Oral Must Knows Flashcards
APU Auto Shutdown - Ground
- Underspeed
- FADEC Critical Fault
- Overspeed
- Sensor Fail
- High Oil Temp
- EGT Over Temp
- Low Oil Pressure
- Fire
APU Auto Shutdown - Air
- Underspeed
- FADEC Critical Fault
- Overspeed
DC HOT BATT BUS 1 Items
- Battery 1
- Engine 1 Oil Level
- Engine 1A/2A Fire Bottle
- Engine 1 Fuel/Hydraulic SOV
- Courtesy/Service Lights
- DC Ceiling Lights
DC HOT BATT BUS 2 Items
- Battery 2
- Engine 2 Oil Level
- Engine 1B/2B Fire Bottle
- Engine 2 Fuel/Hydraulic SOV
- CMC
- Panel Refueling
- Water/Waste Sys. Controller
Higher Level Functions - Elevator
- Gain on Speed
- AOA Limiting
- Thrust Compensation
Higher Level Functions - Rudder
- Gain on Speed
- Turn Coordination
- Yaw Dampener
- Stroke Limiting (high speed panel limiting)
- Rudder flight authority (low speed, ensures enough rudder authority during ATTCS event)
Higher Level Functions - Spoilers
- Gain on speed
- Roll spoiler scheduling with airspeed and speed brake deployment
NOTE: Speed brakes/Ground Spoilers are not available in Direct Mode
Conditions That Will…
Close the ECS PACKS
- A bleed source is not available for the PACK
- The respective Pack button is OFF
- Any engine start with WoW (both PACKs close)
- Respective engine is starting (no WoW) and opposite engine is not starting
- Any engine is starting and APU is the bleed source (both PACKs close)
- Respective bleed leak
- Respective BIT failure
Conditions That Will…
Open the APU Bleed
- Commanded open when the following conditions occur simultaneously:
- APU bleed switch is set to AUTO
- APU bleed is available
- No APU/left bleed duct leak
- Left engine bleed is unavailable
- No anti-ice requested
Conditions That Will…
Open the Cross Bleed
- Commanded open when the following conditions are met:
* XBLEED button is push in (AUTO)
* One side providing bleed pressure and there is not a bleed source on the opposite side
* APU bleed button pushed out for main engine start
* Engine 2 start in the air
* APU bleed off for Engine 1 start in the air
* No bleed leak
Conditions That Will…
Open engine bleed valve
- Engine bleed valve is commanded open when the following conditions are met simultaneously:
- Respective bleed switch is AUTO
- Respective engine bleed is available
- No fire is detected in respective engine
- No bleed leak is detected
Conditions That Will…
Shutoff Recirculation Fans
- The DUMP button is pressed
- Smoke is detected in the recirculation bay
- Both PACKs are commanded OFF
- Cargo bay fire signal activates
Conditions That Will…
Disengage Autopilot
- Quick disconnect button
- AP button on the Guidance Panel
- Manual pitch trim is actuated
- Stick Shaker actuated
- Windshear
- Direct Mode
- Aileron/Elevator disconnect
- Exerting strong force on the yoke
- Internal fault
Conditions That Will…
Disengage Autothrottle
- Pressing either AT disconnect button on the thrust levers
- Pressing the AT button on the guidance panel
- Automatically disengages:
* After touchdown
* When thrust lever is moved beyond the TO/GA detent
Visibility requirements:
* Standard visibility for takeoff
* Lower than standard visibility for takeoff
- Standard vis - 5000 RVR
- Lower than standard:
- 1600 RVR = 1/4 RVV
- 12/12/10 = RCLM (day only), or HIRL, or CL
- 10/10/10 = RCLM and HIRL, or CL
- 5/5/5 = HIRL and CL
Interior Safety Inspection:
Manuals & Documents
- Two EPCs
- Two Normal Checklists
- Two icing conditions, cold weather, cold soaked operations
- Two lightning strike, turbulent air penetration, hot weather
- Two ECS off takeoff, engine battery start checklist
- Two CAT II INFORMATION and CALLOUTS cards
- QRH
- AML
- W&B manifest
- Jumpseat briefing card
- Passenger count card
- Passenger briefing safety information cards
- TOLD cards
- Airworthiness Cert/Registration
- Radio station cert
Interior safety inspection:
Equipment
Doorway:
1. PBE (1)
2. Halon fire extinguisher (1) - pressure in green, pin installed
3. Crash axe (1)
Captain’s side:
1. Flashlight
2. Life vest
3. Jumpseat life vest
4. Circuit breakers - closed/collared
5. Escape rope
6. Headset
First officer’s side:
1. Flashlight
2. Circuit breakers - closed/collared
3. Life vest
4. Escape rope
5. Landing gear and RAT safety pins (4)
6. Headset
Aft control pedestal:
1. Observer 02
2. Observer audio panel
3. Headset
Observer seat - check condition
Walk around:
Left FWD fuselage
- Forward passenger door
- AC power receptacle - secured or in use
a) Ground service switch - “IN USE” if attached with proper power requirements
b) LAN connection
c) steering switch
d) interphone connection - Left smart probes (2) /TAT sensor/Ice detector
a) smart probes #1&3 - read static pressure, dynamic pressure, AOA (sensor holes)
b) no dents or missing paint inside boxed/bracketed area
Walk around:
Nose section
- Static discharge strips (6) must be on airplane.
- Downlock springs
a) red towing light - parking brake is on, toe brakes are on, steering is on - Windshield wipers - stopped on metal and not glass
- Radome - latched
- Forward avionics bay - “plug-type” door, will become flush with fuselage when plane is pressurized
a) fly by wire battery vent - hole forward of the avionics bay - Lower FWD antenna- DME 1
Walk around:
Nose landing gear
- Wheels/tires -
AC ESS BUS
- AC FUEL PUMP 2A
- ACMP 3A
- SF-ACE 1 FLAP CH 1 AC FEED
- SF-ACE 2 SLAT CH 2 AC FEED
