____KIAS or below before discharging the fire extinguishers.
100, 100
When extending the cable, use small weight bags of ____ lbs. If no wieghts are available extend the cable at no more than ____ speed.
5-20, 1/4
…It is for this reason that ____broken wires are allowed for the hoist cable.
No
IF A QUESTION IS TRUE OR FALSE WHICH IS IT?
It’s true.
Checklists in the TO CL-2 Gunner/Hoist ____ be verbalized.____notify the crew up on initiation and completion of a TO CL 2 checklist.
Do not need to, only
The MTR HOT light will reset once the motor has cooled sufficiently, approximately____ minutes, depending on…
30
The CABLE FEET reading on the rescue hoist pendant is for reference only. Accuracy is +-_____ft .
5
The hoist contains _____ usable ft of cable an dhas a fuillotine-type cable cutter…
250’
The hoist capacity of 600lbs and speed is variable from —– fpm when raising a load (4th cable layer) using…
0-345
…fuel quantity indicator may take up to —-to stabilize at the actual fuel quantity. Indicated fuel quantity may lag actual fuel quantity by as much as —– lbs. Fuel dumping will stop when the switch is placed in the OFF position, or automatically when either the left or right tank reaches the actual stand pipe that prevents fuel dump below — lbs per tank.
60 seconds, 600, 250
The stabilator manual slew switch should be —- until limit switch stops stabilator movement.
Bumped
If the helicopter is shut down and/or hydraulic power is removed with one tail rotor cable failure, disconnection of the other tail rotor cable —- occur when force from the boost servo cannot react against control cable quadrant spring tension. The quadrant spring —- displace the cable and boost servo piston enough to unlatch the quadrant cable.
Will, Will
With the UES II prior to starting engines, ensure main rotor blades are aligned with the aircraft centerling +- ____ degrees before engaging the rotor brake.
20
Regarding TGT the 2.5 minute limit (contingency power) range is
879-903
Regarding TGT the 10 minute limit range is
846-879
During takeoff, the stabilator has not begun trailing edge up movement by —– KIAS and manual control is not available, do not exceed the variable VNE arc on the PFD or longitudinal control may be lost.
30-50
Fuel dumping…This can leave one fuel tank with 250 lbs and the other with up to —-lbs.
1450
The term —-is used to report a complete failure of the weapon to fire.
Misfire
—-refers to a weapon not rendering a dangerous condition.
Safe
No further attemp to clear the weapons will be made after intiating the —-. Do not attempt to remove the affected weapon in flight.
Join Up Checklist
The yaw boost servo is still pressurized and the mechanical control system is still intact allowing limited tail rotor control. Because of the limited yaw control range available, —– is required.
A roll on landing 40 KIAS or above
During fuel dumping a fuel venting condition is extremely hazardous when the helicopter is on the ground or in a hover since —- produced by the helicopter could ignite vapor and spilled fuel.
Static electricity
If NR decreases from 100-96% with an increase in Q during steady flight with no engine malfunction the ____ may have failed.
Main transmission planetary carrier
The STAB DEGRADED advisory indicates that the stabilator control has reverted to a condition of reduced functionality in either speed or control. Full stabilator range of motion ______ available.
May not be
Loss of DC power will result in the engine anti-ice and engine inlet anti ice valves failing to the open position. This will reduce power available _______. The respective anti-ice advisory lights will not illuminate.
Up to 20% Q per engine
During electrical system failures, although not specifically listed as checklist steps, it is prudent to check for______.
Popped circuit breakers
If AC electrical power is not available _____ fire bottle (s) can be discharged.
Only the reserve
Opening the cockpit windows before the cabin doors will draw smoke from the cabin into the cockpit. ______ to help prevent smoke generated in the cabin from entering the cockpit.
Point blower vents aft
….if the decision is made to shut down an engine in flight______ while retarding the PCL from FLY to IDLE, monitoring Q, NG, TGT, NP, and ENG OUT warning light on.
Take at least five full seconds
If lighting strike occurs whereby all aircraft electrical power and electronics subsystems and controls are lost (including EDECU and the engine alternator) both engines immediately advance to maximum power with no ________ protection.
Both B and C
NP over speed protection
TGT limiting
After performing an aircraft emergency shutdown, when egressing from an aircraft with munitions and flares in board requires a minimum egress distance of _____ from the aircraft.
600’
Even though not specifically listed as checklist steps, making _______ are prudent actions during critical emergencies if time permits.
Mayday transmissions and setting the transponder to EMER
If APU OIL HOT caution illuminates a _______ cooling period is required before checking oil level.
30 minute
Bank angles shall be limited to _____ when PRI SERVO 1 FAIL or PRI SERVO 2 FAIL caution is illuminated.
30 degrees
While operating in a salt spray environment for any period of time, a TGT ride of ____ or more for constant torque is an indication of engine performance degradation and possible salt encrustation. A TGT ride of greater than ____ for constant torque may result in compressor stall.
20, 40
A ____ kt crosswind or tailwind may increase torque required by up to 4% over 0 wind values.
3-5
The cooling cart should be utilized when OAT is greater than ______ and the avionics system is operating.
39
If icing conditions are encountered, turn on all anti-icing equipment immediately. If torque required increases ____ above that required for level flight…
20%
Prolonged hovering flight in temperatures above ____ at higher gross weight may cause transmission oil temperature to rise into the yellow precautionary range.
35
All anti-ice systems must be turned on prior to entering visible moisture at ambient temperature of _____ or less.
4
When aerial refueling the No 2 tank will fill faster than the No 1 tank. If both fuel tanks are not refueled to the full level, a fuel imbalance of up to _____ is possible
1200 lbs
If AC electrical power is not available, only the _____ compartment or the _____ compartment has fire protection.
Number 1 engine
APU
Upon impact of a crash of _____ G’s or more the omnidirectional inertia switch will automatically fire both extinguishing containers into both engine compartments.
10
If an emergency start must be made without AC electrical power, the ____ engine must be started first because only the ____ engine start control valve can receive power from the battery via DC essential bus.
Number 1
Number 1