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ATI Recurrent study

QuestionAnswer
Below AH/DH go-around for- NO AUTOLAND Visual reference lost on FP approach Not in position to land on FP approach
What causes a pack off light? 1. Pack selector off 2. Pack trip 3. Loss of air to pack
What does pulling the engine fire handle do? 1. Closes engine and spar fuel valve 2. Closes bleed air valve 3. Trips field and generator breaker 4. Shuts off hydraulic fluid 5. Arms fire extinguisher 6. Silences fire bell *APU is the same except for hydraulics
Auto brakes disarm when… 1. Pedal brakes applied 2. Thrust levers advance after landing 3. Speed brake lever moved to retract after landing 4. Disarm or off selected 5. Auto brake fault 6. Normal anti skid fault
Alternate airport for departure should be within how many miles? 375 nm for the 757/767
Dual engine failure 1. Both engine start selectors - FLT 2. Both thrust levers - Idle 3. Both fuel control switches- cutoff, then run 4. If engine stalled or at EGT limit repeat above step
V1 cut profile At 400’- LNAV or heading select. Declare emergency At 1000’- Set vertical speed 0-200 Retract flaps on schedule Flaps then at VREF+80- “Flight level change, Set max continuous thrust” “Center command, _____checklist. After TO check”
What causes a pack inop light 1. Pack outlet temp too high 2. Pack compartment overheat 3. Pack temp control failure
What does the alternate flap switch do? 1. Arms electric motors 2. Shuts hydraulic valves 3. Depressurizes actuators
What are the nose gear steering angles? Tiller- 65 degrees Rudder pedals- 7 degrees
767- 300 wingspan 156’ 1” without winglets 166’ with winglets
Minimum fuel temperature 3 degrees above the freeze point of the fuel being used.
Cargo door wind limits Pemco- 40 knots Precision- up to canopy 45 knots Above canopy 25 knots 767- open 60 knots Operating 40 knots
Aborted engine start Fuel control switch (affected side)- cutoff
CABIN ALTITUDE or rapid depressurization 1. Don Oxygen masks 2. Establish crew communications 3. Check cabin altitude and rate 4. If cabin uncontrollable - Passenger oxygen switch- push for one second’ Thrust levers- idle Extend speed brakes Limit speed is structural integrity in doubt. If not d
Brake pressure sources 767 right, center, center, right 757 right, left, right, right
Stab trim light comes on when- 1. Runaway trim 2. Autopilot trim is opposite elevator control 3. Manual trim opposite direction of autopilot trim
The fuel config light comes on when- 1. Less than 2000lbs in each main tank 2. Imbalance- 2000lbs (767) 1800 (757) 3. 1200lbs in center tanks and center pumps off
What causes a takeoff warning? 1. Flaps not set 2. Parking brake set 3. Spoilers not retracted 4. Stabilizer not in takeoff range
Engine limit, surge or stall 1. A/T arm switch off 2. Thrust lever (affected side)- confirm- retard until within limits or idle
RTO autobrakes when- 1. RTO selected 2. Airplane is on the ground 3. Ground speed above 85 knots 4. Both thrust levers retarded to idle
Function of the pitch enhancement system- Utilizes a hydraulic motor in the right system to drive a pump that uses trapped fluid in the left system to move stabilizer
Turn radii 767-300 146’ 767-200 129’ 757-200 120’
Enroute engine failure flow A/T off TMSP- cont Throttle (good engine) set cont FMS execute eng out Set engine out altitude in MSP Driftdown Seat belt sign on
Busses the the HDG powers Standby AC and DC Lt and rt transfer busses Lt instrument transfer bus Hot battery bus Battery bus
Busses powered by the battery Hot battery bus Battery bus Standby AC and DC
Max center tank fuel when mains not full 767- 22,050 757- 2,000
Created by: Bostanley
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