-
VMO - VENTRAL FUEL TANK EMPTY, FLAPS 0
335 KIAS (SEA LEVEL - 12,000 FEET)
-
VMO - VENTRAL FUEL TANK NOT EMPTY
280 KIAS
-
-
MMO
(Mach trim system fail/inoperative and autopilot disengage)
Mach .73
-
-
VFE/VFO - FLAPS 15
220 KIAS
-
VFE/VFO - FLAPS 25
175 KIAS
-
VFE/VFO - FLAPS 45
165 KIAS
-
AIR BRAKES (FLAPS 0 ONLY)
NO LIMIT
-
-
BIRD STRIKE
NORMAL CONDITIONS
280 KIAS TO 8000 FEET
-
BIRD STRIKE
Cold ground soak, heat is on for required time limit
280 KIAS to 8000 feet
-
BIRD STRIKE
HEAT IS OFF <-10 C
257 KIAS TO 8000 FEET
-
MAXIMUM TAILWIND
(TAKEOFF AND LANDING)
10 KIAS
-
MAXIMUM OPERATING ALTITUDE
41,000 FEET
-
MAXIMUM ALTITUDE FLAPS LOWERED OR GEAR EXTENDED
20,000 FEET
-
MAXIMUM ALTITUDE - FLAPS 15
(DESCENT AND HOLDING)
15,000 FEET
-
MINIMUM FIELD PRESSURE ALTITUDE FOR TAKEOFF AND LANDING
-2000 FEET
-
MAXIMUM FIELD PRESSURE ALTITUDE FOR TAKEOFF AND LANDING
- Aircraft Equipped with High Datum (ProLine 21)
- 13,000 feet
-
MAXIMUM RAMP WEIGHT
28,120 POUNDS
-
MAXIMUM TAKEOFF WEIGHT
28,000 POUNDS
-
MAXIMUM LANDING WEIGHT
23,350 POUNDS
-
MAXIMUM ZERO FUEL WEIGHT
18,450 POUNDS
-
MINIMUM ZERO FUEL WEIGHT
14,120
-
MAXIMUM BATTERY AMPS BEFORE TAKEOFF (B1 AND B2)
20 AMPS
-
MAXIMUM CONTINUOUS GENERATOR LOAD
300 AMPS
-
MAXIMUM TRANSIENT GENERATOR LOAD
400 AMPS (2 MIN)
-
STARTER LIMITS
30 sec/1 min - 30 sec/1 min - 30 sec/30 min
-
-
-
TAKEOFF ITT
978 C (5 MIN)
-
TAKEOFF (APR OPERATING) - N1
100% RPM
-
TAKEOFF (APR OPERATING) - N2
100.8% RPM
-
TAKEOFF (APR OPERATING) - ITT
996 C (5 MIN)
-
TAKEOFF TRANSIENT - ITT
1006 C (5 sec) / 1016 C (2 sec)
-
MAXIMUM CONTINUOUS N1
100% RPM
-
MAXIMUM CONTINUOUS N2
100.8% RPM
-
MAXIMUM CONTINUOUS ITT
968 C
-
MAXIMUM CRUISE ITT
932 C
This is not a limitation, but engine life will be extended if 932 C is not exceeded during cruise operation.
-
MAXIMUM OVERSPEED N1
MAXIMUM OVERSPEED N2
103% RPM (5 SEC)
-
STARTING ITT
(UNRESTRICTED)
978 C
-
STARTING ITT
(TRANSIENT)
996 C (10 SEC) / OVER 996 C (5 SEC)
-
MAXIMUM OIL TEMPERATURE
(SEA LEVEL TO 30,00 FEET)
127 C
-
MAXIMUM OIL TEMPERATURE
(ABOVE 30,000 FEET)
140 C
-
MAXIMUM TRANSIENT OIL TEMPERATURE
149 C (2 MIN)
-
MINIMUM OIL TEMPERATURE
(STARTING)
-40 C
-
MINIMUM OIL TEMPERATURE
(TAKEOFF)
30 C
-
OIL PRESSURE LIMIT
(TAKEOFF, MAXIMUM CONTINUOUS, AND CLIMB)
38-46 PSI
-
OIL PRESSURE LIMIT
(MINIMUM IDLE)
25 PSI
-
OIL PRESSURE TRANSIENT MAXIMUM
55 PSI (3 MIN)
-
OIL CONSUMPTION RATE
.01 GAL PER HOUR
-
ENGINE FUEL COMPUTER
REQUIRED FOR FLIGHT
-
ENGINE SYNCHRONIZER SWITCH
OFF FOR TAKEOFF
-
AUTOMATIC PERFORMANCE RESERVE
(APR)
- MUST BE ARMED FOR TAKEOFF
- (EXCEPT FOR CREW TRAINING ONLY)
-
WING FUEL QUANTITY
1268 GAL/8500 LB
-
VENTRAL FUEL QUANTITY
233 GAL/1500 LB
-
TOTAL FUEL QUANTITY
1501 GAL/10,000 LB
-
MINIMUM WING FUEL REQUIRED WITH FUEL IN THE VENTRAL TANK
3450 LB PER SIDE
-
VENTRAL TANK FUEL RESTRICTION BEFORE FLIGHT
COMPLETELY FULL OR EMPTY
-
WING FUEL CONTENTS FOR VENTRAL TANK FUEL TRANSFER
3300 LB PER SIDE
-
MAXIMUM WING FUEL IMBALANCE
(FLIGHT, TAKEOFF, AND LANDING)
500 LBS
-
MAXIMUM FUEL TEMPERATURE
57 C
-
AIRFRAME ICING REQUIREMENTS
MUST BE CLEAR OF SNOW, ICE, AND FROST BEFORE TAKEOFF
-
APPROVED DE-ICE FLUIDS
TKS80, R328, OR FLUID SPECIFICATION DTD 406B
-
ICING DETECTION LIGHT REQUIREMENTS
MUST BE OPERATIVE PRIOR TO FLIGHT INTO ICING CONDITIONS AT NIGHT
-
MAXIMUM TEMPERATURE FOR ALL FLIGHT REGIMES
