SIM0215 Flashcards
LCALHR LOE 2
ALTN eng start FWD CARGO DOOR FLIGHT MANAGEMENT R REVERSER UNLOCKED DIVERSION
LHRYYC LOE 1
R GEN OFF VNAV FAIL VOLCANIC ASH UNRELIABLE A/S CARGO FIRE
ATHLHR LOE 3
C HYD PRIM 1 PRESS C HYD PRIM 2 OVHT NADP 1 R PACK TEMP ( abv 10000') Diversion - strong limiting winds
Airspeed Unreliable Memory items
AP OUT
AT OUT
FD BOTH OFF
Set the following Gear Up attitude and thrust
Clean - 4degrees / 75% N1
FLAP - 10 degrees/ 80% N1
UNRELIABLE AIRSPEED
What items are considered RELIABLE
Attitude
N1
GROUND SPEED
Radio Altitude
Engine Failure in the Cruise
Memory Items
Disconnect Auto throttle (Autothrottle arm switch off) SELECT Max Con SET Max Con TRIM - rotary switch ( AP is still in ) SELECT ENG OUT CRZ SET ALT on MCP Slow to Engine Out Speed Select VNAV
MAY DAY
QRH
What is the procedure for Alternative Engine Start? (LOE 2 LCA)
Manual Override start procedure
1 “Open Start Valve” then set engine start selector to GND
2 At 50% N3 “close start valve”
Confirm Engine start selector returns to Auto
ENGINE FAILURE DURING CLIMB at 500’ 15 degrees Pitch up
Visual clues are lost. Control with aileron and rudder
Pitch down to 10 degrees nose up
“CONFIRM THE FAILURE”
(Recall items Engine Fire Checklist)
Full power live engine. (Disconnect AT)
Acceleration Alt - vs 0
FLAP 1, Flap up
FLCH
Flaps up - Max continuous
HYDRAULICS
What does the LEFT system control ?
FLIGHT CONTROLS ONLY
HYDRAULICS
What does the CENTRE system control ?
Flight controls Flaps and Slats Landing Gear Tail Skid HDG Nose wheel Steering Alternate Brakes
HYDRAULICS
What does the RIGHT system control ?
Flight controls
Normal Brakes
PES
Actions to set up BACK COURSE ILS
Tune front course for radiating ILS (271)
Set BC on standby AH
Use HDG SEL and VS
DONT USE LOC
What is CRITICAL FUEL ?
Critical fuel is fuel additional to normal fuel to allow the aircraft to divert to an ETOPS ADEQUATE ALTERNATE
What THREE scenarios does Cirrus take into account when calculating Critical Fuel ?
- Pressurisation failure followed by two engine diversion
- Engine failure and pressurisation failure followed by single engine diversion
- Engine failure followed by drift down to stabilising altitude and a single engine diversion.