C560XL Emergency Memory Items
ENGINE FAILURE, OR FIRE, OR MASTER
WARNING DURING TAKEOFF
SPEED BELOW V1 - TAKEOFF SHOULD BE ABORTED
1.
2.
3.
4.
BRAKES - MAXIMUM PILOT EFFORT
THROTTLES - IDLE
THRUST REVERSER - DEPLOY ON UNAFFECTED ENGINE
THRUST REVERSER INDICATOR LIGHTS - CHECK ILLUMINATION OF
ARM, UNLOCK AND DEPLOY LIGHTS.
5. THRUST REVERSER - REVERSE POWER ON UNAFFECTED ENGINE
SPEED ABOVE V1 - TAKEOFF SHOULD NORMALLY BE CONTINUED
1. ROTATE - VR
2. LANDING GEAR - UP (AFTER POSITIVE RATE-OF-CLIMB)
3. CLIMB - V2 UNTIL LEVEL OFF ALTITUDE
XLS
ENGINE FAILURE, OR FIRE, OR MASTER
WARNING DURING TAKEOFF
SPEED BELOW V1 - TAKEOFF SHOULD BE ABORTED
1.
2.
3.
4.
BRAKES - MAXIMUM PILOT EFFORT
THROTTLES - IDLE
THRUST REVERSER - DEPLOY ON UNAFFECTED ENGINE
THRUST REVERSER INDICATOR LIGHTS - CHECK ILLUMINATION OF
ARM, UNLOCK AND DEPLOY LIGHTS.
5. THRUST REVERSER - REVERSE POWER ON UNAFFECTED ENGINE
SPEED ABOVE V1 - TAKEOFF SHOULD NORMALLY BE CONTINUED
1. ROTATE - VR
2. LANDING GEAR - UP (AFTER POSITIVE RATE-OF-CLIMB)
3. Airspeed - V2 UNTIL LEVEL OFF ALTITUDE
4. Wing XFLow – ON (if wing anti-ice is ON)
C560XL Emergency Memory Items
ENGINE FIRE
(LH OR RH ENGINE FIRE WARNING LIGHT ON)
1. THROTTLE (affected engine) - IDLE
IF LIGHT REMAINS ON
2. ENGINE FIRE SWITCH (affected engine) - LIFT COVER AND PUSH
3. EITHER ILLUMINATED BOTTLE ARMED LIGHT - PUSH
C560XL Emergency Memory Items
ENGINE FAILURE DURING FINAL APPROACH
1.
2.
3.
4.
AP TRIM DISC - PRESS AND RELEASE
POWER (operating engine) - INCREASE AS REQUIRED
AIRSPEED - VAPP + 10
FLAPS - TAKEOFF AND APPROACH (15º)
C560XL Emergency Memory Items
EMERGENCY RESTART - TWO ENGINES
1. IGNITION SWITCHES - BOTH ON
2. FUEL BOOST PUMPS - BOTH ON
3. THROTTLES - IDLE
C560XL Emergency Memory Items
THRUST REVERSER INADVERTENT
DEPLOYMENT DURING TAKEOFF
SPEED BELOW V1 - TAKEOFF SHOULD BE ABORTED
1. BRAKES - AS REQUIRED
2. THROTTLES - IDLE
SPEED ABOVE V1 - TAKEOFF SHOULD NORMALLY BE CONTINUED
1. EMERGENCY STOW SWITCH - EMER
2. THROTTLE (affected engine) - CHECK IDLE
3. ROTATE - VR
4. LANDING GEAR - UP (after positive rate of climb).
DO NOT EXCEED 140 KIAS UNTIL THRUST REVERSER STOWS.
5. CLIMB - V2
C560XL Emergency Memory Items
THRUST REVERSER INADVERTENT INFLIGHT
DEPLOYMENT
1.
2.
3.
4.
CONTROL WHEEL/AP TRIM DISC - GRIP/PRESS AND RELEASE
EMERGENCY STOW SWITCH - EMER (affected engine)
THROTTLE (affected engine) - CHECK IDLE
AIRSPEED - REDUCE TO 140 KIAS OR BELOW
C560XL Emergency Memory Items
THRUST REVERSER UNLOCK LIGHT ON IN
FLIGHT
1. EMERGENCY STOW SWITCH - EMER (affected engine)
2. THRUST REVERSER LEVERS - CHECK THRUST REVERSER LEVERS
STOWED (full forward) POSITION
C560XL Emergency Memory Items
RAPID DECOMPRESSION
(CAB ALT WARNING LIGHT ON)
1. OXYGEN MASKS - DON AND 100% OXYGEN
2. MICROPHONE SWITCHES - MIC OXY MASK
3. EMERGENCY DECENT - AS REQUIRED
C560XL Emergency Memory Items
EMERGENCY DESCENT
1.
