Term
| Center of gravity problems affecting longitudinal stability during flight should be considered prior to ________. (Ref: T.O. 1T-1A-1) |
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Definition
| personnel movement within the cabin area |
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Term
What is true with an engine shutdown due to a failed turbine rotor shaft? (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| A loud bang will be audible and engine restart is not possible. |
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Term
If the engine will not start with the ignition switch in STBY, the manual mode should be used. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
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Term
If either electronic fuel control fails, the synchronization system is still operative. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
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Term
A popped fuel system circuit breaker ___________________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
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Term
Operating transfer pumps dry ____________________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
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Term
In the event of an engine fire, following fire extinguisher bottle actuation, jet pump switches should be placed in the off position to _________________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| stop fuel flow to the engine |
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Term
During preflight inspection, a drop of fuel hanging on the sniffle valve ______. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
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Term
During crossfeed operation, the boost pump in the nonselected fuel feed chamber willnot activate if the boost pump switch is in AUTO and the fuel feed line pressure drops below 5 psi. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
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Term
In the event of a fuel quantity indicator failure, which of the following are true? (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| Both gauges' dial pointers move off scale to below the zero mark to indicate an inoperative condition |
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Term
In the event of electrical system failure, excluding the aircraft battery, placing the battery switch to the EMER position causes the battery to power the _________________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| emergency bus, standby battery and standby bus |
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Term
What provides ground fault protection for external power? (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| Battery protection circuits |
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Term
Fuel quantity indicators are unreliable at high angles of attack and/or any angles of side-slip. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
|
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Term
Due to high hydraulic pump output and low hydraulic reservoir capacity, a pressure line rupture will cause _____________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| A rapid and complete loss of system hydraulics |
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Term
If it is necessary to press the DOWN LOCK RELEASE switch to move the LDG GR handle to the UP position, the crew member should suspect ________________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| a malfunction of the landing gear ground safety switch |
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Term
Normal landing gear extension takes approximately _____ seconds andretraction takes approximately _____ seconds. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
|
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Term
Do not land with the brakes applied. A failed touchdown protection mechanism could result in ___________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| blown tires and damage to the aircraft |
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Term
When the "ANTI-SKID FAIL" annunciator is illuminated, anti-skid braking is not available and braking will be in the power brake mode. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
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Term
Normal braking can be used with emergency braking because the systems are independent. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
|
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Term
The parking brake should not be set ___________________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| if the brakes are hot, during low temperatures, when an accumulation of moisture is present, using the copilot's brake pedals |
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Term
In reference to the flap system, if the 26 VAC primary shed bus is lost ____________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| flap asymmetry detection is not available and the flap position indicator will be inoperative |
|
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Term
Failure to set the proper AOA value ________________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| may cause erroneous on-speed indications |
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Term
The rudder is _________ linked to the nosewheel steering system. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
|
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Term
The rudder boost ______ the loss of thrust in an asymmetric condition. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| is not designed to fully compensate for |
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Term
Which of the following affects the flight deck accelerometer (G meter)? (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
| speed, altitude, weight and fuel loading |
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Term
Aircraft ______ power is required for clock display lighting. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
|
|
Term
The aft fuselage door is designed such that the lower section must be opened prior to the upper section. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
|
|
Term
Discoloration, crazing, or scratches will weaken the structural strength of the windows. (Ref: T.O. 1T-1A-1)
6
Ref: TO 1T-1A-1 |
|
Definition
|
|
Term
Cabin window shades are to be open for ________________. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
|
Definition
|
|
Term
When throttles are advanced to ______ on the ground, the cabin is pressurized to a positive 80 to 120 foot differential. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
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Definition
|
|
Term
The "CABIN PRESSURE LO" annunciator illuminates when cabin altitude exceeds _______. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
|
Definition
|
|
Term
Electric heat subsystem can only be used when the aircraft is _______. (Ref: T.O. 1T-1A-1)
Ref: TO 1T-1A-1 |
|
Definition
| On the ground and operating on external power |
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
|
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Term
|
Definition
|
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Term
|
Definition
| 550-600 (4) 600-700 (2) 700-720 (1) |
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
|
|
Term
| Max Oil Pressure Starting |
|
Definition
|
|
Term
| Max Transient Oil Pressure |
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Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Max Oil Temperature for Idle |
|
Definition
|
|
Term
| Oil Temperature for Starting |
|
Definition
|
|
Term
| Max Transient Oil Temperature |
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Definition
|
|
Term
|
Definition
|
|
Term
| Under cold starting procedures, normal oil temperature between ____ and ____ is limited to _____ |
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Definition
|
|
Term
| Normal Hydraulic Pressure is |
|
Definition
|
|
Term
| Normal Nitrogent Pressure is |
|
Definition
|
|
Term
| Normal Oxygen Pressure is |
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Definition
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Term
|
Definition
|
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Term
|
Definition
|
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Term
|
Definition
|
|
Term
| Max fuel imbalance for takeoff |
|
Definition
|
|
Term
| Max fuel imbalance for flight |
|
Definition
|
|
Term
| Max fuel imbalance for landing |
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Definition
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Term
|
Definition
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Term
|
Definition
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Term
|
Definition
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Term
| What does a red dash mean in the 781 |
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Definition
|
|
Term
| What does a red slash mean in a 781 |
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Definition
| Minor maintenance required |
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Term
| What does a red X mean in the 781 |
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Definition
|
|
Term
| What do black initials mean in the 781 |
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Definition
|
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Term
| Oil must be changed every |
|
Definition
|
|
Term
| What inspections are required daily? |
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Definition
| Tire Pressure, Oxygen, Nitrogen |
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Term
| Tire pressure check must be accomplished how many hours before the first flight of the day? |
|
Definition
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