CITATION CJ2 (CE 525A) SN 0001 & Subs.
ENGINE FAILURE OR FIRE OR MASTER WARNING
DURING TAKE OFF
• SPEED BELOW V1 - TAKEOFF REJECTED
Brakes…………………………………AS REQUIRED
Throttles……………………….…………………..IDLE
Speed brakes……………………………….....EXTEND
1.
2.
3.
• SPEED ABOVE V1 - TAKEOFF CONTINUED
1.
2.
3.
4.
5.
6.
Maintain Directional Control
Accelerate to VR
Rotate at VR, Climb at V2
Landing Gear -UP (after positive rate-of-climb)
WING/ENGINE XFLOW Switch –WINGX FLOW
(if WING/ENGINEANTI-ICE Switches are in WING/ENG
At 1500 feet AGL, retract flaps at V2 +10 then
accelerate to V ENR (VT )
ENGINE FAILURE DURING FINAL APPROACH
1.
2.
3.
Thrust (Operating Engine)….. INCREASE as required
Airspeed…………………………………………...VAPP
Flaps.............................TAKEOFF AND APPROACH
ENGINE FIRE (LH OR RH ENGINE FIRE WARNING
LIGHT ILLUMINATED)
1.
2.
3.
Throttle (Affected Engine)….……………………IDLE
IF LIGHT REMAINS ILLUMINATED
Engine Fire Button ……...…LIFT COVER and PUSH
Either Illuminated Bottle Armed Button …….…..PUSH
EMERGENCY RESTART – TWO ENGINES
1. Ignition Switches….…………………………BOTH ON
2. L/R Fuel Boost Switches….…………………BOTH ON
3. Throttles……………………………………………IDLE
4. If Altitude Allows INCREASE AIRSPEED TO 200 KIAS
ELECTRICAL FIRE OR SMOKE &
ENVIRONMENTAL SYSTEM SMOKE OR ODOR
& SMOKE REMOVAL
1.
Oxygen Masks………………………..DON and EMER
2.
Microphone Select Switches….…….MIC OXY MASK
CABIN ALT (CABIN ALTITUDE)
1.
2.
3.
4.
Oxygen Masks…………….DON and 100% OXYGEN
Microphone Select Switches…..…. .MIC OXY MASK
Emergency Descent…………………...AS REQUIRED
Passenger Oxygen….….MAKE SURE passengers are
receiving oxygen
MEMORY ITEMS & LIMITATIONS
SPEEDS
MMO (Above 29,300 feet)…………….……………..0.720 MACH
VMO (8,000 to 29,300feet)……………………………….............. 275 KIAS
VMO (Below 8,000 feet)…………………………………260 KIAS
Max Autopilot Speeds………………...… 275 KIAS/0.720 MACH
VA…………………………………………..See Figure 2-8 (AFM)
Takeoff and Approach Flap 150 (VFE 150)…..………….200 KIAS
Flap Land 350 (VFE 350)….…………………………...... 161 KIAS
Max Speed Flaps Failed to Ground 60 ……………...….140 KIAS
VLE…………………………………………………...…200 KIAS
VLO (Extending)…………..…………………….............200 KIAS
VLO (Retracting)………………………………………...200 KIAS
Maximum Tire Ground Speed………………………..... 165 KIAS
Min Speed in Sustained Icing…(Not a Limit)...……......160 KIAS
VMCG - 89 KIAS
VMCA - 0 Flap-89 KIAS; 15 Flap –81 KIAS
0
o
o
WEIGHT LIMITS
Ramp…………………………………………...12,500 lbs, 5670 kg
Take Off……………………………………….............12,375 lbs, 5613 kg
Max Landing…………………………………...11,500 lbs, 5216 kg
Zero Fuel ……………………………………..…9,300 lbs, 4219 kg
EMERGENCY DESCENT
1.
2.
3.
4.
AP TRIM DISC Button…….…PRESS and RELEASE
Throttles…………………………………………..IDLE
Speed Brakes……………………………...….EXTEND
Airplane Pitch Attitude……...APPROXIMATELY 20
DEGREES NOSE DOWN
BATT O’TEMP (BATTERY OVERTEMPERATURE
1.
2.
3.
Volt/Amp…………………………………..….. NOTE
Battery Switch ………………………….…..….EMER
Volt/Amp……………….………..NOTE DECREASE
AUTOPILOT MALFUNCTION
1.
AP TRIM DISC Button……PRESS AND RELEASE
ELECTRIC ELEVATOR TRIM RUNAWAY
1.
2.
3.
4.
AP/TRIM DISC Button……PRESS AND RELEASE
Throttles…………….……………….AS REQUIRED
Speed Brakes………...………………AS REQUIRED
Manual Elevator Trim… ……………AS REQUIRED
5.
PITCH TRIM Circuit Breaker (L PANEL)….... PULL
EMERGENCY EVACUATION
1.
2.
3.
4.
5.
6.
7.
8.
9.
8.
9.
