FOM and Random stuff for Oral Flashcards
Captain will conduct the takeoff when vis. is
1600 RVR or less
1/4 statute mile or less (if no RVR is reported for that runway).
On the approach what must we have to be considered stabilized
(1000’ COOT)
- 1000’ descent rate by 1000’ AGL
- Configured
- On proper flight path
- On speed
- Trimmed
When vis is less than 3/4 mile or RVR is 4000 on a CAT 1 ILS the aircraft must have:
Dual or single flight director and a coupled autopilot
If a low time FO, the captain will make all Takeoff, Approach below 3000’ and all landings if any of the following conditions exist:
(AABCCRVW)
- Anytime Captain deems necessary
- Airports (special)
- Braking action less than good.
- Crosswind greater than 15kts.
- Contaminated RWY
- RVR 4000 or less
- Visibility 3/4 miles or less
- Windshear in the vicinity
Without TDZ light and or CL lights, including runways with installed but inoperative TDZ lights and or CL lights RVR cannot be blow
1800 RVR
If 10-9 says 600 RVR and you have CL lights and RWY edge light you can land. PSA lowest minima is 500 RVR
What are standard turbo jet landing mins
4000 RVR or 3/4 statute mile vis
What are standard turbo jet takeoff mins
5000 RVR or 1 statute mile vis.
What is fuel burn
Fuel to destination plus 1 approach at Destination
What is Takeoff fuel
Burn, Reserve, Hold and Alt if needed
Takeoff Alternate requirements
4600 lbs of fuel, one hour from departure airport at normal cruise speed in still air one engine inop. (300nm)
Flex Takeoff is prohibited when
ABCDEFG
Anti-skid inop
Bleeds-14th stage anti-ice is on
Contaminated RWY
De-iced
Engine is unable to produce max rated thrust
Field limitation
Gusts-windshear warning or forecast are present
Fuel required if Takeoff Alternate is required
4600lbs Per Flap AD.
Pitch trim is provided by
2 independent motors that actuate a jackscrew and moves the whole horizontal stabilizer
Flaps are powered by
2 PDU’s and a flex drive
If one PDU fails on the flaps what speed will they operate
Half speed
GND LIFT DUMPING switch in AUTO, arming of the system is achieved by:
Both engines greater than 79% N1
Thrust levers position to T/O power
Wheel speed greater than 45kts
Spoilerons will deploy when:
Thrust levers at idle or less than 40% N1 AND, WOW
and 1 of the 2 conditions:
Wheel speed greater than 16kts
RA less than 5 feet
Ground and flight spoilers deploy when:
Thrust levers at idle or less than 40% N1 AND any 2 of the 3 conditions:
L or R MLG WOW
Wheel speed greater than 16 kts
RA less than 5 feet AGL
Anti-Skid is armed when
35kts wheel speed
WOW signal for 5 secs.
Less than 10kts wheel speed Anti-skid will disengage
Tiller and rudder limits
Tiller-70 degrees
Rudders-5 degrees
After landing when will CPAM change CPC’s
WOW and after 3 mins.
Reserve fuel is based upon
No less than 45 minutes, long range cruise power setting at FL250.
Each generator control unit (GCU) controls and monitors the related AC generator system and provides protection and voltage regulation for its
respective generator.
Over/ Undervoltage
Over/ Underfrequency
Generator or bus overcurrent
What is powered by the AC ESS BUS
BATE
Bleed detection controllers L/R AOA probe heater Left TCAS ESS TRU 1 • This bus is normally fed from AC BUS 1.