ISA +35 C
-
MINIMUM TEMPERATURE
(TAKEOFF AND LANDING)
-40 C
-
MINIMUM TEMPERATURE
(ENROUTE)
-75 C
-
MAXIMUM RUNWAY SLOPE FOR TAKEOFF
2% UPHILL OR DOWNHILL
-
AIR BRAKE USAGE
RESTRICTED TO FLAPS 0
-
CABIN HIGH DATUM SELECTION
LIMITED TO AIRFIELDS GREATER THAN 9,000 FEET
-
INTER-COMPARTMENT DOOR POSITION
OPEN DURING TAKEOFF AND LANDING
-
LIFT DUMP USE
ONLY WHEN AIRCRAFT IS ON GROUND
-
MAXIMUM LOAD FACTOR
FLAPS EXTENDED
2.0 G
-
MAXIMUM LOAD FACTOR
FLAPS RETRACTED
2.73 G
-
MINIMUM FLIGHT CREW REQUIREMENT
2 PILOTS
-
MAXIMUM PRESSURE DIFFERENTIAL
8.55 PSI
-
REJECTED TAKEOFF = OR < 90 KIAS
(SINGLE REJECTION WAITING PERIOD)
25 MINUTES
-
REJECTED TAKEOFF = OR < 90 KIAS
(TWO OR MORE REJECTIONS WAITING PERIOD)
45 MINUTES
-
REJECTED TAKEOFF
>90 KIAS REQUIREMENT
BRAKE INSPECTION
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
NORMAL OPERATION
100%
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
OPERATING LIMITS
Maximum Operating EGT
1350 F
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
OPERATING LIMITS
Maximum Operating Altitude
0 - 30,000 ft Pressure Altitude
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
OPERATING LIMITS
Maximum Starting Altitude
0 - 20,000 ft Pressure Altitude
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
STARTING CYCLE LIMITS
Maximum Transient EGT
15 seconds maximum duration..........1400 F to 1500 F
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
STARTING CYCLE LIMITS
Hung Start Duration
- Above 50% and Below 95% RPM ...... 10 second maximum
- Shutdown the APU if the READY TO LOAD light does not illuminate within 60 seconds of start.
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
STARTING CYCLE LIMITS
Starter Continuous Cranking Limits
- 1st Start Attempt ......... 30 seconds ON/3 minutes OFF
- 2nd Start Attempt ........... 30 seconds ON/3 minutes OFF
- 3rd Start Attempt ............ 30 seconds ON/30 minutes OFF
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
MAXIMUM GENERATOR ELECTRICAL LOADS
- The Maximum Transient Generator Load May Exceed Maximum Continuous Load:Maximum Continuous Operation ......... 0.80
- Transient Operation .......... 1.2 < 10 seconds
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
COMBINED BLEED AIR OPERATIONS
Simultaneous operation of APU bleed air and main engine bleed air is not permitted. Both systems may be operated briefly (1 minute maximum) during change over from one system to another.
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
OPERATION IN KNOWN ICING CONDITIONS
- Operation in known icing conditions: Flight operations of the APU are not approved when the airplane is in icing conditions
- Ground de-icing procedures:
-
The APU must be shut down during ground de-icing operations of the airplane
-
GARRETT GTC36-150W AUXILIARY POWER UNIT
APU OPERATION DURING AIRPLANE REFUELING
- Airplane refueling with the APU running is limited to center point refuel only. Gravity wing refueling is prohibited with the APU running.
- Starting of the APU while refueling is in progress is prohibited.
- Airplane refueling with the APU running is prohibited if the ambient temperature is above 40 C or when the airplane contains JP4 or is being refueled with JP4.
- Airplane boost pumps must be OFF prior to commencing refueling operations.