Parking Brake………………………………………SET
Throttles…………………………………...BOTH OFF
L/R Engine Fire Buttons…...……….…. BOTH PRESS
Illuminated BOTTLE ARMED Buttons…...…BOTH PRESS
(If Fire Suspected)
Battery Switch……………………………………. OFF
Emergency Locator Transmitter (ELT) MAKE SURE SYSTEM
IS ACTIVATED (if required for search and rescue services)
Airplane and immediate area…… CHECK FOR BEST
ESCAPE ROUTE
●IF THROUGH CABIN DOOR
Cabin Door……………………………….………OPEN
Move Away From Airplane
●IF THROUGH EMERGENCY EXIT
Procedure complete
Emergency Exit Door…...….REMOVE AND THROW
EXIT DOOR OUT OF AIRPLANE
Move Away From Airplane
Procedure complete
ENVIRONMENTAL LIMITS
Max Operating Altitude………………………..45,000 ft, 13,716 m
Max Landing/Take Off A ltitude………………...14,000 ft, 4267 m
Max Engine Start Alt………….………...………14,000 ft, 4,267 m
Max Takeoff Alt (Flaps15 )………………............……..14,000 ft, 4,267 m
Max Battery /EPU Start Altitude …………….…14,000 ft, 4,267 m
Max Ambient Temp…………………..........….. Ref AFM Fig 2.9 and 4.7
(RAT) Takeoff/Landing
+55 º
(RAT) Enroute
+58 º
Minimum Ambient Temp…………….....................(Surface) -54 C
Minimum Battery Start Temp………………………..............-18 C
Minimum Takeoff/Landing and Engine Start (Cold Soaked) -33 C
Max NiCad Battery Starts……………………………...........…..3 per hour
A Generator Assist Start = ⅓ NiCad Battery Start
EPU= 0 Cycle NiCad Battery Start
Starter Limitations
Three Starts Per 30 Minutes with 60 Sec Rest Between Starts
Max Tail Wind Component Aircraft (Dry Runway)………....10 kts
Max Crosswind Component Aircraft (not a limit)…...............26 kts
Max Tail Wind Component Engine Start (Surface to 10,000 ft) 16 kts
(above 10,000 to 14,000 ft)....... 0 kts
Max Cross Wind Component (Engine Starts)……...................16 kts
Max Operating Oil Consumption (per engine)….......023 gal. .087 ltr
Minimum Battery Voltage For Starting…………......….…..24 VDC
Min/Max External Power Current for Start…….......800/1,100 amps
0
For Training Purposes Only - Refer to AFM for Complete Emergency Procedures
Orlando Learning Center
-1AFM Rev. 6
0
0
0
Rev. 1.0
ENGINE LIMITATIONS
ITT ………………..During Start……………………….. 15 Seconds Only…………………………...1000 ºC
ITT ………………..Tak e Off……… …………………….5 Minutes Max 2-Eng…10 Min 1-E ng……..820ºC
ITT ………………..Flight………………………………...Max Continuous…………………………....805º C
N1………………………………………During Start Sequence........………………………………....10 SE C
N1………………………………………Max T ake Off & MCT..………...……….…....................................105.2
N2…………………………………………….Starting…………………………………………….8% to 12%
N2………………………………………Start Sequence E nds……………………………………………45%
N2……………………………………………Anti-Ice Idle………..… …………………...70.4 ± 2.5% (70%)
N2……………………………………………..Flight Idle…………………………..…..…64.3 ± 2.5% (65%)
N2……………………………………………Ground Idle………….………..…………….53.4 ± 2.5%(54% )
N2……………………………………...M ax Continuous/Max....………………………………………98.8%
ELECTRICAL
HOT BATTERY BUS
1. L ights (L uggage/E xit)
2. Volt meter
3. E mergency B attery Pack (5G)
(E mergency E xit L ights)
4. ELT
EMER BATTERY BUS
1. Comm 1
2. Nav. 1 and Marker Beacon
3. ST A NDB Y HS I
4. FloodL ights
5. A irspeed /A ltimeter(Vibrat or)
6. *A udio Panels # 1 & 2
7. ST A NDB Y N1 Digits
8. R H Pitot Static Heat
9. Landing gear control/and Hydraulic Control
10. Flap control
11. Landing gear monitor (lights/horn)
12. AHRS # 2
GCU
R egulates to 29V
Parallels Electrical Loads
ProtectsElectrical System
GENERAL
Battery Over T emp System: First light comes on at 63ºC(145ºF) Second light at 71ºC(160ºF)
When battery switch is in the E ME R . Position; both Hot and E ME R busses are powered.
When airborne with dual Generator Failure: Battery Switch “ON” batterypower will last aproximately 10 minutes.
When airborne with dual Generator Failure: Battery Switch “E ME R ” battery power lasts a minimum of 30 minutes.
Max Generator A mps allowed in Flight to FL 410: 300 amps, 50% overload permitted for 2 minutes.
Max Generator A mps allowed on Ground and above FL 410: 250 amps.
W indshield B leed: “H igh” at Temps –18ºC and below, “L ow” at Temps above –18ºC.
Max intentional fuel differential 200 lbs. Max emergency fuel differential 600 lbs.
Speed brakes must be retracted prior to 50 ft on landing.
T ouch and Go landings utilizing ground flaps are PR OHIB IT E D.
T ake off with thrust attenuators and anti-skid inoperative is PR OHIB IT E D.
T ake off / L anding with thrust attenuators stowed ( Use Dispatch Checklist Tab CC3).
T ake off / L anding with anti-skid inoperative (Use Dispatch Checklist Tab CC2)
For Training Purposes Only - Refer to AFM for Complete Emergency Procedures
Orlando Learning Center
-2AFM Rev. 6
Rev. 1.0