26-50 Flashcards
(24 cards)
- What are the maximum temperature limits for the AN/DAS-1 A during operation and non-operation?
A. +55 and +85 degrees C
B. +55 and +90 degrees C
C. +60 and +85 degrees C
D. +60 and +90 degrees C
A. +55 and +85 degrees C
- The AN/DAS -1 A sensor can be used to inspect the ___________ of the wings (and visual ice detector, if equipped) for ice accumulation.
A. Leading edge
B. Pilot tubes
C. Gear
D. None of the above
A. Leading edge
- Operating procedures, techniques, etc which could result in damage to equipment if not carefully followed.
A. Warning
B. Caution
C. Note
D. None of the above
B. Caution
- __________-Express non-mandatory provisions.
A. Shall
B. Should and may
C. Will
D. If
B. Should and may
- The EPO switch disconnects ___________.
A. All AC power from the GCS
B. Incoming AC power and UPS output
C. UPS output
D. None of the above
A. All AC power from the GCS
- There are three ranges of condition lever settings. The _______________ position provides for normal operations, the detention position closes fuel shut off valve and ________ mechanically feathers the propeller and closes the fuel shut off valve.
Full forward, full aft
- Outboard wining tanks feed the inboard tanks via __________.
Gravity
- The fuel load is distributed among____________ fuel tanks in the MQ-9?
7
- Below what fuel feed pressure does the RCM turn on the electric fuel pump that is not in use to supply fuel from the header tank to the engine?
15 psi
- If the header tank pressure exceeds _________ psi, a return solenoid failure warning is downlinked to the GCS.
4.6
- (ER) Gross take off weight of the extended range configuration is __________.
11,700 pounds
- The aircraft is equipped with 6 batteries (2 sets of 3) with a total rating of 84 ampere hours. At minimum system amperage of about 60 amperes, this would provide a flight time of approximately 70 minutes of flight time. With airborne modem on, expected usage is about 88 amperes with approximately __________ of flight time remaining.
48 minutes
- Batteries can be recharged in flight for the Block 1 MQ-9 variant.
True or false
False
- If Bus 1 fails, no -essential equipment such as KU-band ADT, will continue to receive power from Bus 2 via the PPDM 1
True or false
False
- The transmission of the C-band LOS datalink is referred to as the _____ and _______, while the Ku-band SATCOM transmissions and Block 5 CDL transmission are called ________ and _________.
Uplink, downlink, command link, return link
- If a rack switch is performed with a gaining rack’s controls improperly positioned, the aircraft will automatically be sent lost link until the gaining rack’s controls are set to the proper position.
True or false
True
- _______ is indicated by a complete list of HUD video with continued presence of telemetry.
Video source failure
- With a left PSO rack failure or rack lack up, the pilot has the option of sending the aircraft lost link prior to executing the PSO-1 rack lock up checklist
True or false
True
- If no emergency mission is loaded on PSO 2, then as soon as the rack switch buttons is pressed, the emergency mission start point will immediately change to ______________ regardless of what the PSO-1 tracker display shows.
Waypoint 1
- Store scan be jettisoned with the nose gear extended
True or false
False
- Loss of control may be indicated by complete failure of the aircraft to respond to pilot control command. This may be caused by?
A. Airspeed or pilot/static failure
B. AOA failure below 120 KIAS with stall protect on or SAS failure
C. Autopilot sensor failure, structural failure or airframe icing
D. All of the above
All of the above
- Pilot heat does not guarantee the absence of ice from the pilot/static system. Moisture can freeze in the unheated areas. This malfunction may be indicated by “FCA (1,2,3) PPT- Airspeed sensor faulty” warning message, abnormal attitude, abnormal airspeed or a combination of any of these. These conditions may result in:
A. Aircraft pitch oscillations
B. Loss of datalink
C. Loss of aircraft control
D. All of the above
All of the above
- When battery voltage drops below _______ volts, all electrical power may be lost.
22
- Do not allow the engine to windmill between ____ and ____ percent RPM.
18-28