-
ENGINE FIRE, FAILURE OR INADVERTENT THRUST REVERSER DEPLOYMENT DURING TAKEOFF
Below V1 - Takeoff Aborted
- Thrust Levers: Close
- Brakes: Apply
- AIR BRAKES: Deploy
- Thrust Reversers: Deploy
-
ENGINE FIRE, FAILURE OR INADVERTENT THRUST REVERSER DEPLOYMENT DURING TAKEOFF
After V1 - Takeoff Continued
- Landing Gear (when positive climb established): UP
- Main Air Valves: CLOSE Both
- F/DK Valve: CLOSE
-
ENGINE FIRE IN FLIGHT
Fire Bell Sounds and
ENG 1 FIRE Annunciator and ENG 1 FIRE ↑ Repeater
Or
ENG 2 FIRE Annunciator and ENG 2 FIRE ↑ Repeater
Thrust Lever (Affected Engine): Close
- If Fire Warning Persists:
HP COCK (affected engine) : Close - LP COCK (affected engine): Close
- ENG EXT: SHOT 1
- If Engine Shutdown Occurs During Initial Climb:
-
MAIN AIR VLVs 1 & 2: Close - F/DK VLV: Close
-
ENGINE FIRE ON GROUND
Fire Bell Sounds and
ENG 1 FIRE Annunciator and ENG 1 FIRE ↑ Repeater
Or
ENG 2 FIRE Annunciator and ENG 2 FIRE ↑ Repeater
- START PWR switch (Starting Only): PUSH FOR ABORT
- HP COCK (Affected Engine): CLOSE
- LP COCK (Affected Engine): CLOSE
- ENG EXT (Affected Engine): SHOT 1
-
OIL LOW PRESSURE
Annunciators:
OIL 1 LO PRESS or OIL 2 LO PRESS
OIL PRESSURE: Check gauge reading
- If Below 25 PSI:
HP COCK (affected engine): CLOSE
-
DOUBLE ENGINE FAILURE
- ProLine 21:
ENG IGNITION 1 & 2: ON - Thrust Levers: CLOSE
- Crew Oxygen: Don mask if above 15,000 feet
- Mic Selector: OXY-MIC is above 15,000 feet
- Engine Indications: Monitor
-
INADVERTENT THRUST REVERSER DEPLOYMENT IN FLIGHT
Annunciators:
UNLCK and REVRS
HP COCK (affected engine): CLOSE
-
DEPRESSURIZATION
Horn Sounds and CABIN ALTITUDE Annunciator
- ProLine 21:
Crew Oxygen: Don Masks - Mic Selector: OXY-MIC
-
REAR EQUIPMENT BAY OVERHEAT
Annunciator:
REAR BAY OVHT
- MAIN AIR VLVs 1 & 2: CLOSE
- F/DK VLV: OPEN Fully
-
HIGH PRESSURE AIR OVERHEAT
Annunciators:
HP AIR 1 OVHT or HP AIR 2 OVHT
- MAIN AIR VLV (affected engine): CLOSE
- F/DK VLV: CLOSE
-
EMERGENCY DESCENT
- Thrust Levers: CLOSE
- Speed: MMO/VMO unless structural damage is suspected
- AIR BRAKE: OPEN
-
ELECTRICAL FIRE OR SMOKE
- ProLine 21:
Crew Oxygen: Don Masks - 100% EMERG - Mic Selector: OXY-MIC
- Smoke Goggles: Don and Vent
- Cabin Notices: ON
-
FUSELAGE FIRE OR SMOKE
Fire or smoke from cabin furnishings or equipment other than from electrical/electronic sources.
- ProLine 21:
- Crew Oxygen: Don Masks - 100% EMERG
- Mic Selector: OXY-MIC
- Smoke Goggles: Don and Vent
- Cabin Notices: ON
-
SMOKE FROM AIR CONDITIONING DUCTS
- ProLine 21:
- Crew Oxygen: Don Masks - 100% EMERG
- Mic Selector: OXY-MIC
- Smoke Goggles: Don and Vent
- Cabin Notices: ON
-
BRAKE FAILURE
Total or partial (asymmetric) failure of normal braking
- Brake Pedals: Release
- WHEEL BRAKE Lever: EMERGY
- Brake Pedals: Apply gently - Use one continuous application if possible
-
EGPWS WARNING
PULL UP MESSAGE ON PFD and/or PULL UP, or TERRAIN, TERRAIN PULL UP or OBSTACLE, OBSTACLE, PULL UP AURAL ALERT
- Go-Around button: Push
- Thrust: Take-off N1
Pitch Attitude: Increase and climb as required to avoid terrain/obstacle
-
WINDSHEAR WARNING
RED WINDSHEAR MESSAGE ON PFD and/or WINDSHEAR, WINDSHEAR, WINDSHEAR AURAL ALERT
- Go-Around button: Push
- Thrust: Take-off N1
- Pitch Attitude: Increase as required to arrest descent, allowing airspeed to decrease to intermittent stick shaker activation
-
EMERGENCY EVACUATION
- Airplane: Stop
- WHEEL BRAKE Lever: PARK
- HP COCKS: CLOSE
- LP COCKS: CLOSE
- EMERG LIGHTS (if required): MAN
- PA: Order Evacuation
- DUMP VALVE: OPEN
- BATT: OFF
-
FIRE BELL SOUNDS AND
APU PANEL - APU FIRE
with
MWS PANEL - APU FIRE
- STOP: Push momentarily
- MASTER: OFF
- FIRE Extinguisher: Lift Guard, Select ON
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