2.
3.
4.
5.
AP TRIM DISC - PRESS AND RELEASE
IGNITION - ON
THROTTLES - IDLE
SPEED BRAKE - EXTEND
AIRPLANE PITCH ATTITUDE – INITIALLY TARGET 20º NOSE DOWN
C560XL Emergency Memory Items
ENVIRONMENTAL SYSTEM SMOKE OR ODOR
1. OXYGEN MASKS - DON AND EMER
2. MICROPHONE SWITCHES - MIC OXY MASK
C560XL Emergency Memory Items
SMOKE REMOVAL
1. OXYGEN MASKS - DON AND EMER
2. MICROPHONE SWITCHES - MIC OXY MASK
C560XL Emergency Memory Items
BATTERY OVERTEMPERATURE
(BATT O’TEMP > 160º WARNING LIGHT ON)
1. AMPERAGE - NOTE
2. BATT SWITCH - EMER
3. AMPERAGE - NOTE DECREASE
C560XL Emergency Memory Items
AUTOPILOT MALFUNCTION
1. AP TRIM DISC SWITCH - PRESS AND RELEASE
C560XL Emergency Memory Items
EMERGENCY EVACUATION
1. PARKING BRAKE - ON
2. THROTTLES - BOTH CUT OFF
3. LH/RH ENGINE FIRE SWITCHES - BOTH PRESS
4. LH/RH FIRE BOTTLE ARMED SWITCHES - BOTH PRESS
(if fire suspected)
5. APU MASTER SWITCH - OFF
6. BATT SWITCH - OFF
C560XL Emergency Memory Items
APU FIRE
1. APU FIRE WARNING SWITCH – LIFT COVER AND PUSH
C560XL Emergency Memory Items
WHEEL BRAKE FAILURE
1. BRAKE PEDALS – REMOVE FEET FROM BRAKE PEDALS
2. EMERGENCY BRAKE HANDLE – PULL AS REQUIRED
XLS
WINDSHEAR WARNING
1. THRUST – T/O DETENT
2. AIRPLANE PITCH ATTITUDE – INITIAL PITCH OF 10 DEGREES
(Flight Director Go-Around Pitch Command)
3. SPEED BRAKE – CONFIRM RETRACTED
BASIC AIRPLANE LIMITS
Engine Instruments
N1 Fan Speed
Red line …………………...…………...………………… 100%
Green band ……...……………..…………………. 20 to 100%
N2 Turbine Speed
Flashing red light, steady digital readout …….………. > 101%
Normal operating …………………...….………… 47 to 101%
ITT
Red line …………….….……………..…………….…… 720°C
Green band ……….……………………………..…… 0°- 720°C
Oil Temperature
Red Line ……………………..……….……………….…. 121°C
Green band ……………………….………….…. 10° to 121°C
Oil Pressure
Red line (Min) ………….….……….……..…..………... 20 PSID
Yellow band ……….…………………..………. 20 to 45 PSID
Green band …………………………………… 45 to 140 PSID
Red line ……………………………......…………..… 140 PSID
Red Triangle (Max) ……………….………………… 250 PSID
XLS LIMITATIONS
Engine Instruments
N1 Fan Speed
Red line ………………...…………...….………………… 100%
Green band ……...…………..………….…………. 20 to 100%
N2 Turbine Speed
Flashing red light, steady digital readout …….….……. > 101%
Normal operating …………………...….……….… 47 to 101%
ITT
Red line …………….….……………..………….……… 740°C
Green band ……….……………………………..…… 0°- 720°C
Oil Temperature
Red Line ……………………..……….……………….…. 121°C
Green band ……………………….…………….….10° to 121°C
Oil Pressure
Red line (Min) ….…….….……….……..…...………... 20 PSID
Yellow band …….…………………..…………. 20 to 45 PSID
Green band …………………………………… 45 to 161 PSID
Red line …………………………......……………..…161 PSID
Red Triangle (Max) .….….……………… 250 PSID (5 MIN.)
