General Flashcards
Pilot aborts starts for:
1) No Oil Pressure within 20 seconds of ITT rise.
2) No N1 by 40% N2.
3) No stable GRD idle within 90 seconds of ITT rise.
FADEC aborts starts for:
1) Insufficient ITT rise within 20 seconds after fuel flow.
2) ITT limit exceeded.
TRU max current Limit?
100 Amps.
Minimum battery temperature for APU Start?
-20C
Minimum battery temperature for engine start?
-10C
Flap setting for anti-ice Type 2, 3, or 4.
Flaps 1.
Tail height.
21 feet.
Aircraft width?
73 feet.
Aircraft length?
63 feet.
Monitored doors?
1) L and R Nose.
2) Passenger door.
3) Emergency exit door.
4) Baggage door.
5) Tail come access door.
6) Lav doors.
Which electrical bus is the Cabin Door on?
Left Battery.
Cabin entry door holds at closed for how many seconds?
10 seconds, +- 2.
Cabin entry door “Pressure Warning” LED light means what?
Cabin is pressurized.
Baggage compartment heated? Pressurized?
No. No.
Battery type and amps?
44 amp/hr Ni-CAD.
Engine Generator Amps?
300 Amps, Above FL350 275 Amps.
APU Amps?
275 Amps.
Fuel boost pumps turns on for:
SLAC
1) Starting engines.
2) Low Pressure sensed.
3) APU running without R engine running.
4) Crossfeed operation.
Accessory Gearbox driven systems.
SOAPFH
1) Starter/Generator.
2) Oil Pump.
3) Alternator.
4) PMA (Permanent Magnet Alternator)
5) Fuel Pump.
6) Hydraulic Pump.
Latitude Engines.
PW306D1, 5907 pounds of thrust.
Service Air:
*Available anytime Bleed-Air source in on.
1) Cabin Recirculation Valve.
2) Enables ACM (Air Cycle Machine) low temp limit valve.
PITOT/STATIC Heat:
1) Pitot
2) Static
3) Angle of Attack.
ENG/STAB heat:
HIRES
1) Horizontal Stabilizer.
2) Inboard wing, (1/3).
3) RAT probes.
4) Engine Inlets.
5) Stator Vanes.
What is powered by the hydraulic system:
BLTSSN
1) Brakes.
2) Landing Gear.
3) Thrust Reversers.
4) Speed Brakes.
5) Spoilers.
6) Nose wheel steering.
Bootstrap Accumulator ensures:
Hydraulic pump lubrication during engine start.
Elevator trim tabs:
1) Aerodynamically fairs elevator in position with the stabilizer.
2) Above Mach 0.77 helps prevent Mach tuck.
What is a RED CAS message and it’s indicators?
Warning message:
- Flashing Master Warning Light.
- Audio Alert: Aural or (2) Chimes.
- CAS message remains until resolved.
What is a AMBER CAS message and it’s indicators?
Caution message:
- Master Caution light.
- (1) Chime.
- CAS message remains until resolved.
What is a WHITE CAS message and it’s indicators?
Advisory message.
- CAS message flashes for 5 seconds, then steady.
Engine Ground Idle?
57% N2.
Engine Flight Idle?
65% N2.
CDFA Requirements:
Continuous Descent Final Approach:
VAST (Vertical decent, Altimeter, Straight, Temp)
- Straight in Approach Minimums.
- Published descent angle.
- Cold correction if needed.
- Local altimeter setting.
Emergency Descent Mode Requirements:
- Aircraft Above 30,000 Feet.
- Autopilot Engaged.
- Cabin Altitude exceeds 14,500 feet.
Flight Abort Mode Requirements:
- Descent is initiated.
- Flight never reaches 6000 feet above takeoff field elevation.
- Flight time less than 10 minutes.
TOGA button actions when pressed:
- Cancels Autopilot.
- Flight Director rolls wings level.
- Flight Director pitches for 7.5 degrees in the air, 10.0 degrees on the ground.
- Sequences the FMS for missed Approach.
Generator cooling requirements:
Engine Idle with Generator load of <75 amps for 4 minutes prior to shutdown or wait 35 minutes after shutdown to start.
Oxygen bottle size and location:
77 cubic feet, left nose compartment.
Minimum Flap Maneuvering Speed
UP - 150 kts
1 - 145 kts
2 - 140 kts
FULL - VREF+10
RVSM Requirements
1 Autopilot
1 Altitude Alerting Device
1 ATC Altitude Reporting Transponder
2 Air Data Computers
2 Pitot Probe Heaters linked to ADC in use
160 kt Minimum Airspeed in RVSM Airspace
Zero Fuel Weight
21,430 pounds
