Random SOP etc Flashcards
Abort for
(C-20 SOP)
- Fire/Indication
- Engine Failure
- Uncommanded Thrust Reverser Deployment
- Loss of Directional Control
Sensor Priority of FMS
- GPS
- DME-DME
- VOR/DME
- IRS
Systems affected by a DADC failure
- Airspeed
- Altimeter
- AOA
- Vertical Speed
- Pressurization
- Transponder
Configuration Modes on FMS
- Dual
- Single
- Independent
- Initiated Transfer
CAS msg with loss of lateral navigation
- “CPL DATA INVALID”
Engine Fire Extinguisher pressure reading
- 600-625 psi & 70°
Fuel Hopper
- Quantity - How filled
- Quantity: 190 gallons
- Filled: Ejector Pump
Fuel in excess of 29,500 lbs
- Display
- DUs: Max 15,000 lbs/side
- b/u Fuel Qty Ind: Direct from Probes
Aux Pump throughput
- 1 gallon/min
B/u Fuel Qty Indicator Check indications
D(isp): all 8s
I(ndicator):
- Normal: 7,7,14, flash for 30sec, CAS msg
- Abnormal: 9,9,18 (sensor is not in fuel)
(e.g. contaminated)
Considerations for Restarting an Engine
“FFEVER”
Fire
FOD
Erratic Operations
Vibration
Excessive EGT
Rotation
Time for Door Seals to Deflate
- Front: 15 sec
- Rear: 5 sec
Where is the Configuration Deviation List
- AFM or OM, APP B
Immediate Action items for Rejected Takeoff
- Power Levers…..IDLE
- Max Braking…..AS REQ’D
- Speed Brakes…..Deploy
- Thrust Reverser…..AS REQ’D
- Advise Tower
Can the Batteries be charged on EXT DC
No, only with AC buses powered
Minimum acceptable voltage on Battery Integrity Check
22V DC
Battery Rating
28V, 40 AmpHr
What buses show as powered on EPMP w/ BATT switches on and no other sources of power
ESS DC and ESS AC
BATTS - ON
Acceptable readings for ESS BUSes
- AC: 115 VAC, 400 Hz
- DC: 22-27 V
What buses are powered when EXT BATTERY switch is selected on
- ESS DC: Batteries
- ESS AC: E-Inverter (Phase A)
Where is the list of items powered by E-BATTs?
QRH: Electrical system Abnormal Procedures
(Section EA)
Flight Guidance Panel (FGP), Flight Mode Annunciator (FMA) Sections
“SLAVE”
Speed
Lateral
Auto-throttle
Vertical
Elevation
Estimate Vref speeds
VrefNF = ~100+GW (in 1,000s)
e.g. 54,000 lbs GW
VrefNF = ~154 kts
Vref39 = VrefNF - 20 (e.g. 134)
Vref20 = Vref39 + 5 (e.g. 139)
Vref10 = Vref20 +5 (e.g. 144)
Holding Speeds
- 0’-6,000’: 200 KIAS
- 6,001’-14,000’: 230 KIAS
- 14,001’+: 265 KIAS
What to do for dual converter failure (cockpit setup)
“NAACP”
Normal - (SG1)
Alt - (SG2)
Alt - (SG3)
Crossflow Valve - OPEN
Pumps (all but 1 Fuel Boost Pump - OFF)