BASIC AIRPLANE LIMITS
SPEED LIMITS
MMO (Above 26,515ft) ……...…………. 0.75 Mach (indicated)
VMO (Below 8,000ft) …………………………………... 260 KIAS
VMO (8,000ft to 26,515ft)………………………………. 305 KIAS
Autopilot Operation………. 305 KIAS or 0.75 Mach Indicated
VA
……………………………. Varies with weight & altitude
VSB ….…………………………………………………. No Limit
VLE ……………………………………………………. 250 KIAS
VLO ……………………………………………………... 200 KIAS
VFE (flaps 7º or 15º)
………………………………... 200 KIAS
VFE (flaps 35º, fully extended)
…………………….. 175 KIAS
Turbulent Air Penetration
……………………….…. 180 KIAS
Max Tire Ground Speed
……………………….…. 165 KIAS
Min Speed in Icing (except for approach & landing)..160 KIAS
VMCG (AB, Rudder Bias) ……………………..………. 81 KIAS
VMCA
………………………………………………….. 90 KIAS
BASIC AIRPLANE LIMITS
WEIGHT LIMITS
Max. Ramp Weight….………………….…………… 20,200lbs / 20,400 XLS
Max. Takeoff Weight……………………………….. 20,000lbs / 20,200 XLS
Max. Landing Weight
……………………….……... 18,700lbs
Max. Zero Fuel Weight (ZFW) …………………….. 15,000lbs / 15,100 XLS
Minimum Flight Weight (Gust Loading)
Max. Fuel Imbalance (Normal)
….……...……………... 400lbs
Max Fuel Imbalance (Emergency)
Tailcone Baggage Compartment
…………... 12,400lbs
……………………. 800lbs
………….…………... 700lbs
BASIC AIRPLANE LIMITS
ALTITUDES
….……………….…………… 45,000ft
Max. Operating Altitude
Max. Takeoff/Landing
……….………….…………….. 14,000ft
AMBIENT TEMPERATURES
Max. Temp., Takeoff & Landing
….……...….……… ISA +39°C
Min. Temp., Takeoff & Landing
.………….……………. -54°C
WINDS
Max. Tailwind Component
Crosswind Component
……………...……...…...….… 10kts
…... Direct 90° Crosswind - Dry/Wet 24 Kts
Contaminated Runway
Runway > 150' in Width 15 kts
< 150' in Width 10 kts
FOM Table 2.4.2 / 2.4.3
BASIC AIRPLANE LIMITS
MISCELLANEOUS LIMITS
Engine Starts:
Max. ITT ……………...………..……..…….………………720°C
(670°C FOR 7 Secs.)
N1 Indication by ……….………..………...……………….25%N2
Gen. Assist Start ..…..….Operating engine stable, GND IDLE
Battery Start Limit
………….…….…..……3 Engine starts in 1 hour*
Starter Limit …...…...………..……..…3 Engine starts in 30 min
with a 90 sec rest between start cycles
*Gen. Assist Start Equals ….….………….……1/3 battery start
GPU amperage set ……..……………………800 to 1000 Max.
Fuel:
All commercial Jet Fuel ……….………………………Approved
Aviation Gas ………………...……………………..Not approved
Prist ……………………………..……………….….Not Required
BASIC AIRPLANE LIMITS
MISCELLANEOUS LIMITS
Thrust Reversers:
Max. Reverse Thrust ……………………75% of takeoff thrust
Landing ………….….…………… Reduce thrust to idle, 60kts
Max. Allowable Deploy Time
…….……. 3 min/10 min period
Touch and Go Landings …………………….….… Prohibited
Operational….…………
Check
Conducted prior to first flight of the day
Use to back airplane ………………….…………… Prohibited
Landing Gear and Brakes:
Antiskid ………………………... Must be operational for takeoff
BASIC AIRPLANE LIMITS
MISCELLANEOUS LIMITS
Flight Controls:
Vortex Generators …..………………26 each wing for dispatch
Boundary Layer Energizers (BLE) …11 each wing for dispatch
Elevator Trim …....Preflight check completed prior to dispatch
Rudder Bias & Heater (AB) …….Must be operational for flight
Avionics:
AOA System ….Operable and preflight check prior to dispatch
Min. Autopilot Engagement Altitudes:
Enroute …………….…………………………………1000ft AGL
………………………………………………180’ AGL Precision / 300’ AGL
Approach
Non-Precision
RADOME FAIL Annunciator ON……………30 min ground time
and dispatch VMC
Category II Approaches …………………….…...Not Approved
PFD Reversionary Modes ..….…….Not approved for dispatch
Reversion of Both PFD’s to the MFD ………………Prohibited